Method for the modular balancing of a turbomachine rotor
    1.
    发明授权
    Method for the modular balancing of a turbomachine rotor 有权
    涡轮机转子模块平衡的方法

    公开(公告)号:US07555939B2

    公开(公告)日:2009-07-07

    申请号:US12019076

    申请日:2008-01-24

    IPC分类号: G01M1/00

    摘要: A method of balancing a first turbomachine module (20), including along an axis of rotation a bearing plane (22) on one side and a junction plane (24) on the other, with respect to a rotor (1) including said module (20), in which an equivalent complementary module is defined such that the two modules form a rotor equivalent to said rotor by assembling along the junction plane (24), the total unbalance of said equivalent rotor and the corresponding correction to be made to said module are determined, which method includes the following steps: the concentricity deviation of the bearing (22) of the first module (20) with respect to the axis perpendicular to the junction plane (24) is determined; the theoretical geometric unbalance of said equivalent complementary module is calculated; a short journal (40) is mounted on the first module adjacent to the junction plane (24) to form a short rotor whose axis of rotation is substantially coincident with the axis of the module (20) and the unbalance of the short rotor is measured; and the total unbalance of said module is determined by adding to the unbalance of the short rotor a systematic unbalance corresponding to the geometric unbalance.

    摘要翻译: 一种平衡第一涡轮机模块(20)的方法,所述第一涡轮机组件(20)包括相对于包括所述模块的转子(1)沿着旋转轴线在一侧的轴承平面(22)和另一侧的接合平面(24) 20),其中定义等效的互补模块,使得两个模块通过沿着接合面(24)组装形成与所述转子等效的转子,所述等效转子的总不平衡和对所述模块的相应校正 确定该方法,该方法包括以下步骤:确定第一模块(20)的轴承(22)相对于垂直于结平面(24)的轴的同心度偏差; 计算所述等效补充模块的理论几何不平衡; 短路颈(40)安装在与接合面(24)相邻的第一模块上以形成短转子,其旋转轴线基本上与模块(20)的轴线重合,并测量短转子的不平衡 ; 并且通过增加短转子的不平衡来确定对应于几何不平衡的系统不平衡来确定所述模块的总体不平衡。

    METHOD FOR THE MODULAR BALANCING OF A TURBOMACHINE ROTOR
    2.
    发明申请
    METHOD FOR THE MODULAR BALANCING OF A TURBOMACHINE ROTOR 有权
    涡轮转子模块平衡方法

    公开(公告)号:US20080245138A1

    公开(公告)日:2008-10-09

    申请号:US12019076

    申请日:2008-01-24

    IPC分类号: G01M1/00

    摘要: A method of balancing a first turbomachine module (20), comprising along an axis of rotation a bearing plane (22) on one side and a junction plane (24) on the other, with respect to a rotor (1) comprising said module (20), in whichan equivalent complementary module is defined such that the two modules form a rotor equivalent to said rotor by assembling along the junction plane (24), the total unbalance of said equivalent rotor and the corresponding correction to be made to said module are determined, which method comprises the following steps: the concentricity deviation of the bearing (22) of the first module (20) with respect to the axis perpendicular to the junction plane (24) is determined; the theoretical geometric unbalance of said equivalent complementary module is calculated; a short journal (40) is mounted on the first module adjacent to the junction plane (24) to form a short rotor whose axis of rotation is substantially coincident with the axis of the module (20) and the unbalance of the short rotor is measured; and the total unbalance of said module is determined by adding to the unbalance of the short rotor a systematic unbalance corresponding to the geometric unbalance.

    摘要翻译: 一种平衡第一涡轮机模块(20)的方法,所述第一涡轮机组件(20)相对于包括所述模块的转子(1)沿着旋转轴线包括一侧的支承平面(22)和另一侧的接合平面(24) 20),其中定义等效的互补模块,使得两个模块通过沿着接合面(24)组装形成与所述转子等效的转子,所述等效转子的总不平衡和对所述模块的相应校正 确定该方法,该方法包括以下步骤:确定第一模块(20)的轴承(22)相对于垂直于结面(24)的轴的同心度偏差; 计算所述等效补充模块的理论几何不平衡; 短路颈(40)安装在与接合面(24)相邻的第一模块上以形成短转子,其旋转轴线基本上与模块(20)的轴线重合,并测量短转子的不平衡 ; 并且通过增加短转子的不平衡来确定对应于几何不平衡的系统不平衡来确定所述模块的总体不平衡。