• DocumentCode
    1026758
  • Title

    Selenium Power Rectifiers for A-C Aircraft Systems

  • Author

    Embry, Alvin L.

  • Author_Institution
    Design engineer, Tungar and metallic rectifier section, lighting engineering division, General Electric Company, West Lynn, Mass.
  • Volume
    64
  • Issue
    8
  • fYear
    1945
  • Firstpage
    596
  • Lastpage
    600
  • Abstract
    Increasing electric-power requirements for large aircraft have brought about the introduction of a-c power systems. Two major systems have been developed. In the first power is generated at variable frequency and converted to direct current; in the second power is generated at sub-stantially constant frequency, and both a-c and d-c power are used. In both systems selenium rectifiers can be used as converters. Rectifier units developed to supply 28.5-volt regulated d-c power, which include stepdown transformers and voltage-regulating equipment, are described in this paper. Ratings vary from 100 to 800 amperes.
  • Keywords
    Aircraft; Conductors; Design engineering; Frequency measurement; Induction generators; Instruments; Power generation; Power systems; Rectifiers; Time measurement;
  • fLanguage
    English
  • Journal_Title
    American Institute of Electrical Engineers, Transactions of the
  • Publisher
    ieee
  • ISSN
    0096-3860
  • Type

    jour

  • DOI
    10.1109/T-AIEE.1945.5059183
  • Filename
    5059183