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Fuselage as ground conductor

 
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Eric M. Jones



Joined: 10 Jan 2006
Posts: 565
Location: Massachusetts

PostPosted: Fri Feb 07, 2014 5:04 pm    Post subject: Fuselage as ground conductor Reply with quote

Bob N., et al.:

When one builds an airplane with the starter and the battery some distance apart, using the fuselage as a ground conductor is usually (?) done. What is the resistance of a typical fuselage used in this way? Can it carry 200A or so for the starter?

What are your thoughts?


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nuckolls.bob(at)aeroelect
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PostPosted: Sat Feb 08, 2014 5:48 am    Post subject: Fuselage as ground conductor Reply with quote

At 07:04 PM 2/7/2014, you wrote:
Quote:


Bob N., et al.:

When one builds an airplane with the starter and the battery some
distance apart, using the fuselage as a ground conductor is usually
(?) done. What is the resistance of a typical fuselage used in this
way? Can it carry 200A or so for the starter?

What are your thoughts?

The fuselage of a metal airplane taken as a whole
is entirely capable of carrying and/all electrical system
ground loads. As a rule of thumb, we used to consider
the tip-to-tail resistance of an airplane like the Beechjet
to be on the order of 0.001 ohms.

How about attaching a high current conductor to the
airframe? Imagine a 1" diameter disk of .032 aluminum
being approached radially from all directions by an
array of 0.032" square aluminum wires (roughly 20AWG
equivalent). You can attach 3.14/.032 numbers of
these wires to the edge of the disc for a total of
100 such wires. What's the current carrying capacity/
resistance of 100 strands of 20AWG in either aluminum or copper?

The point of this exercise is to support the notion
that the sheet resistance of just about any part
of an airframe is very low; assuming all the pieces
are well attached to each other, point-to-point
resistance between any two locations on the airframe
is also very low.

Airplanes that get into conductor troubles with
grounding over time are instances where a particular
contiguous piece of aluminum has experienced the
effects of moisture and high density electron
flow at the joints where gas-tightness is lost.

You can ground batteries at the tail to about any
mechanically robust feature that is protected from
the weather and stays dry.

http://tinyurl.com/mcv3c9j

I would ground a crankcase to the firewall
sheet at a centralize grounding location like the
B&C ground bus and not depend on engine mount
for ground.

Other than that, the only caveats for airframe
grounding are the potential for injecting
electrical system noise into vulnerable appliances
by injudicious choices for grounding the
victim . . . ground loops.

Bob . . .


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PostPosted: Sat Feb 08, 2014 11:09 am    Post subject: Fuselage as ground conductor Reply with quote

Good Afternoon Bob,

Obviously, I am getting into this a bit late, but what about airplanes like the newer Bonanzas where all skins and stringers were painted prior to assembly? No doubt that the rivets when driven would spread to contact each joined skin, but would that be sufficient area to carry the current?

Happy Skies,

Old Bob

In a message dated 2/8/2014 8:17:22 A.M. Central Standard Time, nuckolls.bob(at)aeroelectric.com writes:
Quote:
--> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>

At 07:04 PM 2/7/2014, you wrote:
Quote:
--> AeroElectric-List message posted by: "Eric M. Jones" <emjones(at)charter.net>

Bob N., et al.:

When one builds an airplane with the starter and the battery some
distance apart, using the fuselage as a ground conductor is usually
(?) done. What is the resistance of a typical fuselage used in this
way? Can it carry 200A or so for the starter?

What are your thoughts?

The fuselage of a metal airplane taken as a whole
is entirely capable of carrying and/all electrical system
ground loads. As a rule of thumb, we used to consider
the tip-to-tail resistance of an airplane like the Beechjet
to be on the order of 0.001 ohms.

  How about attaching a high current conductor to the
airframe? Imagine a 1" diameter disk of .032 aluminum
being approached radially from all directions by an
array of 0.032" square aluminum wires (roughly 20AWG
equivalent). You can attach 3.14/.032 numbers of
these wires to the edge of the disc for a total of
100 such wires. What's the current carrying capacity/
resistance of 100 strands of 20AWG in either aluminum or copper?

The point of this exercise is to support the notion
that the sheet resistance of just about any part
of an airframe is very low; assuming all the pieces
are well attached to each other, point-to-point
resistance between any two locations on the airframe
is also very low.

Airplanes that get into conductor troubles with
grounding over time are instances where a particular
contiguous piece of aluminum has experienced the
effects of moisture and high density electron
flow at the joints where gas-tightness is lost.

You can ground batteries at the tail to about any
mechanically robust feature that is protected from
the weather and stays dry.

http://tinyurl.com/mcv3c9j

I would ground a crankcase to the firewall
sheet at a centralize grounding location like the
B&C ground bus and not depend on engine mount
for ground.

Other than that, the only caveats for airframe
grounding are the potential for injecting
electrical system noise into vulnerable appliances
by injudicious choices for grounding the
victim . . . ground loops.

  Bob . . . = Use ilities ay - MATRONICS WEB FORUMS - List Contribution Web Site p;  


[quote][b]


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