The invention relates to a protective cover of a multi-rotor aircraft. The protective cover is installed on a central disc of an aircraft. The protective cover comprises a cover body with an arc-shaped cross section. The bottom surface of the cover body is equipped with flanges. A main control system in the central disc is prevented from contact with water, a protection function is achieved, and the service life of the aircraft is prolonged.


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    Title :

    Protective cover of multi-rotor aircraft


    Contributors:
    SUN XIKUO (author) / SUN XIYI (author)

    Publication date :

    2015-09-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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