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 |
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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