发明名称 |
AIRFOIL SHAPE FOR COMPRESSOR INLET GUIDE VANE |
摘要 |
An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE A. X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances can be joined smoothly with one another to form a complete inlet guide vane airfoil shape.
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申请公布号 |
US2012051927(A1) |
申请公布日期 |
2012.03.01 |
申请号 |
US20100872160 |
申请日期 |
2010.08.31 |
申请人 |
LAMASTER CHRISTOPHER EDWARD;CHALUVADI VENKATA SIVA P.;KASPERSKI DONALD JOSEPH;GENERAL ELECTRIC COMPANY |
发明人 |
LAMASTER CHRISTOPHER EDWARD;CHALUVADI VENKATA SIVA P.;KASPERSKI DONALD JOSEPH |
分类号 |
F01D5/14 |
主分类号 |
F01D5/14 |
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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