Modular turbine enclosure
    2.
    发明授权
    Modular turbine enclosure 有权
    模块化涡轮机外壳

    公开(公告)号:US08726609B1

    公开(公告)日:2014-05-20

    申请号:US13676269

    申请日:2012-11-14

    Abstract: The present application provides a modular enclosure for use with an equipment platform and a turbo-machine. The modular enclosure may include a first number of walls attached to a number of legs of the equipment platform and a second number of walls attached to the legs of the equipment platform. The first number of walls may include a number of pivotable panels. The second number of walls may include an access aperture therein. The equipment platform may provide a roof for the modular enclosure.

    Abstract translation: 本申请提供了用于与设备平台和涡轮机一起使用的模块化外壳。 模块化外壳可以包括连接到设备平台的多个支腿的第一数量的壁和附接到设备平台的腿的第二数量的壁。 第一数量的墙壁可以包括多个可枢转的面板。 第二数量的壁可以包括其中的进入孔。 设备平台可为模块化外壳提供屋顶。

    MODULAR TURBINE ENCLOSURE
    3.
    发明申请
    MODULAR TURBINE ENCLOSURE 有权
    模块式涡轮机外壳

    公开(公告)号:US20140130422A1

    公开(公告)日:2014-05-15

    申请号:US13676269

    申请日:2012-11-14

    Abstract: The present application provides a modular enclosure for use with an equipment platform and a turbo-machine. The modular enclosure may include a first number of walls attached to a number of legs of the equipment platform and a second number of walls attached to the legs of the equipment platform. The first number of walls may include a number of pivotable panels. The second number of walls may include an access aperture therein. The equipment platform may provide a roof for the modular enclosure.

    Abstract translation: 本申请提供了用于与设备平台和涡轮机一起使用的模块化外壳。 模块化外壳可以包括连接到设备平台的多个支腿的第一数量的壁和附接到设备平台的腿的第二数量的壁。 第一数量的墙壁可以包括多个可枢转的面板。 第二数量的壁可以包括其中的进入孔。 设备平台可为模块化外壳提供屋顶。

    SYSTEM FOR OXIDANT INTAKE
    4.
    发明申请

    公开(公告)号:US20190154261A1

    公开(公告)日:2019-05-23

    申请号:US15820739

    申请日:2017-11-22

    Abstract: A gas turbine system includes a plenum that includes an inlet and an outlet. The inlet is configured to receive a flow of oxidant and the outlet is configured to direct the flow of oxidant in a downstream direction. Additionally, a support system is coupled to the plenum and to a cone. The support system enables the cone to move along the support system from a first position to a second position. The cone includes an upstream end and the upstream end is removably coupled to the outlet of the plenum in the first position. When the cone is in the first position, the cone is configured to direct the flow of oxidant in the downstream direction to a gas turbine engine. The upstream end is disposed upstream of the outlet and is decoupled from the outlet when the cone is in the second position.

    Radial Diffuser Exhaust System
    8.
    发明申请
    Radial Diffuser Exhaust System 有权
    径向扩散器排气系统

    公开(公告)号:US20140271168A1

    公开(公告)日:2014-09-18

    申请号:US13798614

    申请日:2013-03-13

    CPC classification number: F01D25/30

    Abstract: The present application provides a radial diffuser exhaust system for use with a gas turbine engine. The radial diffuser exhaust system may include a radial diffuser positioned within an asymmetric exhaust collector. The asymmetric exhaust collector may include a closed end chamber and an exhaust end chamber. The closed end chamber may have a first size, the exhaust end chamber may have a second size, and the first size may be smaller than the second size.

    Abstract translation: 本申请提供了一种与燃气涡轮发动机一起使用的径向扩散器排气系统。 径向扩散器排气系统可以包括位于不对称排气收集器内的径向扩散器。 不对称排气收集器可以包括封闭端室和排气端室。 封闭端室可以具有第一尺寸,排气端室可以具有第二尺寸,并且第一尺寸可以小于第二尺寸。

    DIFFUSER REMOVAL TOOL
    10.
    发明申请

    公开(公告)号:US20180128181A1

    公开(公告)日:2018-05-10

    申请号:US15348446

    申请日:2016-11-10

    Abstract: A diffuser removal tool for displacing an exhaust diffuser from a gas turbine engine is provided, which includes a pair of support arms, a clamp and wedge assembly coupled to an exhaust diffuser, and a lead screw assembly coupled between the support arms and to the clamp and wedge assembly via a wedge of the clamp and wedge assembly. The tool also includes a pair of linear bearing assemblies coupled to the support arms and to the clamp and wedge assembly via wedges of the clamp and wedge assembly. The lead screw assembly is configured to displace the diffuser in an axial direction relative to a longitudinal axis of the gas turbine engine while the linear bearing assemblies are configured to both enable the displacement of the diffuser in the axial direction while vertically supporting the diffuser to maintain alignment between the diffuser and the gas turbine engine.

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