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中文核心期刊

纤维增强泡沫夹芯壳极限承载与损伤模式分析

ANALYSIS OF ULTIMATE LOAD-BEARING CAPACITY AND DAMAGE MODES OF FIBER-REINFORCED FOAM SANDWICH SHELLS

  • 摘要: 夹芯复合材料因其优异的比刚度与比强度, 在深海装备等轻量化结构设计中展现出巨大潜力. 然而, 当前关于复合材料夹芯壳体, 尤其是在等容重比 (结构重量比排水重量) 约束下纯碳纤维与夹芯构型极限承载机理和损伤演化规律的系统试验与数值研究仍然不足. 为此, 本文制备了等容重比的纯碳纤维和碳纤维-泡沫-碳纤维夹芯薄壁壳体, 开展了四点压缩试验, 进一步在Abaqus中嵌入Fortran编写的三维Hashin失效损伤子程序并结合内聚力单元来进行两种壳体模型的数值仿真. 试验结果表明, 在等容重比条件下, 碳纤维-泡沫-碳纤维夹芯壳体的平均峰值载荷较纯碳纤维壳体提高约24.7%, 刚度提升约151.9%, 显著改善了壳体结构承载与抗变形性能. 观察破坏形貌与应变响应可知, 纯碳纤维壳体的失效源于碳纤维层间分层, 而夹芯壳体的失效主要源于最大主应力主导的泡沫芯材断裂, 且当芯材强度逐渐提升时, 夹芯壳体的损伤模式会从泡沫芯材的脆性断裂转为碳纤维复合材料层的破坏. 数值仿真模拟获得的纯碳纤维与夹芯壳体的载荷-位移曲线, 环向应变分布以及损伤形貌与试验结果吻合良好, 验证了基于三维Hashin失效准则与内聚力模型联合预测碳纤维复合材料壳体失效的有效性. 本工作可为后续碳纤维复合材料大深度高耐压壳体设计优化与制造应用提供重要支撑.

     

    Abstract: Sandwich composites have shown great potential in the design of lightweight structures for deep-sea equipment due to their excellent specific stiffness and specific strength. However, systematic experimental and numerical studies on composite sandwich shells, particularly regarding the ultimate load-bearing mechanisms and damage evolution laws of pure carbon fiber and carbon fiber-foam-carbon fiber sandwich configurations under the equal weight-to-displacement ratio condition, remain insufficient. Therefore, this study prepares pure carbon fiber and carbon fiber-foam-carbon fiber sandwich thin-walled shells with equal weight-to-displacement ratios, conducts four-point compression tests, and further embeds a Fortran-written three-dimensional Hashin failure damage subroutine in Abaqus and combines it with cohesive elements to conduct numerical simulations of these two types of shell models. The test results show that under the equal weight-to-displacement ratio condition, the average peak load of the carbon fiber-foam-carbon fiber sandwich shells is approximately 24.7% higher than that of the pure carbon fiber shells, and the stiffness is increased by about 151.9%. This significantly improves the load-bearing capacity and deformation resistance of the shell structure. From the failure morphology and strain response, it can be seen that the failure of the pure carbon fiber shell is caused by interlaminar delamination of the carbon fiber layers, while the failure of the sandwich shells is mainly due to the fracture of the foam core material dominated by the maximum principal stress. Moreover, as the strength of the core material gradually increases, the damage mode of the sandwich shell will shift from the brittle fracture of the foam core material to the failure of the carbon fiber composite layers. The load-displacement curves, circumferential strain distributions, and damage morphologies obtained through the numerical simulations of both the pure carbon fiber shells and sandwich shells show good agreement with the experimental results, validating the effectiveness of the combined approach using the three-dimensional Hashin failure criterion and the cohesive model for predicting the failure of carbon fiber composite shells. This work provides important support for the subsequent design optimization, manufacturing, and application of high-pressure-resistant carbon fiber composite shells in the deep-sea environment.

     

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