材料科学
复合材料
蜂巢
蜂窝结构
复合数
极限抗拉强度
微观结构
堆积
聚合物
航空航天
压缩(物理)
抗压强度
压力(语言学)
碳纤维增强聚合物
纤维
比强度
工作(物理)
仿生学
结构材料
比模量
灵敏度(控制系统)
仿生材料
智能材料
损伤容限
结构工程
芯(光纤)
环氧树脂
夹芯板
拉伸试验
碳纤维
作者
Jianxun Du,Honghao Zhang,Jin Dong,Chaoqi Xu,Tengfei Wang,Chenhao Xue,Jing Xiao
摘要
ABSTRACT Inspired by the internal microstructure of beetle elytra, this study proposes a detachable protective structure fabricated from carbon fiber composites. The structure, compatible with additive manufacturing techniques, incorporates biomimetic mortise‐tenon connections. This configuration, comprising a honeycomb core combined with biomimetic mortise‐tenon joints, effectively dissipates impact energy, thereby mitigating stress concentration and reducing environmental sensitivity in heterogeneous material joining systems. Through numerical simulations, we systematically investigated the impact resistance under various working conditions and parameters, along with the dynamic response mechanisms of laminated honeycomb assemblies. Multiple configurations of biomimetic mortise‐tenon honeycomb structures were manufactured using polymer‐based composites via additive manufacturing. Quasi‐static compression tests demonstrated that the PLA‐CF composite achieves exceptional specific energy absorption of 5.8 kJ/kg, while PC‐based structures exhibit superior compressive resistance of 20.2 kN, confirming the tunable mechanical performance through polymer selection and structural design. Furthermore, a CFRP laminated structure with bio‐inspired mortise‐tenon connections was developed using biomimetic stacking sequences, with its stress distribution and failure modes under tensile loading analyzed. This work provides critical insights into the design of disassemblable joining systems for heterogeneous materials and highlights their potential for enabling reusable polymer‐based composite structures in lightweight aerospace applications, pending further experimental validation.
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