VansAirForceForums  
Home > VansAirForceForums

Addicted to the site?
Donate yearly (please).
Advertise in here!
Today's Posts | Insert Pics






  #1  
Old 09-20-2007, 01:02 PM
N787R N787R is offline
 
Join Date: Apr 2007
Location: San Jose, Ca
Posts: 60
Default Grounding to Airframe & corrosion

When using the airframe for ground wire return (Like the stuff on the wing tip), Does that cause more corrosion?
Grounding causes current to flow via airframe. Flow of current can encourage corrosion.
I always see a lot of corrosion around battery cables in my car. That is why I was concerned.

Ben
Reply With Quote
  #2  
Old 09-20-2007, 01:38 PM
az_gila's Avatar
az_gila az_gila is offline
 
Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 3,954
Exclamation Use correct materials...

Not a problem if you use the correct materials for the ground connection.

Check the Electrical section in AC 43.13

However, for aluminum structures the use of cadmium plated steel hardware (standard AN hardware) is the correct procedure.

gil A
__________________
Gil Alexander
EAA Technical Counselor, Airframe Mechanic
RV-6A VSB (Very Slow Build)
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
Reply With Quote
  #3  
Old 09-20-2007, 01:43 PM
gmcjetpilot's Avatar
gmcjetpilot gmcjetpilot is offline
 
Join Date: Jan 2005
Posts: 3,606
Default Do one better

Cad plating is magic. Seriously its good stuff and this follows the galvanic scale of dissimilar metals. You may get away with some poor pairs for a while, especially if its really dry. However mosture will accelerate galvanic corrosion, but not over night, it may take many years. Good for you to be concern. Of course mosture adds to the mix. Here's from the FAA standard practice AC mentioned above. Its a good start and shows proper ground studs. (Click)






__________________
George McQueen
Raleigh, NC area.
RV-4, RV-7, ATP, CFII, MEI, 737/757/767

Last edited by gmcjetpilot : 09-20-2007 at 01:49 PM.
Reply With Quote
  #4  
Old 09-21-2007, 10:08 AM
MNRVFlyer MNRVFlyer is offline
 
Join Date: Feb 2007
Location: MN
Posts: 148
Default

George,

I really like reading your posts. If I see something you posted I always read it. Sometimes I even understand them! Thanks!
Reply With Quote
  #5  
Old 09-22-2007, 10:52 AM
minute2 minute2 is offline
 
Join Date: Mar 2007
Location: Beaverton, OR
Posts: 36
Default Good question

This had never occured to me, but once you mention it I realize how obvious this is. I immediately thought of a Mythbusters episode where they used the powersupply from a small radio and some salsa to corrode away a 1 inch diameter steel bar. I believe that corrosion would be accelerated anywhere the current passes that anodic and cathodic potentials exist. The use of cadmium plated hardware for the ground hookup prevents corrosion at the attachment of the ground, however, there could/would be corrosion occuring elsewhere. I think we get away with this because the airplane, and its electronics, operate for relatively short periods of time and the corrosion that results is minimal. The real corrosion acts slowly over thousands of hours while the plane sits at its tiedown with the current for the corrosion cells generated by difference in electrochemical potental between metals. (rust never sleeps)
__________________
RV-8A: Finished wings, working on fuselage.
Reply With Quote
  #6  
Old 09-22-2007, 01:14 PM
marchudson marchudson is offline
 
Join Date: Feb 2006
Location: East Texas
Posts: 84
Default ground return

What about a ground return line to a common ground bus?
I understand this adds weight but no grounding problems
to worry about. Just an idea.
Reply With Quote
  #7  
Old 09-22-2007, 04:39 PM
nucleus nucleus is online now
 
Join Date: Sep 2006
Posts: 725
Talking Do Both!

Quote:
Originally Posted by marchudson View Post
What about a ground return line to a common ground bus?
I understand this adds weight but no grounding problems
to worry about. Just an idea.
If I were to build another plane, I would do both, ground to the airframe and a ground wire. Redundancy, and this is what Honda does on their cars, so it must be good. Most electrical problems I have seen are ground faults.

Nucleus
Reply With Quote
  #8  
Old 09-22-2007, 08:47 PM
az_gila's Avatar
az_gila az_gila is offline
 
Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 3,954
Exclamation Modern cars

Quote:
Originally Posted by nucleus View Post
If I were to build another plane, I would do both, ground to the airframe and a ground wire. Redundancy, and this is what Honda does on their cars, so it must be good. Most electrical problems I have seen are ground faults.

Nucleus
May not be a good extrapolation. Modern cars seem to isolate body parts with rubber/sealer/shock mounts to keep things quite and stop squeaks. This might be the reason for the separate ground returns.

Most aircraft electrical problems I have seen have been broken wires and poorly made connectors...

gil A
__________________
Gil Alexander
EAA Technical Counselor, Airframe Mechanic
RV-6A VSB (Very Slow Build)
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
Reply With Quote
  #9  
Old 09-23-2007, 02:32 AM
Pilottonny Pilottonny is offline
 
Join Date: Jan 2006
Location: Belgium
Posts: 536
Default Do you prime/paint?

Hello Ben,

Don’t forget that your battery is out in the wet part of the car and the acid of the battery (fumes) helps the corrosion a lot! Also the currents through the battery terminals are a lot higher than through the average ground connector of your equipment.

I am actually at the stage where I am wiring stuff in the fuselage. All my parts are primed, inside and out, before final assembly. This will obviously cause bad ground if I was using the airframe as a ground conductor. So I am running a ground wire to the center wing spar and to some other strategic places, where ground wires from various equipment (strobe power supply, AP-servo, flap motor, etc.) connect to. For all the wings-stuff, I use the wing spar for local ground, because it is anodized and is a good conductor, being bolted to the center section. So far I have not bothered with any special materials for the connections, just plated screws, nuts and washers, with standard ring terminals. As long as everything stays dry (which all these connections normally should), I guess there will be no problems for many years.

Just in case, I will put the ground connections on my “annual” check list, anyway.

Regards, PilotTonny.
__________________
"Pilottonny"
Tonny Tromp
Lanaken, Belgium (EU)
RV9A, Registration: PH-VAN
ECI-Titan IOX-320 with dual EI.
Waiting on paperwork before first flight.......
Reply With Quote
  #10  
Old 09-23-2007, 07:27 AM
DanH's Avatar
DanH DanH is offline
 
Join Date: Oct 2005
Location: Wetumpka, AL
Posts: 2,008
Default

<<because it is anodized and is a good conductor>>

No....anodizing is an insulator.
__________________
Dan Horton
RV-8 QB - Alabama
Barrett IO-390
Reply With Quote
Reply


Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump


All times are GMT -6. The time now is 08:34 PM.


The VAFForums come to you courtesy Delta Romeo, LLC. By viewing and participating in them you agree to build your plane using standardized methods and practices and to fly it safely and in accordance with the laws governing the country you are located in.