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基于蜂窝背板的层合靶抗弹侵彻数值研究

作者:时间:2021-12-15点击数:

全文下载: 202106010.pdf


文章编号: 1672-6987202106-0082-07 DOI 10.16351/j.1672-6987.2021.06.010




赵昌方, 朱宏伟, 任杰, 仲健林*(南京理工大学 机械工程学院,江苏 南京 210094)


摘要: 蜂窝结构具有良好的力学性能,属于一种穿孔板,具有较大的抗弹发展潜力。基于蜂窝背板,设计了一种考虑层间特性的钢/碳纤维复合材料/陶瓷/穿孔蜂窝铝层合靶,并采用有限元软件对不同攻角的弹丸侵彻特性进行了数值模拟。结果表明,攻角对靶板抗弹性能的影响非常大。随着攻角的减小,层合靶的变形增大,陶瓷层形成陶瓷锥导致的破坏区域增大。对于钢板和碳纤维板,弹孔的直径基本没有变化,但长度增大。对于蜂窝铝穿孔背板,斜侵彻时变形更大,对弹丸的干扰效果更好。垂直侵彻时弹丸的剩余速度最大,60°攻角侵彻时弹丸的剩余速度最小,降低了约350 m·s-1

关键词: 蜂窝穿孔板; 层合靶; 碳纤维复合材料; 抗弹侵彻


中图分类号: TJ 03 N 945.13文献标志码: A

引用格式: 赵昌方,朱宏伟,任杰,等.基于蜂窝背板的层合靶抗弹侵彻数值研究[J. 青岛科技大学学报(自然科学版), 2021, 42(6): 82-88.


ZHAO Changfang, ZHU Hongwei, REN Jie, et al. Numerical study on the anti-projectile penetration of laminated target with honeycomb backplaneJ. Journal of Qingdao University of Science and TechnologyNatural Science Edition), 2021 426): 82-88.


Numerical Study on the Anti-projectile Penetration of Laminated

Target with Honeycomb Backplane


ZHAO Changfang, ZHU Hongwei, REN Jie, ZHONG Jianlin

(School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China)


Abstract: Honeycomb structure has a great mechanical properties and belongs to a perforated plate, which has a good potential for anti-projectile. Based on honeycomb backplane, a laminated target of steel/carbon fiber composite/ceramic/perforated honeycomb aluminum was designed. The inter-layer characteristics were considered, and the penetration characteristics of projectile with different attack angles were numerically simulated by finite element software. The results showed that the attack angle had a great influence on the anti-projectile of the target plate. The deformation of the laminated target increased with the decrease of the angle of attack, and the failure area caused by the formation of "ceramic cone" in the ceramic layer increased. For steel plate and carbon fiber composite plate, the diameter of the projectile hole was basically unchanged, but the length increased. For honeycomb aluminum perforated back plate, the deformation was greater when oblique penetration, and the interference effect on projectile was better. During vertical penetration, the residual velocity of the projectile was the largest, and the residual velocity of the projectile was the smallest when the attack angle was 60°, which decreased about 350 m·s-1.

Key words: honeycomb perforated plate; laminated target; carbon fiber composite; anti-projectile penetration



收稿日期: 2021-02-18

基金项目: 国家自然科学基金项目(12002169);国家留学基金项目(202106840033);江苏省研究生科研与实践创新计划项目(KYCX21_0342);南京理工大学优秀博士培养基金项目(2021.

作者简介: 赵昌方(1995—),男,博士研究生.*通信联系人.


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