• DocumentCode
    3151545
  • Title

    Electrical generation and distribution for the more electric aircraft

  • Author

    Avery, C.R. ; Burrow, S.G. ; Mellor, P.H.

  • Author_Institution
    Univ. of Bristol, Bristol
  • fYear
    2007
  • fDate
    4-6 Sept. 2007
  • Firstpage
    1007
  • Lastpage
    1012
  • Abstract
    The aircraft industry is developing the more electric aircraft (MEA) with an ultimate goal of distributing only electrical power across the airframe. The replacement of existing systems with electric equivalents has, and will continue to, significantly increase the electrical power requirement. This has created a need for the enhancement of generation capacity and changes to distribution systems. The higher powers will push distribution voltages higher in order to limit conduction losses and reduce cable size, and hence weight. A power electronic interface may be required to regulate generator output into the distributed power form.
  • Keywords
    aircraft; electric vehicles; power distribution; MEA; distribution systems capacity; electric aircraft; electrical distribution; electrical generation; power electronic interface; Aerospace electronics; Aircraft propulsion; Control systems; Distributed power generation; Engines; Power distribution; Power electronics; Power generation; Synchronous generators; Turbines; Aircraft Distribution; Aircraft Generation; More Electric Aircraft;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Universities Power Engineering Conference, 2007. UPEC 2007. 42nd International
  • Conference_Location
    Brighton
  • Print_ISBN
    978-1-905593-36-1
  • Electronic_ISBN
    978-1-905593-34-7
  • Type

    conf

  • DOI
    10.1109/UPEC.2007.4469088
  • Filename
    4469088