An improved rotor model with equivalent dynamic effects of the support structure

被引:18
作者
Choi, BL [1 ]
Park, JM [1 ]
机构
[1] Korea Univ, Dept Mech Engn & Appl Mech, Sungbuk Gu, Seoul, South Korea
关键词
D O I
10.1006/jsvi.2000.3510
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Dynamic effects of the support structure are important in vibration analyses of a rotor. It may well happen in real machines such as centrifugal pumps or turbines operating on a flexible structure. This paper suggests an improved rotor model for including the support effects efficiently into the rotor-bearing system. The support FRFs are used to extract the spring-mass models which have the same dynamic characteristics of the support structure. These regenerated models are directly inserted into the rotor. On the other hand, the impedance coupling method, which is often used in structural vibration problems, is presented to verify the suggested modelling technique. It is based on the FRFs of each substructure and the constraint conditions of interface co-ordinates. To demonstrate the applicability and validity of the analytical procedures, they are applied to the rotor of a double suction centrifugal pump. As a result, they show a good agreement with each other. (C) 2001 Academic Press.
引用
收藏
页码:569 / 581
页数:13
相关论文
共 25 条
  • [1] Buckley AN, 1996, ELEC SOC S, V96, P1
  • [2] DYNAMIC STABILITY OF A CANTILEVER SHAFT-DISK SYSTEM
    CHEN, LW
    KU, DM
    [J]. JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 1992, 114 (03): : 326 - 329
  • [3] OPTIMUM DESIGN OF ROTOR-BEARING SYSTEMS WITH EIGENVALUE CONSTRAINTS
    CHEN, TY
    WANG, BP
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1993, 115 (02): : 256 - 260
  • [4] Ewins D., 1986, MODAL TESTING THEORY
  • [5] FORRAI L, 1996, 96GT407 AM SOC MECH, P1
  • [6] GREENHILL LM, 1995, DES ENG TECHN C DE, V84, P991
  • [7] Harris T.A., 1966, ROLLING BEARING ANAL
  • [8] HONG SW, 1996, J KSNVE, V6, P71
  • [9] VIBRATIONS OF TIMOSHENKO BEAMS BY VARIABLE ORDER FINITE-ELEMENTS
    HOUMAT, A
    [J]. JOURNAL OF SOUND AND VIBRATION, 1995, 187 (05) : 841 - 849
  • [10] JETMUNDSEN B, 1988, J AM HELICOPTER SOC, P55