超高分子量聚乙烯纤维增强层合厚板抗高速钝头弹侵彻的理论模型.pdf
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- 关 键 词:
- 超高 分子量 聚乙烯 纤维 增强 厚板 高速 钝头弹侵彻 理论 模型
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第10卷第3期
中国舰船研究
Vol10 No3
015年6月
Chinese Journal of Ship Research
Jun.2015
阿络出版地址:htlp/www.crki.net/kcms/detail/42.1755.1.20150525.1638002.html
期刊网址:www.ship-research.
引用格式:陈长海,徐文献,朱锡,等超高分子量聚乙烯纤维増强层合厚板抗高速飩头弹侵砌的理论模型[J].中国舰船研
究,2015,10(3):63-69,83
CHEN Changhai, XU Wenxian, ZHU Xi, et al. Theoretical model for thick ultra-high molecular weight polyethylene fi
ber reinforeed laminates penetrated by high-velocity blunt-nosed projectiles[ J]. Chinese Journal of Ship Research
2015,10(3):63-69,83
超高分子量聚乙烯纤维增强层合厚板
抗高速钝头弹侵彻的理论模型
陈长海',徐文献2,朱锡’,侯海量′
1海军工程大学舰船工程系,溯北武汉430033
2海军湛江匙区装备修理监修室,广东湛江524005
摘要:结合超高分子量聚乙烯纤维增强塑料(UFRP)层合厚板抗高速侵彻的特点,将整个侵彻过程分为开坑
镦粗、剪切压缩和拉伸变形3个阶段。通过改进开坑懒粗阶段的计算方法和拉伸变形阶段的计算过程,基于能
量守恒原理建立UFRP层合厚板抗高速钝头弹侵彻的弹体侵彻深度和靶板弹道极限的计算模型,并给出相应的
计算流程图。通过采用该模型计算相关文献试验T况下的弹体侵彻深度和层合厚板弹道极限,发现计算值
文献试验结果均吻合较好。改进后的模型考虑了弹丸初速度对开坑繳粗阶段侵彻深度的影响,能够对高速钝
头弹侵UFRP层合厚板的弹体侵彻深度和层合厚板的弹道极限进行合理的预测,并可降低试验成本。
关键词:层合厚板;高速侵彻;舰船防护;超高分子量聚乙烯
中图分类号:U661.43;TB332
文献标志码:A
DOI:10.3969issn.1673-3185.2015.053.011
Theoretical model for thick ultra-high molecular weight polyethylene fiber
reinforeed laminates penetrated by high-velocity blunt-nosed projectiles
CHEN Changhai, XU Wenxian, ZAU Xi, ROU Hailiang
I Department of Naval Architecture Engineering, Naval University of Engineering, Wuhan 430033, China
2 Naval Supervisor Office of Equipment Maintenance in Zhanjiang Area, Zhanjiang 524005, China
Abstract Due to the high penetration-resistance of thick ultra-high molecular weight polyethylene fiber
reinforced plastic (UFRP)laminates under high velocities, the whole penetration process is divided into
three phases: cratering & mushrooming phase, shearing& compression phase, and stretching deformation
phase. By altering the computation method for the cratering& mush rooming phase and the calculation pro
ces for the stretching deformation phase, an analytical model is established based on the energy conserva
tion principle to compute the penetration depth of projectiles as well as the ballistic limits of laminates in
the case of thick UFRP laminates being penetrated by high-velocity blunt-nosed projectiles. The corre-
sponding computation flow charts are also presented. Moreover, penetration depths of projectiles and ballis
tie limits of thick laminates under different test conditions are calculated with the model in a correlative or
der. It is seen that good agreements are obtained between the theoretically values and experimental results
Therefore, the improved model, which considers the projectile initial velocity effects on penetration dept
during the cratering mushrooming phase, can be employed to reasonably predict the penetration depths
Ind can reduce experimental costs, demonstrating both theoretical and engineering values
Key words: thick laminate; high-veloeity penetration; warship protection; ultra-high molecular weight
polyethylene(UHMWPE)
收稿日期:2014-12-10
网络出版时间:2015-5-2516:38.00
甚金项目:国家自然科学基金资助项目(51409253,51179200)
作者简介:陈长海(通信作者),男,1985年生,博土,讲师。研究方向:肥船结枃抗爆抗侵彻。E-mai:chenchanghail0746@163.com
朱锡,男,1961年生,教授,博土生导师。研究方向:材料结构,复合材料,舰船结构抗爆与防护。E-mailezhuxi816@163.com
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