关键字
协会热线:029-84276641
            首页微电机期刊
 
  综述
  伺服与控制
  设计与研究
  专题讲座
  检测技术
  工艺技术
  经验交流
  实用技术
  读者园地
  技术交流
  使用与维护
  标准评述
  工艺与装备
  驱动与控制
  应用研究
  测试研究
  精品连载
 
标题:电磁解锁器设计与仿真分析
作者:徐岩,窦满峰,张晨
2018年第2期  访问次数:231次

摘要:为了满足卫星系统中机械连接的性能需求,提出一种可以保证系统间可靠分离和锁紧的电磁解锁器。利用电磁系统磁路计算原理设计尺寸为54 mm×50 mm×50 mm的电磁解锁器,介绍了结构及工作原理,通过仿真分析了锥角角度、端盖厚度、静铁心长度以及隔磁衬筒长度对其行程-力特性的影响,最终依据理论结果研制了试验样机,试验验证了其锁紧与解锁性能。结果表明:在尺寸条件限制情况下,该机构在温度变化范围为-55℃~175℃,行程为65mm时,初始机械分离力均在15N以上,输入功率小于230W,可有效实现分离与锁紧功能。
关键词:电磁解锁器;锥形铁心;行程-力特性
Abstract: It is necessary to develop a locking and unlocking device for the satellite systems. In this paper, an electromagnetic locking and unlocking device with a dimension of 54 mm×50 mm×50 mm was designed through the principles of magnetic circuit, the structure and working principles were described. Then, the force-displacement characteristic was researched based on magnet simulation software through the analysis of cover plate, conical angle, and magnetic separator. The locking and unlocking performances were tested in the end. Based on the condition of limited size, it shows that the electromagnetic unlocking device can obtain the min initial separation force of 15 N and the input power is less than 230W within the stroke of 65 mm with temperature range of -55℃~175℃,which satisfied the design requirements.
Key words: electromagnetic unlocking device; conical armature; displacementforce characteristics
 
 
 
    广告服务 |   商务合作 |   使用帮助 |   网站地图 |     主办:中国电器工业协会微电机分会      挂靠:西安微电机研究所有限公司      地址:西安市高新区上林苑四路36号(710117)
   copyright © www.china-micromotor.com.cn all rights reserved.     版权所有:微电机网     陕ICP备05005551号-2
 

西安微电机研究所有限公司公众平台
二维码

《微电机》杂志公众平台二维码