The invention belongs to the technical field of aerospace vehicles, and relates to an airplane provided with wind-ball-driving wind wheels on main lift force front edges. The airplane comprises a fuselage, a power device, a left wing, a right wing, an empennage and an undercarriage. The left wing and the right wing are the same in structure and size and are symmetrically arranged at the left side and the right side of the longitudinal symmetrical face of the fuselage. The left wing comprises a left motor, a left clutch, a left wing shaft, the left wind wheel, a left wind ball, a left fixed wing, a left flap and a left aileron. The right wing comprises a right motor, a right clutch, a right wing shaft, the right wind wheel, a right wind ball, a right fixed wing, a right flap and a right aileron. The left wind ball and the right wind ball rotate under driving of front incoming flow or the left motor and the right motor, most of the front incoming flow is lifted to the upper surface of the left wing and the upper surface of the lower wing and accelerates rear flow, and lift force generated by the left wing and the right wing is greatly increased. The airplane can take off and land within a short distance and is maneuverable and flexible in flight.


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    Titel :

    Airplane provided with wind-ball-driving wind wheels on main lift force front edges


    Beteiligte:
    WANG ZHICHENG (Autor:in)

    Erscheinungsdatum :

    08.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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