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论文:2012,Vol:30,Issue(1):129-137 |
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引用本文: |
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张开富, 曾佩杰, 栾超, 牟伟强, 李原. 空间多姿态下自动钻铆托架变形分析与调平方法[J]. 西北工业大学 |
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Zhang Kaifu, Zeng Peijie, Luan Chao, Mu Weiqiang, Li Yuan. An Effective Deformation Analysis and Leveling Method for Work Positioning of Automatic Riveting System in Multi-Pose Space[J]. Northwestern polytechnical university |
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空间多姿态下自动钻铆托架变形分析与调平方法 |
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张开富, 曾佩杰, 栾超, 牟伟强, 李原 |
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西北工业大学 现代设计与集成制造技术教育部重点实验室,陕西 西安 710072 |
摘要: |
飞机壁板自动钻铆系统中托架具有自重大、跨距长、变形量大等特点,其变形误差随工作姿态的不同而改变,从而导致壁板钻铆超差。文章在对自动钻铆托架结构设计基础上,建立了托架横梁弯曲变形模型,根据钻铆点位与横梁变形曲线的空间关系构建了壁板钻铆点位变形量数学模型;针对传统调平补偿方法无法精确满足托架变形量动态变化的问题,采用迭代优化方法建立了托架多姿态变形补偿调平算法;并采用有限元仿真方法分析了托架处于各角度时钻铆点位的变形量及外法线向量;将理论算法数据与仿真数据进行了对比分析,验证了文中提出的托架变形分析与调平算法的正确性和有效性。 |
关键词:
自动钻铆
托架
变形分析
迭代优化
有限元仿真
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An Effective Deformation Analysis and Leveling Method for Work Positioning of Automatic Riveting System in Multi-Pose Space |
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Zhang Kaifu, Zeng Peijie, Luan Chao, Mu Weiqiang, Li Yuan |
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The Ministry of Education Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Northwestern Polytechnical University, Xi'an 710072, China |
Abstract: |
The panel work positioner of automation riveting system has some characteristics: it is heavy,its span islong, and its deformation is large.Its deformation errors change as its working pose changes, thus leading to that thepanel' s tolerances are exceeded.Then the panel is defective.In order to control the deformation of the work posi-tioner,sections 1 through 3 of the full paper present a deformation analysis and leveling method for work positionerof automation drilling and riveting system in multi-pose space,which we believe is more effective than previousones.Section 1 does two things: (1) it establishes a deformation model of the work positioner' s crossbeam basedon the position model of automatic drilling and riveting system; (2) it establishes the deformation model of panel' sdrilling and riveting points by the geometrical relationship between each point and the crossbeam' s deformationcurve.Section 2 presents an algorithm compensating for the deformation errors of the work positioner in multi-posespace based on the iterative optimizing method.Section 3 does two things: (1) it uses the finite element method toanalyze the deformations and the out normal vectors of the drilling and riveting points in multi-pose space; (2) itanalyzes contrastively the theoretical deformation errors and simulation errors.The simulation results,presented inFigs.9 through 11 and Table 2,and their analysis indicate that our method is indeed accurate for calculating thework positioner' s deformation errors,thus compensating effectively for the deformation errors. |
Key words:
aircraft
algorithms
analysis
calculations
computer software
control
deformation
errors
evalua-tion
finite element method
flowcharting
fuselages
geometry
iterative methods
measurements
models
numerical methods
optimization
riveting
schematic diagrams
simulation
wings
automat-ic riveting system
work positioner
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收稿日期: 2011-04-30
修回日期:
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DOI: |
基金项目: 航空科学基金(2010ZE53050);国家商用飞机制造工程技术研究中心创新基金(SAMC11-JS-07-200);西北工业大学基础研究基金(JC201032)资助 |
通讯作者:
Email: |
作者简介: 张开富(1977-),西北工业大学副教授、博士,主要从事飞机先进装配技术、数字化制造技术等研究。
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张开富 在本刊中的所有文章 |
曾佩杰 在本刊中的所有文章 |
栾超 在本刊中的所有文章 |
牟伟强 在本刊中的所有文章 |
李原 在本刊中的所有文章 |
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参考文献: |
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[1] Atre Amarendra,Johnson W S. Analysis of the Effects of Interference and Sealant on Riveted Lap Joints. Journal of Aircraft,2007, 44(2): 353~364 [2] Park J H,Atluri S N. Fatigue Growth of Multi-Cracks near a Row of Fastener-Holes in a Fuselage Lap-Joint. Computational Me-chanics, 1993, 13(3): 189~203 [3] Shishkin S S. Computation of the Contact Load in a Rivet Bond. Journal of Machinery Manufacture and Reliability,2010,39(1): 43~46 [4] Blanchot V,Daidie A. Riveted Assembly Modeling: Study and Numerical Characterisation of a Riveting Process. Journal of Ma-terials Processing Technology, 2006, 180(1-3): 201~209 [5] Iyer K,Rubin C A, Hahn G T. Influence of Interference and Clamping on Fretting Fatigue in Single Rivet-Row Lap Joints. Jour-nal of Tribology, 2001, 123(4): 686~698 [6] Cai W. Fixture Optimization for Sheet Panel Assembly Considering Welding Gun Variations. Proceeding of the Institution of Me-chanical Engineers,Part C: Journal of Mechanical Engineering Science, 2008, 222 (2): 235~246 [7] Skorupa M,Skorupa A,Machniewicz T,Korbel A. Effect of Production Variables on the Fatigue Behaviour of Riveted LapJoints. International Journal of Fatigue, 2010, 32(7): 996~1003 [8] Li Jun,Hua Hongxing,Shen Rongying. Dynamic Stiffness Analysis of a Beam Based on Trigonometric Shear Deformation Theo-ry. Journal of Vibration and Acoustics, 2008, 130: 101~107 [9] 张伯鹏,张年松. 机床横梁重力变位的自演进补偿. 清华大学学报, 2006, 46 (2): 191~193Zhang Bopeng,Zhang Niansong. Self-Evolutionary Compensation of Machine Tool Crossbeam Deformation Induced by Gravity.Journal of Tsinghua University, 2006, 46 (2): 191~193 (in Chinese) [10] 王洪才,李福才,刘俊龙,孙 文. 数控落地铣镗床滑枕变形补偿系统. 齐齐哈尔大学学报 2002, 18(3)100~104Wang Hongcai,Li Fucai,Liu Junlong,Sun Wen. Beam Sag System for CNC Milling and Boring Machine Tool. Journal of Qiqi-har University(Natural Science Edition), 2002, 18(3)100~104 (in Chinese) [11] Kashyap S,Devries W R. Finite Element Analysis and Optimization in Fixture Design. Structural Optimization. 1999(18):193~201 [12] 陈允全,卜 昆,董一巍,刘 杰. 基于 ANSYS 的数控托架变形求解方法研究. 机床与液压, 2007, 35 (10): 77~79Chen Yunquan,Bu Kun,Dong Yiwei,Liu Jie. Research on a Calculation Method Based on ANSYS for the Deformation of CNCFacility. Machine Tool & Hydraulics, 2007, 35 (10): 77~79 (in Chinese) [13] Bira F,Bosetti P,Oboe R,Tondini F, Trento Univ. A New Direct Deformation Sensor for Active Compensation of Positioning Er-rors in Large Milling Machines. Advanced Motion Control, 2006. 9th IEEE International Workshop 126~131 [14] 秦现生,汪文旦,楼阿莉,尉 藤. 大型壁板数控钻铆的三点快速调平算法. 航空学报, 2007, 28 (26): 1455~1460Qin Xiansheng,Wang Wendan,Lou Ali,Wei Teng. Three-Point Bracket Regulation Algorithm for Drilling and Riveting of Aero-foil. Acta Aeronautica et Astronautica Sinica, 2007, 28 (26): 1455~1460 (in Chinese) [15] 郭志敏,蒋君侠,柯映林. 基于 POGO 柱三点支撑的飞机大部件调姿方法. 航空学报, 2009, 30(7): 1319~1324Guo Zhimin,Jiang Junxia,Ke Yinglin. Posture Alignment for Large Aircraft Parts Based on Three POGO Sticks Distributed Sup-port. Acta Aeronautica et Astronautica Sinica, 2009, 30(7):1319~1324 (in Chinese) [16] 西安飞机工业(集团)有限责任公司. 一种用于自动钻铆托架变形的修补数据处理方法. 中国发明专利, CN1920715A.2007, 2Xi'an Aircraft Industry (Group) Company Limited. Method for Data Modification and Supplement for Automatic Rivet Bracket De-formation. Chinese patent,CN1920715A. 2007, 2 (in Chinese) |
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