树脂基复合材料靶板抗高速破片侵彻性能研究

刘龙浩; 邵明哲; 张屹龙; 栾贻浩; 付志强; 朱丽平

doi:10.19554/j.cnki.1001-3563.2026.11.032

PDF(2353 KB)

包装工程（技术栏目） ›› 2026, Vol. 47 ›› Issue (11) : 308-317. DOI: 10.19554/j.cnki.1001-3563.2026.11.032

装备防护

树脂基复合材料靶板抗高速破片侵彻性能研究

刘龙浩¹, 邵明哲¹, 张屹龙¹, 栾贻浩^1*, 付志强¹, 朱丽平²

作者信息 +

Resistance of Resin Matrix Composite Target Plates to High-velocity Fragment Penetration

LIU Longhao¹, SHAO Mingzhe¹, ZHANG Yilong¹, LUAN Yihao^1*, FU Zhiqiang¹, ZHU Liping²

Author information +

文章历史 +

摘要

目的为探究不同树脂基复合材料靶板对高速破片的抗侵彻性能,筛选出抗侵彻最优组合,为防护材料的结构选型与优化设计提供理论依据。方法基于LS-DYNA软件建立高速破片侵彻有限元模型,采用数值模拟方法开展仿真分析。选取碳纤维增强环氧树脂复合材料（CFRP）、碳纤维增强聚醚醚酮复合材料（CF/PEEK）、超高分子量聚乙烯增强环氧树脂复合材料（UHMWPE/EP）以及芳纶增强环氧树脂复合材料（AF/EP）4种树脂基复合材料,设计4种靶板组合：以CF/PEEK为迎弹面分别与 CFRP、UHMWPE/EP、AF/EP复合,另以CFRP为迎弹面与CF/PEEK复合。针对1.1 g柱状楔形破片,在2 000 m/s的冲击速度下开展侵彻仿真,破片损伤行为采用Johnson-Cook失效准则进行描述,4种树脂基复合材料的冲击损伤特征均采用Chang-Chang失效准则进行评估。结果仿真结果表明,以CF/PEEK为迎弹面,CFRP为背弹面的靶板抗侵彻性能最优：该组合下破片动能可在12 μs内降为0 J,背弹面最大变形量仅为2.22 mm,较其他组合降低约30%,且靶板内能吸收率最高。结论通过对4种靶板组合的侵彻性能系统分析,确定CF/PEEK-CFRP组合为最优防护方案,达到了预期研究目的,为高速破片防护结构的工程应用提供了指导。

Abstract

The work aims to investigate the penetration resistance of different resin-matrix composite targets against high-velocity fragments, identify the optimal combination for penetration resistance, and provide a theoretical basis for the structural selection and optimization of protective materials. A finite element model of high-velocity fragment penetration was established using LS-DYNA software. Numerical simulation methods were employed to conduct the analysis, with carbon fiber-reinforced epoxy composite (CFRP), carbon fiber-reinforced polyetheretherketone composites (CF/PEEK), ultra-high molecular weight polyethylene-reinforced epoxy composites (UHMWPE/EP), and aramid-reinforced epoxy composites (AF/EP). Four composite target combinations were designed: CF/PEEK as the impact-facing surface paired with CFRP, UHMWPE/EP, AF/EP; and another with CFRP as the impact-facing surface combined with CF/PEEK. Penetration simulations were conducted for a 1.1 g cylindrical wedge-shaped fragment at an impact velocity of 2 000 m/s. The fragment damage behavior was described using the Johnson-Cook failure criterion, while the impact damage characteristics of the four resin-based composites were evaluated using the Chang-Chang failure criterion. Simulation results indicated that the target plate with CF/PEEK as the impact-facing surface and CFRP as the back surface exhibited the best penetration resistance. Under this configuration, the fragment kinetic energy was reduced to 0 J within 12 μs, the maximum deformation of the back surface was only 2.22 mm, approximately 30% lower than other configurations, and the target plate achieved the highest internal energy absorption rate. Through a systematic analysis of the penetration resistance of the four target plate combinations, the CF/PEEK-CFRP configuration is identified as the optimal protection scheme, achieving the intended research objectives and providing guidance for the engineering application of high-speed fragment protection structures.

导出引用

刘龙浩, 邵明哲, 张屹龙, 栾贻浩, 付志强, 朱丽平. 树脂基复合材料靶板抗高速破片侵彻性能研究[J]. 包装工程. 2026, 47(11): 308-317 https://doi.org/10.19554/j.cnki.1001-3563.2026.11.032

LIU Longhao, SHAO Mingzhe, ZHANG Yilong, LUAN Yihao, FU Zhiqiang, ZHU Liping. Resistance of Resin Matrix Composite Target Plates to High-velocity Fragment Penetration[J]. Packaging Engineering. 2026, 47(11): 308-317 https://doi.org/10.19554/j.cnki.1001-3563.2026.11.032

中图分类号： TB332

参考文献

[1] 陆阳予, 张庆明, 薛一江, 等. 多层复合结构对高速破片的防护特性[J]. 兵工学报, 2020, 41(S2):169-175.
LU Y Y, ZHANG Q M, XUE Y J, et al.Protective Characteristics of Multilayer Composite Structure Against High-Speed Fragments[J]. Acta Armamentarii, 2020, 41(S2):169-175.
[2] 陈雪, 朱龙宇, 薛钦洋, 等. 防空导弹用树脂基复合材料研究进展[J]. 空天防御, 2024, 7(6):76-95.
CHEN X, ZHU L Y, XUE Q Y, et al.Research Progress of Resin Matrix Composites for Air Defense Missiles[J]. Air & Space Defense, 2024, 7(6):76-95.
[3] YANG G J, PARK M, PARK S J.Recent Progresses of Fabrication and Characterization of Fibers-Reinforced Composites:A Review[J]. Composites Communications, 2019, 14:34-42.
[4] HU K F, SCHONBERG W P.Ballistic Limit Curves for Non-Spherical Projectiles Impacting Dual-Wall Spacecraft Systems[J]. International Journal of Impact Engineering, 2003, 29(1-10):345-355.
[5] Livermore Software Technology Corporation (LSTC). LS-DYNA 971 R6.1.0 keyword user's manual[R]. US:Livermore Software Technology Corporation.
[6] QU K F, WU C Q, LIU J, et al.Ballistic Performance of Multi-Layered Aluminium and UHMWPE Fibre Laminate Targets Subjected to Hypervelocity Impact by Tungsten Alloy Ball[J]. Composite Structures, 2020, 253:112785.
[7] KARAHAN M, KARAHAN N, ALI NASIR M, et al.Effect of Structural Hybridization on Ballistic Performance of Aramid Fabrics[J]. Journal of Thermoplastic Composite Materials, 2019, 32(6):795-814.
[8] NAYAK S, SAHOO B P, NAYAK R K, et al.Improvement of Low-Velocity Impact and Tribo-Mechanical Properties of Unsymmetrical Hybrid Composites through Addition of Nanoclay[J]. Bulletin of Materials Science, 2024, 47(4):237.
[9] STEPHEN C, SHIVAMURTHY B, MOURAD A I, et al.Experimental and Finite Element Study on High-Velocity Impact Resistance and Energy Absorption of Hybrid and Non-Hybrid Fabric Reinforced Polymer Composites[J]. Journal of Materials Research and Technology, 2022, 18:5406-5418.
[10] MEDVEDOVSKI E.Ballistic Performance of Armour Ceramics:Influence of Design and Structure. Part 1[J]. Ceramics International, 2010, 36(7):2103-2115.
[11] PRAKASH A, RAJASANKAR J, ANANDAVALLI N, et al.Influence of Adhesive Thickness on High Velocity Impact Performance of Ceramic/Metal Composite Targets[J]. International Journal of Adhesion and Adhesives, 2013, 41:186-197.
[12] GUIDA M, SELLITTO A, MARULO F, et al.Analysis of the Impact Dynamics of Shape Memory Alloy Hybrid Composites for Advanced Applications[J]. Materials, 2019, 12(1):153.
[13] TEPEDUZU B, KARAKUZU R.Ballistic Performance of Ceramic/Composite Structures[J]. Ceramics International, 2019, 45(2):1651-1660.
[14] WU S B, XU Z H, HU C X, et al.Numerical Simulation Study of Ballistic Performance of Al₂O₃/Aramid-Carbon Hybrid FRP Laminate Composite Structures Subject to Impact Loading[J]. Ceramics International, 2022, 48(5):6423-6435.
[15] BERK B, KARAKUZU R, TOKSOY A K.An Experimental and Numerical Investigation on Ballistic Performance of Advanced Composites[J]. Journal of Composite Materials, 2017, 51(25):3467-3480.
[16] 杨豹. 舰船复合装甲抗高速破片侵彻性能研究[D]. 武汉:武汉理工大学, 2022:27-28.
YANG B.Research on the Anti-Penetration Performance of High-Speed Fragmentation of Composite Armor for Ships[D]. Wuhan:Wuhan University of Technology, 2022:27-28.
[17] FELI S, ASGARI M R.Finite Element Simulation of Ceramic/Composite Armor under Ballistic Impact[J]. Composites Part B:Engineering, 2011, 42(4):771-780.
[18] 辛春亮, 朱星宇, 薛再清, 等. 有限元分析常用材料参数手册[M]. 2版. 北京:机械工业出版社, 2022.
XIN C L, ZHU X Y, XUE Z Q, et al.Handbook of Common Material Parameters for Finite Element Analysis[M]. 2nd ed. Beijing:China Machine Press, 2022.
[19] KEMPESIS D, IANNUCCI L, DEL ROSSO S, et al.A Representative Volume Element Model for Ultra-High-Molecular-Weight-Polyethylene Composites[J]. Composite Structures, 2021, 262:113609.
[20] GARCIA-GONZALEZ D, RUSINEK A, JANKOWIAK T, et al.Mechanical Impact Behavior of Polyether-Ether-Ketone (PEEK)[J]. Composite Structures, 2015, 124:88-99.
[21] 贾飞, 刘彦池, 苑大威, 等. 基于LS-DYNA的巡飞弹安全性分析研究[J]. 现代信息科技, 2021, 5(23):43-47.
JIA F, LIU Y C, YUAN D W, et al.Research on Safety Analysis of Cruiser Based on LS-DYNA[J]. Modern Information Technology, 2021, 5(23):43-47.
[22] 张佳琦. 碳纤维-铝合金板抗弹击数值分析[J]. 中国科技信息, 2023(17):108-113.
ZHANG J Q.Numerical Analysis of Impact Resistance of Carbon Fiber-Aluminum Alloy Plate[J]. China Science and Technology Information, 2023(17):108-113.