Invention Application
- Patent Title: COMBUSTOR DILUTION HOLE PASSIVE HEAT TRANSFER CONTROL
- Patent Title (中): COMBUSTOR稀释孔被动热传递控制
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Application No.: US14601037Application Date: 2015-01-20
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Publication No.: US20160209033A1Publication Date: 2016-07-21
- Inventor: Steven W. Burd
- Applicant: United Technologies Corporation
- Main IPC: F23R3/00
- IPC: F23R3/00
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
- US10132498B2 Thermal barrier coating of a combustor dilution hole Public/Granted day:2018-11-20
Information query
