GAS TURBINE
    1.
    发明申请
    GAS TURBINE 有权
    燃气轮机

    公开(公告)号:US20110135451A1

    公开(公告)日:2011-06-09

    申请号:US12857131

    申请日:2010-08-16

    IPC分类号: F01D11/00 F01D5/08

    摘要: A gas turbine includes a turbine section; an annular combustor disposed upstream of the turbine section and configured to discharge a hot gas flow on an outlet side to the turbine section; an outer shell delimiting the combustor and splittable at a parting plane; a plenum enclosing the outer shell; a rotor; a turbine vane carrier encompassing the rotor; a plurality of stator vanes disposed on the vane carrier, and at least two sealing segments forming a ring, each of the at least two sealing segments having an inner edge and a head and a foot section and being movably mounted on the inner edge by the foot section to the outer shell and by the head section to the turbine vane carrier so as to mechanically connect the combustor to the turbine vane carrier.

    摘要翻译: 燃气轮机包括涡轮部分; 设置在所述涡轮部分的上游并且被配置为将出口侧的热气流排放到所述涡轮部分的环形燃烧器; 外壳限定燃烧器并在分型平面处可分开; 包围外壳的增压室; 转子 包围转子的涡轮叶片载体; 设置在所述叶片载体上的多个定子叶片和形成环的至少两个密封段,所述至少两个密封段中的每一个具有内边缘和头部和脚部,并且可移动地安装在所述内边缘上 脚部到外壳,并且通过头部到达涡轮叶片载体,以便将燃烧器机械地连接到涡轮叶片载体。

    THERMAL MACHINE
    2.
    发明申请
    THERMAL MACHINE 有权
    热机

    公开(公告)号:US20110113790A1

    公开(公告)日:2011-05-19

    申请号:US12860620

    申请日:2010-08-20

    IPC分类号: F02C7/12

    摘要: A thermal machine including a wall defining a hot gas duct for transferring a hot gas stream and a cooling jacket disposed at a distance from the wall on an outside of the hot gas duct so as to define a cooling duct with an inlet and an outlet. The cooling duct is configured to conduct a cooling medium along an external face of the wall from the inlet to an outlet in a direction counter to a flow of hot gas in the hot gas duct. An impingement cooling plate is disposed at the inlet of the cooling duct and includes cooling baffle holes configured such that cooling medium entering the cooling duct through the cooling baffle holes flows in a direction perpendicular to the wall. The impingement cooling plate is positioned such that an inflow-side edge sealingly abuts the wall of the hot gas duct so as to reduce a transverse flow of the cooling medium through the cooling duct.

    摘要翻译: 一种热机器,其包括限定用于传输热气流的热气管道的壁和在所述热气体管道的外部设置为距离所述壁一定距离的冷却套管,以限定具有入口和出口的冷却管道。 所述冷却管道构造成沿着所述壁的外表面沿与所述热气体管道中的热气流相反的方向从入口向出口导入冷却介质。 冲击冷却板设置在冷却管道的入口处,并且包括冷却挡板孔,其构造成使得通过冷却挡板进入冷却管道的冷却介质沿垂直于壁的方向流动。 冲击冷却板被定位成使得流​​入侧边缘密封地邻接热气管道的壁,以便减少冷却介质通过冷却管道的横向流动。

    GAS TURBINE HAVING AN IMPROVED COOLING ARCHITECTURE
    3.
    发明申请
    GAS TURBINE HAVING AN IMPROVED COOLING ARCHITECTURE 有权
    具有改进的冷却结构的气体涡轮机

    公开(公告)号:US20110110761A1

    公开(公告)日:2011-05-12

    申请号:US12857171

    申请日:2010-08-16

    IPC分类号: F02C7/16

    摘要: A thermal machine includes a hot gas channel; a shell bounding the hot gas channel; a cooling shirt surrounding the shell; and a cooling channel disposed between the shell and the cooling shirt and configured to convection cool the hot gas channel with a cooling medium, wherein the cooling shirt includes at least one local divergence in the guidance of the cooling medium so as to compensate for non-uniformities in at least one of a thermal load on the shell and a flow of the cooling medium in the cooling channel.

    摘要翻译: 热机器包括热气通道; 封闭热气通道的壳体; 围绕外壳的冷却衬衫; 以及冷却通道,其设置在所述外壳和所述冷却衬衫之间并且被配置为用冷却介质对所述热气体通道进行对流,其中所述冷却衬衫在所述冷却介质的引导中包括至少一个局部散度, 在壳体上的热负荷和冷却通道中的冷却介质流中的至少一个中的均匀性。