Survey of Automated Flexible Docking Assembly Technology for Large-scale Components

被引：1
|
作者：
Zhao H. [1 ]
Ge D. [1 ]
Luo L. [1 ]
Yin Y. [1 ]
Ding H. [1 ]
机构：
[1] State Key Laboratory of Digital Manufacturing Equipment and Technology, Huazhong University of Science and Technology, Wuhan
来源：
Jixie Gongcheng Xuebao/Journal of Mechanical Engineering | 2023年 / 59卷 / 14期
关键词：
control; digital measurement technology planning; docking assembly; large components; pose adjustment;
D O I：
10.3901/JME.2023.14.277
中图分类号：
学科分类号：
摘要：
The docking assembly of large components is an important part of the final assembly of large aerospace vehicles. With the increasing demand for rapid response to space missions, such as launching emergency satellites and commercial communication satellites, it is urgent to improve the rapid assembly and launch capability of large aircraft such as launch vehicles. In order to improve the reliability and efficiency of the docking assembly, the assembly mode is moving from the original manual mode to the direction of automation, digitization, and intelligence. The three key technologies involved in the automatic flexible docking assembly of large components are reviewed. The principle, characteristics and application of the pose adjustment mechanism, digital measurement technology, planning and control technology of large-scale component docking assembly are summarized in detail. The future research directions of automatic flexible docking assembly technology for large-scale component are also discussed. © 2023 Chinese Mechanical Engineering Society. All rights reserved.
引用
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页码：277 / 297
页数：20
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共 134 条
  • [11] WILLIAMS G, CHALUPA E, RAHHAL S., Automated positioning and alignment systems[J], SAE Transactions, 109, 1, pp. 737-745, (2000)
  • [12] Alabama factory makes missiles with robots
  • [13] FLYNN R, PAYTON-STEWART K, BREWER P, Et al., Unique material handling and automated metrology systems provides backbone of accurate final assembly line for business jet, (2016)
  • [14] DILLHOFER T, ESTEBAN D G., IFAC (integrated fuselage assembly cell)[J], SAE Transactions, pp. 937-946, (2006)
  • [15] Liang CHENG, Qing WANG, Jiangxiong LI, Et al., A posture evaluation method for a large component with thermal deformation and its application in aircraft assembly[J], Assembly Automation, 34, 3, pp. 275-284, (2014)
  • [16] Hua LIU, Weidong ZHU, Yinglin KE, Pose alignment of aircraft structures with distance sensors and CCD cameras[J], Robotics and Computer-Integrated Manufacturing, 48, pp. 30-38, (2017)
  • [17] WANG Qing, LIANG Qin, LI Jiangxiong, Et al., Estimation and alignment method of wing position and orientation for aircraft digital assembly[J], Journal of Zhejiang University, 48, 7, pp. 1287-1294, (2014)
  • [18] Qing WANG, Yadong DOU, Jiangxiong LI, Et al., An assembly gap control method based on posture alignment of wing panels in aircraft assembly[J], Assembly Automation, 37, 4, pp. 422-433, (2017)
  • [19] GUO Zhimin, JIANG Junxia, KE Yinlin, Posture alignment for large aircraft parts based on three POGO sticks distributed support[J], Acta Aeronautica Et Astronautica Sinica, 30, 7, pp. 1319-1324, (2009)
  • [20] ZHANG Bin, Baoguo YAO, Yinglin KE, A novel posture alignment system for aircraft wing assembly[J], Journal of Zhejiang University-Science A, 10, 11, pp. 1624-1630, (2009)
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