原位成型工艺参数对CF/PEEK热塑性复合材料层间结合的影响

Effect of processing parameters on interlaminar bonding of CF/PEEK thermoplastic composites during in situ consolidation

  • 摘要: 热塑性复合材料的层间性能是表征其整体质量的重要指标之一。对于热塑性复合材料自动铺放原位成型过程,复合材料层间性能受到温度场、聚合物热降解、结晶、层间结合及孔隙率等多种机制的耦合影响。其中,层间结合是形成层间整体结构的主要影响因素。由于成型速度快,铺层保温和保压时间短,自动铺放原位成型通常难以形成完美的层间结合。本文研究了高性能碳纤维增强聚醚醚酮(CF/PEEK)复合材料在自动铺放原位成型过程中的层间结合机制。基于影响层间结合的两个主要过程:紧密接触和聚合物分子链扩散,分别进行了理论模型预测及试验验证,探讨了工艺参数对原位成型层间结合过程的影响及其机制,并分析了层合板层间剪切强度随工艺参数的变化规律。结果表明,分子链扩散所需要的时间远低于紧密接触过程,因而紧密接触为影响CF/PEEK层间结合的主要过程。对于紧密接触过程,激光温度的影响最为显著,而铺放速率和铺放压力的影响相当。在激光温度450℃、铺放速率100 mm/s的成型条件下,CF/PEEK复合材料的层间剪切强度达到最大值58.5 MPa。

     

    Abstract: Interlaminar property is an important indicator to evaluate the overall quality of composite components. In the process of automated fiber placement (AFP) in-situ consolidation, the interlaminar properties of the composites are affected by the processes such as temperature history, polymer degradation, crystallization, interlaminar bonding, and void content. Interlaminar bonding is the primary factor of forming the overall structure between layers of the components. It is usually difficult to form perfect interlaminar bonding due to the short dwell time of temperature and pressure caused by the fast processing speed. In this study, the mechanism of interlaminar bonding during AFP in situ consolidation for high performance carbon fiber reinforced poly-ether-ether-ketone (CF/PEEK) composites was investigated. Theoretical model prediction and experimental verification were carried out for the two main processes of interlaminar bonding: Intimate contact and polymer diffusion. The influence and mechanisms of process parameters on the interlaminar bonding during in-situ consolidation process were explored and the effect of the processing parameters on the interlaminar shear strength was also analyzed. The results indicate that the time required for polymer diffusion is much lower than that of intimate contact, thus the intimate contact is considered as the main process affecting the interlaminar bonding of CF/PEEK. In addition, for the process of intimate contact, the influence of laser temperature is the most significant, while the influence of placement speed and compaction force is comparable. Interlaminar shear strength of CF/PEEK composites reaches a maximum value of 58.5 MPa at laser temperature of 450℃ and placement speed at 100 mm/s.

     

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