首页 | 本学科首页   官方微博 | 高级检索  
     

转子-定子系统碰摩可靠性灵敏度研究
引用本文:张义民,刘巧伶,李鹤,闻邦椿. 转子-定子系统碰摩可靠性灵敏度研究[J]. 航空动力学报, 2006, 21(5): 848-853
作者姓名:张义民  刘巧伶  李鹤  闻邦椿
作者单位:东北大学,机械工程与自动化学院,沈阳,110004;吉林大学,机械科学与工程学院,长春,130025
基金项目:国家自然科学基金 , 辽宁省自然科学基金
摘    要:针对仅考虑质量偏心的Jeffcott转子-定子系统碰摩的动力学方程,进行了旋转机械转子-定子系统的碰摩可靠性灵敏度分析,应用Kronecker代数,矩阵微分理论,四阶矩技术,矩阵摄动理论,概率统计方法,可靠性理论和灵敏度技术系统地发展了转子-定子系统碰摩的可靠性灵敏度分析方法,研究了转轴刚度和阻尼、定子刚度和阻尼、偏心距和定子径向刚度对可靠度灵敏度的影响,并给出了数值分析解.

关 键 词:航空、航天推进系统  转子-定子系统  碰摩  可靠性灵敏度
文章编号:1000-8055(2006)05-0848-06
收稿时间:2005-08-27
修稿时间:2005-08-27

Reliability sensitivity investigation of impact-rub for rotor-stator systems
ZHANG Yi-min,LIU Qiao-ling,LI He and WEN Bang-chun. Reliability sensitivity investigation of impact-rub for rotor-stator systems[J]. Journal of Aerospace Power, 2006, 21(5): 848-853
Authors:ZHANG Yi-min  LIU Qiao-ling  LI He  WEN Bang-chun
Affiliation:School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110004, China;Institute of Mechanical Science and Engineering, Jilin University, Changchun 130025, China;School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110004, China;School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110004, China
Abstract:On the basis of the impact-rub dynamics equations of Jeffcott rotor-stator systems with imbalance,the reliability sensitivity investigation of rotor-stator systems of rotating machinery under impact-rub is presented.Techniques from Kronecker algebra,matrix calculus,fourth moment analysis,probabilistic perturbations,reliability theory and sensitivity technique are employed to systematically develop the mathematical and numerical expressions for reliability sensitivity analysis of rotor-stator systems.The effects of shaft stiffness and damping, stator stiffness and damping,radial clearance and stator radial stiffness on reliability sensitivity are studied and discussed.The numerical results are obtained.
Keywords:aerospace propulsion system  rotors-stator  Impact-rub  reliability sensitivity  
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