DocumentCode
1615276
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
fYear
2013
Firstpage
755
Lastpage
758
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);
fLanguage
English
Publisher
ieee
Conference_Titel
Chinese Automation Congress (CAC), 2013
Conference_Location
Changsha
Print_ISBN
978-1-4799-0332-0
Type
conf
DOI
10.1109/CAC.2013.6775835
Filename
6775835
Link To Document