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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Multi-Wave Vibration Caused by Flutter Instability and Nonlinear Tip-Shroud Friction
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Multi-Wave Vibration Caused by Flutter Instability and Nonlinear Tip-Shroud Friction

机译:颤振不稳定性和非线性叶罩摩擦引起的多波振动

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摘要

Measurements revealed the contribution of multiple traveling waves to the flutter vibrations of bladed disks. Saturated flutter vibration, whether in this multi-wave or in its better-understood single-wave form, is a nonlinear phenomenon. However, it is still not understood of what physical origin the relevant nonlinearities are, and under what conditions single-wave or multi-wave flutter vibration occurs. Recent theoretical work suggests that multi-wave flutter vibration can be explained by strongly nonlinear frictional inter-blade coupling. The verity of this hypothesis is strictly limited by the simplicity of the considered model, namely, a cyclic chain of seven oscillators with frictional coupling and rather unrealistic aeroelastic behavior. In this work, it is demonstrated that nonlinear dynamical contact interactions at tip-shrouds are a likely cause for the observed multi-wave flutter vibration. To this end, a more realistic structural turbine blade row model with a more realistic aeroelastic behavior is considered. Some insight into its intriguing dynamics, dependence of limit states on initial conditions, and eigenvalue placement is provided. For instance, it is shown that there is an intimate relation between internal combination resonance conditions of certain traveling wave modes and the spectral content of single- and multi-wave flutter oscillations.
机译:测量表明,多个行波对叶片盘颤动的影响。无论是这种多波形式还是其更好理解的单波形式,饱和颤振都是一种非线性现象。然而,仍然不清楚有关的非线性是什么物理起源,以及在什么条件下发生单波或多波颤振。最近的理论工作表明,多波颤振可以通过强非线性摩擦叶片间耦合来解释。该假设的真实性受到所考虑模型的简单性的严格限制,即,具有摩擦耦合和相当不现实的气动弹性行为的七个振荡器的循环链。在这项工作中,证明了端盖处的非线性动力接触相互作用是观察到的多波颤振的可能原因。为此,考虑具有更现实的空气弹性行为的更现实的结构涡轮叶片排模型。提供了一些有关其有趣的动力学,极限状态对初始条件的依赖性以及特征值放置的见解。例如,表明在某些行波模式的内部组合共振条件与单波和多波颤振的频谱含量之间存在密切关系。

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    《Journal of Engineering for Gas Turbines and Power》 |2020年第2期|021013.1-021013.8|共8页
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    Institute of Aircraft Propulsion Systems University of Stuttgart Stuttgart 70569 Germany;

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