Invention Grant
- Patent Title: Gas turbine engine component cooling circuit with respirating pedestal
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Application No.: US15112497Application Date: 2015-01-26
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Publication No.: US10370981B2Publication Date: 2019-08-06
- Inventor: Thomas N. Slavens , Brooks E. Snyder
- 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.
- International Application: PCT/US2015/012805 WO 20150126
- International Announcement: WO2015/123006 WO 20150820
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D25/12 ; F01D9/02 ; F23R3/00 ; F01D11/08 ; F01D25/30
Abstract:
A component according to an exemplary aspect of the present disclosure includes, among other things, a pedestal that traverses a flow channel disposed between a first wall and a second wall. The pedestal includes at least one interior bore configured to communicate a cooling fluid inside of the pedestal.
Public/Granted literature
- US20160333702A1 GAS TURBINE ENGINE COMPONENT COOLING CIRCUIT WITH RESPIRATING PEDESTAL Public/Granted day:2016-11-17
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