Thermal management system for gas turbine engine

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United States of America Patent

PATENT NO 9863318
SERIAL NO

14533611

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Abstract

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A method of thermal management for a gas turbine engine comprising selectively positioning a valve to communicate a bypass flow into either an Environmental Control System (ECS) pre-cooler or an Air Oil Cooler (AOC) “peaker” through a common inlet.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Murphy, Michael Joseph Windsor, US 22 316

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