Gas turbine engine system with synchronization features for gearbox operation

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 11067006
APP PUB NO 20200284201A1
SERIAL NO

16293030

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A gas turbine engine includes a first spool and a second spool. The first spool includes a compressor stage, a first turbine stage, and a first shaft configured to transmit rotational energy between the first turbine stage and the compressor stage. The second spool includes a fan, a second turbine stage, and a second shaft configured to transmit rotational energy between the second turbine stage and the fan.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE CORPORATION450 S MERIDIAN STREET INDIANAPOLIS IN 46225-1103

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Copeland, Andrew D Greenwood, US 19 170
Gebhard, John R Fishers, US 12 24
Kempers, Adam L Indianapolis, US 7 23

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