飞机零部件自适应装配系统研究

中国机械工程

飞机零部件自适应装配系统研究

石章虎1,2,3;邓珍波1,2;罗勇1,2;毕修文1,2;殷国富2,4

1.航空工业成都飞机工业(集团)有限责任公司，成都，610037
2.四川省航空智能制造装备工程技术研究中心，成都，610037
3.南京航空航天大学机电学院，南京，210016
4.四川大学机械工程学院，成都，610065

出版日期:2020-06-25 发布日期:2020-07-22
基金资助:
国家自然科学基金资助项目(51475152)

Research on Adaptive Assembly Systems for Aircraft Parts

SHI Zhanghu1,2,3;DENG Zhenbo1,2;LUO Yong1,2;BI Xiuwen1,2;YIN Guofu2,4

1.AVIC Chengdu Aircraft Industrial(Group)Co.,Ltd.,Chengdu,610037
2.Sichuan Provincial Engineering Research Center for Aircraft Intelligent Manufacturing Equipment,Chengdu,610037
3.College of Mechanical and Electrical Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing,210016
4.School of Mechanical Engineering，Sichuan University，Chengdu,610065

Online:2020-06-25 Published:2020-07-22

摘要/Abstract

摘要： 针对当前飞机零部件装配型架自动化程度低、装配过程可控性差等问题，研究了一种飞机零部件自适应装配系统。该系统集成了虚拟技术、激光跟踪仪检测技术与柔性定位技术，采用了基于力与位移的全闭环控制方法，借助虚拟装调系统实现关键部件的自适应定位与装夹。系统采用某型机机头锥作为自适应装配验证对象，完成了对该部件的自适应精确装调，保证了安装精度，实现了装配过程中力与位移的监控。

关键词: 飞机零部件, 自适应装配系统, 虚拟技术, 柔性定位技术, 全闭环

Abstract: Aiming at the problems during the assembly processes of aircraft parts, such as low automation and poor controllability, an adaptive assembly system was presented for aircraft parts.The system integrated digital virtual technology, laser tracker detection technology and flexible location technology.A full-closed control method was used based on forces and displacements.The key parts were located and clamped adaptively by virtual assembly system.In order to verify the functions of the intelligent system, the nose cone of aircraft was assembled.The results show that the system may guarantee aircraft parts assembled adaptively and accurately.The force and displacement during the assembly processes were under control.

Key words: aircraft parts, adaptive assembly system, virtual technology, flexible location technology, full-closed loop

中图分类号:

石章虎1,2,3;邓珍波1,2;罗勇1,2;毕修文1,2;殷国富2,4. 飞机零部件自适应装配系统研究[J]. 中国机械工程.

SHI Zhanghu1,2,3;DENG Zhenbo1,2;LUO Yong1,2;BI Xiuwen1,2;YIN Guofu2,4. Research on Adaptive Assembly Systems for Aircraft Parts[J]. China Mechanical Engineering.

参考文献

[1]王云渤, 张关康, 冯宗律, 等.飞机装配工艺学(修订本) [ M ] .北京: 国防工业出版社, 1990：1-50.

WANG Yunbo, ZHANG Guankang, FENG Zonglü, et al.Aircraft Assembly Process(Revised Edition)[M].Beijing: Defense Industry Press, 1990:1-50.

[2]EIMARAGHY H, SCHUH G.Managing Variations in Products, Processes and Manufacturing Systems [J].Manufacturing Technology, 2009,58(1):441-446.

[3]HU S J, KO J, WEYAND L, et al.Assembly System Design and Operations for Product Variety[J].Manufacturing Technology, 2011,60(2):715-733.

[4]刘检华，白书清，段华，等.面向手工装配的计算机辅助装配过程控制方法[J].计算机集成制造系统，2009, 15（12）：2391-2398.

LIU Jianhua, BAI Shuqing, DUAN Hua, et al.Computer Aided Assembly Process Control Method for Manual Assembly[J].Computer Integrated Manufacturing Systems, 2009,15(12):2391-2398.

[5]何胜强.飞机数字化装配技术体系[J].航空制造技术，2010(23):32-37.

HE Shengqiang.Digital Assembly Technology System of Aircraft[J].Aeronautical Manufacturing Technology, 2010(23):32-37.

[6]王亮, 李东升, 刘贵凤, 等.飞机壁板类组件数字化装配柔性工装技术及应用[J].航空制造技术,2010(10):58-61.

WANG Liang, LI Dongsheng, LIU Guifeng, et al.Flexible Tooling Technology and Application for Digital Assembly of Aircraft[J].Aeronautical Manufacturing Technology, 2010(10):58-61.

[7]许国康.大型飞机自动化装配技术[J].航空学报, 2008, 29(3): 734-740.

XU Guokang.Automatic Assembly Technology for Large Aircraft[J].Acta Aeronautica et Astronautica Sinica, 2008, 29(3): 734-740.

[8]郭飞燕, 王仲奇, 康永刚, 等.基于坐标孔的翼肋柔性装配协调方法[J].中国机械工程, 2014,25(24):3271-3277.

GUO Feiyan, WANG Zhongqi, KANG Yonggang, et al.Flexible Assembly Method of Ribs Based on Coordinate Holes[J].China Mechanical Engineering,2014,25(24):3271-3277.

[9]邹冀华, 周万勇, 韩先国.飞机装配中基于3 -RPS 的并联机构法向调整算法[J].中国机械工程, 2011,22(5):557-560.

ZOU Jihua, ZHOU Wanyong, HAN Xianguo.Normal Adjusting Algorithm of a 3-RPS Parallel Mechanism in Airplane Assembly[J].China Mechanical Engineering,2011,22(5):557-560.

[10]刘春.飞机大部件数字化对接装配系统中若干关键技术研究[D].杭州：浙江大学, 2013.

LIU Chun.Research on Several Key Technologies in Aircraft Digital Assembly System[D].Hangzhou: Zhejiang University,2013.

[11]罗中海, 孟祥磊, 巴晓甫, 等.飞机大部件调姿平台力位混合控制系统设计[J].浙江大学学报(工学版), 2015, 49(2): 265-274.

LUO Zhonghai, MENG Xianglei, BA Xiaofu, et al.Design on Hybrid Force Position Control of Large Aircraft Components Posture Alignment Platform[J].Journal of Zhejiang University (Engineering Science), 2015, 49(2): 265-274.

[12]俞慈君, 李江雄, 余锋杰, 等.带工程约束的点匹配算法[J].机械工程学报, 2010，46 (5): 183-190.

YU Cijun, LI Jiangxiong, YU Fengjie, et al.3D Points Registration Algorithm with Engineering Constraints[J].Journal of Mechanical Engineering, 2010,46 (5): 183-190.

[13]庄存波,刘检华,熊辉, 等.复杂产品装配现场动态实时可视化监控系统[J].计算机集成制造系统, 2017,23(6):1264-1276.

ZHUANG Cunbo, LIU Jianhua, XIONG Hui, et al.Assembly Shop Floor Dynamic and Real-time Visual Monitoring System for Complex Product[J].Computer Integrated Manufacturing Systems, 2017,23(6): 1264-1276.