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$500 on these. They ended up to be super labor intensive and the amount of laser on the brackets didn't help. They really turned out well, a very pretty piece. 1.14lbs less than stock. Yours will be quite a bit less because of the design, but well talk about that. Thanks for the compliments guys, it was a fun part to build!That was fast! They look awesome as usual for your stuff! PM me the price when you get it figured out, so I can budget for a few of them. Thanks!
Any plans for a tee top?
Aluminum loses 50%+ of its strength when you weld on it. You can get it cryo. gen treated or heat treated after the weld process to regain most of that temper strength, but have not really had any personal experience with the re tempering process on alum. My honest answer to how much weaker...not sure. Wish I had a better answer as to strength, but all I know is alum is never a great choice when it needs to be welded on. Ever see an airplane with an alum welded part..thats why. Next time you board, notice all the rivets holding the wing panels on. Thanks!Nice!
I have a question (if you don`t mind) for you alt cause your in the biz (cause I`m into a long term project lol).
If I build the same thing in 7071 aluminum but 25% thicker, theoretically it is the same weight (right?), but how much weaker (theoretically lol) will it be using the standard mount positions?
Unobtanium is hard to find up here but lots of aluminum sources.
Aluminum loses 50%+ of its strength when you weld on it. You can get it cryo. gen treated or heat treated after the weld process to regain most of that temper strength, but have not really had any personal experience with the re tempering process on alum. My honest answer to how much weaker...not sure. Wish I had a better answer as to strength, but all I know is alum is never a great choice when it needs to be welded on. Ever see an airplane with an alum welded part..thats why. Next time you board, notice all the rivets holding the wing panels on. Thanks!
Dan
I think I have commited myself for the t top with loudhandle, but haven't settled on a height. With my time as limited as its ever been Ill have to see what I can come up with for a universal type jig for length without spending too much time on it. Just not a great time of year to be doing change ups, and im not one to rush through it, but im sure I can make it happen. Thanks!Aluminum is old school in aviation. Carbon Fiber is the new aluminum.
Hopefully you guys will get to fly on an 787 soon and you'll know what I am talking about. Talk about Cadillac. And way overbuilt.
Nice post. A T-type post will handle more force than a flat post. If you do rejig, I'd be interested.
Lol ya To say I've been spread pretty thin this year is a large understatement. Sorry I missed ya yesterday no time to bs until things calm down. Couple more weeks. Pm me some info and I'll make a phone call.Hey if you would quit building new stuff maybe you could bs a little so I don't have to go to work.
What about building a titanium over structure?