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纤维/金属网增强层板低速冲击损伤机理和演化
引用本文:王沁宇,卓家桂,李新顶,闵济东,胡文盛,谈建平,万云. 纤维/金属网增强层板低速冲击损伤机理和演化[J]. 力学季刊, 2023, 44(1): 160-171. DOI: 10.15959/j.cnki.0254-0053.2023.01.016
作者姓名:王沁宇  卓家桂  李新顶  闵济东  胡文盛  谈建平  万云
作者单位:1. 福建福清核电有限公司;2. 上海一核阀门股份有限公司;3. 华东理工大学机械与动力工程学院;4. 华东交通大学土木建筑学院
基金项目:国家自然科学基金青年基金(12002126);;江西省自然科学基金(20224BAB201016);
摘    要:本文首先通过落锤低速冲击实验测试了纯玻璃纤维增强环氧树脂复合材料和304不锈钢丝网(SSWM)/玻璃纤维混杂复合材料的力学性能,探究了SSWM嵌入数量对混杂复合材料抗冲击性能的影响.随后采用Abaqus有限元软件建立了混杂复合材料的低速冲击模型,分别采用三维Hashin失效准则和Jason-Cook破坏准则模拟了纤维/基体和SSWM的损伤;建立了基于表面接触的内聚力模型来模拟界面分层;编写了VUMAT用户子程序定义混杂复合材料层合板的渐进失效过程.结果表明:相较于纯玻璃纤维增强环氧树脂层合板,SSWM/玻璃纤维混杂增强环氧树脂层合板的抗冲击性能更优,其中铺层形式为铺层III的混杂复合材料抗冲击性能最佳.通过对比发现有限元仿真结果与实验结果吻合良好,表明建立的模型适用于SSWM/玻璃纤维混杂增强环氧树脂复合材料低速冲击损伤的评估.通过分析仿真结果发现混杂复合材料的低速冲击损伤主要是冲击区域的纤维断裂、基体破坏和层间分层;SSWM通过吸收和传递冲击能量从而提升了混杂复合材料的抗冲击性能.

关 键 词:复合材料  混杂结构  低速冲击  有限元仿真  损伤机理和演化

Damage Mechanism and Evolution of Fiber/Metal Wire Reinforced Plastic Laminate Under Low-Velocity Impact
WANG Qinyu,ZHUO Jiagui,LI Xinding,MIN Jidong,HU Wensheng,TAN Jianping,WAN Yun. Damage Mechanism and Evolution of Fiber/Metal Wire Reinforced Plastic Laminate Under Low-Velocity Impact[J]. Chinese Quarterly Mechanics, 2023, 44(1): 160-171. DOI: 10.15959/j.cnki.0254-0053.2023.01.016
Authors:WANG Qinyu  ZHUO Jiagui  LI Xinding  MIN Jidong  HU Wensheng  TAN Jianping  WAN Yun
Abstract:In this paper, the mechanical properties of pure glass fiber reinforced epoxy resin composites and Stainless Steel Wire Mesh (SSWM)/glass fiber hybrid composites were investigated through drop weight low-speed impact tests, and the influence of the number of SSWM embeddings on the impact resistance of hybrid composites was explored. Then the finite element software Abaqus was used to establish the low-velocity impact model of hybrid composites, and three-dimensional Hashin failure criterion and Jason-Cook failure criterion were used to simulate the damage of fiber/matrix and SSWM, respectively. The cohesive force behavior based on surface contact was established to simulate the interface stratification. The user subroutine of VUMAT was written to define the progressive failure process of hybrid composite laminates. The results show that compared with the pure glass fiber reinforced epoxy resin laminates, SSWM/ glass fiber reinforced epoxy resin hybrid laminates have better impact resistance, and Ply III hybrid composite has the best impact resistance. By comparison, it is found that the finite element simulation results are in good agreement with the experimental results, indicating that the established model is suitable for the low-velocity impact damage assessment of SSWM/ glass fiber reinforced epoxy resin hybrid composites. The simulation results show that the low-velocity impact damage of hybrid composites is mainly represented as fiber fracture, matrix failure and interlayer delamination in the impact area. SSWM improves the impact resistance of hybrid composites by absorbing and transferring the impact energy.
Keywords:composite material   hybrid structure   low-velocity impact   numerical simulation   failure mechanism and evolution  
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