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08-28-2012, 02:42 PM
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Join Date: May 2006
Location: Sammamish, WA
Posts: 652
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Wiring between main and starter contactor...
I'm using a short length of battery type cable made by B&C to connect my main contactor to the starter contactor. Both contactors are from B&C. The orientation of the terminal bolts on the contactors does not make for using copper bar easily.
I've enclosed a picture. My question is, do you the think the radius of the bend will put too much stress on this wire? If so, what would you suggest?
Thanks,
Michael-

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Michael Burbidge
Sammamish, WA
RV-14A Empennage
RV-9A Flying?340 hours!
Last Donation: December 2019
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08-28-2012, 06:22 PM
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Join Date: Jan 2005
Location: Mtns of N.E. Georgia
Posts: 1,322
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Cable
Looks ok to me from here. If you're worried about it, make a new one with welding cable. It is super flexible and should make that radius easily.
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LAUS DEO
Mannan J.Thomason, MSGT. USAF (RET)
VAF788
"Bucket List" checkoff in progress!
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08-28-2012, 07:24 PM
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Join Date: Feb 2005
Location: Stoughton, WI
Posts: 473
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Bend it
You can shorten the wire and bend the terminal connection over 90 degrees to make a neater installation. That being said, it looks OK as it is as long as it will not rub against the battery box.
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Frank Smidler
N96FS, RV-6
Flying 1/11/09
1085 hr
2WI6 Stoughton, WI
Formally of Lafayette, IN
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08-28-2012, 07:59 PM
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Join Date: Jan 2005
Location: KPYM
Posts: 2,686
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...or do it like i did with a twist in the copper bar.
 . CJ
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RV-7 Flying - 1,200 Hours in 5 Years!
The experiment works!
TMX-IO-360, G3i ignition & G3X with VP-X
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08-28-2012, 08:00 PM
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Join Date: Feb 2005
Location: Abilene, TX
Posts: 724
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You probably knew this, but when you crimp the terminals on, make sure they are "clocked" so you don't have to twist the cable when you put the ends on the studs. Don't want to introduce any stress. 
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Sam Evans
RV7-A O-360 C/S
VAF#812
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11-11-2012, 07:30 AM
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Join Date: Oct 2005
Location: San Antonio, TX
Posts: 281
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CJ,
Where did you get that copper bar you used to interconnect the contactors and what size/thickness is it? Also, how did you do the black on there, it looks like rubber. Thanks
Matt
Quote:
Originally Posted by Captain_John
...or do it like i did with a twist in the copper bar.
 . CJ
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11-11-2012, 07:42 AM
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Join Date: Jan 2008
Location: Granbury, TX
Posts: 543
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Vans sells copper bus bars. http://vansaircraft.com/cgi-bin/stor...oduct=buss-bar
To me it looks like the black is just heat shrink tubing.
Hope this helps,
Jason
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Jason Tremble
RV-7A (Flying and Sold)
RV-10 in process (@#$$%# Cabin Top & Doors)
Paid for 2020
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11-11-2012, 07:44 AM
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Join Date: Mar 2005
Location: Dallas area
Posts: 10,762
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Quote:
Originally Posted by idleup
CJ,
Also, how did you do the black on there, it looks like rubber. Thanks
Matt
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Looks like heat-shrink tubing to me.
p.s. Obviously Jason types faster than I do. My recent eye surgery has slowed my keyboard!
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Mel Asberry, DAR since the last century.
EAA Flight Advisor/Tech Counselor, Friend of the RV-1
Recipient of Tony Bingelis Award and Wright Brothers Master Pilot Award
USAF Vet, High School E-LSA Project Mentor.
RV-6 Flying since 1993 (sold)
<rvmel(at)icloud.com>
Last edited by Mel : 11-11-2012 at 07:46 AM.
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11-11-2012, 08:32 AM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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Quote:
Originally Posted by UnPossible
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If you want to equal #2 gauge wire, you should use two strips of Vans bus bar in parallel.
One strip is only about 55% the copper cross-section area of a #2 wire.
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Gil Alexander
EAA Technical Counselor, Airframe Mechanic
Half completed RV-10 QB purchased
RV-6A N61GX - finally flying
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
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11-11-2012, 10:13 AM
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Join Date: Oct 2005
Location: 08A
Posts: 9,477
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Quote:
Originally Posted by Michael Burbidge
My question is, do you the think the radius of the bend will put too much stress on this wire?
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No. The minimum radius for a wire is roughly the same as the minimum bend radius for sheet or bar material with thickness equal to the individual wire strand diameter. Put another way, the concern is cracking of the individual strands, just like cracking an aluminum sheet part by using a bend radius that is too small.
You're not anywhere near the plastic region for those wire strands.
Concern about "preload stress" is baseless. Consider your torque-to-length Lycoming connecting rod bolts, or the stress on your landing gear right now, sitting quietly in the hangar.
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Dan Horton
RV-8 SS
Barrett IO-390
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