Return-Path: Received: from seraph2.grc.nasa.gov ([128.156.10.11] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2892796 for flyrotary@lancaironline.net; Tue, 16 Dec 2003 06:24:16 -0500 Received: from lombok-fi.grc.nasa.gov (lombok-fi.grc.nasa.gov [139.88.112.33]) by seraph2.grc.nasa.gov (Postfix) with ESMTP id 1607F68A85 for ; Tue, 16 Dec 2003 06:24:16 -0500 (EST) Received: from apataki-fi.grc.nasa.gov (apataki-fi.grc.nasa.gov [139.88.112.35]) by lombok-fi.grc.nasa.gov (NASA GRC TCPD 8.12.10/8.12.10) with ESMTP id hBGBOFQx020662 for ; Tue, 16 Dec 2003 06:24:15 -0500 (EST) Received: from GESS20.grc.nasa.gov (gess20.grc.nasa.gov [139.88.63.20]) by apataki-fi.grc.nasa.gov (8.12.10 GRC/8.12.10) with ESMTP id hBGBOFid015059 for ; Tue, 16 Dec 2003 06:24:15 -0500 (EST) Message-Id: <5.1.0.14.2.20031216061319.03668fa0@pop.grc.nasa.gov> X-Sender: scberki@pop.grc.nasa.gov X-Mailer: QUALCOMM Windows Eudora Version 5.1 Date: Tue, 16 Dec 2003 06:24:15 -0500 To: "Rotary motors in aircraft" From: Joseph Berki Subject: Fuel system Mime-Version: 1.0 Content-Type: text/plain; charset="us-ascii"; format=flowed Thanks for the response on fuel system ideas. Rusty explained the secondary rail and I hope I got this right. Fuel is delivered at pressure to primary injector rail then to secondary rail then to regulator which feeds the return line back to the tank. My thinking was that i intended to connect both strake tanks together with a tunnel and a sump in the center where fuel would be pumped to the rail system. Even though the tanks are connected I was not sure how quickly they would level if fuel was returned to only one tank. I was thinking of splitting the rail system into two and returning to both tanks ie forward rotor to port tank and rear rotor to starboard tank. If the fuel could level on all conditions then the fuel could be returned to one tank. To implement this you would need two primary rails two secondary rails and two regulators. I may not need to split the rail system. Joe Berki Limo EZ