An aircraft includes a fuselage and a pair of channel wings which may vary incidence with respect to the fuselage and a pair of channel canards which can also vary incidence with respect to the fuselage and that can move independently of each other for the purpose of vertical takeoff and landing as well as forward and reverse flight. The wings may have multiple channels and may be powered by single propeller or contra-rotating propellers. The thrust to the propellers may be provided with an internal combustion engine or electric motors or a turbo prop or hybrid system. The channel wing allows the fuselage to maintain a level pitch with respect to the horizon. The aircraft will also have increased maneuverability in hover because it can independently vary the incidence of the wings and canards and be able to tightly turn about a point.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft having independently variable incidence channel wings with independently variable incidence channel canards


    Beteiligte:

    Erscheinungsdatum :

    2020-06-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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






    VERTICAL TAKE-OFF AIRCRAFT WITH CANARDS AND PRIMARY WINGS

    BECCHI PAOLO | Europäisches Patentamt | 2022

    Freier Zugriff

    Variable Incidence Wing Aircraft having a Wing Stowage Mode

    IVANS STEVEN RAY / GRONINGA KIRK LANDON | Europäisches Patentamt | 2023

    Freier Zugriff