Gas turbine engine sump pressurization system
    2.
    发明授权
    Gas turbine engine sump pressurization system 有权
    燃气轮机发动机油底壳加压系统

    公开(公告)号:US08915057B2

    公开(公告)日:2014-12-23

    申请号:US14237384

    申请日:2013-02-09

    Abstract: A sump pressurization system for a gas turbine engine comprises a first hollow shaft and a second hollow shaft disposed within the first hollow shaft and defining a cavity therebetween. Each of the first and second hollow shafts has a common axis of rotation. Also included is a source of pressurized air to pressurize the cavity and a plurality of hollow tubes disposed in the cavity. The tubes are oriented perpendicular to the axis of rotation and are connected to and rotatable with the first hollow shaft. A plurality of apertures in the second hollow shaft are in fluid communication with the tubes, such that pressurized air flowing through the tubes passes through the apertures into the interior of the second hollow shaft.

    Abstract translation: 用于燃气涡轮发动机的油底壳加压系统包括第一中空轴和设置在第一空心轴内并在其间限定空腔的第二中空轴。 第一和第二空心轴中的每一个具有共同的旋转轴线。 还包括用于对空腔加压的加压空气源和设置在空腔中的多个中空管。 管垂直于旋转轴线定向并且与第一空心轴连接并且可旋转。 第二空心轴中的多个孔与管流体连通,使得流过管的加压空气通过孔进入第二空心轴的内部。

    Hydrodynamic Intershaft Piston Ring Seal
    3.
    发明申请

    公开(公告)号:US20190226585A1

    公开(公告)日:2019-07-25

    申请号:US15879535

    申请日:2018-01-25

    Abstract: Sealing assemblies and systems and their assembly methods are provided. For example, a seal assembly is provided for use between an inner shaft and an outer shaft that are rotatable about a common axis. The seal assembly comprises a first end ring having an aft face; a second end ring positioned aft of the first end ring and having a forward face; a first hydrodynamic portion defined on the aft face of the first end ring; a second hydrodynamic portion defined on the forward face of the second end ring. A seal element is disposed between the first end ring and the second end ring such that the seal element is positioned between the first hydrodynamic portion and the second hydrodynamic portion.

    GAS TURBINE ENGINE SUMP PRESSURIZATION SYSTEM
    4.
    发明申请
    GAS TURBINE ENGINE SUMP PRESSURIZATION SYSTEM 有权
    气体发动机发动机压缩系统

    公开(公告)号:US20140345246A1

    公开(公告)日:2014-11-27

    申请号:US14237384

    申请日:2013-02-09

    Abstract: A sump pressurization system for a gas turbine engine comprises a first hollow shaft and a second hollow shaft disposed within the first hollow shaft and defining a cavity therebetween. Each of the first and second hollow shafts has a common axis of rotation. Also included is a source of pressurized air to pressurize the cavity and a plurality of hollow tubes disposed in the cavity. The tubes are oriented perpendicular to the axis of rotation and are connected to and rotatable with the first hollow shaft. A plurality of apertures in the second hollow shaft are in fluid communication with the tubes, such that pressurized air flowing through the tubes passes through the apertures into the interior of the second hollow shaft.

    Abstract translation: 用于燃气涡轮发动机的油底壳加压系统包括第一中空轴和设置在第一空心轴内并在其间限定空腔的第二中空轴。 第一和第二空心轴中的每一个具有共同的旋转轴线。 还包括用于对空腔加压的加压空气源和设置在空腔中的多个中空管。 管垂直于旋转轴线定向并且与第一空心轴连接并且可旋转。 第二空心轴中的多个孔与管流体连通,使得流过管的加压空气通过孔进入第二空心轴的内部。

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