The simultaneous solution of the generalized Reynolds equation
three-dimensional energy equation
three-dimensional heat transfer equation and force equilibrium equation were presented and the changes of the lubricant viscosity and density with the temperature and pressure were taken into account.Consequently
the three-dimensional temperature field was obtained with the heat flux continuity condition imposed at the interface between the oil film and the bush.The result show that the maximum temperature did not appear at the interface between the film and bush and the point of the maximum temperature was different along the film thickness direction at different circumferential locations.The differences of the bearing performances were validated between the three-dimensional temperature model and the two-dimensional temperature model.A Newton-Raphson approach was used in solving the generalized Reynolds equation and the force balance equations
simultaneously.For the energy equation and the heat transfer equation
the finite difference method was carried out with the help of a sweeping scheme.The approaches we used were found to be fast converged and saved computing time greatly.
Analysis of thermal characteristics of oil⁃cooled aviation wet friction clutch
Thermal characteristics for bearing combined EHL theory with CFD method
Fretting wear of discontinuous interface considering centrifugal force and thermal stress
Study on thermometry of leading edge of rotating turbine blade by thermochromic liquid crystal
Anisotropic heat transfer model of finger seal based on porous media
Related Author
Weidi KONG
Wuzhong TAN
Wei HUANG
Rupeng ZHU
Heyun BAO
ZHAO Zhiqiang
WANG Tao
LU Fengxia
Related Institution
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