北京航空航天大学学报2026，Vol.52Issue(6)：1990-1999,10.DOI:10.13700/j.bh.1001-5965.2024.0221
可重复使用运载器连接结构损伤容限分析
Damage tolerance analysis on reusable launch vehicle connection structures
摘要
Abstract
A damage tolerance test of the metal-composite connection structure with initial damage was conducted for the composite skin-metal skeleton structure used in the reusable launch vehicle,and a damage tolerance performance prediction model of the corresponding structure was created.The research results show that metal structures containing initial cracks at the edge of the connection hole will undergo crack expansion under fatigue load.Due to the geometric asymmetry of the connection structure,the crack expansion rates on the upper and lower surfaces are inconsistent,resulting in crack observation from the outer surface causing an error in the damage size.Extrusion load causes some delamination expansion in composite laminates with preset delaminations;extrusion fatigue damage to the composite materials is the primary cause of the damage.Delamination around composite connection holes will drastically reduce the life of the metal-composite connection structure.The damage tolerance design of the metal-composite connection structure should focus on composite hole edge delamination damage.The prediction results of the established metal-composite structure damage tolerance performance prediction model are in good agreement with the test results.It can well predict the damage expansion process and extended life of the structure,and can be used to guide the damage tolerance design of this type of structure.关键词
可重复使用运载器/结构/损伤容限/有限元法/损伤检测Key words
reusable launch vehicle/structure/damage tolerance/finite element method/damage detection分类
航空航天引用本文复制引用
李配缘,蔡巧言,黎增山,冯家赫..可重复使用运载器连接结构损伤容限分析[J].北京航空航天大学学报,2026,52(6):1990-1999,10.基金项目
中国运载火箭技术研究院自主研发重点项目资金支持 Financial Support for Key Independent Research and Development Projects of China Academy of Launch Vehicle Technology （）
