发明名称 |
ENHANCED COOLING FOR BLADE TIP |
摘要 |
In a featured embodiment, a gas turbine engine component comprises an airfoil having a leading edge, a trailing edge, and pressure and suction side walls extending from the leading edge to the trailing edge. The airfoil extends from a base to a tip. A shelf is formed in the tip, and extends from the pressure side wall, around the leading edge, to the suction side wall. |
申请公布号 |
WO2015094498(A1) |
申请公布日期 |
2015.06.25 |
申请号 |
WO2014US63974 |
申请日期 |
2014.11.05 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
AUXIER, JAMES T.;SLAVENS, THOMAS N.;DONNELL, BRANDON S.;GIRMA, YAFET |
分类号 |
F01D5/18;F01D5/20;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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