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    • 5. 发明授权
    • Coated component and production process
    • 涂层成分及生产工艺
    • US07556851B2
    • 2009-07-07
    • US11330577
    • 2006-01-12
    • Stefan Lampenscherf
    • Stefan Lampenscherf
    • B32B15/04B32B3/10
    • G01K11/20Y10T428/12611Y10T428/12771Y10T428/12778Y10T428/24289Y10T428/24298Y10T428/24314Y10T428/24331
    • The invention relates to a coated turbine component adapted for exposure to a hot gas flow, comprising a component body comprising a base material, a thermal barrier coating applied to the base material, and a thermographic phosphor arranged within, on or beneath the thermal barrier coating surface adapted to emit light corresponding to a temperature of the thermographic phosphor. The invention also relates to a method for producing a coated turbine component comprising applying a first thermal barrier coating containing an activator to a component body base material, the activator providing the thermal barrier layer coating with thermographic properties such that light is emitted corresponding to a temperature of the thermographic phosphor, applying a second thermal barrier coating that does not contain the activator on top of the first thermal barrier coating, and removing a portion of the second thermal barrier coating to expose the thermographic phosphor layer underlying the second thermal barrier coating. The invention also relates to a method for producing a coated turbine component comprising applying a thermal barrier coating to a component body, trenching the thermal barrier coating to form a base at the bottom of the trench and applying a thermographic phosphor to the base of the trench.
    • 本发明涉及一种适用于暴露于热气流的涂覆涡轮机部件,包括一个组件主体,该组件主体包括一个基体材料,一个施加到基材的热障涂层,以及一个布置在热障涂层内或之上的热敏照相荧光粉 表面适于发射对应于热敏照相荧光体的温度的光。 本发明还涉及一种用于生产涂覆的涡轮机部件的方法,包括将包含活化剂的第一热障涂层施加到部件主体基材上,所述活化剂为热障层涂层提供热成型性质,使得光对应于温度 的热成像荧光体,在第一热障涂层的顶部上施加不包含活化剂的第二热障涂层,以及去除第二热障涂层的一部分以暴露第二热障涂层下面的热敏照相荧光体层。 本发明还涉及一种用于制造涂覆的涡轮机部件的方法,包括将热障涂层施加到部件主体上,将该热障涂层开沟,以在该沟槽的底部形成底座,并将该热敏成像荧光体施加到该沟槽的底部 。