Invention Grant
- Patent Title: Gas turbine engine component having curved turbulator
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Application No.: US14765390Application Date: 2014-01-31
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Publication No.: US10316668B2Publication Date: 2019-06-11
- Inventor: Mosheshe Camara-Khary Blake , Lisa K. Osborne , Thomas N. Slavens
- 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/US2014/013981 WO 20140131
- International Announcement: WO2014/175937 WO 20141030
- Main IPC: F01D5/14
- IPC: F01D5/14 ; F01D5/18 ; F01D9/06 ; F01D25/08
Abstract:
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a wall that forms a portion of an outer periphery of at least one cavity and at least one curved turbulator that extends from said wall.
Public/Granted literature
- US20150377029A1 GAS TURBINE ENGINE COMPONENT HAVING CURVED TURBULATOR Public/Granted day:2015-12-31
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