The invention relates to a single-rotor aircraft and a control method thereof, and belongs to the technical field of aircrafts. A single-rotor aircraft comprises a fuselage and wings, and is characterized in that the fuselage comprises an upper-stage fuselage and a lower-stage fuselage, and the upper-stage fuselage and the lower-stage fuselage are fixedly connected through a net-shaped connecting structure; the lower-stage fuselage comprises a cylindrical duct, a duct fan is mounted in the duct, four steering engines are mounted at the tail of the duct, and each steering engine is connected with a rudder blade; metal regulators are installed on the upper-level fuselage and the lower-level fuselage, and the upper-level fuselage and the lower-level fuselage are fixedly connected through carbon rods penetrating through the metal regulators on the upper-level fuselage and the lower-level fuselage. Meanwhile, the invention provides a control method of the single-rotor aircraft.

    本发明涉及一种单旋翼飞行器及其控制方法,属于飞行器技术领域。一种单旋翼飞行器,包括机身和机翼,其特殊之处在于,所述机身包括上级机身和下级机身,上级机身和下级机身之间通过网状的连接结构固定连接;所述下级机身包括筒状的涵道,涵道内安装涵道风扇,所述涵道的尾部安装四个舵机,每个舵机连接一个舵叶;上级机身和下级机身上安装有金属调节器,穿过上级机身和下级机身上的金属调节器的碳棒将上级机身和下级机身固定连接。同时,提供该单旋翼飞行器的控制方法。


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    Title :

    Single-rotor aircraft and control method thereof


    Additional title:

    一种单旋翼飞行器及其控制方法


    Contributors:
    LI SIZHE (author) / CHU BAIXING (author) / LU JINGZHI (author) / WANG JIAYU (author) / SONG CHANG (author)

    Publication date :

    2024-10-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen



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