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

转子特性参数的预估和临界响应的预报
引用本文:廖明夫,蒲秋洪,钟志才.转子特性参数的预估和临界响应的预报[J].航空动力学报,2003,18(3):367-372.
作者姓名:廖明夫  蒲秋洪  钟志才
作者单位:1. 西北工业大学,旋转机械与风能装置测控研究所,陕西,西安,710072
2. 中国燃气涡轮研究院,四川,成都,610500
摘    要:建立了转于系统临界转速和阻尼比的估计方法。利用转子升速至80%~90%的临界转速之前的数据就可估计出转子的临界转速和阻尼比,而无须使转子越过临界转速。由此可避免转子过临界时的剧烈振动。本文还给出了转子在临界转速处的不平衡响应的预报方法。实验结果表明,本文建立的方法是有效的。

关 键 词:航空、航天推进系统  转子  临界转速  阻尼比  预估
文章编号:1000-8055(2003)03-0367-06
收稿时间:2002/7/18 0:00:00
修稿时间:2002年7月18日

Estimation of Critical Speed and Damping Ratio of a Rotor and Prediction of the Rotor Response at Critical Speed
LIAO Ming-fu,PU Qiu-hong and ZHONG Zhi-cai.Estimation of Critical Speed and Damping Ratio of a Rotor and Prediction of the Rotor Response at Critical Speed[J].Journal of Aerospace Power,2003,18(3):367-372.
Authors:LIAO Ming-fu  PU Qiu-hong and ZHONG Zhi-cai
Institution:Northwestern Polytechnical University,Xi'an 710072,China;Gas Turbine Establishment of China,Chendu 610500,China;Gas Turbine Establishment of China,Chendu 610500,China
Abstract:This paper presents methods for estimating critical speed and damping ratio of a rotor and predicting the rotor response to imbalance at the critical speed. The estimation and prediction are carried out by means of the vibration values measured during the escalation stage of the rotor speed but below critical speed. In this way the critical speed and damping ratio can be obtained without running the rotor over its critical speeds, therefore a violent and dangerous vibration of the rotor at critical speed can be avoided. Additionally the prediction of the rotor response to imbalance at critical speed can give an assessment of condition of the rotor balance. Experimental results show that the critical speed and damping ratio can satisfactorily be estimated by these methods below 80 percent of the critical speed.
Keywords:aerospace propulsion system  rotor  critical speed  damping ratio  prediction  
本文献已被 CNKI 万方数据 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