X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [129.116.87.143] (HELO MAIL01.austin.utexas.edu) by logan.com (CommuniGate Pro SMTP 4.3.4) with ESMTP id 1002807 for flyrotary@lancaironline.net; Wed, 15 Jun 2005 10:13:57 -0400 Received-SPF: none receiver=logan.com; client-ip=129.116.87.143; 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: EFI Bleeder Circuit (Was Engine Not Starting) Date: Wed, 15 Jun 2005 09:13:12 -0500 Message-ID: <87DBA06C9A5CB84B80439BA09D86E69E016C1A27@MAIL01.austin.utexas.edu> X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: EFI Bleeder Circuit (Was Engine Not Starting) Thread-Index: AcVxsPZXt0Rs+xFYTACadmvXgtoKWAAAX3DA From: "Mark R Steitle" To: "Rotary motors in aircraft" Jofar, The real purpose of the bleed circuit is to allow the pump to reprime itself. Once that happens, the pump builds up pressure again, and forces all the remaining air out through the pressure regulator. With a 5-gal tank sitting on the floor, my system (running one pump) can reprime itself in about 10 seconds. Yes, under the right circumstances, that could be the longest 10 seconds of my life. This should only happen if you run a tank dry. But if that happens, the procedure will be to switch to the other tank (should have fuel), then turn on the boost pump. That should reduce the recovery time to something less than 10 seconds. Mark -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of jesse farr Sent: Wednesday, June 15, 2005 8:47 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Engine Not Starting I don't know nothing (actually pretty much anything) about any of this but=20 that has never stopped me from having and voicing an opinion; so, if=20 injectors only fire small percentage of time and fuel & compressed air flow=20 not sufficient at times to clear out in time to get started while flying ac,=20 bleed return definitly sounds like good idea. But, if sufficiently far away=20 from injectors, then even though now have flow established to the bleed=20 point, you will still have slow go to purge remaining compressed air, vapor=20 and allow fuel to actually flow from there to injectors and inject. It may=20 just take a few seconds longer but that is still a tight a-- time of flying,=20 starting, praying, cursing own stupidity, etc.. Could I suggest might be better to put bleed point at end of fuel rail so as to pass vapor all the=20 way more quickly ? After all, small orfice and line return to tank shouldn't=20 create that much more of a problem. Is there some other problem there that I=20 simply do not know enough to understand ? jofarr, soddy tn