Retrofitting methods and devices for large steam turbines
    1.
    发明授权
    Retrofitting methods and devices for large steam turbines 有权
    大型蒸汽轮机的改装方法和装置

    公开(公告)号:US09328612B2

    公开(公告)日:2016-05-03

    申请号:US13631882

    申请日:2012-09-29

    Abstract: A method of replacing rotating metal blades of a steam turbine inserted into a rotor having one or more existing grooves for inserting root sections of the metal blades is described, the method including the steps of providing replacement blades having radially inwards directed root sections of fiber-reinforced composite material, changing the shape of the one or more grooves in the rotor to form a cavity for the insertion of the root sections of fiber-reinforced composite material and inserting the replacement blades into the rotor.

    Abstract translation: 描述了一种替代插入转子的旋转金属叶片的方法,所述旋转金属叶片具有用于插入金属叶片根部的一个或多个现有凹槽,该方法包括以下步骤:提供具有径向向内定向的纤维 - 改变转子中的一个或多个槽的形状,以形成用于插入纤维增强复合材料的根部的空腔并将替换叶片插入转子中。

    Control system for an axial flow turbine

    公开(公告)号:US09638053B2

    公开(公告)日:2017-05-02

    申请号:US13903274

    申请日:2013-05-28

    Abstract: The invention relates to an axial flow turbine and method of operating thereof. The turbine comprises a last stage of rotating blades located towards a downstream end of the turbine having a distal region at an end of the airfoil of the blades. A monitoring control system has at least one sensor in the distal region of at least one last stage blade for measuring at least one physical property of the airfoil and a control element that is capable of influencing at least one physical property of the distal region. The control system further includes a controller that adjusts the control element based on at least measured physical property so by controlling the at least one physical property.

    CONTROL SYSTEM FOR AN AXIAL FLOW TURBINE
    3.
    发明申请
    CONTROL SYSTEM FOR AN AXIAL FLOW TURBINE 有权
    轴流式涡轮机控制系统

    公开(公告)号:US20130323054A1

    公开(公告)日:2013-12-05

    申请号:US13903274

    申请日:2013-05-28

    Abstract: The invention relates to an axial flow turbine and method of operating thereof. The turbine comprises a last stage of rotating blades located towards a downstream end of the turbine having a distal region at an end of the airfoil of the blades. A monitoring control system has at least one sensor in the distal region of at least one last stage blade for measuring at least one physical property of the airfoil and a control element that is capable of influencing at least one physical property of the distal region. The control system further includes a controller that adjusts the control element based on at least measured physical property so by controlling the at least one physical property.

    Abstract translation: 本发明涉及一种轴流涡轮机及其操作方法。 涡轮机包括位于涡轮的下游端的旋转叶片的最后一级,其具有在叶片的翼型的端部处的远侧区域。 监视控制系统在至少一个最后一级叶片的远侧区域中具有至少一个传感器,用于测量翼型件的至少一个物理特性和能够影响远端区域的至少一个物理特性的控制元件。 所述控制系统还包括控制器,所述控制器基于至少所测量的物理属性来调节所述控制元件,从而通过控制所述至少一个物理属性。

    Rotor blade with edge protection
    4.
    发明授权

    公开(公告)号:US09803483B2

    公开(公告)日:2017-10-31

    申请号:US14925059

    申请日:2015-10-28

    CPC classification number: F01D5/28 F01D5/147 F01D5/282 F01D5/286 F05D2250/38

    Abstract: The invention relates to sheath for a blade that has a uniform assembly direction over the radial height of the sheath whether the blade has a straight or curved trajectory. This is achieved by the a sheath formed around the edge, having a first inner surface wherein a first tangential vector projected tangentially to the first inner surface in a direction away from the head portion in an longitudinal plain forms a first angle with the rotational axis that does not vary over the radial height of the sheath while a second tangential vector projected tangentially from any point of the second inner surface of the sheath in a direction towards the head portion intersects the first tangential vector.

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