Analytical model was presented for a novel laminated gas foil thrust bearing. The performance of this thrust bearing was studied by coupling the foil deformation equation and the compressible gas-lubricated Reynolds equation solved by finite difference method(FDM). Due to the variable stiffness characteristic in radial direction and circumferential direction of supported foils
the second wedging effect phenomenon and two pressure peaks were found
and the load capacity was improved compared with traditional gas foil thrust bearings. Bearing load capacity
friction torque and dynamic stiffness all declined with the decrease of minimum film thickness
but dynamic damping changed very little. There was optimum height of wedge to obtain higher load capacity and lower torque
which reduced the loss. Meanwhile
higher dynamic stiffness and higher dynamic damping can be achieved at the optimum height of wedge.
Analysis of squeeze process and engagement characteristics of wet friction clutch
Dynamic performance of radial magnetic⁃gas bearing system
Numerical modelling of elastic ring squeeze film damper based on thick plate and force coefficient identification
A calculation method for solution of discharge coefficients in aerostatic bearing
组合式弹性金属密封泄漏特性实验研究与结构优化
Related Author
Wei HUANG
Heyun BAO
Chu ZHU
Rupeng ZHU
Zhenyu XIE
Licheng CHEN
Jiansheng HAO
Yan WU
Related Institution
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