The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 01, 2022

Filed:

Sep. 30, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Harris Shafique, Longueuil, CA;

David Waddleton, Candiac, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/22 (2006.01); F02C 9/36 (2006.01); B64D 37/10 (2006.01); F02C 7/236 (2006.01); F02C 7/224 (2006.01);
U.S. Cl.
CPC ...
F02C 7/236 (2013.01); B64D 37/10 (2013.01); F02C 7/224 (2013.01); F02C 9/36 (2013.01); Y02T 50/60 (2013.01);
Abstract

A method of pumping fuel in a fuel system of a composite aircraft having a gas turbine engine includes feeding un-heated fuel from a fuel tank to the gas turbine engine, by using an ejector pump to draw the fuel from the fuel tank and feeding the fuel through an engine fuel pump within a main fuel line upstream of the gas turbine engine. Fuel from the main fuel line is bled and directed to the ejector pump via a motive flow pump assembly, the motive flow pump assembly including a motive flow pump generating a motive flow for the ejector pump. The bleed fuel flow is then passed through a hydrophobic fuel screen located upstream of the motive flow pump.


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