Volume 32 Issue 5
May  2017
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Detailed deduction and analysis of the general analytical model of coupling vibration in a rotor system[J]. Journal of Aerospace Power, 2017, 32(5): 1112-1119. doi: 10.13224/j.cnki.jasp.2017.05.012
Citation: Detailed deduction and analysis of the general analytical model of coupling vibration in a rotor system[J]. Journal of Aerospace Power, 2017, 32(5): 1112-1119. doi: 10.13224/j.cnki.jasp.2017.05.012

Detailed deduction and analysis of the general analytical model of coupling vibration in a rotor system

doi: 10.13224/j.cnki.jasp.2017.05.012
  • Received Date: 2016-08-25
  • Publish Date: 2017-05-28
  • Based on the mechanism of linear and nonlinear forces on the rotor system, the linear scale factor, nonlinear scale factor and coupling ratio was introduced as characteristic parameters, the general expressions of damping and stiffness forces were established, so a general form of linear and nolinear coupling vibration model was formulated. Considering a single-disc rotor system excited only by mass unbalance force, the steady-state and transient-state solutions were derived through multi-scale method. The analysis on the analytical solutions showed the vibration mechanism of linear and nonlinear coupling effects and responses. The influence of transient time scale factor on responses was analyzed through numerical calculation. When transient time scale factor was larger, the transient-state solution decayed faster, approaching the steady-state solution closer. The amplitude-frequency characteristics were also analyzed by the short time Fourier transform of the steady-state solution. It can be seen that the first harmonic generation has nonlinear characteristics and the third harmonic generation has double-peak characteristics, further elaborating the influences of nonlinear scale factor on the coupling vibration of the rotor system.

     

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