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气动锤铆过程仿真分析与试验 被引量:14

Simulation and test on process of percussive Impact riveting
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摘要 为提高锤铆工艺质量,提出一种对锤铆过程仿真分析的方法,并获得锤铆工艺所需铆接时间.建立气动铆枪的运动学模型,结合Matlab仿真得到不同输入气压下(0.2~0.6 MPa)冲锤的冲击速度及其冲击频率;在ABAQUS中对锤铆过程进行有限元分析,将运动学模型的仿真结果(冲锤的冲击速度及频率)应用至有限元模型中,以获得规定的镦头尺寸为目标,得到不同输入气压下需要的铆接时间.实验得到铆钉在0.2~0.6MPa不同气压下的铆接时间,实验值与仿真值的偏差在15%之内,验证此仿真方法的可行性.结果表明,铆枪的输入气压及铆接时间是影响锤铆工艺的关键因素. Kinematic modeling and simulation of percussive impact riveting are presented to improve the quality of riveting process. Kinematic model of rivet gun is setup to determine the output speed and frequency of hammer under different input pneumatic pressure, ranging from 0. 2 MPa to 0. 6 MPa; Process of percussive impact riveting is simulated in ABAQUS, and by setting different speed of hammer (acquired in the kinematic model), the corresponding riveting time is acquired when the driven rivet head dimension is acceptable. Finally, riveting tests are carried out for model validation donghuiyue, Deviation between the simulation and experimental results is under 15%, which shows the effectiveness of the proposed method. All above end up with an conclusion that input pressure and riveting time has a great influence on riveting process.
出处 《浙江大学学报(工学版)》 EI CAS CSCD 北大核心 2014年第8期1411-1418,共8页 Journal of Zhejiang University:Engineering Science
基金 国家自然科学基金资助项目(51305395) 中央高校基本科研业务费专项资金资助项目(2014FZA4003)
关键词 锤铆 运动学模型 铆接时间 有限元仿真 percussive riveting kinematic model riveting time finite element analysis
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  • 1焦圣喜,韩立强,岳晓峰,王平凯.一种新的机器人手-眼视觉目标定位方法[J].武汉理工大学学报,2008,30(1):130-133. 被引量:2
  • 2Liu D K. A simplified approach for evaluating bendability and springback in plastic bending of anisotropic sheet metals. Journal of Materials Processing Technology 1997; 66(1-3): 9-17.
  • 3Zeng Z W, Liu X, Deng Y M, et ah A parametric study of magneto-optic imaging using finite-element analysis applied to aircraft rivet site inspection. IEEE Transactions on Magnetics 2006; 42(11): 3737-3744.
  • 4Moreno J, Valiente A. Stress intensity factors in riveted steel beams. Engineering Failure Analysis 2004; 42(11): 777-787.
  • 5Mu W Q, Li Y, Zhang K F, et al. An effective method of studying interference-fit riveting for 2117-T4 aluminum slug rivet. 2010 International Conference onComputer and Communication Technologies in Agriculture Engineering. 2010; 2:303-307.
  • 6Dong H Y, Ke Y L. Study on machining deformation of aircraft monolithic component by FEM and experiment. Chinese Journal of Aeronautics 2006; 19(3): 247-254.
  • 7Yang Y H, Liu D, He Z Y, et al. Optimization of preform shapes by RSM and FEM to improve deformation homogeneity in aerospace forgings. Chinese Journal of Aeronautics 2010; 23(2): 260-267.
  • 8Rans C, Straznicky P V, Alderliesten R. Riveting process induced residual stresses around solid rivets in mechanical joints. Journal of Aircraft 2007; 44(1): 323-329.
  • 9de Rijck J J M, Homan J J, Schijve J, et al. The driven rivet head dimensions as an indication of the fatigue performance of aircraft lap joints. International Journal of Fatizue 2007; 29(12): 2208-2218.
  • 10Urban M R. Analysis of the fatigue life of riveted sheet metal helicopter airframe joints. International Journal of Fatigue 2003; 25(9-11): 1013-1026.

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