The invention discloses an airphibious four-rotor aircraft. The airphibious four-rotor aircraft comprises four execution mechanisms and a driving deformation mechanism. The driving deformation mechanism comprises a driving motor, two driving shafts and two driven shafts. The driving shafts and the driven shafts are arranged on supporting seats, and the driving motor is provided with two motor output shafts; each motor output shaft is connected with the corresponding driving shaft through a coupler, and each driving shaft is connected with the corresponding driven shaft through a gear pair; and rotor supports of two execution mechanisms are connected with the two driving shafts respectively, and rotor supports of the other two execution mechanisms are connected with the two driven shafts respectively. Air-land double purposes of the four-rotor aircraft can be conveniently and rapidly achieved, and when the road is flat, the airphibious four-rotor aircraft can serve as a robot trolley to walk; when obstacles occur, the robot trolley can be transformed to the four-rotor aircraft to fly over the obstacles; and the two manners are switched for walking, energy consumption can be saved, and the cruising power of the aircraft can be improved.


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    Titel :

    Airphibious four-rotor aircraft


    Beteiligte:
    TANG CHAOQUAN (Autor:in) / MA BI (Autor:in) / ZHU HUA (Autor:in) / ZHOU GONGBO (Autor:in) / HU ERYI (Autor:in)

    Erscheinungsdatum :

    26.08.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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