发明名称 Film cooling method and method of manufacturing a hole in gas turbine engine part
摘要 A cooled cast part (22) has an exterior surface. A cooling passageway system extends from at least one inlet port to a plurality of outlet ports (40, 42). The passageway system includes a first passageway (55) to at least a first (42) of the outlets and surrounding at least one post (66). The system includes a second passageway (62) to at least a second (40) of the outlets passing through the at least one post (66).
申请公布号 EP1813775(A3) 申请公布日期 2010.11.03
申请号 EP20070250282 申请日期 2007.01.24
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 LUCZAK, BLAKE J.;COUCH, ERIC L.
分类号 F01D5/18;B23P15/02;F02C7/18 主分类号 F01D5/18
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