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US Patent 9255490 Gas turbine and operating method thereof
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Patent
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Date Filed
September 24, 2009
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Date of Patent
February 9, 2016
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Patent Application Number
13056064
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Patent Citations Received
US Patent 11994293 Impingement cooling apparatus support structure and method of manufacture
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US Patent 11767766 Turbomachine airfoil having impingement cooling passages
US Patent 11913341 Clearance control system for gas turbine
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US Patent 11994292 Impingement cooling apparatus for turbomachine
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Patent Inventor Names
Hiroki Takahashi
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Kazumasa Takata
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Masaki Satoh
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Masato Hayashi
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Norio Oogai
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Satoshi Mizukami
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Souji Hasegawa
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Tatsuo Ishiguro
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Yoshiaki Nishimura
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Yuya Fukunaga
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•••
Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
9255490
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Patent Primary Examiner
Steven Sutherland
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