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    • 3. 发明授权
    • Method of forming a thermal barrier coating system
    • 形成热障涂层系统的方法
    • US06447854B1
    • 2002-09-10
    • US09621422
    • 2000-07-21
    • David V. RigneyAntonio F. MaricocchiDavid J. WortmanRobert W. BruceJoseph D. Rigney
    • David V. RigneyAntonio F. MaricocchiDavid J. WortmanRobert W. BruceJoseph D. Rigney
    • C23C1430
    • C23C14/083C23C14/566
    • A method for producing a thermal barrier coating system on an article that will be subjected to a hostile environment. The thermal barrier coating system is composed of a metallic bond coat and a ceramic thermal barrier coating having a columnar grain structure. The method generally entails forming the bond coat on the surface of a component, and then grit blasting the bond coat with an abrasive media having a particle size of greater than 80 mesh. The component is then supported within a coating chamber containing at least two ingots of the desired ceramic material. An absolute pressure of greater than 0.014 mbar is established within the chamber containing oxygen and an inert gas. Thereafter, the ceramic ingots are vaporized with an electron beam such that the vapor deposits on the surface of the component to form a layer of the ceramic material on the surface.
    • 一种在受到恶劣环境的制品上制备热障涂层系统的方法。 热障涂层系统由金属粘合涂层和具有柱状晶粒结构的陶瓷热障涂层组成。 该方法通常需要在部件的表面上形成粘合涂层,然后用具有大于80目的粒度的研磨介质喷砂粘结涂层。 然后将该组分支撑在包含至少两个所需陶瓷材料锭的涂覆室内。 在含有氧气和惰性气体的室内建立大于0.014毫巴的绝对压力。 此后,陶瓷锭用电子束蒸发,使得蒸汽沉积在部件的表面上以在表面上形成陶瓷材料层。
    • 5. 发明授权
    • Apparatus and method for gas phase coating of hollow articles
    • 中空制品气相涂层装置及方法
    • US5368888A
    • 1994-11-29
    • US945755
    • 1992-09-16
    • David V. Rigney
    • David V. Rigney
    • C23C10/06C23C16/04C23C16/458C23C8/36
    • C23C16/045C23C10/06C23C16/458
    • Apparatus and method for simultaneously coating interior and exterior surfaces of articles, such as advanced turbine airfoils, the interior surfaces defined by narrow, complex passageways. The apparatus and method, in addition to providing for simultaneous coating of interior and exterior surfaces, also permits additional control over the coating process by permitting control over the partial pressure of reactive gas introduced into the reaction chamber. The apparatus also permits for subsequent thermal treatment of the coated parts in an inert gas atmosphere with no intermediate cooling step thereby reducing costs while eliminating the potential for damage due to handling by the elimination of at least one handling operation.
    • 用于同时涂覆物品的内部和外部表面的装置和方法,例如先进的涡轮机翼型,由狭窄的复杂通道限定的内表面。 除了提供内表面和外表面的同时涂布之外,该设备和方法还允许通过允许控制引入反应室的反应气体的分压来对涂布过程进行附加控制。 该装置还允许在惰性气体气氛中随后热处理涂覆部件,而不需要中间冷却步骤,从而降低成本,同时消除由于通过消除至少一个操作操作而导致的损坏的可能性。
    • 8. 发明授权
    • Apparatus and method for gas phase coating of hollow articles
    • 中空制品气相涂层装置及方法
    • US5221354A
    • 1993-06-22
    • US787466
    • 1991-11-04
    • David V. Rigney
    • David V. Rigney
    • C23C10/06C23C16/04C23C16/458
    • C23C16/045C23C10/06C23C16/458
    • Apparatus and method for simultaneously coating interior and exterior surfaces of articles, such as advanced turbine airfoils, the interior surfaces defined by narrow, complex passageways. The apparatus and method, in addition to providing for simultaneous coating of interior and exterior surfaces, also permits additional control over the coating process by permitting control over the partial pressure of reactive gas introduced into the reaction chamber. The apparatus also permits for subsequent thermal treatment of the coated parts in an inert gas atmosphere with no intermediate cooling step thereby reducing costs while eliminating the potential for damage due to handling by the elimination of at least one handling operation.
    • 用于同时涂覆物品的内部和外部表面的装置和方法,例如先进的涡轮机翼型,由狭窄的复杂通道限定的内表面。 除了提供内表面和外表面的同时涂布之外,该设备和方法还允许通过允许控制引入反应室的反应气体的分压来对涂布过程进行附加控制。 该装置还允许在惰性气体气氛中随后热处理涂覆部件,而不需要中间冷却步骤,从而降低成本,同时消除由于通过消除至少一个操作操作而导致的损坏的可能性。