复合材料科学与工程 ›› 2026, Vol. 0 ›› Issue (6): 20-27.DOI: 10.19936/j.cnki.2096-8000.20260628.003

• 基础与力学性能研究 • 上一篇    下一篇

拉挤碳纤维增强复合材料力学性能测试及其失效机理分析

李逸轩1,2, 任宏亮1,2, 刘卫生3, 李成良3, 黄辉秀3, 李闯2, 李永丰2*, 张辉2*   

  1. 1.东华大学 材料科学与工程学院 先进纤维材料全国重点实验室,上海 201620;
    2.东华大学 民用航空复合材料协同创新中心,上海 201620;
    3.中材科技风电叶片股份有限公司,北京 100192
  • 收稿日期:2025-04-24 发布日期:2026-07-03
  • 通讯作者: 张 辉(1984—),男,博士,研究员,博士生导师,研究方向为碳纤维增强树脂基复合材料,zhanghui@dhu.edu.cn。李永丰(1987—),男,博士,副教授,硕士生导师,研究方向为轻质高强材料-结构一体化设计与整体制造,yfli@dhu.edu.cn。
  • 作者简介:李逸轩(2001—),男,硕士,学生,研究方向为碳纤维增强树脂基复合材料。
  • 基金资助:
    江苏省重点研发计划(BE2021014-3)

Mechanical properties test and failure mechanism analysis of pultruded carbon fiber reinforced composite

LI Yixuan1,2, REN Hongliang1,2, LIU Weisheng3, LI Chengliang3, HUANG Huixiu3, LI Chuang2, LI Yongfeng2*, ZHANG Hui2*   

  1. 1. National Key Laboratory of Advanced Fiber Materials, College of Materials Science and Engineering, Donghua University, Shanghai 201620, China;
    2. Center for Civil Aviation Composites, Donghua University, Shanghai 201620, China;
    3. Sinoma Wind Power Blade Co., Ltd., Beijing 100192, China
  • Received:2025-04-24 Published:2026-07-03

摘要: 本研究针对拉挤碳纤维增强热固性树脂基复合材料(拉挤碳纤维增强复合材料)在复杂载荷下的力学行为,通过多种力学试验,结合数字图像相关测量技术(Digital Image Correlation,DIC)与扫描电镜(Scanning Electron Microscopy,SEM)阐明其失效机制,并基于三维实体单元和三维Hashin破坏准则,对拉挤碳纤维复合材料开孔拉伸的应变场与力学响应进行预测。结果表明,材料在不同受力方向表现出显著的各向异性失效行为,纵向拉伸与压缩性能均明显高于横向拉伸与压缩性能,其主要原因为拉挤成型复合材料在不同工况下的失效模式具有方向依赖性。纵向拉伸失效以纤维-基体界面脱黏引发应力重分布进而导致纤维脆性断裂为主,而横向拉伸则表现为基体主导的断裂伴随界面脱黏。在压缩工况下,纵向失效源于纤维微屈曲,横向失效则以基体剪切屈服诱导界面脱黏与纤维局部屈服为主。由于纤维的断裂与屈服载荷明显高于基体,因此纵向力学性能显著优于横向。在剪切失效模式中,复合材料呈现多裂纹扩展特征,失效始于缺口附近的水平基体裂纹,沿试样深度方向扩展为多个平行于纤维的基体裂纹,最终导致材料整体失效。此外,开孔拉伸强度可达1 246.83 MPa,表现为典型的孔边应力集中诱发的纤维-基体界面纵向劈裂失效。通过对开孔拉伸进行数值模拟预测了材料失效机理,偏差为11.06%。最后,将DIC技术与传统应变片法进行对比分析,发现其在任何应力水平下的差异均小于4%,验证了此试验中通过DIC全场应变得到的应变云图与应力-应变曲线的可靠性。本研究通过多种基础力学试验分析了拉挤成型碳纤维复合材料的失效机理,为复杂载荷下的结构设计与失效评估提供了理论依据。

关键词: 碳纤维复合材料, 拉挤成型, 力学性能, 有限元仿真, 数字图像相关测量技术

Abstract: This study investigates the mechanical behavior of pultruded carbon fiber-reinforced thermosetting resin matrix composites(pultruded CFRP) under complex loading conditions. Through a series of mechanical tests combined with digital image correlation(DIC) and scanning electron microscopy(SEM), the failure mechanisms were elucidated. A three-dimensional solid element model incorporating the 3D Hashin failure criterion was employed to predict the strain field and mechanical response of pultruded CFRP under open-hole tension. The results indicate that the material exhibits significant anisotropic failure behavior under different loading directions. Both longitudinal tensile and compressive properties are markedly superior to their transverse counterparts, primarily due to the direction-dependent failure modes in pultruded composites. Under longitudinal tension, failure is dominated by fiber-matrix interfacial debonding, triggering stress redistribution and subsequent fiber brittle fracture, whereas transverse tension failure is governed by matrix-dominated fracture accompanied by interfacial debonding. Under compressive loading, longitudinal failure originates from fiber micro-buckling, while transverse failure is characterized by matrix shear yielding-induced interfacial debonding and localized fiber yielding. Since the fracture and yielding loads of fibers are substantially higher than those of the matrix, the longitudinal mechanical properties significantly outperform the transverse properties. In shear failure mode, the composite exhibits multiple crack propagation features, initiated by horizontal matrix cracks near the notch, which develop into multiple parallel matrix cracks along the fiber direction, ultimately leading to global failure. Additionally, the open-hole tensile strength reaches 1 246.83 MPa, demonstrating a typical fiber-matrix interfacial longitudinal splitting failure induced by hole-edge stress concentration. Numerical simulation of open-hole tension predicted the material’s failure mechanism with a deviation of 11.06%. Finally, a comparative analysis between DIC and conventional strain gauge measurements revealed discrepancies of less than 4% at all stress levels, validating the reliability of the DIC-derived full-field strain maps and stress-strain curves. This study systematically analyzes the failure mechanismsof pultruded CFRP through multiple fundamental mechanical tests, providing a theoretical basis for structural design and failure assessment under complex loading conditions.

Key words: carbon fiber reinforced polymer, pultrusion, mechanical property, finite element simulation, non-contact digital image correlation method

中图分类号: