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Ultrasonic flaw detection system, ultrasonic flaw detection method and aircraft structure

机译:超声波探伤系统,超声波探伤方法及飞机结构

摘要

According to one implementation, an ultrasonic test system includes at least one ultrasonic transducer, at least one ultrasonic sensor and a damage detection part composed of at least circuitry. The at least one ultrasonic transducer transmits an ultrasonic wave toward at least one test region. The at least one ultrasonic sensor detects the ultrasonic wave which has passed through the at least one test region. The damage detection part is configured to detect whether there is a damage in the at least one test region, based on a difference between a waveform corresponding to the ultrasonic wave detected by the at least one ultrasonic sensor and a reference waveform. The at least one ultrasonic transducer and the at least one ultrasonic sensor are disposed at positions which apart from each other with an interval longer than 300 mm.
机译:根据一种实施方式,一种超声测试系统包括至少一个超声换能器,至少一个超声传感器以及由至少电路组成的损坏检测部分。至少一个超声换能器朝着至少一个测试区域发射超声波。至少一个超声波传感器检测已经通过至少一个测试区域的超声波。损伤检测部被配置为基于与由至少一个超声波传感器检测出的超声波对应的波形与基准波形之间的差,来检测至少一个测试区域中是否存在损伤。至少一个超声换能器和至少一个超声传感器布置在彼此间隔大于300mm的位置处。

著录项

  • 公开/公告号JP6317708B2

    专利类型

  • 公开/公告日2018-04-25

    原文格式PDF

  • 申请/专利权人 株式会社SUBARU;

    申请/专利号JP20150118956

  • 发明设计人 高橋 孝平;副島 英樹;

    申请日2015-06-12

  • 分类号G01N29/46;G01N29/48;

  • 国家 JP

  • 入库时间 2022-08-21 13:07:34

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