US Patent 10125625 Gas turbine engine component with performance feature
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Patent abstract
A gas turbine engine component (50, 100, 150, 160, 174, 206, 236), including: a surface (54) subject to loss caused by a wear instrument during operation of the component in a gas turbine engine and a performance feature (80, 82, 102, 152, 162, 172, 200, 230) associated with the surface. The surface and the performance feature interact in a manner that changes with the loss such that a change in performance of the gas turbine engine resulting from the loss is mitigated.
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Patent Inventor Names
Ahmed Kamel0
Daniel J. Ryan0
David G. Maire0
Dhafer Jouini0
Gerald J. Bruck0
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Patent Citations Received
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Patent Jurisdiction
Patent Number
101256250
Date of Patent
November 13, 2018
0Patent Application Number
148161560
Date Filed
August 3, 2015
0Patent Citations Received
Patent Primary Examiner
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Patent citations received
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US Patent 10125625 Gas turbine engine component with performance feature
Infobox
Is a
Patent jurisdiction
Patent number
10125625
Date of patent
November 13, 2018
Patent application number
14816156
Date Filed
August 3, 2015
Patent primary examiner
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