Return-Path: Received: from envelope.rose-hulman.edu ([137.112.8.21] verified) by logan.com (CommuniGate Pro SMTP 4.2b6) with ESMTP-TLS id 245698 for flyrotary@lancaironline.net; Wed, 07 Jul 2004 02:56:22 -0400 Received: from bob (c-24-8-167-234.client.comcast.net [24.8.167.234]) (authenticated (0 bits)) by envelope.rose-hulman.edu (8.11.6/8.11.6) with ESMTP id i676tn620775 (using TLSv1/SSLv3 with cipher RC4-MD5 (128 bits) verified NO) for ; Wed, 7 Jul 2004 01:55:50 -0500 (EST) From: "Alex Madsen" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] Re: High Temperature Epoxy Selection Date: Wed, 7 Jul 2004 12:55:35 -0500 Message-ID: <005801c4644b$9bc63700$6401a8c0@bob> MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.2627 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2600.0000 Nice site. I will call them tomorrow and see what they have to say. Maybe I can get a test sample or the "student experiment" discount. Alex Madsen P.S. (I am not sure if I should mention this yet) If all goes will with manifold development I may eventually look into compost exhaust with this stuff: http://www.graphitestore.com/itemDetails.asp?item_id=1561&prd_id=6&cat_i d=4&curPage=1 This will be an even more interesting experiment. Alex Madsen -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Marvin Kaye Sent: Wednesday, July 07, 2004 12:43 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: High Temperature Epoxy Selection I did a Google search on "high temperature laminating epoxy" and came up with a huge amount of hits. I particularly liked what I saw at De-Comp Composites... http://www.decomp.com/indexA.htm. Once there and poking around I noticed that some of their product line is used by Boeing... quite the recommendation. Down in the hi-temp laminating area I spotted all sorts of resin systems, all requiring post cure, and all with very impressive strength numbers. I clicked on their link to a hi-temp flame retardant system (http://www.decomp.com/laminate/htlfr.htm) which is good to a HDT of 375F, has a mixed specific gravity of 1.11 (figure 11% thicker than water... excellent for layups) and thought it would be an ideal candidate. Post cures in a kitchen oven (if the parts will fit and the Missus doesn't mind) is actually quite simple, as is vacuum bagging. You don't actually need a real vacuum pump, as you can pull a good vacuum with a shop-vac or on the intake side of your air compressor. I buy my bagging supplies from FibreGlast Developments (hardware & fittings, bagging plastic, sealing tape) but I get my peel ply from Aircraft Spruce and my breather ply from Joanne Fabrics (polyester fiber-fill batt insulation). ACS is also a reasonbly priced source for carbon fiber ($16.95/yd is excellent). I have paid as much as $37/yd for wider crow's foot weave, but that is a bit of a specialty product... much stronger than plain weave, goes around curves really well and pleasant to work with... it's just expensive. Attached is my latest CF creation.. it's a ventral fin I added to the tail of the IVP I've been talking about. There are 14 plies around the edges and there's about no deflection when you beat on it. It's basically 4 plies CF each side over a hardwood-strengthened foam core with the edges wrapped and the whole thing peel plyed. I really enjoy composite work, and am always happy to talk about it. Enough for now. Thanks for listening.