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AeroElectric-List Digest: 11 Msgs - 09/12/08

 
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nuckolls.bob(at)cox.net
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PostPosted: Sat Sep 13, 2008 9:09 am    Post subject: AeroElectric-List Digest: 11 Msgs - 09/12/08 Reply with quote

At 08:48 AM 9/13/2008 -0700, you wrote:
Quote:
Vern,

you quoted Carling switch ratings, but if you read further down on the
page, you find the following:

"Types of Loads:
An electric load is the amount of electric power delivered or required
at any specific point or points on a system. The requirement originates
at the energy consuming equipment of the consumers. More simply put, a
load is the piece of equipment you turn on and off.

<snip>
Quote:
Are you sure you are using the switches within their rated specs???????????

My experience using AC rated switches on DC circuits with high inrush
currents (landing/taxi lights and strobes in particular) is failure after
failure.

Eric....this includes ROCKER SWITCHES TOO!.... Cessna rocker switches used
in the 70's for example (AC rated "Mr Coffee Maker switches).

My $.02 worth......

Scott A Klemptner
bmwr606 on Yahoo IM


Scott,

Keep in mind that RATINGS have to do with SWITCH
SERVICE LIFE generally given in the tens of thousands of
cycles with various conditions. Our use of switches in
light aircraft is exceedingly light-duty in terms
of service life.

For example, a master switch (one of those cited in
the constellation of failures) operates ONCE PER FLIGHT-CYCLE
and carries very small currents compared to the switch's
RATINGS.

Scott, please review the arguments offered in the
piece at:

http://www.aeroelectric.com/articles/Switch_Ratings.pdf

and explain where you find discrepancies of fact or
logic. I'll suggest that had Vern sat in his airplane
one afternoon and put 1000 cycles on any of the failed
switches, he would NOT have experienced a
failure. Yet, over a period of many flight hours
and a mere handful of operations he experienced
failures that speak to long term effects of ENVIRONMENT
that include DEFICIENCIES of process either in fabrication
of the switch as described here . . .

http://www.aeroelectric.com/articles/Anatomy_of_a_Switch_Failure/Anatomy_of_a_Switch_Failure.html

or installation of the switch as hypothesized in
my earlier treatise published this morning.

The old AC vs. DC as a critical driving force in
switch life is a myth. Further, it is clear that the
study before us has nothing to do with switch
life in terms of ratings, operating cycles, or
application. Root cause of these failures will be
loss of conduction integrity in one or more of the
ten metal-to-metal joints that make up the switch's
current path.

Bob . . .


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nuckolls.bob(at)cox.net
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PostPosted: Sat Sep 13, 2008 9:28 am    Post subject: AeroElectric-List Digest: 11 Msgs - 09/12/08 Reply with quote

At 12:52 PM 9/13/2008 -0400, you wrote:
Quote:

<retasker(at)optonline.net>

A comment on the below comments:

If you look at the schematic Vern posted, you would see that he is using
NTC surge limiters on each light. These minimize startup surges caused by
the very low cold filament resistance of the lamps.

On the other hand, it depends on the time constants of the NTC surge
limiters vs the time constants of the lamp filaments as to whether these
are effective when in wig-wag mode.

Dick Tasker

A couple of years ago, the effectiveness/value of surge
limiters in Wig-Wag systems was discussed here on the List.
I went to the workbench and took this trace from the
operating current of a 55W halogen lamp flashed at
about 2 flashes per second.

http://www.aeroelectric.com/Pictures/Curves/Wig_Wag_Currents.jpg

Note that the first time the lamp gets power we
see the characteristic cold-filament inrush current.
However, on subsequent turn-ons, the lamp does not
have enough time to cool such that the 7x inrush
experience is repeated.

Bob . . .


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