The invention discloses a multi-rotor-wing aircraft stander. The multi-rotor-wing aircraft stander comprises a machine body and a cantilever, and is characterized in that when the stander is horizontally arranged, the outer contour of the cross section of the cantilever is of a polygon with an angle facing upwards; a biosector of an upward-facing angle is perpendicular to the horizontal plane; in order to prevent the stander from cutting hands, the polygon is a round-angle polygon; the polygon is a regular polygon; the polygon is an odd-number polygon; the odd-number polygon is a triangle or a pentagon. The multi-rotor-wing aircraft stander has beneficial effect that the air resistance of an aircraft in the flying process can be reduced.


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    Title :

    Multi-rotor-wing aircraft stander


    Contributors:
    YONG CHANGMING (author) / LI YALAN (author)

    Publication date :

    2015-05-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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