不锈钢极薄带蜂窝夹芯梁的冲击三点弯曲性能

Impact three-point bending performance of ultra-thin stainless-steel strip honeycomb sandwich beams

  • 摘要: 不锈钢极薄带凭借其超薄、高比强度、优异的成形性,以及不锈钢基体固有的耐腐蚀等诸多优点,成为蜂窝夹芯结构又一理想芯材。为了获得不锈钢极薄带蜂窝夹芯结构的动态响应规律、失效模式以及冲击耗能机制,本研究提出以50 μm SUS304不锈钢极薄带作为基材并使用辊压成形和激光点焊工艺制备蜂窝芯,采用热压复合工艺制备碳纤维增强树脂基(CFRP)面板/不锈钢极薄带蜂窝夹芯梁。利用落锤冲击试验机开展了100 J~400 J能量范围内的三点弯曲冲击性能研究,并结合ABAQUS/Explicit建立蜂窝夹芯梁的有限元模型,全面分析了夹芯梁在冲击载荷下的响应规律。研究结果表明,所制夹芯梁在各冲击能量下的载荷-挠度曲线冲击响应过程可分为初始加载、稳定攀升和卸载衰竭三个阶段。当冲击能量从100 J增至400 J时,其峰值载荷提升22.7%,而回弹位移由0.94 mm下降至0.63 mm,吸能效率下降15.1%。不锈钢极薄带蜂窝夹芯梁的损伤失效模式主要表现为CFRP面板的层间脱粘、纤维基体的损伤破裂及蜂窝芯的塑性压溃。其中蜂窝芯的塑性变形和CFRP面板层间的分层损伤是夹芯梁的主要耗能机制,在100 J~400 J冲击能量下分别占比57%~69%和11%~23%。不锈钢极薄带蜂窝夹芯梁的弯曲损伤失效分为弹性变形、面板断裂和芯层压溃与结构整体失效三个阶段,且随冲击能量增加其抗弯性能显著增强,但回弹能力降低且吸能效率下降。其能量耗散主要源于蜂窝芯的塑性压溃与CFRP面板层间损伤的协同作用。

     

    Abstract: Stainless-steel Ultra-thin strips, with their ultra-thin profile, high specific strength, excellent formability, and inherent corrosion resistance of the stainless-steel matrix, have emerged as an ideal core material for honeycomb sandwich structures. To investigate the dynamic response characteristics, failure modes, and impact energy dissipation mechanisms of stainless steel ultra-thin strip honeycomb sandwich structures under impact, this study proposes the fabrication of honeycomb cores using 50 μm-thick SUS304 ultra-thin stainless-steel strips as the substrate material, manufactured through roll forming and laser spot welding processes. Carbon fiber reinforced polymer (CFRP) face sheets/stainless steel ultra-thin strip honeycomb sandwich beams were prepared through hot-pressing composite process. Drop-weight impact tests were conducted within 100 J-400 J energy range for three-point bending impact experiments. A finite element model of the sandwich beam was established using ABAQUS/Explicit to comprehensively analyze its response under impact loading. Results indicate that the load-deflection curves of the sandwich beams under various impact energies exhibit three characteristic stages: initial loading, stable progression and unloading recession. When impact energy increased from 100 J to 400 J, the peak load rose by 22.7%, while rebound displacement decreased from 0.94 mm to 0.63 mm, accompanied by a 15.1% reduction in energy absorption efficiency. The primary failure modes include CFRP face sheet delamination, fiber/matrix damage and fracture, along with plastic crushing of the honeycomb core. Plastic deformation of the honeycomb core (57%-69%) and delamination damage in CFRP face sheets (11%-23%) constitute the main energy dissipation mechanisms across 100 J-400 J impact energies. The bending damage failure of stainless steel ultra-thin strip honeycomb sandwich beams can be divided into three stages: elastic deformation, face sheet fracture, and core crushing accompanied by structural collapse. As the impact energy increases, their bending resistance significantly improves, while resilience diminishes and energy absorption efficiency decreases. The primary mechanisms for energy dissipation arise from the synergistic effect between the plastic crushing of the honeycomb core and the interlaminar damage in the CFRP face sheets.

     

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