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:
Aug. 09, 2022

Filed:

Aug. 20, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Jasraj Chahal, Lasalle, CA;

Brant Duke, Lasalle, CA;

Carmine Lisio, Laval, CA;

Jim R. Jarvo, Saint Bruno, CA;

Giancarlo Zingaro, Pointe-Claire, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/58 (2006.01); B64C 11/30 (2006.01); B64D 27/10 (2006.01); B64D 31/00 (2006.01); F02C 9/28 (2006.01);
U.S. Cl.
CPC ...
F02C 9/58 (2013.01); B64C 11/305 (2013.01); B64D 27/10 (2013.01); B64D 31/00 (2013.01); F02C 9/28 (2013.01); F05D 2220/323 (2013.01); F05D 2220/325 (2013.01); F05D 2270/02 (2013.01); F05D 2270/20 (2013.01); F05D 2270/52 (2013.01);
Abstract

An electronic controller for an engine and a propeller, a control system and related methods are described herein. The control system comprises the controller having a first channel and a second channel independent from and redundant to the first channel. Each channel comprises a control processor configured to receive first engine and propeller parameters and to output, based on the first engine and propeller parameters, at least one engine control command and at least one propeller control command. Each channel also comprises a protection processor configured to receive second engine and propeller parameters and to output, based on the second engine and propeller parameters, at least one engine protection command and at least one propeller protection command. The control system comprises sensors for measuring the parameters of the engine and/or the propeller and effectors configured to control the engine and the propeller.


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