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

基于滞回碰摩力模型的转子系统碰摩响应研究
引用本文:曹登庆,杨 洋,王德友,陈华涛,姜广义.基于滞回碰摩力模型的转子系统碰摩响应研究[J].航空发动机,2014,40(1):1-9.
作者姓名:曹登庆  杨 洋  王德友  陈华涛  姜广义
作者单位:1. 哈尔滨工业大学 航天学院,哈尔滨 150001;2. 中航工业沈阳发动机设计研究所,沈阳 110015
基金项目:国家重大基础研究项目资助
摘    要:转/静子碰摩是影响旋转机械的稳定性与安全性的重要因素之一,而碰摩力的表征则是预测转子系统动力学响应的关键问题。讨论了已有转/静子碰摩力模型的适用范围,重点阐述滞回碰摩力模型的物理意义,并与几种经典的碰摩力模型进行比较;以Jeffcott转子作为典型例子,基于滞回碰摩力模型给出系统的碰摩响应,并与采用线性碰摩力模型所得到的碰摩响应进行比较;利用数值仿真的结果分析静子刚度、转子偏心距等因素对采用滞回碰摩力模型的转子碰摩响应的影响。数值仿真的结果表明:采用滞回碰摩力模型得出的失稳速度(1226 rad/s)低于采用线性碰摩力模型得出的失稳速度(1476 rad/s),且系统的动力学特性更为复杂,因此,可以更真实地反应碰摩的物理实质。

关 键 词:Jeffcott转子  碰摩  线性模型  赫兹模型  滞回模型

Study on Rub-impact Responses of Rotor Systems Based on Hysteretic Rub-impact Force Model
Authors:CAO Deng-qing  YANG Yang  WANG De-you  CHEN Hua-tao  JIANG Guang-yi
Institution:1. School of Astronautics, Harbin Institute of Technology, Harbin 150001, China; 2. AVIC Shenyang Engine Design and Research Institute, Shenyang 110015, China
Abstract:The rub-impact of rotor/stator is one of the major factors for the stability and safety of rotating machine, while the characterization of the rub-impact force is a key problem in the prediction of dynamical responses of the rotor system. The applicable scope of the existing rotor/stator rub-impact force models was discussed, the physical significances of the hysteretic rub-impact force model was described clearly, and the comparison between the hysteretic rub-impact force model and classical ones was conducted. Taking the Jeffcott rotor as a typical example, the rub-impact responses of system based on the hysteretic rub-impact force model are given and used to compare with the result form the system with linear rub-impact force model. The effects of stator stiffness and the rotor eccentricity on rub-impact responses of the rotor system with the hysteretic rub-impact force model were given to analyze by the numerical results. The numerical simulation results show that the stability threshold speed (1226 rad/s) of the system in terms of the hysteretic rub-impact force model is less than that (1476 rad/s) of the system with linear rub-impact force model, and the dynamic characteristics are more complicated, therefore, the essential physical property of rub-impact can be reflected more veritably.
Keywords:Jeffcott rotor  rub-impact  linear model  Hertz model  hysteretic model
本文献已被 CNKI 维普 等数据库收录!
点击此处可从《航空发动机》浏览原始摘要信息
点击此处可从《航空发动机》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