US Patent 10156150 Gas turbine engine stator vane platform cooling
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Patent abstract
An airfoil component for a gas turbine engine includes a platform joined to an airfoil. The platform includes a flow path surface that extends between spaced apart lateral surfaces. The airfoil extends from the flow path surface. A contoured surface adjoins the flow path surface and one of the lateral surfaces.
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Patent Inventor Names
Seth J. Thomen0
Wieslaw A. Chlus0
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Patent Applicant
Patent Jurisdiction
Patent Number
101561500
Date of Patent
December 18, 2018
0Patent Application Number
147692080
Date Filed
March 10, 2014
0Patent Citations Received
Patent Primary Examiner
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Patent Citations Received
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US Patent 10156150 Gas turbine engine stator vane platform cooling
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10156150
Date of patent
December 18, 2018
Patent application number
14769208
Date Filed
March 10, 2014
Patent primary examiner
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