Modified oil film force model for investigating motion characteristics of rotor-bearing system

被引:3
作者
He, Hong-jun [1 ]
Jing, Jianping [1 ]
机构
[1] Shanghai Jiao Tong Univ, State Key Lab Mech Syst & Vibrat, Shanghai 200240, Peoples R China
基金
中国国家自然科学基金;
关键词
Dynamic characteristic; motion; nonlinear force model; rotor; vibration;
D O I
10.1177/1077546314532118
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
The oil film force induced from bearings has a direct influence on the stable operation of a rotor system because the change in motion characteristics will lead to variation of the oil film force. An accurate oil film force model is therefore critical to predict the motion characteristic state of a rotor system. The linear oil film force model and the Muszynska model are employed by many scholars to predict linear force and nonlinear oil film force respectively. When the rotor system has a larger eccentricity ratio, the changing law of the rotor system is not predicted by the Muszynska model. In this paper an improved oil film force model is developed for the motion changing law. This model is based on short bearing assumption with the turbulence effect and rotor motion equation included. The motion law is well described by this model. In particular the dynamic characteristics can be described well by the modified model. To verify the simulation results of the modified model, an experiment is carried out. Finally, there is a comparison between theoretical and experimental results and it is found that the theoretical results are in good agreement with the experimental results. This paper provides a reference for further research of the motion changing law of rotor systems.
引用
收藏
页码:756 / 768
页数:13
相关论文
共 21 条
  • [1] Aerodynamic-rotordynamic interaction in axial compression systems - Part II: Impact of interaction on overall system stability
    Al-Nahwi, AA
    Paduano, JD
    Nayfeh, SA
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2003, 125 (03): : 416 - 424
  • [2] [Anonymous], 1986, La Mecc. Ital.
  • [3] CAPONE G, 1991, ENERG ELETTR, V3, P105
  • [4] Cheng M, 2006, ARCH APPL MECH, V76, P215, DOI 10.1007/S00419-006-0017-9
  • [5] Childs D. W., 1987, P ASME 11 BIENN C ME, V2, P427
  • [6] Ding Q, 2002, J SOUND VIBRATION, V252, P17
  • [7] Rotordynamic coefficients in stepped labyrinth seals
    Eser, D
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2002, 191 (29-30) : 3127 - 3135
  • [8] AIR-FLOW IN CAVITIES OF LABYRINTH SEALS
    ESER, D
    KAZAKIA, JY
    [J]. INTERNATIONAL JOURNAL OF ENGINEERING SCIENCE, 1995, 33 (15) : 2309 - 2326
  • [9] Numerical analysis of nonlinear rotor-seal system
    Hua, J
    Swaddiwudhipong, S
    Liu, ZS
    Xu, QY
    [J]. JOURNAL OF SOUND AND VIBRATION, 2005, 283 (3-5) : 525 - 542
  • [10] Iwatsubo T., 1980, 1 WORKSH ROT DYN INS, P139