The present invention relates to a wing folding air-ground dual-purpose aircraft, which comprises a rack, double-side wings, propellers, an undercarriage, an engine, a power switching system, a transmission shaft and a transmission shaft engagement mechanism, wherein the power output by the engine can be switched between the propeller and the undercarriage tire through the power switching system so as to achieve purposes of flying and driving on the ground, the double-side wings can perform rotating inclining around the transmission shaft as the center so as to change the propeller propulsion force output direction and achieve vertical takeoff and parallel flying of the aircraft, and after landing, the double-side wings can achieve the connection of the propeller and the transmission shaft through the transmission shaft engagement mechanism, the wings can be folded toward the aircraft tail direction after the disconnecting, and the aircraft body narrows after the folding so as to drive on the ground. The wing folding air-ground dual-purpose aircraft the present invention has the following characteristics that the wings can rotate and can be folded so as to achieve vertical takeoff, and the output power can be switched, such that the aircraft can rapidly drive on the ground independent on the propeller rotation.


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    Titel :

    Wing folding air-ground dual-purpose aircraft


    Erscheinungsdatum :

    28.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60F VEHICLES FOR USE BOTH ON RAIL AND ON ROAD , Fahrzeuge für den Verkehr sowohl auf Schienen als auch auf Straßen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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