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Title:Calculation on effective electromagnetic force for electromagnetic riveting based on equivalent circle method
Authors: Nie Peng1 2 Wang Yong1 2 Li Haiwei3 Li Bobo1 2 
Unit: 1. National Key Laboratory of Aerospace Manufacturing Technology  Shenyang Aerospace University 2. School of Mechanical and Electrical Engineering Shenyang Aerospace University 3. Shenyang Aircraft Industry (Group) Co.  Ltd. 
KeyWords: electromagnetic riveting  equivalent circle method  induced current  effective electromagnetic force discharge voltage  distance between  coils 
ClassificationCode:TG391
year,vol(issue):pagenumber:2021,46(12):141-174
Abstract:

 In the case of ignoring the influence of resistance and energy loss in the air, the electromagnetic riveting discharge coil and driving coil model were simplified by the equivalent circle method to calculate the self-inductance and mutual inductance, and the calculation formula of the induced current and the effective electromagnetic force was derived. Then, the interaction model of the discharge coil and the driving coil was built by finite element software ANSYS Electronics Suite, and the induced current and effective electromagnetic force of the driving coil were analyzed by changing the discharge voltage and the distance between the discharge coil and the drive coil. Furthermore, the distribution law of induced current under this condition was similar to the distribution law of effective electromagnetic force, but the position of the maximum value for the effective electromagnetic force was 18 mm from the center of the drive coil, and the discharge current also reached its maximum value at the same position. In addition, both the decrease of the distance between the two coils and the increase of the discharge voltage increased the effective electromagnetic force. The simulation result was compared with the numerical value obtained by the simplified computation of the equivalent circle method under this condition. The results show that the computation method of the effective electromagnetic force proposed is correct, and the result is reliable.

Funds:
辽宁省自然科学基金资助项目(201602564)
AuthorIntro:
作者简介:聂 鹏(1972-),男,博士,教授,硕士生导师 E-mail:niehit@163.com 通信作者:王 勇(1995-),男,硕士研究生 E-mail:1031715313@qq.com
Reference:

 [1]   田中沙季, 赤堀俊和,新家光雄,. 航空機用Ti5Al2Sn2Zr4Mo4Cr鍛造材のミクロ組織と疲労特性の関係[J]. 日本金属学会誌,2020,61(10):2017-2024.


 


Saki Tanaka, Toshikazu Akahori, Mitsuo Shinie, et al. Relationship between microstructure and fatigue properties of Ti5Al2Sn2Zr4Mo4Cr forged materials for aircraft [J]. Journal of the Japan Institute of Metals, 2020, 61(10):2017-2024.


 


[2]   Palanikumar K. Editorial preface: A special issue on advances in materials, manufacturing and applied sciences[J]. Materials Today: Proceedings,2019.


 


[3]   聂鹏, 李聪,王哲峰,.航空钛合金管件端口电磁校形技术[J].火力与指挥控制,2019,44(2):155-160165.


 


Nie P,Li C,Wang Z F,et al.Electromagnetic calibration technology of aviation titanium alloy pipe fitting port[J].Fire Power and Command Control,2019,44(2):155-160165.


 


[4]   庞桂兵, 张赟阁,赵益昕,.高速率成形技术进展[J].大连工业大学报,2014,33(5):381-386.


 


Pang G B, Zhang Y G, Zhao Y X, et al. Highspeed forming technology progress[J].Journal of Dalian University of Technology,2014,33(5):381-386.


 


[5]   Jiang H, Li G Y, Zhang X, et al . Fatigue and failure mechanism in carbon fiber reinforced plastics/aluminum alloy single lap joint produced by electromagnetic riveting technique[J]. Composites Science and Technology,2017,152(10):1-10.


 


[6]   王呈顺. 在碳纤维复合材料中的电磁铆接技术浅析[J].电子世界,2017155(17):1-89.


 


Wang C S.Analysis of electromagnetic riveting technology in carbon fiber composite materials[J].Electronic World, 2017155(17):1-89.


 


[7]   赵建国, 郭洪杰,董帅.铆钉成形技术研究及性能评价[J].航空制造技术,2015(23):114-116.


 


Zhao J G,Guo H J,Dong S.Research and performance evaluation of rivet forming technology[J].Aviation Manufacturing Technology, 2015(23):114-116.


 


[8]   曹增强, 刘洪.电磁铆接技术[J].塑性工程学报,200714(1):120-123.


 


Cao Z Q,Liu H.Electromagnetic riveting technology[J].Chinese Journal of Plasticity Engineering,200714(1):120-123.


 


[9]   余祥峰. 钛合金铆钉电磁铆接破坏行为研究[D]. 福州:福州大学,2014.


 


Yu X F. Research on Electromagnetic Riveting Failure Behavior of Titanium Alloy Rivets[D]. Fuzhou:Fuzhou University, 2014.


 


[10]Deng J H, Tang C, Zheng Y M, et al. Effect of coil parameters on rivet deformation in low voltage electromagnetic riveting[J]. Advanced Materials Research, 2013, 602-604:1887-1890.


 


[11]焦其祥. 电磁场与电磁波[M].3.北京:科学出版社,2019.


 


Jiao Q X. Electromagnetic Field and Electromagnetic Wave[M]. The 3rd Edition. Beijing: Science Press, 2019.


 


[12]尹真. 电动力学[M].3.北京:科学出版社,2010.


 


Yin Z. Electrodynamics[M]. The 3rd Edition. Beijing: Science Press, 2010.


 


[13]杨桂通. 弹性力学[M].3.北京:高等教育出版社,2018.


 


Yang G T. Elasticity[M]. The 3rd Edition. Beijing: Higher Education Press, 2018.


 


[14]尚福林. 塑性力学基础[M].西安:西安交通大学出版社,2015.


 


Shang F L. Fundamentals of Plastic Mechanics[M]. Xi'an: Xi'an Jiaotong University Press, 2015.


 


[15]Deng J H, Tang C, Fu M W, et al. Effect of discharge voltage on the deformation of Ti Grade 1 rivet in electromagnetic riveting[J]. Materials Science & Engineering A,2014, 591:26-32.


 


[16]聂鹏, 冯志超,王哲峰.大型钛合金筒形件电磁冲模校圆研究[J].现代制造工程,201914(8):82-86.


 


Nie P,Feng Z C,Wang Z F.Study on the rounding of electromagnetic punching die for large titanium alloy cylindrical parts[J].Modern Manufacturing Engineering,201914(8):82-86.

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