TC4/SiC三维预应力约束复合结构抗侵彻性能研究

Investigation on the Anti-penetration Performance of TC4/SiC Three-dimensional Prestressed Constrained Composite Structure

  • 摘要: 防弹陶瓷因具有高硬度与低密度特性而广泛应用于复合装甲,金属封装结构可通过对陶瓷施加三维约束并引入预应力来抑制裂纹扩展。本文采用显式动力学有限元法,建立了等质量Ⅰ型构型(单层SiC+双层TC4封装)与Ⅱ型构型(双层SiC+三层TC4封装)TC4/SiC三维预应力约束复合结构,系统分析了结构参数对预应力场分布及抗侵彻性能的影响规律。研究结果表明:SiC层厚度增加导致TC4层对内部陶瓷的三维约束作用减弱,且改变TC4厚度配比对SiC预应力影响较大。虽然背板增厚会导致陶瓷内部预应力水平下降,但增强的背部支撑效应有效抑制了陶瓷的早期拉伸层裂,显著提升了陶瓷粉化耗能,该增益效应主导了靶板抗侵彻性能的提升。在Ⅱ型最优构型(厚度比T2T4 = 5∶1,T1T3T5 = 2∶2∶17)下,T4陶瓷层比吸能(Specific Energy Absorption, SEA)较基准工况提升247.5%,且与最优Ⅰ型构型相比,弹体剩余质量减少9.3%,具有更好的减重潜力。此外,圆头弹在侵彻初期易发生塑性镦粗,前置陶瓷层对弹体侵蚀效能较强;尖头弹端部应力集中致使陶瓷提前破碎,冲击载荷向后置结构提前转移,弹体剩余速度较圆头弹工况高7.9%,弹体剩余质量增加4.1%。

     

    Abstract: Ballistic ceramics are widely used in composite armor owing to their high hardness and low density. Metal encapsulation structures suppress crack propagation by applying three-dimensional confinement to ceramics and introducing prestress. In this study, explicit dynamic finite element models of equal-mass Type Ⅰ (single SiC layer + dual TC4 encapsulation) and Type Ⅱ (dual SiC layers + triple TC4 encapsulation) TC4/SiC three-dimensional prestressed constrained composite structures were established, and the effects of structural parameters on the prestress field distribution and anti-penetration performance were systematically analyzed. Results show that increasing SiC layer thickness weakens the three-dimensional confinement of the TC4 layer on the internal ceramics, and adjusting the TC4 thickness ratio can also significantly influence the SiC prestress level. Although increasing backing plate thickness reduces the internal prestress of ceramics, the enhanced backing support effect effectively suppresses early tensile delamination of ceramics and substantially improves ceramic pulverization energy absorption, with this enhancement effect dominating the improvement in anti-penetration performance. In the optimal Type Ⅱ configuration (thickness ratio T2T4 = 5∶1, T1T3T5 = 2∶2∶17), the specific energy absorption (SEA) of the T4 ceramic layer increases by 247.5% compared to the baseline case, and the projectile residual mass decreases by 9.3% relative to the optimal Type Ⅰ configuration, demonstrating superior weight reduction potential. Furthermore, the blunt-nose projectile tends to undergo plastic upsetting during the initial penetration phase, resulting in stronger erosion of the projectile by the front ceramic layer; stress concentration at the tip of the conical-nose projectile causes premature ceramic fracture and early transfer of impact load to the rear structure, with the projectile residual velocity 7.9% higher and residual mass 4.1% greater than in the blunt-nose projectile case.

     

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