可重复使用运载器连接结构损伤容限分析OA
Damage tolerance analysis on reusable launch vehicle connection structures
针对可重复使用运载器冷结构中应用的复合材料蒙皮-金属骨架结构,开展了含初始损伤的金属-复材连接结构的损伤容限试验,并建立对应结构的损伤容限性能预测模型.研究结果表明:含孔边裂纹的金属结构在疲劳载荷作用下会发生裂纹扩展,而且由于连接不对称的影响,上下表面的裂纹扩展速率不一致,致使从外表面进行裂纹观测会造成对损伤尺寸的保守统计;含预置分层的复合材料层合板在挤压载荷作用下出现一定的分层扩展,其主要损伤还是由于复材的挤压疲劳破坏;复材孔边分层会急剧降低金属-复材连接结构的寿命;金属-复材连接结构的损伤容限设计应该重点关注复材孔边分层损伤;建立的金属-复材结构损伤容限性能预测模型预测结果与试验结果吻合良好,能很好的预测结构的损伤扩展过程和扩展寿命,可用于指导该类结构的损伤容限设计.
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.
李配缘;蔡巧言;黎增山;冯家赫
北京宇航系统工程研究所,北京 100076中国运载火箭技术研究院,北京 100076北京航空航天大学 航空科学与工程学院,北京 100191北京航空航天大学 航空科学与工程学院,北京 100191
航空航天
可重复使用运载器结构损伤容限有限元法损伤检测
reusable launch vehiclestructuredamage tolerancefinite element methoddamage detection
《北京航空航天大学学报》 2026 (6)
1990-1999,10
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
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