METHODS OF RESIZING HOLES
    3.
    发明申请
    METHODS OF RESIZING HOLES 有权
    矫正角膜的方法

    公开(公告)号:US20140124100A1

    公开(公告)日:2014-05-08

    申请号:US13669754

    申请日:2012-11-06

    Abstract: Methods of reducing an initial cross-sectional area of a hole in a component to a predetermined cross-sectional area including preparing a composition comprising at least an aluminum alloy with a melting temperature higher than aluminum, applying the composition to an interior surface of the hole, and then heating the component to cause a metal within the component to diffuse from the component into the composition and react with the aluminum alloy in the composition to form a coating on the interior surface of the hole. The heating step is performed to selectively modify the initial cross-sectional area of the hole and thereby directly attain the predetermined cross-sectional area thereof.

    Abstract translation: 将组件中的孔的初始横截面积减小到预定横截面积的方法包括制备至少包含熔融温度高于铝的铝合金的组合物,将该组合物施加到孔的内表面 ,然后加热组分以使组分内的金属从组分扩散到组合物中并与组合物中的铝合金反应,以在孔的内表面上形成涂层。 执行加热步骤以选择性地修改孔的初始横截面积,从而直接达到其预定的横截面面积。

    TURBINE COMPONENTS WITH PASSIVE COOLING PATHWAYS
    9.
    发明申请
    TURBINE COMPONENTS WITH PASSIVE COOLING PATHWAYS 有权
    涡轮组件与无源冷却路径

    公开(公告)号:US20140099183A1

    公开(公告)日:2014-04-10

    申请号:US13645729

    申请日:2012-10-05

    Abstract: The present application provides a turbine component for use in a hot gas path of a gas turbine. The turbine component may include an outer surface, an internal cooling circuit, a number of cooling pathways in communication with the internal cooling circuit and extending through the outer surface, and a number of adaptive cooling pathways in communication with the internal cooling circuit and extending through the outer surface. The adaptive cooling pathways may include a high temperature compound therein.

    Abstract translation: 本申请提供了一种在燃气轮机的热气路径中使用的涡轮机部件。 涡轮机部件可以包括外表面,内部冷却回路,与内部冷却回路连通并延伸穿过外表面的多个冷却通路,以及与内部冷却回路连通并延伸通过的多个自适应冷却通道 外表面。 适应性冷却途径可包括其中的高温化合物。

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