Gland for transferring cooling medium to the rotor of a gas turbine
    11.
    发明授权
    Gland for transferring cooling medium to the rotor of a gas turbine 失效
    将冷却介质传送到燃气轮机的转子的压盖

    公开(公告)号:US5738488A

    公开(公告)日:1998-04-14

    申请号:US745542

    申请日:1996-11-12

    摘要: A gas turbine rotor steam gland includes a steam inlet supply scroll for supplying steam through radial slots to an axially extending passage in the rotor for steam cooling of hot gas path component parts. The scroll decreases in diameter in the circumferential direction of cooling medium flow to match its velocity with the surface speed of the rotor. An aft labyrinth seal is provided about the rotor. Forwardly of the scroll, a plurality of labyrinth-type seals are interspersed with extraction ports. The extraction ports, except for the final forwardmost extraction port, are maintained at a pressure below the pressure of the inlet supply steam whereby steam leakage past the seals flows into the extraction ports for removal. The final forward extraction port is maintained at sub-ambient pressure such that final steam leakage past the forward seals and ambient air leakage past the forwardmost seal combine and are extracted from the steam gland.

    摘要翻译: 燃气轮机转子蒸汽密封盖包括蒸汽入口供应涡卷,用于通过径向槽将蒸汽提供给转子中的轴向延伸的通道,用于蒸汽冷却热气体通道部件。 涡卷在冷却介质流动的圆周方向上的直径减小,以使其速度与转子的表面速度相匹配。 围绕转子设置了一个后迷宫密封。 对于涡卷,多个迷宫式密封件散布有抽出口。 除了最后的最前面的抽出口之外的抽出口保持在低于入口供应蒸汽的压力的压力,由此通过密封件的蒸汽泄漏流入萃取口以除去。 最后的前进提取口保持在低于环境压力,使得通过前密封件的最终蒸汽泄漏和通过最前面密封的环境空气泄漏结合在一起并从蒸汽密封管中取出。

    Method and apparatus for gas turbine engine temperature management
    12.
    发明授权
    Method and apparatus for gas turbine engine temperature management 有权
    燃气轮机发动机温度管理方法和装置

    公开(公告)号:US08517663B2

    公开(公告)日:2013-08-27

    申请号:US12241165

    申请日:2008-09-30

    IPC分类号: F02C7/18

    CPC分类号: F02C7/12 F02C7/18 F02C9/18

    摘要: A cooling system for a turbine engine, as well as a methodology for controlling the cooling system, is described. A valve member is disposed between a cooling fluid passage and a wheel space of the turbine engine and operates to admit cooling fluid to the wheel space for cooling thereof. The valve assembly is responsive to a condition in the wheel space and varies the flow of additional cooling fluid to the wheel space based on that condition.

    摘要翻译: 描述了一种用于涡轮发动机的冷却系统,以及用于控制冷却系统的方法。 阀构件设置在冷却流体通道和涡轮发动机的车轮空间之间,并且操作以将冷却流体接纳到车轮空间以进行冷却。 阀组件响应于车轮空间中的状况,并且基于该条件改变附加的冷却流体到车轮空间的流动。

    Method and Apparatus for Gas Turbine Engine Temperature Management
    13.
    发明申请
    Method and Apparatus for Gas Turbine Engine Temperature Management 有权
    燃气轮机发动机温度管理方法与装置

    公开(公告)号:US20100080685A1

    公开(公告)日:2010-04-01

    申请号:US12241165

    申请日:2008-09-30

    IPC分类号: F02C7/18

    CPC分类号: F02C7/12 F02C7/18 F02C9/18

    摘要: A cooling system for a turbine engine, as well as a methodology for controlling the cooling system, is described. A valve member is disposed between a cooling fluid passage and a wheel space of the turbine engine and operates to admit cooling fluid to the wheel space for cooling thereof. The valve assembly is responsive to a condition in the wheel space and varies the flow of additional cooling fluid to the wheel space based on that condition.

    摘要翻译: 描述了一种用于涡轮发动机的冷却系统,以及用于控制冷却系统的方法。 阀构件设置在冷却流体通道和涡轮发动机的车轮空间之间,并且操作以将冷却流体接纳到车轮空间以进行冷却。 阀组件响应于车轮空间中的状况,并且基于该条件改变附加的冷却流体到车轮空间的流动。

    Axial and circumferential seal for stacked rotor and/or stator assembly
    16.
    发明申请
    Axial and circumferential seal for stacked rotor and/or stator assembly 失效
    用于堆叠转子和/或定子组件的轴向和周向密封

    公开(公告)号:US20070110567A1

    公开(公告)日:2007-05-17

    申请号:US11270925

    申请日:2005-11-11

    IPC分类号: F04D29/08

    摘要: Disclosed herein is a rotor assembly for a steam turbine including a stacked rotor section having rotor plates. The rotor plates include a main body portion having a plate shape and a first axial face and a second axial face opposite to the first axial face. The rotor plates also include an airfoil base surface at an outer radial edge of the main body portion. The rotor plates further include buckets which extend radially outward from the airfoil base surface. And the rotor plates yet further include a seal disposed to prevent steam exposure to the first and second axial faces.

    摘要翻译: 本文公开了一种用于蒸汽轮机的转子组件,其包括具有转子板的堆叠转子部分。 转子板包括具有板形状的主体部分和与第一轴向面相对的第一轴向面和第二轴向面。 转子板还包括在主体部分的外径向边缘处的翼型件基面。 转子板还包括从翼型件基部表面径向向外延伸的铲斗。 并且转子板还包括设置成防止蒸汽暴露于第一和第二轴向面的密封件。

    Methods and apparatus for integral radial leakage seal
    17.
    发明授权
    Methods and apparatus for integral radial leakage seal 失效
    一体式径向泄漏密封的方法和装置

    公开(公告)号:US06877956B2

    公开(公告)日:2005-04-12

    申请号:US10328053

    申请日:2002-12-23

    IPC分类号: F01D5/22 F01D11/00

    摘要: A method and apparatus for fabricating a rotor assembly for a turbine is provided. The method includes forming a cover on each bucket radial tip wherein the cover includes a leading edge side in a direction of rotation, and a trailing edge side in the direction of rotation wherein the leading edge and trailing edges are parallel with respect to each other, and wherein the leading edge and trailing edges are skewed with respect to the axis of rotation. The method includes forming an extension in the cover leading edge side, forming a groove in the cover trailing edge side, and attaching each bucket to the radially outer rim, such that the extension in the cover leading edge side of one cover is in mating engagement with the groove in the cover trailing edge side of an adjoining cover.

    摘要翻译: 提供了一种用于制造用于涡轮机的转子组件的方法和装置。 该方法包括在每个铲斗径向末端上形成盖,其中盖包括沿旋转方向的前缘侧和沿着旋转方向的后缘侧,其中前缘和后缘相对于彼此平行, 并且其中前缘和后缘相对于旋转轴线倾斜。 该方法包括在盖引导边缘侧形成延伸部,在盖后缘侧形成槽,并将每个铲斗附接到径向外缘,使得一个盖的盖前缘侧的延伸部配合接合 其中凹槽位于相邻盖的盖后缘侧。

    Method and apparatus for turbomachine active clearance control
    18.
    发明申请
    Method and apparatus for turbomachine active clearance control 有权
    用于涡轮机主动间隙控制的方法和装置

    公开(公告)号:US20050069406A1

    公开(公告)日:2005-03-31

    申请号:US10675364

    申请日:2003-09-30

    IPC分类号: F01D11/20 F01D11/22 F01D1/00

    摘要: An apparatus for providing active clearance control between blade tips and seals in a turbomachine comprising: a first stator carrier segment, with stator seals centripetally disposed on it; a second stator carrier segment located along a same circumference as the first stator carrier segment, also with stator seals centripetally disposed on it; a shell that adjustably houses the first stator carrier segment and the second carrier segment; at least one displacement apparatus in operable communication with at least one stator carrier segment and configured to position the at least one stator carrier segment to provide active clearance control to the stator seals disposed on the at least one stator carrier segment.

    摘要翻译: 一种用于在涡轮机中的叶片尖端和密封之间提供主动间隙控制的装置,包括:第一定子承载段,定子密封件向心地设置在其上; 沿与第一定子承载段相同的圆周定位的第二定子载体段,其中定子密封件向心地设置在其上; 壳体,其可调节地容纳所述第一定子承载段和所述第二载体段; 至少一个位移设备,其与至少一个定子承载段可操作地连通并且被配置为定位所述至少一个定子承载段,以对设置在所述至少一个定子承载段上的所述定子密封件提供主动间隙控制。