GAS TURBINE AND TURBINE BLADE FOR SUCH A GAS TURBINE
    1.
    发明申请
    GAS TURBINE AND TURBINE BLADE FOR SUCH A GAS TURBINE 有权
    气体涡轮机和涡轮叶片用于这种气体涡轮机

    公开(公告)号:US20140112798A1

    公开(公告)日:2014-04-24

    申请号:US14061018

    申请日:2013-10-23

    CPC classification number: F01D5/081 F01D5/082 F01D5/187 F05B2240/801

    Abstract: A gas turbine includes a rotor concentrically surrounded by a casing, with an annular hot gas channel axially extending between the rotor and the casing. The rotor is equipped with a plurality of blades, which are arranged on the rotor in an annular fashion. Each of the blades is mounted with a root in a respective axial slot on a rim of the rotor radially extending with an airfoil into said hot gas channel and adjoining with an axially oriented root surface to an annular rim cavity. Cooling means are provided at the root of each of said blades to receive cooling air being injected into said rim cavity through stationary injecting means. An optimized cooling is achieved by providing the root surface to be an essentially plane surface and the cooling means including a scoop for capturing and redirecting at least part of the injected cooling air, which scoop is designed as a recess with respect to the root surface.

    Abstract translation: 燃气轮机包括同轴地由壳体包围的转子,其中环形热气通道在转子和壳体之间轴向延伸。 转子配备有多个叶片,其以环形的方式布置在转子上。 每个叶片安装有根部,位于转子边缘上的相应轴向槽中,其径向延伸,翼型进入所述热气通道并与轴向定向的根表面邻接到环形边缘空腔。 冷却装置设置在每个所述叶片的根部处以接收通过静态喷射装置注入到所述边缘空腔中的冷却空气。 通过将根表面设置为基本上平面的表面来实现优化的冷却,并且冷却装置包括用于捕获和重定向至少部分喷射的冷却空气的铲斗,该铲斗被设计为相对于根表面的凹部。

    METHOD AND COOLING SYSTEM FOR COOLING BLADES OF AT LEAST ONE BLADE ROW IN A ROTARY FLOW MACHINE
    2.
    发明申请
    METHOD AND COOLING SYSTEM FOR COOLING BLADES OF AT LEAST ONE BLADE ROW IN A ROTARY FLOW MACHINE 有权
    用于冷却旋转流动机中的一个叶片的叶片的方法和冷却系统

    公开(公告)号:US20140086743A1

    公开(公告)日:2014-03-27

    申请号:US14031660

    申请日:2013-09-19

    CPC classification number: F01D5/186 F01D5/08 F01D5/187 F01D5/225 F01D11/10

    Abstract: A method and a cooling system for cooling blades of at least one blade row in a rotary flow machine includes an axial flow channel which is radially limited on the inside by a rotor unit and at the outside by at least one stationary component, the blades are arranged at the rotary unit and provide a shrouded blade tip facing radially to said stationary component. Pressurized cooling air is fed through from radially outside towards the tip of each of said blades in the at least one blade row, and the pressurized cooling air enters the blades through at least one opening at the shrouded blades' tip.

    Abstract translation: 用于在旋转流动机械中至少一个叶片排的叶片的冷却方法和冷却系统包括轴向流动通道,该轴向流动通道由转子单元在内部径向限制,并且在外部由至少一个固定部件限定,叶片是 布置在所述旋转单元处并且提供面向所述静止部件的径向的被覆盖的叶片尖端。 加压冷却空气从至少一个叶片排中的径向外侧向每个所述叶片的顶端供给,并且加压冷却空气通过所覆盖的叶片尖端处的至少一个开口进入叶片。

    BLADE OF A ROTARY FLOW MACHINE WITH A RADIAL STRIP SEAL
    3.
    发明申请
    BLADE OF A ROTARY FLOW MACHINE WITH A RADIAL STRIP SEAL 有权
    具有径向条纹密封的旋转流动机的叶片

    公开(公告)号:US20150064012A1

    公开(公告)日:2015-03-05

    申请号:US14467752

    申请日:2014-08-25

    Abstract: The invention refers to a blade of a rotary flow machine including an airfoil having a suction surface and a pressure surface joining each other along a trailing and a leading edge. A radially outward directed airfoil tip and a radially inward directed end joining an inner platform connect the airfoil to a shank at a radial end of the airfoil and providing, at least one shank pocket radially encircled by an axially extending portion of the platform. At least one radially extending rim extends from the trailing edge side of the shank and has an essentially radially orientated first slot for receiving a seal. A mount extends radially inwardly from said shank pocket. The first slot has a first aperture on a shank surface orientated in an axial direction.

    Abstract translation: 本发明涉及一种旋转流动机的叶片,其包括具有抽吸表面和沿着后缘和前缘彼此连接的压力表面的翼型件。 径向向外定向的翼型端头和连接内平台的径向向内的端部将翼型件在翼型件的径向端处连接到柄部,并且提供由平台的轴向延伸部分径向包围的至少一个柄袋。 至少一个径向延伸的边缘从柄的后缘侧延伸并且具有用于接收密封件的基本上径向定向的第一槽。 安装座从所述柄袋径向向内延伸。 第一槽具有在轴向方向上定向的柄表面上的第一孔。

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