Title :
High-efficiency control strategy of Aeronautical fuel pump motor
Author :
Minchi Kuang ; Jihong Zhu
Author_Institution :
Dept. of Comput. Sci. & Technol., Tsinghua Univ., Beijing, China
Abstract :
Aeronautical fuel pump motors require small size, large torque and high efficiency. In order to reduce the phase current and increase the efficiency of fuel pump motors, this paper takes surface-mount permanent magnet synchronous motor as research object and proposes a high-efficiency control strategy. This strategy reduces the impacts of armature reaction and harmonics in phase current. The experimental results show that the phase current is reduced and the efficiency of fuel pump motor is increased.
Keywords :
aerospace engines; electric current control; fuel pumps; machine control; permanent magnet motors; synchronous motors; aeronautical fuel pump motor; armature reaction; high-efficiency control strategy; phase current harmonics; phase current reduction; surface-mount permanent magnet synchronous motor; Armature; Fuel pumps; Harmonic analysis; Hysteresis motors; Permanent magnet motors; Voltage control; aeronautical fuel pump motor; armature reaction; harmonics; high-efficiency control; permanent magnet synchronous machine (PMSM);
Conference_Titel :
Chinese Automation Congress (CAC), 2013
Conference_Location :
Changsha
Print_ISBN :
978-1-4799-0332-0
DOI :
10.1109/CAC.2013.6775835