Propulsion system arrangement for turbofan gas turbine engine

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United States of America Patent

PATENT NO 11661906
SERIAL NO

17371672

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Abstract

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An integrated propulsion system according to an example of the present disclosure includes, among other things, a fan section, a gas turbine engine, a geared architecture, a nacelle assembly and a mounting assembly. The nacelle assembly includes a fan nacelle and an aft nacelle, the fan nacelle arranged at least partially about a fan and the engine, and the fan nacelle arranged at least partially about a core cowling to define a bypass flow path.

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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
Eckett, Christopher A West Hartford, US 9 32
Suciu, Gabriel L Glastonbury, US 580 8113

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