• DocumentCode
    1088963
  • Title

    Higher voltage aircraft power systems

  • Author

    Cotton, I. ; Nelms, A.

  • Author_Institution
    Univ. of Manchester, Manchester
  • Volume
    23
  • Issue
    2
  • fYear
    2008
  • Firstpage
    25
  • Lastpage
    32
  • Abstract
    Modern aircraft designs are focused on minimising the use of engine bleed air, eliminating gearboxes, and reducing the reliance on hydraulic systems. Instead, many of these mechanical systems will be replaced with electrical versions. The increasing amounts of electrical power that will be shipped through an aircraft means that it is increasingly difficult to rely on low voltage power systems owing to voltage drop and weight constraints. This discusses the challenges that relate to the safe use of higher voltage systems within aircraft.
  • Keywords
    aircraft power systems; high-voltage techniques; higher voltage aircraft power systems; low voltage power systems; voltage drop; Air gaps; Aircraft propulsion; Breakdown voltage; Cotton; Engines; Low voltage; Mechanical systems; Power demand; Power system reliability; Power systems;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/MAES.2008.4460728
  • Filename
    4460728