Gas turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 10989112
APP PUB NO 20200049066A1
SERIAL NO

16411341

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE PLCLONDON

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Dunning, Pascal Derby, GB 31 70
Townes, Roderick M Derby, GB 47 346
Whittle, Michael J Derby, GB 88 314

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