COOLING SYSTEM AND METHOD FOR AN AXIAL FLOW TURBINE
    1.
    发明申请
    COOLING SYSTEM AND METHOD FOR AN AXIAL FLOW TURBINE 审中-公开
    轴流式涡轮机冷却系统及方法

    公开(公告)号:US20140003907A1

    公开(公告)日:2014-01-02

    申请号:US13929227

    申请日:2013-06-27

    Abstract: An axial flow turbine is described having a casing defining a flow path for a working fluid therein, a rotor co-axial to the casing, a plurality of stages, each including a stationary row of vanes circumferentially mounted on the casing a rotating row of blades, circumferentially mounted on the rotor, with an inner face of the casing exposed to the working fluid having one or more essentially circumferential grooves of increasing depth each ending in an extraction port with a bore.

    Abstract translation: 描述了轴流涡轮机,其具有限定其中的工作流体的流动路径的壳体,与壳体同轴的转子,多个级,每个级包括周向地安装在壳体上的静止行叶片,旋转的叶片行 周向地安装在转子上,其中暴露于工作流体的壳体的内表面具有一个或多个具有增加深度的基本上周向的凹槽,每个凹槽终止于具有孔的抽出口。

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