The present invention pertains to the technical field of electrically powered aircraft. According to the present invention, such an electrically powered aircraft (1) is required to comprise at least one non-retractable main landing gear (2a, 2b), wherein said main landing gear (2a, 2b) comprises a wheel (3) and linkage kinematics (4) for attaching said wheel (3) to a structural component (5) of said aircraft (1), and wherein said structural component (5) supports and transmits the loads exerted by the main landing gear (2a, 2b) to a fuselage of the aircraft (1) as well as performs an aerodynamic stability function.


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    Title :

    ELECTRICALLY POWERED AIRCRAFT


    Additional title:

    ELEKTRISCH ANGETRIEBENES FLUGZEUG
    AVION ÉLECTRIQUE


    Contributors:

    Publication date :

    2023-05-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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