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US Patent 8647053 Cooling arrangement for a turbine component
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Is a
Patent
Date Filed
August 9, 2010
Date of Patent
February 11, 2014
Patent Application Number
12852688
Patent Citations Received
US Patent 11994293 Impingement cooling apparatus support structure and method of manufacture
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US Patent 11767766 Turbomachine airfoil having impingement cooling passages
US Patent 11885236 Airfoil tip rail and method of cooling
0
US Patent 11994292 Impingement cooling apparatus for turbomachine
0
Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
8647053
Patent Primary Examiner
Dwayne J White
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