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Structural integrity diagnostic system, structural integrity diagnostic method and aircraft structure

机译:结构完整性诊断系统,结构完整性诊断方法和飞机结构

摘要

PROBLEM TO BE SOLVED: To reduce restrictions in structural soundness diagnosis of a structure and improve defect detection accuracy. A structural soundness diagnosis system according to an embodiment is a structure having a plate-shaped first inspection area having no bent portion and a second inspection area including a bent plate-shaped portion. It is a structural soundness diagnosis system that performs structural soundness diagnosis of the above, and is an ultrasonic vibrator that oscillates ultrasonic waves in the first inspection area, and the transmitted waves of the ultrasonic waves that have passed through the first inspection area. An ultrasonic sensor that detects at least one waveform of the reflected wave of the ultrasonic waves reflected in the first inspection area, a strain sensor that detects the amount of distortion in the second inspection area, and an ultrasonic sensor that detects it. A signal processing unit that obtains an index indicating the soundness of the structure including the first inspection area and the second inspection area based on the generated waveform and the strain amount detected by the strain sensor. And have. [Selection diagram] Fig. 7
机译:要解决的问题:减少结构声音诊断的限制,提高缺陷检测精度。根据实施例的结构声音诊断系统是具有不具有弯曲部分的板状第一检查区域和包括弯曲板状部分的第二检查区域的结构。它是一种结构声音诊断系统,其执行上述结构声音诊断,并且是超声振动器,其振荡在第一检查区域中的超声波,以及通过第一检查区域的超声波的透射波。超声波传感器,其检测在第一检查区域中反射的超声波的反射波的至少一个波形,该应变传感器检测第二检查区域中的失真量,以及检测其的超声波传感器。一种信号处理单元,其获得指示包括第一检查区域和第二检查区域的结构的声音的索引,其基于所产生的波形和由应变传感器检测的应变量。并且有。 [选择图]图7

著录项

  • 公开/公告号JP2021156721A

    专利类型

  • 公开/公告日2021-10-07

    原文格式PDF

  • 申请/专利权人 株式会社SUBARU;

    申请/专利号JP20200056962

  • 发明设计人 副島 英樹;中野 拓也;

    申请日2020-03-27

  • 分类号G01N29/032;

  • 国家 JP

  • 入库时间 2022-08-24 21:32:04

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