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US Patent 10233775 Engine component for a gas turbine engine

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Contents

Is a
Patent
Patent

Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10233775
Date of Patent
March 19, 2019
Patent Application Number
14881188
Date Filed
October 13, 2015
Patent Citations Received
‌
US Patent 10989070 Shroud for gas turbine engine
‌
US Patent 11746661 Turbine blade and turbine including the same
‌
US Patent 11261794 Acoustic device and gas turbine
‌
US Patent 12006837 Ceramic matrix composite article and method of making the same
0
‌
US Patent 11352888 Turbine blade having gas film cooling structure with a composite irregular groove and a method of manufacturing the same
‌
US Patent 10823416 Purge cooling structure for combustor assembly
Patent Primary Examiner
‌
Igor Kershteyn
Patent abstract

An engine component for a gas turbine engine includes a film-cooled wall having a hot surface facing hot combustion gas and a cooling surface facing a cooling fluid flow. A film hole in the wall has an inlet, an outlet, and a passage connecting the inlet and outlet that defines an inflection point.

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