US Patent 10041374 Gas turbine engine component with platform cooling circuit
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Patent abstract
A component according to an exemplary aspect of the present disclosure includes, among other things, a platform and a feed cavity that feeds a cooling fluid inside of the platform. The feed cavity includes a leg portion and a main body portion that extends from the leg portion inside of the platform. A cooling cavity is inside the platform and in fluid communication with the feed cavity.
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Patent Inventor Names
Brandon W. Spangler0
Gina Cavallo0
Ky H. Vu0
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Patent Number
100413740
Date of Patent
August 7, 2018
0Patent Application Number
146651820
Date Filed
March 23, 2015
0Patent Citations Received
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US Patent 10041374 Gas turbine engine component with platform cooling circuit
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10041374
Date of patent
August 7, 2018
Patent application number
14665182
Date Filed
March 23, 2015
Patent primary examiner
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