Chordal seal

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United States of America Patent

PATENT NO 9863259
SERIAL NO

14708939

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Abstract

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An airfoil for a gas turbine engine includes a first airfoil. A first chordal seal is located adjacent a first end of the airfoil. A second chordal seal is located adjacent a second end of the airfoil. The first chordal seal includes a first edge parallel to a first edge on the second chordal seal.

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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
Blake, Mosheshe Camara-khary Manchester, US 8 53
Boeke, Mark A Plainville, US 18 99
Rajchel, Kevin Vernon, US 3 33
Simms, Vincent E Bloomfield, US 3 22

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