US Patent 8915713 Offset counterbore for airfoil cooling hole

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Is a

Patent

Patent attributes

Patent Jurisdiction

United States Patent and Trademark Office

Patent Number

8915713

Patent Inventor Names

Bradley Taylor Boyer0

Date of Patent

December 23, 2014

Patent Application Number

13245990

Date Filed

September 27, 2011

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

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US Patent 12006837 Ceramic matrix composite article and method of making the same

Patent Primary Examiner

‌

Igor Kershteyn

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