Gas turbine engine airfoil

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United States of America Patent

PATENT NO 9599064
SERIAL NO

14626392

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Abstract

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A gas turbine engine includes a fan section, a compressor section and a turbine section, one of which includes an airfoil. The airfoil includes pressure and suction sides extending in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a maximum chord length projection that is not in an axial view.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Ford, Barry M Middletown, US 28 220
Gallagher, Edward J West Hartford, US 73 536
Li, Linda S Middlefield, US 25 224
Liu, Ling Glastonbury, US 149 924
Monzon, Byron R Cromwell, US 37 284
Whitlow, Darryl Middletown, US 25 221

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