• 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