Invention Grant
- Patent Title: Thermal barrier coating of a combustor dilution hole
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Application No.: US14601037Application Date: 2015-01-20
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Publication No.: US10132498B2Publication Date: 2018-11-20
- Inventor: Steven W. Burd
- 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: O'Shea Getz P.C.
- Main IPC: F23R3/04
- IPC: F23R3/04 ; F23R3/00 ; F23R3/06 ; F23R3/50
Abstract:
Aspects of the disclosure are directed to a liner associated with a combustor of an aircraft engine, comprising: a thermal barrier coating, and a base metal, wherein the thermal barrier coating comprises a contoured surface on a flowpath side proximate to an exit of a hole formed by the thermal barrier coating and the base metal.
Public/Granted literature
- US20160209033A1 COMBUSTOR DILUTION HOLE PASSIVE HEAT TRANSFER CONTROL Public/Granted day:2016-07-21
Information query
