The invention belongs to the technical field of aviation aircrafts, and discloses a wing-propeller-rudder integrated aircraft and a flight control method.The aircraft is composed of an aircraft body, wing-propeller-rudder integrated wings, a flight control system, a power system and a distribution system, and at least two sets of tandem wing-propeller-rudder integrated wings are arranged on the aircraft body; vertical take-off and landing, low-speed flight and hovering of the aircraft can be achieved like a multi-rotor aircraft, taxiing take-off, climbing, high-speed level flight and gliding landing of the aircraft can also be achieved like a fixed wing, and in order to improve the stability and economical efficiency of flight conversion of the aircraft, a large foldable fixed wing can be additionally arranged, the wing-propeller-rudder integrated wing is designed into a foldable structure, and therefore the aircraft can be folded and unfolded. The storage and the transportation are convenient; different undercarriages are selected to adapt to different airports and platforms to complete take-off and landing of the aircraft, and the flight elevation angle of the wing-paddle-rudder integrated wing and distribution of the power system are controlled through the flight control system to be applied to different flight states.

    本发明属于航空飞行器技术领域,公开了一种翼桨舵一体飞行器及飞行控制方法,飞行器由机体、翼桨舵一体机翼、飞控系统、动力系统和分配系统组成,在机体上至少设置两组纵列式翼桨舵一体机翼,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进行滑跑起飞、爬升、高速平飞、滑降,为提高其飞行转换的平稳性与经济性,可以通过加装大型可折叠固定翼,把翼桨舵一体机翼设计成可折叠结构,方便于储存与运输;选择不同的起落架以适应不同的机场和平台完成飞行器起降,通过飞控系统控制翼桨舵一体机翼飞行仰角与动力系统分配应用于不同的飞行状态。


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    Titel :

    Wing, propeller and rudder integrated aircraft and flight control method


    Weitere Titelangaben:

    一种翼桨舵一体飞行器及飞行控制方法


    Beteiligte:
    ZHANG HONGLING (Autor:in) / ZHOU BO (Autor:in) / ZU JIHONG (Autor:in) / JIANG HUA (Autor:in) / ZHANG ZHENG (Autor:in) / QI FANG (Autor:in) / SHI XIAOCHEN (Autor:in) / LI YIFEI (Autor:in)

    Erscheinungsdatum :

    16.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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