低速冲击载荷下C/C-PMI夹芯板动态响应数值分析

Numerical analysis of the dynamic response of C/C-PMI sandwich panels under low-velocity impact loading

  • 摘要:
    目的 为揭示C/C编织层合板与PMI泡沫组成的夹芯结构在低速冲击载荷下的动态响应及损伤演化机理,明确冲击能量及关键结构参数对结构力学性能的影响规律。
    方法 首先,构建耦合VUMAT复合材料渐进损伤与考虑应变率效应的PMI泡沫可压缩塑性有限元模型;然后,针对低速冲击载荷下夹芯板结构的动态响应展开系统的研究,并定量分析考虑泡沫芯材应变率效应与否对结果的影响;最后,针对夹芯板的关键结构参数进一步开展敏感性分析。
    结果 结果显示,不考虑应变率效应将严重低估夹芯结构的动态承载能力;C/C-PMI夹芯板的主要破坏机制为基体拉伸、基体压缩和泡沫芯层的压溃损伤,其中PMI芯层的塑性压溃是结构主要的能量耗散途径,其吸能占比达82.3%;最大撞深随着冲击能量的增加呈非线性增长,并在约60 J后由未穿透损伤转变为局部穿透失效;芯层比是影响结构抗冲击响应的主导参数,当芯层比增至 8.25 时,结构吸能效率显著提升,若继续增大,则易诱发上面板过早穿透及芯层局部压溃。从工程应用的角度来看,以吸能缓冲为主的结构宜采用约 8.25 的芯层比,而以整体承载和低损伤为主的甲板/舱壁宜采用较低的芯层比并优先增厚迎撞面。
    结论 所做研究可为舰船复合材料轻量化甲板、舱壁及局部防护结构的抗低速冲击设计与安全评估提供参考。

     

    Abstract:
    Objectives This study aims to reveal the dynamic response and damage evolution mechanisms of sandwich structures composed of woven C/C laminates and PMI foam under low-velocity impact loading, and to clarify the influence of impact energy and key structural parameters on their mechanical performance.
    Methods A numerical simulation model was established, incorporating a progressive damage model for the composite laminates implemented via a VUMAT subroutine and a crushable foam plasticity model for the PMI foam considering strain rate effects. A systematic investigation was conducted on the dynamic response of the sandwich panels under low-velocity impact, quantitatively analyzing the influence of the foam core's strain rate effect on the simulation results. Furthermore, a sensitivity analysis was performed on the key structural parameters of the sandwich panel.
    Results The results indicate that neglecting the strain rate effect severely underestimates the dynamic load-carrying capacity of the sandwich structure. The primary failure mechanisms of the C/C-PMI sandwich panels include matrix tension, matrix compression, and foam core crushing. The plastic crushing of the PMI core acts as the primary pathway for energy dissipation, accounting for 82.3% of the total energy absorption. The maximum indentation depth increased nonlinearly with impact energy, and a transition from non-penetrating damage to local penetration occurred at about 60 J under the present configuration. The core-to-face-sheet thickness ratio was identified as the dominant structural parameter; the energy absorption efficiency increased significantly when the ratio increased to 8.25, whereas a further increase promoted premature face-sheet penetration and localized core crushing. For naval engineering applications, a core-to-face thickness ratio of about 8.25 is recommended for energy-absorbing structures. For decks and bulkheads prioritizing overall load-bearing and low damage, a lower ratio is preferable, prioritizing the thickening of the front face-sheet.
    Conclusions The results provide a reference for the impact-resistant design and safety assessment of lightweight composite ship structures.

     

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