Electron beam physical vapor deposition apparatus and crucible therefor
    2.
    发明授权
    Electron beam physical vapor deposition apparatus and crucible therefor 有权
    电子束物理气相沉积设备及其坩埚

    公开(公告)号:US06589351B1

    公开(公告)日:2003-07-08

    申请号:US09624808

    申请日:2000-07-24

    IPC分类号: C23C1600

    摘要: An electron beam physical vapor deposition (EBPVD) apparatus and a method for using the apparatus to produce a coating material (e.g., a ceramic thermal barrier coating) on an article. The EBPVD apparatus generally includes a coating chamber that is operable at elevated temperatures and subatmospheric pressures. An electron beam gun projects an electron beam into the coating chamber and onto a coating material within the chamber, causing the coating material to melt and evaporate. An article is supported within the coating chamber so that vapors of the coating material deposit on the article. The operation of the EBPVD apparatus is enhanced by the inclusion of a crucible that supports the coating material and is configured to be efficiently cooled so as to reduce the rate at which the process temperature increases within the coating chamber.

    摘要翻译: 电子束物理气相沉积(EBPVD)装置和使用该装置在制品上制备涂层材料(例如,陶瓷热障涂层)的方法。 EBPVD设备通常包括可在升高的温度和低于大气压的压力下操作的涂覆室。 电子束枪将电子束投射到涂层室中并且涂覆在腔室内的涂层材料上,导致涂层材料熔化和蒸发。 在涂层室内支撑制品,使得涂层材料的蒸气沉积在制品上。 通过包括支撑涂层材料的坩埚来增强EBPVD装置的操作,并且被配置为被有效地冷却,以便降低涂覆室内工艺温度升高的速度。

    THERMAL BARRIER COATING SYSTEMS
    6.
    发明申请
    THERMAL BARRIER COATING SYSTEMS 审中-公开
    热障涂层系统

    公开(公告)号:US20090162690A1

    公开(公告)日:2009-06-25

    申请号:US11963976

    申请日:2007-12-24

    IPC分类号: B32B15/04

    摘要: Coating system for a metallic substrate includes a strengthened bond coat including a bond coat inner layer and an aluminum-containing layer overlying the bond coat inner layer. The bond coat inner layer is formed by deposition of a bond coat composition including, in weight percent, 14-20% Cr, 5-8% Al, 8-12% Co, 3-7% Ta, 0.1-0.6% Hf, 0.1-0.5% Y, up to about 1% Si, 0.005-0.020% Zr, 0.04-0.08% C, 0.01-0.02% B, with a remainder including Ni and incidental impurities, wherein the bond coat composition is substantially free of rhenium. The coating system includes an optional thermal barrier coating which may be a yttria-stabilized zirconia.

    摘要翻译: 用于金属基材的涂布系统包括包含粘合涂层内层和覆盖在粘合涂层内层上的含铝层的强化粘合涂层。 粘结涂层内层通过沉积粘结涂层组合物形成,该组合物包含重量百分比为14-20%的Cr,5-8%的Al,8-12%的Co,3-7%的Ta,0.1-0.6%的Hf, 0.1-0.5%Y,至多约1%Si,0.005-0.020%Zr,0.04-0.08%C,0.01-0.02%B,余量包括Ni和杂质,其中粘合涂层组合物基本上不含铼 。 涂层系统包括可选的热障涂层,其可以是氧化钇稳定的氧化锆。

    Turbine engine components with environmental protection for interior passages
    9.
    发明授权
    Turbine engine components with environmental protection for interior passages 有权
    涡轮发动机部件具有环境保护用于内部通道

    公开(公告)号:US08545185B2

    公开(公告)日:2013-10-01

    申请号:US11959595

    申请日:2007-12-19

    IPC分类号: F01D5/18

    摘要: Turbine airfoil components with protective layers and methods therefore. The components are each formed to have a platform, an airfoil extending upwardly from the platform, and a shank extending downwardly from the platform. The shank has an exterior wall and an internal passage, and the airfoil has a cooling flow channel inside the airfoil for flowing a cooling flow therethrough. The component has an interior chromide coating contacting at least a portion of an interior surface of the shank and interdiffused with a base metal thereof, and an exterior chromide coating contacting at least a portion of an exterior surface of the shank and interdiffused with the base metal thereof. The interior and exterior chromide coatings do not have an aluminide coating deposited thereon.

    摘要翻译: 涡轮机翼部件具有保护层和方法。 这些部件各自形成为具有平台,从平台向上延伸的翼型件和从平台向下延伸的柄部。 柄具有外壁和内部通道,并且翼型件具有用于使冷却流通过其中的翼型件内的冷却流动通道。 该组件具有内部铬化物涂层,其接触柄的内表面的至少一部分并且与其基体金属相互扩散,并且外部铬化物涂层与柄的外表面的至少一部分接触并与基底金属相互扩散 其中。 内部和外部铬酸盐涂层不具有沉积在其上的铝化物涂层。

    Coatings for gas turbine components
    10.
    发明授权
    Coatings for gas turbine components 有权
    燃气轮机组件涂料

    公开(公告)号:US09297089B2

    公开(公告)日:2016-03-29

    申请号:US13543423

    申请日:2012-07-06

    IPC分类号: C25D3/50 C25D5/50 C25D7/10

    CPC分类号: C25D5/50 C25D7/10

    摘要: A gas turbine component for use in a gas turbine engine includes a substrate and a non-aluminide protective coating with a platinum-group metal. The platinum-group metal resides in a gamma-prime phase of the underlying material. The platinum-group metal can impart the protective coating with superior corrosion-resistance, while the absence of aluminide in the protective coating facilitates use of the protective coating at high-stress and/or high-fatigue portions of the component. The protective coating optionally includes chromide and can also be combined with aluminide at select portions of the component.

    摘要翻译: 用于燃气涡轮发动机的燃气轮机部件包括基体和具有铂族金属的非铝化物保护涂层。 铂族金属位于下层材料的γ'相中。 铂族金属可以使保护涂层具有优异的耐腐蚀性,而保护涂层中不存在铝化物有助于在组件的高应力和/或高疲劳部分使用保护涂层。 保护涂层任选地包括铬化物,并且还可以在组分的选定部分与铝化物组合。