COMPOSITE ARTICLE AND FABRICATION METHOD
    35.
    发明申请
    COMPOSITE ARTICLE AND FABRICATION METHOD 有权
    复合材料和制造方法

    公开(公告)号:US20100239842A1

    公开(公告)日:2010-09-23

    申请号:US12789787

    申请日:2010-05-28

    Inventor: Wayde R. Schmidt

    Abstract: A refractory metal composite article includes a refractory metal ceramic section and a refractory metal ceramic coating disposed directly adjacent to the refractory metal ceramic section. The refractory metal ceramic section and the refractory metal ceramic coating form a composite porous matrix. Each of the refractory metal ceramic section and the refractory metal ceramic coating includes at least one of a refractory metal carbide, a refractory metal silicide, or a refractory metal boride. A solid filler is disposed within pores of the composite porous matrix, and the solid filler is selected from a polymer material, a ceramic material, a metallic material, a glass material, and a glass ceramic material.

    Abstract translation: 难熔金属复合制品包括难熔金属陶瓷部分和直接邻近难熔金属陶瓷部分设置的难熔金属陶瓷涂层。 难熔金属陶瓷部分和难熔金属陶瓷涂层形成复合多孔基体。 耐火金属陶瓷部分和难熔金属陶瓷涂层中的每一个包括难熔金属碳化物,难熔金属硅化物或难熔金属硼化物中的至少一种。 固体填料设置在复合多孔基体的孔内,固体填料选自聚合物材料,陶瓷材料,金属材料,玻璃材料和玻璃陶瓷材料。

    LOW TRANSIENT THERMAL STRESS TURBINE ENGINE COMPONENTS
    39.
    发明申请
    LOW TRANSIENT THERMAL STRESS TURBINE ENGINE COMPONENTS 有权
    低瞬态热应力涡轮发动机组件

    公开(公告)号:US20090028697A1

    公开(公告)日:2009-01-29

    申请号:US11829391

    申请日:2007-07-27

    Abstract: A turbine vane includes a platform; and at least one airfoil mounted to the platform and having a trailing edge and a leading edge, wherein the vane is composed of a functionally graded material having a first material and a second material, wherein the trailing edge includes a greater amount of the first material than the second material, and the leading edge includes a greater amount of the second material than the first material.

    Abstract translation: 涡轮叶片包括平台; 以及安装到所述平台并具有后缘和前缘的至少一个翼型件,其中所述叶片由具有第一材料和第二材料的功能梯度材料组成,其中所述后缘包括更大量的所述第一材料 并且前缘包括比第一材料更多的第二材料。

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