Geared gas turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 10590854
SERIAL NO

15006474

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Abstract

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A turboshaft engine includes a high speed spool that connects a high pressure compressor with a high pressure turbine. A low speed spool connects a low pressure compressor with a low pressure turbine. A speed change mechanism includes an input that is in communication with the low spool and a fixed gear ratio. An output turboshaft is in communication with an output of the speed change mechanism.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Sheridan, William G Southington, US 273 5642

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