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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (11): 127639-127639.doi: 10.7527/S1000-6893.2022.27639

• Fluid Mechanics and Flight Mechanics • Previous Articles     Next Articles

Analysis method and distribution characteristics of non-uniform slip flow at fluid-solid interface of gas foil bearing

Jingyang ZHANG1(), Zhe CHEN1, Yuanwei LYU1, Yijian SUN1, Jingzhou ZHANG2, Weidong CHEN1,3, Xinyang LUO4   

  1. 1.College of Astronautics,Nanjing University of Aeronautics and Astronautics,Nanjing  211106,China
    2.College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing  210016,China
    3.State Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics,Nanjing  210016,China
    4.Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration,Nanjing Engineering Institute of Aircraft Systems,Nanjing  211106,China
  • Received:2022-06-16 Revised:2022-08-30 Accepted:2022-09-30 Online:2023-06-15 Published:2022-10-14
  • Contact: Jingyang ZHANG E-mail:zjy@nuaa.edu.cn
  • Supported by:
    Aeronautical Science Foundation of China(201928052008);Scientific Research and Practice Innovation Foundation of Nanjing University of Aeronautics and Astronautics(xcxjh20211505)

Abstract:

To solve the problem of the analysis method for the variable scale flow in the micro clearance of the airborne gas foil bearing under large overload and large eccentricity, a coupled iterative interface non-uniform slip flow analysis method of the shear stress equation, the slip correction Reynolds equation and the gas film thickness equation based on elastohydrodynamic lubrication are established by deducing the local shear stress to calculate the slip velocity equation. The differences of the slip flow field between the non-uniform slip model and the traditional model and the evolution law of the circumferential non-uniform slip velocity are compared. The results show that the slip velocity distribution obtained by the non-uniform slip model is more consistent with the local Knudsen number. The maximum effect of the local slip on the gas film pressure is 10.6%, and the gas film pressure distribution is in good agreement with the experimental results. With the increase of the bearing number and eccentricity, slip sequentially occurs on the foil side and the shaft side. The slip regions expand from the minimum gas film thickness to both sides along the circumferential direction with continuously increasing slip velocity. The area of the slip region on the shaft side is up to twice as large as that on the foil side.

Key words: gas foil bearing, non-uniform slip flow, ultimate shear stress, slip velocity, gas film pressure

CLC Number: