TURBINE INTRUSION LOSS REDUCTION SYSTEM
    11.
    发明申请
    TURBINE INTRUSION LOSS REDUCTION SYSTEM 有权
    涡轮冲击减少系统

    公开(公告)号:US20140093359A1

    公开(公告)日:2014-04-03

    申请号:US13633651

    申请日:2012-10-02

    Abstract: Systems and devices configured to reduce windage and mixing losses in a turbine by redirecting and/or aligning a direction of a leakage flow with the flowpath of the main flow of a turbine are disclosed. In one embodiment, a device includes: a base configured to connect to a diaphragm of a turbine; and a radial portion connected to the base and extending radially inboard from the base toward a rotor of the turbine, the radial portion oriented to adjust a direction of travel of a leakage flow of working fluid radially inboard at an angle complementary to a primary working fluid path of the turbine.

    Abstract translation: 公开了通过将泄漏流动的方向与涡轮主流的流路重新导向和/或对准来减少涡轮机中的风阻和混合损失的系统和装置。 在一个实施例中,一种装置包括:基座,其构造成连接到涡轮的隔膜; 以及径向部分,其连接到所述基部并且从所述基部朝向所述涡轮机的转子径向向内延伸,所述径向部分被定向成以与主工作流体互补的角度径向地调节工作流体的泄漏流的行进方向 涡轮机路径。

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