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:
Jun. 07, 2022

Filed:

May. 29, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Patrick Manoukian, Saint-Laurent, CA;

Philippe Beauchesne-Martel, Brossard, CA;

Olivier Bibor, Montreal, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 21/00 (2006.01); B64C 27/32 (2006.01); B64D 31/06 (2006.01); B64D 45/00 (2006.01); F01D 21/14 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); B64C 27/32 (2013.01); B64D 31/06 (2013.01); B64D 45/00 (2013.01); F01D 21/14 (2013.01);
Abstract

Systems and methods for operating an engine of a rotorcraft are described herein. An engine parameter indicative of torque of the engine is obtained. A decrease of the torque of the engine is detected. At least one rotorcraft parameter indicative of at least one command to control the rotorcraft is obtained and evaluated to determine whether one of an autorotation mode and a powered flight mode of the rotorcraft has been commanded. When the powered flight mode of the rotorcraft has been commanded and the decrease of the torque has been detected, a shaft shear of the engine is detected and a signal indicative of the shaft shear is transmitted. When the autorotation mode of the rotorcraft has been commanded and the decrease of the torque has been detected, detection of the shaft shear is disabled during operation in the autorotation mode.


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