发明名称 |
GAS TURBINE ENGINE COMPONENT COOLING PASSAGE WITH ASYMMETRICAL PEDESTALS |
摘要 |
A gas turbine engine component includes spaced apart walls that provide a cooling passage that extends in a first direction. A pedestal is arranged in the cooling passage and interconnects the walls in a thickness direction that is transverse to the first direction. The pedestal is asymmetrical in the thickness direction. |
申请公布号 |
EP3080416(A1) |
申请公布日期 |
2016.10.19 |
申请号 |
EP20140869625 |
申请日期 |
2014.12.02 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
THISTLE, Charles;THORNTON, Lane |
分类号 |
F02C7/18;F01D5/08;F01D25/12 |
主分类号 |
F02C7/18 |
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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