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Europa-List: Re: lightning bonding

Subject: Europa-List: Re: lightning bonding
From: TELEDYNMCS@aol.com
Date: Wed, 11 Jun 2008 08:05:22
In a message dated 6/11/2008 3:03:20 AM Eastern Daylight Time,  
europa-list@matronics.com writes:

Not  sure thats a terribly good idea.

Hi Carl, et al,

Apparently, the FAA and Aeromot think it is a good idea. The Ximango is a  
certified aircraft, has aluminum fuel tanks and they, too, are bonded  to the 
rest of the metallic parts in the aircraft. In their parts manual,  Aeromot 
refers to these bonding straps installed as "lightning  bonding."

As it has been explained to me by our resident composite Guru here at the  
'Possum Werks, what happens in composite airplanes in a lightning strike to make

 them explode is the super heating of residual moisture that is trapped 
within  the layers of epoxy and cloth at the time of manufacture. When the 
strike

passes through the composite, trapped moisture rapidly heats, expands and  the

structure comes apart explosively.

Having designed, installed and tested lightning protection systems on over  
7000 cellular telephone sites, I've seen this phenomenon quite a  bit with 
fiberglass antenna masts on poorly grounded sites. When a cell antenna  takes a

direct hit it explodes. The tower can take a direct hit and only slight  
discoloration will result. The result of an exploded antenna mast is  similar to
what 
you see after one of those exploding cigars goes off. If the  site is 
properly grounded and bonded, this almost never happens, though. 

What you are trying to do with bonding metallic parts in a plastic  airplane 
is give the lightning a low resistance path to pass through and  exit the 
airplane so that it doesn't take a high resistance (i.e.,  through the 
composite)

path to exit and destroy the airplane. Low resistance is  the key here. By 
providing a low resistance path for the  lightning to pass though you reduce or

eliminate the instantaneous heating  that occurs in high resistance paths 
during a discharge. You also want to  prevent arcing that would occur at loose

metallic fittings, such as rod  ends and any metallic parts that are bolted 
together. These are points of high  resistance and arcing (and welding) can 
result.

What you are doing here is  making all the metallic parts equal in resistance,

therefore equal in potential  when charged. Ohm's law at work. I've heard of 
more than one  occurrence of gliders that did not have bonded control systems 
being  struck in flight and having their control rods welded to the point 
where the  aircraft was no longer controllable and the occupant(s) were forced
to 
bail  out. 

These bolted connections are precisely where the bonding straps are  
installed on the Ximango. The bonding straps that are installed, given  their 
size,

are designed to take a lot more current than a simple static  discharge. They 
are essentially the same thing we install to bond  and protect towers, 
transmission equipment, batteries, fencing, coax,  antennae, etc., in cell sites
---From 
lightning. The reason braided cable is used  is surface area. The more surface

area, the more current it can handle. Braided  cable has much, much more 
surface area than typical  Tefzel aircraft wire or a solid wire, thus more 
current

handling  capacity.

Is it a cure all? No. There is no such thing as perfect lightning  
protection. Will it help save your bacon in a residual discharge situation?  
Probably.

Will it save your bacon in a direct hit? Probably not.

Fred, as far as a source on the bonding straps, try Harger. _www.harger.com_ 
(http://www.harger.com) . If it has anything to do with  lightning protection, 
Harger carries it.

Hope it helps!

Regards,

John  Lawton
Whitwell, TN (TN89)
N245E -  Flying


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