---------------------------------------------------------- AeroElectric-List Digest Archive --- Total Messages Posted Thu 10/02/03: 19 ---------------------------------------------------------- Today's Message Index: ---------------------- 1. 06:29 AM - relay diagram for Microair PTT (Sigma Eta Aero) 2. 07:47 AM - Re: Fast-ons (Robert L. Nuckolls, III) 3. 08:08 AM - Re: Alternator speeds and belt tensions. (Robert L. Nuckolls, III) 4. 08:18 AM - Re: Use of individual wires from a Mil-Spec (Robert L. Nuckolls, III) 5. 08:20 AM - Re: relay diagram for Microair PTT (Robert L. Nuckolls, III) 6. 08:45 AM - Re: Dielectric grease recommendations (Robert L. Nuckolls, III) 7. 09:37 AM - Re: Re: Alternator speeds and belt tensions. (Jim Jewell) 8. 10:33 AM - Re: relay diagram for Microair PTT (Sigma Eta Aero) 9. 10:57 AM - GPS-35 / Transponder / Autopilot (Phil Birkelbach) 10. 12:57 PM - Re: relay diagram for Microair PTT (Robert L. Nuckolls, III) 11. 01:52 PM - Re: relay diagram for Microair PTT (Sigma Eta Aero) 12. 02:15 PM - Re: Use of individual wires from a Mil-Spec (Charlie Kuss) 13. 02:15 PM - Re: Low voltage warning circuit (Robert L. Nuckolls, III) 14. 02:39 PM - Re: relay diagram for Microair PTT (RSwanson) 15. 02:57 PM - Re: Dielectric grease recommendations (Eric M. Jones) 16. 05:54 PM - Re: relay diagram for Microair PTT (Robert L. Nuckolls, III) 17. 06:22 PM - Re: relay diagram for Microair PTT (Sigma Eta Aero) 18. 07:13 PM - Re: Re: Alternator speeds and belt tensions. (Richard Sipp) 19. 08:50 PM - Re: Re: Low voltage warning circuit (Steven DiNieri) ________________________________ Message 1 _____________________________________ Time: 06:29:58 AM PST US From: Sigma Eta Aero Subject: AeroElectric-List: relay diagram for Microair PTT --> AeroElectric-List message posted by: Sigma Eta Aero --0-1662827501-1065101367=:90978 How exactly are the relays wired on the Microair PTTs? The schematic that Microair supplies is a little confusing for me. I don't like always having it hot. When the relays are installed how does it decide who gets to transmit if both switches are pushed (whoever is first? It becomes hot again so both can talk at the same time?) Which relays to use (prefereably something small and light and cheap)? Thanks! Joa --------------------------------- --0-1662827501-1065101367=:90978

How exactly are the relays wired on the Microair PTTs?  The schematic that Microair supplies is a little confusing for me. 

I don't like always having it hot.  When the relays are installed how does it decide who gets to transmit if both switches are pushed (whoever is first? It becomes hot again so both can talk at the same time?)

Which relays to use (prefereably something small and light and cheap)?

Thanks!

Joa


--0-1662827501-1065101367=:90978-- ________________________________ Message 2 _____________________________________ Time: 07:47:31 AM PST US From: "Robert L. Nuckolls, III" Subject: Re: AeroElectric-List: Fast-ons --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" At 06:16 AM 10/2/2003 +0200, you wrote: >--> AeroElectric-List message posted by: "John F. Herminghaus" > > >Bob, > >Just out of curiosity, why doesn't B&C use fast-ons on their voltage >regulators? > >John Herminghaus The regulator was designed in the year 8 BFO . . . (before fast ons). We were not even considering their suitability and utility in system fabrication at the time. We wrestled with whether or not to use terminal screws or some kind of connector (95% of my customers for certified product shun terminal strips . . . too easy to mess up wire placement in the field). Terminal strips were chosen for cost effectiveness. Now that these regulators are part of STC'd kits, they are for all practical purposes, cast in stone. If I do any new designs for OBAM aircraft, they will be fitted with a connector. Bob . . . ________________________________ Message 3 _____________________________________ Time: 08:08:11 AM PST US From: "Robert L. Nuckolls, III" Subject: AeroElectric-List: Re: Alternator speeds and belt tensions. --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" At 06:27 PM 10/1/2003 -0700, you wrote: >--> AeroElectric-List message posted by: "Jim Jewell" > >Hi "jerb", > >The last I heard spinning an alternator at 8000 rpm. is well within any >usefull limitations on it's bearing life. B&C alternators have racked up tens of thousands of flight hours running well over 10KRPM with great success. >As far as belt friction and adverse heat generation are conserned the older >style V-belts are happier on larger pulleys. I expect this is a big part of >why the auto industry went over to the Micro-V type belts. >Depending on the size of the larger alternator pulley you choose you might >find that the alternator output at idle is adversely effected. agree >In the past more than one builder has encountered the need to add a blister >to the cowl to clear the alternator pulley. The likelihood of this occurring >is increased when a larger diameter pulley is installed. correct >I in fact have a 3.5" pulley on my O360. this pulley clears the cowling by >about 1/4" and I might have to consider reducing it's size for cowling >clearance reasons. >The engine came with accessories and the "starter ring" had been modified to >utilize a Gates Micro-V belt that drives the alternator. >He also made the 3.5" pulley It looks to me the fellow that made the pulley >modifications did a great job and I will go with his idea until testing and >actual use cause a change of course. that was a LOT of trouble and expense for nearly immeasurable benefit . . . >I will certainly be happy to hear from a qualified person if what I have had >quoted to me as safe alternator RPM. limitations needs to be brought up to >speed (;}. > >I think a look in the archives will show that this has been hashed out some >before. >Try searching the archives wit (alternator rpm) or (alternator speed). Someone asked the question a few days ago, "What is the method for PROPER tightening of the alternator belt." A fair question since I've used the phrase many times. I and folks at B&C have been digging through the engineering literature on belts. If one wishes to install a belt for a particular tension, there are many non-cheap instruments you can purchase to actually measure and thus facilitate adjustment of belt tension. Okay, how do we pick a PROPER tension and can it be done without relying on expensive and seldom used instrumentation. Further, in light of more than half a century of "stick the crowbar in there, stretch 'er tighter than hell and cinch it down" techniques used in FBO and OBAM aircraft shops alike, belt life has not bubbled up to the top of our most pressing maintenance problems. After several days of picking though the sparse data, I'm about to conclude that actual tension settings for any particular application are empirically derived by the system engineer, not the belt engineer. Belts are loosely spec'd for horsepower ratings assuming a certain RPM (usually 1750 - common motor output speed for many industrial situations) on the smallest pulley . . . which has nothing in common with the way we use the belts on airplanes. Intuitively, a belt running too tight is overstressed and life is reduced while bearing loads are excessive and reduces life of those components as well. A belt too loose slips, wears rapidly and prevents the alternator from running at max performance. The range of tension values between too tight and too loose is huge. Obviously, from the pilot's perspective, the best thing is to err on the side of too tight and watch the belt for service life issues on the ground instead of discovering them in the air. Given our knowledge of decades of service history watching quality (Gates) belts run quality (ND) alternators, the loosely defined tightening technique defined above seems quite adequate. Every time I fly, fingers run over the surface of the belt looking for any signs of frayed edges and eyes look for signs of overheat-polish on belt sides. A tug on the belt confirms that it still "cinched down tight." I've never had to abort a mission due to discovery of a questionable alternator belt. Sooo . . . if it were my airplane, (and given the small cost of a belt compared to other costs of owning an airplane) I'd continue to do the crowbar operation for tightening and put a new belt on the a new battery every year. Both of these items will be at the bottom of the list for flight safety and/or maintenance concerns. Bob . . . ________________________________ Message 4 _____________________________________ Time: 08:18:52 AM PST US From: "Robert L. Nuckolls, III" Subject: Re: AeroElectric-List: Use of individual wires from a Mil-Spec C-27500 cable --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" At 11:11 PM 10/1/2003 -0400, you wrote: >--> AeroElectric-List message posted by: Charlie Kuss > >Bob & Listers, > I was given a large quantity of Mil Spec Aviation wiring from a friend. > Some of this wire was 22 & 20 gauge C-27500 shielded 2 & 3 wire cable. > Some of this cable had been stripped of it's outer sheath and shielding. > This cable has color coded wires inside (red, blue & yellow). Are these > individual wires OK to use on my RV-8A project? It appears that the > insulation is slightly thinner on these wires as compared to individual > Mil 22759/16 wires. I'd like to use this wire, but I want to make sure > that I am not "cutting corners" in doing so. Opinions please. >Charlie Kuss >RV-8A going cross eyed looking at wiring schematics >SE Florida Mil-C-27500 is an ASSEMBLY specification for bringing a variety of materials (wires, shielding and outer jackets) together into bundles of wire that may be shielded. See: http://www.awcwire.com/pdf/CT-G4-M27500.pdf Given the relatively modern incarnation of this specification it is unlikely that anything you find assembled under it will be unsuited for use in your airplane. I'd say, "drive on and let not your heart be troubled." Bob . . . ________________________________ Message 5 _____________________________________ Time: 08:20:25 AM PST US From: "Robert L. Nuckolls, III" Subject: Re: AeroElectric-List: relay diagram for Microair PTT --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" At 06:29 AM 10/2/2003 -0700, you wrote: >--> AeroElectric-List message posted by: Sigma Eta Aero > >--0-1662827501-1065101367=:90978 > > >How exactly are the relays wired on the Microair PTTs? The schematic that >Microair supplies is a little confusing for me. > >I don't like always having it hot. When the relays are installed how does >it decide who gets to transmit if both switches are pushed (whoever is >first? It becomes hot again so both can talk at the same time?) > >Which relays to use (prefereably something small and light and cheap)? > >Thanks! > >Joa I'm not familiar with any schematics provided by Microair that incorporate relays. Can you point me to an internet resource where I can find the drawing in question? Bob . . . ________________________________ Message 6 _____________________________________ Time: 08:45:30 AM PST US From: "Robert L. Nuckolls, III" Subject: Re: AeroElectric-List: Dielectric grease recommendations --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" At 04:11 PM 9/28/2003 -0400, you wrote: >--> AeroElectric-List message posted by: Gkb5577@aol.com > >I'm new to the forum. I just got some dielectric grease off Ebay--3 tubes ( >big ones) for about $20. I'm curious too can bearing grease work? The idea >must have started some time ago with an old-timer and I JUST BET that the >type >actually isn't all that important. (?????) Geoff If one is pre-disposed to use guckums to enhance the performance of a connection and there is a rational justification for them, probably any grease would add some level of enhancement. Having said that, I've never seen a magic potion called out on the installation drawings for any crimped terminal going into a production airplane. There is a VERY strong reluctance to use a design where "protective" processes are necessary or useful. We work hard to design out the need for any such techniques on the assembly line. Had a conversation just yesterday about a bofa-fide need to seal exposed terminals on a vendor supplied product that gets routinely rained on every time the airplane descends from altitude. We moved the sealing process from our assembly line to the manufacturer's facility where it can be inspected and controlled. There was no way we were going to ask a line mechanic to do this with repeatable results. Bottom line is that there may be a valid, engineered requirement for sprays, goops and goos in the assembly of your airplane . . . if you're concerned about a particular situation, let's pick it apart and discover the physics behind the need. Bob . . . ________________________________ Message 7 _____________________________________ Time: 09:37:46 AM PST US From: "Jim Jewell" Subject: Re: AeroElectric-List: Re: Alternator speeds and belt tensions. --> AeroElectric-List message posted by: "Jim Jewell" ----- Original Message ----- From: "Robert L. Nuckolls, III" Subject: AeroElectric-List: Re: Alternator speeds and belt tensions. > >The engine came with accessories and the "starter ring" had been modified to > >utilize a Gates Micro-V belt that drives the alternator. > >He also made the 3.5" pulley It looks to me the fellow that made the pulley > >modifications did a great job and I will go with his idea until testing and > >actual use cause a change of course. > > that was a LOT of trouble and expense for nearly > immeasurable benefit . . . Right you are Bob, It sure looks cool though! ... Lets just call it a dramatic non event (:-)! Jim in Kelowna ________________________________ Message 8 _____________________________________ Time: 10:33:54 AM PST US From: Sigma Eta Aero Subject: Re: AeroElectric-List: relay diagram for Microair PTT --> AeroElectric-List message posted by: Sigma Eta Aero --0-1913595621-1065116012=:42806 www.microair.com.au/admin/uploads/ 760_install_&_user_manual_ver_M.pdf It's hard to read for some reason in this PDF but in my manual (hardcopy with the radio) it's on about page 20 and is the third "option" called "PTT relays for single mic operation". I asked a fellow here at work and he said just use two dpdt relays and wire the appropriate terminals for NC and NO but I'm wanting specific suggestions for relays that are small, light, and cheap (solid state maybe?). I'm surprised this hasn't been addressed before since it's a pain to get the co-pilot to stop talking whenever you want to make a radio call. Thanks! Joa ++++++++++++++++++++++ "Robert L. Nuckolls, III" wrote: I'm not familiar with any schematics provided by Microair that incorporate relays. Can you point me to an internet resource where I can find the drawing in question? --------------------------------- --0-1913595621-1065116012=:42806
www.microair.com.au/admin/uploads/ 760_install_&_user_manual_ver_M.pdf
 
It's hard to read for some reason in this PDF but in my manual (hardcopy with the radio) it's on about page 20 and is the third "option" called "PTT relays for single mic operation".
 
I asked a fellow here at work and he said just use two dpdt relays and wire the appropriate terminals for NC and NO but I'm wanting specific suggestions for relays that are small, light, and cheap (solid state maybe?). 
 
I'm surprised this hasn't been addressed before since it's a pain to get the co-pilot to stop talking whenever you want to make a radio call.
 
Thanks!
 
Joa
 

++++++++++++++++++++++
"Robert L. Nuckolls, III" <bob.nuckolls@cox.net> wrote:
I'm not familiar with any schematics provided by
Microair that incorporate relays. Can you point me to
an internet resource where I can find the drawing
in question?





--0-1913595621-1065116012=:42806-- ________________________________ Message 9 _____________________________________ Time: 10:57:14 AM PST US From: "Phil Birkelbach" Subject: AeroElectric-List: GPS-35 / Transponder / Autopilot --> AeroElectric-List message posted by: "Phil Birkelbach" I am going to have the Garmin GPS-35 feeding the heading info to my TruTrak autopilot and I was wondering if I could also hook this signal up to my Garmin GTX-327 transponder for the automatic ALT/STBY switch? I would assume that if I paralleled the two that it may work but I thought that I would ask. Godspeed, Phil Birkelbach - Houston Texas RV-7 N727WB (Reserved) - Canopy http://www.myrv7.com ________________________________ Message 10 ____________________________________ Time: 12:57:34 PM PST US From: "Robert L. Nuckolls, III" Subject: Re: AeroElectric-List: relay diagram for Microair PTT --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" At 10:33 AM 10/2/2003 -0700, you wrote: >--> AeroElectric-List message posted by: Sigma Eta Aero > >--0-1913595621-1065116012=:42806 > >www.microair.com.au/admin/uploads/ 760_install_&_user_manual_ver_M.pdf > > >It's hard to read for some reason in this PDF but in my manual (hardcopy >with the radio) it's on about page 20 and is the third "option" called >"PTT relays for single mic operation". > >I asked a fellow here at work and he said just use two dpdt relays and >wire the appropriate terminals for NC and NO but I'm wanting specific >suggestions for relays that are small, light, and cheap (solid state maybe?). > >I'm surprised this hasn't been addressed before since it's a pain to get >the co-pilot to stop talking whenever you want to make a radio call. > >Thanks! Downloaded the manual . . . UGHhhhh! I offered to do real wiring diagrams that depicted how to connect wires together and now I see that the latest manual is not only worse for diagrams, (nobody should attempt to hook up the system in the manner depicted) the .pdf file was generated with some odd-ball font that probably only prints in part of the world. Okay, you want opposite mic disable when a PTT button is pushed. Do you want the copilot to have radio access too or just intercom? Let's figure out what's needed and do a real wiring diagram. Bob . . . ________________________________ Message 11 ____________________________________ Time: 01:52:23 PM PST US From: Sigma Eta Aero Subject: Re: AeroElectric-List: relay diagram for Microair PTT --> AeroElectric-List message posted by: Sigma Eta Aero --0-1573740537-1065127919=:49265 You mean an intercom that requires a button to be pushed to talk to the co-pilot? No, I'm fine with the always hot intercom, it's just the always hot PTT (transmit on the radio) that I don't like. I would like both the pilot and the co-pilot to have PTT buttons and when one pushes theirs it cuts the other person off from talking. If you can't read the diagram I can describe what they are doing (though you obviously know already Im sure). Both relays have one NC terminal going to each mic ring terminal and another terminal in parallel with each other going between the PTT pin (7) and ground. Basically it works so when one PTT is pushed that relay closes the radio PTT circuit and opens the other persons microphone connection so that they cant talk. The Microair circuit looks fine and is pretty elementary(well, it is to me *after* the EE from work explained it!). Im just wanting your expertise in finding a couple nice tiny (but inexpensive) relays (preferably something I can solder in line and just cover with heat shrink) that will work with the currents we have here. Would be great though if you could add this feature to your manual since as you noticed the Microair manual is pretty lacking! Im sure others that arent using a separate intercom would benefit. Thanks Bob! Joa "Robert L. Nuckolls, III" wrote: Okay, you want opposite mic disable when a PTT button is pushed. Do you want the copilot to have radio access too or just intercom? Let's figure out what's needed and do a real wiring diagram. --------------------------------- --0-1573740537-1065127919=:49265

You mean an intercom that requires a button to be pushed to talk to the co-pilot?  No, I'm fine with the always hot intercom, it's just the always hot PTT (transmit on the radio) that I don't like. 

 

I would like both the pilot and the co-pilot to have PTT buttons and when one pushes theirs it cuts the other person off from talking.

 

If you can't read the diagram I can describe what they are doing (though you obviously know already Im sure).  Both relays have one NC terminal going to each mic ring terminal and another terminal in parallel with each other going between the PTT pin (7) and ground.  Basically it works so when one PTT is pushed that relay closes the radio PTT circuit and opens the other persons microphone connection so that they cant talk.

 

The Microair circuit looks fine and is pretty elementary(well, it is to me *after* the EE from work explained it!).   Im just wanting your expertise in finding a couple nice tiny (but inexpensive) relays (preferably something I can solder in line and just cover with heat shrink) that will work with the currents we have here.

 

Would be great though if you could add this feature to your manual since as you noticed the Microair manual is pretty lacking!  Im sure others that arent using a separate intercom would benefit.

 

Thanks Bob!

 

Joa


"Robert L. Nuckolls, III" <bob.nuckolls@cox.net> wrote:
Okay, you want opposite mic disable when a PTT button
is pushed. Do you want the copilot to have radio access
too or just intercom? Let's figure out what's needed
and do a real wiring diagram.


--0-1573740537-1065127919=:49265-- ________________________________ Message 12 ____________________________________ Time: 02:15:18 PM PST US From: Charlie Kuss Subject: Re: AeroElectric-List: Use of individual wires from a Mil-Spec C-27500 cable --> AeroElectric-List message posted by: Charlie Kuss At 10:18 AM 10/2/2003 -0500, you wrote: >--> AeroElectric-List message posted by: "Robert L. Nuckolls, III" > >At 11:11 PM 10/1/2003 -0400, you wrote: >>--> AeroElectric-List message posted by: Charlie Kuss >> >>Bob & Listers, >> I was given a large quantity of Mil Spec Aviation wiring from a friend. >> Some of this wire was 22 & 20 gauge C-27500 shielded 2 & 3 wire cable. >> Some of this cable had been stripped of it's outer sheath and shielding. >> This cable has color coded wires inside (red, blue & yellow). Are these >> individual wires OK to use on my RV-8A project? It appears that the >> insulation is slightly thinner on these wires as compared to individual >> Mil 22759/16 wires. I'd like to use this wire, but I want to make sure >> that I am not "cutting corners" in doing so. Opinions please. >>Charlie Kuss >>RV-8A going cross eyed looking at wiring schematics >>SE Florida > > Mil-C-27500 is an ASSEMBLY specification for bringing a variety > of materials (wires, shielding and outer jackets) together into > bundles of wire that may be shielded. See: > > http://www.awcwire.com/pdf/CT-G4-M27500.pdf > > Given the relatively modern incarnation of this specification > it is unlikely that anything you find assembled under it > will be unsuited for use in your airplane. I'd say, "drive > on and let not your heart be troubled." > > Bob . . . Bob, Thanks for your opinion. My mind is now relieved! :-) I had already visited the web page listed above. I have even printed it out. I like the table which explains what the numbers after the / in the Mil-Spec number mean. (They relate to the type of insulation on the wire) I've found several other useful pages on Allied's site. Charlie Kuss ________________________________ Message 13 ____________________________________ Time: 02:15:18 PM PST US From: "Robert L. Nuckolls, III" Subject: AeroElectric-List: Re: Low voltage warning circuit --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" > > >On the schematic and BOM (9021-620 dated 9/14/2) R116 is 68 but in the >pictures included in > >http://www.aeroelectric.com/articles/lvwarn/9021-620.pdf >this resistor is 62. Now if each is off the 5% tolerance in the right >direction this won t matter mathematically but I can t judge how this >otherwise affects the circuit, nor can I assume that there will be a >statistical fluke making my point moot, so I need to ask what is the >correct value? I bashed this out in a hurry but I think the schematic and BOM have been brought into agreement with present manufacturing configuration. See http://www.aeroelectric.com/articles/lvwarn/9021-620.pdf If you've downloaded this recently, your browser may have the old version in cache . . . hit the reload button after download to make sure you get the latest. The schematic and BOM pages will have Rev A 10/2/3 in the title block on the latest document. Bob . . . ________________________________ Message 14 ____________________________________ Time: 02:39:08 PM PST US From: "RSwanson" Subject: Re: AeroElectric-List: relay diagram for Microair PTT --> AeroElectric-List message posted by: "RSwanson" > I asked a fellow here at work and he said just use two dpdt relays and wire the appropriate terminals for NC and NO but I'm wanting specific suggestions for relays that are small, light, and cheap (solid state maybe?). Try http://www.jameco.com/ , they have a nice assortment of solid and coil relays at very reasonable prices. R ________________________________ Message 15 ____________________________________ Time: 02:57:54 PM PST US From: "Eric M. Jones" Subject: AeroElectric-List: Re: Dielectric grease recommendations --> AeroElectric-List message posted by: "Eric M. Jones" Many people think a dielectric grease might contaminate the surface of a conductor. Of course this is not true, the grease merely fills in the air gaps. Although a "proper" crimp may be gas tight, only the conductor under the crimp is so blessed. Under a microscope the cable will be seen to possess many small channels in the pack. In theory, the channels can wick moisture and contaminants (historically battery acid) into the crimp. Why is this a concern? If all the metal in the joint were the same, we might still want to exclude water because it can freeze and force the joint open. However, a more critical need is to seal the airspaces because of the likelihood that electrolytic corrosion will occur. The metal crimp itself may be aluminum or brass or copper, the plating may be nickel or more likely tin, and the wire may be copper, and ever nickel tin or zinc plated. So electrolytic corrosion can occur. Indoors this is rarely an issue, but aircraft see a lot of water in their lives; it's a good idea to keep it out of the crimp. Regards, Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge MA 01550-2705 Phone (508) 764-2072 Email: emjones@charter.net When the Okies moved to California they raised the average IQ of both states. ---Will Rogers ________________________________ Message 16 ____________________________________ Time: 05:54:57 PM PST US From: "Robert L. Nuckolls, III" Subject: Re: AeroElectric-List: relay diagram for Microair PTT --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" At 01:51 PM 10/2/2003 -0700, you wrote: >--> AeroElectric-List message posted by: Sigma Eta Aero > >--0-1573740537-1065127919=:49265 > > >You mean an intercom that requires a button to be pushed to talk to the >co-pilot? No, I'm fine with the always hot intercom, it's just the always >hot PTT (transmit on the radio) that I don't like. > > >I would like both the pilot and the co-pilot to have PTT buttons and when >one pushes theirs it cuts the other person off from talking. > > >If you can't read the diagram I can describe what they are doing (though >you obviously know already Im sure). Both relays have one NC terminal >going to each mic ring terminal and another terminal in parallel with each >other going between the PTT pin (7) and ground. Basically it works so >when one PTT is pushed that relay closes the radio PTT circuit and opens >the other persons microphone connection so that they cant talk. Wasn't concerned about reading Microair's diagram, just wanted to know how you wanted the system to work. The important part of working is do you want pilot priority (pushing pilot PTT overrides copilot even if already pushed) or mutual priority (first come first served with no override from either position). >The Microair circuit looks fine and is pretty elementary(well, it is to me >*after* the EE from work explained it!). Im just wanting your expertise >in finding a couple nice tiny (but inexpensive) relays (preferably >something I can solder in line and just cover with heat shrink) that will >work with the currents we have here. Tiny relays and soldering in-line are mutually incompatible features. Tiny relays mount to etched circuit boards and very non-robust terminals. Years ago, the relay of choice for what you're wanting to do was Potter-Brumfield 4PDT KHA series relays. They're cheap from Digikey (cat #PB142), and can either be soldered to directly with wires and heat- shrink or you can install them in a socket (Cat #PB144) and hold relay in place with spring wire bail (Cat #PB146). >Would be great though if you could add this feature to your manual since >as you noticed the Microair manual is pretty lacking! Im sure others that >arent using a separate intercom would benefit. I can do that, but it's two drawings to offer the variants cited above. Bob . . . PS. get into your email client option and shut off the HTML feature. Your message to the list was transmitted in both text and html . . . ________________________________ Message 17 ____________________________________ Time: 06:22:27 PM PST US From: Sigma Eta Aero Subject: Re: AeroElectric-List: relay diagram for Microair PTT --> AeroElectric-List message posted by: Sigma Eta Aero --0-381469590-1065144131=:62240 Whichever is easier. Probably first come first served since I will be flying from the back seat a bit (or I wouldn't even put a PTT there). Also, I assume diodes will have to go across the switching contacts to prevent spikes? Don't know what to do about the HTML messages- I'm using Yahoo Mail and went into preferences but couldn't find any way to switch it off. Thanks! Joa ********************************************************** Wasn't concerned about reading Microair's diagram, just wanted to know how you wanted the system to work. The important part of working is do you want pilot priority (pushing pilot PTT overrides copilot even if already pushed) or mutual priority (first come first served with no override from either position). --------------------------------- --0-381469590-1065144131=:62240

Whichever is easier.  Probably first come first served since I will be flying from the back seat a bit (or I wouldn't even put a PTT there).

Also, I assume diodes will have to go across the switching contacts to prevent spikes?

Don't know what to do about the HTML messages- I'm using Yahoo Mail and went into preferences but couldn't find any way to switch it off. 

Thanks!

Joa

 

 

**********************************************************
Wasn't concerned about reading Microair's diagram, just
wanted to know how you wanted the system to work. The important
part of working is do you want pilot priority (pushing pilot
PTT overrides copilot even if already pushed) or mutual priority
(first come first served with no override from either position).


--0-381469590-1065144131=:62240-- ________________________________ Message 18 ____________________________________ Time: 07:13:56 PM PST US From: "Richard Sipp" Subject: Re: AeroElectric-List: Re: Alternator speeds and belt tensions. --> AeroElectric-List message posted by: "Richard Sipp" Sorry that I can't quote a source, but recently I read that a practical way to measure drive belt tension on an alternator is to measure the torque required to turn the alternator pulley until it slips in the pulley with the belt adjusted where you think it should be. Unfortunately I also don't recall what the suggested torque reading was...maybe 10 ft. lbs. Anyway, it should be easy to set by any other method and then measure the "slip" torque. Dick Sipp RV10 N110DV RV4 N250DS ________________________________ Message 19 ____________________________________ Time: 08:50:55 PM PST US From: "Steven DiNieri" Subject: RE: AeroElectric-List: Re: Low voltage warning circuit --> AeroElectric-List message posted by: "Steven DiNieri" Bob, how could I make the low volt warning threshold adjustable or lower than 13v? I need a device to monitor rear batteries under load in a "rec vehicle" and trigger a remote start at a voltage just above the typical alarm in a large power inverter. Steve DiNieri Rv-6a n221rv I bashed this out in a hurry but I think the schematic and BOM have been brought into agreement with present manufacturing configuration. See http://www.aeroelectric.com/articles/lvwarn/9021-620.pdf If you've downloaded this recently, your browser may have the old version in cache . . . hit the reload button after download to make sure you get the latest. The schematic and BOM pages will have Rev A 10/2/3 in the title block on the latest document. Bob . . .