首页 >

基于分区接触-粘接的长桁对接结构导波仿真-增刊

吕佳龙1,徐钰森1,白生宝2,陈健1   

  1. 1. 南京航空航天大学
    2. 中国飞机强度研究所
  • 收稿日期:2026-06-01 修回日期:2026-06-23 发布日期:2026-06-26
  • 通讯作者: 陈健

Guided wave simulation study for stringer joint structures based on a zoned model

  • Received:2026-06-01 Revised:2026-06-23 Published:2026-06-26

摘要: 复杂多钉长桁对接结构广泛应用于现代飞机机身、机翼等主承力部件,其服役安全性对航空器结构可靠性具有重要影响。服役过程中,由于铆接孔及搭接界面等几何不连续区域的存在,局部应力集中显著,在飞行循环载荷等交变载荷作用下,疲劳微裂纹易在铆接孔边缘萌生并沿铆钉排扩展,形成多部位损伤。导波监测因其对微小损伤敏感、覆盖范围广,被认为是实现此类结构损伤识别的有效手段。然而,长桁对接结构中普遍存在预紧力、摩擦接触及多界面耦合等非线性因素,使导波在连接区域内的传播行为复杂,其传播机理仍缺乏系统认识。针对上述问题,本文提出一种基于分区粘结–摩擦接触模型的复杂多钉长桁对接结构导波传播有限元仿真方法。首先,通过稳态静力分析获取不同预紧力作用下连接界面的接触应力分布规律,揭示预紧力作用下接触压力非均匀的分布特征。在此基础上,基于被连接件半顶角理论确定铆钉压紧作用形成的接触影响区域,并结合界面接触压力分布特征对连接界面进行分区建模,将接触区域划分为粘结接触区与摩擦接触区,从而建立粘结—摩擦复合接触模型,实现复杂连接界面的准确建模。最后,通过导波监测试验对仿真结果进行验证,并对多通道导波信号进行对比分析。结果表明,铆钉连接区域的接触力学特性对导波传播具有显著影响,所提出的仿真方法可为复杂连接结构的导波建模与结构健康监测提供理论与数值支撑。

关键词: 导波, 铆钉连接, 长桁对接结构, 结构健康监测, 仿真方法

Abstract: Complex multi-rivet stringer splice joints are extensively employed in primary load-bearing components of modern aircraft, such as fuselages and wings, and their operational safety critically influences the reliability of the aircraft structure. During service, significant local stress concentrations arise due to geometric discontinuities, such as rivet holes and lap interfaces. Under alternating loads like flight cyclic loads, micro-fatigue cracks are prone to initiate at rivet hole edges and propagate along rivet rows, resulting in multiple-site damage. Guided wave monitoring is regarded as an effective approach for damage identification in such structures, owing to its sensitivity to minor defects and extensive coverage. However, nonlinear factors prevalent in stringer splice joints, including preload, frictional contact, and multi-interface coupling, complicate the propagation behavior of guided waves within the joint region. A systematic understanding of the underlying propagation mechanisms is still lacking. To address these issues, this paper proposes a finite element simulation method for guided wave propagation in complex multi-rivet stringer splice joints, based on a zoned bond–friction contact model. First, the distribution of contact stress on the joint interface under varying preloads is obtained through steady-state static analysis, revealing the non-uniform characteristics of contact pressure distribution induced by preload. Subsequently, the contact-affected zone formed by rivet clamping is determined using the half-apex angle theory of the joined parts. Combined with the interfacial contact pressure distribution, the joint interface is modeled in zones, divided into bonded contact and frictional contact regions, thereby establishing a composite bond–friction contact model to achieve accurate modeling of the complex joint interface. Finally, guided wave monitoring experiments are conducted to validate the simulation results, followed by a comparative analysis of multi-channel guided wave signals. The results demonstrate that the contact mechanical properties of the riveted joint region significantly influence guided wave propagation. The pro-posed simulation method provides theoretical and numerical support for guided wave modeling and structural health monitoring of complex jointed structures.

Key words: guided waves, riveted joints, stringer splice joint structure, structural health monitoring (SHM), simulation method

中图分类号: