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107 条记录 (耗时 0.01 秒)

    Rotor blade ring of an axial flow turbomachine
    31.
    发明授权
    Rotor blade ring of an axial flow turbomachine 失效
    轴流涡轮机的转子叶片环

    公开(公告)号：US4699569A

    公开(公告)日：1987-10-13

    申请号：US877123

    申请日：1986-06-23

    申请人： Kurt Gloor

    发明人： Kurt Gloor

    IPC分类号： F01D5/22 ,  F01D5/24

    CPC分类号： F01D5/225 ,  F01D5/24 ,  F05D2260/96

    摘要： In the rotor blade ring of an axial flow turbomachine, the rotor blades are each provided at their radially outer ends with a shroud plate and are fastened at their radially inner ends, by means of a root, in a corresponding groove of the machine rotor. The shroud plates are connected together in the peripheral direction by means of wires rolled into turned recesses. Grooves (10), with a clear width (w.sub.1) which is dimensioned larger than the width (w.sub.2) of the shroud plate turned recess (8) provided for the wire (7) to be rolled in, are machined in the end surface (6) of the shroud plate (2). A spacer means (11), surrounding the wire at least in the region of the rolling positions and removable after rolling, is laid in the grooves during the rolling procedure. This material is preferably a hard paper which is burnt to ashes during machine operation.

    摘要翻译： 在轴流式涡轮机的转子叶片环中，转子叶片各自在其径向外端处设置有护罩板，并且通过根部在其径向内端处紧固在机器转子的相应凹槽中。 护罩板通过卷成转动凹槽的金属丝在圆周方向上连接在一起。 具有宽度（w1）的凹槽（10）的尺寸被设计成大于被设置用于被卷绕的线材（7）的护罩板转动凹部（8）的宽度（w2），在端表面 6）。 至少在轧制位置的区域中包围线材的间隔装置（11）在轧制过程之后被放置在槽中。 这种材料优选是在机器操作期间被烧成灰的硬纸。

    Bladed rotor assembly, and method of forming same
    32.
    发明授权
    Bladed rotor assembly, and method of forming same 失效
    叶片转子组件及其形成方法

    公开(公告)号：US4684326A

    公开(公告)日：1987-08-04

    申请号：US602066

    申请日：1984-04-19

    申请人： Mark E. Wassell ,  John G. Mosimann

    发明人： Mark E. Wassell ,  John G. Mosimann

    IPC分类号： F01D5/22 ,  F01D5/24 ,  F01D5/30 ,  F01D5/32

    CPC分类号： F01D5/326 ,  F01D5/22 ,  F01D5/225 ,  F01D5/24

    摘要： The Assembly has a submerged root, turbine-wheel-blading configuration, and utilizes circumferentially oriented, buried, friction damping wires, and continuous, overlapping, tip shrouds to minimize vibratory response. The wires, in the presence of blade vibration, simultaneously rub on both the blades and surfaces of a recess in the wheel in which the blade roots are fixed. The continuous tip shrouding provides additional damping through shroud-to-shroud interface rubbing. The assembly has a stack of identical blades, obviating any need for relatively weak locking blades or pieces. The method defines the steps of forming a peripheral recess in a wheel, in which to secure root ends of blades, and setting the damping wires (or wire) therein prior to installing the blade root ends, and uniformly spacing-apart the blades after securing the same to the wheel.

    摘要翻译： 该组件具有淹没的根部，涡轮机叶轮构造，并且利用周向定向的，埋入的摩擦阻尼线以及连续的，重叠的尖端护罩以使振动响应最小化。 在刀片振动的情况下，电线同时摩擦在叶片根部固定的车轮上的凹槽的两个叶片和表面上。 连续的尖端护罩通过护罩对护罩接口摩擦提供额外的阻尼。 组件具有相同刀片的堆叠，消除了对相对较弱的锁定刀片或件的任何需要。 该方法限定了在车轮中形成周边凹槽的步骤，其中固定刀片的根部端部，并且在安装刀片根部末端之前将阻尼丝（或线）设置在其中，并且在固定之后均匀地间隔开刀片 相同的轮子。

    Vibration supression for turbine blades
    33.
    发明授权
    Vibration supression for turbine blades 失效
    涡轮叶片的振动抑制

    公开(公告)号：US4268223A

    公开(公告)日：1981-05-19

    申请号：US942143

    申请日：1978-09-14

    申请人： Emil Anner ,  Harry Brunner ,  Hans J. Meister

    发明人： Emil Anner ,  Harry Brunner ,  Hans J. Meister

    IPC分类号： F01D5/24

    CPC分类号： F01D5/24 ,  Y10S416/50

    摘要： A method and apparatus for suppressing vibration in turbine blading and the like is disclosed. A damping tube is inserted through an aperture in each of a plurality of turbine blades. By expanding the damping tube after it is inserted in the blades the tube is firmly secured to each blade. A wire may be inserted through the damping tube and is secured by crimping the expanded tube portions. The tube may be divided into circumferential segments with each tube being widened for example by means of a center punch at an end portion which extends through the final blade of each segment.

    摘要翻译： 公开了一种用于抑制涡轮叶片等中的振动的方法和装置。 阻尼管通过多个涡轮机叶片中的每一个中的孔插入。 通过在将阻尼管插入叶片之后扩张阻尼管，该管牢固地固定到每个叶片上。 线可以插入通过阻尼管，并且通过压接膨胀的管部分来固定。 管可以被分成圆周段，每个管例如通过在延伸穿过每个段的最终叶片的端部处的中心冲头加宽。

    ASSEMBLY OF VANE UNITS
    40.
    发明申请
    ASSEMBLY OF VANE UNITS 审中-公开

    公开(公告)号：US20200256199A1

    公开(公告)日：2020-08-13

    申请号：US16645013

    申请日：2018-09-17

    申请人： SULZER TURBO SERVICES VENLO B.V.

    发明人： Jozef H.G. MATTHEIJ ,  Twan Antonius Martinus ALTHUIZEN

    IPC分类号： F01D5/24 ,  F01D25/24 ,  F01D9/04

    摘要： A vane assembly includes a plurality of vane units and a connecting part. Each vane unit includes a base having a through-hole positioned between opposing longitudinal faces of the base. The connecting part includes a lacing bar that is insertable into and through the through-holes for coupling at least two adjacent vane units into the vane assembly. In the vane assembly the connecting part is arranged through the through holes of the plurality of vane units clamping the vane units on the lacing bar.