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:
Jan. 25, 2022

Filed:

Mar. 08, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

David Waddleton, Candiac, CA;

Benjamin Renaud, Montreal, CA;

Sebastien Bergeron, Chambly, CA;

Etienne Plamondon, Candiac, CA;

Jean-Gabriel Gauvreau, Varennes, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/30 (2006.01); F02C 9/36 (2006.01); F04D 27/00 (2006.01); F04D 29/58 (2006.01); F04D 29/40 (2006.01);
U.S. Cl.
CPC ...
F02C 9/30 (2013.01); F02C 9/36 (2013.01); F04D 27/006 (2013.01); F04D 29/406 (2013.01); F04D 29/5873 (2013.01); F05D 2220/323 (2013.01); F05D 2260/211 (2013.01);
Abstract

A liquid fuel system for an aircraft engine includes a first fuel supply conduit hydraulically connected to a fuel source, a second fuel supply conduit hydraulically connected to the engine, a fuel return conduit hydraulically connected to the second fuel supply conduit, and a fuel pump. The fuel pump has a main inlet hydraulically connected to the first fuel supply conduit, an outlet hydraulically connected to the second fuel supply conduit, and an intermediate inlet hydraulically connected to the fuel return conduit. The intermediate inlet is located between the main inlet and the outlet and in use has a pressure between the main inlet pressure and the outlet pressure. A method of supplying a liquid fuel to an aircraft engine is also described.


Find Patent Forward Citations

Loading…