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卫星蜂窝夹层结构跨尺度强度分析

陈夜 杨轩 朱孔军 马超 丁毅

航天器工程2026,Vol.35Issue(2):57-62,6.
航天器工程2026,Vol.35Issue(2):57-62,6.DOI:10.3969/j.issn.1673-8748.2026.02.007

卫星蜂窝夹层结构跨尺度强度分析

Research on Cross-scale Intensity of Satellite Honeycomb Sandwich Structures

陈夜 1杨轩 1朱孔军 2马超 1丁毅2

作者信息

  • 1. 上海卫星工程研究所,上海 201109
  • 2. 南京航空航天大学 航空航天结构力学及控制全国重点实验室,南京 210016
  • 折叠

摘要

Abstract

To further enhance the precision of satellite structural design,this paper investigates multiple failure modes of honeycomb sandwich structures.A mesoscopic finite element model with embedded inserts,honeycomb cores,and other key components is developed for typical sat-ellite honeycomb sandwich structures with inserts.Three failure modes are simulated,and the corresponding critical loads are derived.Taking a camera-equipped satellite as the study case,a cross-scale modeling approach that integrates macroscopic and mesoscopic analyses is proposed.Intensity analysis results show that the maximum von Mises stress in the aluminum honeycomb lattice near the camera mounting foot reached 312MPa,which exceeds the material yield strength,thus revealing the damage mechanisms of the honeycomb core.The proposed method overcomes the issue of low analysis accuracy in conventional macroscopic modeling approaches.This study provides a reference for intensity analysis of high load-bearing satellite structures and promotes the lightweight design of satellite structures on the premise of ensuring structural safety.

关键词

蜂窝夹层结构/有限元/跨尺度/强度分析

Key words

honeycomb sandwich structure/finite element/cross-scale/intensity analysis

分类

航空航天

引用本文复制引用

陈夜,杨轩,朱孔军,马超,丁毅..卫星蜂窝夹层结构跨尺度强度分析[J].航天器工程,2026,35(2):57-62,6.

基金项目

航空航天结构力学及控制全国重点实验室开放课题(MCAS-E-0325G02) (MCAS-E-0325G02)

航天器工程

1673-8748

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