The invention discloses an aircraft with the leading edge provided with wind balls for driving wind wheels, and belongs to the technical field of aircrafts. The aircraft comprises an aircraft body, a power device, a left wing, a right wind, an empennage and an undercarriage. The left wing and the right wing are the same in structure and size and are symmetrically arranged on the left and right sides of the longitudinal symmetric face of the aircraft body. The left wing comprises a left motor, a left clutch, a left wing shaft, the left wind wheel, the left wind ball, a left fixed wing and a left auxiliary wing. The right wing comprises a right motor, a right clutch, a right wing shaft, the right wind wheel, the right wind ball, a right fixed wing and a right auxiliary wing. The left wind ball and the right wind ball are driven by coming flow in front or driven by the left motor and the right motor to rotate. A majority of the coming flow in front is lifted to the upper surface of the left wing and the upper surface of the right wing and accelerated to flow backwards, and lift force generated by the left wing and the right wing is greatly increased. The aircraft can achieve short-distance taking off and landing and flexible in flying.


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    Title :

    Aircraft with leading edge provided with wind balls for driving wind wheels


    Contributors:

    Publication date :

    2015-07-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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