TURBOMACHINE FLOW IMPROVEMENT SYSTEM
    1.
    发明申请
    TURBOMACHINE FLOW IMPROVEMENT SYSTEM 审中-公开
    涡轮增压系统

    公开(公告)号:US20130205795A1

    公开(公告)日:2013-08-15

    申请号:US13369882

    申请日:2012-02-09

    IPC分类号: F02C7/00 F02C3/00 F01D9/00

    摘要: A turbomachine includes a housing that defines a flow path, and a stage arranged within the housing. The stage includes a plurality of rotating airfoil members and a first plurality of stationary airfoil members. A second plurality of stationary airfoil members is arranged directly adjacent to the first plurality of stationary airfoil members. A flow improvement system is associated with each of the first and second pluralities of stationary airfoil members. The flow improvement system establishes a predetermined clocking of each of the first plurality of stationary airfoil members relative to each of the second plurality of stationary airfoil members to improve flow characteristics along the flow path.

    摘要翻译: 涡轮机包括限定流路的壳体和布置在壳体内的台架。 台架包括多个旋转翼型件和第一多个固定翼型件。 第二多个固定翼型件直接布置在第一多个固定翼型件附近。 流动改进系统与第一和第二多个固定翼型件中的每一个相关联。 流动改进系统相对于第二多个固定翼型件中的每一个建立第一多个固定翼型件中的每一个的预定定时,以改善沿着流动路径的流动特性。

    TURBOMACHINE INCLUDING FLOW IMPROVEMENT SYSTEM
    2.
    发明申请
    TURBOMACHINE INCLUDING FLOW IMPROVEMENT SYSTEM 审中-公开
    涡轮机包括流量改进系统

    公开(公告)号:US20130209216A1

    公开(公告)日:2013-08-15

    申请号:US13369843

    申请日:2012-02-09

    IPC分类号: F01D9/04

    摘要: A turbomachine includes a housing including a fluid path, and a first stage arranged within the housing. The first stage includes a first plurality of airfoil members and a second plurality of airfoil members. A second stage is arranged within the housing relative to the first stage. The second stage includes a third plurality of airfoil members and a fourth plurality of airfoil members. A flow improvement system is associated with each of the first and second stages. The flow improvement system establishes a predetermined clocking of each of the first plurality of airfoil members relative to corresponding ones of each of the third plurality of airfoil members, and each of the second plurality of airfoil members relative to each of the fourth plurality of airfoil members. The predetermined clocking is configured and disposed to improve flow characteristics along the flow path.

    摘要翻译: 涡轮机包括包括流体路径的壳体和布置在壳体内的第一级。 第一阶段包括第一多个翼型件和第二多个翼型件。 第二阶段相对于第一阶段布置在壳体内。 第二级包括第三多个翼型件和第四多个翼型件。 流程改进系统与第一和第二阶段中的每一个相关联。 流动改进系统相对于第三多个翼型构件中的每一个中的对应翼型构件建立了第一多个翼型构件中的每一个的预定时钟,并且第二多个翼型构件中的每一个相对于第四多个翼型构件 。 预定的时钟被配置和布置成改善沿着流动路径的流动特性。