GAS TURBINE ENGINE COMPONENT

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20200024986A1
SERIAL NO

16273345

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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There is disclosed a component arranged to extend across a bypass duct (22) of a gas turbine engine (10), comprising: an outlet guide vane (24); and a structural support (26) arranged to structurally support a radially inner component of the gas turbine engine (10). The outlet guide vane (24) and the structural support (26) are contiguous at a merged portion (32) which is at a radially outer region of the component.

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Patent Owner(s)

  • ROLLS ROYCE PLC

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
BARBAROSSA, Fernando London, GB 4 11
DI, MARE Luca London, GB 8 13
RIFE, Max E London, GB 3 11

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