GAS TURBINE ENGINE COMPRESSOR ROTOR ASSEMBLY AND BALANCING SYSTEM
    1.
    发明申请
    GAS TURBINE ENGINE COMPRESSOR ROTOR ASSEMBLY AND BALANCING SYSTEM 有权
    气体涡轮发动机压缩机转子总成和平衡系统

    公开(公告)号:US20140140849A1

    公开(公告)日:2014-05-22

    申请号:US13684056

    申请日:2012-11-21

    CPC classification number: F01D5/027 F01D5/06 F01D5/3015 F01D5/3038

    Abstract: A method for balancing a compressor rotor assembly including a forward weldment (211) and an aft weldment (212) includes pre-balancing the aft weldment (212) of the compressor rotor assembly (210) with compressor disks (220) prior to populating the compressor disks (220) with circumferentially installed compressor rotor blades (230). Pre-balancing the aft weldment (212) includes measuring a rotational balance of the aft weldment (212). Pre-balancing the aft weldment (212) also includes determining a number of underplatform weights (260) needed and a location for each underplatform weight (260) within a circumferential slot (236) of one the compressor disks (220). Pre-balancing the aft weldment (212) further includes mounting each underplatform weight (260) in the determined location.

    Abstract translation: 一种用于平衡包括前向焊接件(211)和后部焊件(212)的压缩机转子组件的方法包括:在压缩机转子组件(210)的后部焊件(212)与压缩机盘(220)预先平衡之前, 具有周向安装的压缩机转子叶片(230)的压缩机盘(220)。 预平衡后焊件(212)包括测量后焊件(212)的旋转平衡。 预平衡船尾焊件(212)还包括确定在压缩机盘(220)之一的圆周槽(236)内的所需的底板数量(260)和每个底板下重量(260)的位置。 预平衡船尾焊件(212)还包括将每个底板重量(260)安装在所确定的位置。

    Gas turbine engine compressor rotor assembly and balancing system
    2.
    发明授权
    Gas turbine engine compressor rotor assembly and balancing system 有权
    燃气涡轮发动机压缩机转子总成和平衡系统

    公开(公告)号:US09404367B2

    公开(公告)日:2016-08-02

    申请号:US13684056

    申请日:2012-11-21

    CPC classification number: F01D5/027 F01D5/06 F01D5/3015 F01D5/3038

    Abstract: A method for balancing a compressor rotor assembly including a forward weldment (211) and an aft weldment (212) includes pre-balancing the aft weldment (212) of the compressor rotor assembly (210) with compressor disks (220) prior to populating the compressor disks (220) with circumferentially installed compressor rotor blades (230). Pre-balancing the aft weldment (212) includes measuring a rotational balance of the aft weldment (212). Pre-balancing the aft weldment (212) also includes determining a number of underplatform weights (260) needed and a location for each underplatform weight (260) within a circumferential slot (236) of one the compressor disks (220). Pre-balancing the aft weldment (212) further includes mounting each underplatform weight (260) in the determined location.

    Abstract translation: 一种用于平衡包括前向焊接件(211)和后部焊件(212)的压缩机转子组件的方法包括:在压缩机转子组件(210)的后部焊件(212)与压缩机盘(220)预先平衡之前, 具有周向安装的压缩机转子叶片(230)的压缩机盘(220)。 预平衡后焊件(212)包括测量后焊件(212)的旋转平衡。 预平衡船尾焊件(212)还包括确定在压缩机盘(220)之一的圆周槽(236)内的所需的底板数量(260)和每个底板下重量(260)的位置。 预平衡船尾焊件(212)还包括将每个底板重量(260)安装在所确定的位置。

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