A concept for an advanced aircraft power system was identified that uses 20-kHz, 440-V, sin-wave power distribution. This system was integrated with an electrically powered flight control system and with other aircraft systems requiring secondary power. The resulting all-electric secondary power configuration reduced the empty weight of a modern 200-passenger, twin-engine transport by 10 percent and the mission fuel by 9 percent.


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    Titel :

    Advanced secondary power system for transport aircraft


    Beteiligte:
    Hoffman, A. C. (Autor:in) / Hansen, I. G. (Autor:in) / Beach, R. F. (Autor:in) / Plencner, R. M. (Autor:in) / Dengler, R. P. (Autor:in) / Jefferies, K. S. (Autor:in) / Frye, R. J. (Autor:in)

    Erscheinungsdatum :

    01.05.1985


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch