Return-Path: Received: from fep02-mail.bloor.is.net.cable.rogers.com ([66.185.86.72] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2989649 for flyrotary@lancaironline.net; Thu, 12 Feb 2004 18:57:23 -0500 Received: from CR754193A ([24.43.221.42]) by fep02-mail.bloor.is.net.cable.rogers.com (InterMail vM.5.01.05.12 201-253-122-126-112-20020820) with ESMTP id <20040212235712.ECAL181170.fep02-mail.bloor.is.net.cable.rogers.com@CR754193A> for ; Thu, 12 Feb 2004 18:57:12 -0500 From: "Neil Kruiswyk" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] EFI Fuel Pressure Date: Thu, 12 Feb 2004 18:57:47 -0500 Message-ID: <000601c3f1c4$03e88540$6402a8c0@CR754193A> MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.2616 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 X-Authentication-Info: Submitted using SMTP AUTH LOGIN at fep02-mail.bloor.is.net.cable.rogers.com from [24.43.221.42] using ID at Thu, 12 Feb 2004 18:57:12 -0500 Scott, You're only dealing with a column of fuel 40" high and not the weight of all 5 gallons. Assuming the return line is 3/8th inch ID (which would be on the big side), 40 inches works out to a grand total of 4.4 cubic inches of fuel, or, a grand total of .11 lbs/sq in. (Did I remember my grade 11 math correctly?) Neil -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Scott Stout Sent: February 12, 2004 9:41 AM To: Rotary motors in aircraft Subject: [FlyRotary] EFI Fuel Pressure In a NA 13b setup, using the stock fuel pressure regulator what is the pressure on the fuel rail? Is this the ideal pressure? Driving this question is I have to have to get fuel return fittings welded to my tanks, well the highest point on the tank is not in the easiest of spots to plumb to, thus I would like to return to a point about half way down the tank. So, not only does the fuel have to be pumped up 40" or so it also has to overcome 5gal or so of fuel weight above the return fitting. External to the rotary lists, some of those who I have floated the idea with have said the engine will run rich as the fuel rail pressure will increase. However, it doesn't seem to make sense to me as the pressure in the fuel rail will probably be higher, much higher, than the pressure needed to overcome the push through the return fuel line. What are your thoughts? Thank You. -Scott http://home.att.net/~the_stouts_zenith_801/ >> Homepage: http://www.flyrotary.com/ >> Archive: http://lancaironline.net/lists/flyrotary/List.html