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Effect of manufacturing defect on mechanical performance of plain weave carbon/epoxy composite based on 3D geometrical reconstruction

机译:基于3D几何重构的制造缺陷对平纹碳/环氧复合材料力学性能的影响

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摘要

The investigation on the effect of manufacturing defect on the mechanical performance of composite is essential for the design and application in practice. In this study, the plain weave carbon fiber reinforced polymer (CFRP) laminates are fabricated by the autoclave process and vacuum bag process (VBP), respectively. Uniaxial tensile testes are conducted with a digital image correlation (DIC) system to obtain the macroscopic mechanical performance and local strain distribution. The internal microdefects of composite laminates are captured by micron-resolution computed tomography (mu CT) detection technique, including the size and distribution of void, total volume fraction and geometrical parameters of yarns. Based on the Texgen software and Monte-Carlo algorithm, virtual samples with various void contents are constructed to evaluate the impact of defect using finite element solver ABAQUS/Standard. To substantiate this work, we present a comparative study considering both autoclave and VBP. The effect of void defect on the mechanical performances of CFRP laminate is analyzed through finite element method (FEM). The results reveal that the effect of void defect on the surface strain distribution of laminate is significant, especially the value of maximum strain, which will increase obviously with the void defect content. In addition, the overall stiffness predicted by numerical simulation, taking the effect of void defect into account, is lower than that of theoretical.
机译:研究制造缺陷对复合材料机械性能的影响对于实际设计和应用至关重要。在这项研究中,平纹碳纤维增强聚合物(CFRP)层压板分别通过高压釜工艺和真空袋工艺(VBP)制成。使用数字图像相关(DIC)系统进行单轴拉伸测试,以获得宏观的机械性能和局部应变分布。复合材料层压板的内部微缺陷是通过微米分辨率计算机断层扫描(mu CT)检测技术捕获的,包括空隙的大小和分布,总体积分数和纱线的几何参数。基于Texgen软件和Monte-Carlo算法,使用有限元求解器ABAQUS / Standard构建具有各种空隙含量的虚拟样本,以评估缺陷的影响。为了证实这项工作,我们提出了同时考虑高压釜和VBP的比较研究。通过有限元方法(FEM)分析了空隙缺陷对CFRP层压板力学性能的影响。结果表明,空隙缺陷对层压板表面应变分布的影响特别明显,最大应变值随空隙缺陷含量的增加而明显增加。此外,考虑到空隙缺陷的影响,通过数值模拟预测的整体刚度低于理论值。

著录项

  • 来源
    《Composite Structures》 |2018年第9期|38-52|共15页
  • 作者单位

    Peking Univ, Coll Engn, Dept Mech & Engn Sci, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China;

    Beijing Inst Technol, Beijing Key Lab Lightweight Multifunct Composite, Beijing 100081, Peoples R China;

    Nanjing Tech Univ, Sch Mech & Power Engn, Nanjing 210009, Jiangsu, Peoples R China;

    Beijing Inst Technol, Beijing Key Lab Lightweight Multifunct Composite, Beijing 100081, Peoples R China;

    Peking Univ, Coll Engn, Dept Mech & Engn Sci, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China;

    Peking Univ, Coll Engn, Dept Mech & Engn Sci, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Plain weave CFRP laminates; Defects; Strain field; Numerical simulations;

    机译:平纹CFRP层压板;缺陷;应变场;数值模拟;

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