Gas turbine engine component with compound cusp cooling configuration

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United States of America Patent

PATENT NO 9869186
SERIAL NO

15243220

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Abstract

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A component for a gas turbine engine including a gas path wall having a first surface and a second surface. A cooling hole extends through the gas path wall from an inlet in the first surface through a transition to an outlet in the second surface. Cusps are formed on the transition.

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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
Xu, JinQuan East Greenwich, US 121 1312

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