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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Unbalance response of a magnetic suspended dual-rotor system
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Unbalance response of a magnetic suspended dual-rotor system

机译:磁悬浮双转子系统的不平衡响应

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The magnetic suspended dual-rotor system applied in more electric aero-engine can eliminate the wear and lubrication system of mechanical bearings and solve the vibration control issue of system effectively, which provides the possibility to improve the performance of aero-engine significantly. This research focuses on the unbalance response of the magnetic suspended dual-rotor system. First, a structure of dual-rotor system supported by two active magnetic bearings and two permanent magnetic bearings is presented. With proportional derivative (PD) control adopted, the bearing characteristics of active magnetic bearings are modeled as the equivalent stiffness and equivalent damping, and the permanent magnetic bearings are modeled as elastic support. Then, the Riccati transfer matrix method with good numerical stability is used to establish the model of the magnetic suspended dual-rotor system unbalance response. Subsequently, the validity of the present formulation has been tested against some known results available in literature and the simulation results obtained by finite element method (FEM). Finally, the dynamic characteristics of the unbalance response are investigated. The results reveal that the influence of the inner rotor imbalance excitation on the magnetic suspended dual-rotor system unbalance response is much larger than that of the outer rotor imbalance excitation. In addition, the critical speeds increase with the proportional coefficient, and the derivative coefficient can affect the amplitudes of the unbalance response, but not critical speeds. From the perspectives of the maximum bearing capacity and maximum displacement of active magnetic bearing-rotor system, the possibility of the magnetic suspended dual-rotor system safely crossing the critical speeds of the first three orders is investigated.
机译:应用于更多电动航空发动机的磁悬浮双转子系统可以消除机械轴承的磨损和润滑系统,有效解决系统的振动控制问题,为大幅提高航空发动机的性能提供了可能。这项研究集中在磁悬浮双转子系统的不平衡响应上。首先,提出了一种由两个主动磁轴承和两个永磁轴承支撑的双转子系统的结构。在采用比例微分(PD)控制的情况下,主动磁轴承的轴承特性建模为等效刚度和等效阻尼,而永磁轴承则建模为弹性支撑。然后,采用数值稳定性好的Riccati传递矩阵法建立了磁悬浮双转子系统不平衡响应的模型。随后,已经针对文献中可获得的一些已知结果以及通过有限元方法(FEM)获得的模拟结果测试了本制剂的有效性。最后,研究了不平衡响应的动态特性。结果表明,内转子不平衡励磁对磁悬浮双转子系统不平衡响应的影响远大于外转子不平衡励磁的影响。此外,临界速度随比例系数增加,而导数系数会影响不平衡响应的幅度,但不会影响临界速度。从主动磁轴承-转子系统的最大承载能力和最大位移的角度,研究了磁悬浮双转子系统安全越过前三个阶的临界速度的可能性。

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