CLUTCH WITH SWIRL BREAKS
    4.
    发明申请

    公开(公告)号:US20200347892A1

    公开(公告)日:2020-11-05

    申请号:US16401044

    申请日:2019-05-01

    Abstract: A clutch system configured to transmit torque between an input shaft and an output shaft. The clutch system includes a clutch. The clutch includes: an input portion disposed at an end of the input shaft; an output portion disposed at an end of the output shaft; a sliding component that slides axially between the input and output portions to engage the clutch; and swirl breaks. The input portion, the output portion, and the sliding component each comprises walls. The swirl breaks are affixed to a one of the walls.

    Turbomachine having swirl-inhibiting seal
    5.
    发明授权
    Turbomachine having swirl-inhibiting seal 有权
    涡轮机具有漩涡抑制密封

    公开(公告)号:US09394800B2

    公开(公告)日:2016-07-19

    申请号:US13745890

    申请日:2013-01-21

    Abstract: Various embodiments include a turbomachine including a swirl-inhibiting seal. In various particular embodiments, a turbomachine includes: a rotor section having sets of axially disposed blades; a diaphragm section at least partially surrounding the rotor section, the diaphragm section including a set of nozzles positioned between adjacent sets of axially disposed blades, wherein the set of nozzles includes at least one nozzle having: a base section coupled to the diaphragm section; a blade coupled to the base section; and a radial tip section coupled to a radial end of the blade, the radial tip section including an axially extending flange having a slot extending therethrough for controlling fluid flow within the turbomachine.

    Abstract translation: 各种实施例包括包括旋转抑制密封件的涡轮机。 在各种具体实施例中,涡轮机包括:具有一组轴向设置的叶片的转子部分; 至少部分地围绕所述转子部分的隔膜部分,所述隔膜部分包括位于相邻的轴向设置的叶片组之间的一组喷嘴,其中所述一组喷嘴包括至少一个喷嘴,所述喷嘴具有:联接到所述隔膜部分的基部; 叶片,其联接到所述基部; 以及联接到所述叶片的径向端部的径向末端部分,所述径向末端部分包括轴向延伸的凸缘,所述凸缘具有延伸穿过其中的狭槽,以控制所述涡轮机内的流体流动。

    SWIRL INTERRUPTION SEAL TEETH FOR SEAL ASSEMBLY
    6.
    发明申请
    SWIRL INTERRUPTION SEAL TEETH FOR SEAL ASSEMBLY 有权
    SWIRL中断密封密封件组件

    公开(公告)号:US20160024954A1

    公开(公告)日:2016-01-28

    申请号:US14875726

    申请日:2015-10-06

    Abstract: A seal assembly for sealing between a rotating component and a stationary component in a turbomachine. The seal assembly includes a plurality of radially inwardly projecting, axially spaced teeth extending from the stationary component, wherein at least one of the plurality of teeth has at least one axially extending hole therethrough. Axial flow of an operating fluid through the holes acts as an air-curtain to interrupt swirl flow in a seal cavity, therefore reducing steam force that could act to destabilize rotordynamics.

    Abstract translation: 用于在涡轮机中的旋转部件和固定部件之间进行密封的密封组件。 密封组件包括从固定部件延伸的多个径向向内突出的轴向隔开的齿,其中多个齿中的至少一个齿具有穿过其中的至少一个轴向延伸的孔。 通过孔的工作流体的轴向流动用作气幕以阻止密封腔中的漩涡流动,因此减小了可能使动力学不稳定的蒸汽力。

    Clutch with swirl breaks
    7.
    发明授权

    公开(公告)号:US10982722B2

    公开(公告)日:2021-04-20

    申请号:US16401044

    申请日:2019-05-01

    Abstract: A clutch system configured to transmit torque between an input shaft and an output shaft. The clutch system includes a clutch. The clutch includes: an input portion disposed at an end of the input shaft; an output portion disposed at an end of the output shaft; a sliding component that slides axially between the input and output portions to engage the clutch; and swirl breaks. The input portion, the output portion, and the sliding component each comprises walls. The swirl breaks are affixed to a one of the walls.

    TURBOMACHINE HAVING SWIRL-INHIBITING SEAL
    8.
    发明申请
    TURBOMACHINE HAVING SWIRL-INHIBITING SEAL 有权
    具有SWIRL-INHIBITIC SEAL的涡轮发酵

    公开(公告)号:US20140205444A1

    公开(公告)日:2014-07-24

    申请号:US13745890

    申请日:2013-01-21

    Abstract: Various embodiments include a turbomachine including a swirl-inhibiting seal. In various particular embodiments, a turbomachine includes: a rotor section having sets of axially disposed blades; a diaphragm section at least partially surrounding the rotor section, the diaphragm section including a set of nozzles positioned between adjacent sets of axially disposed blades, wherein the set of nozzles includes at least one nozzle having: a base section coupled to the diaphragm section; a blade coupled to the base section; and a radial tip section coupled to a radial end of the blade, the radial tip section including an axially extending flange having a slot extending therethrough for controlling fluid flow within the turbomachine.

    Abstract translation: 各种实施例包括包括旋转抑制密封件的涡轮机。 在各种具体实施例中,涡轮机包括:具有一组轴向设置的叶片的转子部分; 至少部分地围绕所述转子部分的隔膜部分,所述隔膜部分包括位于相邻的轴向设置的叶片组之间的一组喷嘴,其中所述一组喷嘴包括至少一个喷嘴,所述喷嘴具有:联接到所述隔膜部分的基部; 叶片,其联接到所述基部; 以及联接到所述叶片的径向端部的径向末端部分,所述径向末端部分包括轴向延伸的凸缘,所述凸缘具有延伸穿过其中的狭槽,以控制所述涡轮机内的流体流动。

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