飞机复合材料机身壁板装配技术分析与展望  

Analysis and Prospect of Assembly Technology of Aircraft Composite Fuselage Panel

作　　者：陈文亮[1] 李奕星 冯素玲[1,2] CHEN Wenliang;LI Yixing;FENG Suling(Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;COMAC Shanghai Aircraft Manufacturing Co.,Ltd.,Shanghai 201324,China)

机构地区：[1]南京航空航天大学,南京210016 [2]中国商飞上海飞机制造有限公司,上海201324

出　　处：《航空制造技术》2024年第16期59-73,共15页Aeronautical Manufacturing Technology

基　　金：国家自然科学基金(51875283)。

摘　　要：复合材料以其优异的综合性能在航空航天领域得到了大量应用,其应用范围逐渐从次承力结构向主承力结构扩展,包括在机身结构的组成方面,传统的金属组装壁板逐渐被复合材料整体壁板所取代。由于复合材料壁板具有不同于传统金属材料壁板的装配工艺特点,因此对其装配方法和装配工艺提出了新的要求。针对圆筒状机身复合材料机身壁板的装配过程,分别介绍了复合材料机身壁板大尺寸测量技术、复合材料机身壁板装配定位调姿技术和复合材料机身壁板的先进制孔连接技术,系统总结了近年来国内外相关研究进展和应用情况,指出了飞机大尺寸复合材料结构装配技术未来的研究与应用方向。Composite materials are widely used in the aerospace field due to their excellent comprehensive properties.The application range of composite materials is gradually expanding from secondary load-bearing structures to main load-bearing structures.The traditional metal assembly panels constituting the fuselage structure are gradually been replaced by composite integral panels.The composite panels with assembly processing characteristics that are different from traditional metal panels,therefore,new requirements for assembly methods and assembly processes are proposed.Aiming at the assembly process of aircraft composite fuselage panels,the large-scale measurement technology,the assembly positioning and attitude adjustment technology,and the advanced hole connection of composite fuselage panels are introduced.Research progress and application situation at home and abroad in recent years are systematically summarized,and the future research and application development direction of aircraft large-scale composite structure assembly technology is expounded.

关 键 词：飞机装配 复合材料 机身壁板 测量 柔性工装 定位调姿 机械连接 

分 类 号：V262.4[航空宇航科学与技术—航空宇航制造工程]