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    L brush seal for turbomachinery application
    3.
    发明授权
    L brush seal for turbomachinery application 有权
    L刷密封用于涡轮机械应用

    公开(公告)号：US09587505B2

    公开(公告)日：2017-03-07

    申请号：US14097753

    申请日：2013-12-05

    Applicant: General Electric Company

    Inventor： Debabrata Mukhopadhyay ,  Xiaoqing Zheng

    IPC: F01D11/08 ,  F16J15/32 ,  F01D11/00

    CPC classification number: F01D11/08 ,  F01D11/001 ,  F05D2240/56 ,  F16J15/3288 ,  F16J15/441 ,  F16J15/4472

    Abstract: A seal arrangement between radially-opposed rotating and stationary components in a turbomachine includes a first rotating component, a second stationary component, and a brush seal located radially therebetween. The brush seal has an axially-extending portion secured to the second stationary component, and an inwardly-extending portion extending across a gap between the first and second components. An inner ring portion of the second stationary component is located radially inward of, and in engagement with the axially-extending portion and at least part of the inwardly-extending portion of the brush seal, wherein an end of the axially-extending portion of the brush seal remote from the inwardly-extending portion is sandwiched between a pair of side rails fixed between the inner ring portion and an outer ring portion of the second stationary component.

    Abstract translation: 在涡轮机中的径向相对的旋转和静止部件之间的密封装置包括第一旋转部件，第二固定部件和径向位​​于其间的刷子密封件。 刷密封具有固定到第二固定部件的轴向延伸部分，以及延伸穿过第一和第二部件之间的间隙的向内延伸的部分。 第二固定部件的内环部分位于电刷密封件的轴向延伸部分和向内延伸部分的至少部分的径向内侧并与其接合，其中轴向延伸部分的端部 远离所述向内延伸部分的刷密封夹在固定在所述第二固定部件的所述内环部分和外环部分之间的一对侧轨之间。

    Individually compliant segments for split ring hydrodynamic face seal
    4.
    发明授权
    Individually compliant segments for split ring hydrodynamic face seal 有权
    单圈流体动力面密封单元

    公开(公告)号：US09534502B2

    公开(公告)日：2017-01-03

    申请号：US14226583

    申请日：2014-03-26

    Applicant: General Electric Company

    Inventor： Azam Mihir Thatte ,  Karimulla Shaik Sha ,  Rahul Anil Bidkar ,  Xiaoqing Zheng

    IPC: F01D11/00 ,  F01D1/04

    CPC classification number: F01D11/003 ,  F01D1/04 ,  F01D11/001 ,  F05D2220/31 ,  F05D2240/53 ,  Y02E20/16

    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。

    Rotary machine aspirating seal assembly and method of assembling the same
    6.
    发明授权
    Rotary machine aspirating seal assembly and method of assembling the same 有权
    旋转机吸气密封组件及其组装方法

    公开(公告)号：US09291067B2

    公开(公告)日：2016-03-22

    申请号：US14076982

    申请日：2013-11-11

    Applicant: General Electric Company

    Inventor： Xiaoqing Zheng ,  Norman Arnold Turnquist ,  Michael Dennis Mack ,  Rahul Anil Bidkar ,  Azam Mihir Thatte

    IPC: F01D11/00 ,  F01D11/02 ,  F16J15/34 ,  F16J15/44 ,  F16J15/00 ,  F16J15/447

    CPC classification number: F01D11/003 ,  F01D11/02 ,  F16J15/002 ,  F16J15/3404 ,  F16J15/3412 ,  F16J15/4472

    Abstract: An aspirating face seal for use with a rotary machine includes a rotating seal ring including a radially outer surface that includes an oblique portion. A stationary seal ring is coupled proximate the rotating seal ring such that a first gap is defined therebetween. The stationary seal ring is movable along a centerline axis of the rotary machine between an open position and a sealed position, and includes an extension member that extends across the first gap. An auxiliary seal includes at least one seal tooth that includes a seal tooth tip. The at least one seal tooth extends radially inward from the extension member such that a second gap is defined between the seal tooth tip and the oblique portion.

    Abstract translation: 与旋转机一起使用的抽吸面密封件包括旋转密封环，其包括包括倾斜部分的径向外表面。 固定密封环在旋转的密封环附近耦合，使得在其间限定第一间隙。 固定密封环可沿着旋转机器的中心线在打开位置和密封位置之间移动，并且包括延伸穿过第一间隙的延伸构件。 辅助密封件包括至少一个包括密封齿顶端的密封齿。 所述至少一个密封齿从所述延伸构件径向向内延伸，使得在所述密封齿顶部和所述倾斜部分之间限定第二间隙。

    SYSTEM AND METHOD FOR THRUST BEARING ACTUATION TO ACTIVELY CONTROL CLEARANCE IN A TURBO MACHINE
    7.
    发明申请
    SYSTEM AND METHOD FOR THRUST BEARING ACTUATION TO ACTIVELY CONTROL CLEARANCE IN A TURBO MACHINE 有权
    用于轴承动作的动力系统和方法，用于动力控制涡轮机间的间隙

    公开(公告)号：US20150247415A1

    公开(公告)日：2015-09-03

    申请号：US14193077

    申请日：2014-02-28

    Applicant: General Electric Company

    Inventor： Deepak Trivedi ,  Norman Arnold Turnquist ,  Xiaoqing Zheng ,  Murat Inalpolat

    IPC: F01D11/22 ,  F01D25/16 ,  F16C41/00

    CPC classification number: F01D11/22 ,  F01D3/00 ,  F01D17/26 ,  F01D21/08 ,  F01D25/16 ,  F16C17/04 ,  F16C41/004 ,  F16C2360/23

    Abstract: An actuation system to control clearance in a turbomachine including a shaft bearing including at least one axially displaceable thrust bearing. The axially displaceable thrust bearing configured to axially displace a rotating component relative to a stationary component to control the clearance therebetween. The system further including a plurality of actuators coupled to the at least one axially displaceable thrust bearing and configured to actuate the at least one axially displaceable thrust bearing to control the clearance. The plurality of actuators is configured to deactivate a diametrically opposed actuator in the event of an actuator failure to maintain zero moment. In a topography network, each diametrically opposed actuator pair is coupled to a single control line. In an alternate topography network, alternating actuators are coupled to a single control line. In addition, a method of actuating a thrust bearing to control clearance in a turbomachine is disclosed.

    Abstract translation: 一种用于控制涡轮机中的间隙的致动系统，包括具有至少一个可轴向移动的推力轴承的轴承座。 轴向移动推力轴承构造成相对于静止部件轴向移动旋转部件以控制它们之间的间隙。 所述系统还包括耦合到所述至少一个可轴向移动的推力轴承并被构造成致动所述至少一个可轴向移动的止推轴承以控制所述间隙的多个致动器。 多个致动器构造成在执行器失效以保持零时刻的情况下停用直径相对的致动器。 在地形网络中，每个直径相对的致动器对耦合到单个控制线。 在替代的地形网络中，交替的致动器耦合到单个控制线。 此外，公开了一种致动推力轴承以控制涡轮机中的间隙的方法。

    INTER-STAGE SEAL FOR A TURBOMACHINE
    8.
    发明申请
    INTER-STAGE SEAL FOR A TURBOMACHINE 审中-公开
    用于涡轮机的间歇式密封

    公开(公告)号：US20150071771A1

    公开(公告)日：2015-03-12

    申请号：US14025010

    申请日：2013-09-12

    Applicant: General Electric Company

    Inventor： Xiaoqing Zheng ,  Thomas Joseph Farineau ,  Revanth Krishna Nallam

    IPC: F01D11/00

    CPC classification number: F01D11/005 ,  F01D5/3007 ,  F01D11/001

    Abstract: An inter-stage seal for a turbomachine includes a sealing member extending from a first end to a second end through an intermediate portion having a sealing surface, a first mounting member extending from a first end portion coupled to the sealing member adjacent the first end to a second, cantilevered end portion having a first rotor mounting element, and a second mounting member extending from a first end portion coupled to the sealing member adjacent the second end to a second, cantilevered end portion having a second rotor mounting element.

    Abstract translation: 用于涡轮机的级间密封件包括密封构件，该密封构件从第一端延伸通过具有密封表面的中间部分延伸到第二端，第一安装构件从与第一端相邻的密封构件的第一端部延伸到 第二悬臂端部，其具有第一转子安装元件，以及第二安装构件，其从与第二端部相邻的密封构件的第一端部延伸到具有第二转子安装元件的第二悬臂端部。

    Systems and Methods for Reducing or Limiting One or More Flows Between a Hot Gas Path and a Wheel Space of a Turbine
    9.
    发明申请
    Systems and Methods for Reducing or Limiting One or More Flows Between a Hot Gas Path and a Wheel Space of a Turbine 审中-公开
    用于减少或限制涡轮机的热气道和车轮空间之间的一个或多个流量的系统和方法

    公开(公告)号：US20150040567A1

    公开(公告)日：2015-02-12

    申请号：US13962244

    申请日：2013-08-08

    Applicant: General Electric Company

    Inventor： Guoqiang Lu ,  Xiaoqing Zheng ,  Jong Youn Pak

    IPC: F01D11/02

    CPC classification number: F01D11/02 ,  F01D11/001

    Abstract: A turbine assembly is disclosed herein. The turbine assembly may include a rotor with at least one bucket extending radially therefrom. The turbine assembly also may include a stator assembly positioned adjacent to the at least one bucket. Moreover, the turbine assembly may include a seal assembly. The seal assembly may include a first flange extending in a substantially axial direction from the at least one bucket. The seal assembly also may include a second flange extending from the stator assembly in the substantially axial direction opposite the first flange. The second flange may include at least one protuberance projecting towards the first flange.

    Abstract translation: 本文公开了一种涡轮机组件。 涡轮机组件可以包括具有从其径向延伸的至少一个铲斗的转子。 涡轮机组件还可以包括邻近至少一个铲斗定位的定子组件。 此外，涡轮机组件可以包括密封组件。 密封组件可以包括从至少一个铲斗沿基本轴向方向延伸的第一凸缘。 密封组件还可以包括在与第一凸缘相对的基本轴向方向上从定子组件延伸的第二凸缘。 第二凸缘可以包括朝向第一凸缘突出的至少一个凸起。

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