An electrically or hybrid powered multirotor aircraft with complete redundancy on all of its functions of lift, of propulsion, and of control, the aircraft having optimized energy consumption and comprising: a longitudinal structure having two longitudinal beams; a fuselage fastened to the longitudinal structure; two fixed wings serving essentially to provide the aircraft with lift in cruising flight and arranged at respective ends of the longitudinal structure and in a common first plane; at least six rotors serving essentially to provide the aircraft with lift during stages of takeoff and landing, the rotors being arranged in a common second plane distinct from the first plane and parallel to the first plane in such a manner as not to be situated vertically above or below a fixed wing; and two propulsion propellers. An electrical or hybrid power plant serves to drive the rotors and the propulsion propellers in rotation.


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    Title :

    AERONEF MULTIROTOR A MOTORISATION ELECTRIQUE OU HYBRIDE AVEC UNE CONSOMMATION ENERGETIQUE OPTIMISEE


    Additional title:

    MULTIROTOR AIRCRAFT WITH HYBRID OR ELECTRIC ENGINE WITH OPTIMISED ENERGY CONSUMPTION
    LUFTFAHRZEUG MIT MEHREREN ROTOREN UND ELEKTRO- ODER HYBRIDMOTOR MIT OPTIMIERTEM ENERGIEVERBRAUCH


    Contributors:

    Publication date :

    2021-01-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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