US Patent 9279330 Gas turbine engine component with converging/diverging cooling passage
Patent 9279330 was granted and assigned to United Technologies on March, 2016 by the United States Patent and Trademark Office.
Is a
Current Assignee
Date Filed
July 9, 2012
0
Date of Patent
March 8, 2016
0
Patent Application Number
13544210
0
Patent Inventor Names
Glenn Levasseur
0
JinQuan Xu
0
Patent Jurisdiction
Patent Number
Patent Primary Examiner
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