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US Patent 10184343 System and method for turbine nozzle cooling

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
February 5, 2016
Date of Patent
January 22, 2019
Patent Application Number
15016498
Patent Citations Received
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US Patent 11702941 Airfoil with baffle having flange ring affixed to platform
0
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US Patent 11519281 Impingement insert for a gas turbine engine
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US Patent 11525401 Impingement baffle for gas turbine engine
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US Patent 10584596 Gas turbine engine components having internal cooling features
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10184343
Patent Primary Examiner
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David E Sosnowski

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