JeeperMatt
NAXJA Forum User
- Location
- Whidbey Island, WA (misplaced Texan)
I'm a DIY guy, so I've decided to build my body armor panels. Before getting too deep into designs and whatnot I had a couple questions to throw out there for y'all's opinions, experiences, and so on.
1. Weld-on vs bolt-on. I know the sheetmetal is pretty damn thin, and I don't want to go blowing holes all over the place. If welding them on is alright, I plan on tacking then welding in small sections at opposite ends to minimize warpage and other issues.
Bolt-on would alleviate the warpage/hole blowing issues entirely. I do a ton of metal-work on a regular basis (airframer in the Navy), so counter-sinking holes and whatnot is something I'm quite proficient at. Bit more tedious, considering that some panels would require disassembling the interior to access the backside for bolts. Also, sealing the panels to the body to prevent water-intrusion. The bolt-on method also ties into the material selection I address below (I know you can't weld aluminum to steel without a bonding strap, and that's way over my intended budget)
2. Steel vs aluminum. Again, thanks to my job I have access to a ton of scrap aluminum (let me specify, this is scrap metal that we can no longer use on the aircraft). My main thought here is weight-savings as I know steel can add up in the heft department fairly quickly.
I've done some research on what's on the market already, granted it's pretty much Wrangler-exclusive. However, the alloy of choice seems to be 6061 compared to the 5056 that I have access to. This doesn't seem to be an issue as overall tensile strength for 5056 is nearly double that of 6061 (42000psi compared to 17000). There's a good variety of metal thickness and tempering available as well.
Suggestions on what thickness and tempering would be best? The majority of what I can get is T3, with a good amount of T6 thrown in too - all in the typical thicknesses. I just don't want to go through all the effort only to have it gouge and chunk off on the first hit.
Appreciate any ideas, suggestions, and thoughts y'all can throw my way!
- M@
1. Weld-on vs bolt-on. I know the sheetmetal is pretty damn thin, and I don't want to go blowing holes all over the place. If welding them on is alright, I plan on tacking then welding in small sections at opposite ends to minimize warpage and other issues.
Bolt-on would alleviate the warpage/hole blowing issues entirely. I do a ton of metal-work on a regular basis (airframer in the Navy), so counter-sinking holes and whatnot is something I'm quite proficient at. Bit more tedious, considering that some panels would require disassembling the interior to access the backside for bolts. Also, sealing the panels to the body to prevent water-intrusion. The bolt-on method also ties into the material selection I address below (I know you can't weld aluminum to steel without a bonding strap, and that's way over my intended budget)
2. Steel vs aluminum. Again, thanks to my job I have access to a ton of scrap aluminum (let me specify, this is scrap metal that we can no longer use on the aircraft). My main thought here is weight-savings as I know steel can add up in the heft department fairly quickly.
I've done some research on what's on the market already, granted it's pretty much Wrangler-exclusive. However, the alloy of choice seems to be 6061 compared to the 5056 that I have access to. This doesn't seem to be an issue as overall tensile strength for 5056 is nearly double that of 6061 (42000psi compared to 17000). There's a good variety of metal thickness and tempering available as well.
Suggestions on what thickness and tempering would be best? The majority of what I can get is T3, with a good amount of T6 thrown in too - all in the typical thicknesses. I just don't want to go through all the effort only to have it gouge and chunk off on the first hit.
Appreciate any ideas, suggestions, and thoughts y'all can throw my way!
- M@
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