Method for coating turbine engine components with high velocity particles
    1.
    发明申请
    Method for coating turbine engine components with high velocity particles 审中-公开
    用高速颗粒涂覆涡轮发动机部件的方法

    公开(公告)号:US20060269685A1

    公开(公告)日:2006-11-30

    申请号:US11142055

    申请日:2005-05-31

    CPC分类号: C23C24/04

    摘要: A method for coating a surface of a metal component comprises the steps of cold gas-dynamic spraying a powder material on the metal component surface to form a coating, the powder material being sufficiently heated to impact the metal component surface at between about 30% and about 70% of the powder material's melting temperature in kelvins. Another method for coating a surface of a metal component using a powder material comprises the steps of heating the metal component surface to between about 30% and about 70% of the substrate's melting temperature, and then of the powder material's melting temperature in kelvins, and cold gas-dynamic spraying the powder material on the metal component surface to form a coating.

    摘要翻译: 用于涂覆金属部件表面的方法包括以下步骤:在金属部件表面上冷气动态喷射粉末材料以形成涂层,粉末材料被充分加热以在金属部件表面之间约30%和 约70%的粉末材料在开尔文的熔化温度。 使用粉末材料涂覆金属组分的表面的另一种方法包括以下步骤:将金属组分表面加热到基材的熔融温度的约30%至约70%之间,然后将粉末材料的熔融温度加热到开尔文, 冷却气体动力地将粉末材料喷涂在金属部件表面上以形成涂层。

    Magnesium repair and build up
    2.
    发明申请
    Magnesium repair and build up 有权
    镁修复和建立

    公开(公告)号:US20060240192A1

    公开(公告)日:2006-10-26

    申请号:US11114470

    申请日:2005-04-25

    IPC分类号: B05D3/12

    CPC分类号: C23C24/04

    摘要: The present invention provides methods and materials for use in applying a coating on a surface of a magnesium component. The method includes the steps of: accelerating a coating powder to a velocity of between about 500 to about 1200 meters/second, wherein the coating powder comprises a material selected from the group consisting of aluminum, aluminum alloys, titanium, titanium alloys, and composites; directing the coating powder through a convergent-divergent nozzle onto the surface of the magnesium component; and forming a coating on the surface of the magnesium component so as to substantially cover the surface of the magnesium component. The coating thickness may be between approximately 0.1 to approximately 1.0 mm.

    摘要翻译: 本发明提供了用于在镁组分的表面上施加涂层的方法和材料。 该方法包括以下步骤:将涂层粉末加速至约500至约1200米/秒的速度,其中涂层粉末包括选自铝,铝合金,钛,钛合金和复合材料的材料 ; 将涂层粉末通过会聚扩散喷嘴引导到镁组分的表面上; 并在镁组分的表面上形成涂层,以便基本上覆盖镁组分的表面。 涂层厚度可以在约0.1至约1.0mm之间。

    Method for producing functionally graded coatings using cold gas-dynamic spraying
    3.
    发明申请
    Method for producing functionally graded coatings using cold gas-dynamic spraying 审中-公开
    使用冷气动喷涂生产功能梯度涂层的方法

    公开(公告)号:US20070098912A1

    公开(公告)日:2007-05-03

    申请号:US11261063

    申请日:2005-10-27

    IPC分类号: B05D1/08 H05H1/26

    CPC分类号: C23C24/04

    摘要: A method is provided for forming a graded coating on a surface of a substrate. The method comprises the step of cold gas-dynamic spraying powder mixtures on the substrate surface to form the graded coating thereon. The method does not distort the substrate and does not require the use of an apparatus that needs to be stopped and re-started each time the composition of the graded coating changes. Moreover, the method is generally inexpensive, efficient, and yields high quality graded coatings.

    摘要翻译: 提供了一种在衬底的表面上形成渐变涂层的方法。 该方法包括在基材表面上冷气体动态喷涂粉末混合物以在其上形成分级涂层的步骤。 该方法不会使基板变形,并且不需要使用每次分级涂层的组成改变时需要停止和重新启动的装置。 此外,该方法通常是廉价,有效的,并且产生高质量的分级涂层。

    Cold gas-dynamic spraying method for joining ceramic and metallic articles
    4.
    发明申请
    Cold gas-dynamic spraying method for joining ceramic and metallic articles 审中-公开
    用于连接陶瓷和金属制品的冷气体动态喷涂方法

    公开(公告)号:US20070215677A1

    公开(公告)日:2007-09-20

    申请号:US11376669

    申请日:2006-03-14

    IPC分类号: B23K31/02

    摘要: A method for joining a first component surface to a ceramic component surface includes cold gas-dynamic spraying a first metal powder onto the ceramic component surface to form a first metal coating. The first component surface is then bonded to the metal coating on the ceramic component surface. The bonding step may be a thermal process such as a brazing process. A mechanical bond may also be formed by an interference fitting such as press or shrink fitting.

    摘要翻译: 将第一组分表面与陶瓷组分表面接合的方法包括将第一金属粉末冷却气体动态喷涂到陶瓷组件表面上以形成第一金属涂层。 然后将第一组分表面结合到陶瓷组件表面上的金属涂层。 接合步骤可以是诸如钎焊工艺的热处理。 机械接合也可以通过诸如压力或收缩配合的干涉配件形成。

    Methods for coating a magnesium component
    5.
    发明授权
    Methods for coating a magnesium component 有权
    涂覆镁组分的方法

    公开(公告)号:US07455881B2

    公开(公告)日:2008-11-25

    申请号:US11114470

    申请日:2005-04-25

    IPC分类号: B05D1/02

    CPC分类号: C23C24/04

    摘要: The present invention provides methods and materials for use in applying a coating on a surface of a magnesium component. The method includes the steps of: accelerating a coating powder to a velocity of between about 500 to about 1200 meters/second, wherein the coating powder comprises a material selected from the group consisting of aluminum, aluminum alloys, titanium, titanium alloys, and composites; directing the coating powder through a convergent-divergent nozzle onto the surface of the magnesium component; and forming a coating on the surface of the magnesium component so as to substantially cover the surface of the magnesium component. The coating thickness may be between approximately 0.1 to approximately 1.0 mm.

    摘要翻译: 本发明提供了用于在镁组分的表面上施加涂层的方法和材料。 该方法包括以下步骤:将涂层粉末加速至约500至约1200米/秒的速度,其中涂层粉末包括选自铝,铝合金,钛,钛合金和复合材料的材料 ; 将涂层粉末通过会聚扩散喷嘴引导到镁组分的表面上; 并在镁组分的表面上形成涂层,以便基本上覆盖镁组分的表面。 涂层厚度可以在约0.1至约1.0mm之间。

    Thermal barrier coating resistant to penetration by environmental contaminants
    6.
    发明申请
    Thermal barrier coating resistant to penetration by environmental contaminants 有权
    隔热涂层耐环境污染物渗透

    公开(公告)号:US20070036997A1

    公开(公告)日:2007-02-15

    申请号:US11170836

    申请日:2005-06-30

    IPC分类号: B32B15/04 B32B9/00

    摘要: A turbine engine component includes an electron beam-physical vapor deposition thermal barrier coating covering at least a portion of a substrate. The thermal barrier coating includes an inner layer having a columnar-grained microstructure with inter-columnar gap porosity. The inner layer includes a stabilized ceramic material. The thermal barrier coating also includes a substantially non-porous outer layer, covering the inner layer and including the stabilized ceramic material. The outer layer is deposited with continuous line-of-sight exposure to the vapor source under oxygen deficient conditions. The outer layer may further comprise a dopant oxide that is more readily reducible than the stabilized ceramic material. During deposition, the outer layer may also have an oxygen deficient stoichiometry with respect to the inner layer. Oxygen stoichiometry in the outer layer may be restored by exposure of the coated component to an oxidizing environment.

    摘要翻译: 涡轮发动机部件包括覆盖基板的至少一部分的电子束物理气相沉积热障涂层。 隔热涂层包括具有柱状间隙孔隙的柱状微结构的内层。 内层包括稳定的陶瓷材料。 热障涂层还包括基本上无孔的外层,覆盖内层并且包括稳定的陶瓷材料。 在缺氧条件下,外层沉积有连续的视线暴露于蒸汽源。 外层还可以包含比稳定的陶瓷材料更容易还原的掺杂剂氧化物。 在沉积期间,外层也可能具有相对于内层的缺氧化学计量。 可以通过将涂覆的组分暴露于氧化环境来恢复外层中的氧化学计量。

    Method for coating turbine engine components with metal alloys using high velocity mixed elemental metals
    7.
    发明申请
    Method for coating turbine engine components with metal alloys using high velocity mixed elemental metals 审中-公开
    使用高速混合元素金属用金属合金涂覆涡轮发动机部件的方法

    公开(公告)号:US20070098913A1

    公开(公告)日:2007-05-03

    申请号:US11261068

    申请日:2005-10-27

    IPC分类号: B05D1/08 H05H1/24

    CPC分类号: C23C24/04

    摘要: A plurality of powders is admixed to form a substantially homogenous powder mixture comprising each of the alloy elements. At least one of the powders consists essentially of a substantially pure elemental metal. The substantially homogenous powder mixture is cold gas-dynamic sprayed on the substrate to form a coating of the alloy elements. The coating is then heated until the alloy elements inter-diffuse and form the alloy. In an exemplary embodiment, the substantially homogenous powder mixture includes stoichiometric amounts of each of the alloy elements, and each of the powders consists essentially of a substantially pure form of one of the alloy elements.

    摘要翻译: 将多种粉末混合以形成包含每种合金元素的基本均匀的粉末混合物。 至少一种粉末基本上由基本上纯的元素金属组成。 基本上均匀的粉末混合物是冷气体动态喷涂在基材上以形成合金元素的涂层。 然后加热涂层直到合金元素互相扩散并形成合金。 在一个示例性实施方案中,基本均匀的粉末混合物包括化学计量的每种合金元素,并且每种粉末基本上由合金元素之一的基本上纯的形式组成。

    Chromium and active elements modified platinum aluminide coatings
    8.
    发明申请
    Chromium and active elements modified platinum aluminide coatings 有权
    铬和活性元素改性的铂铝化物涂层

    公开(公告)号:US20060046091A1

    公开(公告)日:2006-03-02

    申请号:US10928545

    申请日:2004-08-26

    IPC分类号: B32B19/00 B32B9/00

    摘要: The present invention provides a chromium and active elements modified platinum aluminide coating that may be used on a surface of a gas turbine engine component such as a turbine blade. The coating may be used as a protective coating that impedes the progress of corrosion, oxidation, and sulfidation in superalloy materials that comprise the substrate of the turbine blade. Additionally, the coating may be used as a bond coat onto which a thermal barrier coating is deposited. The presence of active elements as well as chromium and platinum provides improved corrosion, oxidation, and sulfidation resistance. The coating is applied using an electron beam physical vapor deposition. The coating is applied alternatively using selected sequential diffusion processing steps involving chromium, platinum and aluminum.

    摘要翻译: 本发明提供了可用于诸如涡轮叶片的燃气涡轮发动机部件的表面上的铬和活性元素改性的铂铝化物涂层。 该涂层可以用作阻碍在构成涡轮叶片的基底的超级合金材料中的腐蚀,氧化和硫化进程的保护涂层。 此外,涂层可以用作粘合涂层,其上沉积有热障涂层。 活性元素以及铬和铂的存在提供了改善的腐蚀,氧化和耐硫化性。 使用电子束物理气相沉积涂覆涂层。 使用包括铬,铂和铝的选择的顺序扩散处理步骤交替施加涂层。

    Method for coating turbine engine components with rhenium alloys using high velocity-low temperature spray process
    9.
    发明申请
    Method for coating turbine engine components with rhenium alloys using high velocity-low temperature spray process 审中-公开
    使用高速低温喷涂工艺用铼合金涂覆涡轮发动机部件的方法

    公开(公告)号:US20070116890A1

    公开(公告)日:2007-05-24

    申请号:US11285044

    申请日:2005-11-21

    IPC分类号: H05H1/24

    摘要: A method of forming a wear-resistant coating on a substrate surface includes the step of cold gas-dynamic spraying a material comprising a rhenium-based composition onto the substrate surface. A metal layer may be formed on the substrate surface prior to the cold gas-dynamic spraying step, and a heat treatment may be performed after the gold gas-dynamic spraying step.

    摘要翻译: 在基材表面上形成耐磨涂层的方法包括将包含铼基组合物的材料冷气动态喷涂到基材表面上的步骤。 在冷气动态喷涂步骤之前,可以在基板表面上形成金属层,并且可以在金气动态喷涂步骤之后进行热处理。

    Method for repairing titanium alloy components
    10.
    发明申请
    Method for repairing titanium alloy components 审中-公开
    修复钛合金部件的方法

    公开(公告)号:US20060045785A1

    公开(公告)日:2006-03-02

    申请号:US10930506

    申请日:2004-08-30

    IPC分类号: B22F7/04

    摘要: A method for repairing a titanium alloy surface of a turbine component includes the step of cold gas-dynamic spraying a powder material comprising at least one titanium alloy directly on the titanium alloy surface. The method may further include the steps of hot isostatic pressing the cold gas-dynamic sprayed turbine component, and performing a separate heat treating step after the hot isostatic pressing. Thus, the cold gas-dynamic spray process and post-spray processing can be employed to effectively repair degraded areas on compressor turbine components.

    摘要翻译: 一种用于修复涡轮机部件的钛合金表面的方法包括将包含至少一种钛合金的粉末材料直接在钛合金表面上进行冷气动态喷射的步骤。 该方法可以进一步包括热等静压式冷气动喷射涡轮机部件的步骤,以及在热等静压之后执行单独的热处理步骤。 因此,可以采用冷气体动态喷雾处理和后喷雾处理来有效地修复压缩机涡轮机部件的退化区域。