AeroElectric-List Digest Archive

Sun 10/23/05


Total Messages Posted: 12



Today's Message Index:
----------------------
 
     1. 08:23 AM - Re: welding cable (Gaylen Lerohl)
     2. 08:53 AM - Re: Re: welding cable  (Charlie Kuss)
     3. 09:33 AM - Re: welding cable (Bob McCallum)
     4. 10:04 AM - Re: Re: Circuit Breakers (Robert L. Nuckolls, III)
     5. 10:22 AM - Re: Hobbs meter wiring (Robert L. Nuckolls, III)
     6. 10:44 AM - Re: Hobbs meter wiring (Gerry Holland)
     7. 11:34 AM - Re: welding cable (Eric M. Jones)
     8. 12:42 PM - Re: Re: welding cable (Bob McCallum)
     9. 01:11 PM - Re: [Bulk] Re: welding cable (Kevin Horton)
    10. 04:20 PM - Re: Fatwire (Eric M. Jones)
    11. 06:43 PM - Resource..... (Jim Baker)
    12. 11:38 PM - Re: Hobbs meter wiring (Werner Schneider)
 
 
 


Message 1


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    Time: 08:23:56 AM PST US
    From: Gaylen Lerohl <lerohl@rea-alp.com>
    Subject: Re: welding cable
    --> AeroElectric-List message posted by: Gaylen Lerohl <lerohl@rea-alp.com> Mil Spec, Tefzel insulated wire's advantage is that the individual strands of copper wire are tin coated to improve corrosion resistance. #4 and even #2 AWG wire really isn't that difficult to work with! Regards, Gaylen Lerohl Bob McCallum wrote: >--> AeroElectric-List message posted by: "Bob McCallum" <robert.mccallum2@sympatico.ca> > >Extremely well! It's designed to be run over by trucks and to be dragged >over hot, recently welded, steel, sometimes with sharp edges, in an >industrial environment. Probably survive your engine compartment better than >almost any other wiring material. > >Bob McC > > >----- Original Message ----- >From: "peter goudinoff" <peterg@dakotacom.net> >To: "AeroElectric-List Digest List" <aeroelectric-list-digest@matronics.com> >Subject: AeroElectric-List: welding cable > > > > >>--> AeroElectric-List message posted by: peter goudinoff >> >> ><peterg@dakotacom.net> > > >>as suggested, I'm installing #4 welding cable for my battery hookups >>any idea how this stuff will do inside the engine compartment? >> >>peter goudinoff >>Legacy #200 >> >> > > > >


    Message 2


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    Time: 08:53:42 AM PST US
    From: Charlie Kuss <chaztuna@adelphia.net>
    Subject: Re: welding cable
    --> AeroElectric-List message posted by: Charlie Kuss <chaztuna@adelphia.net> Listers, For those who object to the weight penalty of welding cable, I suggest using marine battery cables. I'm using these for my battery to ground and battery to master contactor cables. They use standard automotive insulation, with tinned copper stranded wire. I live near the ocean, so cable corrosion is an issue for me. I rejected using the welding cable, as it's wire is not "tinned" and it is much heavier than needed. Marine cable is just as flexible as welding cable. I'm using standard aircraft Tefzel 2 AWG cables from the master contactor to the starter. As Gaylen mentioned, it is not that hard to work with. However, I feel that Bob N. makes a good point with his observation that aircraft cable is stiff enough to possibly damage the terminals on your battery. Charlie Kuss >--> AeroElectric-List message posted by: "John Schroeder" ><jschroeder@perigee.net> > >But it sure is an order of magnitude easier to work with because of the >flexibility. Win some and lose some on this item > >Do not archive > >JOhn Schroeder > > >On Sat, 22 Oct 2005 21:06:48 -0500, bob noffs <icubob@newnorth.net> wrote: > > > hi all, > > i have heard that welding cable is tough as nails. i have also heard > > that > > the toughness comes at quite a weight penalty compared to other cable > > available. > > >-- > >


    Message 3


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    Time: 09:33:45 AM PST US
    From: "Bob McCallum" <robert.mccallum2@sympatico.ca>
    Subject: Re: welding cable
    --> AeroElectric-List message posted by: "Bob McCallum" <robert.mccallum2@sympatico.ca> Gaylen; It's disadvantage is that in these gauges it is very stiff and can impart sufficient load on a battery terminal to break it off from metal fatigue induced by vibration. This is the reason that Bob suggests welding cable to be superior to aircraft wire in this application. As for the weight disadvantage, mentioned by someone else, the wire itself weighs exactly the same whether its welding cable or mil spec wire, gauge for gauge in the same material. The difference is only in the insulation covering the wire, and that's only a very few ounces per foot. Total weight penalty for the whole plane probably a fraction of a pound. The only real (although slight) weight difference would be if you were to buy Eric's "Super CCA" wire which is lighter due to a material difference. (aluminium) Bob McC ----- Original Message ----- From: "Gaylen Lerohl" <lerohl@rea-alp.com> Subject: Re: AeroElectric-List: welding cable > --> AeroElectric-List message posted by: Gaylen Lerohl <lerohl@rea-alp.com> > > Mil Spec, Tefzel insulated wire's advantage is that the individual > strands of copper wire are tin coated to improve corrosion resistance. > #4 and even #2 AWG wire really isn't that difficult to work with! > > Regards, > Gaylen Lerohl > > Bob McCallum wrote: > > >--> AeroElectric-List message posted by: "Bob McCallum" <robert.mccallum2@sympatico.ca> > > > >Extremely well! It's designed to be run over by trucks and to be dragged > >over hot, recently welded, steel, sometimes with sharp edges, in an > >industrial environment. Probably survive your engine compartment better than > >almost any other wiring material. > > > >Bob McC > > > > > >----- Original Message ----- > >From: "peter goudinoff" <peterg@dakotacom.net> > >To: "AeroElectric-List Digest List" <aeroelectric-list-digest@matronics.com> > >Subject: AeroElectric-List: welding cable > > > > > > > > > >>--> AeroElectric-List message posted by: peter goudinoff > >> > >> > ><peterg@dakotacom.net> > > > > > >>as suggested, I'm installing #4 welding cable for my battery hookups > >>any idea how this stuff will do inside the engine compartment? > >> > >>peter goudinoff > >>Legacy #200 > >> > >> > > > > > > > > > >


    Message 4


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    Time: 10:04:36 AM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: Circuit Breakers
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 10:28 PM 10/22/2005 -0400, you wrote: >--> AeroElectric-List message posted by: N1deltawhiskey@aol.com > >Gosh no! Who would agree to do that? Just flipping them off-on-off- a few >times. . . . and I'll add: It's best to do this while the breaker is under load. You're INTENDING for the high temperatures of electric arcing to "clean" the contact surfaces. Bob . . .


    Message 5


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    Time: 10:22:12 AM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: Hobbs meter wiring
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 11:16 PM 10/22/2005 +0200, you wrote: >--> AeroElectric-List message posted by: Werner Schneider <glastar@gmx.net> > >Hello Charlie, > >sorry, it took a little bit longer to find it, in Europe it is from >Conrad Electronics article 185990 an adjustable sensor from 1.2 to 8 mbar. > >They are from Micro Pneumatic Logic and actually from the MPL 503 series >http://www.pressureswitch.com/products500.html > >They have more such products, also for larger load (503 is up to 20mA). A caveat for incorporation of these switches into the aircraft environment: I've suggested many times that electrical devices fail most often in small aircraft due to the effects of old age as opposed to usage. Nature is a patient supplier of environmental stresses that are almost never considered in the lab testing of a product or even suggested on the product's data sheets. These little pressure switches are amazing devices and probably do everything the spec sheets say. However, if RECORDING elapsed hours is an important part of KNOWING when or how to do things on your airplane . . . then to what degree will you direct pilot's attention to the proper operation of the Hobbs meter on a per-flight basis? A checklist item perhaps? I've suggested one way to control an hour meter at: http://www.aeroelectric.com/PPS/Engine/Gaging/Oil_P_Warn.pdf Here, a very robust pressure switch is used for TWO tasks. (1) Warn of low oil pressure (and master left on) and (2) operate the hourmeter. This switch gets something of a pre and post-flight check automatically and in a manner that draws attention to it's functionality without extraordinary attention as a checklist item. Of course, one can argue that the normally open and normally closed contacts of even this switch can operate at variance with each other. If one wishes to take the extra step, you can add a transistor and a few resistors to the circuit such that only one set of contacts operate both the low pressure warning AND operate the hour meter. This is but one example of "robust design" with a goal of making sure the desired operation happens while minimizing the cost of ownership which includes both maintenance $time$ and operating $time$. The secondary fallout is that failure of the switch to do it's intended function is more likely to come to your attention without being prompted by either an operating or maintenance procedure. There are undoubtedly other solutions. I think this is a good example of the though processes one should exercise whenever some relatively fragile, sensitive, obviously NON robust product is being considered for your project. Bob . . .


    Message 6


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    Time: 10:44:09 AM PST US
    Subject: Re: Hobbs meter wiring
    From: Gerry Holland <gholland@gemini-resourcing.com>
    --> AeroElectric-List message posted by: Gerry Holland <gholland@gemini-resourcing.com> Bob Hi! I'm using a device called Power Genie to supply start and stop Voltage to Hobbs Meter. About to start my Rotax Engine. OK? Find it at: http://www.powergenie.central5.com/ Regards Gerry


    Message 7


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    Time: 11:34:25 AM PST US
    From: "Eric M. Jones" <emjones@charter.net>
    Subject: Re: welding cable
    --> AeroElectric-List message posted by: "Eric M. Jones" <emjones@charter.net> --> AeroElectric-List message posted by: "Bob McCallum" <robert.mccallum2@sympatico.ca> > Total weight penalty for the whole plane probably a fraction of a pound. > The only real (although slight) weight >difference would be if you were to buy Eric's "Super CCA" wire which is >lighter due to a material difference. (aluminium) >Bob McC Just a couple thoughts--calling CCA "Aluminum" is arguable. There's has been a long history of aluminum wiring problems but ZERO history of CCA problems. As for weight, I think one of the best excerpts from the Aeroelectric List on the subject is on Bob's website at-- http://www.aeroelectric.com/articles/economics_of_weight_reduction.html Regards, Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge MA 01550-2705 (508) 764-2072 "Hey, it ain't rocket surgery!" --Anonymous


    Message 8


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    Time: 12:42:19 PM PST US
    From: "Bob McCallum" <robert.mccallum2@sympatico.ca>
    Subject: Re: welding cable
    --> AeroElectric-List message posted by: "Bob McCallum" <robert.mccallum2@sympatico.ca> Eric; I apologise for categorizing "CCA" as aluminium Eric, what I meant was, it is based on aluminium wire which lends lightness. Yes I realise you've gone to a lot of trouble to research the copper plated aluminium and then to develop an acceptable insulation system for it all to eliminate the aluminium wire short-comings of the past while imparting to your wire the advantages of copper. I should have said "aluminium based" or "copper clad aluminium" not "aluminium". I was trying to promote your wire not imply any failing in it. Bob McC ----- Original Message ----- From: "Eric M. Jones" <emjones@charter.net> > > Just a couple thoughts--calling CCA "Aluminum" is arguable. There's has been > a long history of aluminum wiring problems but ZERO history of CCA problems. > As for weight, I think one of the best excerpts from the Aeroelectric List > on the subject is on Bob's website at-- > > http://www.aeroelectric.com/articles/economics_of_weight_reduction.html > > Regards, > Eric M. Jones > www.PerihelionDesign.com


    Message 9


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    Time: 01:11:23 PM PST US
    From: Kevin Horton <khorton01@rogers.com>
    Subject: Re: welding cable
    --> AeroElectric-List message posted by: Kevin Horton <khorton01@rogers.com> On 23 Oct 2005, at 14:33, Eric M. Jones wrote: > --> AeroElectric-List message posted by: "Eric M. Jones" > <emjones@charter.net> > > --> AeroElectric-List message posted by: "Bob McCallum" > <robert.mccallum2@sympatico.ca> > > >> Total weight penalty for the whole plane probably a fraction of a >> pound. >> The only real (although slight) weight >> difference would be if you were to buy Eric's "Super CCA" wire >> which is >> lighter due to a material difference. (aluminium) >> Bob McC >> > > Just a couple thoughts--calling CCA "Aluminum" is arguable. There's > has been > a long history of aluminum wiring problems but ZERO history of CCA > problems. How many years of history of CCA use in aviation are there? How many aircraft are using it? Is the service history long and deep enough to draw any conclusions from? Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8


    Message 10


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    Time: 04:20:27 PM PST US
    From: "Eric M. Jones" <emjones@charter.net>
    Subject: Re: Fatwire
    --> AeroElectric-List message posted by: "Eric M. Jones" <emjones@charter.net> > Just a couple thoughts--calling CCA "Aluminum" is arguable. There's has > been > a long history of aluminum wiring problems but ZERO history of CCA > problems. How many years of history of CCA use in aviation are there? How many aircraft are using it? Is the service history long and deep enough to draw any conclusions from? Kevin Horton RV-8 (finishing kit) Kevin, Good question. Hard to answer. Many aircraft companies use CCA but it certainly is not as old as the use of copper. See-- http://www.thomasnet.com/products/wire-copper-clad-aluminum-94430808-1.html The point I have tried to make elsewhere is that if you have the expertise, aluminum is the best choice of metal to use for conductors. Those power company high tension lines you see everywhere are aluminum with a steel core. Many economic factors figure into it. The cable www.PerihelionDesign.com makes is made from ASTM B-566 10% Copper (by volume) Clad Aluminum. The only proprietary thing about it is how on God's Green Earth we procured less than a ton of raw material from which to make it and how we talked anyone into making less than 10,000 feet of it. This still amazes me. Regards, Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge MA 01550-2705 (508) 764-2072 "Democracy must be something more than two wolves and a sheep voting on what to have for dinner." - James Bovard


    Message 11


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    Time: 06:43:13 PM PST US
    From: "Jim Baker" <jlbaker@telepath.com>
    Subject: Resource.....
    --> AeroElectric-List message posted by: "Jim Baker" <jlbaker@telepath.com> Ran across this neat/consice bit of an info table this evening.... http://www.epanorama.net/documents/wiring/wire_resistance.html Jim Baker 580.788.2779 '71 SV, 492TC Elmore City, OK


    Message 12


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    Time: 11:38:14 PM PST US
    From: Werner Schneider <glastar@gmx.net>
    Subject: Re: Hobbs meter wiring
    --> AeroElectric-List message posted by: Werner Schneider <glastar@gmx.net> Hello Bob, here my 0.2 cents to this (air pressure) switch, however generally I agree on your sight. I think the difference comes from me using the Hobbs meter NOT as total engine time function instead of total FLYING time function: > These little pressure switches are amazing devices and probably > do everything the spec sheets say. However, if RECORDING elapsed > hours is an important part of KNOWING when or how to do things on > your airplane . . . then to what degree will you direct pilot's > attention to the proper operation of the Hobbs meter on a per-flight > basis? A checklist item perhaps? > > I have a cross-check with my GPS, as it does also log my flight time. > I've suggested one way to control an hour meter at: > > http://www.aeroelectric.com/PPS/Engine/Gaging/Oil_P_Warn.pdf > > Here, a very robust pressure switch is used for TWO tasks. (1) Warn > of low oil pressure (and master left on) and (2) operate the hourmeter. > This switch gets something of a pre and post-flight check automatically > and in a manner that draws attention to it's functionality without > extraordinary attention as a checklist item. > > I have this switch also incorporated into my plane, however, the first one failed to operate at the beginning (got it replaced for free by B&C with a new design) however my goal is to log plain FLIGHT time so this approach does not work for me. > fragile, sensitive, obviously NON robust product is being considered > for your project. > > This switches are in use in many application in the industries measuring all kind of fluid and gases items (not necessary the same switch type) they're also used since years in one of the flight schools here in Switzerland with great success (as they charge by flight time). So far 150 hrs without any problem hooked up on my dynamic system (I should have noted that maybe as it is NOT an oil pressure switch). Werner > >




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