• DocumentCode
    1369988
  • Title

    Unit equipments for aircraft electric power systems

  • Author

    Finison, H. J.

  • Author_Institution
    Armour Research Foundation of the Illinois Institute of Technology. Chicago, Ill.
  • Volume
    71
  • Issue
    3
  • fYear
    1952
  • fDate
    7/1/1952 12:00:00 AM
  • Firstpage
    145
  • Lastpage
    149
  • Abstract
    THE rapidly expanding use of electric apparatus on aircraft since 1940 has given emphasis to the development of new devices and machines of increased rating and reduced weight for aircraft electric power systems. Outstanding progress has been made in improved designs of reduced weight and space and increased performance and life. Much work still remains in device engineering to work continually toward further improvements as new materials and new techniques become available. Increase in aircraft operating demands will probably continue to mean electric power systems of increased size and improved reliability. These requirements will call for more work in development of devices of increased rating and performance. Still further, many of the devices currently used have not had the benefit of the improved design techniques and materials that are evident in some of the more advanced designs. Hence, it appears that engineering problems related to designs of individual devices ¿ device engineering ¿ will continue to be an important part of engineering for aircraft electric systems.
  • Keywords
    Aircraft propulsion; Airplanes; Assembly; Generators; Power systems; Voltage control;
  • fLanguage
    English
  • Journal_Title
    American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
  • Publisher
    ieee
  • ISSN
    0097-2185
  • Type

    jour

  • DOI
    10.1109/TAI.1952.6371216
  • Filename
    6371216