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    METHOD FOR ON-LINE DETECTION OF RESISTANCE-TO-GROUND FAULTS IN ACTIVE MAGNETIC BEARING SYSTEMS
    1.
    发明申请
    METHOD FOR ON-LINE DETECTION OF RESISTANCE-TO-GROUND FAULTS IN ACTIVE MAGNETIC BEARING SYSTEMS 审中-公开
    主动磁轴承系统中电阻对地面故障的在线检测方法

    公开(公告)号：WO2013109235A2

    公开(公告)日：2013-07-25

    申请号：PCT/US2011/066460

    申请日：2011-12-21

    Applicant: DRESSER-RAND COMPANY ,  GILARRANZ, Jose L. ,  GRIFFIN, Timothy R.

    Inventor： GILARRANZ, Jose L. ,  GRIFFIN, Timothy R.

    IPC: G01R27/20 ,  F16C32/04 ,  G01R31/34

    CPC classification number: H02K7/09 ,  F16C32/0442 ,  F16C37/005 ,  F16C2360/44 ,  F16C2380/26 ,  G01M13/04 ,  G01R31/025 ,  G01R31/343

    Abstract: A magnetic bearing is disclosed that includes a sensing wire wrapped around one or more of the bearing coils and configured to measure the resistance to ground of each bearing coil. With the presence of contaminants such as liquids, a protective coating disposed about the bearing coils degrades over time, thereby reducing the resistance to ground of the bearing coils. The sensing wire transmits the detected resistance to ground of the bearing coils to an adjacent sensing device, which can provide an output that informs a user whether corrective action is required to prevent damage or failure of the magnetic bearing.

    Abstract translation: 公开了一种磁性轴承，其包括缠绕在一个或多个轴承线圈上并且被配置为测量每个轴承线圈的接地阻力的感测线。 随着诸如液体的污染物的存在，围绕轴承线圈布置的保护涂层随着时间的推移而降低，从而降低了轴承线圈的接地阻力。 感测线将检测到的抵抗轴承线圈的电阻传递到相邻的感测装置，该感测装置可以提供输出，通知用户是否需要纠正动作以防止磁性轴承的损坏或故障。

    SYSTEM AND METHOD FOR COOLING A FLUIDIZED CATALYTIC CRACKING EXPANDER
    2.
    发明申请
    SYSTEM AND METHOD FOR COOLING A FLUIDIZED CATALYTIC CRACKING EXPANDER 审中-公开
    用于冷却流化催化裂化膨胀机的系统和方法

    公开(公告)号：WO2017136625A1

    公开(公告)日：2017-08-10

    申请号：PCT/US2017/016348

    申请日：2017-02-03

    Applicant: DRESSER-RAND COMPANY

    Inventor： GRIFFIN, Timothy R. ,  SEAMON, George H. ,  VACHON, Nicholas

    IPC: F01D5/08 ,  F01D5/30 ,  F01D11/00

    CPC classification number: F01D5/081 ,  C10G11/18 ,  C10G75/00 ,  C10G2300/4006 ,  F01D5/082 ,  F01D5/3038 ,  F01D11/001 ,  F01D11/006 ,  F01D25/24 ,  F05D2230/60 ,  F05D2260/22141

    Abstract: System and method for cooling an expander (100) rotor assembly. The system may include an annular body (148) disposed on a rotor disc (128) of the rotor assembly (118). The rotor disc (128) may also include a plurality of rotor blades (140) mounted thereto via respective roots (142). The annular body may define at least one fluid passageway fluidly coupling the roots (142) and the cooling source (112). The annular ring (148) may be configured to prevent mixing of the flue gas (F) with a coolant (C) provided by the cooling source (112) and flowing through the at least one fluid passageway and contacting at least one root (142). The system may also include a plurality of seal members (192, 292), each disposed between respective platforms (146) of adjacent rotor blades (140) and configured to prevent flue gas (F) flowing though the expander (100) from mixing with the coolant (C).

    Abstract translation: 用于冷却膨胀机（100）转子组件的系统和方法。 该系统可以包括设置在转子组件（118）的转子盘（128）上的环形主体（148）。 转子盘（128）还可以包括经由相应的根部（142）安装到其上的多个转子叶片（140）。 环形主体可限定流体地联接根部（142）和冷却源（112）的至少一个流体通道。 环形环（148）可构造成防止烟道气（F）与由冷却源（112）提供的冷却剂（C）混合并流过至少一个流体通道并接触至少一个根部（142 ）。 该系统还可以包括多个密封构件（192,292），每个密封构件设置在相邻转子叶片（140）的相应平台（146）之间并且被配置为防止流过膨胀器（100）的烟道气（F）与 冷却液（C）。

    TURBINES AND CORRESPONDING METHOD OF DAMPENING
    3.
    发明申请
    TURBINES AND CORRESPONDING METHOD OF DAMPENING 审中-公开

    公开(公告)号：WO2020190280A1

    公开(公告)日：2020-09-24

    申请号：PCT/US2019/022901

    申请日：2019-03-19

    Applicant: DRESSER-RAND COMPANY

    Inventor： ALIUDDIN, Atif Muhammad ,  VACHON, Nicholas ,  SHERLOCK, Graham D. ,  GRIFFIN, Timothy R.

    IPC: F01D5/22 ,  F01D11/00 ,  F01D5/30

    Abstract: A turbine (10) includes a disk (25) having a plurality of protrusions (120) arranged such that any two adjacent protrusions (120) define an axial entry fir tree space (125), each protrusion (120) defining an outermost lobe (165) having an outermost surface (150) and an axial length. A turbine blade (30) includes an airfoil (170), a platform (175), and a blade root (180) having a fir tree arranged to engage a leading protrusion (135) and a trailing protrusion (140). The blade root (180) and the leading protrusion (135) cooperate to define a leading gap (200), and the blade root (180) and the trailing protrusion (140) cooperate to define a trailing gap (215). A leading plug (220) is disposed in the leading gap (200) and a trailing plug (225) is disposed in the trailing gap (215). Each of the leading plug (220) and the trailing plug (225) have a plug (220) length that is at least as great as the axial length.

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