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:
    A. C. Hoffman (Autor:in) / I. G. Hansen (Autor:in) / R. F. Beach (Autor:in) / R. M. Plencner (Autor:in) / R. P. Dengler (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    38 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch