Gas turbine engine component with upstream-directed cooling film holes

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United States of America Patent

PATENT NO 9958160
SERIAL NO

14765222

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Abstract

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A component within a gas turbine engine includes a surface with one or more upstream-directed cooling film holes therethrough.

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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
Dierberger, James A Hebron, US 29 779

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