发明名称 |
TRI-LOBED COOLING HOLE AND METHOD OF MANUFACTURE |
摘要 |
A gas turbine engine component includes first and second wall surfaces, an inlet located at the first wall surface, an outlet located at the second wall surface and a diffusing section positioned between the inlet and the outlet. The diffusing section includes a first lobe, a second lobe adjacent the first lobe and a third lobe adjacent the second lobe. The first lobe and the second lobe meet at a first ridge and the second lobe and the third lobe meet at a second ridge.
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申请公布号 |
US2013205787(A1) |
申请公布日期 |
2013.08.15 |
申请号 |
US201213544101 |
申请日期 |
2012.07.09 |
申请人 |
ZELESKY MARK F.;KOHLI ATUL;LEWIS SCOTT D.;UNITED TECHNOLOGIES CORPORATION |
发明人 |
ZELESKY MARK F.;KOHLI ATUL;LEWIS SCOTT D. |
分类号 |
F01D25/12;F01D5/18;F01D9/02;F02C7/00;F23R3/02 |
主分类号 |
F01D25/12 |
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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