• DocumentCode
    3357055
  • Title

    Progress in electrically-propelled aircraft

  • Author

    Colyer, R.E.

  • Author_Institution
    Cranfield Univ., Swindon
  • fYear
    2007
  • fDate
    10-12 Sept. 2007
  • Firstpage
    357
  • Lastpage
    362
  • Abstract
    In recent years, the performance of electrical drives and power sources has increased to an extent that they have now become viable as propulsion systems for aircraft. Whilst they are unlikely to be applicable to commercial airliners in the foreseeable future, a number of smaller aircraft are under development or have already been produced. The paper examines the advantages (and disadvantages) of the use of electric propulsion and compares an electric drive using currently available components with one employing a conventional internal combustion engine. It then considers a number of examples of aircraft using electrical propulsion and discusses their particular features. It is concluded that on weight and cost most electrical propulsion systems still cannot compete with conventional systems but other factors may override this disadvantage and further expected improvements in electrical system components should see them increasingly employed in the future.
  • Keywords
    aerospace propulsion; electric drives; electric propulsion; electrical drives; electrically-propelled aircraft; internal combustion engine; propulsion systems; Aircraft propulsion; Batteries; Costs; Europe; Fuel cells; Fuel storage; Hydrogen; Internal combustion engines; NASA; Unmanned aerial vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electrical Machines and Power Electronics, 2007. ACEMP '07. International Aegean Conference on
  • Conference_Location
    Bodrum
  • Print_ISBN
    978-1-4244-0890-0
  • Electronic_ISBN
    978-1-4244-0891-7
  • Type

    conf

  • DOI
    10.1109/ACEMP.2007.4510529
  • Filename
    4510529