The invention belongs to the technical field of aviation aircrafts, and discloses a multi-rotor integrated aircraft and a flight control method.The multi-rotor integrated aircraft is composed of an aircraft body, integrated wings, a flight control system and a power system; vertical take-off and landing, low-speed flight and hovering of the aircraft can be achieved like a multi-rotor aircraft, the aircraft can also fly like a fixed wing, multi-rotor flight and fixed wing flight state conversion is completed by controlling the elevation angle of the integrated wing, the endurance is improved by additionally arranging the large foldable fixed wing, and the economic performance of the aircraft is improved. The vector thruster is additionally arranged to improve the maneuvering performance of the aircraft, the integrated wings are designed to be of a foldable structure, storage and transportation are facilitated, and the aircraft can be controlled to do lifting, left-right steering, front-back translation, left-right translation and other motions under the condition that a single integrated wing is not provided with a power adapter through the design that a rudder is additionally arranged on each integrated wing.

    本发明属于航空飞行器技术领域,公开了一种多旋翼集成飞行器与飞行控制方法,飞行器由机体、集成机翼、飞控系统、动力系统组成,在机体上至少设置两组纵列式集成机翼,既可以像多旋翼飞行器一样解决飞行器垂直起降、低速飞行与空中悬停,也可以像固定翼一样飞行,通过对集成机翼的仰角控制完成多旋翼飞行与固定翼飞行状态转换,通过加装大型可折叠固定翼提高续航力提高其经济性能,加装矢量推进器改善其操纵性能,把集成机翼设计成可折叠结构,方便于储存与运输,通过在每个集成机翼上增加方向舵的设计在单个集成机翼没有功率适配器的情况下也可控制飞行器进行升降、左右转向、前后、左右平移等运动。


    Access

    Download


    Export, share and cite



    Title :

    Multi-rotor integrated aircraft and flight control method


    Additional title:

    一种多旋翼集成飞行器与飞行控制方法


    Contributors:
    ZHANG HONGLING (author) / ZHOU BO (author) / ZU JIHONG (author) / JIANG HUA (author) / ZHANG ZHENG (author) / QI FANG (author) / LI YIFEI (author) / SUN RUI (author) / ZHOU FUYANG (author)

    Publication date :

    2024-09-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



    Multi-rotor flight control method, flight controller and aircraft

    SHEN YANG / TAO YONGKANG / ZHANG JUN et al. | European Patent Office | 2022

    Free access

    MULTI-FLIGHT MODE AIRCRAFT WITH INTEGRATED ROTOR WINGS

    KIM JOONG HOON | European Patent Office | 2024

    Free access

    Distributed tilting multi-rotor aircraft and flight control method

    LOU BIN / YAN XUFEI / WANG XIAOBO et al. | European Patent Office | 2021

    Free access

    Flight mode control method of distributed tilting multi-rotor aircraft

    ZHANG DAN / XIE ANHUAN / LOU BIN et al. | European Patent Office | 2021

    Free access

    Distributed multi-rotor tilting wing aircraft and flight control method

    CHEN JINHE / CHEN LIXIA / ZENG WEI et al. | European Patent Office | 2023

    Free access