The invention belongs to the technical field of aircrafts, and discloses a canard high-speed tilting rotor aircraft and a control method thereof.The canard high-speed tilting rotor aircraft comprisesan aircraft body, a front canard, a rear wing, a front rotor, a rear tilting rotor and a tilting mechanism; wherein the front canard and the front rotor are mounted at the front part of the aircraft body,, the front rotor is mounted in a through hole of the front canard, and the rear wing is mounted at the rear part of the aircraft body; and the rear tilting rotor wing is arranged at the rear partof the gravity center of the aircraft body through the tilting mechanism and is positioned in front of the rear wing. Compared with helicopters, autorotorcrafts and multi-rotor aircrafts, the tilt angle of a tilting thrust rotor is adjusted, so that the attitude of the aircraft body does not need to be additionally tilted in flight, and the front rotor on the front canard is closed in a flat flight mode to form a canard type fixed-wing aircraft, so that the forward flight resistance is small, and the speed is remarkably increased; in a flat flight mode, the thrust comes from the backward tilting rotor, the diameter of the rotor is smaller than that of a tilting rotor aircraft, the resistance is small during forward flight, and the speed is higher.

    本发明属于飞行器技术领域,公开了一种鸭翼高速倾转旋翼飞行器及其操纵方法,包括:机身、前鸭翼、后机翼、前旋翼、后倾转旋翼、倾转机构;所述前鸭翼和前旋翼安装在机身的前部,其中前旋翼安装在前鸭翼的通孔内,所述后机翼安装机身的后部;所述后倾转旋翼通过倾转机构安装在机身重心后部,且位于后机翼之前。相对直升机类、自转旋翼机类、多旋翼类飞行器,通过调节倾转推力旋翼的倾斜角使得飞行中机身姿态无需额外倾斜,并且平飞模式下前鸭翼上的前旋翼关闭形成鸭翼式固定翼飞行器,前飞阻力小,速度提高显著;本发明在平飞模式下推力来自于后倾转旋翼,其旋翼直径相对倾转旋翼飞行器较小,在前飞时阻力小,速度更快。


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    Titel :

    Canard high-speed tilting rotor aircraft and control method thereof


    Weitere Titelangaben:

    一种鸭翼高速倾转旋翼飞行器及其操纵方法


    Beteiligte:
    LIU YANTAO (Autor:in) / XU JINGHAI (Autor:in) / ZENG JIAGANG (Autor:in) / CAO YUANBAO (Autor:in) / SUN QIANG (Autor:in) / ZHONG WEIGUI (Autor:in) / TIAN XU (Autor:in) / XIE WANG (Autor:in) / LIU YI (Autor:in) / YING MINGAN (Autor:in)

    Erscheinungsdatum :

    16.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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