Brush seal for high-pressure rotor applications
    31.
    发明授权
    Brush seal for high-pressure rotor applications 失效
    用于高压转子应用的刷子密封

    公开(公告)号:US6079945A

    公开(公告)日:2000-06-27

    申请号:US967640

    申请日:1997-11-10

    CPC分类号: F01D11/005 F16J15/3288

    摘要: A brush seal, which may be used in gas or steam turbine rotor applications, includes a packet of bristles attached to a seal housing. A seal member is slideably-attached to the seal housing, has a planar first surface portion parallel to, and slideably in contact with, a first surface of the seal housing, and has a planar second surface portion which is parallel to, and slideably in contact with, a first side of the bristle packet. A mechanical spring is positioned in compression between the seal housing and the seal member.

    摘要翻译: 可用于气体或汽轮机转子应用中的刷子密封件包括附接到密封壳体的刷毛包。 密封构件可滑动地附接到密封壳体,具有与密封壳体的第一表面平行并可滑动地接触的平面第一表面部分,并且具有平坦的第二表面部分,其平行于并可滑动地 与刷毛包的第一面接触。 机械弹簧被定位在密封壳体和密封构件之间的压缩中。

    OIL WATER SEPARATION APPARATUS
    35.
    发明申请
    OIL WATER SEPARATION APPARATUS 审中-公开
    油水分离装置

    公开(公告)号:US20100326922A1

    公开(公告)日:2010-12-30

    申请号:US12492219

    申请日:2009-06-26

    摘要: In one aspect, the present invention provides a subsea separation vessel for the separation of a mixture comprising oil and water comprising (a) at least one inlet for introducing a oil-water mixture; (b) a flow path for conducting the oil-water mixture; (c) at least one oil-water separation structure; and (d) at least one fluid outlet. The oil-water separation structure includes a multifunctional surface. The oil-water separation structure is located within the flow path and wherein the multifunctional surface is superhydrophobic with respect to water, and either oleophilic or superoleophilic with respect to oil. A method for separating oil from an oil-water mixture is also provided.

    摘要翻译: 一方面,本发明提供了一种用于分离包含油和水的混合物的海底分离容器,其包括(a)用于引入油 - 水混合物的至少一个入口; (b)用于引导油水混合物的流路; (c)至少一个油水分离结构; 和(d)至少一个流体出口。 油水分离结构包括多功能表面。 油水分离结构位于流路内,其中多功能表面相对于水是超疏水的,并且相对于油是亲油的或超亲油的。 还提供了一种从油水混合物中分离油的方法。

    Cooling Circuit for Enhancing Turbine Performance
    36.
    发明申请
    Cooling Circuit for Enhancing Turbine Performance 审中-公开
    用于提高涡轮机性能的冷却回路

    公开(公告)号:US20090074589A1

    公开(公告)日:2009-03-19

    申请号:US11856945

    申请日:2007-09-18

    IPC分类号: F01D5/08

    CPC分类号: F02C7/12 F01D25/12

    摘要: In a gas turbine having a compressor discharge casing, a cooling circuit diverts compressor discharge air toward a high pressure packing (HPP) circuit. The cooling circuit includes an inlet pipe that receives compressor discharge air. One or several cooled cooling air pipes are in fluid communication with the inlet pipe via a pipe manifold, which distributes the discharge air across the cooled cooling air pipes. A seal is disposed upstream of an entrance to the HPP circuit to limit flow into the HPP circuit, and a second seal is disposed downstream of the HPP circuit at turbine wheelspace to limit ingestion and thus the purge flow air required. The circuit serves to reduce required purge flow in the HPP circuit so that an amount of compressor discharge air can be put back to the main flow path, thereby improving turbine performance.

    摘要翻译: 在具有压缩机排放壳体的燃气轮机中,冷却回路将压缩机排出的空气转向高压包装(HPP)回路。 冷却回路包括接收压缩机排出空气的入口管。 一个或几个冷却的冷却空气管通过管道歧管与入口管流体连通,管道歧管将排放空气分配在冷却的冷却空气管道上。 密封件设置在HPP回路入口的上游,以限制流入HPP回路的第二密封件,并且在涡轮机轮距处设置在HPP回路下游的第二密封件,以限制摄入量,从而限制吸入流量所需的空气流量。 该电路用于减少HPP电路中所需的清洗流量,使得压缩机排出空气的量可以放回到主流路,从而提高涡轮机性能。

    Angel wing abradable seal and sealing method
    37.
    发明授权
    Angel wing abradable seal and sealing method 有权
    天使翼可靠密封和密封方法

    公开(公告)号:US07500824B2

    公开(公告)日:2009-03-10

    申请号:US11507562

    申请日:2006-08-22

    IPC分类号: F01D11/00

    CPC分类号: F01D11/001 F01D11/02

    摘要: An abradable seal is provided to improve turbine performance by physically reducing the clearance between a flange portion of the nozzle and an opposed angel wing/seal plate member of the bucket. The provision of an abradable seal also mitigates angel wing/seal plate tooth or fin wear by providing for abradable contact without metal to metal hard rub.

    摘要翻译: 提供可磨损密封件以通过物理地减小喷嘴的凸缘部分和铲斗的相对的天使翼/密封板构件之间的间隙来改善涡轮机性能。 提供可磨损的密封件还通过提供无磨损的接触而减轻天使翼/密封板的齿或翅片磨损,而不会金属与金属的硬摩擦。

    Brush seal arrangement for high pressure applications
    38.
    发明授权
    Brush seal arrangement for high pressure applications 有权
    用于高压应用的刷子密封装置

    公开(公告)号:US06790001B2

    公开(公告)日:2004-09-14

    申请号:US10301586

    申请日:2002-11-22

    IPC分类号: F01D1100

    摘要: In a steam turbine high pressure end seal region, brush seals are provided between first and second pressure regions having a pressure drop in excess of the sealing capacity of an individual brush seal. To use brush seals between the first and second regions, one or more intermediate pressure regions are maintained at a substantially fixed predetermined pressure between the first and second pressure regions. Brush seals are interposed between adjacent pressure regions whereby the pressure drop between adjacent pressure regions is within the sealing capacity of the individual brush seal disposed between the adjacent pressure regions.

    摘要翻译: 在汽轮机高压端部密封区域中,刷密封件设置在第一压力区域和第二压力区域之间,压力区域的压降超过单个刷子密封件的密封能力。 为了在第一和第二区域之间使用刷子密封,一个或多个中间压力区域保持在第一和第二压力区域之间基本上固定的预定压力。 刷子密封件插入在相邻的压力区域之间,由此相邻压力区域之间的压降在设置在相邻的压力区域之间的单个刷子密封件的密封能力内。