A system and method to control flight of an aircraft. The aircraft having an engine with a rotatably nozzle assembly configured to create forward propulsion and yaw control of the aircraft. The engine exhaust passing through the nozzle is redirected with a valve disposed within the nozzle. Lift is created with a lift system carried by the wing of the aircraft. Additional lift is created during flight with a retractable wing extension disposed within the fixed wing of the aircraft.


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    Titel :

    AIRCRAFT WING EXTENSION AND NOZZLE SYSTEM


    Weitere Titelangaben:

    RALLONGE D'AILE D'AERONEF ET SYSTEME DE TUYERES


    Beteiligte:

    Erscheinungsdatum :

    2015-03-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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