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Bifurcation and chaos of the bladed overhang rotor system with squeeze film dampers 被引量:5

Bifurcation and chaos of the bladed overhang rotor system with squeeze film dampers
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摘要 To study the nonlinear dynamic behavior of the bladed overhang rotor system with squeeze film damper (SFD), a blade-overhang rotor-SFD model is formulated using the lumped mass method and the Lagrange approach. The cavitated short bearing model is employed to describe the nonlinear oil force of the SFD. To reduce the scale of the nonlinear coupling system, a set of orthogonal transformations is employed to decouple the one nodal diameter equations of blades, which are coupled with the dy- namical equations of the rotor, with other equations of blades. In this way, the original system with 16+4n (n≥3) degrees of freedom (DoF) is reduced to a system with 24 DoF only. Then the parametric excitation terms in the blade-overhang rotor-SFD model are simplified in terms of periodic transforma- tions. The coupling equations are numerically solved and the solutions are used to analyze the dy- namic behavior of the system in terms of the bifurcation diagram, whirl orbit, Poincaré map and spec- trum plot. A variety of motion types are found such as multi-periodic, quasi-periodic, and chaotic mo- tions. Moreover, the typical nonlinear dynamic evolutions including the periodic-doubling bifurcation and reverse bifurcation are noted. It is noticed that there exist apparent differences in the dynamic behavior between the blade-overhang rotor-SFD models without and with considering the effect of blades. To study the nonlinear dynamic behavior of the bladed overhang rotor system with squeeze film damper (SFD), a blade-overhang rotor-SFD model is formulated using the lumped mass method and the Lagrange approach. The cavitated short bearing model is employed to describe the nonlinear oil force of the SFD. To reduce the scale of the nonlinear coupling system, a set of orthogonal transformations is employed to decouple the one nodal diameter equations of blades, which are coupled with the dynamical equations of the rotor, with other equations of blades. In this way, the original system with 16+4n (n≥3) degrees of freedom (DoF) is reduced to a system with 24 DoF only. Then the parametric excitation terms in the blade-overhang rotor-SFD model are simplified in terms of periodic transformations. The coupling equations are numerically solved and the solutions are used to analyze the dynamic behavior of the system in terms of the bifurcation diagram, whirl orbit, Poincaré map and spectrum plot. A variety of motion types are found such as multi-periodic, quasi-periodic, and chaotic motions. Moreover, the typical nonlinear dynamic evolutions including the periodic-doubling bifurcation and reverse bifurcation are noted. It is noticed that there exist apparent differences in the dynamic behavior between the blade-overhang rotor-SFD models without and with considering the effect of blades.
机构地区 School of Astronautics
出处 《Science China(Technological Sciences)》 SCIE EI CAS 2009年第3期709-720,共12页 中国科学(技术科学英文版)
基金 Supported by the National Natural Science Foundation of China (Grant No. 10632040) the Natural Science Foundation of Hei-Long-Jiang Province of China (Grant No. ZJG0704) the Harbin Science & Technology Innovative Foundation of China (Grant No. 2007RFLXG009)
关键词 bladed OVERHANG rotor system SQUEEZE film DAMPER BIFURCATION chaos bladed overhang rotor system squeeze film damper bifurcation chaos
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  • 1GENTA G. Vibration of structures and machines:3^rd Edition[M]. New York: Springer, 1998.
  • 2CHUN S B, LEE C W. Vibration analysis of shaft-bladed disc system by using substructure synthesis and assumed modes method[J]. Journal of Sound and Vibration, 1996, 189: 587-608.
  • 3CRAWLEY E F, MOKADAM D R. Stagger angle dependence of inertial and elastic coupling in bladed discs[J]. Journal of Vibration, Acoustics, Stress and Reliability in Design, 1984, 106: 181-188.
  • 4ADILETTA G, GUIDO A R. Chaotic motions of a rigid rotor in short journal bearings[J]. Nonlinear Dynamics,1996, 10: 251-269.
  • 5GENTA G. On the stability of rotating blade arrays[J].Journal of Sound and Vibration, 2003, 273: 805-836.
  • 6黄文虎,武新华,焦映厚,夏松波,陈照波.非线性转子动力学研究综述[J].振动工程学报,2000,13(4):497-509. 被引量:55

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