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OA
Study on four-point bending performance of bonded repairs in composite foam sandwich structures with non-penetrating damage
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.
This study investigates the flexural mechanical properties of repaired composite foam sandwich struc-tures 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 fail-ure 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 fail-ure 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.
刘国春;沈赫;孙华伟
中国民用航空飞行学院 航空工程学院,成都 641450中国民用航空飞行学院 航空工程学院,成都 641450中国民用航空飞行学院 航空工程学院,成都 641450
通用工业技术
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
foam sandwich structurefour-point bendingfinite element analysisprogressive damage analysisadhesive repaircomposites
《复合材料科学与工程》 2026 (4)
63-71,9
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