A detachable multiaxial aircraft is related. The aircraft includes a fuselage and a number of lift arm assemblies. The lift arm assembly includes a landing chassis, an electric motor mounted on the landing chassis, and a propeller fixed on the electric motor. The lift arm assembly further includes a shell located on the landing chassis and surrounding the propeller. The fuselage includes a first connector, and the shell includes a second connector. The lift arm assembly is detachably connected to the fuselage by the first connector and the second connector.


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    Title :

    DETACHABLE MULTIAXIAL AIRCRAFT


    Contributors:

    Publication date :

    2019-06-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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