三维编织碳纤维/环氧树脂复合材料热氧环境下低速冲击性能弱化分子降解规律及损伤分布

Molecular degradation process and damage distribution for low speed impact properties weakening of three-dimensional braided carbon fiber/epoxy resin composites under thermo-oxidative environment

  • 摘要: 三维编织碳纤维复合材料在热氧环境中低速冲击性能变化机理研究对结构件耐久性设计具有重要指导意义。以三维四向碳纤维/环氧树脂复合材料为研究对象,结合ReaxFF反应分子动力学和Micro-CT技术,分析了热氧处理后基体分子结构变化和损伤空间分布特征,揭示热氧老化对编织复合材料低速冲击性能影响。研究表明,在180℃热氧环境下处理384 h后,复合材料基体分子结构发生断裂和重组,分子片段种类和数量增多,固有体积增大,分子链自由活动空间减小,自由体积减小,材料整体体积减小;主要气体产物由多到少为H2O、CO2和H2,质量下降。热氧损伤包括界面裂纹和基体裂纹,表现出明显方向性,主要沿面内方向分布和传递,最大裂纹深度为0.91 mm,体积分数为0.23%;基体分子结构变化和面内方向损伤致使编织复合材料低速冲击性能降低,沿面内方向冲击强度和刚度降低程度(分别为23.8%和28.9%)大于面外方向(分别为5.6%和8.6%)。

     

    Abstract: The investigation into the change mechanism of low-speed impact performance of three-dimensional braided carbon fiber composites in thermo-oxidative environment holds significant guiding implications for the durability design of structural components. Utilizing ReaxFF reaction molecular dynamics and Micro-CT techniques, this study analyzed the changes of molecular structure and the spatial distribution characteristics of damage within the matrix after thermos-oxidative treatment. It revealed the effects of thermo-oxidative environment on the low-speed impact properties of braided composites. The findings indicate that following 384 hours of treatment at 180°C, the molecular structure of matrix undergoes fragmentation and recombination, leading to an increase in molecular fragments, natural volume expansion, and reduction in free volume, which induced the whole volume degradation. The primary gaseous products, in descending order, are H2O, CO2, and H2, which induced the whole mass degradation. Thermo-oxidative-treatment induced damage exhibits a pronounced directional effect, predominantly distributed and propagated along the in-plane direction, encompassing interface cracks and matrix cracks. The maximum crack depth was measured at 0.91 mm, with a volume fraction of 0.23%. These changes in molecular structure and matrix damage along in-plane direction result in diminished low-speed impact performance of the braided composites. Specifically, the decrease in impact strength and stiffness is more pronounced in the in-plane direction (23.8% and 28.7%, respectively) compared to the out-of-plane direction (5.6% and 8.6%).

     

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