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浙江大学学报(工学版)
JOURNAL OF ZHEJIANG UNIVERSITY (ENGINEERING SCIENCE)
    
Data integration for aircraft digital assembly system
DOU Ya-dong, WANG Qing, LI Jiang-xiong, KE Ying-lin
State Key Laboratory of Fluid Power Transmission and Control, Zhejiang University, Hangzhou 310027, China
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Abstract  

Aircraft assembly data consist of large amount of scattered data, which represents complex assembly relationships as well as other important assembly information.Analysis, classification and integration of this information has become the major challenge in developing aircraft digital assembly system. A novel efficient framework was proposed to integrate this multi-dimensional data in aircraft assembly system based on cascade structure. Firstly, the assembly information was analyzed and classified according to different assembly requirements and scenarios. The cascade structure tree of task, object and device was then created respectively combined with the semantic definition of the structure. Finally, a complete integrated data model for the entire assembly process was established using relational theory. This data integration method has already been applied in aircraft assembly projects, the results show that the proposed data model has good versatility and flexibility, which can increase the efficiency of the assembly process.

Published: 26 December 2015
CLC:  TP 273  
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Cite this article:

DOU Ya-dong, WANG Qing, LI Jiang-xiong, KE Ying-lin. Data integration for aircraft digital assembly system. JOURNAL OF ZHEJIANG UNIVERSITY (ENGINEERING SCIENCE), 2015, 49(5): 858-865.

URL:

http://www.zjujournals.com/eng/10.3785/j.issn.1008-973X.2015.05.007     OR     http://www.zjujournals.com/eng/Y2015/V49/I5/858


飞机数字化装配系统数据集成技术

针对飞机数字化装配系统中装配数据零散、关系复杂、难于管理等特点,提出一种基于多重结构关联的数据关系模型,实现飞机数字化装配系统数据集成.结合装配工艺需求对数字化装配数据的来源进行分析,基于工艺意图对装配数据分类组织.建立逻辑上独立又互相关联的多重结构任务树、对象树和设备树,并给出多重结构的语义化定义.基于关系理论,建立完整的多重结构数据关系模型.装配数据集成技术已应用于飞机数字化装配系统,结果表明,该数据模型能够有效集成装配数据,并支持数据结构的重用和扩展．

［1］ 刘善国. 先进飞机装配技术及其发展［J］. 航空制造技术,2006,10:38-41．
LIU Shan-guo. Advanced aircraft assembly technol-ogy and development ［J］. Aeronautical manufactur-ing technology,2006,10:38-41．
［2］ 卢鹄,于勇,杨五兵,等. 飞机单一产品数据集成模型研究［J］. 航空学报,2010,31:0836-0841．
LU Hu, YU Yong, YANG Wu-bing, et al. Researchon Integration model of single source aircraft prod-uct data ［J］. Acta Aeronautica et Astronautica Si-nica,2010,31:0836-0841．
［3］ SEBASTIEN G, CLEMENT F. Application of the CMII model to an integrated engineering and man-ufacturing development environment［J］.InternationalJournal of Interactive Design and Manufacturin-g,2007,1(1):513．
［4］ SCOTT M, DAVID S. 747 Data Management Syst-em Development and Implementation［EB /OL］.（1999）［2014-08-02］. h-ttp:∥www.Kinematics.com/images/DMS-2.pdf.
［5］ 陈哲涵,杜福洲,唐晓青.基于关键测量特性飞机装配检测数据建模研究［J］.航空学报,2012,33:2143-2152．
CHEN Zhe-han, DU Fu-zhou, TANG Xiao-qing. K-ey measurement characteristics based inspection data modeling for aircraft assembly ［J］. Acta Aero-nautica et Astronautica Sinica,2012,33:2143-2152．
［6］ 靳江艳,黄翔,卢鹄,等. 飞机设计域向工装域映射机理研究［J］.航空学报,2012,33:2330-2337．
JIN Jinag-yan, HUANG Xiang, LU Hu, et al. Res-earch on mapping mechanism from product design to tooling concept design for aircraft ［J］.Acta Aeronautica et Astronautica Sinica, 2012,33:2330-2337．
［7］ 张佳朋,刘检华,宁汝新,等. 面向离散装配的过程和数据集成管理技术［J］. 计算机集成制造系统,2011,4: 0716:0725．
ZHANG Jia-peng, LIU Jian-hua, NING Ru-xin,et al.Integration management method of process and datafor discrete assembly ［J］. Computer Integrated M-anufacturing Systems,2011,4:0716:0725．
［8］ 韩清华,郑保,郭宏利,等. 采用激光跟踪仪测量飞机外形［J］. 航空计测技术,2004,1:00150018．
HAN Qing-hua, ZHENG Bao, GUO-Hongli, et al. Measurement of aircraft outline by using laser tracker equipment ［J］. Aviatioin Metrology & Me-asurent Technology,2004,1:00150018．
［9］ 曲巍巍,董辉跃,柯映林. 机器人辅助飞机装配制孔中位姿精度补偿技术［J］. 航空学报,2011,32:1951-1960．
QU Wei-wei, DONG Hui-yue, KE Ying-lin. Pose accuracy compensation technology in robot aidedaircraft assembly drilling process ［J］. Acta Aeron-autica et Astronautica Sinica,2011,32:1951-1960．
［10］ WHITNEY, D.E. The role of key characteristics in the design of mechanical assemblies ［J］.Assembly Automation,2006,26(4),315-322．
［11］ 王恒,宁汝新,唐承统. 三维装配尺寸链的自动生成［J］. 机械工程学报,2005,41(6):181-187．
WANG Heng, NING Ru-xin, TANG Cheng-tong. Automation generation of 3D assembly dimension chains ［J］. Journal Of Mechanical Engineering, 2005,41(6):181-187．
［12］ ZHENG L Y, MCMAHON C A, et al. Key chara-cteristics management in product lifecycle manage-ment: a survey of methodologies and practices［J］. Proceedings of the Institution of Mechanical E-ngineers, Part B: Journal of Engineering Manu-facture,2008,222:989-1008．
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