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:
Nov. 10, 2020

Filed:

May. 12, 2020
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Carmine Lisio, Laval, CA;

Michel Labrecque, St-Bruno, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/00 (2006.01); F02C 3/04 (2006.01); B64D 35/00 (2006.01); B64D 27/10 (2006.01); F02C 9/00 (2006.01); B64D 31/06 (2006.01); F02C 9/58 (2006.01);
U.S. Cl.
CPC ...
B64D 31/00 (2013.01); B64D 27/10 (2013.01); B64D 31/06 (2013.01); B64D 35/00 (2013.01); F02C 3/04 (2013.01); F02C 9/00 (2013.01); F02C 9/58 (2013.01); F05D 2220/323 (2013.01); F05D 2270/05 (2013.01); F05D 2270/114 (2013.01);
Abstract

The present disclosure provides a method and a system for controlling operation of an engine of an aircraft. The method comprises, at a controller of the engine, obtaining an actual engine output power for the engine, the actual engine output power based on a propeller rotation speed and a propeller blade pitch angle; converting the actual engine output power to a predicted thrust value; determining an actual engine power limit associated with a thrust limit of a propeller coupled to the engine from the predicted thrust value; and setting a maximum engine power limit of the engine using the actual engine power limit associated with the thrust limit of the propeller.


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