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mikeeasley(at)aol.com Guest
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Posted: Tue Oct 13, 2009 5:21 am Post subject: Required Length of Fusible Links |
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B&C sells fusible links that are intended to be 5-6" long. Do they have to be that long? Do you need to allow any space around them for the heat when they smoke? If you're protecting a #22 wire, do you go to #26 in the fusible link?
Thanks,
Mike Easley
Colorado Springs
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nuckolls.bob(at)aeroelect Guest
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Posted: Tue Oct 13, 2009 9:01 am Post subject: Required Length of Fusible Links |
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At 08:12 AM 10/13/2009, you wrote:
Quote: | B&C sells fusible links that are intended to be 5-6" long. Do they have to be that long? Do you need to allow any space around them for the heat when they smoke? If you're protecting a #22 wire, do you go to #26 in the fusible link? |
Fusible links should not be used to generally replace
fuses or circuit breakers. They are used only when
a ROBUST feeder protection is needed. These might
be properly called Micro-ANL current limiters.
If you're considering an application other than
one illustrated in the Z-figures, let's
discus it here on the List.
6" is a good length for meeting the thermal
model that controls the fusing event. You
COVER them in a material capable of containing
the fusing event. Hence the fiberglas/silcone
jacket in the B&C kit. #26 wire is too fragile
to be practical for a/c wiring. #24 is marginal
but okay in applications illustrated.
I've often thought I should not have introduced
the fusible link to the OBAM aircraft community
but then, it's just a collection of simple-ideas
with specific but LIMITED applicability to our
design goals. Let's not start scattering these
guys around the airplane. If you need an isolated,
single strand not conveniently protected by
a fuse at the bus, then consider an in-line
fuse holder.
http://aeroelectric.com/Pictures/Fuses/Fuse_Holders/ifh-2.jpg
Bob . . .
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( . . . a long habit of not thinking )
( a thing wrong, gives it a superficial )
( appearance of being right . . . )
( )
( -Thomas Paine 1776- )
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