Abstract
A dual-rotor system is a core component of an aero-engine, and it is very important to study the nonlinear vibrational characteristics for the aero-engine’s development. Based on analyzing structural characteristics of aero-engine’s rotors, a novel and more practical dual-rotor dynamic coupling model with nonlinear restoring forces of high-pressure and low-pressure rotors is first proposed. In the linear dynamic coupling model, the coupling critical speed, natural frequencies and vibration responses of the low-pressure rotor are analyzed systematically. In the nonlinear dynamic coupling model, the vibrational characteristics of the dual-rotor system with different nonlinear parameters are simulated numerically based on the nonlinear dynamic theory. The improved shooting method combined the harmonic balance method, and the genetic algorithm is proposed to calculate theoretical solutions of the nonlinear dynamic coupling model. The stability of theoretical solutions is investigated by the Floquet theory. The research results show that the dual-rotor system appears very complicated nonlinear vibrations such as nonlinear multitudinal solutions, double period motions, almost periodic motions and chaotic motions. The transition between nonlinear vibrations occurs suddenly.
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Abbreviations
- xi, yi :
-
Displacement in x and y directions
- r i :
-
Radial deflection of the rotor
- θx, θy :
-
Inclination of the low-pressure rotor in x and y directions
- θ, θ1 :
-
Inclination angle of the shaft at the position of the disk, Euler angle representing an inclination of the Z1-axis
- m i :
-
Mass of the dual rotor
- ei, τ :
-
Eccentricity of the dual rotor, skew angle of the low-pressure rotor
- I, Ip :
-
Moment of inertia of the low-pressure shaft, polar moment of inertia of the low-pressure disk
- c11, c12, c21, c22, c :
-
Damping coefficients of the dual rotor
- α, γ, δ, k :
-
Stiffness coefficients of the dual rotor
- β τ :
-
Inclination initial value of the low-pressure rotor
- ωi, ωLj, ωH, ω :
-
Rotating speed of the dual rotor, major critical speed of the low-pressure rotor, major critical speed of the high-pressure rotor, excitation rotational speed
- PLx, PLy, PL, Pθ, PH :
-
Amplitudes of the low-pressure rotor in x and y directions, amplitudes of deflection and amplitude of inclination of the low pressure, amplitude of the high-pressure rotor
- M-XYZ, M-X1Y1Z1, M-X0Y0Z0,:
-
Translating coordinate system and rotating coordinate systems [when i = 1 (2), it is parameters of the low (high) pressure rotor]
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Acknowledgments
This work was supported by the National Key Research and Development Program of China (Grant No. 2017YFB1303304) and the Tianjin Natural Science Foundation of China (Grant No.17JCZDJC38500).
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Liu, J., Wang, C. & Luo, Z. Research nonlinear vibrations of a dual-rotor system with nonlinear restoring forces. J Braz. Soc. Mech. Sci. Eng. 42, 461 (2020). https://doi.org/10.1007/s40430-020-02541-w
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DOI: https://doi.org/10.1007/s40430-020-02541-w