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US Patent 7874138 Segmented annular combustor

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
September 11, 2008
Date of Patent
January 25, 2011
Patent Application Number
12208513
Patent Citations Received
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US Patent 11994293 Impingement cooling apparatus support structure and method of manufacture
0
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US Patent 11767766 Turbomachine airfoil having impingement cooling passages
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US Patent 11773739 Curved seal for adjacent gas turbine components
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US Patent 11994292 Impingement cooling apparatus for turbomachine
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
7874138
Patent Primary Examiner
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William H Rodríguez

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