Turbine casing clearance management system

    公开(公告)号:US09683453B2

    公开(公告)日:2017-06-20

    申请号:US14023582

    申请日:2013-09-11

    CPC classification number: F01D11/22 F05D2220/31 Y02E20/16

    Abstract: Systems and devices configured to reduce thermal design clearances (e.g., between stationary nozzles connected to the inner casing and rotor buckets connected to the rotor) in turbines by actively controlling casing movements and/or locations during turbine operation are disclosed. In one embodiment, a clearance management system includes: a first inner casing support arm shaped to connect to an inner casing of a turbine and extend through an outer casing of the turbine; a seal system disposed about the first inner casing support arm and configured to connect to the outer casing; and a set of actuators disposed on a turbine foundation of the turbine and connected to the first inner casing support arm, the set of actuators located external to the outer casing and configured to adjust a position of the inner casing relative to the outer casing via manipulation of the first inner casing support arm.

    FACE SEAL WITH LOCALLY COMPLIANT HYDRODYNAMIC PADS
    17.
    发明申请
    FACE SEAL WITH LOCALLY COMPLIANT HYDRODYNAMIC PADS 有权
    具有局部合适的水动力垫的表面密封

    公开(公告)号:US20150275685A1

    公开(公告)日:2015-10-01

    申请号:US14226617

    申请日:2014-03-26

    CPC classification number: F01D11/001 F01D1/04 F01D11/003 F01D25/22 F05D2220/31

    Abstract: Embodiments of the present disclosure are directed toward a stator ring configured to be disposed about a rotor of a turbine, wherein the stator ring comprises a plurality of hydrodynamic pads extending from a sealing face of the stator ring, wherein each of the plurality of hydrodynamic pads is configured to hydrodynamically engage with a rotor ring.

    Abstract translation: 本公开的实施例涉及一种被配置为围绕涡轮机的转子设置的定子环,其中定子环包括从定子环的密封面延伸的多个流体动力垫,其中多个流体动力垫 构造成与转子环流体动力接合。

    INDIVIDUALLY COMPLIANT SEGMENTS FOR SPLIT RING HYDRODYNAMIC FACE SEAL
    18.
    发明申请
    INDIVIDUALLY COMPLIANT SEGMENTS FOR SPLIT RING HYDRODYNAMIC FACE SEAL 有权
    分离环水动力面密封件的独立部分

    公开(公告)号:US20150275684A1

    公开(公告)日:2015-10-01

    申请号:US14226583

    申请日:2014-03-26

    Abstract: Embodiments of the present disclosure are directed toward a face seal including a stator ring configured to be disposed about a rotor of a turbine, wherein stator ring comprises a first ring segment and a second ring segment configured to cooperatively form the stator ring, wherein the first and second ring segments are circumferentially split and have at least one bearing element disposed between the first and second ring segments, and wherein the at least one bearing element is configured to enable relative axial motion between the first and second ring segments at interfaces between the first and second ring segments

    Abstract translation: 本公开的实施例涉及一种面密封件,其包括构造成围绕涡轮机的转子设置的定子环,其中定子环包括构造成协同地形成定子环的第一环段和第二环段,其中第一 并且第二环段被周向地分开并且具有设置在第一和第二环段之间的至少一个轴承元件,并且其中所述至少一个轴承元件构造成使得能够在第一和第二环段之间的界面处的第一和第二环段之间的相对轴向运动 和第二环段

    AXIALLY FACED SEAL SYSTEM
    19.
    发明申请
    AXIALLY FACED SEAL SYSTEM 审中-公开
    轴向密封系统

    公开(公告)号:US20150167486A1

    公开(公告)日:2015-06-18

    申请号:US14104155

    申请日:2013-12-12

    CPC classification number: F01D11/08 F01D5/225 F01D11/003 Y02E20/16

    Abstract: A first aspect of the invention provides an axially faced seal system for a radial tip of a turbine component, the system comprising: a stationary turbine component; a rotating turbine component; and a seal ring mounted to the stationary turbine component, the seal ring extending axially to the rotating turbine component and engaging the rotating turbine component on a side surface, wherein the side surface of the rotating turbine component is on a continuous, rotating mating ring having a 360 degree arc.

    Abstract translation: 本发明的第一方面提供了一种用于涡轮机部件的径向末端的轴向面密封系统,该系统包括:固定涡轮机部件; 旋转涡轮机部件; 以及密封环,其安装到所述固定涡轮机部件,所述密封环轴向延伸到所述旋转的涡轮机部件并且在侧表面上与所述旋转的涡轮机部件接合,其中所述旋转涡轮机部件的侧表面在连续的旋转配合环上, 360度弧。

    ROTOR COOLING
    20.
    发明申请
    ROTOR COOLING 有权
    转子冷却

    公开(公告)号:US20150132107A1

    公开(公告)日:2015-05-14

    申请号:US14079610

    申请日:2013-11-13

    CPC classification number: F01D5/085 F01D11/02 F01D25/12 Y02T50/676

    Abstract: Embodiments of the invention relate generally to rotor cooling and, more particularly, to a stator member having at least one passage for the delivery of cooling steam to a bucket root. In one embodiment, the invention provides a turbine comprising: a rotor including a first bucket root; and a stator member having: a rotor bore within which at least a portion of the rotor is disposed; a facing end adjacent to the first bucket root of the rotor; a plurality of seals within the rotor bore for sealing against the rotor, the plurality of seals including a first seal nearest the facing end and a second seal adjacent to the first seal; and a plurality of passages, each extending from a surface of the rotor bore at a point between the first seal and the second seal and extending through the facing end.

    Abstract translation: 本发明的实施方案大体上涉及转子冷却,更具体地,涉及具有用于将冷却蒸汽输送到铲斗根部的至少一个通道的定子构件。 在一个实施例中,本发明提供一种涡轮机,包括:转子,其包括第一铲斗根部; 以及定子构件,其具有:转子孔,所述转子的至少一部分设置在所述转子孔内; 靠近转子的第一铲斗根部的面对端; 所述转子孔内的多个密封件用于密封所述转子,所述多个密封件包括最靠近所述端部的第一密封件和邻近所述第一密封件的第二密封件; 以及多个通道,每个通道在第一密封件和第二密封件之间的点处从转子孔的表面延伸并延伸穿过相对端。

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