Invention Grant
- Patent Title: Turbine engine multi-walled structure with internal cooling element(s)
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Application No.: US15034717Application Date: 2014-11-21
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Publication No.: US10753608B2Publication Date: 2020-08-25
- Inventor: Frank J. Cunha , Stanislav Kostka, Jr.
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Getz Balich LLC
- International Application: PCT/US2014/668887 WO 20141121
- International Announcement: WO2015/122950 WO 20150820
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23M5/00 ; F23M5/08 ; F23R3/06 ; F23R3/50

Abstract:
A structure is provided for a turbine engine. The structure includes a shell with a first surface, and a heat shield with a textured second surface and a textured third surface. The texture of a portion of the second surface is different than the texture of a portion of the third surface. The first surface and the second surface define a first cooling cavity between the shell and the heat shield. The first surface and the third surface define a second cooling cavity between the shell and the heat shield.
Public/Granted literature
- US20160265775A1 TURBINE ENGINE MULTI-WALLED STRUCTURE WITH INTERNAL COOLING ELEMENT(S) Public/Granted day:2016-09-15
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