Low leakage snout sealing system
    5.
    发明授权
    Low leakage snout sealing system 失效
    低泄漏口密封系统

    公开(公告)号:US06454270B1

    公开(公告)日:2002-09-24

    申请号:US09737088

    申请日:2000-12-14

    IPC分类号: F16J1508

    CPC分类号: F16J15/28

    摘要: A low leakage sealing system is provided between a steam pipe and a housing comprised of a pair of shells and a nozzle box movable relative to one another. The sealing system includes large and small diameter sealing rings engaging the pipe and shells or nozzle box and a secondary sealing element disposed between the sealing rings and one of the pipe and shells or nozzle box. The sealing elements comprise frustoconical elements having curved end surfaces forming primary seals with the sealing rings and the housing. In another form, the sealing system includes annular carrier elements having radially opening cavities for receiving sealing rings engageable with the pipe and housing, respectively. The carrier elements are axially spaced from a plurality of sealing rings to provide the low leakage sealing system.

    摘要翻译: 在蒸汽管和由一对壳体组成的壳体和可相对于彼此移动的喷嘴箱之间提供低泄漏密封系统。 密封系统包括与管和壳或喷嘴箱接合的大直径和小直径的密封环,以及设置在密封环与管和壳或喷嘴箱中的一个之间的次级密封元件。 密封元件包括具有弯曲端面的截头圆锥元件,其形成具有密封环和壳体的主密封。 在另一种形式中,密封系统包括具有径向开口腔的环形载体元件,用于接收分别与管道和壳体接合的密封环。 载体元件与多个密封环轴向间隔开以提供低泄漏密封系统。

    Brush seal with positive adjustable clearance control
    7.
    发明授权
    Brush seal with positive adjustable clearance control 失效
    刷子密封带正向可调节间隙控制

    公开(公告)号:US06435514B1

    公开(公告)日:2002-08-20

    申请号:US09736705

    申请日:2000-12-15

    IPC分类号: F16J1544

    CPC分类号: F16J15/3288 F16J15/445

    摘要: The positions of brush seal segments are positively adjusted relative to a housing carrying the brush seal segments and the opposing sealing component by employing members formed of thermally responsive material. The members are heated by heating elements receiving controlled power. By increasing or decreasing the power provided to the heating elements, the members are expanded or contracted to move the brush seal segments toward or away from the opposing sealing component.

    摘要翻译: 相对于通过使用由热响应材料形成的构件,承载刷密封段和相对密封构件的外壳,刷密封段的位置被积极地调整。 这些构件由受到受控制动力的加热元件加热。 通过增加或减少提供给加热元件的功率,这些构件被膨胀或收缩以将刷子密封段朝向或远离相对的密封部件移动。

    Rotary machine having a seal assembly
    8.
    发明授权
    Rotary machine having a seal assembly 有权
    具有密封组件的旋转机器

    公开(公告)号:US06340286B1

    公开(公告)日:2002-01-22

    申请号:US09472916

    申请日:1999-12-27

    IPC分类号: F01D1108

    摘要: A rotary machine includes a rotatable rotor, blades radially mounted on and spaced apart about the rotor, a stationary casing disposed about and radially outward from the rotor and blades defining an annular gap between the casing and tips of the blades, and a flexible abradable seal assembly attached on the casing and disposed within the annular gap such that during differential growth of the rotor and blades relative to the casing the seal assembly flexes and abrades in response to contact by the blade tips and thereby clearance between the casing and blade tips is controlled as to avoid contact by the moving blade tips with the casing.

    摘要翻译: 旋转机器包括可转动的转子,径向安装在转子周围和间隔开的叶片;固定壳体,其设置在转子周围并径向向外,并且在叶片的外壳和顶端之间限定环形间隙,以及柔性可磨损密封件 组件附接在壳体上并且设置在环形间隙内,使得在转子和叶片相对于壳体的差别生长期间,密封组件响应于叶片尖端的接触而弯曲和磨损,从而控制壳体和叶片尖端之间的间隙 以避免活动叶片尖端与壳体接触。

    Supplemental seal for the chordal hinge seals in a gas turbine
    9.
    发明授权
    Supplemental seal for the chordal hinge seals in a gas turbine 失效
    燃气轮机中的弦铰链密封的补充密封

    公开(公告)号:US06752592B2

    公开(公告)日:2004-06-22

    申请号:US10029003

    申请日:2001-12-28

    IPC分类号: F01D904

    摘要: In a gas turbine having a chordal hinge seal between an inner rail of each nozzle segment and an annular axially facing sealing surface of a nozzle support ring, a supplemental seal is disposed between the support ring and inner bands of the nozzle segments on a lower pressure side of the chordal hinge seals. To minimize or prevent leakage flow across the chordal hinge seals, a generally U-shaped supplemental seal having reversely folded U-shaped marginal portions is received in a cavity formed in the axially extending sealing surface of the inner rail of the nozzle segment. At operating conditions, the marginal portions seal against the base of the cavity and the annular sealing surface of the nozzle support ring to prevent leakage flow past the chordal hinge seal from entering the hot gas path. To install the supplemental seal, the seal is first compressed and maintained in a compressed state by applying one or more wraps about the supplemental seal or an epoxy to secure the seal when compressed in the cavity. At operating temperatures, the retention means releases the seal to engage marginal portions against opposite sealing surfaces of the nozzle segment and support ring.

    摘要翻译: 在具有在每个喷嘴段的内轨道和喷嘴支撑环的环形轴向面对的密封表面之间具有弦状铰链密封件的燃气涡轮机中,在较低压力下在支撑环和喷嘴段的内带之间设置补充密封 侧面铰链密封。 为了最小化或防止跨弦铰链密封件的泄漏流动,具有反向折叠的U形边缘部分的大致U形补充密封件容纳在形成在喷嘴段的内轨道的轴向延伸的密封表面中的空腔中。 在操作条件下,边缘部分密封在空腔的底部和喷嘴支撑环的环形密封表面上,以防止通过弦状铰链密封件的泄漏流进入热气路径。 为了安装补充密封件,首先将密封件压缩并保持在压缩状态,通过在补充密封件或环氧树脂周围施加一个或多个包装件以在压缩在空腔中时固定密封件。 在操作温度下,保持装置释放密封件以将边缘部分接合在喷嘴段和支撑环的相对的密封表面上。