07 - Systems, Subsystems and Equipment
RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS
X. Hu¹, Y. Fu¹, D. Lyu¹, M. Sun¹, S. Zhao, Beijing Institute of Precision Mechatronics and Controls, Labora, China; J. Fu¹, J. Zhao¹; ¹School of Mechanical Engineering and Automation, Beihang Univers, China
This study focous on an integrated servo motor pump. Using the CFD method, we develop a thermal-fluid-magnetic coupled model for the motor pump, incorporating considerations for multiple losses and the oil-stirring effect of the piston pump. Through numerical solution, our investigation delves into the heat generation and heat transfer mechanisms of the motor pump under transient conditions.