发明名称 |
GAS TURBINE ENGINE SHAPED FILM COOLING HOLE |
摘要 |
A component for a gas turbine engine includes a wall that adjoins an interior cooling passage and provides an exterior surface. A film cooling hole fluidly connects the interior cooling passage and the exterior surface. The film cooling passage includes inlet and outlet passages that fluidly interconnect and adjoin one another in a misaligned non-line of sight relationship. |
申请公布号 |
WO2014197061(A3) |
申请公布日期 |
2015.03.05 |
申请号 |
WO2014US25368 |
申请日期 |
2014.03.13 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
XU, JINQUAN |
分类号 |
F02C7/12;F01D5/18;F01D25/12;F04D29/58 |
主分类号 |
F02C7/12 |
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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