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浙江大学学报(工学版)
J4  2013, Vol. 47 Issue (5): 775-781    DOI: 10.3785/j.issn.1008-973X.2013.05.006
机械工程     
用于飞机数字化装配的浮动入位装置
蒋君侠,张兵,柯映林
浙江大学 机械工程学系,浙江 杭州 310027
A position-following device  for aircraft digital assembly
JIANG Jun-xia, ZHANG Bing , KE Ying-lin
Department of Mechanical Engineering, Zhejiang University, HangZhou 310027, China
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摘要：

针对飞机组件、部件的无应力入位问题,提出一种浮动入位方法,设计浮动入位装置.介绍飞机部件的定位器支撑布局,论述部件姿态调整对工艺球头入位形式的要求|提出浮动入位装置的技术要求,将浮动入位装置划分为直线移动模块、浮动锁紧模块和球头入位模块,对锁紧机构进行分析,并对装置的关键受力部位进行校核|最后,对2种浮动入位装置进行分析与比较.分析结果表明,该装置具有良好的入位适应性,可以有效释放组件、部件入位过程中的内应力,能够提供足够大的锁紧力并且不对飞机组件、部件的姿态产生破坏.
Abstract:

To obtain an accurate support for subassembly or component by ball joint with minimum stress, a position-following method is proposed, and position-following devices are designed. Firstly, the layout of four localizers which support the component is introduced. The principle of position and posture adjustment of the component, requirements of ball-heads' position and posture are analyzed. Secondly, technical requirements of the position-following device are made clear. Position-following device is divided into three modules, i.e. the linear motion module, the locking module and the ball-head supporting module. The locking mechanism is analyzed and stress check of key parts is conducted. Finally, two types of position-following devices are analyzed and compared. The analysis results show that the device has good adaptability, the stress of the subassembly or component of aircraft introduced in the positioning process can be released effectively, the device can provide enough force to lock itself reliably.
出版日期: 2013-05-01
:  TH 111  
基金资助:

浙江省自然科学基金资助项目（Y1110339）.
通讯作者: 柯映林，男，教授，博导.     E-mail: ylke@zju.edu.cn
作者简介: 蒋君侠（1968-)，男，高级工程师，从事飞机数字化装配技术研究工作. E-mail:junxia.jiang@126.com
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引用本文:

蒋君侠,张兵,柯映林. 用于飞机数字化装配的浮动入位装置[J]. J4, 2013, 47(5): 775-781.

JIANG Jun-xia, ZHANG Bing , KE Ying-lin. A position-following device  for aircraft digital assembly. J4, 2013, 47(5): 775-781.

链接本文:

http://www.zjujournals.com/eng/CN/10.3785/j.issn.1008-973X.2013.05.006    或    http://www.zjujournals.com/eng/CN/Y2013/V47/I5/775

［1］ 邹方,薛汉杰,周万勇,等.飞机数字化柔性装配关键技术及其发展［J］.航空制造技术,2006(9):30-35．
ZOU Fang, XUE Han-jie, ZHOU Wan-yong, et al. Key flexible assembly technology and its development of aircraft digital assembly ［J］. Aeronautical Manufa-cturing Technology, 2006(9):30-35．
［2］ BUTTERFIELD J, CROSBY S, CURRAN R, et al. Optimization of aircraft fuselage assembly process usi-ng manufacturing  ［J］.Journal of Computing and Information Science in Engineering, 2007,7(3): 269-275．
［3］ 邹方,张书生.飞机总装自动化校准对接系统 ［J］.航空制造技术,2008(7):32-36．
ZOU Fang, ZHANG Shu-sheng. Automatic alignment & butt system for aircraft final assembly  ［J］. Aeron-autical Manufacturing Technology, 2008(7):32-36．
［4］ 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 Sheng-qiang. Digital assembly technology system of aircraft ［J］.Aeronautical Manufacturing Technology, 2010(23):32-37．
［5］ 郭志敏,蒋君侠,柯映林. 基于定位器的飞机大部件调姿系统静刚度 ［J］.浙江大学学报：工学版, 2010,44(11):2077-2082．
GUO Zhi-min, JIANG Jun-xia, KE Ying-lin. Static sti-ffness of three-axis actuators based posture alignment system for large aircraft components ［J］.Journal of Zhejiang University: Engineering Science, 2010,44(11):2077-2082．
［6］ 邱宝贵,蒋君侠,毕云波,等.大型飞机机身调姿与对接试验系统 ［J］.航空学报,2011,32（5）：908-919．
QIU Bao-gui, JIANG Jun-xia, BI Yun-bo, et al. Posture alignment and joining test system for large ai-rcraft fuselages ［J］. Journal of Aeronautical, 2011,32(5):908-919．
［7］ 范玉青. 现代飞机器制造技术［M］. 北京：北京航空航天大学出版社, 2001:33-36．
［8］ QIU Bao-gui, JIANG Jun-xia, KE Ying-lin.A new principle and device for large aircraft components gai-ning accurate support by ball joint ［J］. Journal of Zh-ejiang University: SCIENCE A, 2011,12(5):405-414．
［9］ 李光俊,许晓东,陈妍君,等. 多点柔性托架激光测量划线系统的应用 ［J］. 航空制造技术,2010(7):32-34．
LI Guang-jun, XU Xiao-dong, CHEN Yan-jun, et al. Application of measurescore system with multipoint fl-exible bracket  ［J］. Aeronautical Manufacturing Tec-hnology, 2010(7):32-34．
［10］ SUNNANBO A.Laser feedback control for robotics in aircraft assembly［D］. Ostergotland, Sweden: Linko-pings University,2003．
［11］ 王巍,黄宇,庄建平.激光跟踪仪在飞机装配工装制造中的应用 ［J］.航空制造技术,2004(12):81-84．
WANG Wei, HUANG Yu, ZHUANG Jiang-ping.Application of laser tracker in assembly jig manufactu-ring for airplane ［J］. Aeronautical Manufacturing Te-chnology, 2004(12):81-84．
［12］ 濮良贵. 机械零件［M］. 北京：高等教育出版社,1982: 61-94．
［13］ 庄茁,由小川,廖剑晖,等. 基于ABAQUS的有限元分析和应用［M］. 北京：清华大学出版社,2009:129-150．
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