复合材料科学与工程 ›› 2025, Vol. 0 ›› Issue (12): 72-78.DOI: 10.19936/j.cnki.2096-8000.20251228.010

• 设计与工艺 • 上一篇    下一篇

基于Lamb波的复合材料不同界面分层损伤扩展监测

武李奇亚, 耿亚南*   

  1. 中国民航大学 交通科学与工程学院,天津 300300
  • 收稿日期:2024-10-24 出版日期:2026-02-06 发布日期:2026-02-06
  • 通讯作者: 耿亚南(1989—),女,博士,讲师,硕士生导师,研究方向为飞机结构损伤与维修,gengyn@126.com。
  • 作者简介:武李奇亚(1999—),男,硕士研究生,研究方向为航空器复合材料结构健康监测。
  • 基金资助:
    国家自然科学基金(U2033209)

Delamination damage propagation monitoring of composites at different interfaces based on Lamb waves

WU-Li Qiya, GENG Yanan*   

  1. School of Transportation Science and Engineering, Civil Aviation University of China, Tanjin 300300, China
  • Received:2024-10-24 Online:2026-02-06 Published:2026-02-06

摘要: 分层损伤是复合材料中常见的损伤之一,会随着工作时间的延长而逐渐扩展,严重削弱复合材料的强度与稳定性,同时分层损伤处于不同界面也会使其各项力学性能发生不同程度的变化,因此能有效地对其进行识别定位与扩展监测对结构整体安全性具有重要意义。本文提出一种基于Lamb波的ToF分层损伤监测方法,通过对比分析复合材料层合板上下表面Lamb波ToF差异,对存在初始分层损伤的复合材料层合板进行损伤界面的定位,并对不同界面的分层损伤扩展进行可在线的持续监测。首先,研究了Lamb波监测分层损伤的原理。其次,建立了分层损伤界面深度、长度与Lamb波在结构中传播速度的关系,得到对分层损伤界面定位与扩展监测的理论基础。最后,通过有限元仿真验证所提出方法的有效性。仿真结果显示,分层损伤界面距离层合板表面越浅,Lamb波信号延迟越明显,上下表面接收的信号时间差异越大,且信号延迟程度与分层损伤长度的增长呈线性关系。

关键词: 结构健康监测, 复合材料, Lamb波, 损伤界面深度, 分层扩展监测

Abstract: Delamination damage is one of the common damage in composite materials, and it will gradually expand with the extension of working time, which will seriously weaken the strength and stability of composite materials. At the same time, the delamination damage at different interfaces will also cause various mechanical changes to different degrees. Therefore, it is of great significance for the overall safety of the structure to effectively identify, locate and expand monitoring it. In this paper, a Lamb wave-based ToF delamination damage monitoring method is proposed. By comparing and analyzing the Lamb wave ToF differences between the upper and lower surfaces of composite laminates, the damage interface of composite laminates with an initial delamination damage is located, and the delamination damage expansion at different interfaces is continuously monitored online. Firstly, the principle of Lamb wave monitoring delamination damage is studied. Secondly, the relationship between the depth and length of the delamination damage interface and the propagation speed of Lamb waves in the structure was established, and the theoretical basis for the location and extension monitoring of the delamination damage interface was obtained. Finally, the effectiveness of the proposed method was verified by finite element simulation. The simulation results show that the shallower the delamination damage interface is from the laminate surface, the more significant the Lamb wave signal delay, and the greater the difference in signal time between the upper and lower surfaces, moreover, the signal delay is linearly related to the increase of delamination damage length.

Key words: structural health monitoring, composite structure, Lamb wave, depth of damage interface, delamination extension monitoring

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