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Fuse Sizing

 
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jpx(at)Qenesis.com
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PostPosted: Mon Jul 07, 2008 5:38 am    Post subject: Fuse Sizing Reply with quote

I just looked through Chapter 10 and didn't find any guidance on
selecting the size of a fuse.
I am quite sure that a 10A fuse is designed to blow at, or barely
above, 10A and thus would be unsuitable for protecting a circuit with
an actual current flow of 10A.

In my case, I have a landing light circuit totalling 9.2A. Mostly it
is 4.6A to each bulb, but there are some common wires at the switch
that carry both loads.

Looking at Bob's Wire Size Selection chart with 10C Rise (which makes
wire selection incredibly easy, compared to the graphs in 43-13-1B), I
could use 18 gauge wire in the wings and 14 gauge wire where both
currents are common.

I can't use a double pole switch to wire each light independently with
separate fuses, because I am already using a double pole switch to
give me off, on or wig wag.

So I need a single circuit with a single fuse. The fuse needs to be
sufficient for the total current. This also means upgrading the 18
gauge wire in the wings to 14 gauge, to avoid having a fuse too big
for the wire.

So my gut feel is to use the 35C Rise part of the table to pick a
current rating for the fuse, which would give me 15A fuse for 14 gauge
wire. Correct ?

Also, the calculations quite clearly include the return to ground part
of the current when calculating wire losses due to resistance. What
equivalent resistance value would be typical of the frame of aluminum
aircraft when used for the ground return ?

Thanks for your advice,

Jeff Page
Dream Aircraft Tundra #10


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PostPosted: Wed Jul 09, 2008 1:31 pm    Post subject: Fuse Sizing Reply with quote

At 09:33 AM 7/7/2008 -0400, you wrote:
Quote:


I just looked through Chapter 10 and didn't find any guidance on
selecting the size of a fuse.
I am quite sure that a 10A fuse is designed to blow at, or barely
above, 10A and thus would be unsuitable for protecting a circuit with
an actual current flow of 10A.

Fuse ratings can vary a lot from style to style
and application to application for the device. There's
no broad-brush statement one can make about "fuses" . . .
the manufacturer's data is always the best place
to go.

In the case of the ATC plastic devices, the data shows

http://www.egauges.com/vdo_mult3.asp?Type=Voltmeter12&Series=Cyber_Red&Units=E

. . . that you can probablyuse a 10A fuse in a circuit
that draws 10A continuously.
Quote:
In my case, I have a landing light circuit totalling 9.2A. Mostly it
is 4.6A to each bulb, but there are some common wires at the switch
that carry both loads.

Lamps also have bodacious inrush current. So look for 15A
protection to reduce probability of nuisance tripping.
Quote:
Looking at Bob's Wire Size Selection chart with 10C Rise (which makes
wire selection incredibly easy, compared to the graphs in 43-13-1B), I
could use 18 gauge wire in the wings and 14 gauge wire where both
currents are common.

I can't use a double pole switch to wire each light independently with
Quote:
separate fuses, because I am already using a double pole switch to
give me off, on or wig wag.

So I need a single circuit with a single fuse. The fuse needs to be
sufficient for the total current. This also means upgrading the 18
gauge wire in the wings to 14 gauge, to avoid having a fuse too big
for the wire.

Likelihood of incrementally overloading a wire to the
extent that the a 14 AWG wire 'burns' if it happens to
be protected by say a 25A fuse is exceedingly low. The
vast majority of overload faults in DC systems are pretty
hard . . . 10-100 times the ratings of fuses or wires.
Further, wires are quite robust. See:

http://aeroelectric.com/Pictures/Wire/22AWG_20A.pdf

That little strand of 22AWG wire in the picture has
be loaded to 20A for over thirty minutes. Its temperature
rose to only 115C while the insulation was rated for
150C.
Quote:
So my gut feel is to use the 35C Rise part of the table to pick a
current rating for the fuse, which would give me 15A fuse for 14 gauge
wire. Correct ?

Also, the calculations quite clearly include the return to ground part
of the current when calculating wire losses due to resistance. What
equivalent resistance value would be typical of the frame of aluminum
aircraft when used for the ground return ?

For all practical purposes, your airplane as a ground conductor
has zero ohms resistance. I've measured tip to tail on a Model
400 Beechjet at 0.0012 ohms. I've measured crankcase to battery
minus on a C-172 at 0.008 ohms . . . where virtually all the
resistance came from poor joints in the connectors and wiring.
The airframe itself was under 1 milliohm.

Don't spend a lot of time on it. I'd go with 14AWG throughout
the system and a 15A fuse. If you find that your landing lights
nuisance trip the fuse after x-times of turning them on, then
up-size to a 20A fuse and leave the wires alone. It will
be just fine.

Bob . . .


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jpx(at)Qenesis.com
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PostPosted: Thu Jul 10, 2008 5:20 am    Post subject: Fuse Sizing Reply with quote

Quote:
In the case of the ATC plastic devices, the data shows
http://www.egauges.com/vdo_mult3.asp?Type=Voltmeter12&Series=Cyber_Red&Units=E . . . that you can probablyuse a 10A fuse in a
circuit
that draws 10A continuously.


The above link points to a voltmeter, not a graph of fuse performance,
which I would like to see.

The rest of the post answered my questions, thank you kindly, so I can
continue with my design.

Do not archive

Jeff Page
Dream Aircraft Tundra #10


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PostPosted: Thu Jul 10, 2008 8:00 am    Post subject: Fuse Sizing Reply with quote

At 09:16 AM 7/10/2008 -0400, you wrote:
Quote:


>In the case of the ATC plastic devices, the data shows
>http://www.egauges.com/vdo_mult3.asp?Type=Voltmeter12&Series=Cyber_Red&Units=E
>. . . that you can probablyuse a 10A fuse in a
>circuit
that draws 10A continuously.

The above link points to a voltmeter, not a graph of fuse performance,
which I would like to see.

Sorry 'bout that. Wrong link on the clipboard. Try

http://aeroelectric.com/Mfgr_Data/Fuses_and_Current_Limiters/Bussman/

Here you'll find data on a large number of Bussmann products
including the ATC plastic fuses. In particular, note the
characteristics of the ANL devices. Those critters are REALLY
robust!

A review of these data sheets will reinforce the notion that
not all devices called "fuses" have the same or even similar
performance. Each product was designed to meet the design goals
for a particular task.

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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