DAMPER PIN FOR DAMPING ADJACENT TURBINE BLADES
    1.
    发明申请
    DAMPER PIN FOR DAMPING ADJACENT TURBINE BLADES 审中-公开
    用于阻尼邻近涡轮叶片的阻尼器

    公开(公告)号:US20170067346A1

    公开(公告)日:2017-03-09

    申请号:US14844280

    申请日:2015-09-03

    Abstract: A damper pin for damping adjacent turbine blades coupled to a rotor disk comprises a first elongated body having a center portion disposed between a first end portion and a second end portion. The first end portion, center portion and second end portion define a generally arcuate top portion of the first elongated body. The first elongated body defines a slot that extends axially therethrough. The damper pin further includes a second elongated body having a generally arcuate top portion. The second elongated body is at least partially disposed within the slot and is slideably engaged in an axial direction with the first elongated body.

    Abstract translation: 用于阻尼与转子盘耦合的相邻涡轮叶片的阻尼器销包括第一细长体,其具有设置在第一端部和第二端部之间的中心部分。 第一端部,中心部分和第二端部限定第一细长主体的大致弓形顶部。 第一细长体限定了轴向延伸穿过其中的狭槽。 减震器销还包括具有大致弓形顶部的第二细长主体。 所述第二细长体至少部分地设置在所述槽内,并且能够与所述第一细长体在轴向方向上可滑动地接合。

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