发明名称 |
Ceramic combustor liner panel for a gas turbine engine |
摘要 |
A combustor assembly includes a support structure (29) and at least one combustor liner panel (30) selectively attached to the support structure (29). The combustor liner panel (30) includes an uncooled ceramic portion (40), a cooled ceramic portion (42) and a support (44) that receives the cooled ceramic portion (42). |
申请公布号 |
EP2051009(A2) |
申请公布日期 |
2009.04.22 |
申请号 |
EP20080253284 |
申请日期 |
2008.10.08 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DIERBERGER, JAMES A.;SCHLICHTING, KEVIN W.;FRELING, MELVIN |
分类号 |
F23R3/00;F23R3/60 |
主分类号 |
F23R3/00 |
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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