AeroElectric-List Digest Archive

Tue 02/17/15


Total Messages Posted: 10



Today's Message Index:
----------------------
 
     1. 04:21 AM - Re: 12v vs 14v System? (mmayfield)
     2. 04:49 AM - Re: Re: 12v vs 14v System? (Werner Schneider)
     3. 06:20 AM - Re: Re: 12v vs 14v System? (Bob McCallum)
     4. 08:06 AM - Re: Risks associated with unproven crimp tools . . . (GLEN MATEJCEK)
     5. 10:26 AM - Re: Re: Risks associated with unproven crimp tools . . . (Robert L. Nuckolls, III)
     6. 11:11 AM - Re: Re: Risks associated with unproven crimp tools . . . (Kent or Jackie Ashton)
     7. 11:12 AM - Re: Re: Risks associated with unproven crimp tools . . . (Ron Walker)
     8. 12:23 PM - Re: Re: Risks associated with unproven crimp tools . . . (Robert L. Nuckolls, III)
     9. 01:30 PM - Re: weird radio trouble (Justin Jones)
    10. 01:43 PM - Re: Re: Risks associated with unproven crimp tools . . . (C&K)
 
 
 


Message 1


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    Time: 04:21:25 AM PST US
    Subject: Re: 12v vs 14v System?
    From: "mmayfield" <mmayfield@ozemail.com.au>
    I didn't ask for "standard voltages". I wrote "standard terms". That is, standard "terminology" to describe a type of system. You have some manufacturers calling it a "12v system" and others a "14v system". What's so hard about keeping the terminology consistent when they're talking about the exact same thing? -------- Mike Read this topic online here: http://forums.matronics.com/viewtopic.php?p=438440#438440


    Message 2


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    Time: 04:49:36 AM PST US
    From: Werner Schneider <glastar@gmx.net>
    Subject: Re: 12v vs 14v System?
    Mike agree with your confusion about standards. We might put it a bit like following: -with engine stopped you will have a 12V system -with engine running you will have a 14V system this not taking into account the digits behind the decimal as well as assuming a standard PB battery Cheers Werner On 17.02.2015 13:19, mmayfield wrote: > > I didn't ask for "standard voltages". I wrote "standard terms". That is, standard "terminology" to describe a type of system. >


    Message 3


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    Time: 06:20:20 AM PST US
    From: Bob McCallum <robert.mccallum2@sympatico.ca>
    Subject: Re: 12v vs 14v System?
    Throwing charging voltages into the mix is where the confusion arises. Going back 100 or so years=2C cars were 6 volt=2C then in the early 50's al ong came the improvement to 12 volt. No one mentioned that those 6 volt bat teries were charged at some higher voltage (which they were) and no one men tioned that the "new" 12 volt cars charged at a higher voltage still. Almos t everyone referes to car electrical systems as "12 volt" and doesn't worry about the subtle detail of actual measured voltages unless trouble shootin g for some perceived problem. When was the last time you heard anyone refer to their 14 volt car???? Aircraft are fundamentally the same. With aircraf t (smaller ones at least) the "standard" systems have traditionally been 12 or 24 volt systems. While bringing the fact of higher charging voltages in to the mix is technically correct=2C there is no need to play semantics of whether the system is 12V or 14V. (or 14.2V or 13.9V) It's the same system. The details of actual measured voltages at any point in time do not change the fact the system is either 12 volt or 24 volt even if you can measure 2 8.4 volts with your voltmeter. Keep it simple as you're unlikely to be tech nically accurate at any point in time. Bob McC > Date: Tue=2C 17 Feb 2015 13:48:09 +0100 > From: glastar@gmx.net > To: aeroelectric-list@matronics.com > Subject: Re: AeroElectric-List: Re: 12v vs 14v System? > t> > > Mike agree with your confusion about standards. We might put it a bit > like following: > > -with engine stopped you will have a 12V system > -with engine running you will have a 14V system > > this not taking into account the digits behind the decimal as well as > assuming a standard PB battery > > Cheers Werner > > On 17.02.2015 13:19=2C mmayfield wrote: .com.au> > > > > I didn't ask for "standard voltages". I wrote "standard terms". That is =2C standard "terminology" to describe a type of system. > > > =========== =========== =========== =========== > > >


    Message 4


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    Time: 08:06:27 AM PST US
    Subject: Re: Risks associated with unproven crimp tools . .
    .
    From: GLEN MATEJCEK <fly4grins@gmail.com>
    I was going down that very path, but the fellow at the rather large welding supply house told me it would take $10 per terminal to do the crimps, or for $10 I could by my own tool. This particular widget can be bolted to a bench or held in a substantial vise and then operated with an appropriately calibrated Inertial Motivator, in this case a 2 1/2 pound sledge. Works like a charm. I did solder the ring end of the crimps, both to definitively seal and electrically bond the joint. The cable end of the crimp is treated with liquid electrical tape and heat shrink tubing. One caution: If there is to be a bend in the cable close to the terminal, approximate the bend prior to setting the crimp. The final product will be much easier to use. > > ***SNIP*** > If you use welding cable for your fat-wires, the weld shop > where you bought the wire can probably sell you terminals and > install them with proven tools. > ***SNIP*** > >


    Message 5


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    Time: 10:26:14 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Risks associated with unproven crimp tools
    . . . Just for grins, I put new terminals on the end of the test article I received. Voltage drop across the segment (terminal to terminal) went down from 9+ millivolts to 2.6 millivolts . . . the calculated drop for the wire itself. In other words, joint resistance at the terminal interface added no resistance I could measure . . . At 10:05 2015-02-17, you wrote: I was going down that very path, but the fellow at the rather large welding supply house told me it would take $10 per terminal to do the crimps, or for $10 I could by my own tool. Yes. A few months back we discussed this item from Harbor Freight . . . http://tinyurl.com/3tfwav3 I just checked the reviews again and they're good. Comes with a broad range of die sets that cover the probable range of needs in our airplanes. I may pop for one of these and do an article on it. If you have more than a half-dozen fat wire terminals to install . . . and you don't want to solder . . . this is a good value option. =C2 This particular widget can be bolted to a bench or held in a substantial vise and then operated with an appropriately calibrated Inertial Motivator, in this case a 2 1/2 pound sledge.=C2 Works like a charm.=C2 I did solder the ring end of the crimps, both to definitively seal and electrically bond the joint.=C2 The cable end of the crimp is treated with liquid electrical tape and heat shrink tubing. =C2 The operative word here is SOLDER . . . keep in mind that the design goal calls for 'gas tight' interface between wire strands and the terminal's wire-trip barrel. The minimum-fuss technique calls for a rather well calibrated mash of wire grip barrel around the strands. One stroke . . . done right. The other technique described in my article calls for filling all voids of the joint with solder and (as necessary) copper wedges. EITHER technique (or as Glen points out) a COMBINATION of processes all go to achievement of the gas-tight design goal . . . lack of calibration for hammer blows becomes moot. The terminals I just installed were solder only. The terminal was snug on the wire so no wedges were called for. One caution: =C2 If there is to be a bend in the cable close to the terminal, approximate the bend prior to setting the crimp.=C2 The final product will be much easier to use. Yes . . . 'aircraft' wire is exceedingly picky for bend allowances. I MUCH prefer welding cable. Bob . . .


    Message 6


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    Time: 11:11:34 AM PST US
    Subject: Re: Risks associated with unproven crimp tools
    . . .
    From: Kent or Jackie Ashton <kjashton@vnet.net>
    Bob, had any experience soldering terminals to copper-cladded aluminum (CCA) cable? I tried a couple of time using a propane torch with flux added and w ithout flux. The solder just did not want to merge with the materials. Alw ays found it pretty easy with copper cable. -kent > On Feb 17, 2015, at 1:24 PM, Robert L. Nuckolls, III <nuckolls.bob@aeroele ctric.com> wrote: > > The operative word here is SOLDER . . . keep in mind > that the design goal calls for 'gas tight' interface > between wire strands and the terminal's wire-trip > barrel.


    Message 7


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    Time: 11:12:48 AM PST US
    From: Ron Walker <n520tx@gmail.com>
    Subject: Re: Risks associated with unproven crimp tools
    . . . First hand experience with this product. I've used it for all battery/ground cables for my 7a and 10. Crimps the copper terminals to the welding cable with ease. --Ron On 2/17/2015 12:24 PM, Robert L. Nuckolls, III wrote: > * Yes. A few months back we discussed this item from > Harbor Freight . . . > > http://tinyurl.com/3tfwav3 > > I just checked the reviews again and they're good. > Comes with a broad range of die sets that cover > the probable range of needs in our airplanes. > I may pop for one of these and do an article > on it. If you have more than a half-dozen > fat wire terminals to install . . . and you don't > want to solder . . . this is a good value option.*


    Message 8


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    Time: 12:23:13 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Risks associated with unproven crimp tools
    . . . At 13:10 2015-02-17, you wrote: Bob, had any experience soldering terminals to copper-cladded aluminum (CCA) cable? I tried a couple of time using a propane torch with flux added and without flux. The solder just did not want to merge with the materials. Always found it pretty easy with copper cable. -kent Yes. At least the cable that Eric was selling a few years ago. He sent me a sample and I successfully crimped and soldered terminals to the wire. Not sure about how much copper cladding 'washes' off into the solder/copper amalgam of a finished joint. To be sure, if the copper is too thin to solder, aluminum exposed by solder at the base of the melt would pose new questions as to the joint's quality. But of course, copper terminals onto copper wire is a low-risk effort. Bob . . .


    Message 9


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    Time: 01:30:24 PM PST US
    Subject: Re: weird radio trouble
    From: Justin Jones <jmjones2000@mindspring.com>
    Condensation forming on all exterior surfaces can also equal condensation on internal surfaces. Make sure all radio connections (especially antenna connections) are clean, d ry, and free from corrosion. I have seen these symptoms with moisture inside of a connector. Good on the g round but when you take off and fly, the temperature drops and the moisture f reezes causing increased resistance. Be sure to recheck all grounds as well. Pay close attention to the grounds t hat were touched in the replacement of the engine. Good luck Justin > On Feb 16, 2015, at 10:19, B Tomm <fvalarm@rapidnet.net> wrote: > > > > A hangar neighbor did an engine overhaul last fall. The airplane didn't f ly for about 5 months. It sat in a hangar the whole time. Now that it's fly ing again, there's a new weird radio problem that we can't figure out. > > Initial radio operation (on the ground) is... not stellar but OK (maybe 4/ 5 for clarity). After airborne for a short time (less than 1/2 hour) commu nications becomes so poor that radio contact with the tower cannot be mainta ined. > > Aircraft is BD4 (aluminum skins) > Comm antenna is on top ala Cessna 172 etc > > The alternator is also new with the engine overhaul. Plane Power internal ly regulated. > > At first we thought it was a low battery (sitting for 5 months) or alterna tor problem but a recently added multimeter reveals 14.5V while flying. > > The hangar has been very humid at times with condensation forming on all t he exterior surfaces. So we are wondering about corrosion or connection iss ues. But comms on the ground are much better than in the air. That may be j ust following the trend that initial communications is always better. It see ms to deteriorate a little after being airborne. > > Any ideas? > > Bevan > > > > > > 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3 D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3 D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3 D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3 D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D >


    Message 10


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    Time: 01:43:59 PM PST US
    From: C&K <yellowduckduo@gmail.com>
    Subject: Re: Risks associated with unproven crimp tools
    . . . Could it be the flux? I've never worked with CCA but it might be worth trying one of the newer electronic solders while being careful not to overheat. In comparison my old standby rosin core solder performs poorly on less than perfectly clean tinned joints. I was given a partial roll that is only identified as a Kester product but it works much better. Ken On 17/02/2015 3:21 PM, Robert L. Nuckolls, III wrote: > <nuckolls.bob@aeroelectric.com> > > At 13:10 2015-02-17, you wrote: > Bob, had any experience soldering terminals to copper-cladded aluminum > (CCA) cable? I tried a couple of time using a propane torch with flux > added and without flux. The solder just did not want to merge with > the materials. Always found it pretty easy with copper cable. > -kent > > Yes. At least the cable that Eric was selling > a few years ago. He sent me a sample and I successfully > crimped and soldered terminals to the wire. > > Not sure about how much copper cladding 'washes' > off into the solder/copper amalgam of a finished > joint. To be sure, if the copper is too thin to > solder, aluminum exposed by solder at the base > of the melt would pose new questions as to the > joint's quality. > > But of course, copper terminals onto copper wire > is a low-risk effort. > > > Bob . . . > >




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