The invention provides a fixed-wing electric aircraft capable of vertically taking off and landing, which is characterized in that lifting force provided by a large-diameter vertical rotor wing (1) can bear the weight of the whole aircraft, two tilting small-diameter front rotor wings (3) mounted at two ends of a fixed main wing (21), two tilting small-diameter rear rotor wings (4) mounted at two ends of a horizontal tail wing (23), and a fixed main wing (22) mounted at two ends of the horizontal tail wing (23), the structural design is high in reliability, the large-diameter rotor wing is high in propelling efficiency, the motor power is reduced, and electricity is saved.

    本发明提出了一种可垂直起降的固定翼电动飞行器,由一个大直径的垂直旋翼(1)提供的升力可承担整机重量,安装在固定主翼21两端的两可倾转的小直径前旋翼3,以及安装在水平尾翼23两端的两可倾转的小直径后旋翼4,承担重心平衡微调整以及水平飞行推力,这样的结构设计可靠性高,大直径旋翼推进效率高,降低电机功率,又省电。


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    Titel :

    Fixed-wing electric aircraft capable of vertically taking off and landing


    Weitere Titelangaben:

    可垂直起降固定翼电动飞行器


    Erscheinungsdatum :

    07.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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