首页|拓扑结构对二维手性负泊松比结构抗冲击性能的影响

拓扑结构对二维手性负泊松比结构抗冲击性能的影响

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柔性材料实现可变形机翼技术对柔性材料力学性能要求较高,现有对于手性结构作为柔性材料驱动可变形机翼的研究以线性小变形为主.为了探究大变形条件下手性结构的力学性能,以三韧带手性、三韧带反手性、四韧带手性、四韧带反手性、六韧带手性的负泊松比结构为研究对象,基于蜂窝结构力学理论,对比分析拓扑结构和胞元几何参数对理想塑性材料本构模型的手性负泊松比结构面内压缩吸能特性的影响.结果表明:手性结构的弹性模量、平台应力和吸能能力与胞元参数α成反比,与胞元参数β成正比;拓扑结构对手性结构吸能特性影响明显,即具有相同单胞几何参数的手性结构吸能能力随着韧带数量的增加显著增强.
Influence of topology on the impact resistance performance of two-dimensionalchiral negative Poisson's ratio structures
Flexible materials to achieve deformable wing technology requires high mechanical properties of flexible materials,the existing research on chiral structures as flexible materials to drive deformable wings is based on the case of linear small deformations.In order to investigate the mechanical properties of chiral structures under large deformation conditions,five common chiral system negative Poisson's ratio structures,such as tri-chiral,anti-tri-chiral,tetra-chiral,anti-tetra-chiral,and hex-chiral structures are taken as the object of study.Based on the theo-ry of cellular structural mechanics,the effect of topological structure and cellular element geometrical parameter on the in-plane compression and energy absorption characteristics of chiral system negative Poisson's ratio structures of the intrinsic model of ideal plastic materials are compared and analysed.The results show that the elastic modu-lus,plateau stress and energy absorption capacity of the chiral structure are inversely proportional to the cell ele-ment parameter α and positively proportional to the cell element parameter β.The topology affects the energy-ab-sorbing properties of chiral structures significantly,i.e.,the energy-absorbing capacity of chiral structures with the same single-cell geometrical parameter is significantly enhanced with the increase in the number of ligaments.

topologychiralitynegative Poisson's ratioimpact resistancemechanical properties

耿一田、郭英男、袁伟、朱小军

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西北工业大学 航空学院,西安 710072

航空工业第一飞机设计研究院 结构设计研究所,西安 710089

拓扑结构 手性 负泊松比 抗冲击 力学性能

西北工业大学硕士研究生创新实践能力培育基金

PF2023041

2024

航空工程进展
中国航空学会 西北工业大学

航空工程进展

CSTPCD
影响因子:0.207
ISSN:1674-8190
年,卷(期):2024.15(5)
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