• DocumentCode
    1346538
  • Title

    Experimental determination of 400-cycle impedance of wire in aircraft power distribution circuits

  • Author

    Andrew, J. D.

  • Author_Institution
    Douglas Aircraft Corporation, Santa Monica, Calif.
  • Volume
    73
  • Issue
    6
  • fYear
    1955
  • Firstpage
    469
  • Lastpage
    478
  • Abstract
    THE measurement of impedance of power distribution circuits is a continuing problem as long as materials, installation methods, and ultimate use of such circuits are constantly undergoing changes. In contrast to transmission lines, power distribution circuits are relatively short and operate at utilization voltages. This simplifies the impedance measuring problem because the effects of capacitance and leakage are negligible at power frequencies. Consequently, the literature shows that the analysis of the problem has been thorough and measurement techniques have been painstaking; however, the measurements have usually been made at 60 cycles and, in the case of 3-phase measurements a neutral wire or earth return has been used. The 3-phase 4-wire electric systems rapidly being developed for aircraft in this country are operated at 400 cycles, and the neutral return is made through the aircraft structure, particularly the conducting aluminum skin. For increased physical reliability, the wire used in aircraft distribution circuits has a different construction than that commonly used in other applications. These differences are sufficient to hinder the use, even by extrapolation, of the results of much research on the general problem of wire impedance measurement.
  • Keywords
    Aircraft; Conductors; Impedance; Power cables; Resistance; Skin; Wires;
  • 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.1955.6367101
  • Filename
    6367101