复合材料科学与工程 ›› 2026, Vol. 0 ›› Issue (4): 63-71.DOI: 10.19936/j.cnki.2096-8000.20260428.008

• 基础与力学性能研究 • 上一篇    下一篇

复合材料泡沫夹层结构非穿透损伤修理的四点弯曲性能研究

刘国春, 沈赫, 孙华伟   

  1. 中国民用航空飞行学院 航空工程学院, 成都 641450
  • 收稿日期:2025-02-25 发布日期:2026-06-16
  • 作者简介:刘国春(1983—),男,硕士,教授,研究方向为复合材料结构设计与分析,liuguochun@cafuc.edu.cn。

Study on four-point bending performance of bonded repairs in composite foam sandwich structures with non-penetrating damage

LIU Guochun, SHEN He, SUN Huawei   

  1. College of Aviation Engineering, Civil Aviation Flight University of China, Chengdu 641450, China
  • Received:2025-02-25 Published:2026-06-16

摘要: 本研究针对复合材料泡沫夹层结构非穿透性损伤的修理结构弯曲力学特性,开展了复合材料面板与芯层材料的基础力学性能测试,构建了基于三维Hashin失效准则、可压溃泡沫塑性模型及B-K胶层失效准则的高精度夹芯结构渐进损伤有限元分析模型,进行了非穿透损伤修理结构的四点弯曲性能试验,探讨了修理结构在弯曲载荷作用下的损伤演化与失效机理,基于高精度有限元分析模型完成了附加铺层修理参数优化。研究结果表明,针对泡沫夹芯维修结构,采用层合板、泡沫夹芯和胶层三种失效准则的有限元模型具有较高的计算精度,弯曲强度和弯曲刚度同试验均值的偏差为4.15%和2.07%。通过有限元分析与试验验证能够有效揭示修理结构承弯的损伤扩展路径及破坏模式,选取的优化修理方案达到了90.68%的强度恢复率,具有较强的工程实用价值。

关键词: 泡沫夹层结构, 四点弯曲, 有限元分析, 渐进损伤, 胶接修理, 复合材料

Abstract: This study investigates the flexural mechanical properties of repaired composite foam sandwich structures with non-penetrating damage. Mechanical performance tests were conducted on composite panels and foam cores, and a high-fidelity finite element analysis model for sandwich structures was established incorporating the 3D Hashin failure criterion, Crushable Foam plasticity model, and B-K adhesive failure criterion. Four-point bending performance tests were performed on repaired structures with non-penetrating damage. The damage evolution and failure mechanisms of the repaired structures under bending loads were systematically investigated through the integration of finite element analysis and experimental results. Parameter optimization of additional repair plies was accomplished based on the high-precision finite element model. The results indicate that the proposed model integrating three failure criteria for laminates, foam cores, and adhesive layers demonstrates high computational accuracy, with deviations of 4.15% in flexural strength and 2.07% in flexural stiffness compared to experimental averages. Both finite element analysis and experimental verification effectively reveal the damage propagation path and failure modes of repaired structures under bending loads. The optimized repair scheme achieved 90.68% strength recovery rate, demonstrating significant engineering applicability.

Key words: foam sandwich structure, four-point bending, finite element analysis, progressive damage analysis, adhesive repair, composites

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