Simple Sonex Wing Fold Bracket
Posted: Mon Nov 14, 2011 12:21 am
All,
I'm new here, and I'm sure this subject has already been discussed, so please just send me to the right spot or web site and I'll hush.
Like a lot of those considering the Sonex, I'd sure like to be able to fold the wings by myself (to more easily pack more planes into a hangar, to put the beast onto an enclosed trailer to store at home, or for stowage in a shipping container at the field). Having to have a second person to detach the wings is a significant inconvenience when one just want to go fly around for a couple of hours. What have folks tried in order to make this happen?
Working from a position of ignorance, the simplest approach I can think of would be similar to the smart external wing folding bracket Dave Thatcher engineered for the CX4. It's not very sexy, but it adds almost no weight to the airplane and it gets the job done. It would have to be modified quite a bit for the Sonex (due to the Sonex's long carry-through spar), but it seems do-able. You'd probably need 3 things:
1) A small support (mini-sawhorse) to hold up the wingtip during wing detach/attach operations. This stays with the trailer/on the ground.
2) A "saddle" to go over the rear of the airplane just in front of the V-Stab, it has craddles to hold the leading edges of both wings once they are folded back. A slicker way to do this would be pins/brackets that pop out from the fuselage rear to engage slots in the bottom of the wing (like the S-18 version of the Thorp T-18 does things), but that's more complex.
3) A removable external wing support and pivot bracket (one needed per wing, these stay on the ground once the wing is on the airplane). This would be the heart of the concept, holding up the root end of the wing while it was being withdrawn from the person at the wingtip, and providing a means for the wing to pivot two ways: First "twisting" so that it is leading-edge down, then pivoting back so it is aligned with the fuselage and can be supported by the cradles (part 2 above). I can imagine a few simple ways this could be done with a rod, a bushing and a trolley to engage the spar. The ideal system would require no modifications to the spar.
Anyway, before I go on--what have smarter folks done?
Thanks for any ideas. If I had $200 per month for hangar rent this wouldn't be an issue.
Mark
I'm new here, and I'm sure this subject has already been discussed, so please just send me to the right spot or web site and I'll hush.
Like a lot of those considering the Sonex, I'd sure like to be able to fold the wings by myself (to more easily pack more planes into a hangar, to put the beast onto an enclosed trailer to store at home, or for stowage in a shipping container at the field). Having to have a second person to detach the wings is a significant inconvenience when one just want to go fly around for a couple of hours. What have folks tried in order to make this happen?
Working from a position of ignorance, the simplest approach I can think of would be similar to the smart external wing folding bracket Dave Thatcher engineered for the CX4. It's not very sexy, but it adds almost no weight to the airplane and it gets the job done. It would have to be modified quite a bit for the Sonex (due to the Sonex's long carry-through spar), but it seems do-able. You'd probably need 3 things:
1) A small support (mini-sawhorse) to hold up the wingtip during wing detach/attach operations. This stays with the trailer/on the ground.
2) A "saddle" to go over the rear of the airplane just in front of the V-Stab, it has craddles to hold the leading edges of both wings once they are folded back. A slicker way to do this would be pins/brackets that pop out from the fuselage rear to engage slots in the bottom of the wing (like the S-18 version of the Thorp T-18 does things), but that's more complex.
3) A removable external wing support and pivot bracket (one needed per wing, these stay on the ground once the wing is on the airplane). This would be the heart of the concept, holding up the root end of the wing while it was being withdrawn from the person at the wingtip, and providing a means for the wing to pivot two ways: First "twisting" so that it is leading-edge down, then pivoting back so it is aligned with the fuselage and can be supported by the cradles (part 2 above). I can imagine a few simple ways this could be done with a rod, a bushing and a trolley to engage the spar. The ideal system would require no modifications to the spar.
Anyway, before I go on--what have smarter folks done?
Thanks for any ideas. If I had $200 per month for hangar rent this wouldn't be an issue.
Mark