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US Patent 10309255 Blade outer air seal cooling passage

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Patent abstractTimelineTable: Further ResourcesReferences
Is a
Patent
Patent
1

Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
1
Patent Number
103092551
Patent Inventor Names
Dmitriy A. Romanov1
Date of Patent
June 4, 2019
1
Patent Application Number
151040921
Date Filed
December 10, 2014
1
Patent Citations Received
‌
US Patent 10690055 Engine components with impingement cooling features
Patent Primary Examiner
‌
Umashankar Venkatesan
1
Patent abstract

A gas turbine engine component includes a structure including a first wall and a second wall that provide a cooling passage. The cooling passage extends a length from a first end to a second end. A cluster of impingement inlet holes is provided in the second wall at the first end. An outlet is provided at the second end.

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