Gas turbine engine with axial movable fan variable area nozzle

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United States of America Patent

PATENT NO 9701415
SERIAL NO

13314365

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Abstract

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A nacelle assembly for a high-bypass gas turbine engine includes a fan variable area nozzle axially movable relative the fan nacelle to define an auxiliary port to vary a fan nozzle exit area and adjust a pressure ratio of the fan bypass airflow during engine operation.

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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
Kohlenberg, Gregory A Kensington, US 24 412
Zamora, Sean P Coventry, US 27 417

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