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:
Sep. 07, 2021

Filed:

Jun. 02, 2020
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Sebastien Bergeron, St-Bruno-De-Montarville, CA;

Etienne Plamondon, Candiac, CA;

Jean Thomassin, Sainte-Julie, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 53/02 (2006.01); F02B 53/10 (2006.01); F02B 55/08 (2006.01); F02D 41/40 (2006.01); F02M 61/10 (2006.01); F02M 61/18 (2006.01); F02M 63/00 (2006.01); F02D 41/38 (2006.01);
U.S. Cl.
CPC ...
F02B 53/10 (2013.01); F02B 53/02 (2013.01); F02B 55/08 (2013.01); F02D 41/403 (2013.01); F02M 61/10 (2013.01); F02M 61/18 (2013.01); F02M 63/0028 (2013.01); F02D 2041/389 (2013.01);
Abstract

A fuel injection system for an aircraft engine has: a first fuel injector having a first actuation inlet, a first fuel inlet connected to a fuel source, and a first fuel outlet connected to the at least one combustion chamber, the first fuel injector defining a first pressure ratio; a second fuel injector having a second actuation inlet, a second fuel inlet connected to the fuel source, and a second fuel outlet connected to the at least one combustion chamber, the second fuel injector defining a second pressure ratio; and an actuation fluid system having a circuit connected to the first actuation inlet and to the second actuation inlet, the first outlet pressure different than the second outlet pressure by having one or both of the first pressure ratio different than the second pressure ratio and a first actuation pressure different than a second actuation pressure.


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