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Rotor dynamics analysis and experiment study of the flywheel spin test system

机译:飞轮自旋测试系统的转子动力学分析与实验研究

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The strength study of the flywheel is important to the flywheel energy storage. The motor and bearing are the key challenges for the high-speed flywheel spin test device in vacuum. By using a small stiffness pivot-jewel bearing and a spring squeeze film damper as the lower support of the flywheel, a simple spin system was designed at a low cost and is suitable for longtime operation. The auxiliary support at the top was not removed until the flywheel passed the first critical speed. The flywheel that kept its rigid state in sub-critical state was tested at the high speed without the top support. The dynamic model of the flywheel-bearing-damper was built by means of the Lagrangian equation to calculate critical speeds, mode shapes and modal damping ratios at different speeds. The lower damper's effects on the modal damping ratios and forced vibration were discussed. The vibrations of the flywheel-bearing-damper system were measured at the different damping coefficients in the experiment. When the lower damper was adjusted to be overdamped, the flywheel ran up to 50000 r/min steadily, and the experimental result was in agreement with the theoretical assumption. The sub-critical rotor dynamics design and pivot-jewel bearing proved to be good solutions to the spin test for the composite flywheel.
机译:飞轮的强度研究对于飞轮的能量存储很重要。电机和轴承是真空中高速飞轮自旋测试设备的关键挑战。通过使用较小刚度的枢轴宝石轴承和弹簧挤压膜减震器作为飞轮的下部支撑,设计了一种简单的旋转系统,成本低廉,适合长时间运行。直到飞轮超过第一临界速度时,顶部的辅助支撑才被移除。在没有顶部支撑的情况下,以高速测试了将飞轮保持在亚临界状态的飞轮。利用拉格朗日方程建立了飞轮轴承阻尼器的动力学模型,以计算临界速度,不同速度下的模态形状和模态阻尼比。讨论了下阻尼器对模态阻尼比和强迫振动的影响。实验中在不同的阻尼系数下测量了飞轮轴承-阻尼器系统的振动。调整下阻尼器过阻尼后,飞轮稳定运行至50000 r / min,实验结果与理论假设相符。亚临界转子动力学设计和枢轴轴承设计证明是复合飞轮旋转测试的良好解决方案。

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