Compressor system

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United States of America Patent

PATENT NO 9890704
SERIAL NO

14785628

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Importance

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Abstract

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In a gas turbine engine, the booster compressor is driven by both the low pressure or fan shaft and high pressure shaft through a differential gear arrangement. The rotational speed of the booster compressor is intermediate between the speed of the fan and the speed of the high pressure compressor.

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Patent Owner(s)

Patent OwnerAddress
DERWENT AVIATION CONSULTING LTDBURTON ON TRENT STAFFORDSHIRE DE14 1SN

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Sellick, Robert J Gloucestershire, GB 1 164
Speak, Trevor H Gloucestershire, GB 5 356

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