Turbomachine component handling assembly

    公开(公告)号:US10294082B2

    公开(公告)日:2019-05-21

    申请号:US15635363

    申请日:2017-06-28

    摘要: The present disclosure is directed to a component handling assembly. The component handling assembly includes a base member, an arm pivotably coupled to the base member, and a beam rotatably coupled to the base member. The component handling assembly also includes a counterweight rotatably coupled to a first end of the beam. The component handling assembly further includes a coupling assembly coupled to a second end of the beam. The coupling assembly is configured for coupling to a component. Rotating the counterweight in a first direction rotates the beam, the coupling assembly, and the component in a second direction.

    Turbine casing jack
    2.
    发明授权

    公开(公告)号:US10280802B2

    公开(公告)日:2019-05-07

    申请号:US15258543

    申请日:2016-09-07

    摘要: An apparatus for lifting an inner casing of a turbine includes a base, an arm, a guide roller, and an adjustment system. The arm has a first end and a second end, and is pivotally connected to the base intermediate the first end and the second end. The guide roller is operatively coupled to the first end of the arm to rotatably engage an exterior surface of the inner casing, and an adjustment system extending from the base and engaging the arm to change an angular position of the arm relative to the base and adjust a position of the guide roller relative to the exterior surface of the inner casing.

    Axial retention assembly for combustor components of a gas turbine engine

    公开(公告)号:US10969106B2

    公开(公告)日:2021-04-06

    申请号:US16539164

    申请日:2019-08-13

    摘要: The present subject matter is directed to an axial retention assembly for combustor components of a gas turbine engine. The axial retention assembly may include a combustor having include a liner defining a liner aperture extending therethrough. Additionally, the combustor may further include a sleeve defining a sleeve aperture extending therethrough, with the sleeve positioned radially outward from and at least partially circumferentially positioned around the liner. Furthermore, the axial retention assembly may include a frame having a mounting projection positioned within the sleeve aperture. Moreover, the axial retention assembly may include a clamp plate adjustably coupled to the frame. In addition, the axial retention assembly may include a clamp plate adjustment rod extending through the liner aperture and threadingly engaging the clamp plate such that relative movement between the liner and the sleeve along the axial centerline is reduced.

    Axial Retention Assembly for Combustor Components of a Gas Turbine Engine

    公开(公告)号:US20210018179A1

    公开(公告)日:2021-01-21

    申请号:US16514296

    申请日:2019-07-17

    IPC分类号: F23R3/60

    摘要: The present disclosure is directed to an axial retention assembly for combustor components of a gas turbine engine. The axial retention assembly may include a combustor having a liner and a casing, with the casing including a flange spaced apart from the liner along an axial centerline of the combustor. Furthermore, the axial retention assembly may include a mounting plate having a first end removably coupled to the flange and a second end positioned inward from the casing in a radial direction. Moreover, the axial retention assembly may include a clamp removably coupled to the liner. Additionally, the axial retention assembly may include a tie rod coupled to the second end of the mounting plate and the clamp to reduce relative movement between the liner and the casing along the axial centerline.