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Experimental Verification of the Dynamic Model of Turbine Blades Coupled by a Sealing Strip

机译:密封条涡轮机叶片动态模型的实验验证

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摘要

This paper presents the experimental-numerical comparison of a bladed system with flexible strip dampers. The experimental results constitute, to the authors’ knowledge, the first published experimental evidence on strip dampers. They explore the in-phase and out-of-phase mode of vibration of two blades coupled by a strip damper. The great influence the mode of vibration has on the strip behaviour and consequent effect on the blades’ response is highlighted, analyzed and successfully simulated numerically. Experiments are made possible by a purposely developed loading system based on compressed air. This non-contact system enables the experimenter to apply a realistic value of contact pressure on the strip without adding spurious stiffness to the system or modifying the contact conditions. The availability of experimental data obtained by imposing realistic contact conditions constitutes a true added value. It is here shown how the full stick linear FRFs (Frequency Response Functions), typically used to predict the response in case of limited excitation on blades coupled by rigid dampers, do not offer significant results in the case of flexible strip dampers.
机译:本文介绍了柔性条带阻尼器的叶片系统的实验数值比较。实验结果构成了作者的知识,第一个关于条带阻尼器的实验证据。它们探讨了由条带阻尼器连接的两个叶片的相位和超相振动模式。突出显示,在数字上突出显示,振动模式对叶片行为的影响以及对叶片响应的影响。通过基于压缩空气的无意开发的装载系统实现了实验。该非接触系统使实验者能够在条带上施加接触压力的逼真值,而不为系统添加杂散刚度或改变接触条件。通过施加现实接触条件获得的实验数据的可用性构成了真正的附加值。这里示出了如何如何预测由刚性阻尼器连接的叶片的有限激发的全粘线性FRF(频率响应函数),通常在柔性阻尼器的情况下不提供显着的结果。

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