Airfoil for a turbofan engine

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12258875
APP PUB NO 20240263565A1
SERIAL NO

18618081

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Abstract

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An airfoil is provided defining a spanwise direction, a chordwise direction, a root end, a tip end, a leading edge end, and a trailing edge end. The airfoil includes: a leading edge extending from the leading edge end; a body extending along the spanwise direction between the root end and the tip end, the body including a plurality of cavity walls defining a plurality of cavities, each of the plurality of cavities having an inlet located at the leading edge; and a porous face sheet positioned on at least one inlet of the plurality of cavities.

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Patent Owner(s)

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

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Ramakrishnan, Kishore Rexford, US 85 367
Wood, Trevor Howard Clifton Park, US 62 435

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