Movable shaft assembly
    11.
    发明授权
    Movable shaft assembly 有权
    活动轴总成

    公开(公告)号:US06174130B1

    公开(公告)日:2001-01-16

    申请号:US09345191

    申请日:1999-06-30

    IPC分类号: F01D1712

    摘要: A shaft assembly for movement of an array of adjustable members comprises a hollow shaft body including a shaft body wall with a wall outer surface. A plurality of spaced apart clevises, secured with the shaft body wall on the wall outer surface, each includes connection means disposed away from the wall outer surface for connection with an actuator for movement of the adjustable members.

    摘要翻译: 用于移动可调节构件阵列的轴组件包括中空轴体,其包括具有壁外表面的轴体壁。 在壁外表面上固定有轴体壁的多个间隔开的夹子各自包括远离壁外表面设置的连接装置,用于与用于可调节构件的运动的致动器连接。

    Asymmetric axial dovetail and rotor disk
    12.
    发明授权
    Asymmetric axial dovetail and rotor disk 失效
    不对称轴向燕尾和转盘

    公开(公告)号:US5310318A

    公开(公告)日:1994-05-10

    申请号:US95231

    申请日:1993-07-21

    IPC分类号: F01D5/30

    CPC分类号: F01D5/3007

    摘要: A rotor disk includes a rim with axially spaced apart forward and aft ends, with the aft end having a larger diameter than the forward end. The rim includes a plurality of straight dovetail slots defining dovetail posts therebetween. Each dovetail post includes a pair of lobes, a neck, and first and second pressure faces facing radially inwardly from the lobes. The first and second pressure faces vary in radial height therebetween from a first magnitude at the rim aft end to a second and smaller magnitude at the rim forward end to shift a portion of the bending loads from the dovetail post at the rim forward end to the dovetail post at the larger rim aft end.

    摘要翻译: 转子盘包括具有轴向间隔开的前端和后端的边缘,其后端具有比前端更大的直径。 轮辋包括多个直线的燕尾槽,其间形成燕尾榫。 每个燕尾柱包括一对叶,颈部以及从叶片径向向内面对的第一和第二压力面。 第一和第二压力面之间的径向高度从边缘后端处的第一幅度到边缘前端处的第二和更小的幅度变化,以将一部分弯曲载荷从轮辋前端的鸠尾柱移动到 在较大的轮辋尾端的燕尾柱。

    Dovetail sealing device for axial dovetail rotor blades
    13.
    发明授权
    Dovetail sealing device for axial dovetail rotor blades 失效
    用于轴向燕尾转子叶片的燕尾密封装置

    公开(公告)号:US5257909A

    公开(公告)日:1993-11-02

    申请号:US931079

    申请日:1992-08-17

    IPC分类号: F01D11/00 F01D5/30

    摘要: A sealing device for compressor axial dovetail rotor blades for a gas turbine engine comprising a sealing member having a finger portion extending from a main body portion which engages a disk hook located on each disk post and forms a first point of contact about which the sealing member rotates. The sealing member further comprises an extended skirt portion which engages the blade platform of the rotor blades forming a second point of contact. The main body has a center of gravity positioned such that during operation of the engine the main body pivots due to centrifugal force about the disk hook such that the skirt portion engages the blade platform. A split ring is located between the disk posts and a tail portion extending from the lower portion of the sealing member and engages the disk post and tail portion during operation of the engine thereby forming a third point of contact. The combination of the skirt element contacting the blade platform and the split ring contacting the tail portion and the disk posts effectively prevents any leakage axially through the rotor blade dovetail.

    摘要翻译: 一种用于燃气涡轮发动机的压缩机轴向燕尾转子叶片的密封装置,包括密封构件,该密封构件具有从主体部延伸的指状部分,该主体部分接合位于每个盘柱上的盘钩,并形成第一接触点,密封构件 旋转 密封构件还包括延伸的裙部,其接合形成第二接触点的转子叶片的叶片平台。 主体具有重心定位,使得在发动机操作期间,主体由于围绕盘钩的离心力枢转,使得裙部接合刀片平台。 开口环位于盘柱和从密封构件的下部延伸的尾部之间并且在发动机操作期间与盘柱和尾部接合,从而形成第三接触点。 接触叶片平台的裙部元件和接触尾部和圆盘柱的开口环的组合有效地防止轴向穿过转子叶片燕尾榫的任何泄漏。