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一种分析非线性转子-支承系统非协调响应的近似方法 被引量:2

An approximate method for analyzing nonsynchronous responses of nonlinear rotor bearing system
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摘要 运用文献[1]提出的线性化法,将系统做非协调响应下的非线性元件转换为等效线性元件和等效外谐和力两部分,随后用子模态综合法并借助二阶非完整约束系统的Routh型方程,建立了全部连接条件下非线性转子-支承系统的运动微分方程;大此基础上,将求解微分方程转化为求解代数方程,从而通过简单地迭代过程便可求得系统的非协调响应,与Runge-Kuta法的结果比较表明:本文的方法简捷、近似程度高。 Using a linear technique of Ref., nonlinear elements are substituted for the sum of the equivalent linear elements and the equivalent external harmonic forces in a state of the nonsynchronous responses.Then,with the aid of Rouths equation with nonholonomic constrains, the differential equations of motion of the equivalent system are derived by component mode synthesis technique,considering all boundary conditions .Further, the set of the differential equations is changed into a set of algebraic equations.The solutions of the algebraic equations can be obtained by simply iterative procedure.Numerical results show that the approximate solution is very near the real solution,and computing efficiency can be improved greatly.
出处 《西安工业学院学报》 1996年第4期345-349,共5页 Journal of Xi'an Institute of Technology
基金 国家航空科学基金
关键词 转子-支承系统 非协调响应 非线性力 近似法 nonlinear systems rotor bearing system nonsynchronous responses analysis method computation method
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同被引文献8

  • 1顾致平,孟光,支希哲.柔性转子─支承系统瞬态响应分析的模态叠加─Riccati传递矩阵法[J].振动工程学报,1995,8(2):178-183. 被引量:5
  • 2Li D F,Gunter E J.Component mode synthesis of large rotor systems[J].ASME,J.of Engineering for Power,1982,104:552~560.
  • 3Nelson H D.Nonlinear analysis of rotor-beating systems using component mode synthesis[J].ASME,J.of Engineering for Power,1983,105:606~614.
  • 4张文.模态综合法在转子动力学中的应用[J].振动与冲击,1984,3:16-24.
  • 5高建民 陈松淇.子模态综合法中动力对接条件的研究[J].西北工业大学学报,1988,6(3):343-350.
  • 6Zhiping Gu,Xizhe Zhi,Guang Meng,Tong Fang.Transient response analysis of large scale rotor-bearing system with strong nonlinear elements by a transfer matrix-newmark formulation itegration method[J].Journal of Sound and Vibration,2003,259(3):559~570.
  • 7梅凤翔.非完整系统力学基础[M]北京工业学院出版社,1985.
  • 8顾致平,陈松淇.连续空间离散时间—Riccati传递矩阵积分法[J].航空动力学报,1991,6(1):46-50. 被引量:3

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