Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Sun, 06 Jun 2004 07:12:34 -0400 Message-ID: X-Original-Return-Path: Received: from c60.cesmail.net ([216.154.195.49] verified) by logan.com (CommuniGate Pro SMTP 4.2b5) with ESMTP-TLS id 141251 for lml@lancaironline.net; Sun, 06 Jun 2004 00:57:46 -0400 Received: from unknown (192.168.1.40) by c60.cesmail.net with QMQP; 06 Jun 2004 00:57:15 -0400 Received: from adsl-67-122-110-7.dsl.sntc01.pacbell.net (adsl-67-122-110-7.dsl.sntc01.pacbell.net [67.122.110.7]) by webmail.spamcop.net (Horde) with HTTP for ; Sat, 5 Jun 2004 21:57:15 -0700 X-Original-Message-ID: <20040605215715.cy4jj4k8ks004g00@webmail.spamcop.net> X-Original-Date: Sat, 5 Jun 2004 21:57:15 -0700 From: bob mackey X-Original-To: lml@lancaironline.net Subject: Re: [LML] Wing Wire conduct MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1" Content-Disposition: inline Content-Transfer-Encoding: 7bit User-Agent: Internet Messaging Program (IMP) 4.0-cvs >> The black electrical conduct that Lancair supplies needs to be completely >> sealed in the fuel bays. Has anyone used an alternate material that only >> needs to be sealed at the ribs? > Why not use thin-walled aluminum tubing? It's lighter than the plastic hose, > fuel proof, and meets your "sealed-at-the-ribs" criterion. Just a thought. Here's one reason not to use aluminum tubing as conduit in a lancair fuel bay: The thermal expansion coefficient of aluminum is very different from the glass and carbon used in the rest of the wing. At temperatures much different from the construction temperature, the aluminum tube might pull (cold) or push (hot) on the ribs enough to create new fuel leaks. Figure the length of the run and the differences between the hottest and coldest service temperature to determine the total strain. See if your ribs will comfortably accept that amount of strain. The same forces will also cause the tubing to expand and shrink relative to the hole they pass through. Make sure the bond is flexible enough to accomodate that strain as well as the longitudinal strain. - bob mackey flying a 235 building a 320 103MD -at- pure-flight.com [use this email address - the one at the top is spam bait]