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非线性支承转子的动平衡
引用本文:唐云冰,罗贵火,章王景璇,高德平.非线性支承转子的动平衡[J].航空动力学报,2005,20(4):600-605.
作者姓名:唐云冰  罗贵火  章王景璇  高德平
作者单位:南京航空航天大学,能源与动力学院,江苏,南京,210016
基金项目:国防基础科研基金资助(01B52008)
摘    要:影响系数法是利用线性系统中校正量和被测量之间的线性关系进行转子动平衡。实际应用中,转子系统往往是支承在具有非线性刚度的轴承上。由于线性假设不成立,直接使用影响系数法进行转子动平衡将十分困难。本文运用Lagrange方程和柔度影响系数,建立了非线性支承多盘转子系统的动平衡计算模型,提出了运用优化算法对非线性系统进行等效线性化来平衡非线性支承转子的方法。计算实例表明转子由不平衡量引起的振动得到了大幅度减少,达到了非线性支承转子动平衡的目的,效果良好。

关 键 词:航空、航天推进系统  转子动平衡  非线性支承  影响系数法  转子动力学
文章编号:1000-8055(2005)04-0600-06
收稿时间:2004/5/18 0:00:00
修稿时间:2004年5月18日

Rotor Balancing Taking Nonlinear Stiffness Characteristics into Account
TANG Yun-bing,LUO Gui-huo,ZHANG Jing-xuan and GAO De-ping.Rotor Balancing Taking Nonlinear Stiffness Characteristics into Account[J].Journal of Aerospace Power,2005,20(4):600-605.
Authors:TANG Yun-bing  LUO Gui-huo  ZHANG Jing-xuan and GAO De-ping
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing210026,China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing210026,China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing210026,China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing210026,China
Abstract:The linear relationship between the corrected value and measured value is used to balance the rotor in the influence coefficient method.When rotor are supported on the bearings having nonlinear stiffness characteristics,it would be difficult to balance the rotors since linear hypothesis would not be valid.The motion equation of a multiple-degree rotor system is formulated by using Lagrange equation and flexibility influence coefficients.The equivalent linearization model of the nonlinear multiple-degree system is used to balance the nonlinear system in this paper.The example shows that the vibration response caused by unbalance mass reduces greatly and the method developed in this paper is successful.
Keywords:aerospace propulsion system  rotor balancing  nonlinear stiffness  influence coefficient  rotor dynamic
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