Title :
Control method of dual-channel hybrid excitation doubly salient starter/generator
Author :
Qiji Ze ; Deliang Liang ; Qiming Sun
Author_Institution :
State Key Lab. of Electr. Insulation & Power Equip., Xi´an Jiaotong Univ., Xi´an, China
Abstract :
Aeronautic starter/generator System is the key technology of aircraft electric power system of more electric aircraft(MEA) and all electric aircraft(AEA), which can effectively improve the efficiency and environmental protection property of hybrid vehicles. Base on the analysis of the principle of a dual-channel hybrid excitation doubly salient machine, this paper selects asymmetrical half-bridge topology and H-bridge topology to control it. Furthermore, a co-simulation model of finite element model and control system was made to analyze two topologies with Maxwell 2D module and Simplorer module in Ansoft. By comparing steady performances when the starter-generator operating at the single channel mode and the dual-channel mode with different turn-on and turn-off angles, the paper provided reference for further experiment and industry application.
Keywords :
electric generators; finite element analysis; machine control; rotors; starting; stators; AEA; Ansoft; H-bridge topology; MEA; Maxwell 2D module; Simplorer module; aeronautic starter-generator system; aircraft electric power system; all electric aircraft; asymmetrical half-bridge topology; cosimulation model; dual-channel hybrid excitation doubly salient machine; dual-channel mode; environmental protection property; finite element model; hybrid vehicles; more electric aircraft; single channel mode; turn-off angles; turn-on angles; Couplings; Generators; Reluctance motors; Rotors; Topology; Torque; Windings; Asymmetrical Half-bridge; Co-simulation Model; Dual-Channel Hybrid Excitation Doubly Salient Starter/Generator; Full-Bridge;
Conference_Titel :
Ecological Vehicles and Renewable Energies (EVER), 2014 Ninth International Conference on
Conference_Location :
Monte-Carlo
Print_ISBN :
978-1-4799-3786-8
DOI :
10.1109/EVER.2014.6844104