Gas-path leakage seal for a gas turbine
    1.
    发明授权
    Gas-path leakage seal for a gas turbine 失效
    燃气轮机的气路泄漏密封

    公开(公告)号:US5657998A

    公开(公告)日:1997-08-19

    申请号:US572355

    申请日:1995-12-14

    摘要: A gas-path leakage seal for generally sealing a gas-path leakage-gap between spaced-apart first and second members of a gas turbine (such as first and second segments of a gas turbine combustor casing). The seal includes a generally imperforate foil-layer assemblage which is generally impervious to gas, is located in the leakage-gap, is spaced apart from the first member, and has a first foil layer. The seal also includes a cloth-layer assemblage contacting the first member and having a first cloth layer generally enclosing and generally enclosingly-contacting the foil-layer assemblage. The first foil layer is made from a metal, ceramic, and/or polymer. The first cloth layer is made from metal, ceramic, and/or polymer fibers. The foil assemblage provides for sealing and flexibility, and the cloth assemblage provides for wear resistance and flexibility. The seal accommodates different surface shapes, assembly misalignment, vibration, and differential thermal growth of the gas turbine members.

    摘要翻译: 一种用于大致密封燃气轮机(例如燃气轮机燃烧器壳体的第一和第二段)的间隔开的第一和第二构件之间的气体路径泄漏间隙的气体路径泄漏密封件。 密封件包括通常不透气体的通常无孔的箔层组合件,位于泄漏间隙中,与第一构件间隔开,并且具有第一箔层。 密封件还包括接触第一构件的布层组合件,并且具有通常包围并且大致封闭地接触箔层组合件的第一布层。 第一箔层由金属,陶瓷和/或聚合物制成。 第一布层由金属,陶瓷和/或聚合物纤维制成。 箔组合提供密封和柔性,布料组合提供耐磨性和柔韧性。 密封件适应燃气轮机构件的不同表面形状,组装不对准,振动和差热发展。

    Method for making a brush seal
    2.
    发明授权
    Method for making a brush seal 失效
    刷子密封方法

    公开(公告)号:US5678898A

    公开(公告)日:1997-10-21

    申请号:US425008

    申请日:1995-04-17

    IPC分类号: A46D1/08 F16J15/32

    CPC分类号: F16J15/3288 A46D1/08

    摘要: A method for making a brush seal includes weaving a single-layer bristle assemblage having two spaced-apart cloth segments joined together by an unwoven section wherein the two cloth segments and the unwoven section share a common first group of warp bristles and wherein the two cloth segments have different groups of weft bristles. The method further includes the step of cutting generally across the unwoven section of the first group of bristles to create free ends. The brush seal so made is useful, for example, to generally seal a leakage gap in a gas path of a gas turbine.

    摘要翻译: 制造刷子密封件的方法包括编织具有两个间隔开的布段的单层刷毛组合件,该织物组合件通过非织造部分连接在一起,其中两个织物段和非织造部分共享共同的第一组经向刷毛,并且其中两个布 片段有不同的纬纱组。 该方法还包括大致切割第一组刷毛组织的部分以产生自由端的步骤。 如此制造的刷密封件例如可用于大致密封燃气轮机的气体通道中的泄漏间隙。

    Positive biased packing ring brush seal combination
    4.
    发明授权
    Positive biased packing ring brush seal combination 有权
    正偏压填料环刷密封组合

    公开(公告)号:US06250641B1

    公开(公告)日:2001-06-26

    申请号:US09199730

    申请日:1998-11-25

    IPC分类号: F16J15447

    摘要: Circumferentially extending sealing segments (45) are disposed about a rotary component (16) and have seal face (34) carrying a plurality of labyrinth seal teeth (36) and a brush seal (37). The segments are movable between large and small clearance positions relative to the rotor at start-up and steady-state operating conditions, respectively. In one form, springs (31) bias the segments radially outwardly at start-up and steam pressure displaces the segments to the small clearance positions at steady-state operations. In a further embodiment, springs bias the segment for movement to the small clearance position, the extent of movement being determined by thermal expansion of centering rings mounting the segments to the stationary components.

    摘要翻译: 周向延伸的密封段(45)围绕旋转部件(16)设置并且具有承载多个迷宫式密封齿(36)和刷密封件(37)的密封面(34)。 分段在启动和稳态运行条件下分别相对于转子在大间隙位置和小间隙位置之间可移动。 在一种形式中,弹簧(31)在启动时径向向外偏压节段,并且在稳态操作时,蒸汽压将段移动到小间隙位置。 在进一步的实施例中,弹簧偏置该段用于移动到小间隙位置,移动的程度由通过将段安装到固定部件的定心环的热膨胀来确定。

    Brush seal segment
    5.
    发明授权
    Brush seal segment 失效
    刷子密封段

    公开(公告)号:US6105966A

    公开(公告)日:2000-08-22

    申请号:US131485

    申请日:1998-08-10

    CPC分类号: F16J15/3288

    摘要: A brush seal segment useful, when circumferentially arrayed with other such segments, to seal the gap between a rotor and a surrounding casing of a rotary machine such as a steam turbine. An annular backing plate has a rim radially-inwardly bounding together upstream-facing and downstream-facing surfaces. Canted bristles abut the upstream-facing surface. The rim is designed to allow the bristles to recover from a rotor rub. In one design, the rim acts as a labyrinth-seal tooth and is shaped to deform, under a radial force, longitudinally away from the upstream-facing surface. In another design, the rim has a more-inwardly projecting second portion near a radially-aligned edge, and only this second portion acts as a labyrinth-seal tooth.

    摘要翻译: 当用其它这种部分周向排列时,用于密封旋转机器(例如蒸汽轮机)的转子和周围壳体之间的间隙的刷密封段是有用的。 环形背板具有径向向内限定在一起的面向上游和下游的表面的边缘。 鬃毛紧靠着面向上游的表面。 轮辋旨在使刷毛从转子摩擦中恢复。 在一种设计中,轮辋用作迷宫式密封齿并且成形为在径向力作用下纵向远离上游侧表面变形。 在另一种设计中,轮辋在径向对齐的边缘附近具有更向内突出的第二部分,并且仅该第二部分用作迷宫式密封齿。

    Turbine brush seal protection device and method
    8.
    发明授权
    Turbine brush seal protection device and method 失效
    涡轮刷密封保护装置及方法

    公开(公告)号:US06206629B1

    公开(公告)日:2001-03-27

    申请号:US09376835

    申请日:1999-08-18

    IPC分类号: F01D4907

    CPC分类号: F16J15/3288 F16J15/3268

    摘要: A turbine brush seal protection device includes an annular substrate having an outer periphery and defining a slot open at the outer periphery. The slot is for receiving a portion of an annular brush seal of a gas turbine subassembly during installation of a gas turbine and such that the annular substrate at least partially covers the annular brush seal of the gas turbine subassembly. The annular substrate at the outer periphery and within the slot thereof is removably mounted to a stationary portion of the gas turbine subassembly. A turbine brush seal protection method includes the steps of providing the annular substrate, placing the annular substrate over a portion of an annular brush seal of a gas turbine subassembly such that the seal portion is inside the slot of the annular substrate during installation of a gas turbine and the annular substrate at least partially covers the annular brush seal of the gas turbine subassembly, mounting the annular substrate at the outer periphery and within the slot thereof to a stationary portion of the gas turbine subassembly, and removing the annular substrate from the stationary portion of the gas turbine subassembly before completion of installation of the gas turbine subassembly.

    摘要翻译: 涡轮刷密封保护装置包括具有外周边并限定在外周边开口的狭槽的环形基板。 所述槽用于在燃气轮机的安装期间接收燃气轮机子组件的环形刷密封件的一部分,并且使得环形衬底至少部分地覆盖燃气轮机子组件的环形刷密封。 在外周和其槽口内的环形基板可拆卸地安装到燃气轮机组件的固定部分。 涡轮刷密封保护方法包括以下步骤:提供环形基板,将环形基板放置在燃气轮机子组件的环形刷密封件的一部分上,使得密封部分在安装气体期间在环形基板的槽内 涡轮机和环形基板至少部分地覆盖燃气轮机子组件的环形刷密封件,将环形基板安装在外周边并且在其槽内,到燃气轮机子组件的固定部分,并将环形基板从固定件 在完成燃气轮机组件的安装之前,燃气轮机组件的一部分。