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转动壳体行波振动的有限元分析方法 被引量:9

Traveling-Wave Vibration of Rotating Shells by Finite Element Method
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摘要 转动壳体由于离心力与哥氏力的影响 ,其振动频率随转速变化 ,并且同一振型对应两个不同频率的前、后行波。本文给出了用有限元法计算转动壳体的有限元公式 ,用 MSC/ NASTRAN的 DMAP语言编制了形成哥氏力矩阵与离心刚度矩阵的程序 。 The finite element equations of the traveling wave vibration of rotating shells with the effects of the Coriolis and centrifugal force are established in this paper.Because of the effect of Coriolis force,the frequencies of forward and backward wave are different even under the rotating coordinate system.This is the main difference between rotating shells and disks.The Coriolis and centrifugal stiffness matrixes are formed by modifying the lump mass matrix and introduced into finite element program MSC/NASTRAN by DMAP (Direct Matrix Abstraction Program).To validate the present analysis,comparisons are made with existing results for a rotating shell and good agreement is obtained.
作者 曹航 朱梓根
出处 《航空动力学报》 EI CAS CSCD 北大核心 2002年第2期222-225,共4页 Journal of Aerospace Power
关键词 转动壳体 行波振动 有限元分析方法 哥氏力矩阵 rotating shells FEM traveling wave vibration
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参考文献1

  • 1蔡肇云 金六周.航空发动机强度设计、试验手册[M].北京:第三机械工业部第六研究院,1981..

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  • 1刘更,沈允文,方宗德,何大为,高向群.航空高速双联斜齿圆柱齿轮行波共振的研究[J].西北工业大学学报,1992,10(3):344-350. 被引量:6
  • 2钟万勰.结构动力方程的精细时程积分法[J].大连理工大学学报,1994,34(2):131-136. 被引量:509
  • 3李永强,郭星辉,李健.科氏力对旋转叶片动频的影响[J].振动与冲击,2006,25(1):79-81. 被引量:11
  • 4李健,郭星辉,李永刚.薄壁圆柱壳旋转波动振动分析[J].东北大学学报(自然科学版),2007,28(4):553-556. 被引量:8
  • 5宋轶民,刘欣,张策,刘建平.高速行星传动内齿圈的有限元分析[J].中国机械工程,2007,18(9):1016-1019. 被引量:11
  • 6Loy C T . Vibrations of rotating thin cylindrical panels. Applied Acoustics, 1995 ;46 : 327--343.
  • 7Liew K M. Harmonic reproducing kernel particle method for free vibration analysis of rotating cylindrical shells. Computer Methods in Applied Mechanics and Engineering,2002 ;191:4141---4157.
  • 8Civalek O. A parametric study of the free vibration analysis of rotating laminated cylindrical shells using the method of discrete singular convolution. Thin-walled Structures,2007;45:692--698.
  • 9Castanier M P, Pierre C. Modeling and analysis of mistuned bladed disk vibration: status and emerging directions [ J]. Journal of Propulsion and Power, 2006, 22 (2) : 384-396.
  • 10Yu C B, Wang J J, Li Q H. On the individual and combined effects of intentional mistuning, coupling and damping on the forced response of bladed disks [ C ]. Berlin: Proceedings of ASME Turbo Expo,2008 :493-499.

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