Method for in-situ eddy current inspection of coated components in turbine engines
    22.
    发明授权
    Method for in-situ eddy current inspection of coated components in turbine engines 失效
    涡轮发动机涂层部件原位涡流检测方法

    公开(公告)号:US06707297B2

    公开(公告)日:2004-03-16

    申请号:US10122836

    申请日:2002-04-15

    IPC分类号: G01N2782

    CPC分类号: G01N27/9046

    摘要: A method for in-situ eddy current inspection of at least one coated component includes applying a drive pulse at a measurement position on an outer surface of the coated component, while the coated component is installed in an operational environment of the coated component. The coated component includes a base metal and a coating disposed on the base metal. The method further includes receiving a response signal from the coated component, comparing the response signal with a reference signal to obtain a compared signal, analyzing the compared signal for crack detection, and determining whether a crack near the measurement position has penetrated into the base metal, if the presence of the crack in the coating is indicated.

    摘要翻译: 用于至少一个涂覆部件的原位涡流检查的方法包括在涂覆部件的外表面上的测量位置处施加驱动脉冲,同时将涂覆部件安装在涂覆部件的操作环境中。 涂覆的部件包括贱金属和设置在母材上的涂层。 该方法还包括从涂覆部件接收响应信号,将响应信号与参考信号进行比较以获得比较信号,分析用于裂纹检测的比较信号,以及确定测量位置附近的裂纹是否穿透到基底金属 如果指示涂层中存在裂纹。