Return-Path: Received: from [129.116.87.170] (HELO MAIL01.austin.utexas.edu) by logan.com (CommuniGate Pro SMTP 4.3c1) with ESMTP id 728818 for flyrotary@lancaironline.net; Mon, 14 Feb 2005 16:41:43 -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: multipart/alternative; boundary="----_=_NextPart_001_01C512DD.DE233194" Subject: Fuel System Design - Jet Pump Date: Mon, 14 Feb 2005 15:40:57 -0600 Message-ID: <87DBA06C9A5CB84B80439BA09D86E69EC07F53@MAIL01.austin.utexas.edu> X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: Fuel System Design - Jet Pump Thread-Index: AcUS3d3uQ6asJNafQ5OiZT9KeHH8yw== From: "Mark R Steitle" To: "Rotary motors in aircraft" This is a multi-part message in MIME format. ------_=_NextPart_001_01C512DD.DE233194 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Ed,=20 Thanks for that excellent article on fuel system design. In reading through it, on page 5, I came to the description of the jet pump and had a thought (that alone is a scary thing). I was thinking that this could be used to eliminate the need for the facet pump in a design such as Tracy's which would simplify things even more than Tracy's system already does. Of course, as in Tracy's design, this would eliminate the need for the fuel selector valve too. As it was designed to do, the Jet Pump would be powered by excess fuel from the main fuel pump located in the left tank. Fuel from the other (right) wing tank would be drawn into the main (left) tank by the Jet Pump. To prevent overfilling the main tank, transfer could be controlled by a small solenoid valve. Since you would be drawing fuel from the right tank pretty much all the time, it may be possible to route the return fuel to the right tank. I guess this idea could also be used with a sump tank. Time for a sanity check. =20 =20 Mark S. =20 =20 ------_=_NextPart_001_01C512DD.DE233194 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Ed,

Thanks for that excellent article on fuel system design. In reading through it, on page 5, I came to the = description of the jet pump and had a thought (that alone is a scary thing). I = was thinking that this could be used to eliminate the need for the facet = pump in a design such as Tracy’s which would simplify things even more than = Tracy’s system already does. Of course, as in Tracy’s design, this would = eliminate the need for the fuel selector valve too. As it was designed to = do, the Jet Pump would be powered by excess fuel from the main fuel pump located = in the left tank. Fuel from the other (right) wing tank would be drawn = into the main (left) tank by the Jet Pump. To prevent overfilling the main = tank, transfer could be controlled by a small solenoid valve. Since you = would be drawing fuel from the right tank pretty much all the time, it may be possible to route the return fuel to the right tank. I guess this = idea could also be used with a sump tank. Time for a sanity = check.

Mark S. =

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