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    DRY GAS BLOW DOWN SEAL
    1.
    发明申请
    DRY GAS BLOW DOWN SEAL 有权
    干气泡密封

    公开(公告)号：US20100254811A1

    公开(公告)日：2010-10-07

    申请号：US12419086

    申请日：2009-04-06

    Applicant: Mark Joseph Kuzdzal ,  Harry Francis Miller ,  Glenn R. Grosso ,  Martin D. Maier ,  David J. Peer

    Inventor： Mark Joseph Kuzdzal ,  Harry Francis Miller ,  Glenn R. Grosso ,  Martin D. Maier ,  David J. Peer

    IPC: F01D11/04 ,  F16J15/447

    CPC classification number: F04D29/102 ,  F01D11/04 ,  F04D29/104 ,  F04D29/122 ,  F04D29/124

    Abstract: A sealing assembly configured to seal a rotating shaft of a turbo machine having a high pressure process gas, comprising a housing defining a bore configured to receive the rotating shaft and sealing assembly, wherein the housing is mounted to a casing of the turbo machine; a first sealing stage comprising a single dry gas seal and configured to blow down the high pressure process gas to a lower pressure; a labyrinth seal mounted longitudinally outward from the first sealing stage; and a second sealing stage mounted longitudinally outward from the labyrinth seal, wherein the second sealing stage comprises a tandem dry gas seal having a primary dry gas seal and a secondary dry gas seal axially spaced with an intermediate labyrinth seal.

    Abstract translation: 密封组件，其构造成密封具有高压处理气体的涡轮机的旋转轴，所述密封组件包括限定被配置为容纳所述旋转轴和密封组件的孔的壳体，其中所述壳体安装到所述涡轮机的壳体; 第一密封阶段，其包括单个干燥气体密封并且构造成将高压处理气体吹走到较低的压力; 从第一密封阶段纵向向外安装的迷宫式密封件; 以及从迷宫式密封件纵向向外安装的第二密封级，其中第二密封级包括具有初级干燥气体密封件和与中间迷宫式密封件轴向间隔开的次级干燥气体密封件的串联干式气体密封件。

    Reduced leakage balance piston seal
    2.
    发明授权
    Reduced leakage balance piston seal 有权
    减少泄漏平衡活塞密封

    公开(公告)号：US09279324B2

    公开(公告)日：2016-03-08

    申请号：US13675368

    申请日：2012-11-13

    Applicant: Stephen G. Clute ,  Mark J. Kuzdzal ,  Glenn R. Grosso ,  David J. Peer

    Inventor： Stephen G. Clute ,  Mark J. Kuzdzal ,  Glenn R. Grosso ,  David J. Peer

    IPC: F01D3/04 ,  F01D11/04 ,  F04D29/22 ,  F01D11/02 ,  F04D29/041

    CPC classification number: F01D3/04 ,  F01D11/02 ,  F01D11/025 ,  F01D11/04 ,  F04D29/0416 ,  F04D29/2266

    Abstract: Balance piston assembly, apparatus, and methods are provided. The assembly includes a balance piston coupled to a rotatable shaft and configured to rotate therewith, the balance piston including a first shelf and a second shelf, the first and second shelves being axially-overlapping and radially-offset. The assembly also includes a seal including a first sealing surface configured to seal with the first shelf and a second sealing surface configured to seal with the second shelf.

    Abstract translation: 提供平衡活塞组件，装置和方法。 所述组件包括联接到可旋转轴并被配置为随其旋转的平衡活塞，所述平衡活塞包括第一搁架和第二搁架，所述第一和第二搁架在轴向上重叠并且径向偏移。 组件还包括密封件，该密封件包括构造成与第一搁板密封的第一密封表面和被配置为与第二搁板密封的第二密封表面。

    Thermal Barrier Coating for Bearing Journal Surfaces of Rotary Shafts
    3.
    发明申请
    Thermal Barrier Coating for Bearing Journal Surfaces of Rotary Shafts 有权
    轴承轴承热障涂层旋转轴表面

    公开(公告)号：US20150043848A1

    公开(公告)日：2015-02-12

    申请号：US14315674

    申请日：2014-06-26

    Applicant: Glenn R. Grosso

    Inventor： Glenn R. Grosso

    IPC: F16C33/10 ,  F16C33/02 ,  F16C37/00 ,  F16C17/02

    CPC classification number: F16C33/1065 ,  F04D17/122 ,  F04D29/04 ,  F04D29/046 ,  F04D29/053 ,  F04D29/057 ,  F04D29/063 ,  F16C17/02 ,  F16C33/02 ,  F16C37/00

    Abstract: A rotary shaft and method for reducing non-uniform heating thereof are provided. The rotary shaft may include a tubular body having a longitudinal axis extending therethrough. An outer surface of the tubular body may define a groove at least partially extending radially inward from the outer radial surface toward the longitudinal axis of the tubular body to define a depth thereof. The rotary shaft may include a thermal barrier at least partially disposed in the groove and configured to absorb at least a portion of heat generated from rotation thereof.

    Abstract translation: 提供了一种用于减少其不均匀加热的旋转轴和方法。 旋转轴可以包括具有延伸穿过其中的纵向轴线的管状体。 管状体的外表面可以限定从外径向内部至少部分地从管状体的纵向轴线向内延伸以限定其深度的凹槽。 旋转轴可以包括至少部分地布置在凹槽中并被构造成吸收由其旋转产生的热量的至少一部分的热障壁。

    Dry gas blow down seal
    4.
    发明授权
    Dry gas blow down seal 有权
    干燥气体吹灭密封

    公开(公告)号：US08061984B2

    公开(公告)日：2011-11-22

    申请号：US12419086

    申请日：2009-04-06

    Applicant: Mark Joseph Kuzdzal ,  Harry Francis Miller ,  Glenn R. Grosso ,  Martin D. Maier ,  David J. Peer

    Inventor： Mark Joseph Kuzdzal ,  Harry Francis Miller ,  Glenn R. Grosso ,  Martin D. Maier ,  David J. Peer

    IPC: F01D11/02

    CPC classification number: F04D29/102 ,  F01D11/04 ,  F04D29/104 ,  F04D29/122 ,  F04D29/124

    Abstract: A sealing assembly configured to seal a rotating shaft of a turbo machine having a high pressure process gas, comprising a housing defining a bore configured to receive the rotating shaft and sealing assembly, wherein the housing is mounted to a casing of the turbo machine; a first sealing stage comprising a single dry gas seal and configured to blow down the high pressure process gas to a lower pressure; a labyrinth seal mounted longitudinally outward from the first sealing stage; and a second sealing stage mounted longitudinally outward from the labyrinth seal, wherein the second sealing stage comprises a tandem dry gas seal having a primary dry gas seal and a secondary dry gas seal axially spaced with an intermediate labyrinth seal.

    Abstract translation: 密封组件，其构造成密封具有高压处理气体的涡轮机的旋转轴，所述密封组件包括限定被配置为容纳所述旋转轴和密封组件的孔的壳体，其中所述壳体安装到所述涡轮机的壳体; 第一密封阶段，其包括单个干燥气体密封并且构造成将高压处理气体吹走到较低的压力; 从第一密封阶段纵向向外安装的迷宫式密封件; 以及从迷宫式密封件纵向向外安装的第二密封级，其中第二密封级包括具有初级干燥气体密封件和与中间迷宫式密封件轴向间隔开的次级干燥气体密封件的串联干式气体密封件。

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