In order to accurately predict the thermal characteristics of angular contact ball bearing in the transmission system under spray lubrication
the bearing thermal elastohydrodynamic lubrication (EHL) model was established
and the micro-contact interface load and friction coefficient between the raceway and ball were obtained. On the basis
heat generation was calculated by using the local generation. Computational fluid dynamics (CFD) method was used to establish a coupled oil-gas two-phase flow model for angular contact ball bearings
including the choice of turbulence model and fluid domain boundary conditions. Furthermore
fuel injection speed
nozzle position and gas fraction were analyzed. Results showed that the application of CFD method with accurate heat generation calculated by the thermal EHL theory could predict the optimal injection speed
the nozzle position and gas fraction of the bearing under various operating conditions
lubrication parameters and geometric parameters. When the injection speed was 5 m/s
the maximum temperature of the bearing chamber was decreased by 440% compared with other injection speeds. When the nozzle position was below the bearing axis
the maximum temperature of the bearing chamber decreased by 430% compared with other positions. When gas fraction was 15%
the maximum temperature of the bearing chamber was improved by 157% compared with other gas fraction.
Evolutionary regularity of dynamic characteristics for precision angular contact ball bearing under combined loads
Analysis of thermal characteristics of oil⁃cooled aviation wet friction clutch
Analysis of oil⁃off tolerance of angular contact ball bearing under condition of high speed and heavy load
Oil atomization analysis of jet lubrication for high speed angular contact ball bearing
Fretting wear of discontinuous interface considering centrifugal force and thermal stress
Related Author
Mingkai WANG
Ke YAN
Shuaijun MA
Jun HONG
Heyun BAO
Weidi KONG
Wuzhong TAN
Wei HUANG
Related Institution
Key Laboratory of Education Ministry for Modern Design and Rotor⁃Bearing System,Xi'an Jiaotong University
National Key Laboratory of Science and Technology on Helicopter Transmission, 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
Harbin Bearing Company Limited,Aero Engine Corporation of China
Ministry of Industry and Information Technology Key Laboratory of Aerospace Bearing Technology and Equipment,Harbin Institute of Technology