Please submit manuscripts in either of the following two submission systems

    ScholarOne Manuscripts

  • ScholarOne
  • 勤云稿件系统

  • 登录

Search by Issue

  • 2024 Vol.31
  • 2023 Vol.30
  • 2022 Vol.29
  • 2021 Vol.28
  • 2020 Vol.27
  • 2019 Vol.26
  • 2018 Vol.25
  • 2017 Vol.24
  • 2016 vol.23
  • 2015 vol.22
  • 2014 vol.21
  • 2013 vol.20
  • 2012 vol.19
  • 2011 vol.18
  • 2010 vol.17
  • 2009 vol.16
  • No.1
  • No.2

Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

期刊网站二维码
微信公众号二维码
Related citation:YE Xue-rong,LIANG Hui-min,ZhaiGuoFu.Optimization design method of contact bounce and breakaway initial velocity for aerospace electromagnetic relay[J].Journal of Harbin Institute Of Technology(New Series),2011,18(5):130-136.DOI:10.11916/j.issn.1005-9113.2011.05.023.
【Print】   【HTML】   【PDF download】   View/Add Comment  Download reader   Close
←Previous|Next→ Back Issue    Advanced Search
This paper has been: browsed 938times   downloaded 656times 本文二维码信息
码上扫一扫!
Shared by: Wechat More
Optimization design method of contact bounce and breakaway initial velocity for aerospace electromagnetic relay
Author NameAffiliation
YE Xue-rong School of Electrical Engineering and Automation,Harbin Institute of Technology,Harbin 150001,China 
LIANG Hui-min School of Electrical Engineering and Automation,Harbin Institute of Technology,Harbin 150001,China 
ZhaiGuoFu School of Electrical Engineering and Automation,Harbin Institute of Technology,Harbin 150001,China 
Abstract:
Aerospace electromagnetic relay is an electric component that has been widely used in aerospace industry.Contact bounce and contact breakaway for initial velocity are the key parameters that have strong influence on reliability and electric life of the relay.Generally,it is difficult to optimize these two parameters simultaneously.In this paper,according to kinetics theory and structural mechanics,a dynamic reaction calculation model of the relay that describes contact bounce and breakaway for initial velocity is proposed.Under the constraints of contact gap and contact force,the optimal combination of debugging parameters is obtained by the application of orthogonal design.It considers the reduction of contact bounce and the augmentation of breakaway for initial velocity as the optimization objectives,and takes the debugging parameters as the optimization variables.All these above ensure the increase of contact breakaway for initial velocity and the decrease of contact bounce simultaneously,and contact arc erosion is also reduced.
Key words:  aerospace electromagnetic relay  debugging parameters  contact bounce  contact breakaway initial velocity  orthogonal design
DOI:10.11916/j.issn.1005-9113.2011.05.023
Clc Number:V442
Fund:

LINKS