Turbine blade and method for producing a turbine blade
    11.
    发明授权
    Turbine blade and method for producing a turbine blade 有权
    涡轮叶片及其制造方法

    公开(公告)号:US06631561B1

    公开(公告)日:2003-10-14

    申请号:US10129850

    申请日:2002-08-12

    Abstract: A method is for producing a turbine blade, in particular, a gas turbine blade, comprising a head, a foot, and a blade section, in addition to an internal canalization system, including individual channels through which coolant gas can pass along a flow path within the turbine blade. The turbine blade also includes a throttle device which influences the passage of the coolant gas without impairing the flow of the coolant gas in the intake area. The throttle device is located in the rear section of the flow path, and is positioned upstream of the exit openings.

    Abstract translation: 一种除了内部管道系统之外,还包括一个头部,一个脚部和一个叶片部分的涡轮机叶片,特别是一种燃气轮机叶片的方法,该内部管道系统包括单独的通道,冷却剂气体可以通过该通道沿流动路径 在涡轮叶片内。 涡轮机叶片还包括节流装置,其影响冷却剂气体的通过,而不损害进气区域中的冷却剂气体的流动。 节流装置位于流路的后部,并且位于出口的上游

    Covering element and arrangement with a covering element and a support structure
    12.
    发明授权
    Covering element and arrangement with a covering element and a support structure 失效
    覆盖元件和布置与覆盖元件和支撑结构

    公开(公告)号:US06602050B1

    公开(公告)日:2003-08-05

    申请号:US09937214

    申请日:2001-09-24

    CPC classification number: F01D11/08 F01D25/246

    Abstract: A covering element is for the protection of components in a machine subjected to high thermal load, in particular of components in a gas turbine. The covering element includes a wall with a hot side capable of being exposed to a hot medium, and with a cool side located opposite the hot side. The cooling side includes a cooling surface capable of being acted upon by a coolant. Holding elements are provided on the cool side.

    Abstract translation: 覆盖元件用于保护承受高热负荷的机器中的部件,特别是燃气轮机中的部件。 覆盖元件包括具有能够暴露于热介质的热侧的壁,以及与热侧相对的冷侧。 冷却侧包括能够被冷却剂作用的冷却表面。 保持元件设置在凉爽的一面。

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