基于ADAMS的航天继电器多余物检测试验条件研究
详细信息    查看全文 | 推荐本文 |
  • 英文篇名:Research of Space Relay Remainders-Detection Technique Based on ADAMS
  • 作者:王国涛 ; 王思易 ; 梁安生 ; 翟国富 ; 王洪元
  • 英文作者:WANG Guotao1,WANG Siyi1,LIANG Ansheng1,2,ZHAI Guofu1,WANG Hongyuan3(1.Military Apparatus Research Institute,Harbin Institute of Technology,Harbin 150001,China; 2.The Communication Training Base of the General Staff of PLA,Zhangjiakou 075100,China; 3.No.513 Institute of China Aerospace and Technology Corporation,Yantai 264000,China)
  • 关键词:航天继电器 ; 多余物 ; ADAMS ; 随机振动
  • 英文关键词:space relay;reminders;ADAMS;random vibration
  • 中文刊名:DYDQ
  • 英文刊名:Low Voltage Apparatus
  • 机构:哈尔滨工业大学军用电器研究所;中国人民解放军总参谋部通信训练基地;中国航天科技集团513所;
  • 出版日期:2013-02-15
  • 出版单位:低压电器
  • 年:2013
  • 期:No.420
  • 基金:国家自然科学基金项目(51077022,61271347)
  • 语种:中文;
  • 页:DYDQ201303004
  • 页数:7
  • CN:03
  • ISSN:31-1419/TM
  • 分类号:16-21+59
摘要
提出了基于ADAMS仿真分析的航天继电器多余物检测试验条件研究方法。通过建立航天继电器内部多余物的运动模型,定义模型各组件间的接触关系,仿真分析了多余物在外加正弦和随机激励下的运动过程,并根据仿真结果研究多余物检测的试验条件。试验结果表明,这种研究方法可以较为准确地仿真分析航天继电器内部多余物在外加激励下的运动过程,是一种简便、直观的微粒碰撞噪声检测(PIND)试验条件研究方法。
        The kinetics model of remainders within space relays was built,and contact relationships of each part were defined.The dynamic simulation under both random and sinusoidal vibration conditions was accomplished based on ADAMS to explore the test conditions of particle impact noise detection(PIND).The experiment results show that this method not only simulates the movement of remainders after excitation in space relays exactly,but also is a more convenient,visualized method to study the test conditions of PIND.
引文
[1]DING M S,WANG G,LI X H.Reliability analysisof digital relay[C]∥8th IEE InternationalConference on Developments in Power SystemProtection,The Netherlands,2004(1):268-271.
    [2]PHIL R.Testing techniques to improve relayreliability[J].EE:Evaluation Engineering,2005,44(4):44-48.
    [3]郑南昌.控制系统继电器可靠性分析与措施[J].火箭推进,2005,31(4):58-62.
    [4]HAMMERSTROM I,KUHN M,WITTNEBEN A.Channel adaptive scheduling for cooperative relaynetworks[C]∥2004 IEEE 60th VehicularTechnology Conference,2004,60(4):2784-2788.
    [5]李大南.航天型号产品多余物及其预防和控制标准的实施检查[J].航天标准化,2006(1):17-20.
    [6]DAVID R F S.Practical limitations of PIND testing[C]∥Proceedings of the 28th ElectronicsComponents Conference.1978(10):281-285.
    [7]MCCULLOUGH R.Hermeticity and particle impactnoise test techniques[C]∥14th Annual Proceedingsof Reliability Physics.1996(8):256-262.
    [8]杜迎,吕栋,潘伟力,等.粒子碰撞噪声检测(PIND)试验的研究[J].电子产品可靠性与环境试验,2005(1):34-39.
    [9]ZHANG H,WANG S J,ZHAI G F.Dynamic modelof particle impact noise detection[C]∥IEEEIECON,2004:2577-2581.
    [10]ZHANG H,WANG S J,ZHAI G F.Test conditionsdiscussion of particle impact noise detection for spacerelay[C]∥IEEE IECON,2004:2566-2572.
    [11]张辉,王淑娟,翟国富.航天继电器多余物微粒碰撞噪声检测的单周期稳定性分析[J].航空学报,2005:26(3):362-366.
    [12]郭卫东.虚拟样机技术与ADAMS应用实例教程[M].北京:北京航空航天大学出版社,2008.
    [13]SU X P,ZHANG N,ZHANG S,et al.Designmethod of shading coil in electromagnetic mechanismof AC contactor based on FEA[C]∥InternationalConference on Electrical Machines and Systems,2008:201-204.

© 2004-2018 中国地质图书馆版权所有 京ICP备05064691号 京公网安备11010802017129号

地址:北京市海淀区学院路29号 邮编:100083

电话:办公室:(+86 10)66554848;文献借阅、咨询服务、科技查新:66554700