An electric aircraft is capable of vertically taking off and landing. The aircraft includes a fuselage, front and rear power units, power pods, main wings, ailerons, front landing gears, a tail wing and a rear landing gear. The power units include first and second electric duct groups. The first electric duct group includes two electric duct fans symmetrically and connected to two sides of a front portion of the fuselage respectively. The second electric duct group includes two electric duct fans symmetrically provided at two sides of a rear portion of the fuselage respectively. The power pods are configured to connect the fuselage to the first electric duct group. The two main wings are symmetrically and foldably connected to two sides of the fuselage respectively. The two ailerons are symmetrically connected to front ends of the two main wings respectively.


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    Titel :

    Electric vertical take-off and landing aircraft


    Beteiligte:
    WU TIANFENG (Autor:in)

    Erscheinungsdatum :

    23.01.2025


    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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