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US Patent 10520193 Cooling patch for hot gas path components
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Patent
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Date Filed
October 28, 2015
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Date of Patent
December 31, 2019
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Patent Application Number
14924742
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Patent Citations Received
US Patent 11460191 Cooling insert for a turbomachine
US Patent 11371702 Impingement panel for a turbomachine
US Patent 11859818 Systems and methods for variable microchannel combustor liner cooling
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US Patent 11994292 Impingement cooling apparatus for turbomachine
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US Patent 11994293 Impingement cooling apparatus support structure and method of manufacture
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US Patent 11255545 Integrated combustion nozzle having a unified head end
US Patent 11767766 Turbomachine airfoil having impingement cooling passages
Patent Inventor Names
Jonathan Dwight Berry
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
10520193
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Patent Primary Examiner
Gerald L Sung
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