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:
Jul. 04, 2023

Filed:

Jun. 05, 2020
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Sarah Theriault, Boucherville, CA;

Poi Loon Tang, Montréal, CA;

Sean McCarthy, Beaconsfield, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); B64F 5/60 (2017.01); B64C 27/06 (2006.01); B64D 37/00 (2006.01); G01P 3/00 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64C 27/06 (2013.01); B64D 37/00 (2013.01); B64F 5/60 (2017.01); G01P 3/00 (2013.01);
Abstract

The present disclosure provides methods and systems for fault detection for a speed sensing system of a multi-engine rotorcraft. A shaft speed for a first engine and a rotor speed for at least one rotor of the multi-engine rotorcraft are obtained. The shaft speed is compared to the rotor speed. When the shaft speed is greater than the rotor speed, a first fault in the speed sensing system is detected and a first speed sensing system fault signal is issued. When the shaft speed is less than the rotor speed, a determination is made regarding whether the first engine is coupled the at least one rotor based on a fuel flow to the first engine. A second fault in the speed sensing system is detected and a second speed sensing system fault signal is issued responsive to determining that the first engine is coupled to the at least one rotor.


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