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基于Δ-Υ等效变换的SGCMG高速转子轴向振动特性分析及验证 被引量:4

Axial Vibration Analysis and Validity of High-Speed Rotor of Cantilever SGCMG Based on a Triangle-Star Equivalent Transformation
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摘要 悬臂式单框架控制力矩陀螺(SGCMG)的轴向振动较为剧烈,频率成分也比较复杂;由于这种SGCMG结构是由众多串、并联,甚至桥联的弹性构件组成的,因此难以建立其精确的轴向动力学模型.首先通过Δ-Υ等效变换的方法,简化了高速转子的轴向串并联关系,进而计算出其轴向刚度;其次详细分析了系统激振源——预紧轴承各零部件的加工波纹所导致的预紧力的波动,并采用相互调幅的形式描述了该波动量;然后建立了高速转子的轴向动力学方程;最后通过数值仿真和实测结果的对比验证了分析的合理性和模型的有效性. Cantilever single gimbal control moment gyroscope(SGCMG) excites severe axial vibration which includes some complex frequency components.Because the SGCMG structure consists of many elastic members with series and parallel,even bridging connection,it is very difficult to directly establish its accurate axial dynamics model.Firstly,the axial connection between components of high-speed rotor is simplified by using the method of equivalent transformation between the triangle and the star;thus,the axial stiffness of the rotor is calculated simply.Secondly,the exciting source for high-speed rotor vibration with the form of cross-amplitude modulation was analyzed which derives from preloading bearing processing error.Thirdly,the high-speed axial rotor axial dynamics equations were established.Finally,validity of the model is verified by comparing results of the numerical simulation based on the model and the experimental test for cantilever SGCMG.
出处 《空间控制技术与应用》 2011年第2期14-20,共7页 Aerospace Control and Application
关键词 Δ-Υ等效变换 轴承加工偏差 高速转子 轴向振动 动力学建模 triangle-star equivalent transformation bearing processing error high-speed rotor axial vibration dynamics modeling
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  • 1解永春.磁悬浮动量轮的主动振动控制[J].航天控制,2001,19(2):1-6. 被引量:4
  • 2李兴林.滚动轴承振动噪声及其评价技术[J].轴承,1995(9):42-46. 被引量:19
  • 3李连军,戴金海.反作用轮系统内干扰建模与仿真分析[J].系统仿真学报,2005,17(8):1855-1858. 被引量:20
  • 4Masterson R A, Miller D W, Grogan R L. Development and Validation of Reaction Wheel Disturbance Models: Empirical Model [ J ]. Journal of Sound and Vibration 2002,249 ( 3 ) : 575-598.
  • 5Harris T A. Rolling Bearing Analysis [ M ]. The 3rd John Wiley and Sons, Inc. 1990.
  • 6Kim S M, Lee K J, Lee S K. Effect of Bearing Support Structure on the High-speed Spindle Bearing Compliance [ J ]. International Journal of Machine Tools and Manufacture, 2002, 42(3) : 365-373.
  • 7航空专业教材编审组.飞行器振动基础[M].南京航空学院,1983.
  • 8[2]Harmrock B J, Dowson D. Ball Bearing Lubricantion. John Wiley and Sons. Inc., 1981.
  • 9[3]Harrist A. Rolling Bearing Analysis (Tnird Edition). John Wiley and Sons. Inc., 1991.
  • 10施维新.汽轮发电机组振动及事故[M].北京:中国电力出版社,1998..

共引文献75

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  • 1郑钢铁.空间飞行器隔振与振动抑制研究进展[C].2007第九届全国振动理论及应学术会议论文集2007.
  • 2闻邦椿.高等转子动力学[M].北京:机械工业出版社,1999.23-46.
  • 3Remedia M, Aglietti G S, Zhang Z, et al. Modeling methodologies for microvibration-related analysis of spacecraft structures [ C]. 12th European Conference on Space Structures, Materials and Environmental Testing, Noordwijk, The Netherlands, March 20 - 23, 2012.
  • 4Gerard B, Guillaume O, Laurent S, et al. Virtual SEA method for analyzing micro-vibration of spacecrafts [ C ]. 12th European Conference on Space Structures, Materials and Environmental Testing, Noordwijk, The Netherlands, March 20 - 23, 2012.
  • 5Jules K, Lin P P. Monitoring the microgravity enviromnent quality on-board the international space station using soft computing techniques [ C ]. 52nd International Astronautical Congress, Toulouse, France, Oct 1 -5, 2001.
  • 6Sicker R J, Kacpura T J. Advanced microgravity acceleration measurement systems being developed [ R ]. Cleveland, USA: NASA Glenn Research Center, March 2002.
  • 7Dyne S J, Tunbridge D E, Collins P P. The vibration environment on a satellite in orbit [ C]. High Accuracy Platform Control in Space, IEE Colloquium on IET, London, UK, June 14, 1993.
  • 8HYDE TT, HA K Q, JOHNSTON J D, et al. Integrated modeling activities for the James Webb Space Tele- scope : optical jitter analysis [ C ]//Proceedings of SPIE Vol. 5487. Bellingham, WA: SPIE, 2004: 588-599.
  • 9ELIAS L M, MILLER D W. A coupled disturbance a- nalysis method using dynamic mass measurement tech- niques [ C ]//AIAA-2002--1252, Denver, Co. : 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Dynamics and Materials Conference. Washington DC: AIAA, 2002.
  • 10MASTERSON R A, Miller D W. Development and vali- dation of empirical and analytical reaction wheel disturb- ance models[ D]. Cambridge: Department of Mechani- cal Engineering, Massachusetts Institute of Technology, 1999.

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