• DocumentCode
    2882985
  • Title

    Power electronics for aircraft application

  • Author

    Taha, Mohamad H.

  • Author_Institution
    Lucas Areosp., Hemel Hempstead, UK
  • fYear
    1999
  • fDate
    1999
  • Firstpage
    42552
  • Lastpage
    42555
  • Abstract
    Advancements in power electronics technologies have been used widely in the aerospace industry. Lucas Aerospace provides a variable frequency voltage for most of the internal power system in the aircraft, however some components may be required to be operated with DC or fixed frequency voltage. An aircraft power conditioning system is shown. It consists of a variable frequency generator. A part of the output of the generator is rectified to provide low voltage (usually 28 V) and high voltage DC. The high voltage is inverted again to give 115 V RMS, 400 Hz constant frequency. This paper presents a research project which is aimed at producing a high power variable frequency to constant frequency converter. Simulation results are presented and compared with the international standard specifications
  • Keywords
    aircraft power systems; 115 V; 28 V; 400 Hz; AC/DC/AC converters; Lucas Aerospace; aircraft application; aircraft power conditioning system; fixed frequency voltage; high voltage inverter; internal power system; international standard specifications; power electronics; rectification; variable frequency generator; variable frequency to constant frequency converter; variable frequency voltage;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Power Electronics for Demanding Applications (Ref. No. 1999/059), IEE Colloquium on
  • Conference_Location
    London
  • Type

    conf

  • DOI
    10.1049/ic:19990332
  • Filename
    771888