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碳纳米管复合材料黏弹阻尼微观模型研究

陈磊 张英琦 王潇

南京航空航天大学学报2025,Vol.57Issue(2):266-274,9.
南京航空航天大学学报2025,Vol.57Issue(2):266-274,9.DOI:10.16356/j.1005-2615.2025.02.007

碳纳米管复合材料黏弹阻尼微观模型研究

Micromechanical Modeling of Viscoelastic Damping Mechanism in Carbon Nanotube Composites

陈磊 1张英琦 1王潇1

作者信息

  • 1. 南京航空航天大学直升机动力学全国重点实验室,南京 210016
  • 折叠

摘要

Abstract

In order to improve the stability of the rotor and explore new ways to replace traditional dampers,this paper studies the method of embedding carbon nanotube(CNT)short fibers into the rotor blades and enhancing structural damping by utilizing their viscoelastic slip effect.A micromechanical model is established to analyze the CNT viscoelastic slip mechanism.Based on the interface critical shear stress and the applied load,the slip behavior of CNT is analyzed,and an explicit expression between microscopic parameters and macroscopic damping is derived.This model fully considers the influence of key parameters such as geometric parameters and mechanical properties of CNTs on their damping effect.The results indicate that the damping effect predicted by the model is in good agreement with the experimental results.By embedding CNTs,the slip damping of the composite material can be significantly improved,reaching about 11 times the damping of the matrix.

关键词

微观力学模型/黏弹滑移/滑移阻尼/碳纳米管复合材料

Key words

micromechanical model/viscoelastic slip/slip damping/carbon nanotube composites

引用本文复制引用

陈磊,张英琦,王潇..碳纳米管复合材料黏弹阻尼微观模型研究[J].南京航空航天大学学报,2025,57(2):266-274,9.

基金项目

国防科技重点实验室基金(61422202101) (61422202101)

国家自然科学基金面上项目(12272169) (12272169)

旋翼专向基金(XYZX040401). (XYZX040401)

南京航空航天大学学报

OA北大核心

1005-2615

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