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ROTOR-BLADE COUPLED VIBRATION ANALYSIS BY MEASURING MODAL PARAMETERS OF ACTUAL ROTOR

机译:测量实际转子模态参数的叶片与叶片耦合振动分析

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The designers of rotor shafts and blades for a traditional turbine-generator set typically employed their own models and process by neglecting the coupled torsional effect. The torsional coupled umbrella mode of recent longer blades systems designed for higher output and efficiency tends to have nearly doubled the frequency of electric disturbance (i.e., 100 or 120 Hz). In order to precisely estimate the rotor-blade coupled vibration of rotating shafts, the analysis must include a process to identify the parameters of a mathematical model by using a real model. In this paper we propose the use of a unique quasi-modal technique based on a concept similar to that of the modal synthesis method, but which represents a unique method to provide a visually reduced model. An equivalent mass-spring system is produced for uncoupled umbrella mode and modal parameters are measured in an actual turbine rotor system. These parameters are used to estimate the rotor-blade coupled torsional frequencies of a 700-MW turbine-generator set, with the accuracy of estimation being verified through field testing.
机译:传统涡轮发电机组的转子轴和叶片的设计人员通常通过忽略耦合的扭转效应而采用自己的模型和过程。最近设计用于更高输出和效率的更长叶片系统的扭转耦合伞形模式往往使电干扰的频率(即100或120 Hz)几乎增加了一倍。为了精确估计旋转轴的转子-叶片耦合振动,分析必须包括通过使用实际模型来识别数学模型的参数的过程。在本文中,我们基于与模态合成方法相似的概念,提出了一种独特的准模态技术的使用,但它代表了一种提供可视化简化模型的独特方法。产生了等效的质量弹簧系统,用于非耦合伞模式,并在实际的涡轮转子系统中测量了模态参数。这些参数用于估算700 MW汽轮发电机组的转子-叶片耦合扭转频率,并通过现场测试验证了估算的准确性。

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