The invention discloses an electric vertical wing tilting four-rotor aircraft which comprises an aircraft body, the aircraft body is connected with a cockpit control room, a battery compartment bag, an external universal warehouse, a main wing and an empennage, the side portion of the empennage and the side portion of the main wing are connected with a horizontal rudder and the empennage respectively, the main wing is connected with a tilting vertical wing through a tilting disc, the tilting vertical wing is connected with a vertical rudder, and the vertical rudder is connected with a horizontal rudder. The tilting vertical wing is connected with a motor, and the motor is connected with a rotating wing. The unmanned aerial vehicle has the beneficial effects that the effects of full-power vertical take-off and landing and full-power horizontal flight are achieved in the aspect of power use; the flight speed of the aircraft is effectively improved, and the high-speed requirement of people on the aircraft is met; the safety of the aircraft during falling is effectively improved, and the crash probability and the casualty risk are effectively reduced.

    本发明公开一种电动垂直翼倾转四旋翼飞行器,包括机体,机体连接有驾驶舱控制室、电池仓包、外部通用货仓、主翼、尾翼,尾翼、主翼的侧部分别连接有水平方向舵,尾翼、主翼通过倾转圆盘连接有倾转垂直翼,倾转垂直翼连接有垂直方向舵,倾转垂直翼连接有电动机,电动机连接有旋转翼。有益效果:在动力使用方面实现了全动力垂直起降与全动力水平飞行的效果;有效提高飞行器的飞行速度,满足了人们对飞行器高速的需求;有效提高飞行器坠落时的安全性,有效减小坠毁几率和伤亡风险。


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    Titel :

    Electric vertical wing tilting four-rotor aircraft


    Weitere Titelangaben:

    一种电动垂直翼倾转四旋翼飞行器


    Beteiligte:
    HE FUKAI (Autor:in)

    Erscheinungsdatum :

    2023-10-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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