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ANL current limiter location on rear battery installations

 
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nuckolls.bob(at)cox.net
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PostPosted: Thu Nov 06, 2008 7:39 am    Post subject: ANL current limiter location on rear battery installations Reply with quote

At 02:13 PM 11/4/2008 -0800, you wrote:
Quote:

> > That interested me since in another context I had been wondering
about ANL location. I was
> puzzling why in Z-24 the ANL was shown downstream of the internally
regulated alternator
> isolation contactor. My thinking was that by having it close to the
alternator it would blow if
> anything (including the isolation contactor) ran amok downstream. What
is the advantage of
> having it at the main bus end ?
> A The ANL limiter (fat fuse) is there to protect the alternator b-lead
wire . . . the source of
> energy that places this wire at risk is NOT the alternator but the
battery. An alternator is
> incapable of putting out enough current to open its own b-lead
protection while the battery is
> capable of fat-wire faults approaching 1000 amps. So, while selecting
the SIZE of the protection
> device is driven by alternator output capability, selecting LOCATION is
associated with the risk
> source . . the BATTERY.
> On some occasions, we have fat wires that can source a fault from
either end . . . in
> which case, you might have a limiter at both ends of the same
conductor. However, I've never
> encountered a situation like this for small aircraft. Bob . . .
The above is in the FAQ's for the list. I would like to clarify a bit
further: If the battery is the current feeder in a frayed B-lead scenario,
and the battery is in the tail (with the master contactor and eng power
bus (FI auto)), then wouldn't the ANL current limiter be located back
there as well? If so, between the battery and contactor, or between the
contactor and main bus loads?

Actually, a frayed b-lead is likely to arc a bit
and "burn clear" like other battery connected fat
wires in airplanes. The ANL is risk mitigation for
shorted diodes . . . an exceedingly rare event
in modern alternators . . . ESPECIALLY those
supported by due diligence on the part of the
designers/rebuilders.

Small aircraft do not get circuit protection in
the battery feeders to the starter and distribution
busses. Only the alternator b-leads got the ANLs
(or similar) to deal with the internally shorted
alternator but that risk too has steadily diminished
over the years.

If you choose to include a limiter in the b-lead,
then about any place in the b-lead wire is okay
but best at the end away from the alternator.

Bob . . .

----------------------------------------)
( . . . a long habit of not thinking )
( a thing wrong, gives it a superficial )
( appearance of being right . . . )
( )
( -Thomas Paine 1776- )
----------------------------------------


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Beemer



Joined: 26 Aug 2006
Posts: 87
Location: Middle Georgia

PostPosted: Thu Nov 06, 2008 2:46 pm    Post subject: ANL current limiter location on rear battery installations Reply with quote

Ahhh, I see. I took your stance to be that the ANL fuse is a much required
item in our OBAM systems. I now take you to mean them to be fine to add, but
not wholly necessary to safety. Correct?

So having no circuit protection in both/either the alternator and/or starter
circuit in a competently-designed system is ok? Hard to swallow, but that's
why I'm asking.

I have an ANL fuse and holder, but in the interest of fewer connections
(hence less to go wrong), I may forego it.

Bradley

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Suzuki G10 three-banger
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tomcostanza



Joined: 19 Oct 2008
Posts: 49

PostPosted: Tue Jul 13, 2010 2:53 am    Post subject: Re: ANL current limiter location on rear battery installat Reply with quote

Bob,

With respect to:

Quote:
Small aircraft do not get circuit protection in
the battery feeders to the starter and distribution
busses.


Why does the battery feeder to the distribution buss not get protected?

Thanks,
-Tom


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