发明名称 |
Method for decreasing a heat load on a combustor liner |
摘要 |
A combustor liner (60) has a stepped combustor liner surface (62) and an overhang portion (66) forming an air cooling slot (64). A contoured rear facing edge (70) of the overhang portion reduces turbulence of combustion gas flow and reduces a combustor liner surface area exposed to combustion gases. A thermal barrier coating (78) is also applied to the contoured rear facing edge, reducing heat flow into the overhang portion and hence reducing the operating temperature of the combustor liner. Thus, the amount of cooling air is reduced, which can reduce exhaust emissions, increase engine performance and extend a working life of the combustor assembly. <IMAGE> |
申请公布号 |
EP1104872(B1) |
申请公布日期 |
2007.04.25 |
申请号 |
EP20000310678 |
申请日期 |
2000.12.01 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
HAGLE, MICHAEL P.;COOPER, JAMES NEIL;JIH, JUNHAUR |
分类号 |
F02C7/18;F23R3/08;F23R3/42 |
主分类号 |
F02C7/18 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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