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
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