应用于飞机装配的并联机构技术发展综述

doi:10.7527/S1000-6893.2018.22572

材料工程与机械制造

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应用于飞机装配的并联机构技术发展综述

潘国威, 陈文亮, 王珉

南京航空航天大学机电学院, 南京 210016

收稿日期:2018-07-28 修回日期:2018-08-20 出版日期:2019-01-15 发布日期:2018-10-10
通讯作者: 陈文亮 E-mail:cwlme@nuaa.edu.cn
基金资助:
江苏省研究生培养创新工程（KYLX15_0299）

A review of parallel kinematic mechanism technology for aircraft assembly

PAN Guowei, CHEN Wenliang, WANG Min

College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received:2018-07-28 Revised:2018-08-20 Online:2019-01-15 Published:2018-10-10
Supported by:
Funding of Jiangsu Innovation Program for Graduate Education (KYLX15_0299)

摘要/Abstract

摘要： 并联机构的闭链结构使其具有良好的精度、刚性及动态性能，可满足飞机装配的精度、效率需求，因此，以并联机构为构型主体的自动化装配装备正越来越多地应用于飞机装配中。首先，概述了当前并联机构发展现状及飞机装配体现出的新特点，分析了并联机构应用于飞机装配的优势。其次，从飞机装配零部件加工和飞机零部件装配调姿定位两个方面综述了应用于飞机装配并联机构的国内外发展现状。然后，探讨了并联机构主要的前沿研究问题，从并联机构可重构设计、性能评价及优化设计、精度建模和力/位协同控制等4个方面，详细分析了并联机构应用于飞机装配中的关键技术。最后，对并联机构应用在飞机装配中未来的发展方向和机遇做了展望。

关键词: 飞机装配, 并联机构, 可重构, 性能评价, 优化设计, 精度建模, 力/位协同控制

Abstract: The closed-form chain structure provides the parallel mechanism with good precision, stiffness and dynamic performance, meeting the precision and efficiency requirements for aircraft assembly. Therefore, the automatic assembly equipment with parallel kinematic mechanism as the main component is more and more applied to aircraft assembly. Firstly, the current situation of parallel mechanism and the new characteristics of aircraft assembly are summarized, analyzing the advantages of parallel kinematic mechanism in aircraft assembly. Secondly, the domestic and foreign research on parallel kinematic mechanism in aircraft assembly is summarized from the component parts manufacture and pose/position adjustment. Thirdly, the main research problems of parallel kinematic mechanism are discussed. The key technologies of parallel mechanism in aircraft assembly are analyzed in detail from four aspects, including reconfigurable design, performance evaluation and optimization design, precision modeling and force/position coordinative control. Finally, the future development direction and opportunities of parallel mechanism in aircraft assembly are prospected.

Key words: aircraft assembly, parallel kinematic mechanism, reconfigurable, performance evaluation, optimal design, precision modeling, force/position coordinative control

中图分类号:

V262.4

潘国威, 陈文亮, 王珉. 应用于飞机装配的并联机构技术发展综述[J]. 航空学报, 2019, 40(1): 522572-522572.

PAN Guowei, CHEN Wenliang, WANG Min. A review of parallel kinematic mechanism technology for aircraft assembly[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(1): 522572-522572.

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

应用于飞机装配的并联机构技术发展综述

A review of parallel kinematic mechanism technology for aircraft assembly

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