The invention relates to the technical field of aircrafts, in particular to a large multifunctional manned fuel aircraft which comprises an aircraft body, a fuel power source is mounted in the aircraft body, the output end of the fuel power source is in transmission connection with a power transfer mechanism, and the power transfer mechanism is in transmission connection with at least six flight structures. The flight structure is in transmission connection with a coaxial reversal angle adjusting transmission mechanism used for coaxial reversal and angle adjustment, the coaxial reversal angle adjusting transmission mechanism is in transmission connection with the power transfer mechanism, and the coaxial reversal angle adjusting transmission mechanism is used for driving the flight structure to coaxially rotate reversely. The flight efficiency of the flight structure is improved. According to the invention, long endurance and rapid flight attitude adjustment and stable flight can be realized.

    本发明涉及飞行器技术领域,尤其涉及一种大型多功能载人燃油飞行器,包括机体,所述机体内安装有燃油动力源,所述燃油动力源的输出端传动连接有动力中转机构,所述动力中转机构传动连接有至少六个飞行结构,所述飞行结构传动连接有用于共轴反转和角度调节的共轴反转角度调节传动机构,所述共轴反转角度调节传动机构与所述动力中转机构传动连接,所述共轴反转角度调节传动机构用于驱动所述飞行结构共轴反转,提升飞行结构的飞行效率。本发明可以实现长续航和飞行姿态快速调整稳定飞行。


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    Titel :

    Large multifunctional manned fuel aircraft


    Weitere Titelangaben:

    一种大型多功能载人燃油飞行器


    Beteiligte:
    HE JIAN (Autor:in)

    Erscheinungsdatum :

    10.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60F VEHICLES FOR USE BOTH ON RAIL AND ON ROAD , Fahrzeuge für den Verkehr sowohl auf Schienen als auch auf Straßen / B64C AEROPLANES , Flugzeuge



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