TURBINE ENGINE HAVING A THRUST REVERSER SYSTEM

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20240401546A1
SERIAL NO

18327629

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A turbine engine includes a fan, a nacelle, and a thrust reverser system. The fan includes a plurality of fan blades. Each fan blade of the plurality of fan blades is rotatable about a pitch axis. The nacelle circumferentially surrounds the fan. The thrust reverser system includes a transcowl that forms a portion of the nacelle. The thrust reverser system translates the transcowl axially forward to an opened position during a reverse thrust condition and pitches the fan blades about the pitch axis to generate a reverse thrust through the turbine engine.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC COMPANY1 NEUMANN WAY MAIL DROP F16 EVENDALE OH 45215-6301

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Hunter, Scott D Seattle, US 6 1

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