A Digital Twin System for Adaptive Aligning of Large Cylindrical Components

被引:0
作者
Fan, Wei [1 ,2 ,3 ]
Xiao, Ruoyao [1 ]
Zhang, Jieru [4 ]
Zheng, Linayu [1 ,2 ,3 ]
Zhou, Jian [1 ]
机构
[1] Beihang Univ, Sch Mech Engn & Automat, Beijing 100191, Peoples R China
[2] Minist Ind & Informat Technol, MIIT Key Lab Intelligent Mfg Technol Aeronaut Adv, Beijing 100191, Peoples R China
[3] Beijing Key Lab Digital Design & Mfg Technol, Beijing 100191, Peoples R China
[4] Beijing Xinfeng Aerosp Equipment Co Ltd, Beijing 100854, Peoples R China
来源
APPLIED SCIENCES-BASEL | 2024年 / 14卷 / 18期
关键词
large aerospace cylindrical component; digital twin; adaptive aligning system; aligning trajectory error prediction; adaptive aligning control;
D O I
10.3390/app14188307
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
Most large aerospace cylindrical components still adopt a manual aligning method with low automation, large manual intervention, and heavy dependence on operator workers, resulting in the low quality and efficiency of large component aligning, which seriously prolongs the manufacturing time of aerospace products. To cope with this issue, based on closed-loop adaptive control and digital twin (DT) technologies, an adaptive aligning system for large cylindrical components, i.e., the DT aligning system, is proposed in this study. For the DT aligning system, through the DT multi-dimensional modeling, i.e., geometric modeling, physical modeling, functional modeling, and data modeling, it can be divided into a physical space, a virtue space, and twin data. Note that the association, mapping, and interaction between physical space and virtual space of the aligning system can be realized via the twin data, thereby realizing real-time virtual display, monitoring, and control of the large component aligning. In addition, based on the measured pose data, aligning stress, and predicted aligning error, an adaptive force/position control method for large component aligning is proposed, and it can achieve real-time decision-making and precise execution of the aligning process. Finally, through application validation, the DT process system can realize the real-time status perception and process execution decision during the large component aligning. Finally, through experimental validation, it is found that the proposed system, i.e., the DT aligning system, can improve the quality and efficiency of the large aerospace cylindrical component aligning, as well as the automation and intelligent level of the aligning system.
引用
收藏
页数:21
相关论文
共 25 条
[1]   Feature-based function block control framework for manufacturing equipment in cloud environments [J].
Adamson, Goran ;
Wang, Lihui ;
Moore, Philip .
INTERNATIONAL JOURNAL OF PRODUCTION RESEARCH, 2019, 57 (12) :3954-3974
[2]  
Bond J., 2013, Mod. Mater. Handl, V68, P48
[3]  
Dai W.B., 2014, Spacecr. Environ. Eng, V31, P584
[4]   A machining accuracy informed adaptive positioning method for finish machining of assembly interfaces of large-scale aircraft components [J].
Fan, Wei ;
Zheng, Lianyu ;
Ji, Wei ;
Xu, Xun ;
Lu, Yuqian ;
Wang, Lihui .
ROBOTICS AND COMPUTER-INTEGRATED MANUFACTURING, 2021, 67 (67)
[5]   Function block-based closed-loop adaptive machining for assembly interfaces of large-scale aircraft components [J].
Fan, Wei ;
Zheng, Lianyu ;
Ji, Wei ;
Xu, Xun ;
Wang, Lihui ;
Lu, Yuqian ;
Zhao, Xiong .
ROBOTICS AND COMPUTER-INTEGRATED MANUFACTURING, 2020, 66
[6]  
Grieves M., 2017, Springer Nat Link, P85, DOI [DOI 10.1007/978-3-319-38756-7_4, 10.1007/978-3-319-38756-7_4 10.1007/978-3-319-38756-7_4]
[7]   Digital manufacturing and flexible assembly technologies for reconfigurable aerospace production systems [J].
Jackson, Keith ;
Efthymiou, Konstantinos ;
Borton, John .
SIXTH INTERNATIONAL CONFERENCE ON CHANGEABLE, AGILE, RECONFIGURABLE AND VIRTUAL PRODUCTION (CARV2016), 2016, 52 :274-279
[8]   How to model and implement connections between physical and virtual models for digital twin application [J].
Jiang, Haifan ;
Qin, Shengfeng ;
Fu, Jianlin ;
Zhang, Jian ;
Ding, Guofu .
JOURNAL OF MANUFACTURING SYSTEMS, 2021, 58 :36-51
[9]   A new method for automatic shaft-hole assembly of aircraft components [J].
Jiang, Junxia ;
Bian, Chen ;
Ke, Yinglin .
ASSEMBLY AUTOMATION, 2017, 37 (01) :64-70
[10]  
Jing Xishuang, 2015, Journal of Beijing University of Aeronautics and Astronautics, V41, P1196, DOI 10.13700/j.bh.1001-5965.2014.0635