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Ground in an all wood airplane

 
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mrspudandcompany(at)veriz
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PostPosted: Mon Jul 21, 2008 7:07 am    Post subject: Ground in an all wood airplane Reply with quote

Bob,

I am building an all wood plane and plan to use dual electronic ignition. A small gnawing issue is grounding. I will have a rear battery with only a single FAT wire ground coming up to the firewall. Even though I will have my 2 ignition systems on separate battery busses this will leave me with a ground, single point of failure. I have been kicking around some other ideas, but am concerned about generating ground loop noise. I would be interested in your take on this.

Thanks, as always for your advise,

Roger
[quote][b]


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nuckolls.bob(at)cox.net
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PostPosted: Mon Jul 21, 2008 8:31 am    Post subject: Ground in an all wood airplane Reply with quote

At 11:02 AM 7/21/2008 -0400, you wrote:

Quote:
Bob,

I am building an all wood plane and plan to use dual electronic
ignition. A small gnawing issue is grounding. I will have a rear battery
with only a single FAT wire ground coming up to the firewall. Even though
I will have my 2 ignition systems on separate battery busses this will
leave me with a ground, single point of failure. I have been kicking
around some other ideas, but am concerned about generating ground loop
noise. I would be interested in your take on this.

The large wires in your airplane are really
robust. The thoughtfully installed ground wire
is as reliable as prop bolts.

The ground loop issue is addressed with the
ground system architectures described in the
'Connection. In the case of a non-conducting
airplane, bringing everything to the single
point ground location on the firewall will
eliminate any concerns for "loops". In fact,
you would have to go out of your way to
create a ground loop in a non-conducting
airplane.

Bob . . .


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mrspudandcompany(at)veriz
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PostPosted: Mon Jul 21, 2008 9:12 am    Post subject: Ground in an all wood airplane Reply with quote

Bob,

Thanks! This was basically my thoughts also, but I wanted to make sure I
wasn't overlooking something.

Roger
At 11:02 AM 7/21/2008 -0400, you wrote:

Quote:
Bob,

I am building an all wood plane and plan to use dual electronic
ignition. A small gnawing issue is grounding. I will have a rear battery
with only a single FAT wire ground coming up to the firewall. Even though
I will have my 2 ignition systems on separate battery busses this will
leave me with a ground, single point of failure. I have been kicking
around some other ideas, but am concerned about generating ground loop
noise. I would be interested in your take on this.

The large wires in your airplane are really
robust. The thoughtfully installed ground wire
is as reliable as prop bolts.

The ground loop issue is addressed with the
ground system architectures described in the
'Connection. In the case of a non-conducting
airplane, bringing everything to the single
point ground location on the firewall will
eliminate any concerns for "loops". In fact,
you would have to go out of your way to
create a ground loop in a non-conducting
airplane.

Bob . . .


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klehman(at)albedo.net
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PostPosted: Mon Jul 21, 2008 3:04 pm    Post subject: Ground in an all wood airplane Reply with quote

Two separate ground straps from engine to firewall (or forest of tabs)
may be a good idea on an electrically dependent engine though. I like
one of those to go to a starter bolt.
Ken

Robert L. Nuckolls, III wrote:
Quote:

<nuckolls.bob(at)cox.net>

At 11:02 AM 7/21/2008 -0400, you wrote:

> Bob,
>
> I am building an all wood plane and plan to use dual electronic
> ignition. A small gnawing issue is grounding. I will have a rear
> battery with only a single FAT wire ground coming up to the firewall.
> Even though I will have my 2 ignition systems on separate battery
> busses this will leave me with a ground, single point of failure. I
> have been kicking around some other ideas, but am concerned about
> generating ground loop noise. I would be interested in your take on
> this.

The large wires in your airplane are really
robust. The thoughtfully installed ground wire
is as reliable as prop bolts.

The ground loop issue is addressed with the
ground system architectures described in the
'Connection. In the case of a non-conducting
airplane, bringing everything to the single
point ground location on the firewall will
eliminate any concerns for "loops". In fact,
you would have to go out of your way to
create a ground loop in a non-conducting
airplane.

Bob . . .



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Eric M. Jones



Joined: 10 Jan 2006
Posts: 565
Location: Massachusetts

PostPosted: Tue Jul 22, 2008 4:21 am    Post subject: Re: Ground in an all wood airplane Reply with quote

Your problem is no different from those of all plastic airplanes. Seawinds have nose-mounted batteries and 32 feet of HUMONGOUS battery cable going to and from the tail mounted engine. (Note: SteinAir sells Seawind builders and others Perihelion Design Super-2-CCA. Perihelion still sells Super-4-CCA but that will go to SteinAir soon too.)

But this brings up the point that metal monocoque fuselage airplanes with rear-mounted batteries often use the fuselage for grounding. I suspect that this is a bad idea, and I suppose that in SOME cases this could cause starting problems and/or structural problems. Hundreds of amps through crappy corroded/primed/riveted joints in thin aluminum sheets scares me.

Has anyone seen, investigated or measured this???

"...faster horses, younger women, older whiskey, and more money..."
--Cowboy Poet Tom T. Hall


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nuckolls.bob(at)cox.net
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PostPosted: Thu Jul 24, 2008 6:59 am    Post subject: Ground in an all wood airplane Reply with quote

At 05:21 AM 7/22/2008 -0700, you wrote:
Quote:


Your problem is no different from those of all plastic airplanes. Seawinds
have nose-mounted batteries and 32 feet of HUMONGOUS battery cable going
to and from the tail mounted engine. (Note: SteinAir sells Seawind
builders and others Perihelion Design Super-2-CCA. Perihelion still sells
Super-4-CCA but that will go to SteinAir soon too.)

But this brings up the point that metal monocoque fuselage airplanes with
rear-mounted batteries often use the fuselage for grounding. I suspect
that this is a bad idea, and I suppose that in SOME cases this could cause
starting problems and/or structural problems. Hundreds of amps through
crappy corroded/primed/riveted joints in thin aluminum sheets scares me.

Has anyone seen, investigated or measured this???

I've heard a variety of horror stories about the effects
of using an airframe as a ground return. Have no idea
where these originated. My best guess is that someone
observed and perhaps even measured the effects of increased
corrosion of joints when subjected to additional stress
of electron flow.

Corrosion testing in the lab is a huge problem when it
comes to relating the effects to a fielded installation.
But let's consider the big picture. How many hours per
year does an airframe take on the extra burden of electron
flow in the sheet metal? 100, 200? How strong are those
currents compared to locally generated electrolytic
currents? I.e., how much total voltage drop is realized
at any locale on any joint as a result of that current flow . . .
especially in light of the fact that point to point
resistance of structure on most airplanes is a milliohm
or less.

It's obvious that the effects cannot be zero. But given
that for every hour the airplane spends "powered up",
it spends 40-100 hours powered down. I have to believe
that the worst case effects of carrying that nav-light
or pitot-heat ground to the airframe is insignificant
in the overall scheme of things. I'll combine this idea
with the fact that the industry still regularly uses
local grounds on EVERY model of aluminum airplane.

Bob . . .


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