AIRFOIL SHAPE FOR A COMPRESSOR VANE
    11.
    发明申请
    AIRFOIL SHAPE FOR A COMPRESSOR VANE 有权
    压缩机VANE的气翼形状

    公开(公告)号:US20120051926A1

    公开(公告)日:2012-03-01

    申请号:US12872148

    申请日:2010-08-31

    CPC classification number: F01D5/141 F05D2250/74

    Abstract: 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 airfoil shape.

    Abstract translation: 具有基本上符合表A所示的X,Y和Z的笛卡尔坐标值的公称轮廓的制品.X和Y是以平滑连续的弧连接时以每英寸限定翼型轮廓部分的距离,以英寸为单位 Z英寸。 Z距离处的轮廓部分可以彼此平滑地连接以形成完整的翼型形状。

    Airfoil shape for a compressor vane
    14.
    发明授权
    Airfoil shape for a compressor vane 有权
    用于压缩机叶片的翼型

    公开(公告)号:US08491260B2

    公开(公告)日:2013-07-23

    申请号:US12872148

    申请日:2010-08-31

    CPC classification number: F01D5/141 F05D2250/74

    Abstract: 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 airfoil shape.

    Abstract translation: 具有基本上符合表A所示的X,Y和Z的笛卡尔坐标值的公称轮廓的制品.X和Y是以平滑连续的弧连接时以每英寸限定翼型轮廓部分的距离,以英寸为单位 Z英寸。 Z距离处的轮廓部分可以彼此平滑地连接以形成完整的翼型形状。

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