X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 1 [X] Return-Path: Received: from sj-iport-5.cisco.com ([171.68.10.87] verified) by logan.com (CommuniGate Pro SMTP 5.1.4) with ESMTP id 1731161 for flyrotary@lancaironline.net; Tue, 02 Jan 2007 16:19:05 -0500 Received-SPF: softfail receiver=logan.com; client-ip=171.68.10.87; envelope-from=echristley@nc.rr.com Received: from sj-dkim-6.cisco.com ([171.68.10.81]) by sj-iport-5.cisco.com with ESMTP; 02 Jan 2007 13:17:58 -0800 Received: from sj-core-4.cisco.com (sj-core-4.cisco.com [171.68.223.138]) by sj-dkim-6.cisco.com (8.12.11/8.12.11) with ESMTP id l02LHwWb005681 for ; Tue, 2 Jan 2007 13:17:58 -0800 Received: from xbh-rtp-201.amer.cisco.com (xbh-rtp-201.cisco.com [64.102.31.12]) by sj-core-4.cisco.com (8.12.10/8.12.6) with ESMTP id l02LHRUh024660 for ; Tue, 2 Jan 2007 13:17:58 -0800 (PST) Received: from xfe-rtp-201.amer.cisco.com ([64.102.31.38]) by xbh-rtp-201.amer.cisco.com with Microsoft SMTPSVC(6.0.3790.1830); Tue, 2 Jan 2007 16:17:38 -0500 Received: from [64.102.38.200] ([64.102.38.200]) by xfe-rtp-201.amer.cisco.com with Microsoft SMTPSVC(6.0.3790.1830); Tue, 2 Jan 2007 16:17:38 -0500 Message-ID: <459ACBF1.6070004@nc.rr.com> Date: Tue, 02 Jan 2007 16:17:37 -0500 From: Ernest Christley Reply-To: echristley@nc.rr.com User-Agent: Mozilla Thunderbird 1.0.7-1.4.1 (X11/20050929) X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: Yet another limp home story References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-OriginalArrivalTime: 02 Jan 2007 21:17:38.0083 (UTC) FILETIME=[6DE0EF30:01C72EB3] Authentication-Results: sj-dkim-6; header.From=echristley@nc.rr.com; dkim=neutral James Maher wrote: > Ernest, > I have been considering several ways to build the tank from alum sheet. > I think that I have settled on the following design: > A one piece sheet that starts at the top front and goes down from > there to the front bottom, > then back along the frame, then up towards the vert fin, then back to > the top front with a flange to weld the sheet at the top front. > This will allow the insertion of flanged baffles just as in the F.G. > tank that can be welded in and then flanged end caps can be welded > in to seal the tank on the sides. > This method would have one weld along the top front and then around > each side plate. You'll leave a lot of fuel capacity in the sides, unless you complicate the design to add a large flange to the top corners that will fit around the curve. > Of coarse there will also be a sump in the bottom of the tank just as > I have in the F.G. tank. I'm hoping the .040 5052 will stretch enough to make a sufficient sump, but I'll have to test it first. The question I have is how to route a drain line to be able to drain the tank for preflight? Everything I've been able to picture means either crawling around under the plane before each flight, or having a drip prone drain filling the INSIDE of the airplane with gas fumes. Neither picture is pretty. How did you handle it? > > I'm not sure how you would be able to include the baffles with your > method unless you were not going to attach them to the top, but you > have probably already figured it out. Rivet the baffles in the bottom, front and back before welding the top/side flange. Weld over them afteward. The top/sides piece will be a flat sheet with two large curves. It should be a simple matter to start from the center and rivet it down. Just like closing up a wing. -- ,|"|"|, Ernest Christley | ----===<{{(oQo)}}>===---- Dyke Delta Builder | o| d |o http://ernest.isa-geek.org |