Return-Path: Received: from [129.116.87.170] (HELO MAIL01.austin.utexas.edu) by logan.com (CommuniGate Pro SMTP 4.3c1) with ESMTP id 741853 for flyrotary@lancaironline.net; Wed, 16 Feb 2005 15:04:19 -0500 Received-SPF: none receiver=logan.com; client-ip=129.116.87.170; envelope-from=mark.steitle@austin.utexas.edu X-MimeOLE: Produced By Microsoft Exchange V6.5.7226.0 Content-class: urn:content-classes:message MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Subject: RE: [FlyRotary] Re: Fuel System Design - Jet Pump Date: Wed, 16 Feb 2005 14:03:34 -0600 Message-ID: <87DBA06C9A5CB84B80439BA09D86E69EC07F72@MAIL01.austin.utexas.edu> X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: [FlyRotary] Re: Fuel System Design - Jet Pump Thread-Index: AcUUYDd38j29EchiTo20+ik89dpGMQAAE38w From: "Mark R Steitle" To: "Rotary motors in aircraft" Ernest,=20 First, I think I'll defer all your questions concerning MAP and throttle positions to Tracy or Ed. I know that you can have WOT at low rpm that requires a different amount of fuel as WOT at high rpm. Engine loads has a lot to do with things, hence the MAP port to the EC-2. The EC-2 instructions clearly state not to attempt adjusting a/f ratios without a prop, or some means to load the engine. To do so is a waste of time... makes sense. =20 One thing I did learn from the referenced efi article is that auto manufacturers went to returnless efi systems for emissions reasons (hot fuel splashing into a partially full fuel tank causes vapors that can end up as smog). The returnless systems run higher fuel pressures (65 psi) to keep the fuel from boiling in the fuel rails and lines. Personally, 38psi is too high for my personal comfort, but that's the nature of fuel injection. The homebuilders seem to like the returnless systems for the simplicity of the design and to get around having to purchase a $500 fuel selector valve. My kit came with the Andair dual selector valve, so that decision was already made for me. Tracy seems to have a good solution to that problem. I would probably copy his design if I didn't already have a selector valve. =20 Mark S. I'm still wondering how important that pressure is. First, didn't we learn earlier that the flow doesn't vary linearly with=20 the pressure differential; that it take a lot more pressure to get a=20 significant difference in flow? This would tend to limit the effect of=20 MAP changes. Referencing somewhere other than MAP will make a=20 difference, just not a whole lot. Would this be a reason that all of the returnless systems are running at higher pressures? Say the MAP varies=20 15", there's less percentage difference between 30"->45" than there is=20 45"->60". That keeps you in the ballpark. The ECM takes up the rest of=20 the slack. Then there is the fact that Ed has flown at least a couple hours with a=20 system that was not referenced to MAP. The original problems were tuned out. Leon, I'm not claiming to know anything. Shoot, I'm still a month away=20 from STARTING my first engine rebuild. But it just seems to me that with an atmospheric controlled regulator, all that you would need would be a=20 throttle position sensor to know how much fuel to dump in the intake.=20 The regulator will relax the pressure as you climb to lean the mixture.=20 And except for barometric difference, the MAP will always be tied to the throttle position. Now all you need is a fuel map that says how much=20 fuel to use at each throttle position. I'm sure I'm missing something,=20 and I'm sure it's not the sort of thing you find in textbooks. >> Homepage: http://www.flyrotary.com/ >> Archive: http://lancaironline.net/lists/flyrotary/List.html