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    • 5. 发明专利
    • Blade groove inspection method of turbine rotor
    • 涡轮转子叶片检查方法
    • JP2009204368A
    • 2009-09-10
    • JP2008045263
    • 2008-02-26
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • AOKI KIYOTAKAFUKUDA TAKASHI
    • G01N29/04
    • PROBLEM TO BE SOLVED: To provide a blade groove inspection method of a turbine rotor, accurately detecting the lug part in the T route type blade groove part provided in the peripheral direction of the turbine rotor, or the side entry type blade groove part provided in the axial direction of the turbine rotor without drawing out a turbine blade.
      SOLUTION: The echo waveform of a health part in the echo produced by the reflection reaching the lug part in the T route type blade groove part is compared with the echo waveform of a flaw part in the echo in the case of a T route type implanted part while focusing an ultrasonic wave on a point using a phase array type ultrasonic probe, a transmission part and a receiving part are arranged in the diametric direction of the turbine rotor in the case of a side entry type implanted part and the ultrasonic wave is point-focused to the side entry type implanted part, so that the ultrasonic wave reflected from the flaw part is reflected from the other surface being an opposed surface to detect a rotor blade groove shaped echo and a flaw leading end part echo to evaluate the presence of the flaw.
      COPYRIGHT: (C)2009,JPO&INPIT
    • 要解决的问题:为了提供一种涡轮转子的叶片槽检查方法,精确地检测在涡轮转子的周向设置的T型叶片槽部中的凸耳部或侧入口型叶片槽 部分设置在涡轮转子的轴向上,而不抽出涡轮叶片。

      解决方案:在T路径型刀片槽部分中的到达凸缘部分的反射产生的回波中的健康部分的回波波形与T中的回波中的缺陷部分的回波波形进行比较 在侧向入射型植入部的情况下,使用相位阵列型超声波探头,透射部和接收部在超声波聚焦超声波的方式配置在涡轮转子的直径方向,并且超声波 波是点对焦于侧入型植入部分,使得从缺陷部反射的超声波从作为相对表面的另一表面反射,以检测转子叶片槽形回波和缺陷前端部回波以评估 存在缺陷。 版权所有(C)2009,JPO&INPIT