TURBINE ENGINE ROTATING CAVITY ANTI-VORTEX CASCADE
    4.
    发明申请
    TURBINE ENGINE ROTATING CAVITY ANTI-VORTEX CASCADE 有权
    涡轮发动机旋转腔体反VORTEX CASCADE

    公开(公告)号:US20100266401A1

    公开(公告)日:2010-10-21

    申请号:US12425552

    申请日:2009-04-17

    IPC分类号: F01D9/00

    CPC分类号: F02C6/08 F01D5/087 F04D29/321

    摘要: A gas turbine engine rotor drum includes spaced apart discs providing a cavity between the discs. The discs are configured to rotate in a rotational direction about an axis. An annular support is mounted on at least one of the discs and within the cavity. A cascade of relatively short anti-vortex members is mounted circumferentially on the annular support. The anti-vortex members include an outer end having a concave surface extending within the cavity radially outward from the annular support. The concave surface faces the rotational direction and promotes swirl as the rotor drum rotates.

    摘要翻译: 燃气涡轮发动机转子鼓包括间隔开的盘,在盘之间提供空腔。 盘构造成围绕轴线在旋转方向上旋转。 环形支撑件安装在至少一个盘上并在空腔内。 相对短的防涡流构件的级联安装在环形支撑件上周向。 防涡流构件包括具有从环形支撑件径向向外延伸的空腔内的凹面的外端。 凹面朝向旋转方向,并随转子鼓旋转而促进涡流。

    Turbine engine rotating cavity anti-vortex cascade
    5.
    发明授权
    Turbine engine rotating cavity anti-vortex cascade 有权
    涡轮发动机旋转腔防漩涡级联

    公开(公告)号:US08540483B2

    公开(公告)日:2013-09-24

    申请号:US13416414

    申请日:2012-03-09

    IPC分类号: F01D9/00

    CPC分类号: F02C6/08 F01D5/087 F04D29/321

    摘要: A gas turbine engine rotor drum includes spaced apart discs providing a cavity between the discs. The discs are configured to rotate in a rotational direction about an axis. An annular support is mounted on at least one of the discs and within the cavity. A cascade of relatively short anti-vortex members is mounted circumferentially on the annular support. The anti-vortex members include an outer end having a concave surface extending within the cavity radially outward from the annular support. The concave surface faces the rotational direction and promotes swirl as the rotor drum rotates.

    摘要翻译: 燃气涡轮发动机转子鼓包括间隔开的盘,在盘之间提供空腔。 盘构造成围绕轴线在旋转方向上旋转。 环形支撑件安装在至少一个盘上并在空腔内。 相对短的防涡流构件的级联安装在环形支撑件上周向。 防涡流构件包括具有从环形支撑件径向向外延伸的空腔内的凹面的外端。 凹面朝向旋转方向,并随转子鼓旋转而促进涡流。

    TURBINE ENGINE ROTATING CAVITY ANTI-VORTEX CASCADE
    6.
    发明申请
    TURBINE ENGINE ROTATING CAVITY ANTI-VORTEX CASCADE 有权
    涡轮发动机旋转腔体反VORTEX CASCADE

    公开(公告)号:US20120171029A1

    公开(公告)日:2012-07-05

    申请号:US13416414

    申请日:2012-03-09

    IPC分类号: F01D9/00

    CPC分类号: F02C6/08 F01D5/087 F04D29/321

    摘要: A gas turbine engine rotor drum includes spaced apart discs providing a cavity between the discs. The discs are configured to rotate in a rotational direction about an axis. An annular support is mounted on at least one of the discs and within the cavity. A cascade of relatively short anti-vortex members is mounted circumferentially on the annular support. The anti-vortex members include an outer end having a concave surface extending within the cavity radially outward from the annular support. The concave surface faces the rotational direction and promotes swirl as the rotor drum rotates.

    摘要翻译: 燃气涡轮发动机转子鼓包括间隔开的盘,在盘之间提供空腔。 盘构造成围绕轴线在旋转方向上旋转。 环形支撑件安装在至少一个盘上并在空腔内。 相对短的防涡流构件的级联安装在环形支撑件上周向。 防涡流构件包括具有从环形支撑件径向向外延伸的空腔内的凹面的外端。 凹面朝向旋转方向,并随转子鼓旋转而促进涡流。

    Turbine engine rotating cavity anti-vortex cascade
    7.
    发明授权
    Turbine engine rotating cavity anti-vortex cascade 有权
    涡轮发动机旋转腔防漩涡级联

    公开(公告)号:US08177503B2

    公开(公告)日:2012-05-15

    申请号:US12425552

    申请日:2009-04-17

    IPC分类号: F01D1/02

    CPC分类号: F02C6/08 F01D5/087 F04D29/321

    摘要: A gas turbine engine rotor drum includes spaced apart discs providing a cavity between the discs. The discs are configured to rotate in a rotational direction about an axis. An annular support is mounted on at least one of the discs and within the cavity. A cascade of relatively short anti-vortex members is mounted circumferentially on the annular support. The anti-vortex members include an outer end having a concave surface extending within the cavity radially outward from the annular support. The concave surface faces the rotational direction and promotes swirl as the rotor drum rotates.

    摘要翻译: 燃气涡轮发动机转子鼓包括间隔开的盘,在盘之间提供空腔。 盘构造成围绕轴线在旋转方向上旋转。 环形支撑件安装在至少一个盘上并在空腔内。 相对短的防涡流构件的级联安装在环形支撑件上周向。 防涡流构件包括具有从环形支撑件径向向外延伸的空腔内的凹面的外端。 凹面朝向旋转方向,并随转子鼓旋转而促进涡流。

    Muffler with integral check valve
    8.
    发明授权
    Muffler with integral check valve 失效
    整流止回阀消声器

    公开(公告)号:US5583325A

    公开(公告)日:1996-12-10

    申请号:US430941

    申请日:1995-04-26

    CPC分类号: F04C29/126 F04C29/065

    摘要: An unbiased valve is located within a muffler. The valve is positioned by the pressure differential across the valve and is either in the full open or full closed position. A pressure equalization tube is provided between the downstream cavity of the muffler and the back of the valve such that flow pattern produced low pressure areas are avoided and the valve can react to actual pressure differentials in the flow.

    摘要翻译: 无偏压阀位于消声器内。 阀门通过阀门上的压差定位,处于完全打开或完全关闭状态。 在消声器的下游腔和阀的后部之间设置压力平衡管,从而避免了产生低压区域的流动模式,并且该阀可以对流动中的实际压差作出反应。