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US Patent 8915713 Offset counterbore for airfoil cooling hole

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
September 27, 2011
Date of Patent
December 23, 2014
Patent Application Number
13245990
Patent Citations Received
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US Patent 12091980 Spring biased shroud retention system for gas turbine engine
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US Patent 11965429 Turbomachine component with film-cooling hole with hood extending from wall outer surface
0
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US Patent 12006837 Ceramic matrix composite article and method of making the same
0
Patent Inventor Names
Bradley Taylor Boyer
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
8915713
Patent Primary Examiner
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Igor Kershteyn

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