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失调叶片盘耦合振动的力学模型
引用本文:阎云聚,顾家柳,徐明.失调叶片盘耦合振动的力学模型[J].航空学报,1993,14(8):365-371.
作者姓名:阎云聚  顾家柳  徐明
作者单位:西北工业大学振动研究所,西北工业大学振动研究所,西北工业大学振动研究所 西安 710072,西安 710072,西安 710072
摘    要: 借助于子结构模态综合法,为研究真实的失调叶片盘耦合振动问题提出了一种非常接近于实际叶片盘的力学模型和简便的理论分析方法;并通过对一个实际失调叶片盘的强迫振动试验,对力学模型、计算公式和程序进行了考核验证。结果表明,试验与计算相当吻合。

关 键 词:失调叶片盘  耦合振动  力学模型  理论分析方法  强迫振动试验  

A MECHANICAL MODEL FOR COUPLING VIBRATION OF MISTUNED BLADED DISK
Yan Yuan-ju,Gu Jia-liu,Xu Min.A MECHANICAL MODEL FOR COUPLING VIBRATION OF MISTUNED BLADED DISK[J].Acta Aeronautica et Astronautica Sinica,1993,14(8):365-371.
Authors:Yan Yuan-ju  Gu Jia-liu  Xu Min
Institution:Institute of Vibration Engineering, Northwestern Poly technical Universitv, Xi'an, 710072
Abstract:Because the coupling vibration of bladed disk is rather harmful to the structural strength of aeromotors, a lot of work has been done for more than 30 years. Many simplified models of mistimed bladed disk were used for theoretical researches because experimental researches on aeromolors are difficult. However, some of the conclusions of many studies are inconsistent or conflicting. This paper developed a better mechanical model of mistuned bladed disk by Modal Synthesis Method for studying the vibration characteristics of real bladed disk assemblies. The model and theoretical analysis are checked by experiment of forced vibration on a real mistuned bladed disk. In terms of this model, the vibrational natures of the bladed disk assemblies can be studied well.
Keywords:mistimed bladed disk  coupling vibration  mechanical model  theoretical analysis method  experiment of forced vibration  
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