Return-Path: Sender: (Marvin Kaye) To: lml Date: Sun, 07 Jul 2002 14:40:13 -0400 Message-ID: X-Original-Return-Path: Received: from smtprelay2.dc3.adelphia.net ([24.50.78.5] verified) by logan.com (CommuniGate Pro SMTP 4.0b4) with ESMTP id 1620627 for lml@lancaironline.net; Sun, 07 Jul 2002 10:37:16 -0400 Received: from worldwinds ([207.175.254.66]) by smtprelay2.dc3.adelphia.net (Netscape Messaging Server 4.15) with SMTP id GYVVA300.Y0A for ; Sun, 7 Jul 2002 10:37:15 -0400 From: "Gary Casey" X-Original-To: "lancair list" Subject: gear leg fairings X-Original-Date: Sun, 7 Jul 2002 07:36:39 -0700 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) Importance: Normal X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2600.0000 When I got to the gear leg fairing part of my ES I was dissatisfied with the shape of the parts in the kit. After briefly thinking about alternative ways to do the job I came up with a technique that might be interesting to others. At the local fabric store I bought some Nylon "Spandex" (should have seen the looks I got). I cut out a piece about the right shape and started taping it to the gear leg and fuselage with small pieces of duct tape. By adjusting the tension in the various directions I was able to get one shape to match the inside half and the "leading edge." I then laid a 1-BID over it. I found that putting the metallic "glitter" side out made it a little easier to verify that the lay-up was in contact. Any more than 1-BID might be heavy enough to deform the rather delicate shape of the Spandex. The outer (armpit) side was a little more difficult, but by this time I was practiced so it went pretty quickly. In retrospect, it would have been better to use at least a couple different overlapping lay-ups as the one piece method wouldn't easily fold around the leading edge, leaving me to do that with micro and sanding. The resulting cured part easily popped off the "mold" and then I trimmed the rough edges and added more BID. I left it at 3-BID for most of it with 4-BID at the overlaps of the sections and at the flange around the periphery. I then permanently joined the inner and outer halves and extended the fairing out to cover the wing root inspection holes. For service the plan is to unscrew the fairing from the fuselage and slide it down the gear leg, exposing the gear attachment and the wing root access. The plan now is to add micro over the top and sand to take out the inevitable imperfections. The limitation of the technique is that the shape has to be concave in at least one direction, giving a way to stretch the fabric into shape. Once in rough shape it is easy to add or reduce tension in a spot to change the shape and the result is inherently smooth with no bumps or wrinkles. Don't know if this technique will result in a part that will stand up to the more discriminating judges, but at about 30 minutes to make a mold, it sure was easy. Gary Casey ES project