Inlet guide vane alignment apparatus and method
    4.
    发明授权
    Inlet guide vane alignment apparatus and method 有权
    进口导向叶片对准装置及方法

    公开(公告)号:US08978262B2

    公开(公告)日:2015-03-17

    申请号:US13689269

    申请日:2012-11-29

    CPC classification number: G01B5/14 F01D25/285 F05D2230/644

    Abstract: Various embodiments include alignment apparatuses and associated methods for use on a turbine (e.g., a gas turbine). In various particular embodiments, an apparatus for aligning an unfixed inlet guide vane (IGV) adjacent a fixed IGV in a gas turbine. In some cases the apparatus includes: a first wedge member for interfacing with the fixed IGV; a second wedge member movably coupled with the first wedge member, the second wedge member for interfacing with the unfixed IGV; and an adjustment apparatus coupled to the first wedge member and the second wedge member, the adjustment apparatus for modifying a position of the second wedge member relative to the first wedge member to actuate movement of the unfixed IGV relative to the fixed IGV.

    Abstract translation: 各种实施例包括在涡轮机(例如燃气轮机)上使用的对准装置和相关联的方法。 在各种具体实施例中,一种用于使与燃气轮机中的固定IGV相邻的未固定入口导叶(IGV)对准的装置。 在一些情况下,该设备包括:用于与固定IGV接口的第一楔形构件; 可移动地与第一楔形构件联接的第二楔形构件,用于与未固定的IGV接合的第二楔形构件; 以及联接到所述第一楔形构件和所述第二楔形构件的调节装置,所述调整装置用于修改所述第二楔形构件相对于所述第一楔形构件的位置,以致所述未固定的IGV相对于所述固定的IGV的移动。

    INLET GUIDE VANE ALIGNMENT APPARATUS AND METHOD
    7.
    发明申请
    INLET GUIDE VANE ALIGNMENT APPARATUS AND METHOD 有权
    进口导向器对准装置和方法

    公开(公告)号:US20140144034A1

    公开(公告)日:2014-05-29

    申请号:US13689269

    申请日:2012-11-29

    CPC classification number: G01B5/14 F01D25/285 F05D2230/644

    Abstract: Various embodiments include alignment apparatuses and associated methods for use on a turbine (e.g., a gas turbine). In various particular embodiments, an apparatus for aligning an unfixed inlet guide vane (IGV) adjacent a fixed IGV in a gas turbine. In some cases the apparatus includes: a first wedge member for interfacing with the fixed IGV; a second wedge member movably coupled with the first wedge member, the second wedge member for interfacing with the unfixed IGV; and an adjustment apparatus coupled to the first wedge member and the second wedge member, the adjustment apparatus for modifying a position of the second wedge member relative to the first wedge member to actuate movement of the unfixed IGV relative to the fixed IGV.

    Abstract translation: 各种实施例包括在涡轮机(例如燃气轮机)上使用的对准装置和相关联的方法。 在各种具体实施例中,一种用于使与燃气轮机中的固定IGV相邻的未固定入口导叶(IGV)对准的装置。 在一些情况下,该设备包括:用于与固定IGV接口的第一楔形构件; 可移动地与第一楔形构件联接的第二楔形构件,用于与未固定的IGV接合的第二楔形构件; 以及联接到所述第一楔形构件和所述第二楔形构件的调节装置,所述调整装置用于修改所述第二楔形构件相对于所述第一楔形构件的位置,以致所述未固定的IGV相对于所述固定的IGV的移动。

    System and Method For Modifying A Rotor
    8.
    发明申请
    System and Method For Modifying A Rotor 有权
    用于修改转子的系统和方法

    公开(公告)号:US20130205589A1

    公开(公告)日:2013-08-15

    申请号:US13847660

    申请日:2013-03-20

    Abstract: A system for modifying a slot in a rotor includes a drill, a clamp connected to the drill and configured to engage with an interior surface of the slot, and means for supporting the drill from a stationary platform adjacent to the rotor. A method for modifying a slot in a rotor includes connecting a coupling to a stationary platform adjacent to the rotor, connecting a drill to the coupling, and locating the drill proximate to the slot. The method further includes inserting a clamp into the slot, engaging the clamp with an interior surface of the slot, and operating the drill to create a cavity in the slot.

    Abstract translation: 用于修改转子中的槽的系统包括钻头,连接到钻头并被配置为与槽的内表面接合的夹具以及用于从邻近转子的固定平台支撑钻头的装置。 用于修改转子中的槽的方法包括将联接件连接到与转子相邻的固定平台,将钻头连接到联接器,以及将钻头定位在靠近槽的位置。 该方法还包括将夹具插入槽中,将夹具与槽的内表面接合,并操作钻头以在槽中产生空腔。

    Fixture for restraining a turbine wheel

    公开(公告)号:US10024164B2

    公开(公告)日:2018-07-17

    申请号:US15277327

    申请日:2016-09-27

    Abstract: A fixture for restraining a wheel of a turbomachine has a dovetail section adapted for insertion into a dovetail slot of the wheel. A mounting section is located adjacent to, or formed integrally with, the dovetail section. At least one coupling ring is attached to the mounting section, and the coupling ring is adapted to be secured to a stationary anchoring point via a restraint. The stationary anchoring point includes at least one counterbore assembly having a coupling ring attached thereto. The counterbore assembly is adapted to be secured to a stationary structure. The stationary structure may be a shell, a flange or a casing of the turbomachine.

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