Return-Path: Received: from atlantic.mail.pas.earthlink.net ([207.217.120.179] verified) by logan.com (CommuniGate Pro SMTP 4.2b3) with ESMTP id 90107 for flyrotary@lancaironline.net; Tue, 25 May 2004 22:49:48 -0400 Received: from ip216-26-75-92.dsl.du.teleport.com ([216.26.75.92] helo=michaelm1.teleport.com) by atlantic.mail.pas.earthlink.net with esmtp (Exim 3.33 #1) id 1BSoUF-0001UN-00 for flyrotary@lancaironline.net; Tue, 25 May 2004 19:49:47 -0700 Message-Id: <5.2.0.9.0.20040525194611.027a4b90@mail.teleport.com> X-Sender: jmpcrftr@mail.teleport.com X-Mailer: QUALCOMM Windows Eudora Version 5.2.0.9 Date: Tue, 25 May 2004 19:49:38 -0700 To: "Rotary motors in aircraft" From: Michael McGee Subject: Re: [FlyRotary] Re: Fuel Pump Design In-Reply-To: Mime-Version: 1.0 Content-Type: text/plain; charset="us-ascii"; format=flowed At 19:17 2004-05-25, you wrote: >Mark Steitle wrote: > > > > > > >Bill, >Yes, the regulator is mounted on the firewall and is located between the >pumps/filters and fuel rail. Also, there is a fuel return line off the >regulator. > < < < < > >Wouldn't it make more sense to make the regulator the last thing in the >circuit? This seems to be typical on just about all automotive EFI >installations, and millions of installations can't be wrong. I think the >logic here is that regulator failures aren't sudden, and when they fail >they bypass more fuel than they should (ie, lowering pressure). In this >setup there is no way that you can get an airlock, at least I don't see >how one would be possible. Proven systems all seem to have the fuel pumps >as close to the tank as possible (inside the tank on most auto >installations), then the filter, followed by a direct line to the fuel >rail and injectors, then to the regulator, then the return. On the >Eagle540 we put the fuel filters between the tanks and pumps, and they are >located just aft of the main spar, just inches away from the tanks (the >filter outlet screws directly into the pump inlet)... out of the pumps to >the selector, on through the flow transducers, then to the rails. The >regulator is at the end of the circuit and returns through the (horribly >expensive) fuel selector as well to direct the return fuel back to the >tank from which we're pumping. Everything has worked extremely well in >ground runs, and we are weeks away from first flight. Just my 2c. > > Yes, and heat soak of the fuel is eliminated with the regulator on the out going end of the fuel rail so as to not make a dead end. After a hot shutdown and heat soak of the fuel rail, the system can be cooled down by just turning on a boost pump and letting the fuel circulate for a few seconds. Mike McGee, RV-4 N996RV, O320-E2G, Hillsboro, OR 13B in gestation mode, RD-1C, EC-2