The invention discloses an energy-saving structure of an aircraft. The energy-saving structure comprises an impeller, a first transmission shaft, a speed regulator, a second transmission shaft, a generator and an energy storage module, the impeller is located on the outer side of a shell of the aircraft, the speed regulator, the generator and the energy storage module are located on the inner side of the shell of the aircraft, the impeller is connected with the speed regulator through a first transmission shaft, the speed regulator is connected with the generator through a second transmission shaft, and the generator is connected with the energy storage module. Through the design of the energy-saving structure of the aircraft, the energy-saving structure can realize conversion and storage of wind energy and electric energy in the flight process of the aircraft. Through partial energy supply, the voyage and flight time of the aircraft can be increased, and the use of fossil fuel is reduced.

    本发明公开了一种飞行器的节能结构,所述节能结构包括:叶轮、第一传动轴、调速器、第二传动轴、发电机和储能模块;所述叶轮位于所述飞行器的机壳外侧,所述调速器、发电机和储能模块位于所述飞行器的机壳内侧,其中,所述叶轮经第一传动轴与所述调速器相连接,所述调速器经第二传动轴与发电机相连,所述发电机与储能模块相连。通过本发明飞行器的节能结构设计,使得飞行器在飞行过程中,节能结构能够实现风能与电能的转化及储备。从而通过进行部分能源补给,能够增加飞行器的航程与飞行时间,减少化石燃料的使用。


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    Titel :

    Energy-saving structure of aircraft


    Weitere Titelangaben:

    一种飞行器的节能结构


    Beteiligte:
    WANG FUYUAN (Autor:in) / LI YANG (Autor:in) / FENG ZHICHAO (Autor:in) / QIAO HONGTAO (Autor:in) / GUO CHUAN (Autor:in)

    Erscheinungsdatum :

    01.07.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F03D Windkraftmaschinen , WIND MOTORS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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