期刊文献+

拉索式电涡流阻尼器力学模型及性能试验研究 被引量:2

Theoretical Model and Performance Tests of Rotational Eddy Current Dampers with Cable
下载PDF
导出
摘要 提出一种新型的拉索式旋转电涡流减震系统,该系统由惯容器、弹簧和阻尼单元组成.为验证该减震系统的减震机理,建立了装配阻尼器的单层框架力学模型,分别进行了单层框架、导体盘为5 mm铜板、10 mm铜板、5 mm铁板、5 mm铜板与5 mm铁板复合时的惯容器和不同材质的导体盘在10、20、30、40 mm气隙下带电涡流阻尼器的振动测试,以分析导体盘与永磁体间的气隙大小、导体盘材质和导体盘厚度对阻尼器附加阻尼比的影响.试验结果表明:在铜板后附加铁板,阻尼增加至铜板的1.9倍、铁板的1.4倍,可最大化增加阻尼;气隙是影响电涡流阻尼的关键因素,当气隙增大时,阻尼比会迅速减小,调节气隙大小是改变结构附加阻尼比最有效和最容易的方法;阻尼器提供的阻尼比最大可达15.40%,证实了该阻尼器具有较强的耗能能力. A novel rotational eddy current damper with cable is proposed,which is composed of inerter,spring and damping elements. In order to validate the mechanism for vibration mitigation, a mechanical model of a single-layer frame equipped with the damper is built. A series of vibration tests are carried out in terms of the frame,inerter and eddy current damper to analyze the impacts of air gap dimension between the conductor plate and permanent magnet, the material and thickness of the conductor plate on additional damping ratio. The conductor plates used in the tests include copper plates with the thickness of 5 mm or 10 mm,iron plate with the thickness of 5 mm,and a composite plate made up of a 5 mm thick copper plate and a 5 mm thick iron plate. In the vibration test,the conductor plates of different materials work in the air gaps of 10 mm,20 mm,30 mm,40 mm.The test results show that the iron plate is added after the copper plate, and the damping is increased to 1.9 times and 1.4 times when the copper plate and iron plate are used alone. The air gap is a critical factor affecting the eddy current damping. When the air gap increases,the damping ratio will decrease rapidly. Adjusting the air gap dimension is the most effective and easiest method to change the damping ratio. The maximum damping ratio provided by the damper is 15.40%,which proves that it has a strong energy dissipation ability.
作者 薛松涛 班鑫磊 谢丽宇 余必龙 XUE Songtao;BAN Xinlei;XIE Liyu;YU Bilong(College of Civil Engineering,Tongji University,Shanghai 200092,China;Department of Architecture,Tohoku Institute of Technology,Sendai 982-8577,Japan;CCCC-FHDI Engineering Co.Ltd.,Guangzhou 510000,China)
出处 《西南交通大学学报》 EI CSCD 北大核心 2020年第2期317-322,共6页 Journal of Southwest Jiaotong University
基金 国家自然科学基金(51478356,51778490) 政府间国际科技创新合作重点专项(2016YFE0127600)。
关键词 惯容器 电涡流阻尼器 阻尼比 自由振动试验 inerter eddy current damper damping ratio free vibration test
  • 相关文献

参考文献5

二级参考文献42

  • 1丁幼亮,耿方方,葛文浩,宋建永,李万恒,王玉倩.多塔斜拉桥风致抖振响应的粘滞阻尼器控制研究[J].工程力学,2015,32(4):130-137. 被引量:24
  • 2吕西林,孟春光,田野.消能减震高层方钢管混凝土框架结构振动台试验研究和弹塑性时程分析[J].地震工程与工程振动,2006,26(4):231-238. 被引量:12
  • 3李杰,艾晓秋.基于物理的随机地震动模型研究[J].地震工程与工程振动,2006,26(5):21-26. 被引量:56
  • 4SODANO H A, BAE J S. Eddy current damping in structures[J]. The Shock and Vibration Digest, 2004, 36(6): 469-478.
  • 5GUNTER E J, HUMPHRIS R R, SEVERSON S J. Design study of magnetic eddy-current vibration suppression dampers for application to cryogenic turbomachinery[R]. NASA, 1983, CR-173273: 1-6.
  • 6CUNNINGHAM R E. Preliminary results on passive eddy-current damper technology for SSME turbomachinery[R]. NASA, 1984, CP-2372: 366-380.
  • 7DIRUSSO E, BROWN G V. Experimental evaluation of a tuned electromagnetic damper for vibration control of cryogenic turbopump rotors [R]. NASA, 1990, TP-3005.
  • 8NIKOLAJSEN J L. A magnetic bearing based on eddy-current repulsion[C]//Proceedings of Rotordynamic Instability Problems in High-performance Turbomachinery, 1986, NASA CP-2443: 461-466.
  • 9NIKOLAJSEN J L. Experimental verification of an eddy-current bearing[C]//Proceedings of Rotordynamic Instability Problems in Highperformance Turbomachinery, 1988, NASA, CP-3026: 389-393.
  • 10CONNOR K A, TICHY J A. Analysis of an eddy current journal bearing[J]. Journal of Tribology, 1988, 110: 320-326.

共引文献34

同被引文献24

引证文献2

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部