The invention discloses a rotorcraft using a control surface to control attitude. The rotorcraft comprises a body, a rotor and an engine, the engine is fixedly connected to the body, a rotor disc, a steering engine and a small rudder are further fixedly arranged on the body, the rotor is arranged in the rotor disc and fixedly connected with a rotating shaft of the engine, and the steering engine and the small rudder are arranged near the edge of the rotor disc. The rotorcraft has the advantages of higher aerodynamic efficiency, less power consumption and longer flight time; the structure is simple, and automatic and intelligent control is easy to achieve; and a translational flight mode is provided, so that accurate positioning in suspension is more convenient.

    本发明公开了一种使用舵面控制姿态的旋翼飞行器,包括机体、旋翼、发动机,所述发动机固定连接在机体上,所述机体上还固定设置有旋翼盘、舵机和小舵,所述旋翼设置于所述旋翼盘内、与发动机的转轴固定连接在一起,所述舵机和小舵设置于旋翼盘的边缘附近。本发明具有更高的气动效率,耗电更少、飞行时间更长;而且结构较为简单,容易实现自动、智能的控制;并且有平移的飞行模式,更方便在悬浮中准确地定位。


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    Titel :

    Rotorcraft using control surface to control attitude


    Weitere Titelangaben:

    一种使用舵面控制姿态的旋翼飞行器


    Beteiligte:
    DAI JIN (Autor:in)

    Erscheinungsdatum :

    05.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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