发明名称 |
PLATFORM COOLING CORE FOR A GAS TURBINE ENGINE ROTOR BLADE |
摘要 |
<p>A rotor blade according to an exemplary aspect of the present disclosure includes, among other things, a platform, an airfoil that extends from the platform, a first cooling core that extends at least partially inside the airfoil, a second cooling core inside of the platform and a first cooling hole that extends between a mate face of the platform and the second cooling core.</p> |
申请公布号 |
WO2015057310(A2) |
申请公布日期 |
2015.04.23 |
申请号 |
WO2014US53042 |
申请日期 |
2014.08.28 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HOUGH, MATTHEW ANDREW;BEATTIE, JEFFREY S. |
分类号 |
F01D5/18;F01D25/12;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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