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US Patent 8375726 Combustor assembly in a gas turbine engine

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
April 28, 2009
Date of Patent
February 19, 2013
Patent Application Number
12431302
Patent Citations Received
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US Patent 11994293 Impingement cooling apparatus support structure and method of manufacture
3
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US Patent 11767766 Turbomachine airfoil having impingement cooling passages
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US Patent 11994292 Impingement cooling apparatus for turbomachine
4
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
8375726
Patent Primary Examiner
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Ted Kim

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