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尺寸稳定性CFRP蜂窝制造方法的研究进展

廖逸坚 卫宇璇 刘硕 朱大雷 马立

宇航材料工艺2025,Vol.55Issue(4):26-33,8.
宇航材料工艺2025,Vol.55Issue(4):26-33,8.DOI:10.12044/j.issn.1007-2330.2025.04.004

尺寸稳定性CFRP蜂窝制造方法的研究进展

Progress in Manufacturing Methods of Dimensionally Stable CFRP Honeycomb

廖逸坚 1卫宇璇 1刘硕 1朱大雷 1马立1

作者信息

  • 1. 北京卫星制造厂有限公司,北京 100094
  • 折叠

摘要

Abstract

In the future,high-precision loads impose stringent requirements on the dimensional stability of spacecraft structures.The sandwich structure of carbon fiber-reinforced polymer(CFRP)honeycomb is a new lightweight structural design with excellent thermal dimensional stability,capable of meeting the design requirements for load-bearing structures under such conditions.This paper reviews the current development status of CFRP honeycomb manufacturing methods.Based on the manufacturing processes and corresponding technology methods that influence the dimensional stability of CFRP honeycomb structures,the manufacturing methods are categorized into two main types:multi-step forming methods and integral forming methods.The technical advantages and disadvantages of various manufacturing methods are analyzed,and the technical challenges of new manufacturing methods are discussed.Finally,the future development direction of manufacturing technology for dimensionally stable CFRP honeycombs is explored.

关键词

空间结构/尺寸稳定性/CFRP蜂窝/制造/轻量化

Key words

Space structure/Dimensional stability/CFRP honeycomb/Manufacture/Lightweight

分类

通用工业技术

引用本文复制引用

廖逸坚,卫宇璇,刘硕,朱大雷,马立..尺寸稳定性CFRP蜂窝制造方法的研究进展[J].宇航材料工艺,2025,55(4):26-33,8.

基金项目

国家重点研发计划(2022YFB3706104) (2022YFB3706104)

宇航材料工艺

OA北大核心

1007-2330

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