高温环境下三维五向碳纤维/环氧树脂编织复合材料圆管冲击压缩性能

Impact compression properties of three-dimensional five directional carbon fiber/epoxy resin braided composite circular tubes at elevated temperatures

  • 摘要: 采用1×1四步法圆形编织技术和树脂传递模塑(RTM)工艺制备了三维五向碳纤维/环氧树脂编织复合材料圆管,并在室温(20℃)和高温场(80℃、110℃、140℃、170℃)环境下使用搭载高温装置的分离式霍普金森压杆(SHPB)对三维五向碳纤维/环氧树脂编织复合材料圆管进行轴向冲击压缩测试。根据实验结果揭示温度和应变率对三维五向碳纤维/环氧树脂编织复合材料圆管的冲击压缩性能和失效行为的耦合影响,并结合体式显微镜和扫描电子显微镜(SEM)对冲击压缩破坏后的试样进行宏观观察和微观形貌观察分析。研究结果表明:温度变化和应变率的不同对三维五向碳纤维/环氧树脂编织复合材料圆管的力学性能有显著影响。室温时,三维五向碳纤维/环氧树脂编织复合材料圆管冲击压缩性能稳定,应变率增加能提高材料压缩强度、压缩模量等力学性能。破坏模式主要是纤维断裂。高温场中,材料力学性能整体下降。抗冲击压缩能力随温度升高而减弱,破坏模式有树脂软化、纤维与树脂界面脱粘现象。应变率对力学性能的影响因高温干扰会发生变化。

     

    Abstract: Three-dimensional five-directional (3D5D) carbon fiber/epoxy resin braided composite circular tubes were prepared by using 1×1 four - step circular braiding technology and resin transfer molding (RTM) process. Axial impact compression tests of the 3D5D carbon fiber/epoxy resin braided composite circular tubes were carried out using a split Hopkinson pressure bar (SHPB) equipped with a high-temperature device in environments of ambient temperature (20℃) and elevated temperature fields (80℃, 110℃, 140℃, 170℃). According to the experimental results, the coupled effects of temperature and strain rate on the impact compression performance and failure behavior of the 3D5D carbon fiber/epoxy resin braided composite circular tubes were revealed. Macroscopic and microscopic morphology observations and analyses of the specimens after impact compression failure were performed by combining a stereo microscope and a scanning electron microscope (SEM). The research results show that the mechanical properties of 3D5D carbon fiber/epoxy resin braided composite circular tubes are significantly affected by the temperature and strain rate. At ambient temperature, the impact compression performance of the 3D5D carbon fiber/epoxy resin braided composite circular tubes is stable, and the increase of strain rate can improve the mechanical properties such as compressive strength and compressive modulus of the material. The failure mode is mainly fiber breakage. In elevated temperature field, the mechanical properties of the material decrease. The impact compression resistance decreases with increasing temperature. The failure modes include resin softening and fiber - resin interface debonding. The influence of the strain rate on the mechanical properties will change due to high temperature interference.

     

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