Spray orientation parameters influencing lubrication initial conditions of gear meshing point were systematic definied through the analysis of spray lubrication process of aero spur gears
then the computational fluid dynamics(CFD) method of spray lubrication process was established. Three kinds of spray parameter including spray angle
spray point position and spray distance were calculated
jet states were obtained with different meshing instantaneous of gears. The varying rules of the oil/air ratio and oil/air total pressure at the entrance of contact point were compared in the meshing process under different spray parameters.Result show that
nozzle should offset a small angle to driving wheel when spray lubrication using engaging-in side in order to get better lubricating effect
and spray point position should offset engaging-in side
spray distance should take into account the structure
Unsteady aerodynamic interactions of contra rotating propeller
Impacts of propeller installation effect on aerodynamic performances for UAV
Effects of mainstream angles of attack on film cooling characteristics of double-jet film cooling holes
Numerical investigation on trailing edge jet and boundary layer ingestion in distributed propulsion system
Research on oil-air multiphase flow of spray lubrication of aero spur gears
Related Author
YANG Xiao
WANG Xuechen
WANG Fengming
TANG Sijia
YAN Wenhui
LI Jie
SHI Wenbo
ZHANG Ke
Related Institution
Department of Precision Instruments, School of Mechanical Engineering, Tsinghua University
The Advanced Aviation Power Innovation Institute
Huiyang Aviation Propeller Company Limited, Aviation Industry Corporation of China, Limited
School of Mechanical and Materials Engineering, North China University of Technology
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics