What's the preferred method for attaching the aluminum fuselage formers? There are pros and cons to both rivets and nutplates, I'm curious what others think.
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Huh, why stainless instead of steel or aluminum? I'm assuming 1/8" protruding head?
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Brooks Cone
Southeast Michigan
Patrol #303, Kit build
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Don't know about the other folks, but I found that by starting at the tail, it was pretty easy to just fit the stringers into the U-shaped brackets, and clamp in place with C-clamps. The stringers bent pretty naturally to a nice, smooth curved shape. Then I drilled, de-burred, and riveted with stainless steel pull rivets, as Mark recommended.Jim Parker
Farmersville, TX (NE of Dallas)
RANS S-6ES (E-LSA) with Rotax 912ULS (100 HP)
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Originally posted by JimParker256Don't know about the other folks, but I found that by starting at the tail, it was pretty easy to just fit the stringers into the U-shaped brackets, and clamp in place with C-clamps. The stringers bent pretty naturally to a nice, smooth curved shape. Then I drilled, de-burred, and riveted with stainless steel pull rivets, as Mark recommended.
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Originally posted by SimonNicholson View Post
That is what I did too. Is taking that stress out of the stringers by pre bending important?
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Donna asked about my unsatisfactory method.
The bottom formers were no problem. When I installed my side formers I did not try starting at the tail like Jim Parker. I was not aware of Mark G's method for bending the formers. Instead I started from the front and worked my way back.
The unmodified formers placed a significant amount of stress on one of the fuselage tubes when I fit into place. By fit, I mean I applied pressure to the stringer to force it into its "clip" and make a nice bend to form the fuselage contour. When I placed pressure on the former, the stringer (Which is really tough material...way stronger than needed...a mark of good quality) would spring into position, but not yield. It did not bend, and this put pressure on the fuselage tubing. I was not comfortable with this at one particular point. Stresses were just too high.
My fix was to remove some material from the former and bend the tubing by using a method I show in photos below. I got the former bent and fit into the clips nicely so I thought. But the shape that resulted from my method did not result in a nice rounded appearance. At every point where I 'shaped' (by drilling a stop hole, cutting into the inside edge of the former, and slightly bending the former at the place where I cut it.) the tubing it resulted in a bend, followed by a straight section of the former. So looking at it from the rear, I got a squarish look rather than a nice rounded shape that it should be. It just looked goofy, and I wasn't going to let it go.
So, I got some replacement stringers from Mark G. (Thanks to scratch Patrol builder Ed Welfred from my neck of the woods for transporting them) and will do them over.
TAKE AWAY for those quick build kit owners just starting: If have some doubt about a task, e-mail Mark G. instead of trying to figure it out on your own. Don't guess, and don't experiment at least until you have found out how Mark does it. I did not do that. I guessed.
You can see the squarish look in the stringer in this photo to the left of the top of the Cleco.
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Brooks Cone
Southeast Michigan
Patrol #303, Kit build
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That's exactly how we made the top former bend for the removed skylight. I also have a couple of spots where removal of inside former material was necessary for a fuel line to pass through. As I stated before, doesn't seem to be a problem, as of 215 hours anyway.
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Ok, unfortunately I'm still kind of confused about this so please bear with me. If I attach the aluminum fuselage formers (I'm not talking about the stringers) with protruding head stainless pop rivets, how then am I supposed to lay a scuff shield over the formers that make up the door sills? Won't the protruding heads look odd and possibly interfere with the cargo doors as well? If anyone can shoot a pic of what they've done I would really appreciate it.
I'm also wondering why stainless since it will possibly corrode both the aluminum and steel parts that it's securing? Where did Bob spec these?
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Originally posted by PaulSA View PostI countersunk the formers - problem solved.......
As for the corrosion worries, there are all sorts of places in the aircraft where materials are mixed. Provided there is no moisture, then there won't be corrosion
For corrosion, yeah that's right, but since I'm at it why not go ahead and use materials that aren't galvanically reactive?
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I used driven rivets in some places but found that there were a lot of places where it was either difficult to get a bucking bar on the back or that things like fuel pipes get in the way. In those places I used pulled C/S rivets.
The tabs are steel and the formers are aluminium so whatever rivets you use, you can't avoid some sort of dissimilar materials. I have primed the aluminium and smeared an anti-corrosive sealant on all the tabs where I have riveted AL to steel.
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