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.
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
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