推进技术 ›› 2014, Vol. 35 ›› Issue (8): 1116-1122.

• 结构 强度 可靠性 • 上一篇    下一篇

润滑气体及箔片材料对气体动压轴承动特性影响分析

方 华1,常海萍1,张镜洋2,马虎跃1   

  1. 江苏省航空动力系统重点实验室,南京航空航天大学 能源与动力学院,江苏 南京 210016;江苏省航空动力系统重点实验室,南京航空航天大学 能源与动力学院,江苏 南京 210016;南京航空航天大学 高新技术研究院,江苏 南京 210016;江苏省航空动力系统重点实验室,南京航空航天大学 能源与动力学院,江苏 南京 210016
  • 发布日期:2021-08-15
  • 作者简介:方 华(1988—),男,硕士生,研究领域为航空航天推进技术。

Analysis of Lubrication Gas and Elastic Foil for Gas Foil Bearing Dynamic Characteristics

  1. Jiangsu Province Key Laboratory of Aerospace Power Systems ,College of Energy and Power,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;Jiangsu Province Key Laboratory of Aerospace Power Systems ,College of Energy and Power,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;College of High and New Technology ,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;Jiangsu Province Key Laboratory of Aerospace Power Systems ,College of Energy and Power,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
  • Published:2021-08-15

摘要: 为研究润滑气体和弹性箔片材料特性对波箔型气体动压轴承动特性的影响,以Hydresil型波箔气体动压轴承为研究对象,建立气体流动控制方程和波箔弹性变形模型,通过有限差分法求解扰动方程获得动特性系数。数值分析了润滑气体动力粘度(4.2×10-6~4.6×10-5Pa·s)、轴承波箔片材料泊松比(0.15~0.45)和弹性模量(70~340GPa)对动特性系数的影响规律。结果表明,在偏心率和转速相同情况下,随气体动力粘度升高,动态刚度系数逐渐增大,且主刚度方向增大最为明显,最大可超过50%,动态阻尼系数也增大,且x方向增大最为明显,最大可达60%;随轴承箔片材料弹性模量的增大,动态刚度系数不断增大,动态阻尼系数在y方向上逐渐增大,在x方向上逐渐减小;轴承箔片材料泊松比对动特性系数影响较小。

关键词: 气体动压轴承;动特性系数;气体动力粘度;泊松比;弹性模量

Abstract: Numerical study for effects of lubrication gas and foil material properties on bump-type foil aerodynamic bearing dynamic characteristics was performed by taking the gas bearing of Hydresil type as the research object. A gas flow control equation and the bump foil elastic deformation model were set up. The finite difference method was used to solve the model for obtaining the dynamic characteristics of gas foil bearings. With reference to the actual situation,the lubrication gas viscosity ranges from 4.2×10-6 to 4.46×10-5Pa·s,bump foil material Poisson’s ratio ranges from 0.15 to 0.45 and the modulus of elasticity ranges from 70 to 340GPa. Results show that under the same eccentricity and rotation speed,with the increase of viscosity,dynamic stiffness coefficients increase gradually,and the main stiffness coefficient increase most obviously and it can be more than 50%. The dynamic damping coefficients increase too,and the values at x direction increase most obviously,the maximum is 60%. Along with the increase of bearing foil material elastic modulus,dynamic stiffiness coefficients increase,dynamic damping coefficients at y direction gradually increase and at x direction it gradually decrease.Poisson’s ratio of bearing foil material has little influence on coefficients of dynamic characteristics.

Key words: Aerodynamic bearing;Dynamic characteristic coefficients;Gas viscosity;Poisson’s ratio;Elasticity modulus