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PARAMETRIC RESONANCES OF A SPINNING CYCLIC SYMMETRIC ROTOR ASSEMBLED TO A FLEXIBLE STATIONARY HOUSING VIA MULTIPLE BEARINGS

机译:旋转轴承对称转子通过多个轴承组装到灵活的固定壳体中的参数共振

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This paper is to present findings from a theoretical study on free vibration and stability of a rotor-bearing-housing system. The rotor is cyclic symmetric and spinning at constant speed, while the housing is stationary and flexible. Moreover, the rotor and housing are assembled via multiple, linear, elastic bearings. For the rotor and the housing, their mode shapes are first obtained in rotor-based and ground-based coordinate systems, respectively. By discretizing the kinetic and potential energies of the rotor-bearing-housing system through use of the mode shapes, a set of equations of motion appears in the form of ordinary differential equations with periodic coefficients. Analyses of the equations of motion indicate that instabilities could appear at certain spin speed in the form of combination resonances of the sum type. To demonstrate the validity of the formulation, two numerical examples are studied. For the first example, the spinning rotor is an axisymmetric disk and the housing is a square plate with a central shaft. Moreover, the rotor and the housing are connected via two linear elastic bearings. Instability appears in the form of coupled vibration between the stationary housing and spinning rotor through three different formats: rigid-body rotor translation, rigid-body rotor rocking, and elastic rotor modes that present unbalanced inertia forces or moments. For the second example, the rotor is cyclic symmetric in the form of a disk with four evenly spaced slots. The housing and bearings remain the same. When the rotor is stationary, natural frequencies and mode shapes predicted from the formula- tion agree well with those predicted from a finite element analysis, which further ensures the validity of the formulation. When the cyclic symmetric rotor spins, instability appears in the same three formats as in the case of axisymmetric rotor. Number of instability zones, however, increases because the cyclic symmetric rotor has more elastic rotor modes that present unbalanced inertia forces or moments.
机译:本文将从对转子-轴承-壳体系统的自由振动和稳定性的理论研究中得出发现。转子是周期性对称的,并且以恒定速度旋转,而壳体则是固定且灵活的。此外,转子和壳体通过多个线性弹性轴承组装。对于转子和壳体,首先分别在基于转子的坐标系和基于地面的坐标系中获得其模态形状。通过使用模态形状离散转子轴承壳体系统的动能和势能,运动方程组以具有周期系数的常微分方程的形式出现。对运动方程的分析表明,不稳定性可能以总和类型的组合共振的形式在一定的自旋速度下出现。为了证明该配方的有效性,研究了两个数值示例。对于第一个示例,旋转转子是轴对称盘,而壳体是带有中心轴的方板。此外,转子和壳体通过两个线性弹性轴承连接。不稳定以固定壳体和旋转转子之间通过三种不同形式的耦合振动形式出现:刚体转子平移,刚体转子摇摆和弹性转子模式,这些模式呈现出不平衡的惯性力或力矩。对于第二示例,转子是具有四个均匀间隔开的槽的盘形式的循环对称。外壳和轴承保持不变。当转子静止时,根据公式预测的固有频率和模态形状与根据有限元分析预测的固有频率和模态形状非常吻合,从而进一步确保了公式的有效性。当环状对称转子旋转时,不稳定性以与轴对称转子相同的三种形式出现。但是,不稳定区域的数量增加了,因为循环对称转子具有更弹性的转子模式,呈现出不平衡的惯性力或力矩。

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    《》|2012年|641-650|共10页
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    W. C. TAI; I. Y. SHEN;

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