航空航天结构轻量化设计与实验方法研究进展  

Advances in Lightweight Design and Experimental Methods for Aerospace Structures

作　　者：王博[1] 郝鹏[1] 田阔 马祥涛 冯少军 WANG Bo;HAO Peng;TIAN Kuo;MA Xiangtao;FENG Shaojun(State Key Laboratory of Structural Analysis,Optimization and CAE Software for Industrial Equipment,Department of Engineering Mechanics,Dalian University of Technology,Dalian 116024,China)

机构地区：[1]大连理工大学工程力学系工业装备结构分析优化与CAE软件全国重点实验室,大连116024

出　　处：《宇航学报》2023年第4期596-606,共11页Journal of Astronautics

基　　金：国家自然科学基金(11825202,U21A20429)。

摘　　要：综述了近年来航空航天结构轻量化设计方法,聚焦薄壁结构与连接结构两类主要承载结构轻量化设计进行总结;针对薄壁结构,分析了面向后屈曲行为的轻量化设计、虑及缺陷的鲁棒性设计以及创新轻质薄壁领域的发展动向;针对连接结构,总结了传力路径与区域应力调控两大类设计方法。此外,就轻量化结构的高精度实验方法与数字孪生模型等共性关键问题进行梳理,并展望了未来航空航天结构轻量化设计方法发展前景,为未来研究工作和装备研发提供参考。The lightweight design methods of aerospace structures in recent years are reviewed and summarized,and the lightweight design of the thin-walled structure and connecting structure is discussed.For thin-walled structures,the development trends of lightweight design for post-buckling behavior,robust design considering imperfections,and innovative thin-walled configuration are analyzed.For connecting structures,two design methods are introduced from the load path and regional stress regulation.In addition,the common key problems such as high-precision experiment methods of lightweight structure and digital twin model are reviewed,and the development prospect of lightweight design methods for aerospace structure in the future are prospected,which could provide reference for future research work and equipment development.

关 键 词：航空航天结构 轻量化设计 薄壁结构 连接结构 优化方法 

分 类 号：V11[航空宇航科学与技术—人机与环境工程]