碳纤维复合材料-金属混杂波纹夹层结构低速冲击性能及剩余压缩强度研究

Study of low-velocity impact performance and residual compressive strength of carbon fiber composite-metal hybrid corrugated sandwich structure

  • 摘要: 纤维复合材料和金属材料混杂设计的轻量化一体结构具有良好的抗冲击性能,并成功在航空航天等领域实现应用。为了进一步提高混杂结构的抗冲击性和多次冲击下的损伤容限,通过在碳纤维层间添加金属层,制备了碳纤维复合材料-金属混杂夹层结构试件。针对该结构,开展了不同冲击能量和冲击次数下的冲击响应试验,并进行CT无损扫描分析。研究探讨了冲击后该结构的剩余压缩强度曲线,并利用无量纲剩余压缩强度系数来评估结构的剩余承载能力和损伤容限。试验结果表明,由于金属层对裂纹扩展的抑制作用,单次冲击在不同能量下对结构剩余压缩强度的影响相对较小,当冲击能量为60 J时,剩余压缩强度降低了5.4%;多次冲击时,复合材料-金属混杂夹层结构的剩余压缩强度表现出损伤累积的起始现象,10 J多次冲击中,当冲击总能量达到100 J时,剩余压缩强度开始显著下降,降低了30.8%。20 J多次冲击中,当冲击总能量达到80 J时,剩余压缩强度下降了12.7%。高能量多次冲击更容易导致该结构纤维层与金属层的脱粘分层。综上所述,该碳纤维复合材料-金属混杂夹层结构在未来轻质可靠承载结构的设计中具有广泛的应用潜力。

     

    Abstract: The integrated lightweight structures composed by fiber composite and metal material exhibit excellent impact resistance and has been applied in fields such as aerospace successfully. To further enhance the impact resistance and damage tolerance of hybrid structures under multiple impacts, the specimens of carbon fiber composite-metal hybrid sandwich structure were manufactured by incorporating metal layers between carbon fiber layers. Then the impact experiments were conducted under different impact energies and numbers. Beyond that, the CT non-destructive scanning analysis of the impacted specimens were also conducted. The post-impact residual compressive strength of the structures was investigated, while the residual load-bearing capacity and damage tolerance of the structure were also evaluated by the dimensionless coefficient. The results illustrate that the influences of the single impact at different energies on the residual compressive strength is relatively small, When the impact energy is 60 J, the residual compressive strength is reduced by 5.4%, which due to the inhibitory effect of the metal layer on crack propagation. As for the case of multiple impacts, the residual compressive strength of the composite-metal hybrid sandwich structure exhibits an initial damage accumulation phenomenon. In multiple impacts at 10 J, when the total impact energy reaches 100 J, the residual compressive strength begins to decrease significantly, dropping by 30.8%. In multiple impacts at 20 J, when the total impact energy reaches 80 J, the residual compressive strength decreases by 12.7%. The results show that multiple impacts with higher energy are more likely to cause debonding and delamination between the fiber layers and metal layers of the structure. And this carbon fiber composite-metal hybrid sandwich structure has extensive application potential in the design of lightweight and reliable load-bearing structures in the future.

     

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