• DocumentCode
    1476745
  • Title

    Automatic temperature control for aircraft

  • Author

    Gund, R. A.

  • Author_Institution
    General Electric Company, Schenectady, N. Y.
  • Volume
    64
  • Issue
    10
  • fYear
    1945
  • Firstpage
    730
  • Lastpage
    734
  • Abstract
    AUTOMATIC temperature control for aircraft long has been neglected, and it is only during the war that adequate attention has been given to this important subject. The increased duties imposed upon flight personnel by the requirements of modern military aircraft, together with the necessity for reducing air drag to the minimum consistent with required cooling, have prompted aircraft designers to give consideration to automatic operation of cowl flaps, oil and coolant flaps, and intercooler doors. Automatic flap operation can be appreciated fully when it is considered that engine cowl flaps fully opened might represent an air drag as high as 40 miles per hour on a 400-mile-per-hour airplane.
  • Keywords
    Coils; Cooling; Heating; Relays; Temperature sensors; Thermostats;
  • fLanguage
    English
  • Journal_Title
    Electrical Engineering
  • Publisher
    ieee
  • ISSN
    0095-9197
  • Type

    jour

  • DOI
    10.1109/EE.1945.6441307
  • Filename
    6441307