Rotor blade profile optimization
    1.
    发明申请
    Rotor blade profile optimization 有权
    转子叶片轮廓优化

    公开(公告)号:US20080101959A1

    公开(公告)日:2008-05-01

    申请号:US11586952

    申请日:2006-10-26

    IPC分类号: B64C27/46

    摘要: An airfoil for a rotor blade including an uncoated profile substantially in accordance with Cartesian coordinate values of X, Y and Z to facilitate balancing performance and durability of the rotor blade and to facilitate improving an operating efficiency of a high-pressure turbine is provided. The profile is carried only to four decimal places, wherein Y represents a distance from a platform on which the airfoil is mounted, and X and Z are coordinates defining the profile at each distance Y from the platform.

    摘要翻译: 提供了一种用于转子叶片的翼型件,其包括基本上根据X,Y和Z的笛卡尔坐标值的未涂覆轮廓,以便于平衡转子叶片的性能和耐久性,并且有助于提高高压涡轮机的操作效率。 配置文件仅承载四位小数,其中Y表示与安装有翼型件的平台的距离,X和Z是从平台每个距离Y定义轮廓的坐标。

    Rotor blade profile optimization
    2.
    发明授权
    Rotor blade profile optimization 有权
    转子叶片轮廓优化

    公开(公告)号:US07497663B2

    公开(公告)日:2009-03-03

    申请号:US11586952

    申请日:2006-10-26

    IPC分类号: F01D5/14

    摘要: An airfoil for a rotor blade including an uncoated profile substantially in accordance with Cartesian coordinate values of X, Y and Z to facilitate balancing performance and durability of the rotor blade and to facilitate improving an operating efficiency of a high-pressure turbine is provided. The profile is carried only to four decimal places, wherein Y represents a distance from a platform on which the airfoil is mounted, and X and Z are coordinates defining the profile at each distance Y from the platform.

    摘要翻译: 提供了一种用于转子叶片的翼型件,其包括基本上根据X,Y和Z的笛卡尔坐标值的未涂覆轮廓,以便于平衡转子叶片的性能和耐久性,并且有助于提高高压涡轮机的操作效率。 配置文件仅承载四位小数,其中Y表示与安装有翼型件的平台的距离,X和Z是从平台每个距离Y定义轮廓的坐标。