This paper discusses aircraft control power requirements provided by lift fan systems. Gas power transfer is described and estimated performance presented. A performance comparison is made between the thrust spoiling system used in the present Army XV-5A flight research vehicle and a gas power transfer system. Gas power can provide adequate aircraft control forces. Thrust spoiling is not needed for fan dynamic response, use of a phase lead network in the control circuit of a gas power transfer system can provide sufficiently rapid fan dynamic response.


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    Titel :

    LIFT FAN PROPULSION SYSTEMS V/STOL AIRCRAFT CONTROL


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    BEELER, E. F. (Autor:in) / VOLK, L. J. (Autor:in)

    Kongress:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1965



    Erscheinungsdatum :

    1965-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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