An aircraft 8 comprises an elongate fuselage 2 for containing cargo or passengers. The fuselage 2 comprises a lower floor and an upper ceiling and opposing fuselage sides extending between the ceiling and floor. The fuselage sides each comprise at least one door 10 which can be selectively opened and closed. The fuselage is divided into multiple zones between the fore and aft of the aircraft, each zone being associated with one of said doors adjacent to said zone and wherein the doors alternate in position between sides of the aircraft such that adjacent zones from fore to aft of the aircraft are associated with a door on an opposing side of the aircraft. The aircraft may be of VTOL type, be electrically powered, and have six wings 12,13,14.


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    Titel :

    Electric vertical take-off and landing vehicle


    Beteiligte:
    FURQAN (Autor:in) / MALCOLM FOSTER (Autor:in) / CALEB RHODES (Autor:in) / LEWIS CHATWIN (Autor:in) / AURELIE GODIN (Autor:in) / LIAM PANG (Autor:in) / ADRIAN MARSLAND (Autor:in) / JONATHAN EVANS (Autor:in) / TED TOMBLIN (Autor:in)

    Erscheinungsdatum :

    05.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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