Method and apparatus for controlling a compressor of a gas turbine engine

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United States of America Patent

PATENT NO 9797314
APP PUB NO 20150354464A1
SERIAL NO

14708716

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Abstract

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A method of operating a gas turbine engine compressor. The method includes: determining an operating point of the compressor, and modulating mass flow of environmental control system input air to maintain the operating point of the gas turbine engine compressor within predetermined limits.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE PLCLONDON SW1E 6AT

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Hillel, Malcolm Derby, GB 3 49
Moes, Thierry Derby, GB 3 105
Stieger, Rory Douglas Derby, GB 6 145

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