US Patent 10329924 Turbine airfoils with micro cooling features
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Patent abstract
A blade used in a gas turbine engine includes a pair of pedestals and an airfoil coupled between the pedestals. The airfoil includes cooling features to cool the airfoil.
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Patent Inventor Names
Brett J. Barker0
Jeffrey F. Rhodes0
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Official Website
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Patent Number
103299240
Date of Patent
June 25, 2019
0Patent Application Number
152147990
Date Filed
July 20, 2016
0Official Website
Patent Primary Examiner
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US Patent 10329924 Turbine airfoils with micro cooling features
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10329924
Date of patent
June 25, 2019
Patent application number
15214799
Date Filed
July 20, 2016
Patent primary examiner
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