计晨, 李素云. 石墨烯增强铝基SiC复合材料抗侵彻机理试验与数值仿真[J]. 中国舰船研究, 2018, 13(4): 16-23. DOI: 10.19693/j.issn.1673-3185.01147
引用本文: 计晨, 李素云. 石墨烯增强铝基SiC复合材料抗侵彻机理试验与数值仿真[J]. 中国舰船研究, 2018, 13(4): 16-23. DOI: 10.19693/j.issn.1673-3185.01147
JI Chen, LI Suyun. Test and numerical simulation of anti-penetration mechanism for reinforced aluminum matrix SiC composites[J]. Chinese Journal of Ship Research, 2018, 13(4): 16-23. DOI: 10.19693/j.issn.1673-3185.01147
Citation: JI Chen, LI Suyun. Test and numerical simulation of anti-penetration mechanism for reinforced aluminum matrix SiC composites[J]. Chinese Journal of Ship Research, 2018, 13(4): 16-23. DOI: 10.19693/j.issn.1673-3185.01147

石墨烯增强铝基SiC复合材料抗侵彻机理试验与数值仿真

Test and numerical simulation of anti-penetration mechanism for reinforced aluminum matrix SiC composites

  • 摘要:
      目的  旨在研究新型轻质复合装甲板——石墨烯增强铝基SiC复合材料装甲靶板的抗侵彻失效机理。
      方法  利用光镜与扫描电镜对石墨烯增强铝基SiC复合材料进行微观形貌观察;结合弹道枪试验,利用AUTODYN有限元软件建立1/2模型,破片质量为30 g,靶板厚度为43 mm,采用不同的本构模型描述材料,进行数值模拟仿真计算。
      结果  结合弹道枪试验及仿真计算,得到石墨烯增强铝基SiC复合材料复合靶板抗侵彻的过程为:破片侵彻靶板时,靶板表层铝合金受破片挤压形成环形卷曲破口,破片继续向后挤压过程中,靶板不断侵蚀破片头部;且破片不断向后冲击剩余靶板形成变形锥,破片速度足够大时,贯穿靶板形成花瓣型破口。
      结论  结合微观形貌观察及弹道枪试验,仿真计算结果显示:Johnson-Cook,Cowper-Symonds及Johnson-Holmquist 3种本构模型中,Johnson-Holmquist本构模型更适合描述石墨烯增强铝基SiC复合材料的抗侵彻机理。

     

    Abstract:
      Objectives  In order to study the anti-penetration failure mechanism of new lightweight composite armor plates, a graphene-reinforced aluminum-based SiC composite armor plate is proposed.
      Methods  The microstructures of graphene reinforced aluminum matrix SiC composites are observed using light and scanning electron microscopy; combined with a ballistic gun test, a half model is established using AUTODYN finite element software, with a fragment mass of 30 g and a target plate thickness of 43 mm. Different constitutive models are used to describe the materials, and numerical simulation is carried out.
      Results  Combining the ballistic gun test and simulation calculations, the anti-penetration process of the graphene reinforced aluminum-based SiC composite target is as follows:when the fragment penetrates the target plate, the aluminum alloy on the target plate is crushed by the fragment, forming a ring-shaped crimp break. During the backward extrusion process, the target plate is continuously eroded by the head, the fragments continue to impact the remaining target plate deformation cone and the fragment speed is great enough to form a petal-shaped breach through the target plate.
      Conclusions  Combining microstructure observation and the ballistic gun test, the simulation results show that among the three constitutive models of Johnson-Cook, Cowper-Symonds and Johnson-Holmquist, the latter is more suitable for describing the anti-penetration mechanisms of graphene-reinforced aluminum-based SiC composites.

     

/

返回文章
返回