STRUCTURAL COOLING FLUID TUBE FOR SUPPORTING A TURBINE COMPONENT AND SUPPLYING COOLING FLUID TO TRANSITION SECTION
    1.
    发明申请
    STRUCTURAL COOLING FLUID TUBE FOR SUPPORTING A TURBINE COMPONENT AND SUPPLYING COOLING FLUID TO TRANSITION SECTION 有权
    用于支撑涡轮组件的结构冷却流体管和供应冷却流体到过渡段

    公开(公告)号:US20130098065A1

    公开(公告)日:2013-04-25

    申请号:US13277630

    申请日:2011-10-20

    IPC分类号: F02C7/20 F02C7/12

    摘要: A shaft cover support for a gas turbine engine is disclosed. The shaft cover support not only provides enhanced support to a shaft cover of the gas turbine engine, but also includes a cooling fluid chamber for passing fluids from a rotor air cooling supply conduit to an inner ring cooling manifold. Furthermore, the shaft cover support may include a cooling shield supply extending from the cooling fluid chamber between the radially outward inlet and the radially inward outlet on the radially extending region and in fluid communication with the cooling fluid chamber for providing cooling fluids to a transition section. The shaft cover support may also provide additional stiffness and reduce interference of the flow from the compressor. In addition, the shaft cover support accommodates a transition section extending between compressor and turbine sections of the gas turbine engine.

    摘要翻译: 公开了一种用于燃气涡轮发动机的轴盖支撑件。 轴盖支撑件不仅对燃气涡轮发动机的轴盖提供增强的支撑,还包括用于将流体从转子空气冷却供应管道传递到内环冷却歧管的冷却流体室。 此外,轴盖支撑件可以包括冷却屏蔽供应源,其从径向向外的入口和径向向外的出口之间的冷却流体室延伸并且与冷却流体室流体连通,以将冷却流体提供给过渡部分 。 轴盖支撑件还可以提供额外的刚度并且减小来自压缩机的流动的干扰。 此外,轴套支撑件容纳在燃气涡轮发动机的压缩机和涡轮机部分之间延伸的过渡部分。