Volume 40 Issue 2
Feb.  2025
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MO Shuai, TANG Xu, CHEN Keren, et al. Nonlinear dynamics of aircraft blended face gear split transmission system[J]. Journal of Aerospace Power, 2025, 40(2):20230265 doi: 10.13224/j.cnki.jasp.20230265
Citation: MO Shuai, TANG Xu, CHEN Keren, et al. Nonlinear dynamics of aircraft blended face gear split transmission system[J]. Journal of Aerospace Power, 2025, 40(2):20230265 doi: 10.13224/j.cnki.jasp.20230265

Nonlinear dynamics of aircraft blended face gear split transmission system

doi: 10.13224/j.cnki.jasp.20230265
  • Received Date: 2023-04-21
    Available Online: 2024-10-01
  • On the premise of considering many factors, such as support stiffness, time-varying meshing stiffness, tooth backlash, comprehensive transmission error, bearing stiffness, etc, the nonlinear dynamic model of blended face gear split transmission system was established. The nonlinear dynamic characteristics of mixed face gear split transmission system were studied. The differential dynamic equation of the system was solved by Runge-Kutta integral method. The nonlinear characteristics of the system were described by phase plane diagram, time domain diagram, frequency domain diagram and Poincare section wavelet analysis diagram, and the bifurcation diagram was used to describe the influences of external excitation frequency and stiffness on the nonlinear behavior of the system. The results showed that under the action of different external excitation and meshing stiffness, the system could present periodic-chaotic alternating motion characteristics.

     

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