Invention Grant
- Patent Title: Thermal barrier coating inside cooling channels
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Application No.: US14799994Application Date: 2015-07-15
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Publication No.: US09869183B2Publication Date: 2018-01-16
- Inventor: Gabriel L. Suciu , Brian D. Merry , James D. Hill , Wesley K. Lord
- 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: F01D5/08
- IPC: F01D5/08 ; F01D5/28

Abstract:
A rotor for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a rotor disk rotatable about an axis and a gas path wall coupled to and radially outward of the rotor disk. The gas path wall bounds a radially inward portion of a gas path. A plurality of rotor spokes are radially intermediate the rotor disk and the gas path wall. The plurality of rotor spokes is circumferentially spaced to define a plurality of cooling channels intermediate the rotor disk and the gas path wall. A thermal barrier coating is disposed on a surface of at least one of the plurality of cooling channels. A method of cooling a rotor assembly is also disclosed.
Public/Granted literature
- US20160032731A1 THERMAL BARRIER COATING INSIDE COOLING CHANNELS Public/Granted day:2016-02-04
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