Gas turbine engine bifurcation located fan variable area nozzle

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United States of America Patent

PATENT NO 11391240
APP PUB NO 20210215120A1
SERIAL NO

17217048

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Abstract

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A turbofan gas turbine engine includes a core engine within a core nacelle, a fan nacelle at least partially surrounding the core nacelle to define a bypass flow path and a variable fan nozzle exit area for bypass flow, and a pylon variable area flow system which operates to effect the bypass flow. A method of operating a turbofan gas turbine engine is also disclosed.

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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
Baltas, Constantine Manchester, US 17 261

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