The invention relates to an aircraft with wind ball driven wind wheels at wing leading edges, belonging to the technical field of aviation aircrafts. The aircraft 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 and right sides of a longitudinal symmetric plane of the fuselage. The left wing comprises a left wind wheel, a left wind ball, a left fixed wing, a left flap and a left aileron; the right wing comprises a right wind wheel, a right wind ball, a right fixed wing, a right flap and a right aileron. Under the action of forwards-coming flow, the left wind ball and the right wind ball can rotate, a majority of the forwards-coming flow is lifted to the upper surfaces of the left and right wings and is accelerated to run back, and thus, a lifting force generated by the left and right wings is greatly increased. The aircraft disclosed by the invention can achieve STOL (Short Take Off and Landing) and is maneuverable and flexible in flight.


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    Titel :

    Aircraft with wind ball driven wind wheels at wing leading edges


    Beteiligte:
    WANG ZHICHENG (Autor:in)

    Erscheinungsdatum :

    22.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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