外部、参数和混合激励下的非对称转子模型:非线性分岔、主动控制和摩擦撞击效应

Randa A. Elashmawey, Nasser A Saeed, Wedad A. Elganini, Mohamed Sharaf
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引用次数: 0

摘要

本文探讨了[公式:见正文]DOF 系统的非线性动力学分析和控制,该系统仿真了非对称转子模型在外部、多参数和混合激励下的横向振动。线性积分谐振控制器([计算公式:见正文])作为主动阻尼器通过磁性致动器与转子耦合。管理转子、控制器和致动器之间非线性相互作用的完整数学模型是根据电磁理论和固体力学原理推导出来的。这导致了一个不连续的 [公式:见正文] DOF 系统与两个 [公式:见正文] DOF 系统的耦合,其中包含了转子和定子之间的摩擦撞击效应。我们采用扰动法,利用分析技术对复杂的数学模型进行了研究,并通过时间响应、吸引盆地、分岔图、[公式:见正文]混沌测试和波恩卡雷回归图进行了数值验证。主要研究结果表明,非对称系统模型在外部激励下可能表现出非零双稳态前旋运动。此外,在多参数激励下,除了三稳解外,它还可以向前或向后旋转。此外,在混合激励的情况下,转子显示出非三维的三稳态解,其中两个对应于前旋轨道,另一个对应于后旋振荡。这些发现通过建立不同的吸引力盆地得到了验证。最后,在各种激励条件下,[公式:见正文]在减轻转子振动和避免非线性灾难性分岔方面的性能。此外,还探讨了在其中一个相连控制器突然失效的情况下转子的动态行为和稳定性。结果表明,所提出的[公式:见正文]能有效消除危险的非线性现象,引导系统做出类似于线性系统的响应,且振荡幅度可控。然而,控制器的突然失效会引起局部摩擦冲击效应,导致非局部准周期振荡,并恢复非线性对系统响应的主导地位。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
An asymmetric rotor model under external, parametric, and mixed excitations: Nonlinear bifurcation, active control, and rub-impact effect
This article explores the nonlinear dynamical analysis and control of a [Formula: see text] DOF system that emulates the lateral vibration of an asymmetric rotor model under external, multi-parametric, and mixed excitation. The linear integral resonant controller ([Formula: see text]) has been coupled to the rotor as an active damper through a magnetic actuator. The complete mathematical model, governing the nonlinear interaction among the rotor, controller, and actuator, is derived based on electromagnetic theory and the principle of solid mechanics. This results in a discontinuous [Formula: see text] DOF system coupled with two [Formula: see text] DOF systems, incorporating the rub-impact effect between the rotor and stator. The complicated mathematical model is investigated using analytical techniques, employing the perturbation method, and validated numerically through time response, basins of attraction, bifurcation diagrams, [Formula: see text] chaotic test, and Poincaré return map. The main findings indicate that the asymmetric system model may exhibit nonzero bistable forward whirling motion under external excitation. Additionally, it can whirl either forward or backward under multi-parametric excitation, besides the trivial stable solution. Furthermore, in the case of mixed excitation, the rotor displays nontrivial tristable solutions, with two corresponding to forward whirling orbits and the other one corresponding to backward whirling oscillation. These findings are validated through the establishment of different basins of attraction. Finally, the performance of the [Formula: see text] in mitigating rotor vibrations and averting nonlinear catastrophic bifurcations under various excitation conditions. Furthermore, the rotor’s dynamical behavior and stability are explored in the event of an abrupt failure of one of the connected controllers. The outcomes demonstrate that the proposed [Formula: see text] effectively eliminates dangerous nonlinearities, steering the system to respond akin to a linear system with controllable oscillation amplitudes. However, the sudden controller failure induces a local rub-impact effect, leading to a nonlocal quasiperiodic oscillation and restoring the dominance of the nonlinearities on the system’s response.
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