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有大预紧效应的多叶径向箔片轴承的分析
引用本文:耿海鹏,戚社苗,虞烈.有大预紧效应的多叶径向箔片轴承的分析[J].航空动力学报,2006,21(3):569-574.
作者姓名:耿海鹏  戚社苗  虞烈
作者单位:西安交通大学,机械电子及信息系统研究所,陕西,西安,710049
基金项目:国家自然科学基金 , 国家科技攻关项目 , 西安交通大学校科研和教改项目
摘    要:针对有大预紧效应多叶径向箔片轴承的结构特点,通过引入辅助分析部件建立箔片轴承的非线性接触有限元仿真模型.在分析过程中通过改变作为刚性体的辅助部件和作为柔性体轴承部件之间的几何位置来模拟大预紧多叶箔片径向轴承的装配过程并最终求得箔片轴承中接触应力应变.将处理轴承间隙压力分布的控制方程-雷诺方程和非线性的接触求解过程耦合起来迭代求解,第一次对有大预紧效应的多叶箔片径向轴承进行了完全气弹耦合数值分析.

关 键 词:航空、航天推进系统  多叶箔片轴承  雷诺方程  接触有限元  大预紧
文章编号:1000-8055(2006)03-0569-06
收稿时间:2005/4/22 0:00:00
修稿时间:2005年4月22日

Analysis of the Multileaf Foil Journal Bearings with Large Preload Effect
GENG Hai-peng,QI She-miao and YU Lie.Analysis of the Multileaf Foil Journal Bearings with Large Preload Effect[J].Journal of Aerospace Power,2006,21(3):569-574.
Authors:GENG Hai-peng  QI She-miao and YU Lie
Abstract:According to the structure characteristics of the multileaf foil journal bearing with large preload effect,the nonlinear Finite Element contact model of the foil bearings was established through introducing the assistant parts.The performance of the foil bearings were investigated using Finite Element Method.The assistant parts were used to help form the last contact relationship of foil bearings in the numerical simulation process.These assistant parts were dealt with as rigid bodies without strain.Through modifying the moving contact relationship between the foil bearing parts,the large preload effect of foil bearing was dealt with using the nonlinear contact Finite Element analysis between rigid bodies and flexible bodies.Solution of the governing hydrodynamic equation dealing with compressible fluid was coupled with the structure resiliency of the foil bearing surfaces.In this paper,a typical five leaves foil bearing with large preload effect was analyzed as a successful case to prove the analysis feasibility and accuracy.
Keywords:aerospace propulsion system  multileaf foil bearing  Reynolds equation  contact finite element  large preload
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