首页 | 本学科首页   官方微博 | 高级检索  
     检索      

有裂纹悬臂转子的振动特性
引用本文:顾家柳,王能谦.有裂纹悬臂转子的振动特性[J].航空动力学报,1986,1(2):117-120,183-184.
作者姓名:顾家柳  王能谦
作者单位:西北工业大学 (顾家柳),西北工业大学(王能谦)
摘    要:本文研究了轴具有横向裂纹的高速悬臂转子的振动特性,提出了监视此裂纹起始及发展的最佳方法。所研究的模型是按一航空涡轮转子建立的,理论分析借传递矩阵-直接积分法,即借传递矩阵导出运动方程,再借直接积分法求解。还对模型裂纹转子作了试验研究,试验结果与理论计算结果在性质上是一致的。通过这一研究发现,转子不平衡响应的三次谐波可能是监视这一类型转子裂纹起始与发展的首要频率分量。

收稿时间:1/1/1986 12:00:00 AM

VIBRATIONAL CHARACTERISTICS OF THE CANTILEVER ROTOR WITH A CRACKED SHAFT
Gu Jialiu and Wang Nengqan.VIBRATIONAL CHARACTERISTICS OF THE CANTILEVER ROTOR WITH A CRACKED SHAFT[J].Journal of Aerospace Power,1986,1(2):117-120,183-184.
Authors:Gu Jialiu and Wang Nengqan
Institution:Northwestern Polytechnical University;Northwestern Polytechnical University
Abstract:The vibrational characteristics of the high speed cantilever rotor with a cracked shaft are investigated to find an optimum vibration monitoring method for a turbine rotor. The model studied is established based on the structure of a real turbine rotor.The transfer matrix-direct integration method proposed by the first author in reference (2) is applied to the theoretical analysis. In consequence it is possibleto avoid making any assumption about the whirling orbit, and modification of some real parameters and whirling orbit of the disk is performed sequentially in the process of numerical integration. In experimental investigation some measures are taken to create a crack very similar to a real crack on the shaft.The results of Fourier analysis of the unbalance responses obtained from both calculations and experiments show that in signature of vibration of the cracked rotor exist very strong 2nd anc 3rd harmonics. The triple-frequency harmonic increases with the rotating speed and reaches maximum at the speed being equal to 1/3 of the critical speed.Since the second harmonic can be caused by the other factors such as misalignment,as a result of this research the authors suggest that operating the rotor in the vicinity of 1/3 of the critical speed and monitoring the triple-frequency component be the best method to detect a crack for this kind of turbine.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号