A propulsion and control propeller with thruster nozzles, primarily for aircraft application is described. Adjustability of rotor blades at the hub and pressurized gas expulsion combined with an air propeller increase power. Both characteristics are combined in one simple device, and, furthermore, incorporate overall aircraft control so that mechanisms which govern lateral and horizontal movement become superfluous.


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    Titel :

    Propulsion and Control Propellers with Thruster Nozzles Primarily for Aircraft Applications


    Beteiligte:
    W. Pabst (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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