In order to research the spherical spiral groove hybrid gas bearings
the nonlinear dynamic lubrication analysis mathematical model of spherical spiral groove hybrid gas bearings was established
based on the parameters of axis instantaneous position and instantaneous displacement speed. The transient perturbation pressure distribution of three-dimensional gas film
stiffness and damping coefficients were numerically computed were solved by using the combination of derivative integration and finite difference method. The influence law of speed
eccentricity ratio and supply pressure on the dynamic characteristics of gas film was researched. The results show that the influence of bearings supply pressure
speed and eccentricity ratio on the stiffness and damping coefficient of gas film was significant. The prediction model to estimate stability of rotor-bearing system was established
helping to predict the stability of bearings by applying Routh-Hurwitz stability criterion. The research provides the theoretical foundation for controlling actively the bearing running stiffness and damping and stemming the instability of gas film.
Linear stability model of rotating stall based on direct numerical techniques:PartⅡ——A simplified model and its applications
Linear stability model of rotating stall based on direct numerical techniques:Part Ⅰ—Theoretical model and algorithm
Design technology of a variable curvature blade type swirl distortion generator
Analysis of squeeze process and engagement characteristics of wet friction clutch
Dynamic performance of radial magnetic⁃gas bearing system
Related Author
HOU Rui-wei
SUN Xiao-feng
Xinyu ZHANG
Baofeng TU
Rui FANG
Guang YANG
Wei HUANG
Heyun BAO
Related Institution
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Helicopter Transmission,College of Mechanical and Electrical Engineering,Nanjing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Helicopter Transmission,Hunan Aviation Powerplant Research Institute,Aero Engine Corporation of China
National Key Laboratory of Science and Technology on Helicopter Transmission, Nanjing University of Aeronautics and Astronautics