ALLOY WITH ION BOMBARDED SURFACE FOR ENVIRONMENTAL PROTECTION
    1.
    发明申请
    ALLOY WITH ION BOMBARDED SURFACE FOR ENVIRONMENTAL PROTECTION 审中-公开
    与环氧树脂合金表面进行环境保护

    公开(公告)号:WO2012040484A3

    公开(公告)日:2012-05-18

    申请号:PCT/US2011052790

    申请日:2011-09-22

    Abstract: An article may include a substrate that comprises a nickel alloy. The substrate may include a modified subsurface region and a bulk region. The modified subsurface region may include a first composition and the bulk region may include a second composition different than the first composition. The modified subsurface region may include at least one of a reactive element or a noble metal, and the modified subsurface region comprises a thickness of less than about 0.3 µm measured in a direction substantially normal to a surface of the substrate. The modified subsurface region may be formed by depositing a layer including at least one of the reactive element or the noble metal in a layer on a surface of the substrate and introducing the at least one of the reactive element or the noble metal into the modified subsurface region using ion bombardment.

    Abstract translation: 制品可以包括包含镍合金的基底。 衬底可以包括改性的地下区域和体区域。 修饰的地下区域可以包括第一组合物,并且本体区域可以包括不同于第一组合物的第二组合物。 修饰的地下区域可以包括反应性元素或贵金属中的至少一种,并且改性的表面下区域包括在基本上垂直于基底的表面的方向上测量的小于约0.3μm的厚度。 可以通过将包含至少一个反应元件或贵金属的层沉积在基板的表面上的层中并将至少一个反应元件或贵金属引入修饰的地下表面中来形成修饰的地下区域 区域使用离子轰击。

    SUBSTRATE FEATURES FOR MITIGATING THERMAL STRESS ON AN ARTICLE COATED WITH A THERMAL BARRIER COATING

    公开(公告)号:SG168491A1

    公开(公告)日:2011-02-28

    申请号:SG2010052389

    申请日:2010-07-16

    Abstract: An article may include an array of features formed in a substrate and may be coated with a coating layer. The array of features may mitigate stress experienced by the coated article. In particular, the array of features may reduce or limit crack propagation at the interface between the substrate and the coating layer. In some examples, the article is an airfoil that includes a tip that defines an edge. An array of features is formed on the surface of the tip, where the array of features is proximate to the edge, and the array of features does not intersect the edge. The airfoil includes a coating layer formed on the surface of the tip and the array of features. FIG.4,14B,14C

    SUBSTRATE FEATURES FOR MITIGATING STRESS

    公开(公告)号:SG168492A1

    公开(公告)日:2011-02-28

    申请号:SG2010052397

    申请日:2010-07-16

    Abstract: An article may include an array of features formed in a substrate and may be coated by a thermal barrier coating (TBC). The array of features may mitigate thermal stress experienced by the coated article. In particular, the array of features may reduce or limit crack propagation at or above the interface of a thermally insulative layer and a bond coat in the TBC. In some embodiments, the array may be formed proximate to and substantially aligned with cooling holes formed in the substrate. In other embodiments, an article may include a first array of features formed in a first location of a substrate and a second array of features formed in a second location of a substrate. The first and second locations may be determined or selected based on a prediction of thermal stresses that the substrate will experience at the first and second locations during use. FIG. 1B

    SUBSTRATE FEATURES FOR MITIGATING STRESS

    公开(公告)号:CA2711175A1

    公开(公告)日:2011-01-17

    申请号:CA2711175

    申请日:2010-07-16

    Abstract: An article may include an array of features formed in a substrate and may be coated with a coating layer. The array of features may mitigate stress experienced by the coated article. In particular, the array of features may reduce or limit crack propagation at the interface between the substrate and the coating layer. In some examples, the article is an airfoil that includes a tip that defines an edge. An array of features is formed on the surface of the tip, where the array of features is proximate to the edge, and the array of features does not intersect the edge. The airfoil includes a coating layer formed on the surface of the tip and the array of features.

    ABRADABLE COATING FOR COMPONENTS IN HIGH-TEMPERATURE MECHANICAL SYSTEMS

    公开(公告)号:CA3051995A1

    公开(公告)日:2020-02-21

    申请号:CA3051995

    申请日:2019-08-14

    Abstract: An article may include a substrate including a metal or alloy; a bond coat directly on the substrate; an intermediate ceramic layer on the bond coat; and an abradable ceramic layer directly on the intermediate ceramic layer. The intermediate ceramic layer includes a stabilized tetragonal prime phase constitution and defines a first porosity. The abradable ceramic layer includes zirconia or hafnia stabilized in the tetragonal prime phase by a second mixture including between about 5 wt. % and about 10 wt. % ytterbia, between about 0.5 wt. % and about 2.5 wt. % samaria, and between about 1 wt. % and about 4 wt. % of at least one of lutetia, scandia, ceria, neodymia, europia, or gadolinia, and a balance zirconia or hafnia. The abradable ceramic layer defines a second porosity, and the second porosity is higher than the first porosity.

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