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卷绕式全柔性太阳翼的有限元建模及固有特性分析

张殊豪 于兆源 孙伟 骆海涛 季文豪

中南大学学报(自然科学版)2025,Vol.56Issue(12):5034-5047,14.
中南大学学报(自然科学版)2025,Vol.56Issue(12):5034-5047,14.DOI:10.11817/j.issn.1672-7207.2025.12.009

卷绕式全柔性太阳翼的有限元建模及固有特性分析

Finite element modeling and natural characteristics analysis of roll-out solar array

张殊豪 1于兆源 2孙伟 1骆海涛 3季文豪1

作者信息

  • 1. 东北大学 机械工程与自动化学院,辽宁 沈阳,110819||东北大学 航空动力装备振动及控制教育部重点实验室,辽宁 沈阳,110819
  • 2. 东北大学 机械工程与自动化学院,辽宁 沈阳,110819
  • 3. 中国科学院 沈阳自动化研究所,辽宁 沈阳,110016
  • 折叠

摘要

Abstract

As a novel flexible solar array developed in recent years,the roll-out solar array(ROSA)has the advantages of light weight,high storage ratio and repeatable expansion and contraction.However,detrimental issues including excessive deformation and persistent vibration are frequently induced by large structural span and low stiffness of ROSA.To analyze and predict the vibration characteristics of this kind of structure,a parametric finite element modeling method of ROSA simulation specimen was established using ANSYS software,incorporating precise geometric configurations of all components.Specifically,preload force in tension cables coupled with flexible integrated modular blanket assembly was directly introduced through defining truss element internal stress of the element.The deformation stress was equivalently introduced at the end segment of the composite thin lenticular tube through modeling with surface effect element.Additionally,the mass variation of drive motor and composite thin lenticular tube during extension and contraction of ROSA was simulated using the virtual material method.A case study was conducted using the full-field digital camera vibration measuring system to obtain the inherent characteristics of the experimental component under hoisting conditions.The first five natural characteristics obtained from the finite element model solution were compared with the experimental results.The influence of pretension force of tension cables,deployment length of ROSA,layup angle of the outer carbon fiber in the composite thin lenticular tube,and adhesive layer thickness on the inherent structural characteristics of ROSA were analyzed using this dynamic model,and their effects on the overall structural performance were explored.The results show that the maximum deviation of 4.690%is demonstrated between the first five natural frequencies obtained from the finite element model and experimental result,thereby validating model accuracy.These findings provide critical guidance for practical structural design of the ROSA.

关键词

卷绕式全柔性太阳翼/有限元建模/视觉测振/模态分析/虚拟材料法

Key words

roll-out solar array/finite element modeling/vision-based vibration measurement/modal analysis/virtual material method

分类

航空航天

引用本文复制引用

张殊豪,于兆源,孙伟,骆海涛,季文豪..卷绕式全柔性太阳翼的有限元建模及固有特性分析[J].中南大学学报(自然科学版),2025,56(12):5034-5047,14.

基金项目

国家自然科学基金资助项目(52475142)(Project(52475142)supported by the National Natural Science Foundation of China) (52475142)

中南大学学报(自然科学版)

OA北大核心

1672-7207

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