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US Patent 8307657 Combustor liner cooling system
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Patent
Date Filed
March 10, 2009
Date of Patent
November 13, 2012
Patent Application Number
12401530
Patent Citations Received
US Patent 12092330 Gas turbine combuster
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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 12085283 Combustor for a gas turbine engine
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US Patent 11767766 Turbomachine airfoil having impingement cooling passages
US Patent 11774098 Combustor for a gas turbine engine
US Patent 11859818 Systems and methods for variable microchannel combustor liner cooling
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US Patent 11885495 Combustor for a gas turbine engine including a liner having a looped feature
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US Patent 11920796 Combustor for a gas turbine engine
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US Patent 11959643 Combustor for a gas turbine engine
0
Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
8307657
Patent Primary Examiner
Ehud Halberstam
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