Home
Editorial Committee
Brief Instruction
Back Issues
Instruction to Authors
Submission on line
Contact Us
Chinese

  The journal resolutely  resists all academic misconduct, once found, the paper will be withdrawn immediately.

Title:Experimental study on equal channel angular pressing and cold upsetting composite forming for 6063 aluminum alloy aviation rivets
Authors: Li Shiqian  He Tao  Huo Yuanming  Yao Tingting  Jia Dongsheng  Li Hanlin 
Unit: Shanghai University of Engineering Science 
KeyWords: 6063 aluminum alloy  equal channel angular pressing(ECAP)  cold upsetting  mechanical property  rivet failure 
ClassificationCode:TG146.21
year,vol(issue):pagenumber:2022,47(8):138-145
Abstract:

 In order to explore the mechanical properties and failure forms of aluminum alloy aviation rivets formed by equal channel angular pressing(ECAP)and cold upsetting(CU) composite forming, for 6063 aluminum alloy aviation rivets, the ECAP-CU composite forming experiments and different types of failure experiments were carried out, and the fracture morphology of formed rivets was observed by SEM. The results show that compared with the rivet formed by single cold upsetting, the maximum tensile load of the rivet by the composite forming is increased by about 14.2% in pure tension, the failure form is pull-off failure of head, the number of holes in the micro-fracture is significantly reduced, and the dimples become shallow. However, in pure shear, the maximum shear load of the rivet by the composite forming is increased by about 15.2%, the failure form is the shear failure of rod along the shearing direction, and the shear dimples on the fracture surface become larger and shallower. When composite loading, the maximum load of the rivet by the composite forming is increased by about 45.6%, the failure form is shear fracture in which the rod is bent with a certain angle, and more shear dimples appear on the fracture surface.

Funds:
上海市自然科学基金资助项目(20ZR1422100);国家重点研发项目(2018YFB1307900);上海市人才发展资金资助项目(2019022)
AuthorIntro:
作者简介:李诗谦(1996-),男,硕士研究生,E-mail:worklishiqian@163.com;通信作者:何涛(1979-),男,博士,教授,E-mail:hetao@sues.edu.cn
Reference:

 [1]王肇宇. 国际航空航天紧固件发展现状及趋势研究[J]. 宇航总体技术, 2018,2(4):1-7.


Wang Z Y. The study of international aerospace fastener status and development trend[J]. Astronautical Systems Engineering Technology, 2018,2(4):1-7.


[2]曹增强. 应对我国大飞机研制的装配连接技术[J]. 航空制造技术, 2009,10(2): 88-91.


Cao Z Q. Assembly connecting technology for the research of China large aircraft[J]. Aeronautical Manufacturing Technology, 2009,10(2): 88-91.


[3]Jin Z, Mallick P K. Effect of cold work on the tensile and fatigue performance of aluminum alloy 5754[J]. Journal of Materials Engineering & Performance, 2006,15(5):540-548.


[4]董义兵, 刘涛, 刘利江. 航空铝合金及其材料加工[J]. 中国高新科技, 2018,11(3): 52-54.


Dong Y B, Liu T, Liu L J. Aviation aluminum alloy and material processing[J]. China High-Tech, 2018,11(3): 52-54.


[5]杨守杰, 戴圣龙. 航空铝合金的发展回顾与展望[J]. 材料导报, 2005,19(2): 76-80.


Yang S J, Dai S L. A glimpse at the development and application of aluminum alloys in aviation industry[J]. Materials Review, 2005,19(2): 76-80.


[6]Huang Y Y, Hu Z L, Wang J J. Research progress on the aluminum alloy with high thermal conductivity[J]. Applied Mechanics and Materials, 2014,32(10): 396-400.


[7]冯晓旻,谢兰生. 铆接变形的有限元分析[J]. 机械制造与自动化, 2009,38(2): 62-63.


Feng X M, Xie L S. Rivet deformation and finite element analysis[J]. Machine Building & Automation, 2009,38(2): 62-63.


[8]刘全明,张朝晖,刘世锋,等. 航空紧固件用钛合金TC16研究与发展[J]. 热加工工艺,201443(4):17-19.


Liu Q M, Zhang C H, Liu S F, et al. Research and development of aerospace fasteners made with TC16 alloy[J]. Hot Working Technology, 201443(4):17-19.


[9]许晓静, 张允康, 邓平安, . 预回复退火对7085铝合金挤压材组织和性能的影响[J]. 材料热处理学报, 2014,35(8): 36-40.


Xu X J, Zhang K Y, Deng P A, et al. Effect of pre-recovery-annealing treatment on microstructure and properties of extruded 7085 aluminum alloy[J]. Transactions of Materials and Heat Treatment, 2014,35(8): 36-40.


[10]Salvo J G J D, Afonso C R M. Fatigue strength and microstructure evaluation of Al 7050 alloy wires recycled by spray forming, extrusion and rotary swaging[J]. Transactions of Nonferrous Metals Society of China, 2020, 30(12): 3195-3209.


[11]Monika Karoń, Marcin Adamiak. Characterization of microstructure and mechanical properties of 6060 aluminum alloy processed by ECAP[J]. Solid State Phenomena, 2018,275(5):81-88.


[12]Gu Y X, Ma A B, Jiang J H, et al. Research progress of ultrafine-grained pure titanium produced by equal-channel angular pressing[J]. Rare Metal Materials & Engineering,2017,47(12):3639-3644.


[13]张忠明, 王锦程, 唐文亭, . 等通道转角挤压(ECAP)工艺的研究现状[J]. 铸造技术, 2004,25(1):10-12.


Zhang Z M, Wang J C, Tang W T, et al. Status of equal channel angular pressing(ECAP)[J], Foundry Technology, 2004,25(1):10-12.


[14]Zhao Y H, Liao X Z, Jin Z, et al. Microstructures and mechanical properties of ultrafine grained 7075 Al alloy processed by ECAP and their evolutions during annealing[J]. Acta Materialia, 2004, 52(15):4589-4599.


[15]Kim W J, Sa Y K, Kim H K, et al. Plastic forming of the equal-channel angular pressing processed 6061 aluminum alloy[J]. Materials Science and Engineering: A,2008, 10(69): 360-368.


[16]杨沛, 郭亚洲, 李玉龙. 航空铆钉的动态力学性能测试[J]. 航空学报, 2014,35(11):3012-3024.


Yang P, Guo Y Z, Li Y L. Dynamic mechanical test of aeronautic rivets[J]. Acta Aeronautica et Astronautica Sinica, 2014,35(11):3012-3024.


[17]汪存显, 高豪迈, 龚煦, . 航空铆钉连接件的抗冲击性能[J]. 航空学报, 2019,40(1):289-301.


Wang C X, Gao H M, Gong X, et al. Impact responses of aeronautic riveting structures[J]. Acta Aeronautica et Astronautica Sinica, 2019,40(1):289-301.


[18]解江, 白春玉, 舒挽, . 航空铆钉动态加载失效实验[J]. 爆炸与冲击, 2017, 37(5):879-886.


Xie J, Bai C Y, Shu W, et al. Dynamic loading failure experiment of aeronautic rivet[J]. Explosion and Shock Waves, 2017, 37(5):879-886.

Service:
This site has not yet opened Download Service】【Add Favorite
Copyright Forging & Stamping Technology.All rights reserved
 Sponsored by: Beijing Research Institute of Mechanical and Electrical Technology; Society for Technology of Plasticity, CMES
Tel: +86-010-62920652 +86-010-82415085     Fax:+86-010-62920652
Address: No.18 Xueqing Road, Beijing 100083, P. R. China
 E-mail: fst@263.net    dyjsgg@163.com