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US Patent 10352566 Gas turbine engine combustor liner panel
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Is a
Patent
Date Filed
April 14, 2014
Date of Patent
July 16, 2019
Patent Applicant
United Technologies
Patent Application Number
14896576
Patent Citations Received
US Patent 12018591 Ring segment assembly in gas turbine engine
0
US Patent 11624284 Impingement jet cooling structure with wavy channel
0
Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
10352566
Patent Primary Examiner
Gerald L Sung
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