Invention Grant
- Patent Title: Gas turbine engine component with platform cooling circuit
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Application No.: US14665182Application Date: 2015-03-23
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Publication No.: US10041374B2Publication Date: 2018-08-07
- Inventor: Brandon W. Spangler , Ky H. Vu , Gina Cavallo
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D25/12
- IPC: F01D25/12 ; F01D25/14 ; F01D25/24 ; F01D5/18 ; F01D9/02 ; F01D5/08 ; F01D5/14
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.
Public/Granted literature
- US20150285097A1 GAS TURBINE ENGINE COMPONENT WITH PLATFORM COOLING CIRCUIT Public/Granted day:2015-10-08
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