Effects of Surface Waviness of Intershaft Bearing on Dynamic Characteristics of Dual Rotor System
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摘要: 针对航空发动机双转子系统,根据转子动力学理论和拉格朗日方程建立中介轴承-双转子系统模型,采用数值仿真方法获得系统动力学特性,借助时变刚度曲线、幅频响应曲线、三维瀑布图、分岔图以及庞加莱截面图等,对比分析了理想中介轴承-双转子系统和考虑波纹度的中介轴承-双转子系统的时变刚度特性、中介轴承力、主共振、频谱特征以及分岔与混沌特性。结果表明,中介轴承波纹度使双转子系统运动状态更加复杂,尤其在较低转速下,波纹度会对双转子系统的动力学特性产生显著影响。Abstract: This work established a dynamic model of intershaft bearing-dual rotors in aero-engine with the theory of rotor dynamics and Lagrange equation. The vibration characteristics were examined by numerical simulation. With the time-varying stiffness curve, amplitude-frequency curve, three-dimensional waterfall plot, bifurcation diagram, Poincare map and so on, the time-varying stiffness characteristic, intershaft bearing force, primary resonance, spectrum characteristic, bifurcation and chaos characteristics of the ideal intershaft bearing-dual rotor system and the system with surface waviness on the intershaft bearing are analyzed comparatively. The results show that the surface waviness of the intershaft bearing complicated the vibration condition of the dual rotor system. The surface waviness has significant influence on the dual rotor system, especially at the lower speed.
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表 1 系统计算参数
参数 数值 低压转子长度L/m 0.4 转速比λ -1.3 低、高压转子粘性阻尼系数C1, C2/(N·s·m-1) 1 400, 1 200 转子弹性模量E/Pa 2×1011 支承刚度α/(N·m-1) 1×107 低、高压转子盘偏心距s1, s2/m 7×106, 3×10-6 低、高压转子盘半径ri, ro/m 0.1, 0.1 低、高压转子盘质量m1, m2/kg 6, 10 低、高压转轴密度ρ1, ρ2/(kg·m-1.5) 7 800, 7 800 低压转轴半径R1/m 0.029 高压转轴内、外半径R2, R3/m 0.064, 0.08 中介轴承内外滚道半径Ri, Ro/m 0.03, 0.062 中介轴承径向游隙δ0/m 2×10-6 中介轴承刚度k/(N·m-1.5) 3×109 滚动体数Nb 9 -
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