复合材料科学与工程 ›› 2024, Vol. 0 ›› Issue (6): 60-68.DOI: 10.19936/j.cnki.2096-8000.20240628.008

• 应用研究 • 上一篇    下一篇

纬向V形机织间隔复合材料压缩性能有限元分析

刘生杰1,2, 邵慧奇1,2, 陈南梁1,2, 蒋金华1,2*, 曾金金3, 陈骏峰4, 白一峰5   

  1. 1.东华大学 产业用纺织品教育部工程研究中心,上海 201620;
    2.东华大学 纺织学院,上海 201620;
    3.上海复合材料科技有限公司,上海 201620;
    4.中国电子科技集团公司第五十二研究所,浙江 310000;
    5.中国电子科技集团公司第三十八研究所,安徽 230094
  • 收稿日期:2023-04-12 出版日期:2024-06-28 发布日期:2024-07-26
  • 通讯作者: 蒋金华(1978—),男,教授,博士,研究方向为产业用纺织品、特种编织织造技术与复合材料,jiangjinhua@dhu.edu.cn。
  • 作者简介:刘生杰(1995—),女,硕士研究生,研究方向为三维机织间隔织物及复合材料。
  • 基金资助:
    上海市自然科学基金(20ZR1400600);中央高校基本科研业务费专项资金项目(2232023G-06)

Finite element analysis of the compressive properties of weft V-shaped woven spacer composites

LIU Shengjie1,2, SHAO Huiqi1,2, CHEN Nanliang1,2, JIANG Jinhua1,2*, ZENG Jinjin3, CHEN Junfeng4, BAI Yifeng5   

  1. 1. Engineering Research Center of Textile Technical Education Ministry, Donghua University, Shanghai 201620, China;
    2. College of Textile, Donghua University, Shanghai 201620, China;
    3. Shanghai Composite Materials Technology Co., Ltd., Shanghai 201620, China;
    4. The 52nd Research Institute of China Electronics Technology Corporation, Zhejiang 310000, China;
    5. The 38nd Research Institute of China Electronics Technology Corporation, Anhui 230094, China
  • Received:2023-04-12 Online:2024-06-28 Published:2024-07-26

摘要: 探究了纬向V形机织间隔复合材料在平压和侧压载荷下的失效机制及破坏模式。采用ABAQUS软件建立复合材料多尺度单胞模型,并设置周期性边界条件。针对纤维束进行弹性性能分析,预测宏观材料弹性常数。利用Fortran语言对UMAT子程序进行二次开发,引入三维Hashin损伤判据和Camanho刚度退化方案,实现对纬向V形三维机织间隔复合材料的渐进损伤分析。结果表明,模拟结果与试验结果相符。在平压载荷作用下,弯曲振幅较大的V形绒经组先发生断裂,振幅小的绒经组后断裂,出现二次峰值载荷。绒经与纬纱交织处和绒经屈曲处出现应力集中,断裂位置集中在绒经屈曲最大处和与面板衔接处,面板无明显破损;在侧压载荷作用下,树脂面板与树脂内纱线为承力主体,面层纬纱承压较大,而间隔层绒经承压较小。断裂主要发生在两排V形绒经之间,失效模式为树脂渐进式破损、纤维脱黏与纱线断裂。

关键词: 纬向V形, 三维机织间隔复合材料, 有限元模拟, 压缩性能

Abstract: The failure modes and damage processes of weft V-shaped woven spacer composites were examined under flat and edgewise compression loads. The ABAQUS program was used to create a multi-scale single-cell composite model and define periodic boundary conditions. The elastic characteristics of fiber bundles were studied in order to predict the macroscopic material elastic constants. For the progressive damage analysis of weft V-shaped 3D woven spacer composites, a subsequent improvement of the UMAT subroutine in Fortran provides a 3D Hashin damage criterion and a Camanho stiffness degradation scheme. The results reveal that the simulated and test outcomes are consistent. Under the flat compression stress, the V-shaped pile warp group with higher bending amplitude cracked first, whereas the pile warp group with lower amplitude fractured subsequently, resulting in a secondary peak load. Stress concentrations at the interweaving of the pile warp and weft, as well as at the pile warp’s flexure, with fractures concentrated at the pile warp’s highest flexure and at the interface with the panel, and no obvious panel breakage; the principal load-bearing entities under edgewise pressure are the resin panel and the inner resin yarn, with the top layer of weft yarn under more pressure and the spacer layer of pile warp under less pressure. Fracture occurs mostly between the two rows of V-pile yarns, with gradual resin breakdown, fiber debonding, and yarn breaking as failure modes.

Key words: weft V-shape, 3D woven spacer composite, finite element simulation, compression properties

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