摘要
随着航空新技术的发展,复合材料结构健康监测(SHM)技术成为飞机结构设计的热点。SHM在设计过程中,除了要考虑在技术实现方面的需求,还应考虑实际维修工作和适航要求对SHM技术的需求。本文结合现阶段复合材料冲击损伤检测维护程序,考虑SHM技术的发展趋势和适航要求,分析了SHM技术运用后的维修场景,提出了复合材料冲击损伤检测维护对SHM技术需求。
Within the development of aviation technology,structural health monitoring(SHM)technology for composite material structure has been hot point of structure design.During the SHM system design process,maintenance work requirement should be considered besides the technology realization requirement.Based on the current maintenance process of composite material impact damage,this paper integrates the development tendency of SHM technology,analyses the maintenance scene based on SHM,and presents the composite material impact damage detection and maintenance requirement to SHM technology.
作者
蔡禹舜
朱昊
卿新林
CAI Yushun;ZHU Hao;QING Xinlin(Shanghai Aircraft Customer Service Co.,Ltd.,Shanghai 200241,China;School of Aerospace Engineering,Xiamen University,Xiamen 361005,China;Beijing Aeronautical Science and Technology Research Institute of COMAC,Beijing 102211,China)
出处
《航空制造技术》
2018年第7期78-82,共5页
Aeronautical Manufacturing Technology
关键词
飞机结构
复合材料
冲击损伤
结构健康监测
设计需求
Aircraft structure
Composite material
Impact damage
Structure health monitoring
Design requirement