脉冲涡流旋转式差分探头设计及飞机多层铆接结构实验测试
DOI:
CSTR:
作者:
作者单位:

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

作者简介:

通讯作者:

中图分类号:

TG115.28TH878

基金项目:

国家重点研发计划(2024YFB3214300)、中央军委装备发展部“慧眼行动”(BF28883A)、江西省自然科学基金(20253BAC280090,20252BAC240318)项目资助


Design of pulsed eddy current rotational differential probe and experimental testing for multi-layer riveted structure of aircraft
Author:
Affiliation:

1.Key Laboratory of Nondestructive Testing of MOE, Nanchang Hangkong University, Nanchang 330063, China; 2.China Aircraft Strength Research Institute, Xi′an 710065, China

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    飞机机身重要承力结构多采用铆接方式装配,铆接部位内部极易萌生疲劳裂纹,及时发现裂纹并获取其位置、长度等信息,对结构损伤评估与维修工作具有重要意义。传统的无损检测技术难以在在役情况下对其进行检测,而脉冲涡流检测技术渗透深度大、检测信息丰富,对深层埋藏缺陷检测具有较大优势。针对飞机铆接结构铆钉孔埋藏缺陷的检测,设计了一种脉冲涡流旋转式差分探头,探头配备水平放置的矩形激励线圈和两个隧道磁阻(TMR)传感器,并开设中央圆孔以通过铆钉头部,减小结构干涉。随后,研究了绝对式探头与差分式探头的旋转检测原理,通过理论推导得到两种探头旋转检测的缺陷信号表达式,并分析两种探头的差异性。接下来,搭建脉冲涡流检测系统并对含有缺陷的铆钉进行旋转检测实验,结合实验结果与理论推导,提出构造旋转特征幅值曲线并提取其峰峰值作为旋转式差分探头的特征值选取方式。最后,对多层铆接结构不同参数的缺陷进行了检测,实验结果表明,研制的旋转式差分探头可对缺陷进行定位,能检测到最小缺陷的尺寸为4 mm×0.2 mm×1 mm(长、宽、深)、埋深6 mm,且缺陷特征幅值随缺陷长度的增加而增大。探头对比结果表明,旋转式差分探头的检测效果在线性度与检测灵敏度方面均优于绝对式探头。

    Abstract:

    Critical load-bearing structures of aircraft fuselages are predominantly assembled by riveting, and fatigue cracks are highly prone to initiate at the riveted locations. Timely detection of such cracks and acquisition of their location, length, and other relevant information are of great significance for structural damage assessment and maintenance. Conventional nondestructive testing techniques are difficult to apply for in-service inspection, whereas pulsed eddy current testing offers a deep penetration depth and rich detection information, thus providing significant advantages in detecting deep-seated buried defects. To address the detection of buried defects around rivet holes in aircraft riveted structures, a pulsed eddy current rotational differential probe has been designed. The probe is equipped with a horizontally placed rectangular excitation coil and two tunneling magnetoresistance (TMR) sensors, and incorporates a central circular hole to accommodate the rivet head, thereby reducing structural interference. Subsequently, the rotational detection principles of both the absolute probe and the differential probe are investigated, and the defect signal expressions for the two types of probes during rotational detection are theoretically derived and compared. Next, a pulsed eddy current testing system is established and rotational detection experiments are conducted on riveted specimens containing defects. By combining the experimental results with the theoretical derivations, a rotational characteristic amplitude curve is constructed, and its peak-to-peak value is extracted as the characteristic value of the rotational differential probe. Finally, defects with different parameters in the multilayer riveted structures are detected. Experimental results demonstrate that the developed rotational differential probe can locate defects and detect a minimum defect size of 4 mm×0.2 mm×1 mm (length × width × depth) at a buried depth of 6 mm. Moreover, the characteristic amplitude of the defect increases with increasing defect length. Probe comparison results indicate that the rotational differential probe outperforms the absolute probe in terms of both linearity and detection sensitivity.

    参考文献
    相似文献
    引证文献
引用本文

秦仍川,李秋锋,樊俊铃,王智搏,卢超,周瑞琪.脉冲涡流旋转式差分探头设计及飞机多层铆接结构实验测试[J].仪器仪表学报,2026,47(7):34-45

复制
分享
相关视频

文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2026-09-24
  • 出版日期:
文章二维码