An electric vertical take-off and landing aircraft having a disc-shaped blended wing-body that houses power sources and controls. Thrust pod arms are attached to the blended wing-body and each arm has a one of a set of thruster pairs. An ingress/egress hatch is attached to the rear surface. Navigation and strobe lights are located on the outside edge. Front landing gear is attached to the upper surface including pair of parallel motor pod struts. Main landing gear is attached proximate the trailing edge and a set of right and left elevons is attached to the rear surface proximate the main landing gear. A cockpit area including a viewing window is formed on the blended-wing.


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    Titel :

    ELECTRIC VERTICAL TAKE-OFF AND LANDING BLENDED WING-BODY ARICRAFT


    Beteiligte:
    TIBBITTS STEPHEN (Autor:in) / GOULD BEN (Autor:in)

    Erscheinungsdatum :

    2021-08-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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