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无头铆钉成型过程的有限元仿真与试验分析

Finite Element Simulation and Experimental Analysis of Headless Rivet Forming Process
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摘要 采用ABAQUS建立有限元分析模型,分析了66°锥形铆模压铆无头铆钉的成型过程。对成型后的试片进行了力学及金相分析,并将结果与普通半圆头铆钉进行对比。研究结果表明,无头铆钉的压铆变形过程为钉杆中间最早涨粗,墩头部分成型,随后钉杆部分逐步与孔壁均匀挤压的过程;随着压铆位移的增加,无头铆钉拉脱强度及剪切强度均呈上升趋势;与传统平铆模成型的半圆头铆钉相比,在锥形铆模的作用下,金属材料向钉杆流动更加均匀,墩头两侧的绝热剪切效应明显弱化。 In this paper,the finite element analysis was established by ABAQUS to analyze the forming process of headless rivet pressed by 66°conical riveting die.Mechanical and metallographic analysis of the formed specimen were carried out,and the results were compared with those prepared by ordinary semi-circular head rivets.The results showed that during pressing deformation,the middle of the nail bar is thickened at the earliest forming the pier head,after which the nail bar is squeezed evenly with the hole wall gradually.With the increase of riveting displacement,the pull-out strength and shear strength of headless rivets elevate.Compared with the semi-circular head rivet formed by traditional flat riveting die,the metal material flows more evenly to the nail rod in conical riveting die,and the adiabatic shear effect on both sides of the pier head is significantly weakened.
作者 吕晓敏 吴林轩 曹臣鹏 王天鹏 刘晚 LV Xiaomin;WU Linxuan;CAO Chenpeng;WANG Tianpeng;LIU Wan(Tianjin Long March Launch Vehicle Manufacturing Co.Ltd.,Tianjin 300462)
出处 《宇航材料工艺》 CAS CSCD 北大核心 2023年第6期93-97,共5页 Aerospace Materials & Technology
关键词 无头铆钉 ABAQUS 静态压铆 绝热剪切带 Headless rivet ABAQUS Static pressure riveting Adiabatic shear band
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  • 1樊战亭,曹增强,葛剑峰,介苏朋.基于PLC的电磁铆接设备控制系统[J].机床与液压,2005,33(11):108-110. 被引量:9
  • 2葛建峰,曹增强,樊战亭,盛熙.电磁铆接过程数值模拟[J].锻压技术,2005,30(6):62-65. 被引量:3
  • 3曹增强,刘洪.电磁铆接技术[J].塑性工程学报,2007,14(1):120-123. 被引量:30
  • 4庄茁,石亦平.ABAQUS实例详解[M].北京:机械工业出版社,2007(1).
  • 5格里高利耶夫.飞机和直升机部件铆接装配[M].北京:国防工业出版社,1988(9).
  • 6Urban M R.Analysis of the fatigue life of riveted sheet metal helicopter airframe joints.International Journal of Fatigue, 2003(25) : 1013-1026.
  • 7Amerendra Atre,W.S.Johnson.Effect of interference on the mechanics of load transfer in aircraft fuselage lap joint s [J].Journal of Engineering Material and Technology, 2007,129( 7 ) : 356-366.
  • 8费军.自动钻铆技术在波音737尾段项目中的应用[J].航空制造技术,2007,50(9):85-89. 被引量:13
  • 9范玉青.现代飞机制造技术[M]北京:北京航空航天大学出版社,2001.
  • 10王云勃;张关康.飞机装配工艺学[M]北京:国防工业出版社,1990.

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