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nuckolls.bob(at)aeroelect Guest
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Posted: Wed Feb 17, 2010 6:03 pm Post subject: S701 Contactor Failure Analysis |
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Last year, Marty Emrath told us about the failure of a new
contactor he had purchased from B&C. B&C replaced the contactor
but Marty was justifiably curious as to root cause of the
failure.
I offered to document a tear-down analysis and Marty sent
me the carcass. I was looking for something fun to do this
afternoon so I took the dead puppy apart.
The pictures at . . .
http://www.aeroelectric.com/Pictures/Contactors/S701_Failure_Teardown/
Are pretty much self explanatory. One thing is for certain.
This product is much more sophisticated than its ancestors
that first took to the air in a C-140.
The last picture tells the tale . . .
http://www.aeroelectric.com/Pictures/Contactors/S701_Failure_Teardown/TearDown_10.jpg
Seems the assembler wasn't really awake yet when this
device went across their work station. One coil wire
was poorly soldered to its terminal . . . the other had
no solder at all.
Thanks for sharing your experience with us Martin!
Bob . . .
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nuckolls.bob(at)aeroelect Guest
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Posted: Wed Feb 17, 2010 6:20 pm Post subject: S701 Contactor Failure Analysis |
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Already had a comment on the analysis . . . someone noted that
the terminals around which the coil wires are wrapped are square
and may indeed have sharp corners.
He reminded me of an arcane point-to-point wiring process
for complex digital circuits called "wire wrap". This
process used special wire, tools, sharp edged square terminal
posts and no solder. The tools were designed to tightly
wrap the wire around the post with enough turns, and
stretching force to create multiple gas-tight joints
on the corners at each connection.
As I recall this technology called for about 6 tightly
spaced turns around the post (24+ points of contact).
Since this coil-form is plastic . . . and soldering these
joints would call for considerable heat and time,
it may well be that the original design calls for
no solder at all.
In this case, the assembler of the failed item was
perhaps not in possession of the right tool. The turns
about both posts are not those produced by a "wire wrap"
tool. The curious thing is that there is SOME solder
on one of the terminals . . . perhaps didn't pass a
continuity test and the solder dab "fixed it" only to
have the other joint fail later.
Guess we'll have to tear down another contactor to
see. I don't think I have one in the shop. I'll go
buy one.
Bob . . .
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rjquillin(at)cox.net Guest
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Posted: Wed Feb 17, 2010 6:48 pm Post subject: S701 Contactor Failure Analysis |
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You have a good recollection.
I just did some wire-wrap late last year.
However, the wire used has Kynar or other insulation that is removed to expose a bare, generally tin coated, conductor.
The wire used to wind the coil, from your pictures, appears to be 'magnet' wire which has an insulating coating. The wire-wrap process, as I have always seen it implemented, is not designed for this type of insulated wire and is not expected to breech the insulation to form a contact.
I believe your original diagnosis of no solder was spot-on.
Ron Q.
At 18:18 2/17/2010, you wrote:
[quote]He reminded me of an arcane point-to-point wiring process
for complex digital circuits called "wire wrap". This
process used special wire, tools, sharp edged square terminal
posts and no solder. The tools were designed to tightly
wrap the wire around the post with enough turns, and
stretching force to create multiple gas-tight joints
on the corners at each connection.
As I recall this technology called for about 6 tightly
spaced turns around the post (24+ points of contact).
Since this coil-form is plastic . . . and soldering these
joints would call for considerable heat and time,
it may well be that the original design calls for
no solder at all.[b]
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Bret Smith
Joined: 09 Jan 2006 Posts: 178 Location: Mineral Bluff, GA
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Posted: Wed Feb 17, 2010 7:13 pm Post subject: S701 Contactor Failure Analysis |
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Thank you Bob, It is always interesting to learn more about the art of
aircraft electronics.
Bret Smith
RV-9A N16BL
Blue Ridge, GA
www.FlightInnovations.com
--
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_________________ Bret Smith
RV-9A (Emp) |
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retasker(at)optonline.net Guest
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Posted: Wed Feb 17, 2010 8:13 pm Post subject: S701 Contactor Failure Analysis |
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Your recollection is generally true and the same as the wire I have used
for all the wire wrapping I have done. However, once upon a time there
was wire sold for wrapping that did not require stripping.
Unfortunately, I don't remember who sold it nor do I have any. Further,
I seem to recall that it was not too successful as it eventually tended
to short anywhere it overlapped under tension.
The wire on the teardown certainly looks like common magnet wire. And
in any case, three or four turns would certainly not be sufficient to
make long term reliable contact in something like this which is likely
to be exposed to rather harsh environmental conditions. I agree with
Bob that they just forgot to solder the wires - the operator probably
got interrupted during assembly.
Dick Tasker
Ron Quillin wrote:
Quote: | You have a good recollection.
I just did some wire-wrap late last year.
However, the wire used has Kynar or other insulation that is removed
to expose a bare, generally tin coated, conductor.
The wire used to wind the coil, from your pictures, appears to be
'magnet' wire which has an insulating coating. The wire-wrap process,
as I have always seen it implemented, is not designed for this type of
insulated wire and is not expected to breech the insulation to form a
contact.
I believe your original diagnosis of no solder was spot-on.
Ron Q.
At 18:18 2/17/2010, you wrote:
> He reminded me of an arcane point-to-point wiring process
> for complex digital circuits called "wire wrap". This
> process used special wire, tools, sharp edged square terminal
> posts and no solder. The tools were designed to tightly
> wrap the wire around the post with enough turns, and
> stretching force to create multiple gas-tight joints
> on the corners at each connection.
>
> As I recall this technology called for about 6 tightly
> spaced turns around the post (24+ points of contact).
> Since this coil-form is plastic . . . and soldering these
> joints would call for considerable heat and time,
> it may well be that the original design calls for
> no solder at all.
*
*
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Please Note:
No trees were destroyed in the sending of this message. We do concede, however,
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mauledriver(at)nc.rr.com Guest
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Posted: Wed Feb 17, 2010 8:22 pm Post subject: S701 Contactor Failure Analysis |
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I'm feeling old... My only hands-on experimental circuit making was pre-digital. Â Over the years I'd pickup electronics mags and see references to "wire wrapped" terminals and never had a clue what it referred to. Â Now I get it... Thanks.
Bill
-- Sent from my Palm Pre
Ron Quillin wrote:
You have a good recollection.
I just did some wire-wrap late last year.
However, the wire used has Kynar or other insulation that is removed to expose a bare, generally tin coated, conductor.
The wire used to wind the coil, from your pictures, appears to be 'magnet' wire which has an insulating coating. The wire-wrap process, as I have always seen it implemented, is not designed for this type of insulated wire and is not expected to breech the insulation to form a contact.
I believe your original diagnosis of no solder was spot-on.
Ron Q.
At 18:18 2/17/2010, you wrote:
Quote: | He reminded me of an arcane point-to-point wiring process
 for complex digital circuits called "wire wrap". This
 process used special wire, tools, sharp edged square terminal
 posts and no solder. The tools were designed to tightly
 wrap the wire around the post with enough turns, and
 stretching force to create multiple gas-tight joints
 on the corners at each connection.
 As I recall this technology called for about 6 tightly
 spaced turns around the post (24+ points of contact).
 Since this coil-form is plastic . . . and soldering these
 joints would call for considerable heat and time,
 it may well be that the original design calls for
 no solder at all.
">http://www.matronics.com/Navigator?AeroElectric-List
com
tronics.com/contribution
| [quote][b]
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nuckolls.bob(at)aeroelect Guest
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Posted: Wed Feb 17, 2010 9:33 pm Post subject: S701 Contactor Failure Analysis |
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At 10:22 PM 2/17/2010, you wrote:
Quote: | I'm feeling old... My only hands-on experimental
circuit making was pre-digital. Â Over the
years I'd pickup electronics mags and see
references to "wire wrapped" terminals and never
had a clue what it referred to. Â Now I get it... Thanks.
Bill
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see:
http://en.wikipedia.org/wiki/Wire_wrap
This is the modern incarnation used on complex backplanes
where gazillion-layer boards are impractical. The no-strip
version is from way-back-when and it didn't hang around
long.
Bob . . .
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nuckolls.bob(at)aeroelect Guest
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Posted: Wed Feb 17, 2010 9:36 pm Post subject: S701 Contactor Failure Analysis |
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Quote: | The wire on the teardown certainly looks like common magnet
wire. And in any case, three or four turns would certainly not be
sufficient to make long term reliable contact in something like this
which is likely to be exposed to rather harsh environmental
conditions. I agree with Bob that they just forgot to solder the
wires - the operator probably got interrupted during assembly.
|
Just for grins, I took a chunk of the wire off the
failed coil and subjected it to a puddle of molten
solder. The insulation was indeed a "solder-eze"
type . . . you can solder through it without pre-
stripping.
The plastic used on the bobbin did melt at soldering
iron temperatures but not quickly. So it seems a rational
deduction that the failed joints were intended to be
soldered. The right temperature and flux combination
would have produced a reliable joint with minimal
effect on the bobbin.
I guess I won't go buy one to take apart . . . perhaps
we'll get another carcass to inspect for other reasons
one day.
Bob . . .
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tomcostanza
Joined: 19 Oct 2008 Posts: 49
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Posted: Thu Feb 18, 2010 3:58 am Post subject: Re: S701 Contactor Failure Analysis |
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If I remember correctly, the wire-wrap technique was only for microamp level circuits; a few milliamps at the most. I never saw any wire-wraps for the approx 1 amp that the contactor would need. Or am I mistaken?
Clear Skies,
Tom
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_________________ Clear Skies,
Tom Costanza
-- in year 17 of a 3 year project |
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bob(at)bob-white.com Guest
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Posted: Thu Feb 18, 2010 7:41 am Post subject: S701 Contactor Failure Analysis |
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I remember using the "no strip" technique many years ago. As I recall,
the wrap tool did slit the insulation as it was wrapped around the
post so that bare wire was wrapped onto the post.
Bob W.
On Wed, 17 Feb 2010 23:30:03 -0600
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> wrote:
Quote: |
At 10:22 PM 2/17/2010, you wrote:
>I'm feeling old... My only hands-on experimental
>circuit making was pre-digital. Â Over the
>years I'd pickup electronics mags and see
>references to "wire wrapped" terminals and never
>had a clue what it referred to. Â Now I get it... Thanks.
>
>Bill
see:
http://en.wikipedia.org/wiki/Wire_wrap
This is the modern incarnation used on complex backplanes
where gazillion-layer boards are impractical. The no-strip
version is from way-back-when and it didn't hang around
long.
Bob . . .
|
--
N93BD - Rotary Powered BD-4 - http://www.bob-white.com
Now Rotary Powered Alpine
http://www.youtube.com/watch?v=FwceNc2ydN8
Cables for your rotary installation - http://roblinstores.com/
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Speedy11(at)aol.com Guest
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Posted: Thu Feb 18, 2010 7:48 am Post subject: S701 Contactor Failure Analysis |
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Bob,
That was one of the most educational episodes ever on the Aeroelectric Connection.
You removed some of the mystery for us.
Thanks,
Stan Sutterfield
Do not archive
[quote][b]
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nuckolls.bob(at)aeroelect Guest
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Posted: Thu Feb 18, 2010 8:14 am Post subject: S701 Contactor Failure Analysis |
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At 05:58 AM 2/18/2010, you wrote:
Quote: |
<Tom(at)CostanzaAndAssociates.com>
If I remember correctly, the wire-wrap technique was only for
microamp level circuits; a few milliamps at the most. I never saw
any wire-wraps for the approx 1 amp that the contactor would
need. Or am I mistaken?
|
Yes, but that was more a function of wire size and
size of the post in the specific process. If one
adequately understood the physics behind making
such joints on 4-cornered posts with the appropriate
insulation and tools, I have no doubt that this
contactor design could exploit the process.
Bob . . .
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nuckolls.bob(at)aeroelect Guest
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Posted: Thu Feb 18, 2010 8:16 am Post subject: S701 Contactor Failure Analysis |
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At 09:37 AM 2/18/2010, you wrote:
Quote: |
I remember using the "no strip" technique many years ago. As I recall,
the wrap tool did slit the insulation as it was wrapped around the
post so that bare wire was wrapped onto the post.
|
Yeah . . . I recall that. It WAS a pretty specialized
wrapping tool.
Bob . . .
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nuckolls.bob(at)aeroelect Guest
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Posted: Thu Feb 18, 2010 8:43 am Post subject: S701 Contactor Failure Analysis |
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At 09:45 AM 2/18/2010, you wrote:
Quote: | Bob,
That was one of the most educational episodes ever on the Aeroelectric Connection.
You removed some of the mystery for us.
Thanks, |
My pleasure my friend . . . it's an extension
of a number of tasks I accomplished on the TC side of the
house for many years.
It was frustrating to me that folks making $multi-million$
decisions had so little knowledge of the physics that
described the failure . . . even less on the physics
that was proposed to fix it.
It took me nearly 8 years to get a brake friction material
changed on a motor that was breaking shafts due to
a vibration that literally screamed at the most
casual observer.
I explored dozens of arm-chair suppositions only
to return to the original hypothesis and proposal
for a fix. Finally got it done but not after
a bucket full of money in warranty costs and
customer dis-satisfaction went down the drain.
I still have a copy of a 6-page letter I wrote to the V.P.
of Engineering describing in minute detail how the
shafts were failing . . . delighted to receive an e-mail
inviting me to a working lunch. Was astounded to find that
he wanted to discuss the letter for about 2 minutes
and talk about fishing the rest of the time . . . sigh.
Here on the list we have a unique opportunity to
tap the combined knowledge and experience of folks
who's paychecks and promotions do not depend on
smoothing the feathers of superiors that know even
less about the problem.
Bob . . . [quote][b]
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rjquillin(at)cox.net Guest
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Posted: Thu Feb 18, 2010 8:47 am Post subject: S701 Contactor Failure Analysis |
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At 08:14 2/18/2010, you wrote:
Quote: | Yeah . . . I recall that. It WAS a pretty specialized
wrapping tool.
Bob . . . |
Frightning;
I still have and can locate the auto strip bit for my electric Gardner WW tool!
Ron Q
do not archive
[quote][b]
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bob(at)bob-white.com Guest
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Posted: Thu Feb 18, 2010 12:37 pm Post subject: S701 Contactor Failure Analysis |
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On Thu, 18 Feb 2010 08:42:28 -0800
Ron Quillin <rjquillin(at)cox.net> wrote:
Quote: | At 08:14 2/18/2010, you wrote:
>Yeah . . . I recall that. It WAS a pretty specialized
> wrapping tool.
>
> Bob . . .
Frightning;
I still have and can locate the auto strip bit for my electric Gardner WW tool!
Ron Q
do not archive
OK, I got curious. You can still buy the thing from Digikey:
|
http://parts.digikey.com/1/parts/996077-tool-slit-n-wrap-manual-w-28-p184-1.html
I can't believe they are charging $232 for one of those things. I'm
sure I didn't pay anything like that. I might even be able to find my
old one if anybody want a real deal.
Bob W.
--
N93BD - Rotary Powered BD-4 - http://www.bob-white.com
Now Rotary Powered Alpine
http://www.youtube.com/watch?v=FwceNc2ydN8
Cables for your rotary installation - http://roblinstores.com/
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retasker(at)optonline.net Guest
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Posted: Thu Feb 18, 2010 2:00 pm Post subject: S701 Contactor Failure Analysis |
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Yeah, I know. I recently looked to see if the OK Industry wrap/strip/unwrap tool I have was still available. My jaw dropped when I found out the answer is yes and it costs $34.33 from Digikey!
[img]cid:part1.07050000.06080202(at)optonline.net[/img]
Do not archive
Bob White wrote: Quote: | Quote: | On Thu, 18 Feb 2010 08:42:28 -0800
Ron Quillin <rjquillin(at)cox.net> (rjquillin(at)cox.net) wrote:
Quote: | At 08:14 2/18/2010, you wrote:
Quote: | Yeah . . . I recall that. It WAS a pretty specialized
wrapping tool.
Bob . . .
|
Frightning;
I still have and can locate the auto strip bit for my electric Gardner WW tool!
Ron Q
do not archive
| OK, I got curious. You can still buy the thing from Digikey:
http://parts.digikey.com/1/parts/996077-tool-slit-n-wrap-manual-w-28-p184-1.html
I can't believe they are charging $232 for one of those things. I'm
sure I didn't pay anything like that. I might even be able to find my
old one if anybody want a real deal.
Bob W.
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emrath(at)comcast.net Guest
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Posted: Fri Feb 19, 2010 12:00 pm Post subject: S701 Contactor Failure Analysis |
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Bob,
Thanks for taking time to do this. Very interesting. I hope my replacement,
provided by B&C "gratis" was not manufactured on the same day...... Marty
Time: 06:03:45 PM PST US
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: S701 Contactor Failure Analysis
Last year, Marty Emrath told us about the failure of a new contactor he had
purchased from B&C. B&C replaced the contactor but Marty was justifiably
curious as to root cause of the failure.
I offered to document a tear-down analysis and Marty sent
me the carcass. I was looking for something fun to do this afternoon so I
took the dead puppy apart.
The pictures at . . .
http://www.aeroelectric.com/Pictures/Contactors/S701_Failure_Teardown/
Are pretty much self explanatory. One thing is for certain. This product is
much more sophisticated than its ancestors that first took to the air in a
C-140.
The last picture tells the tale . . .
http://www.aeroelectric.com/Pictures/Contactors/S701_Failure_Teardown/TearDo
wn_10.jpg
Seems the assembler wasn't really awake yet when this
device went across their work station. One coil wire
was poorly soldered to its terminal . . . the other had
no solder at all.
Thanks for sharing your experience with us Martin!
Bob . . .
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