发明名称 |
TURBINE VANE WITH MISTAKE REDUCTION FEATURE |
摘要 |
A turbine vane for a gas turbine engine has an inner platform, an outer platform, at least one airfoil extending between the inner and outer platforms, and a tab radially extending inward from a front side of the inner platform. The tab contains a mounting aperture and an identification aperture that identifies an engine in which the turbine vane may be installed. |
申请公布号 |
WO2014052220(A1) |
申请公布日期 |
2014.04.03 |
申请号 |
WO2013US61121 |
申请日期 |
2013.09.23 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BERGMAN, RUSSELL J.;BACH, LEONARD A. |
分类号 |
F01D9/02;F01D5/18;F02C7/00 |
主分类号 |
F01D9/02 |
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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