Return-Path: Received: from smtp4.mindspring.com ([207.69.200.64]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Fri, 3 Sep 1999 16:43:51 -0400 Received: from u2kmz (pool-209-138-57-62.bltm.grid.net [209.138.57.62]) by smtp4.mindspring.com (8.8.5/8.8.5) with SMTP id QAA02721 for ; Fri, 3 Sep 1999 16:47:31 -0400 (EDT) From: marklisalally@mindspring.com Message-ID: <000701bef64e$0b7a50c0$3e398ad1@u2kmz> To: "lancair mail" Subject: flow though venting Date: Fri, 3 Sep 1999 16:51:05 -0400 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Thanks to every one for responding to my post concerning closing ES wings, your comments were very helpful at easing my mind. I now have a new problem! constructing a flow through venting system for the fuel tanks. The reason for this is that I plan on using a delta hawk diesel V8 engine and they recommend a positive flow through venting system. I guess this is true for any jet or diesel fueled plane. At first I was going to run a second vent line next to the first one and simply exit it on the trailing edge of the wing tip, until my brain cloud cleared out and I realized what a stupid idea that was, although it would be a convenient way to dump fuel. My second thought is to run the second exit air vent lines toward the fuselage ,where they would be combined and then run the line to a low pressure point at the top of the vertical stabilizer. Dose this sound like a good solution? What have the Lancair IV installing the walter turbines been doing? I plan on sealing my fuel tanks this weekend, so and quick responses to these questions would be Very Very much appreciated. Three weeks till closing wings MARK LALLY >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html