Method and system for limiting power of an engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10823113
APP PUB NO 20190055901A1
SERIAL NO

15681531

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Abstract

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Systems and methods for limiting power of a gas turbine engine for an aircraft are described herein. A blade angle of a propeller blade of the engine and a commanded power for the engine are obtained. A thrust transition direction is determined. The commanded power is compared to a selected threshold based on the blade angle and the thrust transition direction. Power to the engine is limited when the commanded power exceeds the selected threshold.

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Patent Owner(s)

Patent OwnerAddress
PRATT & WHITNEY CANADA CORP1000 MARIE VICTORIN BLVD LONGUEUIL QU J4G 1A1

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Conciatori, Michael Saint-Leonard, CA 6 15
Des, Roches-Dionne Nicolas Montreal, CA 8 40
Lamarre, Sylvain Boucherville, CA 36 249
Lopez, Simon Montreal, CA 7 39

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