Turbomachine radial impeller vibration constraining and damping mechanism
    1.
    发明授权
    Turbomachine radial impeller vibration constraining and damping mechanism 失效
    涡轮机叶片振动约束和阻尼机理

    公开(公告)号:US5984638A

    公开(公告)日:1999-11-16

    申请号:US289795

    申请日:1994-08-12

    IPC分类号: F01D5/24

    CPC分类号: F01D5/24

    摘要: A compressor blade vibration reduction mechanism for a high-speed radial impeller for minimizing fatigue failures from various excitation sources. The vibration reduction mechanism includes a plurality of loose-fitting lashing pins coupling each impeller blade to an adjacent impeller blade. Each lashing pin extends through a first aperture in a blade located adjacent to the blade tip and through a second aperture of an adjacent blade. The second aperture of each blade is located a greater distance from the leading edge of the blade than the first aperture. The second aperture is located in an area of the blade having lower vibration during operation than the blade location where the first aperture is located.

    摘要翻译: 一种用于使来自各种激发源的疲劳失效最小化的用于高速径向叶轮的压缩机叶片减振机构。 减振机构包括将每个叶轮叶片联接到相邻的叶轮叶片的多个松配合的捆扎销。 每个捆扎销延伸穿过位于叶片尖端附近并通过相邻叶片的第二孔的刀片中的第一孔。 每个叶片的第二个孔距离叶片的前缘比第一孔更远的距离。 第二孔位于叶片的操作中比在第一孔所在的叶片位置处具有较低振动的区域。