期刊文献+

基于有限元的转子动力学建模仿真与不平衡响应分析 被引量:5

Dynamic simulation and unbalance response analysis of the rotor based on finite element method
下载PDF
导出
摘要 为了快速确定转子试验器不平衡测点位置,完成转子系统动平衡,借助有限元分析软件建立了地面转子试验器动力学仿真模型,可用于分析转子系统的不平衡响应特性,进而分析出各转速区间内转子各截面不平衡载荷的分布规律。仿真结果表明在一阶临界转速附近,转子前端的不平衡响应较大,在二阶临界转速附近转子后端的不平衡响应较大。最终,动平衡试验结果表明在一阶临界转速内转子前轴承截面对风扇盘不平衡量的变化较为敏感,而后轴承截面无法有效地反映出不平衡量的变化,证明了所采用的转子动力学仿真分析方法的有效性。 In order to rapidly determine the unbalance point of the rotor tester,and to reach dynamic balance of the rotor system,we established the dynamic simulation model of the rotor tester by using finite element analysis software,applied it to analyzing the unbalance response characteristics of the rotor system,and further obtained the distribution rules of the unbalance load of each section of the rotor in each speed range.The simulation results showed that around the first-order critical speed,the unbalance response at the front end of the rotor was bigger;around the second-order critical speed,the unbalance response at the rear end of the rotor was bigger.Dynamic balance test results showed that within the range of the first-order critical speed,the front bearing section of the rotor was most sensitive to the unbalance change of the fan,while the rear bearing section could not reflect the unbalance change.The results have proved the efficiency of the rotor dynamic simulation method.
作者 解梦涛 董江 张强波 XIE Mengtao;DONG Jiang;ZHANG Qiangbo
出处 《现代机械》 2020年第5期70-73,共4页 Modern Machinery
关键词 转子试验器 动平衡 有限元 转子动力学仿真 不平衡响应 rotor tester dynamic balance finite element rotor dynamic simulation unbalance response
  • 相关文献

参考文献3

二级参考文献20

  • 1王四季.发动机转子高速动平衡系统的设计与实现[D].西北工业大学,2005.
  • 2OU Yuanxia, Li Ping. Mode synthesis analysis of vibration of entire engine [J]. Journal of Aerospace Power, 2007, 2(3): 209-214.
  • 3Chiang H W, Hsu C N, Tu S H. Rotor-bearing analysis for turbomachinery single-and dual-rotor systems [ J ]. Journal of Propulsion and Power, 2 0 0 4,2 0 ( 6 ) : 1 096-1 104.
  • 4Sun G, Kaushik N, Palazzolo A, et al. An effective algorithm for blade loss simulations using a high fidelity ball bearing and damper model[A]. American Society of Mechanical Engineering 19th Biennial Conference on Mechanical Vibration and noise[C]. Chicago, USA, September 2003, DETC 2003/VIB 48424.
  • 5Sun G, Palazzolo A. Long duration blade loss simulations including thermal growths dual-rotor gas turbine engine [J]. Journal of Sound and Vibration, 2008, 316 : 147-163.
  • 6Hai P M, Bonello P. An impulsive receptance technique for the time domain computation of the vibration of a whole aero-engine model with nonlinear bearings [J]. Journal of Sound and Vibration, 2008, 318: 592-605.
  • 7Chen G. A new rotor-ball bearing-stator coupling dynamic model for whole aero-engine vibration [J]. Journal of Vibration and Acoustics, 2009, 131 (6): 061009-1-061009-9.
  • 8Chen G, Li C G, Wang D Y. Nonlinear dynamic analysis and experiment verification of rotor-ball bearings- support-stator coupling system for aeroengine with rubbing coupling faults[J]. Journal of Engineering for Gas Turbines and Power, 2010, 132: 022501-1- 022501-9.
  • 9Chen G. Study on nonlinear dynamic response of an unbalanced rotor supported on ball bearing [J]. Jourhal of Vibration and Acoustics, 2009, 131 (6): 061001-1-061001-9.
  • 10Zhai W M. Two simple fast integration methods for large-scale dynamic problems in engineering [J]. International Journal for Numerical Methods in Engineering, 1996, 39(24): 4 199-4 214.

共引文献93

同被引文献55

引证文献5

二级引证文献6

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