geraldmorrissey
Senior Member
Last Activity: Yesterday, 10:01 PM
Joined: 09-24-2013
Location: Edgewood, WA
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When confronted with issues like this I tend to make the part long and trim on assenbly. If you cut too short you may have scrap. Its tough to scrap a... -
I would argue that carbon fiber is more hazardous then glass. Check www.osha.gov technical manual OTM section 3 chapter 1 polymer matrix for more info....Last edited by geraldmorrissey; 03-25-2020, 03:44 PM.Leave a comment:
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You might consider West 105. Its low shrink, fairly thin so it wets out pretty well, has a big customer base and you can buy it by the quart. Worth a...Leave a comment:
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About 35 years ago I was working as a contract engineer at Beech on the Starship. It was months of 7 days a week trying to build tooling, the first airplane...Last edited by geraldmorrissey; 03-23-2020, 12:54 PM.Leave a comment:
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Second most everything Ed said, to give some perspective, aerospace quality laminates used as class one structure on airliners and fighters have a resin...Leave a comment:
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Bear in mind that the majority of weight in a homebuilt composite laminate is resin. Whatever you end up using for resin, if you do not carefully control...Leave a comment:
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New Jundmans are being built in Europe. I know of at least one that was imported into the US and powered with an 0-360. For the fat of wallet. See type...Leave a comment:
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On the forward spars I laid out the upper and lower rib location cap strip holes then used the rivet fan to locate the rest. I used homemade drill blocks...Leave a comment:
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Welcome aboard. Small steps are good.
Gerry
Patrol #30Leave a comment:
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Shop Renovation
Haven't checked in for a while. Been overhauling my shop. It's close to being done. 480 sq ft of 5/8" code X drywall on the ceiling broke my back.... -
You might consider Aircraft Soruce p/n 03-48900. Relieve the fwd flanges where the trailing edge of the ribs fit. I think you could get a pipe cleaner...Leave a comment:
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