Turbo-compressor with geared turbofan

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United States of America Patent

PATENT NO 9879694
SERIAL NO

14612614

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Abstract

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A gas turbine engine includes a fan section. A turbo-compressor section is connected to the fan section through a speed change mechanism.

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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
Sheridan, William G Southington, US 276 6115

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