发明名称 COMBUSTOR FOR GAS TURBINE ENGINE
摘要 A combustor with a liner where each of the walls has a respective circumferential row of dilution holes defined therethrough adjacent a junction between the primary zone and the dilution zone. In the primary zone, the inner surface of each of the walls is covered by at least one heat shield attached thereto and spaced apart therefrom to allow air circulation between the inner surface and the at least one heat shield, the walls each having a plurality of cooling holes defined therethrough having a smaller diameter than that of the dilution holes. In the dilution zone, the inner surface of each of the walls is free of heat shields, and the walls each have a plurality of effusion cooling holes defined therethrough and having a smaller diameter than that of the dilution holes.
申请公布号 US2013180257(A1) 申请公布日期 2013.07.18
申请号 US201213352889 申请日期 2012.01.18
申请人 STASTNY HONZA;VERHIEL JEFFREY RICHARD;SAMPATH PARTHASARATHY 发明人 STASTNY HONZA;VERHIEL JEFFREY RICHARD;SAMPATH PARTHASARATHY
分类号 F23R3/02 主分类号 F23R3/02
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