The invention relates to an aircraft with a battery fused airframe. The aircraft comprises at least one section of battery fusion aircraft body, and the battery fusion aircraft body is of an aircraft body and battery integrated structure; the machine body battery integrated structure comprises a machine body frame, an outer coating layer, an inner coating layer and an inner battery storage layer arranged in the machine body frame; the inner-layer battery storage layer comprises a plurality of battery cabins divided by the machine body frame and battery packs stored in the battery cabins; the outer coating covers the outer side of the machine body frame, and the inner coating covers the inner side of the machine body frame. According to the technical scheme, the airplane with the battery fusion airplane body has the following beneficial technical effects that the battery bearing capacity of the electric propulsion airplane body can be improved, and the carrying capacity of the electric propulsion airplane is not limited.

    本发明涉及具有电池融合机体的飞机。该飞机包括至少一段电池融合机体,电池融合机体为机体电池一体化结构;机体电池一体化结构包括机体框架、外覆层、内覆层和设于机体框架中的内层电池存储层;内层电池存储层包括由机体框架划分出的多个电池舱、以及存储在电池舱内的电池包;外覆层覆盖机体框架外侧,内覆层覆盖机体框架内侧。根据上述技术方案,本发明的具有电池融合机体的飞机能起到以下有益技术效果:能提高电推进飞机机身承载电池容量,且不限制电推进飞机的运载能力。


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    Titel :

    Aircraft with battery fused airframe


    Weitere Titelangaben:

    具有电池融合机体的飞机


    Beteiligte:
    ZHOU XIYUE (Autor:in) / SONG HOUJIN (Autor:in) / CHEN ZHIYU (Autor:in) / ZHANG JIANYANG (Autor:in) / NIE SHIYU (Autor:in)

    Erscheinungsdatum :

    03.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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