AeroElectric-Archive.digest.vol-lg

July 26, 2012 - August 27, 2012



      the biggest reason is higher octane mogas than i can get at the airport.=0A
      >>>-anyway.............i need some advice on grounding.i have a 12 volt p
      ump mounted and it is powered by a battery 20 feet away. i have a handheld 
      switch . i set the plastic can on the table and fuel is transferred thru vi
      nyl tubing. at the airplane end is a metal filter. pumps a gallon a minute.
       i plan to set up a ground to the exhaust pipe [all tanks are grounded to t
      he engine] but i do not know how to ground - the pump or hoses. any advic
      e would be appreciated.=0A>>>=0A>>Hi Bob,=0A>>=0A>>Technically, it's BONDIN
      G you're interested in... grounding isn't much important unless you've expe
      riencing lightening...=0A>>=0A>>You need some metal screen at the 'can', a 
      conductive hose (run a copper wire through it that's the best you can do) a
      nd a connection at the tank inlet on the airplane. -All those nee to be b
      onded together electrically.=0A>>=0A>>Paul=0A>>=0A>>-- =0A>>Please note my 
      new email address!=0A>>millner(at)me.com=0A>>=0A>>=0A>>=======
      =====0A>>-List" target="_blank">http://www.matronics.com/Navigato
      r?AeroElectric-List=0A>>=================
      ====================0A>>http://forums
      .matronics.com=0A>>==================
      ===================0A>>le, List Admin.
      =0A>>="_blank">http://www.matronics.com/contribution=0A>>=====
      ======== =0A>=0A>
      
________________________________________________________________________________
From: "Bill Hibbing" <n744bh(at)bellsouth.net>
Subject: Re: troubleshooting help needed
Date: Jul 26, 2012
OK, here's an update on what I've found without the engine running and using the B&C LR3C troubleshooting checklist. Step one gave me zero ohms resistance from the battery (-) to LR3C pin 7 and the same from the battery (-) to the engine case. Step two gave me a battery bus voltage of 12.64v and a pin 3 voltage of 12.62v. Step three gave me a pin 6 voltage of 12.20, well within the 0.5v tolerance. So far so good. Step four gave me a pin 4 voltage of 11.20v, well within the desired range. Step five. Here's where the fun begins. I measured the voltage at the field terminal and it was zero. Thinking that there may be a continuity problem I pulled the alternator field lead off the alternator and checked again...no voltage. I turned off the power and checked the continuity and found it was good. I also checked the alternator field resistance and it came in at 30.6 ohms. So now I think I may have some sort of a problem here so I hooked everything back up and went back to step 4 and checked pin 4 again. This time it was 1.73 volts at both pin 4 and at the alternator field terminal. The folks at B&C are at Oshkosh right now so getting hold of them might be difficult but maybe Bob can weigh in again on this one. Bill Glasair SIIS-FT ----- Original Message ----- From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> Sent: Saturday, July 21, 2012 9:25 AM Subject: RE: AeroElectric-List: troubleshooting help needed > > > At 08:33 PM 7/20/2012, you wrote: > > [Luckey] > Bob, is that correct - shouldn't Field & Bus voltage oppose each other? > i.e. as Bus voltage goes up, Field current should go down? > > It depends on what is being held constant and what > is being adjusted. > > If SYSTEM LOAD is the variable, then yes . . . the > REGULATOR senses an INCREASE in bus voltage and > reacts by REDUCING field voltage. > > In this instance, we're observing changes in > system performance while the load is constant. > If the field voltage rises in concert with the > bus voltage, then the regulator is commanding > that rise due to internal failure or mis-information > in the voltage sense path and the alternator > is performing normally. > > If the bus voltage falls while the field voltage > rises, then the regulator is flogging a crippled > alternator without success. > > > Bob . . . > > > > ----- > No virus found in this message. > Checked by AVG - www.avg.com > ________________________________________________________________________________
Date: Jul 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: troubleshooting help needed
Your original squawk: When I'm flying at cruise power, or even idling, the voltage wanders up and down from 14.4v to slightly less than 13v. It does go down enough that my Garmin Aera 796 will drop off of ships power and go to it's internal battery. This would indicate to me that this is not a problem with the voltmeter. This does not seem to have any measurable cycle. The amps stay constant at about 16 amps. When I've had the plane flying I've tried turning off equipment one at a time to see if that might have any effect...it didn't. So now I think I may have some sort of a problem here so I hooked everything back up and went back to step 4 and checked pin 4 again. This time it was 1.73 volts at both pin 4 and at the alternator field terminal. You didn't tell us where your ammeter was connected . . . in other words, what current does it measure? The fact that your bus voltage falls so low (13.0 or below) suggests the alternator is going off line completely and that the bus voltage is falling to battery delivery voltage. Your narrative also suggests that your ammeter is looking at ship's loads and not alternator output which would explain the relatively constant ammeter reading. So now I think I may have some sort of a problem here so I hooked everything back up and went back to step 4 and checked pin 4 again. This time it was 1.73 volts at both pin 4 and at the alternator field terminal. This is consistent with an intermittent disconnect of alternator field supply which. If the voltage at pin 4 ever drops so low while pin 6 and 3 are at battery voltage points to failure within the regulator. Suggest you arrange to return it to B&C for inspection/repair. Bob . . . ________________________________________________________________________________
From: "Bill Hibbing" <n744bh(at)bellsouth.net>
Subject: Re: troubleshooting help needed
Date: Jul 27, 2012
Thanks Bob, That's about what I was thinking also. I was hoping that I would find the alternator was the problem as it's a heck of a lot easier to change. Another question for you...I currently have the LR3C mounted on the cabin side of the firewall. Do you see any problem with relocating it to the engine side of the firewall? As long as I have to take it out, a real PITA, I thought I might change the location to a location that is easier to work on it in the case of another failure. Thanks, Bill So now I think I may have some sort of a problem here so I hooked everything back up and went back to step 4 and checked pin 4 again. This time it was 1.73 volts at both pin 4 and at the alternator field terminal. This is consistent with an intermittent disconnect of alternator field supply which. If the voltage at pin 4 ever drops so low while pin 6 and 3 are at battery voltage points to failure within the regulator. Suggest you arrange to return it to B&C for inspection/repair. Bob . . . No virus found in this message. Checked by AVG - www.avg.com 07/27/12 ________________________________________________________________________________
Date: Jul 27, 2012
From: Charlie England <ceengland7(at)gmail.com>
Subject: Re: troubleshooting help needed
On 07/27/2012 11:10 AM, Robert L. Nuckolls, III wrote: > Your original squawk: > > When I'm flying at cruise power, or even idling, the voltage wanders > up and down > from 14.4v to slightly less than 13v. It does go down enough that my > Garmin > Aera 796 will drop off of ships power and go to it's internal > battery. This would > indicate to me that this is not a problem with the voltmeter. This > does not seem > to have any measurable cycle. The amps stay constant at about 16 amps. > When I've had the plane flying I've tried turning off equipment one at > a time to > see if that might have any effect...it didn't. > > So now I think I may have some sort of a problem > here so I hooked everything back up and went back > to step 4 and checked pin 4 again. This time it > was 1.73 volts at both pin 4 and at the alternator > field terminal. > > You didn't tell us where your ammeter was connected . . . > in other words, what current does it measure? > > The fact that your bus voltage falls so low (13.0 or below) > suggests the alternator is going off line completely and that > the bus voltage is falling to battery delivery voltage. > > Your narrative also suggests that your ammeter is looking at > ship's loads and not alternator output which would explain > the relatively constant ammeter reading. > > > So now I think I may have some sort of a problem > here so I hooked everything back up and went back > to step 4 and checked pin 4 again. This time it > was 1.73 volts at both pin 4 and at the alternator > field terminal. > > This is consistent with an intermittent disconnect of > alternator field supply which. If the voltage at pin 4 > ever drops so low while pin 6 and 3 are at battery > voltage points to failure within the regulator. Suggest > you arrange to return it to B&C for inspection/repair. > > Bob . . . > Since the field voltage at the alt wasn't there, & came back after the disconnect/reconnect, it might be worthwhile to disconnect it again & do a resistance check while wiggling the wire & terminations, prior to returning the regulator. Charlie ________________________________________________________________________________
Date: Jul 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: troubleshooting help needed
At 11:45 AM 7/27/2012, you wrote: >Thanks Bob, > >That's about what I was thinking also. I was hoping that I would >find the alternator was the problem as it's a heck of a lot easier >to change. Another question for you...I currently have the LR3C >mounted on the cabin side of the firewall. Do you see any problem >with relocating it to the engine side of the firewall? As long as I >have to take it out, a real PITA, I thought I might change the >location to a location that is easier to work on it in the case of >another failure. Thanks, Many of them are located on the engine side of the fire wall and seem to do just fine. We designed that critter 25 years ago and I never did an on-purpose thermal study. I should probably get one from Bill and put it in the chamber to see what the real ambient limits are. Actually, temperatures on the fire wall while in flight are quite benign. That's another real data gathering exercise that would be useful to conduct. All it takes is time and $ . . . but you're okay if you move it. Bob . . . ________________________________________________________________________________
Date: Jul 27, 2012
From: Jay Pearlman <jay.pearlman(at)yahoo.com>
Subject: LED installations
________________________________ Bob, For the B&C wig-wag, I see a modification on the B&C site putting a resistor in parallel. I was told you are working on an alternative solution for using LEDs. Is there something in the works? ________________________________________________________________________________
Date: Jul 28, 2012
Subject: Z-13/8 in a Long-EZ
From: jeffk <jkember(at)gmail.com>
Just wanted to introduce myself to the group. I purchased a flying Long-EZ and wish to upgrade the panel and rewire aircraft. I purchased the Aeroelectric Connection a number of years ago and wish to thank Bob for all of his work and for providing an electronic version as well (nice to not have to carry about the printed version). My current plan is to go with Z-13/8. I have an automotive alternator (one year old), will be removing the vacuum system and replacing it with a SD-8 and am going with ATC fuses. A box of bits arrived from B and C and I'm sure it won't be the last order. I'm researching alternators, feed wires to such, battery and starter contactors, regulators and where to position all of this. I'm also researching internal vs external regulation on my main alternator. I've been enjoying reading through the archives and wanted to thank everyone for their contributions to the list. Jeff - Long-EZ based in Livermore California ________________________________________________________________________________
Date: Jul 28, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Z-13/8 in a Long-EZ
> >I've been enjoying reading through the archives and wanted to thank >everyone for their contributions to the list. Welcome to the family Jeff! I think you'll be pleased with the level of assistance and encouragement you will receive from members of the List. It's among the busiest Lists on Matronics populated by folks interested in the best-we-know-how-to-do and love airplanes! Keep us apprised of your progress and questions. Bob . . . ________________________________________________________________________________
Subject: Modifying 12V LED Strip Lighting to work in 24/28V
Aircraft
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Jul 28, 2012
LED Strip lighting is usually made for 12V systems. To convert this for 24/28 volt systems see the attached pdf. This is far better than using a stepdown supply or adding a load resistor. -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379414#379414 Attachments: http://forums.matronics.com//files/modify_led_strip_lighting_for_24_28_volts_196.pdf ________________________________________________________________________________
Subject: Re: Modifying 12V LED Strip Lighting to work in 24/28V
Aircraft
From: Etienne Phillips <etienne.phillips(at)gmail.com>
Date: Jul 29, 2012
Strangely enough, I did exactly this at work on Thursday. One thing to remember is that the number of LED's in each of the strips must be the same or the one with less LEDs in it will be brighter, or even blow. Etienne On 28 Jul 2012, at 7:31 PM, Eric M. Jones wrote: > > LED Strip lighting is usually made for 12V systems. To convert this for 24/28 volt systems see the attached pdf. > > This is far better than using a stepdown supply or adding a load resistor. > > -------- > Eric M. Jones > www.PerihelionDesign.com > 113 Brentwood Drive > Southbridge, MA 01550 > (508) 764-2072 > emjones(at)charter.net > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=379414#379414 > > > > > Attachments: > > http://forums.matronics.com//files/modify_led_strip_lighting_for_24_28_volts_196.pdf > > > > > > > ________________________________________________________________________________
Subject: Re: Modifying 12V LED Strip Lighting to work in 24/28V
Aircraft
From: dfritzj <dfritzj(at)yahoo.com>
Date: Jul 29, 2012
This raises a good question: is it okay to light a strip of LEDs by just wiring them in series in a quantity such that each LED sees the appropriate voltage drop? This would seem to eliminate the (admittedly small) energy loss from heating up resistors. On the other hand, failure of one LED would darken the whole string. Thoughts? Dan ________________________________________________________________________________
Date: Jul 29, 2012
Subject: gps
From: bob noffs <icubob(at)gmail.com>
hi all, last week i started looking around for a garmin pilot 3 as a backup. plenty of street pilots available. can an aviation database be downloaded to the street pilot? thanks, bob noffs ________________________________________________________________________________
From: jan <jan(at)CLAVER.DEMON.CO.UK>
Subject: gps
Date: Jul 29, 2012
My understanding is that you can NOT do that .. you need the aircraft version. Did you try on the VAF web site ? You can post a "want to buy" ... Jan _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of bob noffs Sent: 29 July 2012 12:41 Subject: AeroElectric-List: gps hi all, last week i started looking around for a garmin pilot 3 as a backup. plenty of street pilots available. can an aviation database be downloaded to the street pilot? thanks, bob noffs <http://www.matronics.com/Navigator?AeroElectric-List> <http://www.matronics.com/contribution> http://www.w3.org/TR/REC-html40">

My understanding is that you can NOT do that .. you need the aircraft version.

 

Did you try on the VAF web site ?  You can post a “want to buy” …

 

Jan

 


From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of bob noffs
Sent: 29 July 2012 12:41
To: aeroelectric list
Subject: AeroElectric-List: gps

 

hi all, last week i started looking around for a garmin pilot 3 as a backup. plenty of street pilots available. can an aviation database be downloaded to the street pilot?

 thanks, bob noffs

 
 
http://www
      .matronics.com/Navigator?AeroElectric-List
      
http://forums.matronics.com
http://www.matronics.com/
      contribution
 

      
      
      
________________________________________________________________________________
Date: Jul 29, 2012
Subject: Re: gps
From: bob noffs <icubob(at)gmail.com>
jan, i went to the site and how to it didn't just jump out and bite me so i gave it up. i guess i will try that again. bob noffs On Sun, Jul 29, 2012 at 9:34 AM, jan wrote: > My understanding is that you can NOT do that .. you need the aircraft > version.**** > > ** ** > > Did you try on the VAF web site ? You can post a =93want to buy=94 =85** ** > > ** ** > > Jan**** > > ** ** > ------------------------------ > > *From:* owner-aeroelectric-list-server(at)matronics.com [mailto: > owner-aeroelectric-list-server(at)matronics.com] *On Behalf Of *bob noffs > *Sent:* 29 July 2012 12:41 > *To:* aeroelectric list > *Subject:* AeroElectric-List: gps**** > > ** ** > > hi all, last week i started looking around for a garmin pilot 3 as a > backup. plenty of street pilots available. can an aviation database be > downloaded to the street pilot?**** > > thanks, bob noffs**** > > * * > > * * > > ** > > ** > > ** > > ** > > ** > > ** > > ** > > *http://www.matronics.com/Navigator?AeroElectric-List* > > ** > > ** > > ** > > ** > > ** > > *http://forums.matronics.com* > > ** > > ** > > ** > > ** > > ** > > *http://www.matronics.com/contribution* > > ** > > * * > > * > =========== =========== =========== =========== > * > > ________________________________________________________________________________
Date: Jul 29, 2012
Subject: Re: Modifying 12V LED Strip Lighting to work in 24/28V
Aircraft
From: Bill <wtrooper(at)gmail.com>
On Sat, Jul 28, 2012 at 11:35 PM, you wrote ---------------snip-------------- > One thing to remember is that the number of LED's in each of the strips must be the same -----------snip----------- Not to worry, Eric noted this on his pdf below. Bill SF bay area > > Attachments: > > > > > http://forums.matronics.com//files/modify_led_strip_lighting_for_24_28_volts_196.pdf > > ________________________________________________________________________________
Subject: Re: Z-13/8 in a Long-EZ
From: "jdubner" <jdubner(at)yahoo.com>
Date: Jul 29, 2012
Jeff, I also fly an Long-EZ, also with an automotive alternator and ATC fuses. I mounted two fuse blocks back-to-back to a bulkhead and just above the nosewheel cover. Attached is a picture of the battery-bus side of the fuseblocks. (Note: some of the fuses visible are just spares.) The fuses are accessible through the nose access hatch. My alternator is an internally-regulated Hitachi (from a 1979 Datsun pickup) and suffers no ill effects when I disconnect it from the bus with a contactor. $50 at rockauto.com! Email me if I can help you with any electrical or wiring issues. -- Joe Independence, OR www.mail2600.com/cgi-bin/webcam.cgi Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379495#379495 Attachments: http://forums.matronics.com//files/battery_bus_fuse_block_971.jpg ________________________________________________________________________________
From: "Jeff Luckey" <JLuckey(at)pacbell.net>
Subject: Modifying 12V LED Strip Lighting to work in 24/28V
Aircraft
Date: Jul 29, 2012
Are the LEDs shown in that PDF drawn w/ the correct polarity?? _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Bill Sent: Sunday, July 29, 2012 08:35 Subject: Re: AeroElectric-List: Modifying 12V LED Strip Lighting to work in 24/28V Aircraft On Sat, Jul 28, 2012 at 11:35 PM, you wrote ---------------snip-------------- > One thing to remember is that the number of LED's in each of the strips must be the same -----------snip----------- Not to worry, Eric noted this on his pdf below. Bill SF bay area > Attachments: > > http://forums.matronics.com//files/modify_led_strip_lighting_for_24_28_volts _196.pdf <http://forums.matronics.com/files/modify_led_strip_lighting_for_24_28_volts _196.pdf> > No virus found in this message. Checked by AVG - www.avg.com ________________________________________________________________________________
Date: Jul 29, 2012
From: Henador Titzoff <henador_titzoff(at)yahoo.com>
Subject: Modifying 12V LED Strip Lighting to work in 24/28V
Aircraft Good catch, Jeff. -I guess you were Luckey, huh? -Good job! Henador Titzoff --- On Sun, 7/29/12, Jeff Luckey wrote: From: Jeff Luckey <JLuckey(at)pacbell.net> Subject: RE: AeroElectric-List: Modifying 12V LED Strip Lighting to work in 24/28V Aircraft Date: Sunday, July 29, 2012, 11:36 AM =0A=0A=0A =0A =0A=0A =0A=0A=0A=0A=0A=0A=0A=0A=0A=0A=0A=0AAre the LEDs shown in that PDF drawn w/=0Athe correct polarity?? =0A=0A - =0A=0A=0A=0A=0A =0A=0A=0A=0A=0AFrom:=0Aowner-aeroelectric-list-server(at)matronics.com=0A[mail to:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Bill =0ASent: Sunday, July 29, 2012 08:35 =0ATo: aeroelectric-list(at)matronics.com =0ASubject: Re: AeroElectric-List:=0AModifying 12V LED Strip Lighting to wo rk in 24/28V Aircraft =0A=0A=0A=0A - =0A=0A - =0A=0A=0A=0AOn Sat, Jul 2 8, 2012 at 11:35 PM, you wrote =0A=0A=0A=0A - =0A=0A=0A=0A=0A=0A--------- ------snip--------------- =0A=0A=0A=0A=0A=0A> One thing to remember is th at the number of LED's in each of the=0Astrips must be the same =0A=0A=0A =0A=0A=0A-----------snip------------ =0A=0A=0A=0A=0A=0A - =0A=0A=0A=0A =0A=0ANot to worry, Eric noted this on his pdf below. =0A=0A=0A=0A=0A=0A - =0A=0A=0A=0A=0A=0ABill =0A=0A=0A=0A=0A=0ASF bay area =0A=0A=0A=0A=0A=0A - =0A=0A=0A=0A=0A=0A> Attachments: =0A> =0A> http://forums.matronics.com//files/modify_led_strip_lighting_for_24_28 _volts_196.pdf =0A> =0A=0A=0A=0A=0A=0A - -http://www.matronics.com/Navigator?AeroElect ric-Listhttp://forums.matronics.comhttp://www.matronics.com/contribution - =0A=0A=0A=0ANo virus found in this message. =0AChecked by AVG - www.avg.com =====0A=0A ________________________________________________________________________________
From: "Jeff Luckey" <JLuckey(at)pacbell.net>
Subject: Modifying 12V LED Strip Lighting to work in 24/28V
Aircraft
Date: Jul 29, 2012
What's that old saying? It's better to be good than lucky. However, in my case, I'm always Luckey ;) _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Henador Titzoff Sent: Sunday, July 29, 2012 12:47 Subject: RE: AeroElectric-List: Modifying 12V LED Strip Lighting to work in 24/28V Aircraft Good catch, Jeff. I guess you were Luckey, huh? Good job! Henador Titzoff --- On Sun, 7/29/12, Jeff Luckey wrote: From: Jeff Luckey <JLuckey(at)pacbell.net> Subject: RE: AeroElectric-List: Modifying 12V LED Strip Lighting to work in 24/28V Aircraft Date: Sunday, July 29, 2012, 11:36 AM Are the LEDs shown in that PDF drawn w/ the correct polarity?? _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Bill Sent: Sunday, July 29, 2012 08:35 Subject: Re: AeroElectric-List: Modifying 12V LED Strip Lighting to work in 24/28V Aircraft On Sat, Jul 28, 2012 at 11:35 PM, you wrote ---------------snip-------------- > One thing to remember is that the number of LED's in each of the strips must be the same -----------snip----------- Not to worry, Eric noted this on his pdf below. Bill SF bay area > Attachments: > > http://forums.matronics.com//files/modify_led_strip_lighting_for_24_28_volts _196.pdf <http://forums.matronics.com/files/modify_led_strip_lighting_for_24_28_volts _196.pdf> > http://www.matronics.com/Navigator?AeroElectric-List http://forums.matronics.com http://www.matronics.com/contribution No virus found in this message. Checked by AVG - www.avg.com 07/28/12 ________________________________________________________________________________
Subject: Re: Modifying 12V LED Strip Lighting to work in 24/28V
Aircraf
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Jul 30, 2012
Wrong polarity...Rookie mistake see attached correction.... -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379571#379571 Attachments: http://forums.matronics.com//files/modify_led_strip_lighting_for_24_28_volts_reva_199.pdf ________________________________________________________________________________
Subject: Using LEDs in Series
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Jul 30, 2012
> This raises a good question: is it okay to light a strip of LEDs by just wiring them in series in a quantity such that each LED sees the appropriate voltage drop? This would seem to eliminate the (admittedly small) energy loss from heating up resistors. On the other hand, failure of one LED would darken the whole string. Thoughts?Dan Great questionand one that needs a proper answer. LEDs have a characteristic called Forward Voltage (or Vf). This means that the LED will not light until the voltage across it exceeds the Vf. This voltage is usually small , perhaps 2Vf and depends on the diodes materials of construction. The diode itself follows Ohms Law V=IR (or E=IR) when the voltage is above the Vf. Lets see how this works: Put a common LED across a 12V source, and the current will be extremely large, since 12V/~0 Ohms=Huge current. Now we have to understand that the battery or source of power and the wires, etc. have some small resistance, so the current is not quite infinite, but some very large value. (Ka-blam.) But the LED lowers the voltage by its forward voltage (here 2 Vf). Even so 12V-2 Vf =10V and 10V/~0 Ohms is still huge. So we have the bright idea that we can simply use 6 x 2 Vf LEDs, we can get: 12V-2Vf -2Vf -2 Vf -2Vf -2 Vf -2Vf = 0 volts/~0=hmmmmm. The LEDs in this case are each at the voltage where they can almost light. But this is no good for anybody. If we use 5 x 2V LEDs, then 12V-2V-2V-2V-2V-2V= 2V/~0=Current (probably excessive) that is dependent only upon the residual resistance and true source voltage of the circuit. Furthermore it depends on the LEDs Vf being exact and independent of all outside influenceswhich it is most certainly not. Additionally if you build a circuit where the LEDs are on the hairy edge of lighting, dimming them is problematic. What to do, what to do? Add a resistor to the string of LEDs If we use 5 x 2Vf, and want a current of 30 mA, then 12V-2Vf -2Vf -2Vf -2Vf-2Vf =2V/.030A=67 Ohms. This 67 Ohm resistor swamps any likely source resistance (which is usually just a few Ohms), and doesnt allow for much slump in the voltage source (10V and these LEDs are off) The resistor needs to be a wattage of at least I^2 X R=0.030A X 0.030A X 67 Ohms=0.06 Wattsvery small in this case but the wattage calculation of LED current-limiting resistors is important and frequently neglected. Additional note: The voltage source can be as large as one likeseven kilovoltsbut the resistor must be suitable for the voltage. Additional note: Vf is not a parallel-is-lower type of characteristic. Vf values sum in series, but do not sum in parallel, exactly like batteries! This makes putting banks of LEDs in series and parallel together a practical approach. Conclusion: When using LEDs in a string, the current limiting resistor must have a high enough value to make ignoring the source resistance reasonable, and allow for dimming capability headroom as desired. Eric M. Jones, Perihelion Design, 07/30/12 -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379593#379593 ________________________________________________________________________________
Date: Jul 30, 2012
Subject: Re: Using LEDs in Series
From: Christopher Cee Stone <rv8iator(at)gmail.com>
> > LEDs in series is not as potentially problematic as incandescents in > series. Incandescent bulbs are relatively delicate and short lived as they > are a heater that emits light. The life of an LED that is driven at it's > rated current (not over driven) and properly heat sinked (in the case of > high brightness LEDs >1W) is tens of thousands of hours. In the developing > industry of SSL (solid state lighting) it is common practice to series > connect LEDs. In most cases this is preferred as the current is held > constant and the voltage is varied depending on the number of LEDs in the > string (as Eric has described). If you are driving high output devices >1W > you will need to use a constant current driver. You will find that as you > limit current on these higher output devices a limiting resistor will > dissipate considerable power, much more than the LED. > Chris Stone RV-8 Newberg, OR > > > This raises a good question: is it okay to light a strip of LEDs by just > wiring them in series in a quantity such that each LED sees the appropriate > voltage drop? This would seem to eliminate the (admittedly small) energy > loss from heating up resistors. On the other hand, failure of one LED would > darken the whole string. Thoughts?Dan > > > ________________________________________________________________________________
Subject: Re: Using LEDs in Series
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Jul 30, 2012
One last thing: In many cases a simple current-regulated power supply is all you need to drive series/parallel LEDs. This also has the advantage of being essentially noise free. I sell an LED tail light where I used a tiny switching power supply but never could stop the noise (Bob N. has a solution to this...but it is a little complicated) The problem was particularly bad because the LED is in the tail...and frequently so are the antennas. So I changed to a simple current-regulated supply that is a little inefficient, but stone-silent. I have no doubt that there are switching supplies that are very quiet, too. -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379610#379610 ________________________________________________________________________________
Date: Jul 30, 2012
From: Jerome Sipple <jds(at)taxesplusllc.com>
Subject: HUD for GA aircraft
Just a fyi about an interesting blurb I saw in a gizmag email today about a new heads up display for GA aircraft. I have no connection with them, just passing along the info. PAT Avionics shows G-HULP heads-up-display system for recreational aircraft http://www.gizmag.com/pat-avionics-hud-recreational-aircraft/23477/?utm_source=Gizmag+Subscribers&utm_campaign=a4a140692e-UA-2235360-4&utm_medium=email Jerry Sipple Cozy MkIV project ________________________________________________________________________________
Date: Jul 30, 2012
From: Henador Titzoff <henador_titzoff(at)yahoo.com>
Subject: Re: Using LEDs in Series
Eric, a "simple current regulated power supply is nothing more than an acti ve circuit providing variable resistance to keep the current constant while the applied voltage fluctuates. -This means that power is dissipated in its "variable resistance circuit, usually a transistor in its active state. A switched current regulator, on the other hand, keeps the switching transi stors in their on-off states with power dissipated mostly during the switch ing time when they're in the active state. -This has the disadvantage of generating transients and harmonics which may bleed into the wrong places. Do you have a magical circuit that somehow doesn't generate RF interference and also doesn't dissipate very much power? Thanks. Henador Titzoff --- On Mon, 7/30/12, Eric M. Jones wrote: From: Eric M. Jones <emjones(at)charter.net> Subject: AeroElectric-List: Re: Using LEDs in Series Date: Monday, July 30, 2012, 11:06 AM et> One last thing: In many cases a simple current-regulated power supply is all you need to dr ive series/parallel LEDs. This also has the advantage of being essentially noise free. I sell an LED tail light where I used a tiny switching power su pply but never could stop the noise (Bob N. has a solution to this...but it is a little complicated) The problem was particularly bad because the LED is in the tail...and frequently so are the antennas. So I changed to a simp le current-regulated supply that is a little inefficient, but stone-silent. I have no doubt that there are switching supplies that are very quiet, too. -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379610#379610 le, List Admin. ________________________________________________________________________________
Date: Jul 30, 2012
Subject: book
From: Gordon Parker <gptailwind(at)gmail.com>
Bob: Thanks for all the good info that comes thru. I would like to purchase your book but cannot locate how to do it. Could you help thanks. Gordon ________________________________________________________________________________
Subject: Re: Using LEDs in Series
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Jul 30, 2012
> Do you have a magical circuit that somehow doesn't generate RF interference and also doesn't dissipate very much power? Thanks. Henador Titzoff If I did, I wouldn't be posting here. I'd have my jet parked on my private Caribbean Island. But I'd invite everybody over for a Margarita. Seriously, there are two kinds of power supplies...Digital and Analog. ALL the digital stuff makes noise, ALL the analog stuff dissipates power. Is there some magical in-between*? Probably not, but the digital stuff can be made arbitrarily close to noise-free with really good design. This usually involves knowing what frequency spectrum you can use for switching...something that won't interfere. (*Filters are almost all analog...but here I mean the active regulation element) -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379626#379626 ________________________________________________________________________________
Date: Jul 30, 2012
From: Peter Pengilly <peter(at)sportingaero.com>
Subject: Re: HUD for GA aircraft
The big deal about HUDs is that they are focused at infinity with some fancy (heavy) optics. That way you look out the window and everything is in focus, data/target/bad guys laid on top of the scenery. This looks like a see through LCD (or similar), focussed on the plate. I'm not sure that would of huge benefit as you would be continually be re-focussing between the plate and the scenery. So $5000 for something that is only of real use when attacking those pesky ground targets, and then requiring a lot of focus shifting. It would be interesting to know what kind of lag there is between the world moving and the depiction on the glass responding - if it is more that 100ms (that is 0.1 seconds) then it is too slow to be of much use and will only be a hindrance. Thanks for posting. Peter On 30/07/2012 19:45, Jerome Sipple wrote: > Just a fyi about an interesting blurb I saw in a gizmag email today > about a new heads up display for GA aircraft. I have no connection > with them, just passing along the info. > > PAT Avionics shows G-HULP heads-up-display system for recreational > aircraft > > http://www.gizmag.com/pat-avionics-hud-recreational-aircraft/23477/?utm_source=Gizmag+Subscribers&utm_campaign=a4a140692e-UA-2235360-4&utm_medium=email > > Jerry Sipple > Cozy MkIV project > > > * > > > * ________________________________________________________________________________
Date: Jul 30, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: book
At 03:24 PM 7/30/2012, you wrote: >Bob: Thanks for all the good info that comes thru. I would like to >purchase your book but cannot locate how to do it. Could you >help thanks. Gordon My website at http://tinyurl.com/89kaepk . . . has an expanded information set that augments the book. There's also an catalog/ order page at: http://tinyurl.com/36e7ddd where you can enter an order for the book. Thanks for asking. Bob . . . ________________________________________________________________________________
Subject: Re: Latching Relay Redux
From: "user9253" <fran4sew(at)banyanol.com>
Date: Jul 30, 2012
I received this email today from Chuck (quoted below) in reference to my circuit "Contactor PWM.pdf " to reduce contactor holding current. http://forums.matronics.com/download.php?id=32370 > Hello Joe > I built the circuit with one change. I replaced R1 with an adjustable 0-25k ohm pot. Works great, just dial in the PWM for the right duty cycle with R1 for the particular contactor being used. > Thanks Chuck -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379655#379655 ________________________________________________________________________________
Date: Jul 30, 2012
From: Henador Titzoff <henador_titzoff(at)yahoo.com>
Subject: Re: Using LEDs in Series
Therein lies another problem, Eric. For a switching regulator (digital) tha t is "noise free with really good design," you say that it involves knowing what frequency spectrum you can use for switching ... something that won't interfere. -As diverse as our airplanes are, with several systems and wi th ubiquitous installation techniques and paths, how does one design a nois e free switching regulator? -The only way I can think of is to design it with passive filtering and packaging methods such that radiated and conduct ed EMI is reduced to something extremely low. This would also involve exten sive testing to verify the low EMI. That kind of design and testing would c ost a pretty peso. Seems to me the safest way to go is an active linear regulator with a suffi cient back plate to dissipate the heat. Henador Titzoff --- On Mon, 7/30/12, Eric M. Jones wrote: From: Eric M. Jones <emjones(at)charter.net> Subject: AeroElectric-List: Re: Using LEDs in Series Date: Monday, July 30, 2012, 1:42 PM et> > Do you have a magical circuit that somehow doesn't generate RF interferen ce and also doesn't dissipate very much power? Thanks. Henador Titzoff If I did, I wouldn't be posting here. I'd have my jet parked on my private Caribbean Island. But I'd invite everybody over for a Margarita. Seriously, there are two kinds of power supplies...Digital and Analog. ALL the digital stuff makes noise, ALL the analog stuff dissipates power. Is th ere some magical in-between*? Probably not, but the digital stuff can be ma de arbitrarily close to noise-free with really good design. This usually in volves knowing what frequency spectrum you can use for switching...somethin g that won't interfere. (*Filters are almost all analog...but here I mean the active regulation ele ment) -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379626#379626 le, List Admin. ________________________________________________________________________________
Subject: What guage wire for alternator to bus bar
From: "kmiller" <kandd.miller(at)hetnet.nl>
Date: Jul 31, 2012
sorry ( i am a newbie to this forum ) if this is already answered else where, but i would like to know the minimum gauge wire i should use for a 60amp alternator (15V) to the Bus bar which is 5ft away. In normal operation max current draw in flight would be 12 amps ( landing lights , nav lights, radio, transponder, solenoids) In addition, (and this may seem like a silly idea), but I actually want to limit the maximum current that could go into my lithium Ion Phosphate battery immediately after start up to say 10 amps, how would I go about this ? Currently it is drawing max amps out of the alternator for the rotation speed (1200 rpm) for a few minutes, and I think this was the reason for my alternator drive coupling slipping. Keith -------- KIS owner Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379681#379681 ________________________________________________________________________________
Subject: Re: Using LEDs in Series
From: dfritzj <dfritzj(at)yahoo.com>
Date: Jul 31, 2012
Thanks for the in-depth answer, Eric. It sounds like I should stick to a more classic approach. I didn't like the idea of a whole set of lights going out for one failure anyway (too many bad Christmas-tree memories...) Dan ________________________________________________________________________________
Date: Aug 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Latching Relay Redux
At 09:07 PM 7/30/2012, you wrote: > >I received this email today from Chuck (quoted below) in reference >to my circuit "Contactor PWM.pdf " to reduce contactor holding current. >http://forums.matronics.com/download.php?id=32370 > > > Hello Joe > > I built the circuit with one change. I replaced R1 with an > adjustable 0-25k ohm pot. Works great, just dial in the PWM for the > right duty cycle with R1 for the particular contactor being used. > > Thanks Chuck I recommend that the power saving duty cycle be set for not less than 50%. This cuts average voltage to contactor by 50% . . . hence average current by 50% and total power dissipated by 75%. While a 12v contactor will stay energized at voltages of 2v or below, you want to make sure that the contactor stays closed down to battery end of life at 10.5 volts or so. 50% at 14 volts with alternator running gives you 7 volts to hold the contactor . . . 10.5 translates to 5.25 volts or thereabouts . . . probably as low as you want to go. 75% reduction in lost energy is pretty substantial if you're in a battery-only operational mode . . . or struggling to make the most of an 8A alternator. Bob . . . Bob . . . ________________________________________________________________________________
Date: Aug 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Using LEDs in Series
At 09:58 PM 7/30/2012, you wrote: >Therein lies another problem, Eric. For a switching regulator >(digital) that is "noise free with really good design," you say that >it involves knowing what frequency spectrum you can use for >switching ... something that won't interfere. Switching regulators are ubiquitous and definitely here to stay. ALL of the accessories that trumpet 10-30 volt supply inputs are fitted with such power supplies. Operating frequency for such supplies is never 'selected' to be compatible with the operating environment. It's selected as a trade-off for for the components selected to achieve maximum efficiency at rated load. After design goals for efficiency are achieved, then careful board layout for controlling aperture area (radiation concerns) and good management of RF grounds (conduction concerns) and dv/dt limiting (both concerns) will minimize any necessary filtering and shielding to meet DO-160 emissions limits. Anyone who has done this exercise a couple of times will never again be surprised in the lab with failure of a new design to meet emissions limits. It's like learning to bake cakes. After my first few passes through the vibration immunity testing, I never again shook a component of a board . . . it's that 'learning curve' thingy. The filter I crafted for the BuckPucks was a brute force endeavor to fix a problem in systems that were already under construction and parts were on hand. The filter may be more than was really necessary . . . but it proved to be adequate to the task. A detailed study in the RFI lab might show that a simpler filter would do . . . but given the small volume of sales for this particular LED drive solution, it hardly justifies the expense of a finely tuned development effort. The BuckPuck was never intended for use in an aircraft EMC environment else it would not have been built that way. Some of the HID lamp supplies I've played with are similarly burdened with EMC issues for aircraft. That doesn't mean that any of these devices were "poorly designed", it only means that the customer base for thousands of units don't care that the device going into their boat, motorcycle or hot-rod is unsuited to airplanes. In the OBAM aviation world, we are a primo filter for searching out and identifying the best that folks know how to do. But it's a fine demonstration of the need for caveat emptor . . . give it a try in low risk experiments and report findings to the group. If a short-fall in performance is noted, then try something else . . . or modify the product (such as the filter board for the BuckPucks). In any case, the ultimate goodness of the device and the system in fits is up to us and NOT the designer of the device who probably never envisioned his work product going into an airplane . . . and would probably rather that it did not. It used to be that a phone call to Gates about v-belts had to be made in 'disguise' . . . if you mentioned that you were working on an airplane, the standard vociferous response was "our products are not intended for use on aircraft" . . . i.e. "you're on your own my friend". Bob . . . ________________________________________________________________________________
Date: Aug 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: What guage wire for alternator to bus bar
At 07:04 AM 7/31/2012, you wrote: sorry ( i am a newbie to this forum ) if this is already answered else where, but i would like to know the minimum gauge wire i should use for a 60amp alternator (15V) to the Bus bar which is 5ft away. In normal operation max current draw in flight would be 12 amps ( landing lights , nav lights, radio, transponder, solenoids) 6AWG would be good, 4AWG welding cable is readily available, inexpensive and would be better. In addition, (and this may seem like a silly idea), but I actually want to limit the maximum current that could go into my lithium Ion Phosphate battery immediately after start up to say 10 amps, how would I go about this ? Currently it is drawing max amps out of the alternator for the rotation speed (1200 rpm) for a few minutes, and I think this was the reason for my alternator drive coupling slipping. We need more information here. Your alternator drive system should be designed to function at the alternator's rated output. In other words, if it slips under some conditions of loading, then the answer is to fix the drive system, not reduce the load. Where does the 1200 rpm number come from . . . prop RPM? What's the alternator RPM at this time? Bob . . . ________________________________________________________________________________
Date: Aug 01, 2012
From: Ken <klehman(at)albedo.net>
Subject: Re: Latching Relay Redux
Is that 75% power reduction correct?? I would have guessed that a 50% duty cycle gave full voltage and full current for 50% of the time in a pulsed resistance circuit resulting in a 50% power reduction. Not sure about an inductive coil contactor though. Just asking but intuitively I would not have averaged the voltage and applied the I squared power calculation to this. Ken On 01/08/2012 9:02 AM, Robert L. Nuckolls, III wrote: > > > At 09:07 PM 7/30/2012, you wrote: >> >> >> I received this email today from Chuck (quoted below) in reference to >> my circuit "Contactor PWM.pdf " to reduce contactor holding current. >> http://forums.matronics.com/download.php?id=32370 >> >> > Hello Joe >> > I built the circuit with one change. I replaced R1 with an >> adjustable 0-25k ohm pot. Works great, just dial in the PWM for the >> right duty cycle with R1 for the particular contactor being used. >> > Thanks Chuck > > I recommend that the power saving duty cycle > be set for not less than 50%. This cuts average > voltage to contactor by 50% . . . hence average > current by 50% and total power dissipated by > 75%. > > While a 12v contactor will stay energized at > voltages of 2v or below, you want to make sure > that the contactor stays closed down to battery > end of life at 10.5 volts or so. 50% at 14 volts > with alternator running gives you 7 volts to hold > the contactor . . . 10.5 translates to 5.25 volts > or thereabouts . . . probably as low as you want > to go. 75% reduction in lost energy is pretty > substantial if you're in a battery-only operational > mode . . . or struggling to make the most of an > 8A alternator. > > Bob . . . > > ________________________________________________________________________________
Date: Aug 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Latching Relay Redux
At 10:20 AM 8/1/2012, you wrote: Is that 75% power reduction correct?? I would have guessed that a 50% duty cycle gave full voltage and full current for 50% of the time in a pulsed resistance circuit resulting in a 50% power reduction. Not sure about an inductive coil contactor though. Just asking but intuitively I would not have averaged the voltage and applied the I squared power calculation to this. ----------- Excellent question . . . and yes, consideration of contactor inductance paralleled with a diode is critical to the analysis. When to the bench and set this up: Emacs! This test setup produced the following data: Emacs! If I go to 100% duty cycle, this El Cheeso, Stancore/RBM contactor draws 0.9 amps 14.6 volts. Dynamically, the coil current (Yellow trace) shows some ripple at the switching frequency but averages just under 0.5 Amp. In the mean time, the power supply is showing a load of just 0.21 amps or about 25% of the full-on current draw. If I put a 15 ohm resistor in place of the\ contactor, the 100% current goes to the expected 1 amp. At 50% duty cycle, the peak current is still 1 amp with average current falling to the predicted 0.5A . . . hence 50% duty cycle produces only 50% reduction in power in the resistive circuit. The L/R time constant of the inductive circuit prevents achievement of full current during limited on-time. The diode prevents current from falling to zero during off-time. After one hour, the outside temperature of the contactor was not too hot to sustained touch . . . Waayyy cooler than contactor operatied at 100%. Bob . . . ________________________________________________________________________________
Date: Aug 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Using LEDs in Series
I have been experimenting with a product available off eBay that offers 300, .05 x .05 LED's mounted to a 3/8" wide x 16 foot flexible etched circuit strip. http://tinyurl.com/c33w25o The leds are wired in paralleled series-clusters of 3 devices and a 150 ohm resistor. Here's a 2-cluster segment of this product . . . Emacs! You can cut the strip every three devices and attach new power leads at the solder pads visible in the photo. I'm going to be using about 80 feet of this product in my kitchen to put double rows of ceiling accent lighting high up, double rows to replace recessed canister lights over the counters and a third twin-row installation under the cabinets for work lighting. The double-rows will be wired in series to run off 24 volt supplies in the walls. My present lighting is fraught with hot-spots from 11 different fixtures with no accent lighting on a budget of about 700 watts. The working end of my kitchen will be nicely lighted for both appearance and working illumination on a power budget of about 175 watts total. This technique produces very wide-angle illumination that is virtually shadow free. The strips are fitted with peel and stick adhesive. I'm going to use 3/4" wide strips of Formica to assemble one- piece lighting assemblies that make it easy to get the rows installed straight while laying on my back under a cabinet. The light output from these devices is very good. I suspect that one could put a single strip of this product on the under side of a glare shield and get more than enough light . . . with devices easily dimmed. Due to the series wiring of three, 3-volt devices, you would want to control dimming with a series resistance or an adjustable current supply like a Buck-Puck. Ten of these clusters would give you about 30 leds and a max bright current draw of 300 mA. A constant voltage dimmer like B&C sells COULD be modified to have minimum brightness occur at 9 volts instead of the present 4 volts. In any case, This product offers a host of illumination opportunities not the least of which is your airplane. Bob . . . ________________________________________________________________________________
From: "John Loram" <johnl(at)loram.org>
Subject: PM Alternator filter Capacitor - best practices
Date: Aug 01, 2012
What would be considered best practice for installation of the large electrolytic capacitor used to filter the output of a PM alternator: Mount it on the hot side of the firewall and protect the occupants Mount it on the cool side of the firewall and protect the capacitor Would appreciate any speculations, -john- ________________________________________________________________________________
Date: Aug 01, 2012
From: Harley <harley(at)AgelessWings.com>
Subject: Re: PM Alternator filter Capacitor - best practices
Evenin', John, Good timing for this question! Just finished installing mine last week! And no speculation in my case... I put mine inside, behind the passenger's head (Long EZ...pusher engine not as bad as it sounds....a headrest pad and a couple of canopy braces protect the passenger from the electronics on the inside of the firewall) mainly because the installation instructions with the B&C alternator specifically said NOT to mount the cap on the engine side of the firewall because of the heat there! Guess the passenger is less important than the alternator!;-) Harley Dixon Long EZ N28EZ ----------------------------------------------------------------- On 8/1/2012 5:57 PM, John Loram wrote: > What would be considered best practice for installation of the > large electrolytic capacitor used to filter the output of a PM > alternator: > Mount it on the hot side of the firewall and protect the occupants > Mount it on the cool side of the firewall and protect the capacitor > Would appreciate any speculations, -john- > * > * ________________________________________________________________________________
Date: Aug 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: PM Alternator filter Capacitor - best practices
At 04:57 PM 8/1/2012, you wrote: >What would be considered best practice for installation of the large >electrolytic capacitor used to filter the output of a PM alternator: > >Mount it on the hot side of the firewall and protect the occupants > >Mount it on the cool side of the firewall and protect the capacitor > >Would appreciate any speculations, -john- It's utility is limited. See in particular, the second page of http://tinyurl.com/cz7ekrf even with no capacitor, the noises are well under Mil-STD-704 limits for DC power systems. So mounting it 'cool' probably bodes best for service life and has little effect on system performance. Bob . . . ________________________________________________________________________________
From: "John Loram" <johnl(at)loram.org>
Subject: PM Alternator filter Capacitor - best practices
Date: Aug 01, 2012
Hmmmm... so why do we use this cap? -john- _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Wednesday, August 01, 2012 3:23 PM Subject: Re: AeroElectric-List: PM Alternator filter Capacitor - best practices At 04:57 PM 8/1/2012, you wrote: What would be considered best practice for installation of the large electrolytic capacitor used to filter the output of a PM alternator: Mount it on the hot side of the firewall and protect the occupants Mount it on the cool side of the firewall and protect the capacitor Would appreciate any speculations, -john- It's utility is limited. See in particular, the second page of http://tinyurl.com/cz7ekrf even with no capacitor, the noises are well under Mil-STD-704 limits for DC power systems. So mounting it 'cool' probably bodes best for service life and has little effect on system performance. Bob . . . ________________________________________________________________________________
Subject: Re: Using LEDs in Series
From: mapratherid <mapratherid(at)gmail.com>
Date: Aug 01, 2012
This looks pretty cool Bob. But I'm picky about color temp. Any idea what Ke lvin color you'll end up with? Regards, Matt- On Aug 1, 2012, at 1:29 PM, "Robert L. Nuckolls, III" <nuckolls.bob@aeroelec tric.com> wrote: > I have been experimenting with a product available > off eBay that offers 300, .05 x .05 LED's mounted > to a 3/8" wide x 16 foot flexible etched circuit > strip. > > http://tinyurl.com/c33w25o > > The leds are wired in paralleled series-clusters of > 3 devices and a 150 ohm resistor. Here's a 2-cluster > segment of this product . . . > > <1839fa0.jpg> > > You can cut the strip every three devices and attach new > power leads at the solder pads visible in the photo. > > I'm going to be using about 80 feet of this product in > my kitchen to put double rows of ceiling accent lighting high up, > double rows to replace recessed canister lights over the > counters and a third twin-row installation under the cabinets > for work lighting. The double-rows will be wired in series to run > off 24 volt supplies in the walls. My present lighting > is fraught with hot-spots from 11 different fixtures with > no accent lighting on a budget of about 700 watts. The working > end of my kitchen will be nicely lighted for both appearance > and working illumination on a power budget of about 175 > watts total. This technique produces very wide-angle > illumination that is virtually shadow free. > > The strips are fitted with peel and stick adhesive. I'm > going to use 3/4" wide strips of Formica to assemble one- > piece lighting assemblies that make it easy to get the > rows installed straight while laying on my back under > a cabinet. > > The light output from these devices is very good. I suspect > that one could put a single strip of this product on the > under side of a glare shield and get more than enough > light . . . with devices easily dimmed. Due to the > series wiring of three, 3-volt devices, you would want > to control dimming with a series resistance or an > adjustable current supply like a Buck-Puck. Ten of > these clusters would give you about 30 leds and a max > bright current draw of 300 mA. A constant voltage > dimmer like B&C sells COULD be modified to have minimum > brightness occur at 9 volts instead of the present > 4 volts. In any case, This product offers a host of > illumination opportunities not the least of which is > your airplane. > > Bob . . . ________________________________________________________________________________
Date: Aug 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: PM Alternator filter Capacitor - best practices
At 06:45 PM 8/1/2012, you wrote: >Hmmmm... so why do we use this cap? > Now you done it . . . let's see if I recall. I think I first saw it used on a power distribution diagrams for some Rotax powered ultra-lights back when I first started working in OBAM aviation. Shucks . . . the rectifiers of AC to DC power supplies had filter capacitors on them . . . why not the rectified ac output of a PM alternator? The idea was attractive, only the numbers were poorly understood. If you push 1 amp into a 1 Farad capacitor, you get a 1 volt per second rate of rise in voltage. 10 amps is 10 volts per second. Okay, how about a 1 microfarad capacitor? The rise is 1 million times faster or 10M volts per second. Now make the capacitor 20,000 times bigger and the voltage rise rate drops by a factor of 20K or 500 volts per second. Okay, the ripple period in the traces I published for 4000 rpm was 7.5 milliseconds. .0075 x 500 = 3.75 volts is the best ripple reduction we might expect from 20KF on a 10A machine. As you can see from page 2 trace, the pk-pk excursions are already below 400 mv. already 10X better than what we might expect with but with no capacitor. To cut that to say, 40 mV (nice anc quiet comparatively) we'd need a capacitor 100 times 20,000 or 2 Farads. I was startled by the test results with the SD-8 on B&C's alternator stand. There was little or no observable effect at ripple frequency for adding the capacitor. Yeah, we can buy such a critter but it's big, heavy, expensive and goes toward an unnecessary refinement of the system. We know that a 3-phase alternator has about 5% pk-pk ripple (0.75 volts on a 15v system) plus transients. How many Farads would it take to smooth say a 100A machine? The single phase PM alternators like the SD-8 are obviously worse but battery alone combined with loads at or near max ratings have more smoothing effects than the capacitor. Given the physical impracticality of seeing such pristine power, complimentary standards and design goals were adopted to say (in Mil- STD-704) that a 28v system can have 1 VRMS (3+ volts pk-pk) noise from 1 to 5K Hertz and tapering off each side. http://tinyurl.com/78kwfk8 1/2 that value for a 14v system. The complimentary DO-160 design goals tell us to EXPECT this kind of trash on the bus and design to live with it. The capacitor doesn't hurt anything and if you have a particularly bad set of rectifier switching transients (or similar fast rise stuff elsewhere in the system, the 20-20K computer grade capacitor will reduce the effects of that stimulus. Suffice it to say that MOST pilots now flying such capacitors on their PM alternator installations would notice nothing from the cockpit if that capacitor were removed. Radios and audio systems need really clean power and the qualified designer provides smoothing internally. Emacs! Our audio isolation amplifier design uses the LM317 to provide a smooth source of +8 volts to run the circuitry. As a general rule, the kinds of stimulus that benefits from any sort of bus voltage filtering is fast-rise transients at a ripple-current rate. Folks mistakenly believe their inductor/capacitor or just a capacitor is bypassing AUDIO frequency energy when in fact, it's high frequency (fast transients) at the audio rate. As the numbers above suggest, there's no practical way to filter alternator ripple from the bus. The snow-mobile engines with lighting coils converted to electrical system alternators may well have benefited from the use of such capacitors . . . depends on vulnerabilities inherent in their electro-whizzies. Our electro-whizzies are suited by design to live in the world of trashy busses. This is why switchmode power supplies can be so small when delivering outputs in the tens of amps . . . their operating frequencies (hence ripple frequency) is quite high which allows smaller capacitors and inductors to do the same degree of smoothing. You can leave the cap out and see if you hear any alternator whine in the audio . . . odds are that you will not. Bob . . . ________________________________________________________________________________
Date: Aug 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Using LEDs in Series
At 08:13 PM 8/1/2012, you wrote: >This looks pretty cool Bob. But I'm picky about color temp. Any idea >what Kelvin color you'll end up with? You can select for cool, pure, or warm white colors when you order. Given the cheapness of excess brightness for you can probably do some shading with theater lighting gels. I had to match some lighting colors in incandescent lamps about 25 years ago at Videmation. A local theater supply store had every color hue and density imaginable in gels for about $2 a sheet. We fiddled with the filters until we got it right. In my kitchen I'll be using the pure whites and letting colors reflected from surfaces set the mood. At Cessna, blue-white post lighting was a high dollar option for panel illumination. You could get the same thing by putting the appropriate gel over the lamps. Bob . . . ________________________________________________________________________________
From: "John Loram" <johnl(at)loram.org>
Subject: PM Alternator filter Capacitor - best practices
Date: Aug 01, 2012
So we're not trying to control the bandwidth of the regulator loop with the cap? Does the battery do that? Guess I don't really know what the frequency response of a lead-acid battery is. Probably dependent on the state of charge and the condition of the battery. And the load varies all over the place, both real and imaginary components.... What would it look like with and without the cap if the battery were out of the loop? ... Scary! I'm running 3 phase (old Jab 3300). Once I get this thing fired up I'll run some tests and let you know what happens... Just thinking out loud, -john- p.s. ran into a message the other day that you wrote back in 2007. Said you worked for H.L Yoh as a civilian instructor in the early 60's... Same here! At the Naval ETA school on Treasure Island. Wasn't that fun. I learned more electronics in six months instructing those kids than four years of collage! _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Wednesday, August 01, 2012 7:11 PM Subject: RE: AeroElectric-List: PM Alternator filter Capacitor - best practices At 06:45 PM 8/1/2012, you wrote: Hmmmm... so why do we use this cap? Now you done it . . . let's see if I recall. I think I first saw it used on a power distribution diagrams for some Rotax powered ultra-lights back when I first started working in OBAM aviation. Shucks . . . the rectifiers of AC to DC power supplies had filter capacitors on them . . . why not the rectified ac output of a PM alternator? The idea was attractive, only the numbers were poorly understood. If you push 1 amp into a 1 Farad capacitor, you get a 1 volt per second rate of rise in voltage. 10 amps is 10 volts per second. Okay, how about a 1 microfarad capacitor? The rise is 1 million times faster or 10M volts per second. Now make the capacitor 20,000 times bigger and the voltage rise rate drops by a factor of 20K or 500 volts per second. Okay, the ripple period in the traces I published for 4000 rpm was 7.5 milliseconds. .0075 x 500 = 3.75 volts is the best ripple reduction we might expect from 20KF on a 10A machine. As you can see from page 2 trace, the pk-pk excursions are already below 400 mv. already 10X better than what we might expect with but with no capacitor. To cut that to say, 40 mV (nice anc quiet comparatively) we'd need a capacitor 100 times 20,000 or 2 Farads. I was startled by the test results with the SD-8 on B&C's alternator stand. There was little or no observable effect at ripple frequency for adding the capacitor. Yeah, we can buy such a critter but it's big, heavy, expensive and goes toward an unnecessary refinement of the system. We know that a 3-phase alternator has about 5% pk-pk ripple (0.75 volts on a 15v system) plus transients. How many Farads would it take to smooth say a 100A machine? The single phase PM alternators like the SD-8 are obviously worse but battery alone combined with loads at or near max ratings have more smoothing effects than the capacitor. Given the physical impracticality of seeing such pristine power, complimentary standards and design goals were adopted to say (in Mil- STD-704) that a 28v system can have 1 VRMS (3+ volts pk-pk) noise from 1 to 5K Hertz and tapering off each side. http://tinyurl.com/78kwfk8 1/2 that value for a 14v system. The complimentary DO-160 design goals tell us to EXPECT this kind of trash on the bus and design to live with it. The capacitor doesn't hurt anything and if you have a particularly bad set of rectifier switching transients (or similar fast rise stuff elsewhere in the system, the 20-20K computer grade capacitor will reduce the effects of that stimulus. Suffice it to say that MOST pilots now flying such capacitors on their PM alternator installations would notice nothing from the cockpit if that capacitor were removed. Radios and audio systems need really clean power and the qualified designer provides smoothing internally. Emacs! Our audio isolation amplifier design uses the LM317 to provide a smooth source of +8 volts to run the circuitry. As a general rule, the kinds of stimulus that benefits from any sort of bus voltage filtering is fast-rise transients at a ripple-current rate. Folks mistakenly believe their inductor/capacitor or just a capacitor is bypassing AUDIO frequency energy when in fact, it's high frequency (fast transients) at the audio rate. As the numbers above suggest, there's no practical way to filter alternator ripple from the bus. The snow-mobile engines with lighting coils converted to electrical system alternators may well have benefited from the use of such capacitors . . . depends on vulnerabilities inherent in their electro-whizzies. Our electro-whizzies are suited by design to live in the world of trashy busses. This is why switchmode power supplies can be so small when delivering outputs in the tens of amps . . . their operating frequencies (hence ripple frequency) is quite high which allows smaller capacitors and inductors to do the same degree of smoothing. You can leave the cap out and see if you hear any alternator whine in the audio . . . odds are that you will not. Bob . . . ________________________________________________________________________________
Date: Aug 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Latching Relay Redux
At 12:30 PM 8/1/2012, you wrote: >At 10:20 AM 8/1/2012, you wrote: > >Is that 75% power reduction correct?? > >I would have guessed that a 50% duty cycle gave full voltage and >full current for 50% of the time in a pulsed resistance circuit >resulting in a 50% power reduction. Not sure about an inductive coil >contactor though. > >Just asking but intuitively I would not have averaged the voltage >and applied the I squared power calculation to this. >----------- P.S. just for grins, I thermocoupled the contactor and let it stabilize for over an hour. Got a 120 F shell at 50% duty cycle for a 40F rise. Let it run 100% duty cycle to stabilization and got a 180F shell temperature for a 100F rise. At that temperature, the 100% duty cycle current draw was down to .6 amps from the cold start at .9 amps. This copper temperature coefficient of resistance rise in coil accounts for the less than 4x temperature rise for 4x the dissipated power . . . This means that a cooler contactor uses the power you supply it more efficiently by running a lower winding resistance. I.e. ampere turns of magnetic flux that is more proportional to applied voltage because the coil is cooler. By the way, here's one approach to fabricating a "contactor cooler" . . . http://tinyurl.com/bolkoyc On power up, both capacitors are discharged. The 10uf holds down on the comparator pins 2,6 for about 100 milliseconds thus holding the output pin 3 HI, turning the FED on hard and energizing the contactor with full voltage. The 10uF charges up in 100-200 milliseconds thus allowing the 555 to 'hum' at about 200Hz and 50% duty cycle. The diode and RC network across the contactor coil should be mounted right to the contactor terminals. All other components can be remotely located but close proximity to contactor is best. Bob . . . ________________________________________________________________________________
Date: Aug 02, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: PM Alternator filter Capacitor - best practices
At 10:18 PM 8/1/2012, you wrote: So we're not trying to control the bandwidth of the regulator loop with the cap? Does the battery do that? Guess I don't really know what the frequency response of a lead-acid battery is. Probably dependent on the state of charge and the condition of the battery. And the load varies all over the place, both real and imaginary components.... What would it look like with and without the cap if the battery were out of the loop? ... Scary! http://tinyurl.com/bqa6q9p Finely tuned loop dynamics with these regulators is wishful thinking. Here's an exemplar schematic for a PM regulator: http://tinyurl.com/bwomjjz I split out the two functions (regulation and warning light) http://tinyurl.com/c8usyw2 http://tinyurl.com/c6doa97 As you can see in the v-reg schematic, there are no reactive components that would shape closed-loop response. A battery is a very poor 'filter' . . . it delivers energy at 12.5 and below . . . accepts energy at 13.8 and above. That's about 1.3 volts of span where the battery is dynamically 'unhooked'. It stands to reason that the capacitor would have the greatest effect when the alternator set point was too low (under 14.5) and the system was lightly loaded. I'm running 3 phase (old Jab 3300). Interesting. I think your regulator is still quite similar . . . it just adds another diode/scr pair. Once I get this thing fired up I'll run some tests and let you know what happens... I have a fast switching, dynamic load bank I built for tests at HBC some years back. It would be interesting to use it along with a data acquisition system on the test bench to explore the closed loop response of these systems. Just thinking out loud, -john- p.s. ran into a message the other day that you wrote back in 2007. Said you worked for H.L Yoh as a civilian instructor in the early 60's... Same here! At the Naval ETA school on Treasure Island. Wasn't that fun. I learned more electronics in six months instructing those kids than four years of collage! You got that right! I was teaching in the top 4 weeks of a 26 week school at Great Lakes. I went to work on a Friday and they handed me a syllabus for my first section of students along with a copy of "the bible", Termnan's Electrical Engineering Handbook http://tinyurl.com/cbvvjx9 and said, "you get your first class of 20 next Monday." As long as I stayed a day ahead of the class . . . things went well . . . and yes, a lot of fun. After four or so passes through the class materials and figuring out a half dozen ways to explain each concept, it sorta creeps into your DNA. There's no better way to learn something than to be chartered to teach it. Do you have access to a fast data acquisition system that you could hook to your bus for some hard data gathering? I've used cousins to this critter . . . http://tinyurl.com/3jtrxx4 on several tasks at HBC with great results. Being able to jump on an airplane and get hard data in flight without having to involve a dozen folks from the instrumentation lab was a powerful tool. You might consider getting one of these and use it to graph some of the performance qualities of your system. It would be a great augmentation of my ripple studies. Bob . . . ________________________________________________________________________________
Date: Aug 02, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: PM Alternator filter Capacitor - best practices
At 10:18 PM 8/1/2012, you wrote: So we're not trying to control the bandwidth of the regulator loop with the cap? Does the battery do that? Guess I don't really know what the frequency response of a lead-acid battery is. Probably dependent on the state of charge and the condition of the battery. And the load varies all over the place, both real and imaginary components.... What would it look like with and without the cap if the battery were out of the loop? ... Scary! http://tinyurl.com/bqa6q9p Finely tuned loop dynamics with these regulators is wishful thinking. Here's an exemplar schematic for a PM regulator: http://tinyurl.com/bwomjjz I split out the two functions (regulation and warning light) http://tinyurl.com/c8usyw2 http://tinyurl.com/c6doa97 As you can see in the v-reg schematic, there are no reactive components that would shape closed-loop response. A battery is a very poor 'filter' . . . it delivers energy at 12.5 and below . . . accepts energy at 13.8 and above. That's about 1.3 volts of span where the battery is dynamically 'unhooked'. It stands to reason that the capacitor would have the greatest effect when the alternator set point was too low (under 14.5) and the system was lightly loaded. I'm running 3 phase (old Jab 3300). Interesting. I think your regulator is still quite similar . . . it just adds another diode/scr pair. Once I get this thing fired up I'll run some tests and let you know what happens... I have a fast switching, dynamic load bank I built for tests at HBC some years back. It would be interesting to use it along with a data acquisition system on the test bench to explore the closed loop response of these systems. Just thinking out loud, -john- p.s. ran into a message the other day that you wrote back in 2007. Said you worked for H.L Yoh as a civilian instructor in the early 60's... Same here! At the Naval ETA school on Treasure Island. Wasn't that fun. I learned more electronics in six months instructing those kids than four years of collage! You got that right! I was teaching in the top 4 weeks of a 26 week school at Great Lakes. I went to work on a Friday and they handed me a syllabus for my first section of students along with a copy of "the bible", Termnan's Electrical Engineering Handbook http://tinyurl.com/cbvvjx9 and said, "you get your first class of 20 next Monday." As long as I stayed a day ahead of the class . . . things went well . . . and yes, a lot of fun. After four or so passes through the class materials and figuring out a half dozen ways to explain each concept, it sorta creeps into your DNA. There's no better way to learn something than to be chartered to teach it. Do you have access to a fast data acquisition system that you could hook to your bus for some hard data gathering? I've used cousins to this critter . . . http://tinyurl.com/3jtrxx4 on several tasks at HBC with great results. Being able to jump on an airplane and get hard data in flight without having to involve a dozen folks from the instrumentation lab was a powerful tool. You might consider getting one of these and use it to graph some of the performance qualities of your system. It would be a great augmentation of my ripple studies. Bob . . . ________________________________________________________________________________
Subject: Re: PM Alternator filter Capacitor - best practices
From: "Tundra10" <jpx(at)qenesis.com>
Date: Aug 02, 2012
So should the capacitor and 1K resistor be deleted from Z13/8 ? Note 20 indicates the purpose of the capacitor is to smooth the voltage if the battery is offline. However, there is no intentional way of disconnecting the battery, and there are very few failures that could result in the battery being disconnected while the SD-8 still remains connected to the battery bus. In Z13/8 the SD-8 is only turned on in the event of a main alternator failure. Maybe in this circumstance, a little noise in the audio is not significant to the completion of the flight (assuming the capacitor actually helps in a given installation). Jeff Page Dream Aircraft Tundra #10 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379872#379872 ________________________________________________________________________________
From: "John Loram" <johnl(at)loram.org>
Subject: PM Alternator filter Capacitor - best practices
Date: Aug 02, 2012
Thank you for the schematics. Most instructive! > > p.s. ran into a message the other day that you wrote back in 2007. > Said you worked for H.L Yoh as a civilian instructor in the > early 60's... Same here! At the Naval ETA school on Treasure > Island. Wasn't that fun. I learned more electronics in six > months instructing those kids than four years of collage! > > You got that right! I was teaching in the > top 4 weeks of a 26 week school at Great > Lakes. I went to work on a Friday and they > handed me a syllabus for my first section > of students along with a copy of "the bible", > Termnan's Electrical Engineering Handbook > > http://tinyurl.com/cbvvjx9 And thank you for Villard's Memoir. I loved reading every bit of it! Like every self-respecting EE I have kept my copy of Terman. > > and said, "you get your first class of 20 > next Monday." As long as I stayed a day ahead > of the class . . . things went well . . . > and yes, a lot of fun. After four or > so passes through the class materials and > figuring out a half dozen ways to explain each > concept, it sorta creeps into your DNA. There's > no better way to learn something than to > be chartered to teach it. > And in every other class you'd get one 'ringer'. A kid fresh out of engineering school who would nail you to the chalk board at the slightest slip-up!!! You either got those guys on your side right away or you were in for some tough sledding! > Do you have access to a fast data acquisition > system that you could hook to your bus for > some hard data gathering? > > I've used cousins to this critter . . . > > http://tinyurl.com/3jtrxx4 I have a couple of these first generation DI-148Us. It will run at 11 KHz sampling rate on one channel. Tell me more about your dynamic load bank. Sounds like just the ticket. >... > You might consider getting one of these > and use it to graph some of the performance > qualities of your system. It would be a great > augmentation of my ripple studies. > > > Bob . . . > > I'd be happy to contribute! I'm probably a month away from first start and another month coming down off the high!!, -john- ________________________________________________________________________________
Date: Aug 02, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: PM Alternator filter Capacitor - best practices
At 10:55 AM 8/2/2012, you wrote: So should the capacitor and 1K resistor be deleted from Z13/8 ? Don't delete anything. We're having a discussion about the notion that data gathered on an SD-8 with a 'scope about 10 years ago doesn't confirm legacy beliefs about what a capacitor across a power supply does for us. This capacitor MAY have some value in fast, low energy transient mitigation and/or regulation dynamics. John and I will continue to ponder "out loud on the List" but don't take any hypothesis as cause to rise up and evict your capacitor. The capacitor AND 1K resistor are also participants in the self excitation system. Note 20 indicates the purpose of the capacitor is to smooth the voltage if the battery is offline. However, there is no intentional way of disconnecting the battery, and there are very few failures that could result in the battery being disconnected while the SD-8 still remains connected to the battery bus. In Z13/8 the SD-8 is only turned on in the event of a main alternator failure. Maybe in this circumstance, a little noise in the audio is not significant to the completion of the flight (assuming the capacitor actually helps in a given installation). Good questions/suppositions all . . . we'll endeavor to sort it out with greater clarity. Bob . . . ________________________________________________________________________________
Subject: Extending thermocouple leads
From: "Radioflyer" <skyeyecorp(at)airpost.net>
Date: Aug 02, 2012
I think I understand how to do things right with thermocouples, but want to make sure. I have a set of (GRT/EIS) J- type, CHT bayonet thermocouples. The 2 foot leads are terminated from the factory in what I believe to be standard spade terminals. I need to lengthen these leads about 12 feet to reach my MGL Avionics quad CHT display instrument. So I plan to get some J-type wire, crimp on some mating spade terminals and similarly terminate the other end very close to the instrument. (One set of spades will be in the hot engine compartment and the spades on the other end of the extension will be in the cabin.) My understanding is that the parasitic couples at the spade terminals will be cancelled out, so I should get accurate temp readings at the instrument. Correct? Is it worth the trouble to search for stranded J-wire or is solid good enough? --Jose Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379921#379921 ________________________________________________________________________________
Date: Aug 03, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Extending thermocouple leads
At 11:27 PM 8/2/2012, you wrote: I think I understand how to do things right with thermocouples, but want to make sure. I have a set of (GRT/EIS) J- type, CHT bayonet thermocouples. The 2 foot leads are terminated from the factory in what I believe to be standard spade terminals. I need to lengthen these leads about 12 feet to reach my MGL Avionics quad CHT display instrument. So I plan to get some J-type wire, crimp on some mating spade terminals and similarly terminate the other end very close to the instrument. (One set of spades will be in the hot engine compartment and the spades on the other end of the extension will be in the cabin.) My understanding is that the parasitic couples at the spade terminals will be cancelled out, so I should get accurate temp readings at the instrument. Correct? Sort of . . . What do the 'spade' terminals attach to? The "wrong+wrong=right" thing applies only when pairs of wrongness are applied to EACH lead . . . not opposite leads. When thermocouple gages of yore were brought to an instrument on the panel, they too were terminated in ordinary terminals onto studs at the back of the instrument in the cockpit environment. These too introduced small errors that were acceptable in the grand scheme of things. A few degrees of error in hundreds of degrees of reading. Putting ring terminals onto a thermocouple at the 'cold junction' or 'reference junction' end of the wire introduces little error . . . the hotter the environment of the polluting junctions, the greater the absolute error . . . but the percentage of error vis-a-vis local temperature is about the same. Ring terminals used to splice a t/c wire run with a nut-n-screw would be an example of many wrongs adding up to not-too-bad. But the single spade on one end of each side will induce some small errors. Having offered all that, the maximum error you might encounter is insignificant in this situation. You're not going to make decisions based on a few degrees of reading. It's departures from 'normal' and trends that deserve your attention. So don't fuss over the details too much . . . Is it worth the trouble to search for stranded J-wire or is solid good enough? From a measurement perspective, solid and stranded can be interchanged and spliced in the same system. You can get small quantities of a variety of t/c wires from Omega at http://tinyurl.com/cwnomt3 Their part number builder says they'll sell you 25' of TT-J-24S for $30.00 eBay may offer additional opportunities at http://tinyurl.com/cr35ff4 I've got a bunch of thermocouple wire stashed in boxes yet unpacked from the move . . . else I'd offer to send you a hunk of something suited to your task. But in the 105 weather I'm not inclined to rummage around out in an un-conditioned part of the shop! Bob . . . ________________________________________________________________________________
Date: Aug 03, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: PM Alternator filter Capacitor - best practices
>And thank you for Villard's Memoir. I loved reading every bit of it! > >Like every self-respecting EE I have kept my copy of Terman. > >[] > I lost my copy during some move over the years. Thought I might replace it from a used book store someday . . . have you seen what they sell for now? Hang onto the copy you have and be sure to include it in the accounting of your retirement portfolio. And in every other class you'd get one 'ringer'. A kid fresh out of engineering school who would nail you to the chalk board at the slightest slip-up!!! You either got those guys on your side right away or you were in for some tough sledding! I don't recall having encountered that from the run-of-the-mill students. Most of my guys were fresh out of boot-camp. I did have a chief who was re-upping and wanting to expand his technological horizons. He and I had an arm-wrestling match over my dismal record for Friday High-Class honors . . . but that's another story. He did very well in his studies and received benefits befitting his due diligence. >[] > >I have a couple of these first generation DI-148Us. >It will run at 11 KHz sampling rate on one channel. Cool! Let's do some good numbers gathering off your ship's electrical system when it's appropriate. > >Tell me more about your dynamic load bank. Sounds like just the ticket. Here's one I started for my shop some years ago but when the project-of-need went away, it's been waiting for a reason to finish it. The one I built for HBC might still be there but since it never got a corporate acquisition sticker or tool number put on it, it's probably been pitched by now. There's nobody left there who saw what it does or how to use it. [] The thing was used to study the effects of rapid load dump and onset for some led lighting supplies in the Hawker 800. When the cabin lights 'flicker' in a $14M airplane, the boss can only sit there an fume that this crap doesn't happen in his $60K automobile. The notion was to excite the bus with repetitive square-wave loads either manually by external controls while gathering responses and/or trying fixes elsewhere. For our purposes, a 555 timer, a boss-hog fet and a power resistor could be quickly brass-boarded into a similarly useful fixture. [] This test fixture would apply/release a load at some periodic rate (in this case about 0.5Hz) to let you observe system response after the event. Your Dataq DAS in the single channel, fast acquisition mode would do nicely to record the event. Bob . . . ________________________________________________________________________________
Subject: Re: Extending thermocouple leads
From: "Radioflyer" <skyeyecorp(at)airpost.net>
Date: Aug 03, 2012
Bob, thanks for your reply. You asked what the spade terminals were attached to. They are crimped on to the J wires of the thermocouple sensor. The wires are red and white and one of them was magnetic. You are right that a few degrees of error would not much matter for CHT readings. I don't have a sense for how much error my "J-spade-J-spade-instrument" setup would introduce, but if within say ten degrees then it would be ok. I just want to be sure I can reliably tell that my cylinders are not exceeding max allowable temperature. --Jose Read this topic online here: http://forums.matronics.com/viewtopic.php?p=379950#379950 ________________________________________________________________________________
Date: Aug 04, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Extending thermocouple leads
At 01:51 PM 8/3/2012, you wrote: > >Bob, thanks for your reply. You asked what the spade terminals were >attached to. They are crimped on to the J wires of the thermocouple >sensor. The wires are red and white and one of them was magnetic. Do the terminals terminate to a 'sensor' under the cowl or to an instrument behind the panel? >You are right that a few degrees of error would not much matter for >CHT readings. I don't have a sense for how much error my >"J-spade-J-spade-instrument" setup would introduce, but if within >say ten degrees then it would be ok. I just want to be sure I can >reliably tell that my cylinders are not exceeding max allowable temperature. Sure. One way to check your instrument's calibration with as-installed thermocouples is to get one of those in-the-cup immersion heaters for travel-coffee/tea and use it to raise a cup of distilled or R/O water to boiling. You can do this right next to the engine where you've removed a cht sensor bulb and immerse it in the water. Wait several minutes while the reading stabilizes. Compare with boiling point of water at your present atmospheric pressure conditions: http://tinyurl.com/bmptwag and you can see just how close the instrument is to reading true at about 200F. Bob . . . ________________________________________________________________________________
From: Mickey Coggins <mick-matronics(at)rv8.ch>
Date: Aug 04, 2012
Subject: Starter contactor leaking voltage
Thanks Bob, Gents, for the feedback on this. I have done it the way the plans show, and you suggested, and put the starter contactor on the FW. New question (yes, I'm building very slowly) - I have the Van's starter contactor (Part Number = ES 24021) and when I apply 12v to the battery connection, I get about 0.4v on the starter connection. This is before it is energized. When I apply the 12v to the 'S' terminal, I get the full 12v on the starter terminal. Is it normal for some voltage to "leak" even when the device is "idle"? My battery contactors don't do this, and I don't have another starter contactor to test with. Thanks, Mickey ________________________________________________________________________________
Subject: Re: Extending thermocouple leads
From: "Radioflyer" <skyeyecorp(at)airpost.net>
Date: Aug 04, 2012
The extension (thermocouple) wire pair would eventually connect to an instrument on the panel in the cabin. So, Engine side: thermocouple--spades--J wire pair extension--thru firewall. Then Cabin side: extension cont'd--spades--copper--instrument on panel. The extension is 12 feet long because this is in a pusher aircraft. Spades to copper to instrument because I can't connect the J type thermocouples wires directly to the DB15 on the instrument. What I'm thinking is that the parasitic couple between spades and thermocouple wire pair in the hot engine side, and the other parasitic couple of thermocouple wire pair and spades in the cooler cabin will not much affect the absolute temp readings. --Jose Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380062#380062 ________________________________________________________________________________
Subject: Re: Starter contactor leaking voltage
From: "user9253" <fran4sew(at)banyanol.com>
Date: Aug 05, 2012
Theoretically there should be NO leakage through the starter contactor. But the insulation used in the contactor is not perfect. There could be some insignificant leakage. Digital voltmeters have a very high input impedance which allows them to measure insignificant voltage. Try shorting the output terminal to ground with your fingers of one hand while measuring the voltage. Or use an old analog voltmeter which will give more meaningful measurements in this situation. Or use a very small 12v test lamp, the type used for automotive instrument illumination. I do not think there is enough leakage to worry about. Joe -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380080#380080 ________________________________________________________________________________
Subject: Re: Starter contactor leaking voltage
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Aug 05, 2012
repost As others have mentioned, the problem is in how you use your tools...like the voltmeter. Imagine that you have a voltmeter that is infinitely sensitive (infinite impedance). Now it will measure the battery voltage even thru an open switch. In fact, it will measure 500 volts between your belt buckle and your shoe laces. And the top of your hat will be 1000 volts higher than the soles of your New Balance sneakers. You can actually extract some tiny amount of power this way. So meter impedance is not a lack of quality in a meter, it is a necessary and useful characteristic of the measuring device. And in a solid state circuit (like a diode), there will almost always be a voltage on the output that is similar to the input voltage even when the meter is off. And in fact the "leakage voltage" will not be able to light even the tiniest LED...so ignore it. I once designed a Cmos circuit where somebody (okay, me...) forgot to add the power trace to the IC. Years later, an inquisitive technician, tracing an unrelated fault discovered it, but all the shipped product had worked just fine. So just don't make voltage measurements like this. See attached for a better way. -------- -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380088#380088 Attachments: http://forums.matronics.com//files/diode_test_745.pdf ________________________________________________________________________________
Date: Aug 05, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Starter contactor leaking voltage
New question (yes, I'm building very slowly) - I have the Van's starter contactor (Part Number = ES 24021) and when I apply 12v to the battery connection, I get about 0.4v on the starter connection. =C2 This is before it is energized. =C2 When I apply the 12v to the 'S' terminal, I get the full 12v on the starter terminal. Is it normal for some voltage to "leak" even when the device is "idle"? =C2 My battery contactors don't do this, and I don't have another starter contactor to test with. Thanks, Mickey At 07:18 AM 8/5/2012, you wrote: Theoretically there should be NO leakage through the starter contactor. But the insulation used in the contactor is not perfect. There could be some insignificant leakage. Digital voltmeters have a very high input impedance which allows them to measure insignificant voltage. Try shorting the output terminal to ground with your fingers of one hand while measuring the voltage. Or use an old analog voltmeter which will give more meaningful measurements in this situation. Or use a very small 12v test lamp, the type used for automotive instrument illumination. I do not think there is enough leakage to worry about. Joe My thoughts exactly. This thread illustrates a measurement conundrum that has existed since day one in the study and diagnosis of electron flow. The ideal measurement technique should be transparent to quantities being explored. The earliest precision voltmeters (ammeters with resistors in series) were excellent demonstrations of the best-we-knew-how-to-do at the time. Emacs! Note the label at the bottom of the scale=plate that says "1000 ohms per volt". This is another way of saying that this instrument has a basic sensitivity of 1 milliampere full scale and when making a reading on the 150 volt scale, the instrument presents a "load" to the circuit being measured of 1000 x 150 or 150,000 ohms. It will "draw" 1 milliampere of current from the measurement node at 150 volts. These instruments were a grade trade off between sensitivity, accuracy, linearity and calibration drift due to temperature and age. But an instrument like this is fitted with a 'mirrored scale'. The observer lines up the pointer with the reflection of the pointer so as to drive parallax error to zero. This instrument could be both read and relied upon for readings with certainty of 1% or better. If you had measured the "output" from your open starter contactor with such a device, no doubt the reading would be zero . . . and commensurate with your expectations. The day I got hired into Boeing (at $86/week) I went down to Interstate Electronics and bought a Triplett 630 multimeter. It was a 20,000 ohm/volt instrument (50 microamp movement) and exemplary technology for run-of-the-mill bench test instruments. It replaced a 1000 ohm/volt meter that somebody had given me some 5 years earlier. I still have the 630. It was 20 times more sensitive than the earlier instrument and offered accuracies on the order of 2%. But no doubt the Triplett would also say that your contactor was working as expected. Such devices were useless for many investigations into the function of vacuum tubes. The source impedance of many voltages of interest were so high that probing the node with this voltmeter would also show zero volts . . . and the circuit under test would cease to function at all. Probing through sensitive circuitry added new requirements for sensitivity and isolation. This was achieved with some form of amplification. A exemplar instrument is shown here: Emacs! This Heathkit product has an input circuit that looks like this: Emacs! Notice the voltage divider of resistors that total up to more than 9 megohms. Notice too a 1 meg resistor built into the probe. The input impedance for this instrument is over 10 megohms. Further, probing a node with a combination of DC volts of interest that also carries some signal (perhaps even high frequency RF) is only very slightly affected by the probe. This instrument is several hundred times more sensitive than the device at the top of the page. This kind of instrument may also have produced an anomalous reading in the de-energized condition. Modern digital voltmeters have input impedances on the order of 20 megohms. Further, they do not provide any isolation for probe-effects when measuring 'busy circuits'. I have crafted a x10 probe for my Fluke multimeter from an low capacity, oscilloscope probe to conduct the kinds of measurements I used to do with my Heathkit VTVM. Also, I have some load resistors I can stack onto the voltmeter's test lead jacks that deliberately degrade instrument sensitivity so that readings are not influenced by small leakages. The point of this soliloquy is to remind us that not all observations provide good data . . . but all data can be filtered through a healthy level of skepticism supported by an understanding of the circuit under test along with the measuring device's limits. Bob . . . ________________________________________________________________________________
Date: Aug 05, 2012
From: "Richard E. Tasker" <retasker(at)optonline.net>
Subject: Re: Extending thermocouple leads
You are absolutely correct. In fact, it may not affect the readings at all. The way a thermocouple works is that any given metal will generate a voltage from one end to the other if the temperature is different from one end to the other. If one chooses a different metal for a second wire it will generate a different voltage across its length. If one hooks a meter between the two wires at one end it can be calibrated to read the difference in temperature between the two ends because the sum of the two outputs will vary with temperature. If there is no difference in temperature between the two ends, there is no voltage generated so no temperature reading displayed. You can make all kinds of connections and add other materials between the two ends and you will see no temperature reading as long there is no temperature difference. Taking that one step further, if there is no temperature difference between the each end of the things you add, then, even if there is a temperature difference between the far end (cylinder head) and the meter end, it will still read correctly. So, if a spade connection is the same temperature from end to end (which is pretty likely since they are copper - a very good heat conductor) there will be no net voltage generated across the connection. Which means that the reading you get at the meter (or whatever you are using to read the temperature) will still be the same as if you had no spade connection. Where you would get into trouble is if you add a long splice in the thermocouple wire that is not thermocouple wire. For example if you add several feet of copper wire to your too short thermocouple wire. The likelihood of that being the same temperature at each end decreases in proportion to the length of the extension. Bottom line: You will likely see no difference in reading with or without the spade and pin connections. Dick Tasker Radioflyer wrote: > > The extension (thermocouple) wire pair would eventually connect to an instrument on the panel in the cabin. So, Engine side: thermocouple--spades--J wire pair extension--thru firewall. Then Cabin side: extension cont'd--spades--copper--instrument on panel. The extension is 12 feet long because this is in a pusher aircraft. Spades to copper to instrument because I can't connect the J type thermocouples wires directly to the DB15 on the instrument. > > What I'm thinking is that the parasitic couple between spades and thermocouple wire pair in the hot engine side, and the other parasitic couple of thermocouple wire pair and spades in the cooler cabin will not much affect the absolute temp readings. > > --Jose > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=380062#380062 > > -- Please Note: No trees were destroyed in the sending of this message. We do concede, however, that a significant number of electrons may have been temporarily inconvenienced. -- ________________________________________________________________________________
From: Mickey Coggins <mick-matronics(at)rv8.ch>
Date: Aug 05, 2012
Subject: Re: Starter contactor leaking voltage
Joe, Eric, Bob, Thanks so much for the feedback - I tried the lamp, and of course it did not light up. Also used an older analog instrument, and it showed no indication of voltage. Thanks to your help and a bit of time reading up on impedance, I have a better understanding what is happening here. I'm really happy to have run across this "problem" as it allowed me to learn some new stuff. Thanks again! Regards, Mickey On Sun, Aug 5, 2012 at 4:51 PM, Robert L. Nuckolls, III < nuckolls.bob(at)aeroelectric.com> wrote: > New question (yes, I'm building very slowly) - I have the Van's starter > contactor (Part Number = ES 24021) and when I apply 12v to the battery > connection, I get about 0.4v on the starter connection. =C3=82 This is be fore it > is energized. =C3=82 When I apply the 12v to the 'S' terminal, I get the full > 12v on the starter terminal. > > Is it normal for some voltage to "leak" even when the device is "idle"? =C3=82 > My battery contactors don't do this, and I don't have another starter > contactor to test with. > > Thanks, > Mickey > > At 07:18 AM 8/5/2012, you wrote: m > > > > Theoretically there should be NO leakage through the starter contactor. > But the insulation used in the contactor is not perfect. There could be > some insignificant leakage. Digital voltmeters have a very high input > impedance which allows them to measure insignificant voltage. Try shorti ng > the output terminal to ground with your fingers of one hand while measuri ng > the voltage. Or use an old analog voltmeter which will give more > meaningful measurements in this situation. Or use a very small 12v test > lamp, the type used for automotive instrument illumination. > I do not think there is enough leakage to worry about. > Joe > > My thoughts exactly. This thread illustrates > a measurement conundrum that has existed since > day one in the study and diagnosis of electron > flow. The ideal measurement technique should be > transparent to quantities being explored. The > earliest precision voltmeters (ammeters with resistors > in series) were excellent demonstrations of the > best-we-knew-how-to-do at the time. > > [image: Emacs!] > > Note the label at the bottom of the scale=plate that > says "1000 ohms per volt". This is another way of saying > that this instrument has a basic sensitivity of 1 milliampere > full scale and when making a reading on the 150 volt > scale, the instrument presents a "load" to the circuit > being measured of 1000 x 150 or 150,000 ohms. It will > "draw" 1 milliampere of current from the measurement node > at 150 volts. > > These instruments were a grade trade off between > sensitivity, accuracy, linearity and calibration drift > due to temperature and age. But an instrument like > this is fitted with a 'mirrored scale'. The observer > lines up the pointer with the reflection of the pointer > so as to drive parallax error to zero. This instrument > could be both read and relied upon for readings with > certainty of 1% or better. > > If you had measured the "output" from your open starter > contactor with such a device, no doubt the reading would > be zero . . . and commensurate with your expectations. > > The day I got hired into Boeing (at $86/week) I > went down to Interstate Electronics and bought > a Triplett 630 multimeter. It was a 20,000 ohm/volt > instrument (50 microamp movement) and exemplary > technology for run-of-the-mill bench test > instruments. It replaced a 1000 ohm/volt meter > that somebody had given me some 5 years earlier. > I still have the 630. It was 20 times more sensitive > than the earlier instrument and offered accuracies > on the order of 2%. > > But no doubt the Triplett would also say that > your contactor was working as expected. > > Such devices were useless for many investigations into > the function of vacuum tubes. The source impedance of > many voltages of interest were so high that probing > the node with this voltmeter would also show zero > volts . . . and the circuit under test would cease > to function at all. > > Probing through sensitive circuitry added new > requirements for sensitivity and isolation. This > was achieved with some form of amplification. A > exemplar instrument is shown here: > > [image: Emacs!] > > This Heathkit product has an input circuit that > looks like this: > > [image: Emacs!] > > > Notice the voltage divider of resistors that total up to > more than 9 megohms. Notice too a 1 meg resistor built > into the probe. The input impedance for this instrument > is over 10 megohms. Further, probing a node with a > combination of DC volts of interest that also carries > some signal (perhaps even high frequency RF) is only > very slightly affected by the probe. This instrument > is several hundred times more sensitive than the > device at the top of the page. > > This kind of instrument may also have produced an > anomalous reading in the de-energized condition. > > Modern digital voltmeters have input impedances on > the order of 20 megohms. Further, they do not provide > any isolation for probe-effects when measuring 'busy > circuits'. I have crafted a x10 probe for my Fluke > multimeter from an low capacity, oscilloscope probe > to conduct the kinds of measurements I used to do > with my Heathkit VTVM. Also, I have some load resistors > I can stack onto the voltmeter's test lead jacks that > deliberately degrade instrument sensitivity so that > readings are not influenced by small leakages. > > The point of this soliloquy is to remind us > that not all observations provide good data > . . . but all data can be filtered through a > healthy level of skepticism supported by an > understanding of the circuit under test along > with the measuring device's limits. > > ** > > ** Bob . . . > -- Mickey Coggins ________________________________________________________________________________
Date: Aug 05, 2012
From: Henador Titzoff <henador_titzoff(at)yahoo.com>
Subject: Re: Starter contactor leaking voltage
Eric, =0A =0AThis has nothing to do with aviation other than avionics are built with ICs.- I would just like to know how not=0A including the power supply tra ce from pin to circuitry allows the chip circuitry to work as advertised (d atasheet)?- I've never heard of a chip that worked=0A without intended po wer.- Since it was CMOS and CMOS is very =0Aconservative with power, did it somehow derive its power from IO =0Asignals? =0A =0AYou must be an Analog Devices kind of guy. -I worked at Teradyne for s everal years. It was a lot of fun riding the train to South Station every w eekday. Henador Titzoff --- On Sun, 8/5/12, Eric M. Jones wrote: From: Eric M. Jones <emjones(at)charter.net> Subject: AeroElectric-List: Re: Starter contactor leaking voltage Date: Sunday, August 5, 2012, 7:48 AM et> repost - - - - - - As others have mentioned, the problem is in how you use your to ols...like the voltmeter. - - - - - - Imagine that you have a voltmeter that is infinitely sensitive (infinite impedance). Now it will measure the battery voltage even thru an open switch. In fact, it will measure 500 volts between your belt buckle an d your shoe laces. And the top of your hat will be 1000 volts higher than t he soles of your New Balance sneakers. You can actually extract some tiny a mount of power this way. - - - - - - So meter impedance is not a lack of quality in a meter, it is a necessary and useful characteristic of the measuring device. And in a soli d state circuit (like a diode), there will almost always be a voltage on th e output that is similar to the input voltage even when the meter is off. A nd in fact the "leakage voltage" will not be able to light even the tiniest LED...so ignore it. - - - - - - I once designed a Cmos circuit where somebody (okay, me...) for got to add the power trace to the IC. Years later, an inquisitive technicia n, tracing an unrelated fault discovered it, but all the shipped product ha d worked just fine. - - - - - - So just don't make voltage measurements like this. - - - - - - See attached for a better way. - - - - - - -------- -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380088#380088 Attachments: http://forums.matronics.com//files/diode_test_745.pdf le, List Admin. ________________________________________________________________________________
Subject: Safe Wire Types
From: "jhausch" <jimhausch(at)gmail.com>
Date: Aug 05, 2012
Ran across this link. Did some searching here to see if posted previously, but that does not seem to be the case. Anyone's thoughts on this? http://www.vision.net.au/~apaterson/aviation/wire_types.htm Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380111#380111 ________________________________________________________________________________
Date: Aug 05, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Starter contactor leaking voltage
At 01:54 PM 8/5/2012, you wrote: >Joe, Eric, Bob, > >Thanks so much for the feedback - I tried the >lamp, and of course it did not light up. Also >used an older analog instrument, and it showed >no indication of voltage. Thanks to your help >and a bit of time reading up on impedance, I >have a better understanding what is happening >here. I'm really happy to have run across this >"problem" as it allowed me to learn some new stuff. Thanks again! > >Regards, >Mickey I've taken this posting to the List and fixed some syntax/spelling issues, converted to a pdf and posted it to AeroElectric.com article archives. The cleaned up document is available at: http://tinyurl.com/8oe5wbj Bob . . . ________________________________________________________________________________
From: Marvin Dorris Jr <medorrisjr(at)hotmail.com>
Subject: Safe Wire Types
Date: Aug 05, 2012
If you're building a new airplane=2C use TKT Boeing or maybe TKT Airbus. I f you have to fly in something older=2C or something that doesn't have thes e types of wire=2C and something happens=2C blame your aviation safety advi sor if you lose people. And I'm thinking of buying a 1960 Bonanza Debonair?????????? Best Regards to All=2C > Subject: AeroElectric-List: Safe Wire Types > From: jimhausch(at)gmail.com > Date: Sun=2C 5 Aug 2012 13:28:56 -0700 > To: aeroelectric-list(at)matronics.com > > > Ran across this link. Did some searching here to see if posted previously =2C but that does not seem to be the case. > > Anyone's thoughts on this? > http://www.vision.net.au/~apaterson/aviation/wire_types.htm > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=380111#380111 > > > > > > > =========== =========== =========== =========== > > > ________________________________________________________________________________
From: "Gary Baker" <ggbaker(at)zoominternet.net>
Subject: Avionics Seminar for Builders-Wadsworth, OH-September
8, 2012
Date: Aug 05, 2012
EAA Chapter 846 is pleased to announce that we will host an Avionics Seminar at Wadsworth Skypark Airport Saturday, Sept. 8, beginning at 8 am. This type of avionics program has never been offered in the Cleveland, OH, area and should help increase homebuilders' knowledge in this part of their build. Seating will be limited. Attendees will have the opportunity to meet representatives from Aerotronics, Inc., Garmin, Dynon, Grand Rapid Technologies, TruTrak, and Advanced Flight Systems. In a few cases, the owners of the companies will be attending. Hands-on demos will be available and short workshops will be held throughout the day. Pilots who are already flying and want to see the latest upgrades are also invited to attend. There might also be some pilots who did not build their RV, buying an experienced aircraft, and want a better understanding of all things electrical. This seminar should provide answers for everyone. Aerotronics will be awarding a headset to a lucky winner. Dynon will be giving away a D-1, their new portable EFIS, valued at more than $1,400! The other vendors might be kind enough to offer some sort of door prize as well. For more information and registration, please go to <http://www.846.eaachapter.org/avionicsseminar.htm> Avionics Seminar - Chapter 846. Let me know if you have any questions. Gary Baker President EAA Chapter 846 <http://www.846.eaachapter.org/> www.846.eaachapter.org/ Wadsworth, OH 330-321-6274 cid:image001.gif(at)01CC886A.15E9B350 ________________________________________________________________________________
Subject: Re: Starter contactor leaking voltage
From: "user9253" <fran4sew(at)banyanol.com>
Date: Aug 05, 2012
Many troubleshooters have come to the wrong conclusion when testing a circuit with a voltmeter without the circuit being loaded. The troubleshooter might think, "The voltmeter reads 12 volts. Therefore everything up to this point must be OK." Without a load, that hypothesis could be incorrect. No load means no current. No current means no voltage drop. So a voltmeter will read normal voltage even if there is unwanted high resistance in the circuit. The high resistance could be due to a bad switch or a loose connection or corrosion or whatever. Without current flowing through that resistance, there will be no voltage drop across it. A voltmeter could read normal voltage when no current is flowing in a problem circuit. Joe -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380131#380131 ________________________________________________________________________________
Date: Aug 05, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Safe Wire Types
At 03:28 PM 8/5/2012, you wrote: > >Ran across this link. Did some searching here to see if posted >previously, but that does not seem to be the case. > >Anyone's thoughts on this? >http://www.vision.net.au/~apaterson/aviation/wire_types.htm > > This tempest has been bubbling at various vapor-generation rates for decades . . . I'll begin by noting that there's no such thing as a 'safe' airplane . . . nor any other machine which operates in close proximity to people and other living creatures. Each one is simply a tool that offers certain risks associated with its construction and use. Every one of them, used or maintained carelessly will eat more than your lunch . . . There's little about the construction and operation of a OBAM aircraft to compare with an Air Transport category aircraft. The operation, maintenance, system complexities, and exposure to people-induced mishap have very little if anything in common. Mr. Paterson's heart is in the right place and he's privy to many facts surrounding the history of ATC aircraft. Yes, there have been a goodly number of incidents that had origins with electrically induced fires. How do these relate to your RV7 or even Lancair IVP? Air Transport category flight cycles in US number in tens of thousands per day with about 1.8 millions of souls arriving comfortably at their intended destination. The world wide figures would probably more than double that. What are the numbers of incidents of in-flight fire induced by electrical systems where the fire might have been avoided had the INSULATION been something different? There are many electrical systems issues that arise from damage by shipping containers in the hold, accumulation of lint from carpets and clothes in inaccessible places, drips from coffee makers in the galley and potty plumbing. Accumulation of hydraulic fluids, ingress of rainwater, splash from wheel wells, etc. etc. Those airplanes are operated to maximize revenue generating hours per day while our airplanes spend the overwhelming majority of their time parked. The ATC aircraft will experience more flight hours in a few months than your airplane will over it's lifetime . . . and be exposed to a thousand times more situations with a potential for mishap. Root cause of the majority of accidents in small aircraft do not originate with the electrical system at all . . . much less with the kind of insulation on the wires. There are thousands of airplanes flying with cotton covered rubber insulation popular in 1940, tens of thousands flying with nylon over PVC used for a couple decades worth of Cessna/Piper/ Beech production. Yet these less-than-exotic insulations go unnoticed for their alleged hazard . . . because they are very low risk. I've worked some issues on Hawkers originally certified with some exotic insulations that would arc-track and experienced some electrical events that did not precipitate a serious accident. I'm aware of no incidents involving electrical systems where Tefzel or pre-Tefzel insulation was a factor. In other words, I don't see the incident rates going down because the insulation on the wire is Part 25 qualified. Yes, people who are paid to worry are very good at their jobs. Some folks worry as a hobby or even out of a sense of civic duty. But none of these folks seem to put their work product into perspective for how it defines RISK. Even though there are thousands of airplanes flying with allegedly the worst possible insulation on their wires, what is the probability of any one planeload of folks is going to experience a bad day in the breaker box? There are conditions and forces in the overall flight system that contribute much greater factors to the grand equation that defines risk for failure to arrive comfortably at your intended destination. Further, the risk factors for leaking potty pipes and inattentive baggage handlers don't even figure into the grand equation for an RV. I cannot argue qualitatively with the assertions derived from a study of Mr. Patterson's data. I can refer to the performance history in things like King Airs and Beechjets . . . and my acquaintances who investigate accidents involving those kinds of aircraft. I suggest that probability of insulation failure of a Tefzel wire (or even PVC) is WAAaaayyyy out on some small branch of the system reliability matrix for your airplane. So far out that it's not worthy of investment for either capital or emotional resources. When I climb aboard a CJ and get a look at the cockpit crew who looks like they barely have to shave every day . . . or listen to the thumps and crashes coming from the baggage compartment, concerns for insulation on the ship's wiring do not even enter my mind. Bob . . . ________________________________________________________________________________
Date: Aug 05, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Safe Wire Types
At 05:37 PM 8/5/2012, you wrote: If you're building a new airplane, use TKT Boeing or maybe TKT Airbus. If you have to fly in something older, or something that doesn't have these types of wire, and something happens, blame your aviation safety advisor if you lose people. Hmmm . . . where does one purchase this wire? And I'm thinking of buying a 1960 Bonanza Debonair?????????? How about it ol' Bob. Would you recommend the wire bundles be stripped out and replaced? Bob . . . ________________________________________________________________________________
Date: Aug 06, 2012
Subject: Re: Safe Wire Types
From: Bob Verwey <bob.verwey(at)gmail.com>
Not Bob III, but if you want to replace the wiring in a Bonanza be prepared to strip the whole interior out. As a former A&P/IA, and current Bonanza owner, the only issue with the wiring in my opinion, might be some of the circuit breakers, switches and limit switches. On the Beech forum over the past ten years I don't recall seeing to many wiring issues that present a danger. The system might be regarded as old school, but it works! Bob Verwey IO 470 A35 Bonanza ZU-DLW On 6 August 2012 04:39, Robert L. Nuckolls, III < nuckolls.bob(at)aeroelectric.com> wrote: > nuckolls.bob(at)aeroelectric.com**> > > At 05:37 PM 8/5/2012, you wrote: > > If you're building a new airplane, use TKT Boeing or maybe TKT Airbus. If > you have to fly in something older, or something that doesn't have these > types of wire, and something happens, blame your aviation safety advisor if > you lose people. > > Hmmm . . . where does one purchase this wire? > > And I'm thinking of buying a 1960 Bonanza Debonair?????????? > > How about it ol' Bob. Would you recommend the wire > bundles be stripped out and replaced? > > > Bob . . . > > ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Aug 06, 2012
Subject: Re: Safe Wire Types
Good Morning Bob, Bob and All, I would not replace the wiring unless it showed evidence of unintended motion., but would carefully check all of the grounds and check for voltage drop across any suspect CBs and switches. Happy Skies, Old Bob PS Good to be able to meet you in RFD. Wish we could have talked a bit more. In a message dated 8/6/2012 3:44:31 A.M. Central Daylight Time, bob.verwey(at)gmail.com writes: And I'm thinking of buying a 1960 Bonanza Debonair?????????? How about it ol' Bob. Would you recommend the wire bundles be stripped out and replaced? Bob . . . ________________________________________________________________________________
Subject: Re: Safe Wire Types
From: "racerjerry" <gki(at)suffolk.lib.ny.us>
Date: Aug 06, 2012
I cannot argue with anything that has been said here; however, the real problem lies at the ends of the wire. If you hook up your new Taiwan audio gadget with 20 feet of 24 AWG and connect it to a convenient 30 amp circuit breaker, you could find yourself in a would of hurt if the device decides to short out. The breaker will never trip and the wire will become a smoke generator. Ask me how I know. Common hook-up wire purchased at your local electronics or auto parts store that has PVC insulation will get things over with quicker. Fortunately, my experience was in a service truck and not in a confined RV cockpit at altitude. By the time I could get the truck stopped at the side of the road, I was totally helpless and on the ground choking. -------- Jerry King Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380166#380166 ________________________________________________________________________________
Date: Aug 06, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Safe Wire Types
At 09:36 PM 8/5/2012, you wrote: At 03:28 PM 8/5/2012, you wrote: Ran across this link. Did some searching here to see if posted previously, but that does not seem to be the case. Anyone's thoughts on this? http://www.vision.net.au/~apaterson/aviation/wire_types.htm This tempest has been bubbling at various vapor-generation rates for decades . . . I've worked some issues on Hawkers originally certified with some exotic insulations that would arc-track and experienced some electrical events that did not precipitate a serious accident. I'm aware of no incidents involving electrical systems where Tefzel or pre-Tefzel insulation was a factor. In other words, I don't see the incident rates going down because the insulation on the wire is Part 25 qualified. I dug around in the archives and found some of my data and reports generated therefrom for the Hawker incidents cited. Emacs! Emacs! Note that damage to these bundles ORIGINATED with a single, small fault to ground. A contaminated crack or more probably, rubbed through by motion against the airframe. Note that this insulation is a tape WRAPPED around the wires and fused . . . not extruded as a contiguous amorphous sheath. Further, while these materials passed some form of qualification testing at the time the airplane was being designed, there was no investigation as to behaviors under excitation for temperatures produced by an electric arc that would trigger a previously unconsidered form of propagation for combustion . . . now called "arc tracking." A fault in a single wire propagated catastrophic damage to a bundle of wires (but did not set the airplane on fire). The answer for these airplanes is a new breaker (VERY expensive) that can detect both hard faults (shorts and overloads) and soft faults (arcing). Swissair 111 would probably not have suffered its fate had the faulted wire bundles not been routed adjacent to flammable insulation. Does anyone have flammable insulation in their RV? One cannot know the thinking behind selection of this wire 30+ years ago. The military and commercial aviation communities were wrestling with some perceived shortfalls in the insulation of choice for the era and the new kids on the block . . . Teflon and cousins showed a lot of promise. Some folks made some terrible, expensive choices. Don't know how many accidents were caused but I do know of entire fleets of military aircraft that were totally re-wired after carrier based versions contracted dandruff of the wire bundle and started shedding insulation in little flakes. I was working with the Gates-Piaggio GP-180 at the time Lear was looking hard at Tefzel. An export controlled product with strong military implications. I was ready to go with RayChem's Spec 55 wire with very nearly the same properties of Tefzel and not export controlled . . . but about 10-15% more expensive. We ultimately acquired the export license and the GP-180 was wired in Tefzel . . . and probably still is. If it's not wired in Tefzel, then the machine has probably fallen victim to knee-jerk reactions so common to bombardment by Chicken Little worriers without regard to assessment of real risk. Too many designers, regulators and decision makers for modern products are NOT cognizant of history nor are they capable of accurate consideration for magnitude of risk. Their charter is to drive all risks to zero no matter how much it costs. Instead they float with the tide of regulations and recommendations that flow from a constellation of agencies who are paid to worry . . . and worry they do. Present trends plotted into the future suggest that risks associated with all forms of transportation will be driven to ZERO. It's easy. Regulate those systems out of existence with constrictions of critical components like fuel, unattainable efficiency mandates, traffic flow boondoggles and yes . . . insulation on wires. Bob . . . ________________________________________________________________________________
Date: Aug 06, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Safe Wire Types
At 07:40 AM 8/6/2012, you wrote: I cannot argue with anything that has been said here; however, the real problem lies at the ends of the wire. If you hook up your new Taiwan audio gadget with 20 feet of 24 AWG and connect it to a =9Cconvenient=9D 30 amp circuit breaker, you could find yourself in a would of hurt if the device decides to short out. The breaker will never trip and the wire will become a smoke generator. Ask me how I know. Common hook-up wire purchased at your local electronics or auto parts store that has PVC insulation will get things over with quicker. Fortunately, my experience was in a service truck and not in a confined RV cockpit at altitude. By the time I could get the truck stopped at the side of the road, I was totally helpless and on the ground choking. -------- Jerry King Sure. This is why it's important not to loose sight of the whole system by getting distracted with features of one component. Breakers will do their job to keep a wire from burning ASSUMING it is properly sized to the task. Blaming the cloud of noxious smoke on PVC is rather far down the chain of events. I doubt that the wreckage of Swissair 111 produced THE wire that some have hypothesized to have ignited nearby insulation. The crew didn't succumb to a damaged wire that did not enjoy protection from soft faults, it was smoke that was a byproduct of another shortfall in selection and installation of materials. This report speaks to dozens of incidents involving "failures within the entertainment systems" http://tinyurl.com/d6rgttp but without implicating Tefzel failures as root cause. It was Paterson's statement: "Tefzel was found in Swiss Air flight SR111's Inflight Entertainment System (IFEN) which was suspected as being the cause of the inflight fire and subsequent crash of the aircraft off Nova Scotia in November 1998." Well duh . . . how does insulation on hookup wire figure into the failures within components of the in-flight entertainment system? Even if there WAS a faulted wire, had the poor choice of insulation not been present, the airplane might have simply suffered wire bundle damage like the Hawkers. The lessons to be studied here go to the notion that all accidents are propagated on a string of conditions that follow a triggering event. It's useful to consider the cost-benefit-risk- ratios for eliminating the triggering event but foolish to not include contributing conditions as well. All of these accidents would have been stopped by breaking the chain anywhere. If the Swissair 111 incident had not ended sadly, this statement from Airbus would have been humorous: "Airbus spokeswoman Mary Anne Greczyn says the company has rigorous standards for entertainment and other aircraft systems. Airbus provides extra protection on entertainment system wiring by using sleeves and other materials, she says." Protection of wires using sleeves . . . what's up with that? Are the entertainment system wires worthy of special attention not enjoyed by the rest of the wiring in the airplane? Had the folks who first smelled the impending failures been old TV technicians, perhaps their learned sense of smell would have identified first- failure as a capacitor, a resistor or burning ECB material. At no place in any article have I found that Tefzel wire . . . or any other wire is directly responsible for triggering this incident. Yet we see statements like . . . The aviation industry has been grappling for years with problems of cracked and deteriorated wiring causing fires and emergency landings, he says. Adding four miles of entertainment system wire to a jet that may have more than 100 miles of other wires is "like throwing gas on a fire." Lacey believes planes are safer without the systems. "We could choose to do without fancy entertainment systems," he says. "A good book works for me." Fine examples of Chicken Little journalism and arm-chair, bureaucratic accident analysis. I've not seen any direct evidence that this incident (or dozens of others) would have been prevented by replacing the Tefzel wire . . . Tens of thousands of airplanes are flying with PVC insulated wires . . . many of which are fed by appropriately sized breakers that performed as advertised and opened up without so much as melting the insulation much less setting it on fire. Bob . . . ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: Safe Wire Types
Date: Aug 06, 2012
Total waste of time to try and even acquire much less use that wire on a small piston single plane. Wires in our planes are not carrying high Hz AC voltage like the heavy iron I used to work with. As Bob has said repeatedly, stick with regular Tefzel and you'll be golden. Yes there is that one guy that has the one website that has been out there forever written by a person with subjective personal and political motivation, and some of the info is dubious (some of it is outright conjecture) to begin with and also much of it doesn't apply to systems in our planes. Just because someone put something on a webpage somewhere sometime and claims to be an expert does not make it so. Stick with what works well for your installation and don't try to turn your plane into a Boeing! Just my 2 cents as usual. Cheers, Stein From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Marvin Dorris Jr Sent: Sunday, August 05, 2012 5:38 PM Subject: RE: AeroElectric-List: Safe Wire Types If you're building a new airplane, use TKT Boeing or maybe TKT Airbus. If you have to fly in something older, or something that doesn't have these types of wire, and something happens, blame your aviation safety advisor if you lose people. And I'm thinking of buying a 1960 Bonanza Debonair?????????? Best Regards to All, > Subject: AeroElectric-List: Safe Wire Types > From: jimhausch(at)gmail.com > Date: Sun, 5 Aug 2012 13:28:56 -0700 > To: aeroelectric-list(at)matronics.com > > > Ran across this link. Did some searching here to see if posted previously, but that does not seem to be the case. > > Anyone's thoughts on this? > http://www.vision.net.au/~apaterson/aviation/wire_types.htm > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=380111#380111 > > > > > > >============= > > > ________________________________________________________________________________
Date: Aug 06, 2012
From: cardinalnsb <cardinalnsb(at)aol.com>
Subject: wire safety
When I got my 1968 Cardinal, I considered "rewiring" with "new stuff", assuming the "old stuff Cessna used" was inferior. My (deceased) friend looked at it and laughed at me. He said it was fine (not burned or cracked, pliable, etc.), and the problems I would create by the rewiring greatly outweighed his assessment of any deficiency in the wiring. He started in the business fixing mismatched wiring looms in new B52's, avionics install type work in military aircraft, set the nuclear fuses in fighter bombers ("go down to the end of the runway and when you come back we will send the pilot down to fly out"), and ended with a top secret conning tower clearance in ballistic missile subs as field engineer. I figured he knew a lot about safe wire, so I just kept the old Cessna wiring... Skip Simpson ________________________________________________________________________________
Subject: Re: Safe Wire Types
From: "jhausch" <jimhausch(at)gmail.com>
Date: Aug 07, 2012
THis has been very informative. Thanks to all who have replied. I expected folks to say Tefzel was AOK, but did not expect to see good comments about PVC. Again, thanks. very interesting to read (and learn) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380258#380258 ________________________________________________________________________________
Subject: Faulty troubleshooting
From: "user9253" <fran4sew(at)banyanol.com>
Date: Aug 07, 2012
I had recently commented about erroneous troubleshooting techniques. Then I made the same mistake myself. While working on an aviation project in my workshop, I had wires temporarily connected with dabs of solder or alligator clips. Then everything quit working. I tested the 5 VDC bus and it measured 12 volts! Oh no, I thought the 7805 voltage regulator shorted out and ruined my expensive 5-volt components with 12 volts. I removed the 7805 voltage regulator from the circuit board and tested it. There was nothing wrong with it. So I soldered it back in place and turned the power on. This time everything worked fine. Hmm, why weren't the 5-volt parts fried when 12 volts were applied? And where did that 12 volts come from? I checked the PC Board traces for solder bridges, but there were none. Later I realized what must have happened. The negative power supply wire to the circuit board must have had a bad connection. So the board was not even powered up. No wonder nothing worked. So why did my digital volt meter measure 12 volts on the 5-volt bus? Because the meter has high input impedance, it was able to measure the minute voltage leaking through the 7805 voltage regulator. By the way, the voltmeter common lead was connected to the negative supply upstream of the bad connection. This situation is very similar to the diode test that Eric Jones described with a battery and diode and voltmeter all connected in series. Joe -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380330#380330 ________________________________________________________________________________
From: Deems Herring <dsleepy47(at)hotmail.com>
Subject: HUD for GA aircraft
Date: Aug 07, 2012
This: http://www.virtualhud.com/VirtualHud/VirtualHUD.aspx might be better for single engine tractor planes. Deems Date: Mon=2C 30 Jul 2012 22:09:28 +0100 From: peter(at)sportingaero.com Subject: Re: AeroElectric-List: HUD for GA aircraft The big deal about HUDs is that they are focused at infinity with some fancy (heavy) optics. That way you look out the window and everything is in focus=2C ________________________________________________________________________________
From: "Jeff Luckey" <JLuckey(at)pacbell.net>
Subject: How to Select a Scope
Date: Aug 09, 2012
I've been considering purchasing an oscilloscope for hobby/trouble-shooting use. It's been 30+ years since I've fiddled with scopes. I'm looking for counseling/guidance/recommendations. Some things I want to do: 1. Analyze the output of the crank angle sensor in my car - (currently having some starting problems, but I digress) 2. I like to program micro-controllers and would like to do trouble-shooting & analysis 3. Look at the wave-forms produced by an alternator 4. Get the best bang for the buck Questions: 1. I see devises advertised that are combo oscilloscope & logic analyzer. Are these as cool as they appear? 2. How do I decide which frequency range I need? (It seems the higher the MHz rating of a device the higher the cost) Most of the micro-controllers that I work with are clocked around 4 MHz. I once heard that the rating of the scope should be 10x the signal you want to analyze. Is that true? 3. What other criteria should I consider? As always TIA, I look forward to learning something Jeff Luckey ________________________________________________________________________________
Subject: Re: How to Select a Scope
From: Normand Biron <normbiron(at)msn.com>
Date: Aug 09, 2012
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From: Daniel Hooper <enginerdy(at)gmail.com>
Subject: Re: How to Select a Scope
Date: Aug 09, 2012
I have one of these: http://www.tequipment.net/RigolDS1102E.html It's "good" -- it's a pretty good scope for $400. Digital, storage, USB image and data capture, RS-232/USB computer control port. You can also get a DS1052E for $350 if you want to drop down to 50MHz bandwidth for $50 less. I ended up getting the scope case for $50 as well. There are definitely some glitches and usability hitches every now and then, but overall it's great for the money. But, if I had tons of money to blow, I'd definitely get an Agilent Infiniivision scope. For the microcontroller work, you're going to get a lot more productivity mileage out of a Saleae Logic: http://www.saleae.com/logic For $150 not only will it capture 8 channels in parallel, but you can also assign channels to be decoded inline. Many serial formats are supported out of the box. For digital work, I highly recommend it. It will not read any analog inputs, however, so you'd need a scope for that -- but getting that kind of serial decoding in a scope tends to be expensive. Good luck! --Daniel On Aug 9, 2012, at 3:02 PM, Jeff Luckey wrote: > I=92ve been considering purchasing an oscilloscope for hobby/trouble-shooting use. It=92s been 30+ years since I=92ve fiddled with scopes. I=92m looking for counseling/guidance/recommendations. > > Some things I want to do: > > Analyze the output of the crank angle sensor in my car ' (currently having some starting problems, but I digress) > I like to program micro-controllers and would like to do trouble-shooting & analysis > Look at the wave-forms produced by an alternator > Get the best bang for the buck > > > Questions: > I see devises advertised that are combo oscilloscope & logic analyzer. Are these as cool as they appear? > How do I decide which frequency range I need? (It seems the higher the MHz rating of a device the higher the cost) Most of the micro-controllers that I work with are clocked around 4 MHz. I once heard that the rating of the scope should be 10x the signal you want to analyze. Is that true? > What other criteria should I consider? > > As always TIA, I look forward to learning something > > Jeff Luckey > > > > > ________________________________________________________________________________
Subject: B&C 505-1
From: "chris Sinfield" <chris_sinfield(at)yahoo.com.au>
Date: Aug 10, 2012
Hi All I bought ages ago a PM/OV Filter and OV Protection Kit (14v) that I intended to fit to my Jab 3300. Now I have come to the fitting end and wonder if it is still the right part for my Single Phase Jab 20 AMP PM?? as the wiring shows it for a 3 Phase one.. Can someone confirm if this is the correct kit for my new jab? from their site This 14 volt kit provides crucial over-voltage protection to our permanent magnet alternator (BC433-H) and others rated at 30 amps or below. Comes with a clear-yellow warning light that will illuminate if the crowbar over-voltage protection module is tripped (or when the alternator switch is left off), and a filter capacitor to reduce radio noise and enhance regulation. Thanks Chris Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380623#380623 ________________________________________________________________________________
From: Michael Burbidge <mburbidg(at)gmail.com>
Subject: Attaching "uninsulated ring terminals" to 4 awg wire...
Date: Aug 10, 2012
I'm using the "uninsulated ring terminals" for 4 awg wire from the contractors to my bus and alternator. Are the terminals sold by B&C meant to be crimped or soldered? If crimped where can I get a crimper big enough to handle 4 awg. B&C only sells ones that handle up to 10 awg wire. Thanks, Michael- ________________________________________________________________________________
From: Robert Borger <rlborger(at)mac.com>
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire...
Date: Aug 10, 2012
Michael, Harbor Freight has a hydraulic crimper that does the job. http://www.harborfreight.com/hydraulic-wire-crimping-tool-66150.html Best regards, Robert Borger, President Geowhiziks & Doodlebugging, Inc. Certified Petroleum Geophysicist AAPG#101 3705 Lynchburg Dr. Corinth, TX 76208-5331 (H) 940-497-2123 (C) 817-992-1117 Sent from my iPad On Aug 10, 2012, at 20:30, Michael Burbidge wrote: I'm using the "uninsulated ring terminals" for 4 awg wire from the contractors to my bus and alternator. Are the terminals sold by B&C meant to be crimped or soldered? If crimped where can I get a crimper big enough to handle 4 awg. B&C only sells ones that handle up to 10 awg wire. Thanks, Michael- ________________________________________________________________________________
From: <berkut13(at)berkut13.com>
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire...
Date: Aug 10, 2012
Works great, but do NOT go by the wire size markings on the various crimping dies...they are WAY off the mark. (or at least were on my unit) -James -----Original Message----- From: Robert Borger Sent: Friday, August 10, 2012 9:48 PM Subject: Re: AeroElectric-List: Attaching "uninsulated ring terminals" to 4 awg wire... Michael, Harbor Freight has a hydraulic crimper that does the job. http://www.harborfreight.com/hydraulic-wire-crimping-tool-66150.html Best regards, Robert Borger, President Geowhiziks & Doodlebugging, Inc. Certified Petroleum Geophysicist AAPG#101 3705 Lynchburg Dr. Corinth, TX 76208-5331 (H) 940-497-2123 (C) 817-992-1117 Sent from my iPad On Aug 10, 2012, at 20:30, Michael Burbidge wrote: I'm using the "uninsulated ring terminals" for 4 awg wire from the contractors to my bus and alternator. Are the terminals sold by B&C meant to be crimped or soldered? If crimped where can I get a crimper big enough to handle 4 awg. B&C only sells ones that handle up to 10 awg wire. Thanks, Michael- ________________________________________________________________________________
Date: Aug 11, 2012
From: Glen Matejcek <aerobubba(at)earthlink.net>
Subject: Attaching "uninsulated ring terminals" to 4 awg wire...
Hi Michael- I went to a local welding supply house to have them do it. The guy there pointed out he'd have to charge me $10 per crimp, and for the same 10 bucks I could by a hammer-driven die. It's about 2" x 3" x 5", IIRC, is conceptually similar to a cigar tip cutting guillotine (whatever you actually call those things), will crimp terminals to any of the really fat wires, and mounts to a bench, bumper, or in a vise. You could probably use it sitting on concrete, but that would be a little gutsy. Put the wire end ass'y into the device, whack it with a small sledge a few times (until the built-in gauge says you're done) and you're all set. Dirt simple, very effective, and about the cheapest airplane tool I've ever bought. >Subject: AeroElectric-List: Attaching "uninsulated ring terminals" to 4 awg wire... >I'm using the "uninsulated ring terminals" for 4 awg wire from the contractors >to my bus and alternator. Are the terminals sold by B&C meant to be crimped or >soldered? If crimped where can I get a crimper big enough to handle 4 awg. B&C >only sells ones that handle up to 10 awg wire. Glen Matejcek ________________________________________________________________________________
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire...
From: Jared Yates <email(at)jaredyates.com>
Date: Aug 11, 2012
I've got one of those wack-types that I'd like to get rid of. I wasn't happy with the results, but perhaps someone else coudl do better. I anyone is in the market for one, send me a note. On Aug 11, 2012, at 6:24, Glen Matejcek wrote: > > Hi Michael- > > I went to a local welding supply house to have them do it. The guy there pointed out he'd have to charge me $10 per crimp, and for the same 10 bucks I could by a hammer-driven die. It's about 2" x 3" x 5", IIRC, is conceptually similar to a cigar tip cutting guillotine (whatever you actually call those things), will crimp terminals to any of the really fat wires, and mounts to a bench, bumper, or in a vise. You could probably use it sitting on concrete, but that would be a little gutsy. > > Put the wire end ass'y into the device, whack it with a small sledge a few times (until the built-in gauge says you're done) and you're all set. Dirt simple, very effective, and about the cheapest airplane tool I've ever bought. > > > >> Subject: AeroElectric-List: Attaching "uninsulated ring terminals" to 4 awg wire... > > >> I'm using the "uninsulated ring terminals" for 4 awg wire from the contractors >> to my bus and alternator. Are the terminals sold by B&C meant to be crimped or >> soldered? If crimped where can I get a crimper big enough to handle 4 awg. B&C >> only sells ones that handle up to 10 awg wire. > > > Glen Matejcek > > > > ________________________________________________________________________________
Date: Aug 11, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire... At 09:30 PM 8/10/2012, you wrote: > >I'm using the "uninsulated ring terminals" for 4 awg wire from the >contractors to my bus and alternator. Are the terminals sold by B&C >meant to be crimped or soldered? If crimped where can I get a >crimper big enough to handle 4 awg. B&C only sells ones that handle >up to 10 awg wire. > >Thanks, >Michael- Crimp tools for the larger terminals are pretty pricey. Further, most airplanes will need only a handful of large terminals. Consider soldering un-insulated terminals and dressing out with heat shrink. See: http://tinyurl.com/9pbvky8 Bob . . . ________________________________________________________________________________
Date: Aug 11, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire... At 06:05 AM 8/11/2012, you wrote: > >I've got one of those wack-types that I'd like to get rid of. I >wasn't happy with the results, but perhaps someone else coudl do >better. I anyone is in the market for one, send me a note. The problem with beat-n-bash crimpers is lack of verification for having achieved a gas-tight joint. See: http://tinyurl.com/8vk6sxc http://tinyurl.com/93yweyd Without vetting the marriage of wire-to-terminal-to-tool, the easiest way to maximize copper in the wire grip is to stuff wire-wedges into the matrix and then fill all voids with free-flow of an electronic grade 63/37 solder. Works good, lasts a long time. Bob . . . ________________________________________________________________________________
Date: Aug 11, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: B&C 505-1
At 07:58 PM 8/10/2012, you wrote: Hi All I bought ages ago a PM/OV Filter and OV Protection Kit (14v) that I intended to fit to my Jab 3300. Now I have come to the fitting end and wonder if it is still the right part for my Single Phase Jab 20 AMP PM?? as the wiring shows it for a 3 Phase one.. Can someone confirm if this is the correct kit for my new jab? From their site: This 14 volt kit provides crucial over-voltage protection to our permanent magnet alternator (BC433-H) and others rated at 30 amps or below. Comes with a clear-yellow warning light that will illuminate if the crowbar over-voltage protection module is tripped (or when the alternator switch is left off), and a filter capacitor to reduce radio noise and enhance regulation. Thanks Chris This kit is applicable to any PM alternator. Bob . . . ________________________________________________________________________________
Date: Aug 11, 2012
From: Bill Watson <Mauledriver(at)nc.rr.com>
Subject: Re: Attaching "uninsulated ring terminals" to 4
awg wire... I soldered the 4 or 5 big wire terminals in my project and it all worked very well per Bob's tutorial below. In particular, the stuffing of the barrel with copper wedges was a key detail. Did mine with a 25 year old Weller soldering gun. Bill On 8/11/2012 8:24 AM, Robert L. Nuckolls, III wrote: > > > At 09:30 PM 8/10/2012, you wrote: >> >> >> I'm using the "uninsulated ring terminals" for 4 awg wire from the >> contractors to my bus and alternator. Are the terminals sold by B&C >> meant to be crimped or soldered? If crimped where can I get a crimper >> big enough to handle 4 awg. B&C only sells ones that handle up to 10 >> awg wire. >> >> Thanks, >> Michael- > > Crimp tools for the larger terminals are > pretty pricey. Further, most airplanes will > need only a handful of large terminals. Consider > soldering un-insulated terminals and dressing > out with heat shrink. See: > > http://tinyurl.com/9pbvky8 > > > Bob . . . > > > ----- > No virus found in this message. > Checked by AVG - www.avg.com > > ________________________________________________________________________________
Subject: Re: B&C 505-1
From: "chris Sinfield" <chris_sinfield(at)yahoo.com.au>
Date: Aug 11, 2012
Thanks Bob. I got abut worried when I realised it also was for a 3 phase system. Chris Read this topic online here: http://forums.matronics.com/viewtopic.php?p=380681#380681 ________________________________________________________________________________
Date: Aug 11, 2012
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire...
From: Richard Girard <aslsa.rng(at)gmail.com>
The wire size markings on the Harbor Freight crimper are not only mismarked but the make a crappy crimp when you do get them to sort of work. With Amp #4 solder on terminals I have had success with the "G" (5/32") Nico sleeve swager on my GCMP (1/16 to 5/32) tool. I hit it three times the same way I would a Nico sleeve so that there is a slight bubble between each and it worked great. Afterward I used three brushed on coats of enamel paint to seal everything up followed by glue lined heat shrink tubing (your basic belt and suspenders approach). Four years and no sign of corrosion on the open end. On Fri, Aug 10, 2012 at 9:58 PM, wrote: > > Works great, but do NOT go by the wire size markings on the various > crimping dies...they are WAY off the mark. (or at least were on my unit) > -James > > -----Original Message----- From: Robert Borger > Sent: Friday, August 10, 2012 9:48 PM > To: aeroelectric-list(at)matronics.**com > Subject: Re: AeroElectric-List: Attaching "uninsulated ring terminals" to > 4 awg wire... > > > Michael, > > Harbor Freight has a hydraulic crimper that does the job. > > http://www.harborfreight.com/**hydraulic-wire-crimping-tool-**66150.html> > > Best regards, > Robert Borger, President > Geowhiziks & Doodlebugging, Inc. > Certified Petroleum Geophysicist AAPG#101 > 3705 Lynchburg Dr. > Corinth, TX 76208-5331 > (H) 940-497-2123 > (C) 817-992-1117 > > Sent from my iPad > > On Aug 10, 2012, at 20:30, Michael Burbidge wrote: > > mburbidg(at)gmail.com> > > I'm using the "uninsulated ring terminals" for 4 awg wire from the > contractors to my bus and alternator. Are the terminals sold by B&C meant > to be crimped or soldered? If crimped where can I get a crimper big enough > to handle 4 awg. B&C only sells ones that handle up to 10 awg wire. > > Thanks, > Michael- > > -- Zulu Delta Mk IIIC Thanks, Homer GBYM It isn't necessary to have relatives in Kansas City in order to be unhappy. - Groucho Marx ________________________________________________________________________________
Date: Aug 11, 2012
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire...
From: Richard Girard <aslsa.rng(at)gmail.com>
Didn't mean to be rude, our 19 year old cat stepped on the keyboard and sent the post for me. Rick Girard On Sat, Aug 11, 2012 at 5:42 PM, Richard Girard wrote: > The wire size markings on the Harbor Freight crimper are not only > mismarked but the make a crappy crimp when you do get them to sort of work. > With Amp #4 solder on terminals I have had success with the "G" (5/32") > Nico sleeve swager on my GCMP (1/16 to 5/32) tool. I hit it three times the > same way I would a Nico sleeve so that there is a slight bubble between > each and it worked great. Afterward I used three brushed on coats of enamel > paint to seal everything up followed by glue lined heat shrink tubing (your > basic belt and suspenders approach). Four years and no sign of corrosion on > the open end. > > > On Fri, Aug 10, 2012 at 9:58 PM, wrote: > >> >> Works great, but do NOT go by the wire size markings on the various >> crimping dies...they are WAY off the mark. (or at least were on my unit) >> -James >> >> -----Original Message----- From: Robert Borger >> Sent: Friday, August 10, 2012 9:48 PM >> To: aeroelectric-list(at)matronics.**com >> Subject: Re: AeroElectric-List: Attaching "uninsulated ring terminals" to >> 4 awg wire... >> >> >> >> Michael, >> >> Harbor Freight has a hydraulic crimper that does the job. >> >>
http://www.harborfreight.com/**hydraulic-wire-crimping-tool-**66150.html> >> >> Best regards, >> Robert Borger, President >> Geowhiziks & Doodlebugging, Inc. >> Certified Petroleum Geophysicist AAPG#101 >> 3705 Lynchburg Dr. >> Corinth, TX 76208-5331 >> (H) 940-497-2123 >> (C) 817-992-1117 >> >> Sent from my iPad >> >> On Aug 10, 2012, at 20:30, Michael Burbidge wrote: >> >> mburbidg(at)gmail.com> >> >> I'm using the "uninsulated ring terminals" for 4 awg wire from the >> contractors to my bus and alternator. Are the terminals sold by B&C meant >> to be crimped or soldered? If crimped where can I get a crimper big enough >> to handle 4 awg. B&C only sells ones that handle up to 10 awg wire. >> >> Thanks, >> Michael- >> >> >> >> >> >> >> >> >> > > > -- > Zulu Delta > Mk IIIC > Thanks, Homer GBYM > > It isn't necessary to have relatives in Kansas City in order to be unhappy. > - Groucho Marx > > -- Zulu Delta Mk IIIC Thanks, Homer GBYM It isn't necessary to have relatives in Kansas City in order to be unhappy. - Groucho Marx ________________________________________________________________________________
Date: Aug 11, 2012
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire...
From: Richard Girard <aslsa.rng(at)gmail.com>
Okay, I caught my own mistake, the "G" swager is the 1/16", the "P" is the 5/32". Rick On Sat, Aug 11, 2012 at 5:44 PM, Richard Girard wrote: > Didn't mean to be rude, our 19 year old cat stepped on the keyboard and > sent the post for me. > > Rick Girard > > > On Sat, Aug 11, 2012 at 5:42 PM, Richard Girard wrote: > >> The wire size markings on the Harbor Freight crimper are not only >> mismarked but the make a crappy crimp when you do get them to sort of work. >> With Amp #4 solder on terminals I have had success with the "G" (5/32") >> Nico sleeve swager on my GCMP (1/16 to 5/32) tool. I hit it three times the >> same way I would a Nico sleeve so that there is a slight bubble between >> each and it worked great. Afterward I used three brushed on coats of enamel >> paint to seal everything up followed by glue lined heat shrink tubing (your >> basic belt and suspenders approach). Four years and no sign of corrosion on >> the open end. >> >> >> On Fri, Aug 10, 2012 at 9:58 PM, wrote: >> >>> >>> Works great, but do NOT go by the wire size markings on the various >>> crimping dies...they are WAY off the mark. (or at least were on my unit) >>> -James >>> >>> -----Original Message----- From: Robert Borger >>> Sent: Friday, August 10, 2012 9:48 PM >>> To: aeroelectric-list(at)matronics.**com >>> Subject: Re: AeroElectric-List: Attaching "uninsulated ring terminals" >>> to 4 awg wire... >>> >>> >>> > >>> >>> Michael, >>> >>> Harbor Freight has a hydraulic crimper that does the job. >>> >>>
http://www.harborfreight.com/**hydraulic-wire-crimping-tool-**66150.html> >>> >>> Best regards, >>> Robert Borger, President >>> Geowhiziks & Doodlebugging, Inc. >>> Certified Petroleum Geophysicist AAPG#101 >>> 3705 Lynchburg Dr. >>> Corinth, TX 76208-5331 >>> (H) 940-497-2123 >>> (C) 817-992-1117 >>> >>> Sent from my iPad >>> >>> On Aug 10, 2012, at 20:30, Michael Burbidge wrote: >>> >>> mburbidg(at)gmail.com> >>> >>> I'm using the "uninsulated ring terminals" for 4 awg wire from the >>> contractors to my bus and alternator. Are the terminals sold by B&C meant >>> to be crimped or soldered? If crimped where can I get a crimper big enough >>> to handle 4 awg. B&C only sells ones that handle up to 10 awg wire. >>> >>> Thanks, >>> Michael- >>> >>> >>> >>> >>> >>> >>> >>> >>> >> >> >> -- >> Zulu Delta >> Mk IIIC >> Thanks, Homer GBYM >> >> It isn't necessary to have relatives in Kansas City in order to be >> unhappy. >> - Groucho Marx >> >> >> > > > -- > Zulu Delta > Mk IIIC > Thanks, Homer GBYM > > It isn't necessary to have relatives in Kansas City in order to be unhappy. > - Groucho Marx > > -- Zulu Delta Mk IIIC Thanks, Homer GBYM It isn't necessary to have relatives in Kansas City in order to be unhappy. - Groucho Marx ________________________________________________________________________________
Date: Aug 11, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Attaching "uninsulated ring terminals" to
4 awg wire... At 05:16 PM 8/11/2012, you wrote: > >Greetings, > >I know crimp and then solder is frowned upon as unnecessary. I was >wondering if there was a problem with crimping with a whack-type, to >tighten up the strands in the terminal(instead of wedging) and then >soldering. Seems less fussy if you already have the beat-n-bash >crimper, or if you have several to do. Can't imagine any 'problem' . . . just curious as to your lack of confidence in a demonstrably known process. Crimps properly installed are good for the lifetime of the airplane. So are soldered joints. I suppose there's some confidence to be gained if your soldering or crimping skills are questionable. It seems more practical to become good at one if not both processes. I own a drawer full of crimp tools and perhaps a half dozen different soldering systems. This gives me broad options for many combinations of wire, terminal and tool. But to use both techniques on a single installation adds no value unless you're unsure about either process. Getting good at one or both is always better than "stacking" processes because you are not-so-good at either. Would you run a line of screws and nuts down the edge of a wing skin because you were not so good at setting rivets? Bob . . . ________________________________________________________________________________
Date: Aug 12, 2012
From: rayj <raymondj(at)frontiernet.net>
Subject: Re: Attaching "uninsulated ring terminals" to
4 awg wire... Greetings, I wasn't describing stacking processes. I was suggesting that the process of "wedging" might be replaced by compressing the components together with a "whack-n-bash" tool. It would avoid the - find the wire - find the sharpening tool - strip - sharpen - drive - nip - process of wedging. Seems quicker and at least as repeatable as "wedging", if it doesn't introduce additional issues I'm not considering. Just wondering out loud. Thanks, Raymond Julian Kettle River, MN. "And you know that I could have me a million more friends, and all I'd have to lose is my point of view." - John Prine On 08/11/2012 11:03 PM, Robert L. Nuckolls, III wrote: > > > At 05:16 PM 8/11/2012, you wrote: >> >> Greetings, >> >> I know crimp and then solder is frowned upon as unnecessary. I was >> wondering if there was a problem with crimping with a whack-type, to >> tighten up the strands in the terminal(instead of wedging) and then >> soldering. Seems less fussy if you already have the beat-n-bash >> crimper, or if you have several to do. > > Can't imagine any 'problem' . . . just > curious as to your lack of confidence in > a demonstrably known process. Crimps properly > installed are good for the lifetime of the airplane. > So are soldered joints. I suppose there's > some confidence to be gained if your soldering > or crimping skills are questionable. > > It seems more practical to become good at > one if not both processes. I own a drawer full > of crimp tools and perhaps a half dozen different > soldering systems. This gives me broad options > for many combinations of wire, terminal and tool. > > But to use both techniques on a single installation > adds no value unless you're unsure about either > process. Getting good at one or both is always > better than "stacking" processes because you are > not-so-good at either. > > Would you run a line of screws and nuts down the > edge of a wing skin because you were not so good > at setting rivets? > > > Bob . . . > > ________________________________________________________________________________
Date: Aug 13, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Attaching "uninsulated ring terminals" to
4 awg wire... At 02:41 PM 8/12/2012, you wrote: > >Greetings, > >I wasn't describing stacking processes. > >I was suggesting that the process of "wedging" might be replaced by >compressing the components together with a "whack-n-bash" tool. It >would avoid the - find the wire - find the sharpening tool - strip - >sharpen - drive - nip - process of wedging. Hmmm . . . understand. Yes, anything you do to minimize voids in the wire grip before soldering is a good thing to do. If copper 'wedging' is unattractive then reducing the cross section of the terminal barrel is another option. The wire for wedges is pretty easy. Most hardware stores will sell 14/2+ground house wire by the foot. Buy one foot and you'll have 3 feet of wedge material. It's pvc insulation and comes off easy with a pocket knife. I get sharp ends by cutting the pieces with the tool as close to parallel with the wire as it will permit. Pushing the wedges in can be done with the same pair of wire cutters. The last one will need to be driven . . . I use the wire cutter for that too. Bob . . . ________________________________________________________________________________
From: "Stuart Hutchison" <stuart(at)stuarthutchison.com.au>
Subject: Attaching "uninsulated ring terminals" to 4 awg
wire...
Date: Aug 13, 2012
Hi guys, I haven't read all the posts on this thread ... please forgive me if I'm covering old ground. Not everyone's cup-o-tea, but you can make dies like this too. Just cut two bits of the same steel bar to length, hold them together in a vice, drill a big hole at the join from the top in one direction and a small hole from the side. Smooth the end of a rod or pin punch and there you have it, a decent die you can hold in the vice that will retain the shape of your terminal as you crimp away the void, prior to solder and heatshrink. Cheers, Stu ________________________________________________________________________________
Date: Aug 13, 2012
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire...
From: James Kilford <james(at)etravel.org>
> Consider soldering un-insulated terminals and dressing out with heat shrink. I did my large wires with this method, and it worked very well. The blowtorch makes a bit of a mess of the insulation near the terminals, but that gets covered up neatly by heatshrink. James On 11 August 2012 13:24, Robert L. Nuckolls, III < nuckolls.bob(at)aeroelectric.com> wrote: > nuckolls.bob(at)aeroelectric.com**> > > At 09:30 PM 8/10/2012, you wrote: > >> mburbidg(at)gmail.com> >> >> >> I'm using the "uninsulated ring terminals" for 4 awg wire from the >> contractors to my bus and alternator. Are the terminals sold by B&C meant >> to be crimped or soldered? If crimped where can I get a crimper big enough >> to handle 4 awg. B&C only sells ones that handle up to 10 awg wire. >> >> Thanks, >> Michael- >> > > Crimp tools for the larger terminals are > pretty pricey. Further, most airplanes will > need only a handful of large terminals. Consider > soldering un-insulated terminals and dressing > out with heat shrink. See: > >
http://tinyurl.com/9pbvky8 > > > Bob . . . > > ________________________________________________________________________________
Date: Aug 13, 2012
From: Glen Matejcek <aerobubba(at)earthlink.net>
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
wire... You betcha. Instead of all those other steps that invariably eat up $time$, just insert, whack whack, and solder away. It might not sound like much of a deal, but with my dual battery, all-electric airplane, there are 12 such terminals IIRC. As far as making a gas tight joint without solder goes, it seems to be a no-brainer with the tool I have. It takes a couple moderately heavy blows with a 2 1/2 pound sledge to compress it to the gauge depth. Considering the gauge of the materials in the wire and terminal as well as the design of the die, it's hard to imagine how a reasaonable man could over do it and do damage. I tried just to see what would happen, and it seems about all you can do is some sort of gross alignment error that would be quite obvious. Of course, this is also an industrial tool that the welding shop uses to fabricate the cables they sell to professional welders. I suspect that given the duty cycle and environment involved in that application, I will be hard pressed to have a problem with my installation. I did solder my connections as a means of sealing the end of the wire, just because. Heat shrink covers the barrel and bridges to the insulation. One tip: If your cable will need to bend close to the terminal, put that bend in when you attach the terminal. I works wonders- Also, life is easier if you remember to slip the heat shrink over the cable prior to affixing the terminal... you may wonder how I know that! FWIW, YMMV... >Greetings, > >I wasn't describing stacking processes. > >I was suggesting that the process of "wedging" might be replaced by >compressing the components together with a "whack-n-bash" tool. It would >avoid the - find the wire - find the sharpening tool - strip - sharpen - >drive - nip - process of wedging. > >Seems quicker and at least as repeatable as "wedging", if it doesn't >introduce additional issues I'm not considering. > >Just wondering out loud. > >Thanks, >Raymond Julian >Kettle River, MN. Glen Matejcek Glen Matejcek ________________________________________________________________________________
Date: Aug 13, 2012
From: D L Josephson <dlj04(at)josephson.com>
Subject: Re: Attaching "uninsulated ring terminals" to 4
awg Perhaps I'm just being dense, but why not just get the appropriate sized uninsulated ring terminal for the wire you want to use rather than stuffing with more copper? If you want to solder a #4 wire, a #6 or maybe #8 crimp terminal would probably be the right size for a snug fit. You can also make your own, using soft copper refrigeration tubing -- whatever best fits the wire, squeezed flat (in a press if necessary) and drilled at the end. ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: Which 55-60 amp alternator
Date: Aug 13, 2012
Bob, Assuming that in order to end up with an externally regulated 55-60 amp alternator, I will probably have to modify an IR model, which alternator should I buy to start with. I want the fans to turn the correct direction (CCW when viewed at the pulley) for use on a lycoming. I don't want to pay the big bucks for a B&C unit and don't mind doing the work to convert it. Bevan ________________________________________________________________________________
Date: Aug 13, 2012
Subject: Re: Attaching "uninsulated ring terminals" to 4 awg
From: Jared Yates <email(at)jaredyates.com>
I used a Dremel to cut a slot in the barrel, then pinched the slot closed and soldered. I found that I was able to solder successfully without getting the wire anywhere near hot enough to melt the insulation, so if that's a problem I'd suggest trying less heat. Here are some pictures, down about half way: http://jaredyates.com/bearhawk/?p=988 On Mon, Aug 13, 2012 at 1:51 PM, D L Josephson wrote: > > Perhaps I'm just being dense, but why not just get the appropriate sized > uninsulated ring terminal for the wire you want to use rather than stuffing > with more copper? If you want to solder a #4 wire, a #6 or maybe #8 crimp > terminal would probably be the right size for a snug fit. You can also make > your own, using soft copper refrigeration tubing -- whatever best fits the > wire, squeezed flat (in a press if necessary) and drilled at the end. > > ________________________________________________________________________________
Date: Aug 14, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Which 55-60 amp alternator
At 01:23 PM 8/13/2012, you wrote: Bob, Assuming that in order to end up with an externally regulated 55-60 amp alternator, I will probably have to modify an IR model, which alternator should I buy to start with. I'm not sufficiently familiar with the choices to advise you confidently. It would seem that the driving constraint is purely mechanical. Research the parts available to bolt it to the engine including any changes to the stock pulley. Unless you're willing to tackle mechanical integration issues along with electrical, you'd probably want to limit you search to frames already supported by off-the-shelf attach hardware. I want the fans to turn the correct direction (CCW when viewed at the pulley) for use on a lycoming. That used to be a 'thing' to consider with external fans with blades optimized for direction of rotation. [] Modern alternators have internal fans with little if any 'sculpturing' of the blades [] Rotating an alternator 'backwards' in an airplane is unlikely to pose any problems. First, you're exceedingly unlikely to stress your alternator in a manner that produces maximum rated internal heating. The cooling environment under the hood of a car is MUCH worse than under the cowl of your airplane. Further, you're going to be spinning the alternator much faster than the original application design point . . . cooling is not a big issue. I don't want to pay the big bucks for a B&C unit and don't mind doing the work to convert it. You can run it internally regulated . . . you could do a mod similar to that offered by Plane Power for crowbar ov protection and external control of field power. Bob . . . ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: Which 55-60 amp alternator
Date: Aug 14, 2012
Thanks Bob, The online alternator vendors don't supply data such as mounting bracket dimensions, pulley diameter etc. they just say it fit a particular make and model car. Can I assume that a 12V 60 amp Denso alternator has the same mounting dimensions as the 60 amp Plane Power that Vans sells? I'm not sufficiently familiar with the choices to advise you confidently. It would seem that the driving constraint is purely mechanical. Research the parts available to bolt it to the engine including any changes to the stock pulley. Fair enough. Anyone have any experience with this? I've already wired the plane for external control and crowbar as I agree with the philosophy. So I would like to keep it this way. Nothing lasts for ever. So my theory is to buy two alternators online for the price of one B & C or Plane power. Mod them both for external control and one will be then be a spare. :) Unless you're willing to tackle mechanical integration issues along with electrical, you'd probably want to limit you search to frames already supported by off-the-shelf attach hardware. Exactly. Still need top know the dimensional data. Anyone have a Vans, B&C, Plane Power 60amp that it will to measure the mounting bracket boss? That used to be a 'thing' to consider with external fans with blades optimized for direction of rotation. [] Modern alternators have internal fans with little if any 'sculpturing' of the blades [] Rotating an alternator 'backwards' in an airplane is unlikely to pose any problems. First, you're exceedingly unlikely to stress your alternator in a manner that produces maximum rated internal heating. The cooling environment under the hood of a car is MUCH worse than under the cowl of your airplane. Further, you're going to be spinning the alternator much faster than the original application design point . . . cooling is not a big issue. OK, makes sense. I will not be concerned with direction of fans. You can run it internally regulated . . . you could do a mod similar to that offered by Plane Power for crowbar ov protection and external control of field power. I'm confused by the above statement. Does that not make it externally controlled or is there a variation on a theme here? Is there a document that describes the PP mod? Bevan ________________________________________________________________________________
From: Jack Haviland <jghrv6a(at)gmail.com>
Subject: Cooling Low Current Alternators
Date: Aug 15, 2012
Sometime ago, Van's Aircraft sold 30 - 35 amp rebuilt Honda Civic alternators (14184) with the normal fan deleted since it would rotate the wrong way on a Lycoming. They no longer sell them but "remanufactured" 14184 alternators with a fan (and a "lifetime warranty") are readily available from Auto Zone. Is it preferable to remove the fan or leave it on? Same question for the capacitor that is on the Auto Zone unit. When installed on an O-320 D1A, the aft end of the alternator is very close to the No. 1 cylinder exhaust pipe. I'll be installing a shield to try to keep the rectifier diodes cool (along with the blast tube I originally installed). Comments from those who have experience with these low current alternators would be appreciated. JGH RV6A w/ 100 hours ________________________________________________________________________________
Date: Aug 15, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Which 55-60 amp alternator
You can run it internally regulated . . . you could do a mod similar to that offered by Plane Power for crowbar ov protection and external control of field power. I'm confused by the above statement. Does that not make it externally controlled or is there a variation on a theme here? Is there a document that describes the PP mod? Let's make a distinction between internally and externally REGULATED . . . which speaks to the location of the electronics that exercises dynamic control of field current for the purpose of maintaining desired bus voltage. Then there's a legacy design goal for any-time, any-conditions control of alternator function by the pilot. Referring you to an exemplar schematic for an internally regulated alternator . . . http://tinyurl.com/8a9uuns the pathway in green shows how energy from the battery makes it through a controlling device (in this case, an N-channel FET) to the alternator field. Note that both CONTROL and WARNING functions (red) attach to electronics within the regulator's circuitry. If something in that circuitry fails or the FET shorts, then full battery voltage is applied to the field, regulation control is lost and you have an over-voltage condition. There's been a great deal of discussion in the past as to the suitability of internally regulated alternators on airplanes. I have always maintained that I could not recommend the use of IR alternators because they could not offer the legacy any-time, any-condition control by the pilot -OR- an ov protection system in their off-the-shelf configuration. B&C's solution to the problem was to remove the built in regulator and offer an external alternator control system that included the functional trinity for alternator management: Regulation, OV management, LV warning. Plane power went a different route and simply broke the field supply path inside the alternator and brought it out so that absolute, any-time any conditions control was available to the pilot -AND- ov protection could be easily implemented. In this case, Plane Power elected to go with the crowbar ov protection technique pioneered in aircraft by yours truly. The concept was slated to go onto the Beech 38P http://tinyurl.com/7smb4k5 Unfortunately, that program never made it to the production line. The last time I saw N336BA, the fuselage was sitting outside Burt Rutan's hangar at Mojave. http://tinyurl.com/cj3n24a Since that time, crowbar ov protection has be successfully applied to thousands of installations in dozens of aircraft. If you want to convert an off-the-shelf alternator to your use while embracing the legacy design goals for engine driven power sources, you have the option of doing the B&C thingy or the Plane-Power thingy . . . either one works good and lasts a long time. I'm aware of no article which describes the PP modification. It's difficult even to find local alternator repair shops that could assist in making the modifications . . . although it's usually pretty simple to figure out once the alternator is cracked open. There have been some articles that described total bypassing of the internal regulator for going the B&C approach . . . but I don't enjoy ready recall for those documents. Perhaps somebody on the List has a broader insight to your quest. Bob . . . ________________________________________________________________________________
From: "Roger & Jean Curtis" <mrspudandcompany(at)verizon.net>
Subject: Which 55-60 amp alternator
Date: Aug 15, 2012
There have been some articles that described total bypassing of the internal regulator for going the B&C approach . . . but I don't enjoy ready recall for those documents. Perhaps somebody on the List has a broader insight to your quest. Bob . . . Here is an article published by EAA for conversion of an internal regulated to external regulated alternator. http://www.eaa.org/experimenter/articles/2009-09_howto_alternator.asp Roger ________________________________________________________________________________
From: "Valovich, Paul" <pvalovich(at)dcscorp.com>
Subject: Don't Want to Pay BigBucks for B&C
Date: Aug 15, 2012
I went through the same debate in choosing an alternator. Finally decided t hat you really do get what you pay for and went with B&C. No regrets - outstanding performance and customer service. I have a continually updated mental list of things that might go wrong in f light based on how my plane is currently performing. Alternator worries are n't very high on the list (I used Bob's Z13/8 architecture with a B&C SD8 b ackup). Paul ValovicRV-8A N192NM 235 hours ________________________________________________________________________________
Date: Aug 15, 2012
From: Steve Stearns <steve(at)tomasara.com>
Subject: Re: AeroElectric-List Digest: 2 Msgs - 08/14/12
Bevan, Here's an option that might be a fit for you. See if you have a an old-timer auto electric guy with a good reputation in your area. If so, you can go to a local junk yard and buy a used older externally-regulated alternator (40A to 60A) for not much money and confirm how well it fits. If it fits well, take it to the local auto-electric guy and have him test and, if necessary, rebuild it for you. My LongEZ has an old 40A Toyota alternator that, when I got the airplane, was fried (not to mention the previous owner had apparently crudely tried to fix it). I took it in the local auto electric old-timer and, upon looking at it, gave me a sly grin and said "What kind of race car this come out of?". To which I replied somewhat guiltily (knowing not to mention anything to do with aircraft if you want the services of reasonable priced people), "it's off of a custom off-road trike...". "What engine you got in it?" "It's a four cylinder horizontally opposed, kind a like a Volkswagen...". He did a beautiful job rebuilding it and it's worked great ever since. Steve Stearns Boulder/Longmont, Colorado CSA,EAA,IAC,AOPA,PE,ARRL,BARC (but ignorant none-the-less) Restoring (since 1/07) and flying again (8/11!): N45FC O235 Longeze Cothern/Friling CF1 (~1000 Hrs) Flying (since 9/86): N43732 A65 Taylorcraft BC12D On 8/15/2012 12:56 AM, AeroElectric-List Digest Server wrote: > RE: AeroElectric-List: Which 55-60 amp alternator ________________________________________________________________________________
From: <longg(at)pjm.com>
Subject: Don't Want to Pay BigBucks for B&C
Date: Aug 15, 2012
I agree, quality almost always pays for itself. I also use the Z13/8 and it's been great. I've never had to go to backup but it's always nice knowing it's there. Glenn Long -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Valovich, Paul Sent: Wednesday, August 15, 2012 10:01 AM Subject: AeroElectric-List: Don't Want to Pay BigBucks for B&C I went through the same debate in choosing an alternator. Finally decided that you really do get what you pay for and went with B&C. No regrets - outstanding performance and customer service. I have a continually updated mental list of things that might go wrong in flight based on how my plane is currently performing. Alternator worries aren't very high on the list (I used Bob's Z13/8 architecture with a B&C SD8 backup). Paul ValovicRV-8A N192NM 235 hours ________________________________________________________________________________
Date: Aug 15, 2012
Subject: Re: Don't Want to Pay BigBucks for B&C
From: Jared Yates <email(at)jaredyates.com>
One time I politely asked the gentleman from B&C why his oil filter adapter was so much more expensive than the others, and he pointed out that while he doesn't strive to have the lowest price, he does believe that he provides the best value. The theory is that you can buy one of his products instead of two or three of the cheap ones, and save money in the end. It sounded like a good argument to me, though I didn't buy his alternator. I got one from Plane Power instead, and from ACS it was around $350 for the whole package. That seemed like good economy compared to trying to sort out the crowbar protection and brackets for the Autozone version. I'm not flying yet, so it may take a few hundred hours to see if the Plane Power decision ends up saving money over the B&C. Compared to the auto parts store option, I know I've already saved money over spending a few days trying to cut and bend 1/4" steel brackets and opening up the back of the alternator to get the wires fixed. On Wed, Aug 15, 2012 at 10:24 AM, wrote: > > I agree, quality almost always pays for itself. I also use the Z13/8 and it's been great. I've never had to go to backup but it's always nice knowing it's there. > > Glenn Long > > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Valovich, Paul > Sent: Wednesday, August 15, 2012 10:01 AM > To: aeroelectric-list(at)matronics.com > Subject: AeroElectric-List: Don't Want to Pay BigBucks for B&C > > I went through the same debate in choosing an alternator. Finally decided that you really do get what you pay for and went with B&C. > > No regrets - outstanding performance and customer service. > > I have a continually updated mental list of things that might go wrong in flight based on how my plane is currently performing. Alternator worries aren't very high on the list (I used Bob's Z13/8 architecture with a B&C SD8 backup). > Paul ValovicRV-8A N192NM > 235 hours > > ________________________________________________________________________________
Date: Aug 15, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Which 55-60 amp alternator
At 08:56 AM 8/15/2012, you wrote: >There have been some articles that described > total bypassing of the internal regulator for going > the B&C approach . . . but I don't enjoy ready > recall for those documents. Perhaps somebody on > the List has a broader insight to your quest. > > > Bob . . . > >Here is an article published by EAA > >for conversion of an internal regulated > >to external regulated alternator. > > ><http://www.eaa.org/experimenter/articles/2009-09_howto_alternator.asp>http://www.eaa.org/experimenter/articles/2009-09_howto_alternator.asp Cool! I'd not seen that particular article. Thanks for heads-up. A very good article that needed only a few minor corrections. I've captured the article and mirrored it with comments at: http://tinyurl.com/crte9xe Bob . . . ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: Which 55-60 amp alternator
Date: Aug 15, 2012
Thanks everyone, we're getting very close here. It is still unclear to me which 60 amp ND alternator to start with that will fit the Van's mounting bracket (Boss mount?). What have other done? Bevan _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Roger & Jean Curtis Sent: Wednesday, August 15, 2012 6:57 AM Subject: RE: AeroElectric-List: Which 55-60 amp alternator There have been some articles that described total bypassing of the internal regulator for going the B&C approach . . . but I don't enjoy ready recall for those documents. Perhaps somebody on the List has a broader insight to your quest. Bob . . . Here is an article published by EAA for conversion of an internal regulated to external regulated alternator. http://www.eaa.org/experimenter/articles/2009-09_howto_alternator.asp Roger ________________________________________________________________________________
Date: Aug 15, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Which 55-60 amp alternator
At 11:50 AM 8/15/2012, you wrote: >Thanks everyone, we're getting very close here. > >It is still unclear to me which 60 amp ND alternator to start with >that will fit the Van's mounting bracket (Boss mount?). What have other done? > >Bevan > Here's a wild @#S guess. Here's a Lester #14935 that fits 85-88 Tercels. Emacs! Oriley's offers this one for about $100. It's frame geometry appears the same as the B&C L-60 and others popular with the OBAM aviation market. http://tinyurl.com/8vfkj66 If you've got the mount, you could go down to the local parts store and fit check the alternator with the mount and measure the offset from boss-mount bolt holes to the pulley centerline. Of course, you need to find a new pulley too. Bob . . . ________________________________________________________________________________
Date: Aug 15, 2012
From: Bill Settle <billsettle(at)bellsouth.net>
Subject: Which Crimp Tool
I just purchased a nav light which came with metal pins for 22 awg wire as part of an AMP-3SK connector kit. Can someone please direct me to the proper crimper I need for this task? Thanks, Bill Settle RV-8 Winston-Salem, NC ________________________________________________________________________________
Date: Aug 16, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Which Crimp Tool
At 05:24 PM 8/15/2012, you wrote: >I just purchased a nav light which came with metal pins for 22 awg >wire as part of an AMP-3SK connector kit. Can someone please direct >me to the proper crimper I need for this task? http://tinyurl.com/9m5mvfy http://tinyurl.com/9c444zm Bob . . . ________________________________________________________________________________
Date: Aug 16, 2012
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Mooney Alternator woes
My hangar neighbor is trying to figure out why his alternator occasionally drops off line - requiring a weird reset sequence. He has to shut off the battery and field, then go to a low power setting and bring it back up again. Something about resetting an overvoltage protection device. It is an M20S with Cont 550 and gear driven alternator. The first regulator lasted only a couple of years before giving up the ghost and the replacement was a special from Mooney. My first line of thinking is to locate the regulator and test it. Nobody knows where it is hiding. (I'm in DC - the plane is in DE...I'll be home next weekend to help more.) Meanwhile, does anyone have an electronic copy of the Light Plane Maintenance article on troubleshooting alternators...and the Mooney M20S maintenance manual? If we can find it, I'm hoping that we can determine if the regulator is the culprit. Thanks in advance, Ralph RV6A N822AR in N06 - waiting for my engine/prop to come back from overhaul after being hit by a flying hangar door! ________________________________________________________________________________
Date: Aug 16, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Mooney Alternator woes
At 08:27 AM 8/16/2012, you wrote: My hangar neighbor is trying to figure out why his alternator occasionally drops off line - requiring a weird reset sequence. He has to shut off the battery and field, then go to a low power setting and bring it back up again. Something about resetting an overvoltage protection device. It is an M20S with Cont 550 and gear driven alternator. The first regulator lasted only a couple of years before giving up the ghost and the replacement was a special from Mooney. My first line of thinking is to locate the regulator and test it. Nobody knows where it is hiding. (I'm in DC - the plane is in DE...I'll be home next weekend to help more.) Meanwhile, does anyone have an electronic copy of the Light Plane Maintenance article on troubleshooting alternators...and the Mooney M20S maintenance manual? If we can find it, I'm hoping that we can determine if the regulator is the culprit. If it takes a southern Slobovian switch-dance to bring it back on line, it's almost certain to be something electronic. Is the successful reset sequence something different than what is called for in the POH as a response to an OV trip? I've not had any contact with Mooney in 25+ years. I bid an alternator controller for them while at Electro-Mech . . . we didn't get the job. I think Electrodelta out of White Oak, TX got it. It would have been a Mooney-unique product. ED has changed hands and/or moved several times over the years. The guy who ran ED is still hanging around the Wichita area. He MIGHT be a resource for help wrestling with your problem. The LPM article is not likely to be much help. It will be VERY generic. If it were my airplane, I'd jeep another regulator in place of the original to see if the problem goes away. Given the rarity of that regulator, I'd probably go for a one-time STC to install something more contemporary and available. There's nothing magic about alternator controllers . . . only the institutionalized and market driven B.S. in which they reside. B&C regulators are used elsewhere on current production airplanes . . . the FAA might look kindly upon substitution of B&C product for what's already installed. Bob . . . ________________________________________________________________________________
Date: Aug 16, 2012
From: Kelly McMullen <kellym(at)aviating.com>
Subject: Re: Mooney Alternator woes
There are a couple Mooney email lists that have experts that likely can help, including factory tech support. The S model isn't all that old, so there should be good info available. Mapalist mailing list..which requires membership in MAPA. Mapalist(at)lists.mooneypilots.com http://lists.mooneypilots.com/listinfo.cgi/mapalist-mooneypilots.com <http://lists.mooneypilots.com/listinfo.cgi/mapalist-mooneypilots.com> Mooney Tech list which is open to all: http://lists.aviating.com/mailman/listinfo/mooney-tech, mailto:mooney-tech-request(at)aviating.com?subject=subscribe On 8/16/2012 6:44 AM, Robert L. Nuckolls, III wrote: > > > At 08:27 AM 8/16/2012, you wrote: > > > My hangar neighbor is trying to figure out why his alternator > occasionally drops off line - requiring a weird reset sequence. He has > to shut off the battery and field, then go to a low power setting and > bring it back up again. Something about resetting an overvoltage > protection device. > > It is an M20S with Cont 550 and gear driven alternator. The first > regulator lasted only a couple of years before giving up the ghost and > the replacement was a special from Mooney. > > My first line of thinking is to locate the regulator and test it. > Nobody knows where it is hiding. > (I'm in DC - the plane is in DE...I'll be home next weekend to help > more.) > > Meanwhile, does anyone have an electronic copy of the Light Plane > Maintenance article on troubleshooting alternators...and the Mooney > M20S maintenance manual? > > If we can find it, I'm hoping that we can determine if the regulator > is the culprit. > > If it takes a southern Slobovian switch-dance to > bring it back on line, it's almost certain to be > something electronic. Is the successful reset sequence > something different than what is called for in the > POH as a response to an OV trip? > > I've not had any contact with Mooney in 25+ years. I > bid an alternator controller for them while at > Electro-Mech . . . we didn't get the job. I think > Electrodelta out of White Oak, TX got it. It would > have been a Mooney-unique product. ED has changed > hands and/or moved several times over the years. > The guy who ran ED is still hanging around the > Wichita area. He MIGHT be a resource for help > wrestling with your problem. > > The LPM article is not likely to be much help. It > will be VERY generic. If it were my airplane, I'd > jeep another regulator in place of the original to > see if the problem goes away. Given the rarity of > that regulator, I'd probably go for a one-time > STC to install something more contemporary and > available. There's nothing magic about alternator > controllers . . . only the institutionalized and > market driven B.S. in which they reside. > > B&C regulators are used elsewhere on current production > airplanes . . . the FAA might look kindly upon > substitution of B&C product for what's already > installed. > > > Bob . . . > > ----- No virus found in this message. Checked by AVG - www.avg.com ________________________________________________________________________________
Date: Aug 16, 2012
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: Mooney Alternator woes
Thanks - first step is find the installed regulator. I could probably sub-in the B&C one from my 6A on a temp basis to see if it works - that'll be a good starting place...good idea. I'll ask about the reset sequence to see if it is in the POH. -----Original Message----- >From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> >Sent: Aug 16, 2012 9:44 AM >To: aeroelectric-list(at)matronics.com >Subject: Re: AeroElectric-List: Mooney Alternator woes > > >At 08:27 AM 8/16/2012, you wrote: > > >My hangar neighbor is trying to figure out why his alternator >occasionally drops off line - requiring a weird reset sequence. He >has to shut off the battery and field, then go to a low power setting >and bring it back up again. Something about resetting an overvoltage >protection device. > >It is an M20S with Cont 550 and gear driven alternator. The first >regulator lasted only a couple of years before giving up the ghost >and the replacement was a special from Mooney. > >My first line of thinking is to locate the regulator and test >it. Nobody knows where it is hiding. >(I'm in DC - the plane is in DE...I'll be home next weekend to help more.) > >Meanwhile, does anyone have an electronic copy of the Light Plane >Maintenance article on troubleshooting alternators...and the Mooney >M20S maintenance manual? > >If we can find it, I'm hoping that we can determine if the regulator >is the culprit. > > If it takes a southern Slobovian switch-dance to > bring it back on line, it's almost certain to be > something electronic. Is the successful reset sequence > something different than what is called for in the > POH as a response to an OV trip? > > I've not had any contact with Mooney in 25+ years. I > bid an alternator controller for them while at > Electro-Mech . . . we didn't get the job. I think > Electrodelta out of White Oak, TX got it. It would > have been a Mooney-unique product. ED has changed > hands and/or moved several times over the years. > The guy who ran ED is still hanging around the > Wichita area. He MIGHT be a resource for help > wrestling with your problem. > > The LPM article is not likely to be much help. It > will be VERY generic. If it were my airplane, I'd > jeep another regulator in place of the original to > see if the problem goes away. Given the rarity of > that regulator, I'd probably go for a one-time > STC to install something more contemporary and > available. There's nothing magic about alternator > controllers . . . only the institutionalized and > market driven B.S. in which they reside. > > B&C regulators are used elsewhere on current production > airplanes . . . the FAA might look kindly upon > substitution of B&C product for what's already > installed. > > > Bob . . . > > ________________________________________________________________________________
Date: Aug 16, 2012
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: Mooney Alternator woes
Thanks - we'll sign up for them as a resource. -----Original Message----- >From: Kelly McMullen <kellym(at)aviating.com> >Sent: Aug 16, 2012 9:54 AM >To: aeroelectric-list(at)matronics.com >Subject: Re: AeroElectric-List: Mooney Alternator woes > > >There are a couple Mooney email lists that have experts that likely can >help, including factory tech support. The S model isn't all that old, so >there should be good info available. >Mapalist mailing list..which requires membership in MAPA. >Mapalist(at)lists.mooneypilots.com >http://lists.mooneypilots.com/listinfo.cgi/mapalist-mooneypilots.com ><http://lists.mooneypilots.com/listinfo.cgi/mapalist-mooneypilots.com> > >Mooney Tech list which is open to all: >http://lists.aviating.com/mailman/listinfo/mooney-tech, >mailto:mooney-tech-request(at)aviating.com?subject=subscribe > >On 8/16/2012 6:44 AM, Robert L. Nuckolls, III wrote: >> >> >> At 08:27 AM 8/16/2012, you wrote: >> >> >> My hangar neighbor is trying to figure out why his alternator >> occasionally drops off line - requiring a weird reset sequence. He has >> to shut off the battery and field, then go to a low power setting and >> bring it back up again. Something about resetting an overvoltage >> protection device. >> >> It is an M20S with Cont 550 and gear driven alternator. The first >> regulator lasted only a couple of years before giving up the ghost and >> the replacement was a special from Mooney. >> >> My first line of thinking is to locate the regulator and test it. >> Nobody knows where it is hiding. >> (I'm in DC - the plane is in DE...I'll be home next weekend to help >> more.) >> >> Meanwhile, does anyone have an electronic copy of the Light Plane >> Maintenance article on troubleshooting alternators...and the Mooney >> M20S maintenance manual? >> >> If we can find it, I'm hoping that we can determine if the regulator >> is the culprit. >> >> If it takes a southern Slobovian switch-dance to >> bring it back on line, it's almost certain to be >> something electronic. Is the successful reset sequence >> something different than what is called for in the >> POH as a response to an OV trip? >> >> I've not had any contact with Mooney in 25+ years. I >> bid an alternator controller for them while at >> Electro-Mech . . . we didn't get the job. I think >> Electrodelta out of White Oak, TX got it. It would >> have been a Mooney-unique product. ED has changed >> hands and/or moved several times over the years. >> The guy who ran ED is still hanging around the >> Wichita area. He MIGHT be a resource for help >> wrestling with your problem. >> >> The LPM article is not likely to be much help. It >> will be VERY generic. If it were my airplane, I'd >> jeep another regulator in place of the original to >> see if the problem goes away. Given the rarity of >> that regulator, I'd probably go for a one-time >> STC to install something more contemporary and >> available. There's nothing magic about alternator >> controllers . . . only the institutionalized and >> market driven B.S. in which they reside. >> >> B&C regulators are used elsewhere on current production >> airplanes . . . the FAA might look kindly upon >> substitution of B&C product for what's already >> installed. >> >> >> >> Bob . . . >> >> >> >> > > >----- >No virus found in this message. >Checked by AVG - www.avg.com > > ________________________________________________________________________________
Date: Aug 16, 2012
Subject: Shorai Battery Review
From: Christopher Cee Stone <rv8iator(at)gmail.com>
Bob et al, These Shorai batteries are gaining market share in the motorcycle sphere. Still only anecdotal info as to their safety, longevity and failure modes. That being said, at 25% of the weight of AGM lead batteries for the same capacity they offer real advancement in energy storage. As the numbers in service increase in the ground transport market more experiential data should become available. Chris Stone RV-8 Newberg, OR ** ** ** ** ** ** ________________________________________________________________________________
Subject: Should battery be charged with a higher voltage?
From: "user9253" <fran4sew(at)banyanol.com>
Date: Aug 16, 2012
An RV-12 owner recently asked a question on VansAirforce about the charging voltage for the Odyssey PC680 battery. It seems that all of the voltage regulators that come with the Rotax 912 are factory set at 13.6 - 13.8 volts. The regulators are sealed; thus no adjustment is possible. This RV-12 owner wanted to know if the battery should be charged with a higher voltage. So I did some testing. I charged up my PC680, and then disconnected the battery charger on Tuesday. On Wednesday I measured the battery voltage with no load. My cheap meter read 13.01 volts and my Fluke read 13.09 volts. Then I went flying, did some touch & goes and gave a couple of rides. A total of 1.75 hours accumulated on the Hobbs and the engine was started a total of 6 times during the day. The starter uses very little power because the engine starts with only one revolution of the prop. The longest flight was about 30 minutes. At cruise, the Dynon D-180 indicated the normal 13.6 volts (which is 0.2 less than what my handheld voltmeter reads.) The next day, Thursday, I measured the no-load PC680 voltage: my cheap meter read 12.98 and the Fluke read 13.06 volts. The Odyssey Owner's Manual http://www.odysseybattery.com/documents/US-ODY-OM-010_0412.pdf says that the battery is 100 percent fully charged when the open circuit voltage is 12.84 or higher. Since my battery voltage is above 12.84, I have come to the conclusion that the Rotax voltage regulator setting of 13.6 - 13.8 is adequate for normal operations. If the battery is ever discharged for some reason, I intend to fully charge it before flying. Have I come to the correct conclusion about the regulator setting? Joe -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=381033#381033 ________________________________________________________________________________
From: "John MacCallum" <john.maccallum(at)bigpond.com>
Subject: Shorai Battery Review
Date: Aug 17, 2012
They certainly look and sound the part but Lithium Batteries are prone to catching fire that is why there is a prohibition on transporting Them in the holds of Aircraft. The other thing to mention is that such a light battery will alter your C of G position so you would need to re-do your weight and balance Chart. So maybe more info and a bit more testing or time may be required to establish their safety.. Cheers John MacCallum VH-DUU RV 10 # 41016 From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Christopher Cee Stone Sent: Friday, 17 August 2012 12:42 AM Subject: AeroElectric-List: Shorai Battery Review Bob et al, These Shorai batteries are gaining market share in the motorcycle sphere. Still only anecdotal info as to their safety, longevity and failure modes. That being said, at 25% of the weight of AGM lead batteries for the same capacity they offer real advancement in energy storage. As the numbers in service increase in the ground transport market more experiential data should become available. Chris Stone RV-8 Newberg, OR ________________________________________________________________________________
From: "John & Sue Dehnert" <bankshire(at)harboursat.com.au>
Subject: Schumacher 1562a
Date: Aug 17, 2012
Hi all have an off subject question, will the Schumacher 1562a charger maintainer available on Amazon work on the Australian voltage of 240v ac, Schumacher specifications state input voltage 110-140v ac. Thanks for any input on the subject . John ________________________________________________________________________________
From: Robert Borger <rlborger(at)mac.com>
Subject: Re: Schumacher 1562a
Date: Aug 16, 2012
John, Probably not without a step-down transformer/voltage converter. If you can't find a charger-maintainer for your 240v world, you can find voltage converters on Amazon or E-Bay. Best regards, Robert Borger, President Geowhiziks & Doodlebugging, Inc. Certified Petroleum Geophysicist AAPG#101 3705 Lynchburg Dr. Corinth, TX 76208-5331 (H) 940-497-2123 (C) 817-992-1117 Sent from my iPad On Aug 16, 2012, at 18:55, John & Sue Dehnert wrote: Hi all have an off subject question, will the Schumacher 1562a charger maintainer available on Amazon work on the Australian voltage of 240v ac, Schumacher specifications state input voltage 110-140v ac. Thanks for any input on the subject . John ________________________________________________________________________________
From: Bob McCallum <robert.mccallum2(at)sympatico.ca>
Subject: Schumacher 1562a
Date: Aug 16, 2012
John; The international version is model SC1200A, spec sheet attached. (I hope) Couldn't find a quick source or price, but this is a similar charger other than the input is 120-240VAC 50/60Hz The 1562a is 120VAC 60Hz only. Bob McC _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of John & Sue Dehnert Sent: Thursday, August 16, 2012 8:55 PM Subject: AeroElectric-List: Schumacher 1562a Hi all have an off subject question, will the Schumacher 1562a charger maintainer available on Amazon work on the Australian voltage of 240v ac, Schumacher specifications state input voltage 110-140v ac. Thanks for any input on the subject . John ________________________________________________________________________________
Date: Aug 16, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Shorai Battery Review
At 09:41 AM 8/16/2012, you wrote: >Bob et al, > >These Shorai batteries are gaining market share in the motorcycle >sphere. Still only anecdotal info as to their safety, longevity and >failure modes. > >That being said, at 25% of the weight of AGM lead batteries for the >same capacity they offer real advancement in energy storage. > >As the numbers in service increase in the ground transport market >more experiential data should become available. They are certainly impressive in terms of performance but not yet ready for prime time in the TC aircraft world. Check the List archives for 5/10 to 5/15 of last year and the term "lithium battery". Cessna spent a bucket of money on a Li-FePOH battery STC and had 50+ airplanes in the field when they experienced a ramp fire on one of the lithium installations. I'd like to run one in a car . . . or motorcycle but I don't think I'd put one in an airplane yet. Bob . . . ________________________________________________________________________________
Date: Aug 16, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Should battery be charged with a higher voltage?
> > Have I come to the correct conclusion about the regulator setting? >Joe Yes. A SVLA battery will always charge to 100% of capacity with a 13.6 to 13.8 volt bus. The reason bus voltages are set higher is to shorten a cycle time for recharge after a deep discharge. But if you always take off with a very lightly taxed battery then the lower set point is fine. Bob . . . ________________________________________________________________________________
Date: Aug 17, 2012
Subject: Re: Should battery be charged with a higher voltage?
From: rparigor(at)suffolk.lib.ny.us
Hi Joe I have a Rotax 914 not yet flying. I am going to raise the effective set-point on my Ducati regulator to make my Odyssey PC545 battery a little happier. Add a diode: http://www.europaowners.org/main.php?g2_itemId545 Read the manual on Odyssey: http://www.odysseybatteries.com/files.htm Click documentation, you will see that a little higher is desirable. Ron P. ________________________________________________________________________________
Subject: Re: Should battery be charged with a higher voltage?
From: "user9253" <fran4sew(at)banyanol.com>
Date: Aug 17, 2012
Bob, Thanks for your words of wisdom. To Ron P, I could not find any reference to a diode on EuropaOwners.org. But I assume that the diode is inserted in the regulator sense wire. I had thought about doing that, but voltage measurements indicate that my battery is kept fully charged with the 13.6 volt regulator set-point. The charging instructions in the Oddyssey manual http://www.odysseybatteries.com/files/US-ODY-TM-001_0411_000.pdf pertain to a discharged battery. Since my PC680 battery never gets discharged, the Continuous Float Charge voltage of 13.6 is adequate. I appreciate your input. Joe -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=381060#381060 ________________________________________________________________________________
From: Bob McCallum <robert.mccallum2(at)sympatico.ca>
Subject: Re: Should battery be charged with a higher voltage?
Date: Aug 17, 2012
Even if it were to be somewhat discharged it would still fully charge at th e 13.6 volt setting=2C it would just take longer to do so assuming the alte rnator has some headroom above the "normal" electrical loads of the aircraf t. Bob McC > Subject: AeroElectric-List: Re: Should battery be charged with a higher v oltage? > From: fran4sew(at)banyanol.com > Date: Fri=2C 17 Aug 2012 02:50:24 -0700 > To: aeroelectric-list(at)matronics.com > m> > > Bob=2C Thanks for your words of wisdom. > To Ron P=2C > I could not find any reference to a diode on EuropaOwners.org. But I ass ume that the diode is inserted in the regulator sense wire. I had thought about doing that=2C but voltage measurements indicate that my battery is ke pt fully charged with the 13.6 volt regulator set-point. > The charging instructions in the Oddyssey manual > http://www.odysseybatteries.com/files/US-ODY-TM-001_0411_000.pdf > pertain to a discharged battery. Since my PC680 battery never gets disch arged=2C the Continuous Float Charge voltage of 13.6 is adequate. > I appreciate your input. > Joe > > -------- > Joe Gores > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=381060#381060 > > > > > > > =========== =========== =========== =========== > > > ________________________________________________________________________________
Date: Aug 17, 2012
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: Mooney Alternator woes
Will my B&C LR3C-14 regulator properly control the Continental's alternator? I can easily set this up for a ground-run test.... Are there different regulators based on current output capability? Thanks again! -----Original Message----- >From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> >Sent: Aug 16, 2012 9:44 AM >To: aeroelectric-list(at)matronics.com >Subject: Re: AeroElectric-List: Mooney Alternator woes > > >At 08:27 AM 8/16/2012, you wrote: > > >My hangar neighbor is trying to figure out why his alternator >occasionally drops off line - requiring a weird reset sequence. He >has to shut off the battery and field, then go to a low power setting >and bring it back up again. Something about resetting an overvoltage >protection device. > >It is an M20S with Cont 550 and gear driven alternator. The first >regulator lasted only a couple of years before giving up the ghost >and the replacement was a special from Mooney. > >My first line of thinking is to locate the regulator and test >it. Nobody knows where it is hiding. >(I'm in DC - the plane is in DE...I'll be home next weekend to help more.) > >Meanwhile, does anyone have an electronic copy of the Light Plane >Maintenance article on troubleshooting alternators...and the Mooney >M20S maintenance manual? > >If we can find it, I'm hoping that we can determine if the regulator >is the culprit. > > If it takes a southern Slobovian switch-dance to > bring it back on line, it's almost certain to be > something electronic. Is the successful reset sequence > something different than what is called for in the > POH as a response to an OV trip? > > I've not had any contact with Mooney in 25+ years. I > bid an alternator controller for them while at > Electro-Mech . . . we didn't get the job. I think > Electrodelta out of White Oak, TX got it. It would > have been a Mooney-unique product. ED has changed > hands and/or moved several times over the years. > The guy who ran ED is still hanging around the > Wichita area. He MIGHT be a resource for help > wrestling with your problem. > > The LPM article is not likely to be much help. It > will be VERY generic. If it were my airplane, I'd > jeep another regulator in place of the original to > see if the problem goes away. Given the rarity of > that regulator, I'd probably go for a one-time > STC to install something more contemporary and > available. There's nothing magic about alternator > controllers . . . only the institutionalized and > market driven B.S. in which they reside. > > B&C regulators are used elsewhere on current production > airplanes . . . the FAA might look kindly upon > substitution of B&C product for what's already > installed. > > > Bob . . . > > ________________________________________________________________________________
Date: Aug 17, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Mooney Alternator woes
At 10:45 AM 8/17/2012, you wrote: > > >Will my B&C LR3C-14 regulator properly control the Continental's >alternator? I can easily set this up for a ground-run test.... Yes >Are there different regulators based on current output capability? Generally no. The smallest of 35A alternators draws about 3A max . . . so does a 100A machine. There's an advantage for keeping field currents low (control of internally dissipated heat). Larger machines just get more magnetic flux by more turns of larger wire and keeping the field current manageable. Further, unlike generators, the closed loop dynamics of alternators fall into a much smaller universe of characteristics such that regulators can be quite generic. The B&C linear regulator was optimized for the B&C alternators and may not be as nimble footed for transient response on a 'foreign' alternator but not bad enough to raise risk for the success of the experiment. Bob . . . ________________________________________________________________________________
Date: Aug 17, 2012
Subject: snorkel for alternator cooling
From: Janet Amtmann <jgamtmann2(at)gmail.com>
Hello all, This is only marginally electric, but I need information. My RV6 has no alternator cooling other than the (reverse rotation) internal cooling fan. I'd like to install a snorkel to capture some cooling air at the air inlet ramp and lead it (tru a hose) to the rear of the alternator. Does anyone know of a source for these little alum. snorkels? I have no means to weld, braze or solder alum. I guess that I could make one out of an old tin can, but that's kind of tacky. Regards, Jurgen Amtmann ________________________________________________________________________________
From: "Fisher Paul A." <FisherPaulA(at)johndeere.com>
Date: Aug 17, 2012
Subject: snorkel for alternator cooling
How about Aircraft Spruce? http://www.aircraftspruce.com/catalog/appages/du ctflanges.php - Paul From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectr ic-list-server(at)matronics.com] On Behalf Of Janet Amtmann Sent: Friday, August 17, 2012 1:25 PM Subject: AeroElectric-List: snorkel for alternator cooling Hello all, This is only marginally electric, but I need information. My RV6 has no al ternator cooling other than the (reverse rotation) internal cooling fan. I 'd like to install a snorkel to capture some cooling air at the air inlet r amp and lead it (tru a hose) to the rear of the alternator. Does anyone kn ow of a source for these little alum. snorkels? I have no means to weld, b raze or solder alum. I guess that I could make one out of an old tin can, but that's kind of tacky. Regards, Jurgen Amtmann > ________________________________________________________________________________
Date: Aug 17, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: snorkel for alternator cooling
At 01:25 PM 8/17/2012, you wrote: >Hello all, >This is only marginally electric, but I need information. My RV6 >has no alternator cooling other than the (reverse rotation) internal >cooling fan. I'd like to install a snorkel to capture some cooling >air at the air inlet ramp and lead it (tru a hose) to the rear of >the alternator. Does anyone know of a source for these little alum. >snorkels? I have no means to weld, braze or solder alum. I guess >that I could make one out of an old tin can, but that's kind of tacky. Are you sure you need one? I'm aware of no alternator installations in an RV that experienced difficulties attributable to overheating. Is there something different about the way your alternator is installed where it has been confirmed that extra-ordinary cooling is needed? Way back when, we used to do max hot day climbs at best angle with an alternator at full load . . . and then justify the state of the machine's cooling. Truth is that an alternator never gets operated that way. So what ever cooling was added to meet that capricious demand was wasted effort. Bob . . . ________________________________________________________________________________
Date: Aug 17, 2012
From: David <dlposey-atlanta(at)att.net>
Subject: Fwd: Fw: WWII nostalgia folks...: History / THANKS,
MEL.. ________________________________________________________________________________
Date: Aug 18, 2012
From: Werner Schneider <glastar(at)gmx.net>
Subject: Re: Mooney Alternator woes
>> Will my B&C LR3C-14 regulator properly control the Continental's >> alternator? I can easily set this up for a ground-run test.... > > Yes > Just wonder, Ralph you've told, that your B&C is from a RV-6? That would probably be a 14V system where the Mooney has a 28V System, just carefully check. Cheers Werner ________________________________________________________________________________
From: "John MacCallum" <john.maccallum(at)bigpond.com>
Subject: Schumacher 1562a
Date: Aug 18, 2012
>From the specs you have given I don't think it will. If it has a Transformer with multiple taps on the primary winding you may be able to get someone to alter the taps for you. If it hasn't got multiple taps on the Primary you will need a new transformer. If it's switch mode then you are stuck with the 110-140 vac unless you buy a step down transformer. 240 to 110 Vac. Cheers John MacCallum Builder #41016 VH-DUU From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of John & Sue Dehnert Sent: Friday, 17 August 2012 10:55 AM Subject: AeroElectric-List: Schumacher 1562a Hi all have an off subject question, will the Schumacher 1562a charger maintainer available on Amazon work on the Australian voltage of 240v ac, Schumacher specifications state input voltage 110-140v ac. Thanks for any input on the subject . John ________________________________________________________________________________
From: "F. Tim Yoder" <ftyoder(at)yoderbuilt.com>
Subject: Re: snorkel for alternator cooling
Date: Aug 17, 2012
Maybe cut one out of an old aluminum lawn chair leg? ----- Original Message ----- From: Janet Amtmann To: aeroelectric-list(at)matronics.com Sent: Friday, August 17, 2012 11:25 AM Subject: AeroElectric-List: snorkel for alternator cooling Hello all, This is only marginally electric, but I need information. My RV6 has no alternator cooling other than the (reverse rotation) internal cooling fan. I'd like to install a snorkel to capture some cooling air at the air inlet ramp and lead it (tru a hose) to the rear of the alternator. Does anyone know of a source for these little alum. snorkels? I have no means to weld, braze or solder alum. I guess that I could make one out of an old tin can, but that's kind of tacky. Regards, Jurgen Amtmann ________________________________________________________________________________
From: "mark donahue" <markdonahue(at)earthlink.net>
Subject: snorkel for alternator cooling
Date: Aug 17, 2012
can you use the flexible 5/8 in corragated plastic material that we are using to direct air to our magnetos and alternators on the RV 9? Van sells it. Mark Donahue From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of F. Tim Yoder Sent: Friday, August 17, 2012 6:04 PM Subject: Re: AeroElectric-List: snorkel for alternator cooling Maybe cut one out of an old aluminum lawn chair leg? ----- Original Message ----- From: Janet Amtmann <mailto:jgamtmann2(at)gmail.com> Sent: Friday, August 17, 2012 11:25 AM Subject: AeroElectric-List: snorkel for alternator cooling Hello all, This is only marginally electric, but I need information. My RV6 has no alternator cooling other than the (reverse rotation) internal cooling fan. I'd like to install a snorkel to capture some cooling air at the air inlet ramp and lead it (tru a hose) to the rear of the alternator. Does anyone know of a source for these little alum. snorkels? I have no means to weld, braze or solder alum. I guess that I could make one out of an old tin can, but that's kind of tacky. Regards, Jurgen Amtmann href="http://www.matronics.com/Navigator?AeroElectric-List">http://www.matro nics.com/Navigator?AeroElectric-List href="http://forums.matronics.com">http://forums.matronics.com href="http://www.matronics.com/contribution">http://www.matronics.com/c ________________________________________________________________________________
Date: Aug 17, 2012
From: Kelly McMullen <kellym(at)aviating.com>
Subject: Re: snorkel for alternator cooling
I wouldn't recommend it. It is nylon material IIRC. OK but not great for warm temps under cowling. Scat tube would be the aviation product of choice. On 8/17/2012 7:24 PM, mark donahue wrote: > > can you use the flexible 5/8 in corragated plastic material that we > are using to direct air to our magnetos and alternators on the RV 9? > Van sells it. > > Mark Donahue > > *From:*owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] *On Behalf Of > *F. Tim Yoder > *Sent:* Friday, August 17, 2012 6:04 PM > *To:* aeroelectric-list(at)matronics.com > *Subject:* Re: AeroElectric-List: snorkel for alternator cooling > > ----- No virus found in this message. Checked by AVG - www.avg.com ________________________________________________________________________________
Date: Aug 17, 2012
From: rayj <raymondj(at)frontiernet.net>
Subject: Re: snorkel for alternator cooling
FWIW Here's some dead soft aluminum tubing. I don't know if 5/8 is large enough for your needs. http://www.aircraftspruce.com/catalog/mepages/3003versatube.php Raymond Julian Kettle River, MN. "And you know that I could have me a million more friends, and all I'd have to lose is my point of view." - John Prine On 08/17/2012 01:25 PM, Janet Amtmann wrote: > Hello all, > This is only marginally electric, but I need information. My RV6 has no > alternator cooling other than the (reverse rotation) internal cooling > fan. I'd like to install a snorkel to capture some cooling air at the > air inlet ramp and lead it (tru a hose) to the rear of the alternator. > Does anyone know of a source for these little alum. snorkels? I have > no means to weld, braze or solder alum. I guess that I could make one > out of an old tin can, but that's kind of tacky. > > Regards, Jurgen Amtmann > > > > * > > > * > ________________________________________________________________________________
From: "John Ciolino" <JohnCiolino(at)carolina.rr.com>
Subject: snorkel for alternator cooling
Date: Aug 18, 2012
Here's what I did: ACS sells a 1" aluminum flange (p/n 10350-4). Drill a 1" hole in the inlet ramp and rivet the flange in place. If you are good at bending aluminum tubing also order some 1" tubing and you are all set. I tried that and couldn't get the tubing bent without kinking so I used some 1" SCAT tubing. To keep the tubing in place I took a strip of flat aluminum, bent it to direct the tubing to the alternator and attached it to the flange with a hose clamp. I attached the tubing to the aluminum with tie wraps. Good luck. John Ciolino RV-8 N894Y From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Janet Amtmann Sent: Friday, August 17, 2012 2:25 PM Subject: AeroElectric-List: snorkel for alternator cooling Hello all, This is only marginally electric, but I need information. My RV6 has no alternator cooling other than the (reverse rotation) internal cooling fan. I'd like to install a snorkel to capture some cooling air at the air inlet ramp and lead it (tru a hose) to the rear of the alternator. Does anyone know of a source for these little alum. snorkels? I have no means to weld, braze or solder alum. I guess that I could make one out of an old tin can, but that's kind of tacky. Regards, Jurgen Amtmann ________________________________________________________________________________
Subject: Re: snorkel for alternator cooling
From: Chris Hand <chris_hand(at)comcast.net>
Date: Aug 18, 2012
I used the corrugated tubing from Vans for alternator cooling on my -6A and it works fine. Feeds from inlet ramp on that side down to alternator and haven't had a problem with it, flying about 4 years / 310 hours or so. The tube grooves and a little rtv have held it in place without issue. Light, easy, and inexpensive. Chris On Aug 17, 2012, at 7:42 PM, Kelly McMullen wrote: > > I wouldn't recommend it. It is nylon material IIRC. OK but not great for warm temps under cowling. > Scat tube would be the aviation product of choice. > > On 8/17/2012 7:24 PM, mark donahue wrote: >> >> can you use the flexible 5/8 in corragated plastic material that we are using to direct air to our magnetos and alternators on the RV 9? Van sells it. >> >> Mark Donahue >> >> *From:*owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] *On Behalf Of *F. Tim Yoder >> *Sent:* Friday, August 17, 2012 6:04 PM >> *To:* aeroelectric-list(at)matronics.com >> *Subject:* Re: AeroElectric-List: snorkel for alternator cooling >> >> > > > ----- > No virus found in this message. > Checked by AVG - www.avg.com > > > > > ________________________________________________________________________________
Date: Aug 18, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Mooney Alternator woes
At 05:58 PM 8/17/2012, you wrote: > > >>>Will my B&C LR3C-14 regulator properly control the Continental's >>>alternator? I can easily set this up for a ground-run test.... >> >> Yes >Just wonder, Ralph you've told, that your B&C is from a RV-6? That >would probably be a 14V system where the Mooney has a 28V System, >just carefully check. Excellent catch Werner! I didn't perceived he was talking about an LR3C-14, of course he would need the -28. Thanks! Bob . . . ________________________________________________________________________________
Date: Aug 18, 2012
From: John Morgensen <john(at)morgensen.com>
Subject: Re: snorkel for alternator cooling
I found a grey PVC conduit 90 degree fitting with a 4" radius at the Home Depot aviation electronics department. Also, look around your favorite auto parts store for a pre-shaped radiator hose. john On 8/17/2012 7:42 PM, Kelly McMullen wrote: > > > I wouldn't recommend it. It is nylon material IIRC. OK but not great > for warm temps under cowling. > Scat tube would be the aviation product of choice. > > On 8/17/2012 7:24 PM, mark donahue wrote: >> >> can you use the flexible 5/8 in corragated plastic material that we >> are using to direct air to our magnetos and alternators on the RV 9? >> Van sells it. >> >> Mark Donahue >> >> *From:*owner-aeroelectric-list-server(at)matronics.com >> [mailto:owner-aeroelectric-list-server(at)matronics.com] *On Behalf Of >> *F. Tim Yoder >> *Sent:* Friday, August 17, 2012 6:04 PM >> *To:* aeroelectric-list(at)matronics.com >> *Subject:* Re: AeroElectric-List: snorkel for alternator cooling >> >> > > > ----- > No virus found in this message. > Checked by AVG - www.avg.com > > ________________________________________________________________________________
Subject: Re: snorkel for alternator cooling
From: "jonlaury" <jonlaury(at)impulse.net>
Date: Aug 18, 2012
Jurgen, I've attached a photo of a possible solution. I had the same concerns as you because I have a plenum capturing all the cooling ram air and directing it through the cylinders. My engine installation is battery/electrical system dependent (fuel pumps, EFI & ignition) so I wanted a little insurance for my reversed-fan alternator. I fabricated the alternator diode plate plenum in the picture from fiberglass and vinyl-ester resin. The resin will withstand 220 deg before going plastic. Epoxy resin systems will also work. Just check to see that the transition temp meets your needs. You can use the stamped cooling shroud as a mold for your part. Connect to ram air source with SCAT tube size of your choice. I used 3/4". Good luck, John Read this topic online here: http://forums.matronics.com/viewtopic.php?p=381152#381152 Attachments: http://forums.matronics.com//files/franklin_alternator_001_large_129.jpg ________________________________________________________________________________
From: Michael Burbidge <mburbidg(at)gmail.com>
Subject: Stripping large wires...
Date: Aug 18, 2012
I have one of the quality wire strippers from B&C, but it only strips up to 16 awg wire. How do you strip larger wire. For example, I need to strip some 8 awg wire for my power runs. Is 8 awg stranded wire bigger around than 8 awg solid wire? Thanks, Michael- ________________________________________________________________________________
Date: Aug 18, 2012
From: Dennis Roche <r8751(at)yahoo.com>
Subject: Re:
Learn How to Make Money Online Fast http://bestkaleto.com/horkdsc12.php?tuyahooID=1ya6 ________________________________________________________________________________
Date: Aug 18, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Stripping large wires...
At 04:40 PM 8/18/2012, you wrote: > >I have one of the quality wire strippers from B&C, but it only >strips up to 16 awg wire. How do you strip larger wire. For example, >I need to strip some 8 awg wire for my power runs. Is 8 awg stranded >wire bigger around than 8 awg solid wire? I don't have tools for stripping anything larger than 14AWG. All the big stuff I just score carefully with the ol' Swiss Army Knife and use a pair of diagonal cutters to pull of the discard. Do a few practice strips to get the hang of it. Bob . . . ________________________________________________________________________________
Subject: Re: AeroElectric-List Digest: 9 Msgs - 08/18/12
Date: Aug 19, 2012
From: "James Meade" <jnmeade(at)southslope.net>
From Wikipedia. See the reference tables to confirm the entry. "The AWG tables are for a single, solid, round conductor. The AWG of a stranded wire is determined by the total cross-sectional area of the conductor, which determines its current-carrying capacity and electrical resistance. Because there are also small gaps between the strands, a stranded wire will always have a slightly larger overall diameter than a solid wire with the same AWG." http://en.wikipedia.org/wiki/American_wire_gauge ________________________________________________________________________________
Date: Aug 19, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: snorkel for alternator cooling
At 11:58 AM 8/18/2012, you wrote: Thanks to everyone who replied. Bob N. Thanks for your explanation. No, nothing special about my alternator installation, N-D in the standard position for a Lyc. I was only concerned because someone who had done the cooling duct on an RV6 was concerned because I had none. I thought better safe than sorry. Added cooling doesn't hurt anything . . . usually. We added a scupper on the fuselage of the single engine airplanes at Cessna way back when to bring outside ram air into the radio stack. I recall a flurry of activity over that installation when a customer reported damage to radios due to ingress of rain! On the other hand, 'things' added to any project has a cost of ownership in $time$ to install and maintain that thing . . . and loss of weight and volume resources for having installed it. Alternator cooling has been a hot topic of discussion on the various OBAM aviation forums since I've been participating. Folks have attributed many failures of alternators to 'a lack of cooling' but without supporting evidence. I have yet to see any MEASUREMENTS of performance that suggests a reduction of risk for cost or safety for having added cooling to the alternator. I'm not suggesting that you should not add the cooling . . . I have no basis for asserting ANY justification one way or the other. Intuitively, I have observed what happens under the hood of my car for an alternator that gets heavily loaded in the worst of local temperature and airflow conditions yet it has hummed along nicely for 11+ years and 170,000 miles . . . without a forced air cooling feature. The scat tube is light, the time expended in the grand scheme of things is small. But it would be really interesting to know if the effort has any beneficial effect. Bob . . . ________________________________________________________________________________
Subject: Re: snorkel for alternator cooling
From: "jonlaury" <jonlaury(at)impulse.net>
Date: Aug 19, 2012
nuckolls.bob(at)aeroelect wrote: > At 11:58 AM 8/18/2012, you wrote: > ... snip > > The scat tube is light, the time expended in > the grand scheme of things is small. But it > would be really interesting to know if the effort > has any beneficial effect. > > > Bob . . . The cooling shroud that I built and the scat tube (7") are a few ounces and part of the "mission" of this project has been to have fun.Designing and fabbing this thing qualifies. Knowing that I was going to build an airplane that was dependent on electrowhizzies to keep air underneath the wheels, I asked an old-school alternator/starter repair shop guy (the kind of place with alternators up to the rafters and huge, antediluvian black machines peppered with large analog meters and cats sleeping on top) for the best way to keep alternators alive and he said to just keep the diode plate(s) cool. So that is what I did. For both alternators [Wink] John Read this topic online here: http://forums.matronics.com/viewtopic.php?p=381243#381243 ________________________________________________________________________________
Date: Aug 20, 2012
From: Ken <klehman(at)albedo.net>
Subject: 24 volt inverter
There is a small 12 to 24 volt inverter suitable for running things like a Turn and Bank instrument for $2.99 on ebay. Free shipping. Adjustable output, 2 amp, 10 watt nominal or higher with cooling. Having abused one of these a fair bit, I found them surprisingly robust so I thought I'd mention them. My T&B only draws 0.06 amp when running but I needed a 2.5 amp C/B to handle the startup current. ebay item 180924154518 Ken ________________________________________________________________________________
Date: Aug 20, 2012
From: Peter Pengilly <peter(at)sportingaero.com>
Subject: Recording a NMEA GPS stream
Guys, Does anyone know anything about Arduino <http://arduino.cc/en/> boards? Can these devices be used to monitor an NMEA datastream and record to USB stick or SD card? This may sound really basic to some, but it is a question that has been occasionally exercising my brain on and off for some years, how to record the NMEA datastream from a GPS device? About 12 years ago I was involved in re-instrumenting a glider that required the GPS to provide data to a glide computer that provided data to a PDA. I had only worked with 1553 before that and had to learn about NMEA. The PDA software vendor provided a utility that would record the datastream - which was very useful in debugging that installation. Since then I have occasionally wanted to record a NMEA datastream, but not so much that I really looked into it seriously. I have recently re-built my panel <http://www.glosterairparts.co.uk/images/After2.jpg>. The GPS feeds into the EFIS are not working properly so now I _need_ a datastream monitor - this device seems like it might do the trick. Does anyone have any experience using such a board or are there any resources on-line that explain how to do this? Thanks, Pete ________________________________________________________________________________
Date: Aug 20, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Recording a NMEA GPS stream
At 04:01 PM 8/20/2012, you wrote: >Guys, > >Does anyone know anything about <http://arduino.cc/en/>Arduino >boards? Can these devices be used to monitor an NMEA datastream and >record to USB stick or SD card? Sure. There are several add-ons to the generic Arduino boards to talk to SD cards, thumbdrives, etc. http://tinyurl.com/8m7m7sb The NMEA data stream is plain vanilla RS232 levels and formatted data streams of data delivered in a series of bytes. I'm sure you could set up a board to simply record the data as presented or you could parse the string out to record say lat, lot, gs, crs, and date-time . . . a sort of second by second logbook of where you've been and how fast you got there. Bob . . . ________________________________________________________________________________
Date: Aug 20, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: 24 volt inverter
At 12:38 PM 8/20/2012, you wrote: > >There is a small 12 to 24 volt inverter suitable for running things >like a Turn and Bank instrument for $2.99 on ebay. Free shipping. >Adjustable output, 2 amp, 10 watt nominal or higher with cooling. >Having abused one of these a fair bit, I found them surprisingly >robust so I thought I'd mention them. My T&B only draws 0.06 amp >when running but I needed a 2.5 amp C/B to handle the startup current. > >ebay item 180924154518 Good data point Ken. Thanks. I've got a little bit heftier boost supply coming to fabricate into a 19v supply for laptops in the car. Right now, Dr. Dee plugs in a 12Dc->120AC inverter, then the 120AC->19DC supply with the attendant snarl of cords. Tucking one of these boost supplies behind the glove box with appropriate connectors on the console will eliminate the spider web of wire and monkey motion black boxes to a single cord with a 5.5x2.5 connector on each end. The supply was $9 delivered to my po box. http://tinyurl.com/9djfxmr You might want to poke around the installed supply wiring with your hand-held tuned to unused channels and the squelch open. Just be aware of any potential for interference with your VHF AM hardware. Even if you do find some detectable noise, don't go on a crusade to tame it until you know if it's strong enough to be a problem. Being aware is forewarned. The hand-held sniff-test is pretty sensitive and may detect emissions that are insignificant to your installation and use of the airplane. Bob . . . ________________________________________________________________________________
Date: Aug 20, 2012
From: Peter Pengilly <peter(at)sportingaero.com>
Subject: Re: Recording a NMEA GPS stream
Well, a little more surfing has revealed this device ArduLog Data Logger <http://www.hobbytronics.co.uk/arduino/ardulog> looks like what I need, and less than 15. I know this is a UK site, but similar stuff must exist in the US. I guess 5v from a GPS cigarette lighter power supply will work to power it. Pete On 20/08/2012 22:01, Peter Pengilly wrote: > Guys, > > Does anyone know anything about Arduino <http://arduino.cc/en/> > boards? Can these devices be used to monitor an NMEA datastream and > record to USB stick or SD card? > > This may sound really basic to some, but it is a question that has > been occasionally exercising my brain on and off for some years, how > to record the NMEA datastream from a GPS device? About 12 years ago I > was involved in re-instrumenting a glider that required the GPS to > provide data to a glide computer that provided data to a PDA. I had > only worked with 1553 before that and had to learn about NMEA. The PDA > software vendor provided a utility that would record the datastream - > which was very useful in debugging that installation. > > Since then I have occasionally wanted to record a NMEA datastream, but > not so much that I really looked into it seriously. I have recently > re-built my panel > <http://www.glosterairparts.co.uk/images/After2.jpg>. The GPS feeds > into the EFIS are not working properly so now I _need_ a datastream > monitor - this device seems like it might do the trick. > > Does anyone have any experience using such a board or are there any > resources on-line that explain how to do this? > > Thanks, Pete > * > > > * ________________________________________________________________________________
Date: Aug 20, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Recording a NMEA GPS stream
> The GPS feeds into the EFIS are not working properly so now I need > a datastream monitor - this device seems like it might do the trick. Hmmm . . . I missed this point the first pass through your query. For a troubleshooting monitor, you may be better served with a lap-top configured with an RS-232 to USB adapter and a utility to read data streams and put them up on the screen in real time either as a scrolling presentation . . . or parse of some interesting words and display current values in a box on the screen. I used to do this kind of stuff all the time at Beech/RAC/HBC. I could get my laptop and data acquisition system going and installed before the legacy service organizations could get their work orders approved and funded. Damn it was nice to have a dedicated budget for such things! Did all my lap-top work in compiled basic. Bob . . . ________________________________________________________________________________
From: "Chris Fordham" <fconsult(at)telus.net>
Subject: Garmin 327 problem
Date: Aug 20, 2012
Just hoping someone else has run across this problem and better still has a solution. I have a new Garmin 327 installed in a ragwing aircraft. When the Transponder is switched to Alt. the correct altitude shows up on the Garmin but the controllers can't read the altitude, the Ident function works. It's a stand alone Transcal encoder. Thanks Kit ________________________________________________________________________________
From: Henry Hallam <henry(at)pericynthion.org>
Date: Aug 20, 2012
Subject: Re: Garmin 327 problem
Probably an issue with the transponder antenna or connection between the antenna and the transponder. A marginal connection between the xpdr and antenna can give a weak return signal that is strong enough for Mode A / Ident but not strong enough for Mode C. The correct altitude readout on the Garmin 327 indicates that the encoder and encoder-transponder connection is fine. Good luck, Henry On Mon, Aug 20, 2012 at 6:27 PM, Chris Fordham wrote: > Just hoping someone else has run across this problem and better still has a > solution. I have a new Garmin 327 installed in a ragwing aircraft. When the > Transponder is switched to Alt. the correct altitude shows up on the Garmin > but the controllers can't read the altitude, the Ident function works. It's > a stand alone Transcal encoder. > Thanks Kit > > ________________________________________________________________________________
Date: Aug 20, 2012
Subject: Re: Recording a NMEA GPS stream
From: "Jeff B." <loboflyer(at)gmail.com>
If you're really interested in embedded programming and you want to avoid the laptop, the Arduinos probably will fit the bill. However, if you just want to troubleshoot NMEA, then a laptop with serial port (or USB adapter) and software would be fastest. You can probably tap off the GPS' TxD pin to your laptop's RxD pin. A Google search turns up a few programs, none of which I have experience with, but all look useful of some sort. http://www.visualgps.net/visualgps/ http://homepage2.nifty.com/k8/gps/ http://www.aviadesign.com/Monitor/ -Jeff- On Mon, Aug 20, 2012 at 4:00 PM, Robert L. Nuckolls, III < nuckolls.bob(at)aeroelectric.com> wrote: > The GPS feeds into the EFIS are not working properly so now I *need* a > datastream monitor - this device seems like it might do the trick. > > > Hmmm . . . I missed this point the first pass through > your query. For a troubleshooting monitor, you may > be better served with a lap-top configured with an > RS-232 to USB adapter and a utility to read data > streams and put them up on the screen in real time > either as a scrolling presentation . . . or parse > of some interesting words and display current values > in a box on the screen. > > I used to do this kind of stuff all the time at > Beech/RAC/HBC. I could get my laptop and data acquisition > system going and installed before the legacy service > organizations could get their work orders approved > and funded. Damn it was nice to have a dedicated > budget for such things! > > Did all my lap-top work in compiled basic. > > > ** > > ** Bob . . . > > ________________________________________________________________________________
Subject: RS-232 Data Logger
From: Eric Page <edpav8r(at)yahoo.com>
Date: Aug 21, 2012
Pete, If you don't program C, you may find PICAXE controllers a little friendlier to work with than Arduino. The PICAXE boards require more physical prep, but there's block diagram programming software available that makes getting it to do what you want simple. http://www.picaxe.com/ WRT Arduino data logging hardware, see the following: http://www.sparkfun.com/ http://adafruit.com/ http://www.dx.com/ Eric ________________________________________________________________________________
Date: Aug 21, 2012
From: Peter Pengilly <peter(at)sportingaero.com>
Subject: Re: Recording a NMEA GPS stream
Thanks for all the pointers - I don't have a laptop at present so figured a small datalogger would be cheaper! Peter On 21/08/2012 05:44, Jeff B. wrote: > If you're really interested in embedded programming and you want to > avoid the laptop, the Arduinos probably will fit the bill. However, > if you just want to troubleshoot NMEA, then a laptop with serial port > (or USB adapter) and software would be fastest. You can probably tap > off the GPS' TxD pin to your laptop's RxD pin. > > A Google search turns up a few programs, none of which I have > experience with, but all look useful of some sort. > > http://www.visualgps.net/visualgps/ > http://homepage2.nifty.com/k8/gps/ > http://www.aviadesign.com/Monitor/ > > > -Jeff- > > On Mon, Aug 20, 2012 at 4:00 PM, Robert L. Nuckolls, III > > > wrote: > >> The GPS feeds into the EFIS are not working properly so now I >> _need_ a datastream monitor - this device seems like it might do >> the trick. > > Hmmm . . . I missed this point the first pass through > your query. For a troubleshooting monitor, you may > be better served with a lap-top configured with an > RS-232 to USB adapter and a utility to read data > streams and put them up on the screen in real time > either as a scrolling presentation . . . or parse > of some interesting words and display current values > in a box on the screen. > > I used to do this kind of stuff all the time at > Beech/RAC/HBC. I could get my laptop and data acquisition > system going and installed before the legacy service > organizations could get their work orders approved > and funded. Damn it was nice to have a dedicated > budget for such things! > > Did all my lap-top work in compiled basic. > > > Bob . . . > > > * > > > * ________________________________________________________________________________
From: Henry Hallam <henry(at)pericynthion.org>
Date: Aug 21, 2012
Subject: Re: Recording a NMEA GPS stream
The combination of these two should do nicely, no coding required (but you can also use them to learn about microcontrollers if you want to): https://www.sparkfun.com/products/10216 https://www.sparkfun.com/products/8780 Henry On Tue, Aug 21, 2012 at 1:12 PM, Peter Pengilly wrote: > Thanks for all the pointers - I don't have a laptop at present so figured a > small datalogger would be cheaper! > > Peter > > > On 21/08/2012 05:44, Jeff B. wrote: > > If you're really interested in embedded programming and you want to avoid > the laptop, the Arduinos probably will fit the bill. However, if you just > want to troubleshoot NMEA, then a laptop with serial port (or USB adapter) > and software would be fastest. You can probably tap off the GPS' TxD pin to > your laptop's RxD pin. > > A Google search turns up a few programs, none of which I have experience > with, but all look useful of some sort. > > http://www.visualgps.net/visualgps/ > http://homepage2.nifty.com/k8/gps/ > http://www.aviadesign.com/Monitor/ > > > -Jeff- > > On Mon, Aug 20, 2012 at 4:00 PM, Robert L. Nuckolls, III > wrote: >> >> The GPS feeds into the EFIS are not working properly so now I need a >> datastream monitor - this device seems like it might do the trick. >> >> >> Hmmm . . . I missed this point the first pass through >> your query. For a troubleshooting monitor, you may >> be better served with a lap-top configured with an >> RS-232 to USB adapter and a utility to read data >> streams and put them up on the screen in real time >> either as a scrolling presentation . . . or parse >> of some interesting words and display current values >> in a box on the screen. >> >> I used to do this kind of stuff all the time at >> Beech/RAC/HBC. I could get my laptop and data acquisition >> system going and installed before the legacy service >> organizations could get their work orders approved >> and funded. Damn it was nice to have a dedicated >> budget for such things! >> >> Did all my lap-top work in compiled basic. >> >> >> Bob . . . >> >> > > ________________________________________________________________________________
Subject: Re: Recording a NMEA GPS stream
From: "Brantel" <brianchesteen(at)gmail.com>
Date: Aug 21, 2012
I made one of these a while back. Works great! http://www.vansairforce.com/community/showthread.php?t=84045 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=381485#381485 ________________________________________________________________________________
Date: Aug 21, 2012
Subject: Low Voltage Disconnect needed
From: rparigor(at)suffolk.lib.ny.us
Hi Group I am need of Low Voltage Cutoff. Requirements are: ** Ability to handle 10 amps ** When there is a 750mA load, cutoff should occur ~ 11.9 and 12.1 volts ** Minimal parts count, ease of fabrication and low cost ** Somehow once Low Voltage Cutoff threshold is reached, only the secret reed switch (or switches) can reset or bypass things so the battery charger (needs voltage to recognize a battery is hooked up ) can charge, idea is there will be a rare earth magnet in the 12 volt male cigarette lighter plug (attached to the charger) and reed switch/s on the outside of the female receptacle on the battery pack) ** Unless the design allows for very reliable use of Mosfet that isn't going to fail if you look at them the wrong way and even whisper "static electricity", a relay is fine Thx. Ron Parigoris ________________________________________________________________________________
Subject: Adding an electrical system
From: speedy11(at)aol.com
Date: Aug 22, 2012
I am adding an electrical system to a PT-22 per a customer's request. It w ill consist of an overhauled Eclipse Y-150 starter, a RG battery, starter s witch and contactor, a switched bus to power a Becker radio and transponder , a wind driven generator, and associated wiring. Does anyone have experience with adding electrical to a PT-22? Any gotchas? I can't find any generator or alternator that is approved for the PT engine , that's the reason for the wind generator. It will only produce about 5 a mps, so it will barely power the transponder and slowly recharge the batter y and allow occasional radio transmission. Since I'm doing a form 337 for the change, I should be able to use any batt ery. So, we're considering a PC-680 or a lithium ion battery such as the A erovoltz. Otherwise, we'll us a RG-35AXC. Comments? Thanks, Stan Sutterfield Port Orange, FL ________________________________________________________________________________
Date: Aug 22, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Low Voltage Disconnect needed
At 07:17 PM 8/21/2012, you wrote: >Hi Group > >I am need of Low Voltage Cutoff. > >Requirements are: > >** Ability to handle 10 amps > >** When there is a 750mA load, cutoff should occur ~ 11.9 and 12.1 volts > >** Minimal parts count, ease of fabrication and low cost > >** Somehow once Low Voltage Cutoff threshold is reached, only the >secret reed switch (or switches) can reset or bypass things so the >battery charger (needs voltage to recognize a battery is hooked up ) >can charge, idea is there will be a rare earth magnet in the 12 volt >male cigarette lighter plug (attached to the charger) and reed >switch/s on the outside of the female receptacle on the battery pack) > >** Unless the design allows for very reliable use >of Mosfet that isn't going to fail if you look at them the wrong way >and even whisper "static electricity", a relay is fine Here's both all solid state and a relay version of what I think you asked for. I'd go with the MosFet version. FETs are quite rugged these days. http://tinyurl.com/9lc72qs Bob . . . ________________________________________________________________________________
Date: Aug 22, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Adding an electrical system
At 11:14 PM 8/21/2012, you wrote: I am adding an electrical system to a PT-22 per a customer's request. It will consist of an overhauled Eclipse Y-150 starter, a RG battery, starter switch and contactor, a switched bus to power a Becker radio and transponder, a wind driven generator, and associated wiring. Does anyone have experience with adding electrical to a PT-22? Any gotchas? I can't find any generator or alternator that is approved for the PT engine, that's the reason for the wind generator. It will only produce about 5 amps, so it will barely power the transponder and slowly recharge the battery and allow occasional radio transmission. Since I'm doing a form 337 for the change, I should be able to use any battery. So, we're considering a PC-680 or a lithium ion battery such as the Aerovoltz. Otherwise, we'll us a RG-35AXC. What are your design goals for the installation and how do you envision it will be used operationally? Will this airplane be used for cross-country flight? Is it parked in a location serviced by AC mains power? Keep in mind that cranking an engine from the typical battery takes only 5% or so of that battery's capacity. Transponders take typically 2 amps to operate when generating lots of replies. If I recall correctly, the Becker was designed for battery only ops in gliders. It's power demans are: Standby" reception mode =A3 70 mA Reception mode =A3 500 mA Transmission mode =A3 2.5 A Energy demands for this instance are trivial. Further, it has a low voltage warning built in set to trigger at 10.5 volts. http://tinyurl.com/9upvqxg An RG-35 is a beast of a battery . . . 30+ pounds as I recall. B&C did some cranking tests on the SMALLER cousin to the PC-680 and found that it would do a 10-blade crank of a high compression engine (aerobatic aircraft), 5 times in a row (with about a minute cool down between events). The PC-680 should do better yet. How about NO generator, a PC-680 as the only battery and a Battery Minder plugged in while the airplane is parked? Li-FePOH batteries are low risk because you're not going to charge it at a high rate while airborne . . . and it can be recharged at a benign rate while hangared. But take care also that you do not heavily discharge it between flights as they're more sensitive to deep cycle damage than their SVLA cousins. Bob . . . ________________________________________________________________________________
Date: Aug 22, 2012
From: Peter Pengilly <peter(at)sportingaero.com>
Subject: Re: Recording a NMEA GPS stream
Cool, thanks! On 22/08/2012 00:11, Brantel wrote: > > I made one of these a while back. Works great! > > http://www.vansairforce.com/community/showthread.php?t=84045 > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=381485#381485 > > ________________________________________________________________________________
From: Speedy11(at)aol.com
Date: Aug 23, 2012
Subject: Re:Adding an electrical system
Bob, Your points are all well taken. But, the customer wants a complete electrical system installed including some type of charging system. I suggested to him that the demand on the battery will be nominal for the short 1 hours flights he plans in the airplane. There will be no long distance flights. I suggested a battery only electrical system and charging the battery between flights. But, he insists on a system with charging capability. So, the only option is to install an external wind generator for recharging. Do I need a voltage regulator for this setup? As mentioned, the airplane will be flown only occasionally and only locally. It will be in a flying museum in Chile. We will install a charging point for the battery so it can be maintained to full charge between flights. I am considering the RG-35 battery only because it was used in a previous 337-approved PT-22 installation so reapproval will be much easier by using the same battery. >From my experience, a single PC-680 battery will just barely turn over my IO-390. I have two in the plane and have to connect both to get good rotation of the engine. The PT-22 has a radial (not sure yet which one) and I'm not sure that the PC-680 will have enough juice to spin it well. Since we are installing a starter on the engine, we can afford some weight in the aft fuselage (behind seat) for the battery weight. I'm planning to use #2 wire from the battery forward. The power demands from the Becker radio and transponder are minimal. Your numbers are for the VHF radio. Standby" reception mode 70 mA Reception mode 500 mA Transmission mode 2.5 A The transponder requires only Standby - 0.3A Transmit - 1.1A So, the inflight demand on the battery will be zero when the wind generator is producing 5A. I agree that the RG-35AXC is a monster. It is very heavy which translates into extra weight for the stronger battery mount required. What do you think of using an Aerovoltz lithium battery? It has about 550CCA and shelf life is excellent (10% loss over one year). Otherwise, I will lean toward the PC-680 - or maybe a pair of them. The main concern overall for this installation is that the cranking power must be sufficient to start the engine. All other demands on the system are achievable. More thoughts? Stan Sutterfield In a message dated 8/23/2012 3:01:37 A.M. Eastern Daylight Time, aeroelectric-list(at)matronics.com writes: I am adding an electrical system to a PT-22 per a customer's request. It will consist of an overhauled Eclipse Y-150 starter, a RG battery, starter switch and contactor, a switched bus to power a Becker radio and transponder, a wind driven generator, and associated wiring. Does anyone have experience with adding electrical to a PT-22? Any gotchas? I can't find any generator or alternator that is approved for the PT engine, that's the reason for the wind generator. It will only produce about 5 amps, so it will barely power the transponder and slowly recharge the battery and allow occasional radio transmission. Since I'm doing a form 337 for the change, I should be able to use any battery. So, we're considering a PC-680 or a lithium ion battery such as the Aerovoltz. Otherwise, we'll us a RG-35AXC. What are your design goals for the installation and how do you envision it will be used operationally? Will this airplane be used for cross-country flight? Is it parked in a location serviced by AC mains power? Keep in mind that cranking an engine from the typical battery takes only 5% or so of that battery's capacity. Transponders take typically 2 amps to operate when generating lots of replies. If I recall correctly, the Becker was designed for battery only ops in gliders. It's power demans are: Standby" reception mode =A3 70 mA Reception mode =A3 500 mA Transmission mode =A3 2.5 A Energy demands for this instance are trivial. Further, it has a low voltage warning built in set to trigger at 10.5 volts. http://tinyurl.com/9upvqxg An RG-35 is a beast of a battery . . . 30+ pounds as I recall. B&C did some cranking tests on the SMALLER cousin to the PC-680 and found that it would do a 10-blade crank of a high compression engine (aerobatic aircraft), 5 times in a row (with about a minute cool down between events). The PC-680 should do better yet. How about NO generator, a PC-680 as the only battery and a Battery Minder plugged in while the airplane is parked? Li-FePOH batteries are low risk because you're not going to charge it at a high rate while airborne . . . and it can be recharged at a benign rate while hangared. But take care also that you do not heavily discharge it between flights as they're more sensitive to deep cycle damage than their SVLA cousins. Bob . . . ________________________________________________________________________________
Date: Aug 23, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re:Adding an electrical system
> >More thoughts? Sounds like you have a plan. 5A applied to an RG35 probably doesn't represent much of an OV risk. But it would be easy to add crowbar protection right on the b-lead breaker. Bob . . . ________________________________________________________________________________
Date: Aug 23, 2012
Subject: Re: Low Voltage Disconnect needed
From: rparigor(at)suffolk.lib.ny.us
Hi Bob Thx. for the info. Ron P. > Here's both all solid state and a relay version > of what I think you asked for. I'd go with the > MosFet version. FETs are quite rugged these days. > > http://tinyurl.com/9lc72qs ________________________________________________________________________________
Date: Aug 24, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: OT: analog VOM worth battery cost.
At 01:37 AM 8/24/2012, you wrote: Greetings, I have a Triplet 630-NA VOM. I'm wondering if it is a good enough quality VOM to justify putting $15 worth of batteries into. Opinions please. Some thoughts. I keep analog meters around (including the 630 I purchased in 1961 upon being hired into Boeing) because they often yield dynamic data that is difficult or impossible to get from a digital device. Consider replacing only the 1.5v battery which will get the X1 ohms function working . . . which is the most useful in working electrical systems issues anyway. Bob . . . ________________________________________________________________________________
Date: Aug 24, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Resuscitating the Tripplet 630
After my reply on this thread, I was recalling some features of the 630 buried pretty deeply in the grey-matter. I dug mine out and pulled the case off. Replacing JUST the one battery is still a good idea but the cell is 'captured' into position in the battery box by the case. Proper retention of the battery depends on the HV battery being installed. Looking at this configuration sparked an idea that was easy to implement and worked around the fixture problem. I cut a couple 3/4" pieces of hobby shop brass with a 9/16" i.d. 19/32" o.d. Emacs! Tape one piece to the (-) end of AA cell so that you have a recess about 1/8" deep. Tape the other piece to the (+) end looking for a recess about 1/2" deep. Make a conductive "plug" to drop into the (+) cavity. Here's a quick-n-dirty pair of nuts on a 10-32 screw and trimmed flush with a Dremel. Emacs! Drop the "plug" into the (+) end and place it between the cell contacts of the 630 Emacs! This configuration captures the cell between the contacts even though the hv battery is not present. Also, I'm pleased to report that the single AA cell excites ALL resistance ranges EXCEPT the highest range. A little time on the lathe could produce adapters fitted more closely to the dimensions of the AA cell and the mating contacts on the 630. A pleasant distraction . . . Another approach would be to make a 'plug' from plastic or wood that emulates the shape of the 30v battery. You'd want holes in both ends to clear the 630's battery contacts. Then use the standard C-cell and exploit the original design goals for cell retention. Depending on how determined you are to get it all up and running, there is sufficient volume inside to house three 9v alkaline batteries. One where the 30v goes, two on each end of the battery box over the fuses. A bit of wire, some tack soldering and double-sided tape for battery retention could give you a 27v 'work-around' that should bring the x100K range back to life as well. Bit lots sells an alkaline 9v for $2 or less. Bottom line is that there may still be more years of useful utility left in your venerable ol' workhorse. Working the flight line at Boeing, the Simpson 260 was all the tool cribs stocked. We fixed a lot of airplanes with this genere' of measurement tools. Bob . . . ________________________________________________________________________________
From: "Jeff Luckey" <JLuckey(at)pacbell.net>
Subject: Resuscitating the Tripplet 630
Date: Aug 24, 2012
When my dad passed away last year I inherited a lot of old electrical equipment, including a 630. Finding that meter while sorting thru his stuff brought back lots of memories of futzing w/ batteries, lamps & alligator clips as a kid - funny what you remember. Using 3 9-volters to replace the big battery is a great idea - glad to hear that 27 volts is enough. Lots of people, especially younger ones, would just throw-away something like this but I find it strangely satisfying to keep an older, good-quality instrument in service, even if it requires a little engineering. Is that due to age or wisdom??? Pardon the philosophical observations, -Jeff _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Friday, August 24, 2012 11:02 Subject: AeroElectric-List: Resuscitating the Tripplet 630 After my reply on this thread, I was recalling some features of the 630 buried pretty deeply in the grey-matter. I dug mine out and pulled the case off. Replacing JUST the one battery is still a good idea but the cell is 'captured' into position in the battery box by the case. Proper retention of the battery depends on the HV battery being installed. Looking at this configuration sparked an idea that was easy to implement and worked around the fixture problem. I cut a couple 3/4" pieces of hobby shop brass with a 9/16" i.d. 19/32" o.d. Emacs! Tape one piece to the (-) end of AA cell so that you have a recess about 1/8" deep. Tape the other piece to the (+) end looking for a recess about 1/2" deep. Make a conductive "plug" to drop into the (+) cavity. Here's a quick-n-dirty pair of nuts on a 10-32 screw and trimmed flush with a Dremel. Emacs! Drop the "plug" into the (+) end and place it between the cell contacts of the 630 Emacs! This configuration captures the cell between the contacts even though the hv battery is not present. Also, I'm pleased to report that the single AA cell excites ALL resistance ranges EXCEPT the highest range. A little time on the lathe could produce adapters fitted more closely to the dimensions of the AA cell and the mating contacts on the 630. A pleasant distraction . . . Another approach would be to make a 'plug' from plastic or wood that emulates the shape of the 30v battery. You'd want holes in both ends to clear the 630's battery contacts. Then use the standard C-cell and exploit the original design goals for cell retention. Depending on how determined you are to get it all up and running, there is sufficient volume inside to house three 9v alkaline batteries. One where the 30v goes, two on each end of the battery box over the fuses. A bit of wire, some tack soldering and double-sided tape for battery retention could give you a 27v 'work-around' that should bring the x100K range back to life as well. Bit lots sells an alkaline 9v for $2 or less. Bottom line is that there may still be more years of useful utility left in your venerable ol' workhorse. Working the flight line at Boeing, the Simpson 260 was all the tool cribs stocked. We fixed a lot of airplanes with this genere' of measurement tools. Bob . . . No virus found in this message. Checked by AVG - www.avg.com ________________________________________________________________________________
Date: Aug 25, 2012
From: Henador Titzoff <henador_titzoff(at)yahoo.com>
Subject: Resuscitating the Tripplet 630
I'm gonna have to side with Eric on this one. =C2-I think you guys are in a nostalgia induced somnambulism that results in tons of worthless cr*p la ying around the house. By worthless, I mean things that you will never use again. You'll just walk by it and admire it occasionally as you worm your w ay through the make shift aisles to the kitchen for yet another Ruben sandw ich. Some people call it hoarding. The Tripplet 630 was a fine instrument in its day, but it was made for rela tively high voltages and empty state logic, not the low voltages and curren ts in today's solid state devices. Yes, you can use it to trace wires and f ind some resistance problems, but as a general all around instrument, you m ight as well take it with you when you die and donate it to Nicolas Tesla w hen he greets you at the Purrly Gates. I'd much rather have my trusty Fluke 77 or 87 to troubleshoot just about anything, including my mistress going haywire when she finds out I'm married. I have both instruments, one for th e hangar and one for the house. I'm even thinking about getting another one for my bar hopping trips so I can check out women's resistances as I appro ach them with my teleprompter and well rehearsed lines. Yes, it's that vers atile! As Eric Jonez said, the 77 is a darn good instrument. =C2-I've had mine f or over two decades now, and it is indeed a trusty instrument with a nice y ellow protective cover. When I die, I'm gonna take it with me so I can have William Shockley meet me at the Purrly Gates and tell me I made a fine cho ice. Henador Titzoff --- On Fri, 8/24/12, Jeff Luckey wrote: From: Jeff Luckey <JLuckey(at)pacbell.net> Subject: RE: AeroElectric-List: Resuscitating the Tripplet 630 Date: Friday, August 24, 2012, 2:30 PM =0A=0A=0A =0A =0A=0A =0A=0A=0A=0A=0A=0A=0A=0A=0A=0A=0A=0AWhen my dad passed away last year I=0Ainherited a lot of old electrical equipment, including a 630.=C2- =0A=0A =C2- =0A=0AFinding that meter while sorting thru his =0Astuff brought back lots of memories of futzing w/ batteries, lamps & all igator=0Aclips as a kid =93 funny what you remember =0A=0A =C2- =0A=0AUsing 3 9-volters to replace the big=0Abattery is a great idea =93 glad to hear that 27 volts is enough. =0A=0A =C2- =0A=0ALots o f people, especially younger ones,=0Awould just throw-away something like t his but I find it strangely satisfying to=0Akeep an older, good-quality ins trument in service, even if it requires a little=0Aengineering.=C2- Is th at due to age or wisdom??? =0A=0A =C2- =0A=0APardon the philosophical obs ervations, =0A=0A =C2- =0A=0A-Jeff =0A=0A =C2- =0A=0A=0A=0A=0A=0A=0A=0A =0A=0AFrom:=0Aowner-aeroelectric-list-server(at)matronics.com [mailto:owner-ae roelectric-list-server(at)matronics.com]=0AOn Behalf Of Robert L. Nuckolls,=0A III =0ASent: Friday, August 24, 2012=0A11:02 =0ATo: aeroelectric-list(at)matronics.com =0ASubject: AeroElectric-List:=0AResuscitating the Tripplet 630 =0A=0A=0A =0A =C2- =0A=0AAfter my reply on this thread, I was recalling some =0Afeatures of the 630 buried pretty deeply in the grey-matter. =0AI dug mine out and pulled the case off. =0A =0AReplacing JUST the one battery is still a good idea but =0Athe cell is 'captured' into position in the battery box =0Aby the case. Proper retention of the battery depends on =0Athe HV battery being installed. =0A =0ALooking at this configuration sparked an idea that was =0Aeasy to implement and worked around the fixture problem. =0A =0AI cut a couple 3/4" pieces of hobby shop brass with a 9/16" i.d.=0A19/32 " o.d. =0A =0A =0A =0A =0A=C2- Tape one piece to the (-) end of AA cell so that you have =0A=C2- a recess about 1/8" deep. Tape the other piece to the (+) =0A=C2- end looking for a recess about 1/2" deep. Make a conductive =0A=C2- "plug" to drop into the (+) cavity. Here's a quick-n-dirty =0A=C2- pair of nuts on a 10-32 screw and trimmed flush with a =0A=C2- Dremel. =0A =0A =0A =0ADrop the "plug" into the (+) end and place it between =0Athe cell contacts of the 630 =0A =0A =0A =0AThis configuration captures the cell between the contacts even =0Athough the hv battery is not present. =0A =0AAlso, I'm pleased to report that the single AA cell excites ALL =0Aresistance ranges EXCEPT the highest range. A little time =0Aon the lathe could produce adapters fitted more closely =0Ato the dimensions of the AA cell and the mating contacts =0Aon the 630. A pleasant distraction . . . =0A =0AAnother approach would be to make a 'plug' from plastic or =0Awood that emulates the shape of the 30v battery. You'd want =0Aholes in both ends to clear the 630's battery contacts. Then =0Ause the standard C-cell and exploit the original design =0Agoals for cell retention. =0A =0ADepending on how determined you are to get it all up and =0Arunning, there is sufficient volume inside to house three 9v =0Aalkaline batteries. One where the 30v goes, two on each end =0Aof the battery box over the fuses. A bit of wire, some tack =0Asoldering and double-sided tape for battery retention =0Acould give you a 27v 'work-around' that should bring the =0Ax100K range back to life as well. =0A =0ABit lots sells an alkaline 9v for $2 or less. =0A =0ABottom line is that there may still be more years of useful =0Autility left in your venerable ol' workhorse. Working the =0Aflight line at Boeing, the Simpson 260 was all the tool =0Acribs stocked. We fixed a lot of airplanes with this genere' =0Aof measurement tools. =0A =0A =0A =0A=0A =0A=0A=C2-=0ABob . . . =0A=0A=0A=0A=0A=0ANo virus found in thi s message. =0AChecked by AVG - www.avg.com =0A08/24/12=0A=0A ________________________________________________________________________________
Date: Aug 25, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Resuscitating the Tripplet 630
At 05:48 AM 8/25/2012, you wrote: >I'm gonna have to side with Eric on this one. I think you guys are >in a nostalgia induced somnambulism that results in tons of >worthless cr*p laying around the house. By worthless, I mean things >that you will never use again. You'll just walk by it and admire it >occasionally as you worm your way through the make shift aisles to >the kitchen for yet another Ruben sandwich. Some people call it hoarding. What's this about taking sides? If anything, this thread has been a cognizant observation of what these tools represent in utility, history, and teaching value. I don't think anyone has suggested that the 260/630 genre' of tools is a substitute for modern digital instruments. At the same time, there are things an analog instrument will do for the observer that a digital instrument cannot. I still have a lot of vacuum tube era parts and tools. It is my plan to use them as teaching tools for my grandchildren . . . assuming they're interested. Building a vacuum tube receiver or transmitter requires some skill development in schematic reading, stripping wire, soldering, chassis layout, punching/drilling holes, winding coils (after we calculate how big they should be), measuring voltages and currents (yes, the 630 will do nicely). Something a vacuum tube offers that a transistor can never offer is that you can take it apart. Hold, feel and see the pieces. Imagine the boiling of electrons off a hot cathode for launching toward plate. This, like the experiments of Hertz, Helmholtz, Faraday, Volta, Ampere, et. als. is hands-on, see-it, feel-it physics. At the other end of the spectrum, programming a micro-controller is a purely intellectual exercise that has nothing to do with electronics . . . but without it, you cannot exploit the value that electronics can deliver. They are joined at the hip. The elegant solutions are achieve a working understanding of both. When I was in high school, the school board was participating in a dual-track science education experiment. One group of students took chemistry and physics in the contemporary setting while another group studied using more 'modern aids' like films and 'less sophisticated' and hardware- store/lumber-yard tools and materials. This was carried out in two Wichita high schools. The question to be answered was, "Can science be adequately taught in less endowed schools using more rudimentary tools and processes?" Don't know how powers-that-be viewed the outcome of the studies for teaching methods. I took the experimental course in chemistry. I found out from my chemistry teacher years later that I made the highest score in Wichita going in, and the highest score coming out. I can personally attest to the fact that the shiny tools and latest processes do not drive the outcome of a teaching process so strongly as modern 'educators' would have us believe. I think the point of this discussion is to explore the physics and utility of any tool for understanding and without prejudice for it's less than modern shortcomings. Would you similarly denounce a builder's choice to build a replica J-3 as opposed to a Sonex? If this discussion was about applying modern materials and systems to a 1940's restoration, would you decry the effort as whipping a dead horse? As one of my heros, Richard Feynman suggested in the tile of his book, there is a lot of pleasure to be gained from finding things out. http://www.youtube.com/watch?v=Bgaw9qe7DEE&feature=related Those who do not find pleasure in such endeavors are certainly free to focus their efforts elsewhere but let us refrain from obstructing the pleasure of others. Bob . . . ________________________________________________________________________________
Date: Aug 25, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Resuscitating the Tripplet 630
At 04:38 PM 8/24/2012, you wrote: > >Bob, > >I replied to your 1st post before I read the 2nd. I can get 10 >Panasonic 2450 lithium cells for $12 and I'll machine a little case >to make them fit in the 30V position. I think that should take care of it. Cool. Send me some pix. Bob . . . ________________________________________________________________________________
From: Bob McCallum <robert.mccallum2(at)sympatico.ca>
Subject: Resuscitating the Tripplet 630
Date: Aug 25, 2012
While the modern digital instruments can be inexpensive and exceedingly accurate, sometimes that accuracy can be an issue especially when dealing with changing values. Trying to visualize constantly changing numbers or even read their value if the changes are rapid can be very frustrating, sometimes impossible. The old analogue instruments, while they may not read to the ultimate resolution, average changing values very well and in that dynamic situation, where the digital is useless, can give a nice, relatively stable, easy to see, reading. If what you=92re looking for is a steadily falling or rising value, then the analogue will show a nice steady needle movement (or an erratic one to show a not-so-steady change) whereas the rapidly changing numbers on a digital display don=92t help. You=92ll have almost no idea of what is going on. (Measuring the resistance of a potentiometer with both a digital and an analogue meter while smoothly turning the shaft from one extreme to the other to determine if there are any dead spots or if the pot is a linear or logarithmic taper for instance will quickly show the superiority of the analogue meter. If you want to know the precise value of a fixed resistor then the digital will be superior) In short both types are useful. Sometimes the digital is better, sometimes the analogue beats it by a mile. As in most things - - =93It depends=94 Only my .02=A2 opinion Bob McC ________________________________________________________________________________
Date: Aug 25, 2012
Subject: Need a set of leads for Tripplet 310-C
From: rparigor(at)suffolk.lib.ny.us
Hi Group I rescued a Triplett 310-C from certain death about two weeks ago. It's missing the leads for them, anything I have doesn't fit. Any ideas about getting how to get hold of a set? This unit takes two 1.5 volt batteries, not sure what size. Ron Parigoris ________________________________________________________________________________
Date: Aug 25, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Need a set of leads for Tripplet 310-C
At 10:24 AM 8/25/2012, you wrote: Hi Group I rescued a Triplett 310-C from certain death about two weeks ago. It's missing the leads for them, anything I have doesn't fit. I've not run across that model before. Here's a link to the list manuals for Tripplet legacy products: http://tinyurl.com/8tfzxt6 The battery call-outs are: [] Wow! The 1.5 volt cell is an "N" which are still very much available . . . http://tinyurl.com/9ozgmtj The 15v is too . . . http://tinyurl.com/8okd49r But a bit more expensive. Again, replacing the n-cell only might yield a very serviceable device. I think those test lead jacks accept the miniature banana plugs. Here's a link to a surplus store in Orlando that has some $high$ Pomona patch cords for cheap with what I believe is the right sized plug. A couple of these modified on one end with alligator clips would get you some leads. You could cover one of the clips with a red boot and suitably mark the other end to encourage insertion to the (+) jack. When you get it running, show a kid what it does for you. Bob . . . ________________________________________________________________________________
Date: Aug 25, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Resuscitating the Tripplet 630
At 11:48 AM 8/25/2012, you wrote: >Bob, > >There was a Simpson 260 in my dad=92s stuff as >well ' in the same kind of case as you >describe. I think it will get a place of honor on the test bench, too. > >Just for grins I looked on ebay: they go for >$20-$200. Does anyone remember what they sold for new? Yup, at least in 1961 both the Tripplet 630 and Simpson 260 sold for about $70. That's about $500 in today's dollars. It was a week's wages for me at my first job in aviation at Boeing. Bob . . . ________________________________________________________________________________
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Mooney Alternator woes
Date: Aug 26, 2012
Thanks - I joined both lists and have posted my question there. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Thursday, August 16, 2012 9:54 AM Subject: Re: AeroElectric-List: Mooney Alternator woes --> There are a couple Mooney email lists that have experts that likely can help, including factory tech support. The S model isn't all that old, so there should be good info available. Mapalist mailing list..which requires membership in MAPA. Mapalist(at)lists.mooneypilots.com http://lists.mooneypilots.com/listinfo.cgi/mapalist-mooneypilots.com <http://lists.mooneypilots.com/listinfo.cgi/mapalist-mooneypilots.com> Mooney Tech list which is open to all: http://lists.aviating.com/mailman/listinfo/mooney-tech, mailto:mooney-tech-request(at)aviating.com?subject=subscribe On 8/16/2012 6:44 AM, Robert L. Nuckolls, III wrote: > > > At 08:27 AM 8/16/2012, you wrote: > > > My hangar neighbor is trying to figure out why his alternator > occasionally drops off line - requiring a weird reset sequence. He has > to shut off the battery and field, then go to a low power setting and > bring it back up again. Something about resetting an overvoltage > protection device. > > It is an M20S with Cont 550 and gear driven alternator. The first > regulator lasted only a couple of years before giving up the ghost and > the replacement was a special from Mooney. > > My first line of thinking is to locate the regulator and test it. > Nobody knows where it is hiding. > (I'm in DC - the plane is in DE...I'll be home next weekend to help > more.) > > Meanwhile, does anyone have an electronic copy of the Light Plane > Maintenance article on troubleshooting alternators...and the Mooney > M20S maintenance manual? > > If we can find it, I'm hoping that we can determine if the regulator > is the culprit. > > If it takes a southern Slobovian switch-dance to > bring it back on line, it's almost certain to be > something electronic. Is the successful reset sequence > something different than what is called for in the > POH as a response to an OV trip? > > I've not had any contact with Mooney in 25+ years. I > bid an alternator controller for them while at > Electro-Mech . . . we didn't get the job. I think > Electrodelta out of White Oak, TX got it. It would > have been a Mooney-unique product. ED has changed > hands and/or moved several times over the years. > The guy who ran ED is still hanging around the > Wichita area. He MIGHT be a resource for help > wrestling with your problem. > > The LPM article is not likely to be much help. It > will be VERY generic. If it were my airplane, I'd > jeep another regulator in place of the original to > see if the problem goes away. Given the rarity of > that regulator, I'd probably go for a one-time > STC to install something more contemporary and > available. There's nothing magic about alternator > controllers . . . only the institutionalized and > market driven B.S. in which they reside. > > B&C regulators are used elsewhere on current production > airplanes . . . the FAA might look kindly upon > substitution of B&C product for what's already > installed. > > > Bob . . . > > ----- No virus found in this message. Checked by AVG - www.avg.com ________________________________________________________________________________
Date: Aug 26, 2012
Subject: anderoid tablets
From: bob noffs <icubob(at)gmail.com>
hi all, anyone had experience with the garmin app out now for anderoid o.s. ? bob noffs hope it is good as i just ordered the google nexus 7 especially to use that app. ________________________________________________________________________________
Date: Aug 26, 2012
From: jerb <ulflyer(at)verizon.net>
Subject: Re: anderoid tablets
Don't see the relevance of the question now since you already ordered it before asking. ? ? ? At 07:39 PM 8/26/2012, you wrote: >hi all, > anyone had experience with the garmin app out now for anderoid o.s. ? > bob noffs > > hope it is good as i just ordered the google nexus 7 especially > to use that app. > ________________________________________________________________________________
From: "R. curtis" <mrspudandcompany(at)verizon.net>
Subject: Re: anderoid tablets
Date: Aug 27, 2012
> Don't see the relevance of the question now since you already ordered > it before asking. > ? ? ? The relevence, INMHO, is that there are at least a couple of us on the list that may be interested in the Garmin App, and may or may not own an Anderoid. Any info on this might be helpful. Roger ________________________________________________________________________________
From: "Bill Bradburry" <bbradburry(at)bellsouth.net>
Subject: Meter for reading Millivolts
Date: Aug 27, 2012
I think I have a bad EGT thermocouple and I have been trying to test it. One of my EGTs seems ok and the other is really low in temperature reading. When I test the two thermocouples I get either no readings or really high readings that go down when I heat the thermocouple. I bought a new VOM tester that had a temp probe as part of it to try and test the probes. But even with this tester I get nonsense readings. For example, if I plug the probe that came with the meter into the temp slot, it gives believable temp readings, but if I unplug the probe and try to read the output of the probe using the test leads and the 200MV scale, I get a reading of zero. I bought a new probe for the engine, but when I test either the new probe or the old (bad?) one with the test leads and the 200MV scale, I get the same results as above. I need to buy a meter that will read reliably on the MV scale. What meter do you suggest and where can I get one that is not too expensive? Bill B ________________________________________________________________________________
Date: Aug 27, 2012
From: Harley <harley(at)AgelessWings.com>
Subject: Re: Meter for reading Millivolts
Bill... I use this one to test my EGT and CHT thermocouples...it also has a light meter, and a temp sensor built in...I replaced my old B&K (that I had for years before it finally bit the dust) with it, and it's every bit as good... It also measures sound levels...but I haven't really tested that function yet. www.harborfreight.com/5-in-1-digital-multimeter-98674.html They currently have a 20% off coupon here as well that's good online or in the store: http://tinyurl.com/9uf4wfw Harley ----------------------------------------------------------------- On 8/27/2012 10:14 AM, Bill Bradburry wrote: > > I think I have a bad EGT thermocouple and I have been trying to test it. > One of my EGTs seems ok and the other is really low in temperature reading. > When I test the two thermocouples I get either no readings or really high > readings that go down when I heat the thermocouple. > > I bought a new VOM tester that had a temp probe as part of it to try and > test the probes. But even with this tester I get nonsense readings. > For example, if I plug the probe that came with the meter into the temp > slot, it gives believable temp readings, but if I unplug the probe and try > to read the output of the probe using the test leads and the 200MV scale, I > get a reading of zero. > > I bought a new probe for the engine, but when I test either the new probe or > the old (bad?) one with the test leads and the 200MV scale, I get the same > results as above. > > I need to buy a meter that will read reliably on the MV scale. What meter > do you suggest and where can I get one that is not too expensive? > > Bill B > > > ----- > No virus found in this message. > Checked by AVG - www.avg.com > > ________________________________________________________________________________
From: "Bill Bradburry" <bbradburry(at)bellsouth.net>
Subject: Meter for reading Millivolts
Date: Aug 27, 2012
Harley, I didn't see that one in the store. They had this one http://www.harborfreight.com/ac-dc-digital-multimeter-37772.html This is the one I bought and with it I get the nonsense readings that I describe in my previous msg. I wonder is there a trick to the testing to get accurate readings? Bill _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Harley Sent: Monday, August 27, 2012 10:29 AM Subject: Re: AeroElectric-List: Meter for reading Millivolts Bill... I use this one to test my EGT and CHT thermocouples...it also has a light meter, and a temp sensor built in...I replaced my old B&K (that I had for years before it finally bit the dust) with it, and it's every bit as good... It also measures sound levels...but I haven't really tested that function yet. www.harborfreight.com/5-in-1-digital-multimeter-98674.html They currently have a 20% off coupon here as well that's good online or in the store: http://tinyurl.com/9uf4wfw Harley _____ On 8/27/2012 10:14 AM, Bill Bradburry wrote: I think I have a bad EGT thermocouple and I have been trying to test it. One of my EGTs seems ok and the other is really low in temperature reading. When I test the two thermocouples I get either no readings or really high readings that go down when I heat the thermocouple. I bought a new VOM tester that had a temp probe as part of it to try and test the probes. But even with this tester I get nonsense readings. For example, if I plug the probe that came with the meter into the temp slot, it gives believable temp readings, but if I unplug the probe and try to read the output of the probe using the test leads and the 200MV scale, I get a reading of zero. I bought a new probe for the engine, but when I test either the new probe or the old (bad?) one with the test leads and the 200MV scale, I get the same results as above. I need to buy a meter that will read reliably on the MV scale. What meter do you suggest and where can I get one that is not too expensive? Bill B ----- No virus found in this message. Checked by AVG - www.avg.com ________________________________________________________________________________
Date: Aug 27, 2012
From: Harley <harley(at)agelesswings.com>
Subject: Re: Meter for reading Millivolts
I'm not familiar with that one, but looking at the picture, I see an input for K thermocouples...if you plug your thermocouple into those you should get an actual temperature reading (in centigrade, it seems). Maybe you are having a problem when you try to read them as millivolts using the probes on the meter instead? Even the J thermocouples will work in the K thermocouple input, just be a little bit off. Harley ----------------------------------------------------------------- On 8/27/2012 1:36 PM, Bill Bradburry wrote: > > Harley, > > I didn't see that one in the store. They had this one > > http://www.harborfreight.com/ac-dc-digital-multimeter-37772.html > > This is the one I bought and with it I get the nonsense > readings that I describe in my previous msg. I wonder is there > a trick to the testing to get accurate readings? > > Bill > > ----------------------------------------------------------------- > > *From:*owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] *On > Behalf Of *Harley > *Sent:* Monday, August 27, 2012 10:29 AM > *To:* aeroelectric-list(at)matronics.com > *Subject:* Re: AeroElectric-List: Meter for reading Millivolts > > Bill... > > I use this one to test my EGT and CHT thermocouples...it also > has a light meter, and a temp sensor built in...I replaced my > old B&K (that I had for years before it finally bit the dust) > with it, and it's every bit as good... > > It also measures sound levels...but I haven't really tested > that function yet. > > www.harborfreight.com/5-in-1-digital-multimeter-98674.html > <http://www.harborfreight.com/5-in-1-digital-multimeter-98674.html> > > They currently have a 20% off coupon here as well that's good > online or in the store: > http://tinyurl.com/9uf4wfw > > Harley > > ----------------------------------------------------------------- > > On 8/27/2012 10:14 AM, Bill Bradburry wrote: > >> >> I think I have a bad EGT thermocouple and I have been trying to test it. >> One of my EGTs seems ok and the other is really low in temperature reading. >> When I test the two thermocouples I get either no readings or really high >> readings that go down when I heat the thermocouple. >> >> I bought a new VOM tester that had a temp probe as part of it to try and >> test the probes. But even with this tester I get nonsense readings. >> For example, if I plug the probe that came with the meter into the temp >> slot, it gives believable temp readings, but if I unplug the probe and try >> to read the output of the probe using the test leads and the 200MV scale, I >> get a reading of zero. >> >> I bought a new probe for the engine, but when I test either the new probe or >> the old (bad?) one with the test leads and the 200MV scale, I get the same >> results as above. >> >> I need to buy a meter that will read reliably on the MV scale. What meter >> do you suggest and where can I get one that is not too expensive? >> >> Bill B >> >> >> >> >> >> >> >> >> ----- >> No virus found in this message. >> Checked by AVG -www.avg.com <http://www.avg.com> >> >> > > * * > * * > ** > ** > ** > *http://www.matronics.com/Navigator?AeroElectric-List* > ** > ** > *http://forums.matronics.com* > ** > ** > *http://www.matronics.com/contribution* > * * > * > > > * > > No virus found in this message. > Checked by AVG - www.avg.com <http://www.avg.com> > Date: 08/27/12 > ________________________________________________________________________________
Date: Aug 27, 2012
From: Harley <harley(at)AgelessWings.com>
Subject: Re: Meter for reading Millivolts
I just looked up the millivolt readings for a type K thermocouple at room temperature (20 c). And the problem you may be having is trying to read that with the 200 millivolt scale. It is only about 0.8mv! As long as plugging into the thermocouple slot gives you a reading near the proper temperature, the thermocouple is working...I never tried to read them on a millivolt scale as I've always had actual instruments around that could read them and have the tables built in to convert to the proper temperatures...like those two meters we've been talking about. Harley ----------------------------------------------------------------- . On 8/27/2012 1:36 PM, Bill Bradburry wrote: > > Harley, > > I didn't see that one in the store. They had this one > > http://www.harborfreight.com/ac-dc-digital-multimeter-37772.html > > This is the one I bought and with it I get the nonsense > readings that I describe in my previous msg. I wonder is there > a trick to the testing to get accurate readings? > > Bill > > ----------------------------------------------------------------- > > *From:*owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] *On > Behalf Of *Harley > *Sent:* Monday, August 27, 2012 10:29 AM > *To:* aeroelectric-list(at)matronics.com > *Subject:* Re: AeroElectric-List: Meter for reading Millivolts > > Bill... > > I use this one to test my EGT and CHT thermocouples...it also > has a light meter, and a temp sensor built in...I replaced my > old B&K (that I had for years before it finally bit the dust) > with it, and it's every bit as good... > > It also measures sound levels...but I haven't really tested > that function yet. > > www.harborfreight.com/5-in-1-digital-multimeter-98674.html > <http://www.harborfreight.com/5-in-1-digital-multimeter-98674.html> > > They currently have a 20% off coupon here as well that's good > online or in the store: > http://tinyurl.com/9uf4wfw > > Harley > > ----------------------------------------------------------------- > > On 8/27/2012 10:14 AM, Bill Bradburry wrote: > >> >> I think I have a bad EGT thermocouple and I have been trying to test it. >> One of my EGTs seems ok and the other is really low in temperature reading. >> When I test the two thermocouples I get either no readings or really high >> readings that go down when I heat the thermocouple. >> >> I bought a new VOM tester that had a temp probe as part of it to try and >> test the probes. But even with this tester I get nonsense readings. >> For example, if I plug the probe that came with the meter into the temp >> slot, it gives believable temp readings, but if I unplug the probe and try >> to read the output of the probe using the test leads and the 200MV scale, I >> get a reading of zero. >> >> I bought a new probe for the engine, but when I test either the new probe or >> the old (bad?) one with the test leads and the 200MV scale, I get the same >> results as above. >> >> I need to buy a meter that will read reliably on the MV scale. What meter >> do you suggest and where can I get one that is not too expensive? >> >> Bill B >> >> >> >> >> >> >> >> >> ----- >> No virus found in this message. >> Checked by AVG -www.avg.com <http://www.avg.com> >> >> > > * * > * * > ** > ** > ** > *http://www.matronics.com/Navigator?AeroElectric-List* > ** > ** > *http://forums.matronics.com* > ** > ** > *http://www.matronics.com/contribution* > * * > * > > > * > > No virus found in this message. > Checked by AVG - www.avg.com <http://www.avg.com> > Date: 08/27/12 > ________________________________________________________________________________
From: "Bill Bradburry" <bbradburry(at)bellsouth.net>
Subject: Meter for reading Millivolts
Date: Aug 27, 2012
They read Zero with the probes and the thermocouples have ring terminals on them so they will not fit into the sockets on the meter for the thermocouple plug. I need to be able to read them with the probes because I need to check the


July 26, 2012 - August 27, 2012

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