EDGE TREATMENT FOR GAS TURBINE ENGINE COMPONENT
    32.
    发明申请
    EDGE TREATMENT FOR GAS TURBINE ENGINE COMPONENT 审中-公开
    气体涡轮发动机部件的边缘处理

    公开(公告)号:US20160003087A1

    公开(公告)日:2016-01-07

    申请号:US14769834

    申请日:2014-01-30

    Abstract: A gas turbine engine component according to an exemplary aspect of the present disclosure includes, among other things, a body having a first outer face meeting a second outer face at an intersection, the body having a plurality of apertures extending from an opening in the first outer face to an opening on the second outer face; and a coating filling at least a portion of the plurality of apertures.

    Abstract translation: 根据本公开的示例性方面的燃气涡轮发动机部件包括主体,其具有在交叉点处与第二外表面相交的第一外表面的本体,所述主体具有从第一 外表面到第二外表面上的开口; 以及填充所述多个孔的至少一部分的涂层。

    METHOD INCLUDING FIBER REINFORCED CASTING ARTICLE
    33.
    发明申请
    METHOD INCLUDING FIBER REINFORCED CASTING ARTICLE 有权
    包括纤维增强铸件的方法

    公开(公告)号:US20150367412A1

    公开(公告)日:2015-12-24

    申请号:US14744450

    申请日:2015-06-19

    CPC classification number: B22C9/106 B22D29/001 B22D29/002

    Abstract: A method of forming an engine component according to an exemplary aspect of the present disclosure includes, among other things, introducing molten metal into a cavity between a shell and a casting article in the shell. The casting article includes a ceramic portion and a plurality of fibers. The method further includes separately removing the ceramic portion and the fibers from an interior of the component.

    Abstract translation: 根据本公开的示例性方面的形成发动机部件的方法包括:将熔融金属引入壳体和外壳中的铸件之间的空腔中。 铸造制品包括陶瓷部分和多根纤维。 该方法还包括从部件的内部分离地去除陶瓷部分和纤维。

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