The invention discloses an amphibious individual aircraft. The amphibious individual aircraft comprises a support, wherein the support comprises three supporting legs arranged in an isosceles triangle; the upper ends of the supporting legs are fixedly connected with a fixed plate respectively; the two supporting legs which are positioned on the bottom edge are respectively connected with front wheels; the supporting leg positioned at an apex angle is connected with a rear driving wheel; a main body box is mounted on the fixed plate; air channels are respectively arranged on two sides of the main body box; an engine is mounted in the main body box; a power output shaft of the engine penetrates through a gearbox and is connected with a stepless gearbox; two output shaft ends are arranged at each of two ends of the stepless gearbox; first jaw clutches are respectively mounted at the output shaft ends. The amphibious individual aircraft disclosed by the invention is stable and reliable in structure, and compact in integral design. Through the cooperation of the first jaw clutches and second jaw clutches with the stepless gearbox, the conversion between an overland walking mode and a free flight mode can be realized, so that the integral practicability of the aircraft is improved.


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    Title :

    Amphibious individual aircraft


    Contributors:
    ZHAO YANJUN (author) / GE WENQING (author) / WANG YING (author) / LI DONGYING (author)

    Publication date :

    2016-01-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60F VEHICLES FOR USE BOTH ON RAIL AND ON ROAD , Fahrzeuge für den Verkehr sowohl auf Schienen als auch auf Straßen



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