航空学报 > 2020, Vol. 41 Issue (1): 423111-423111   doi: 10.7527/S1000-6893.2019.23111

飞机铆接件隐藏缺陷的远场涡流检测探头优化与试验

赵本勇1, 宋凯1, 宁宁2, 黄华斌2, 张丽攀1   

  1. 1. 南昌航空大学 无损检测技术教育部重点实验室, 南昌 330063;
    2. 中国飞机强度研究所, 西安 710065
  • 收稿日期:2019-04-25 修回日期:2019-05-18 出版日期:2020-01-15 发布日期:2019-09-09
  • 通讯作者: 张丽攀 E-mail:89425434@qq.com
  • 基金资助:
    国家自然科学基金(51865033);国家重大科学仪器设备开发专项(2013YQ140505);航空科学基金(20160956002);无损检测技术教育部重点实验室开放基金(EW201708252)

Optimization and experimentation of remote field eddy current testing probe for hidden defects of aircraft riveting parts

ZHAO Benyong1, SONG Kai1, NING Ning2, HUANG Huabin2, ZHANG Lipan1   

  1. 1. Key Laboratory of Nondestructive Testing, Ministry of Education, Nanchang Hangkong University, Nanchang 330063, China;
    2. Aircraft Strength Research Institute, Xi'an 710065, China
  • Received:2019-04-25 Revised:2019-05-18 Online:2020-01-15 Published:2019-09-09
  • Supported by:
    National Natural Science Foundation of China (51865033);National Major Scientific Instruments and Equipment Development Project (2013YQ140505);Aeronautical Science Foundation of China (20160956002);Open Foundation for key Laboratory of Nondestructive Testing of Ministry of Education of China (EW201708252)

摘要: 远场涡流检测技术因检测深度深和检测结果可靠性高等诸多优点适合飞机多层金属铆接构件的快速检测。针对飞机铆接件铆钉孔沿边隐藏裂纹的原位检测,建立了多层金属铆接构件隐藏缺陷平面远场涡流检测有限元模型,对激励线圈内径、磁路结构以及屏蔽阻尼进行了仿真优化,研制了激励线圈和检测线圈均带组合屏蔽结构的传感器,采用激励-检测线圈环绕铆钉旋转扫描的方式,研究多层金属铆接构件铆钉孔沿边隐藏裂纹信号特征。仿真与试验结果表明:罐形磁芯聚磁效果是柱形磁芯的1.85倍,采用铝+铜组合屏蔽罩能够将远场区提前10 mm,检测线圈位于缺陷正上方时,检测信号的幅值和相位存在极大值,且极大值随着缺陷埋深的增加逐渐下降,研究成果可望用于指导飞机多层金属铆接构件的工程检测实践。

关键词: 无损检测, 远场涡流, 铆接构件, 屏蔽阻尼, 沿边裂纹

Abstract: The remote field eddy current testing technique features a deep depth of detection, high reliability of detection results, and many other advantages, which make it suitable for rapid detection of multi-layer metal riveting components. Aiming at the in-situ detection of hidden cracks along the rivet holes of aircraft riveting, the finite element model for the remote field eddy current detection of the hidden crack plane of multi-layer metal riveting members is established. The inner diameter of exciting coli, magnetic circuit structure, and shielding damping are simulated and optimized. The exciting coil and the detecting coil are combined with the shielding structure. The characteristics of hidden crack signals along the rivet holes of multi-layer metal riveting members are studied. The simulation and experimental results show that the tank shape of the magnetic core is 1.85 times that of the cylindrical of the magnetic core. The shield of the aluminum cover + copper cover can advance the remote field by 10 mm. When the detection coil is directly above the defect, the detected amplitude of the signal value and phase reach the maximum values. And the maximum value decreases with the increase of the buried depth of the defect. The research results are expected to be used to guide the engineering inspection practice of the multi-layer metal riveted components of the aircraft.

Key words: nondestructive testing, remote field eddy current, riveted structure, shield damping, defect around hole

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