The present disclosure proposes a collision load distribution structure of a fuselage, in which the structure comprises: a support unit positioned between a front unit and a rear unit of the fuselage and configured to transmit a collision load of the fuselage by being connected to the front unit and the rear unit; a wing unit positioned inside the support unit and connected to the support unit to transmit a collision load of the fuselage; and a seat unit coupled to a connection frame installed in a second row passenger space of the floor frame constituting the front unit and fastened to a first rear frame extending from the floor frame to the support unit in the height direction.

    本公开提出一种机身的碰撞载荷分布结构,其中该结构包括:支撑单元,定位在机身的前部单元和后部单元之间并且被构造为使机身的碰撞载荷通过连接到前部单元和后部单元而被传递;翼单元,定位在支撑单元内部并且连接到支撑单元以传递机身的碰撞载荷;以及座椅单元,联接到安装在构成前部单元的底板框架的第二排乘客空间中的连接框架并且紧固到在高度方向上从底板框架向支撑单元延伸的第一后部框架。


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    Titel :

    Collision load distribution structure of fuselage


    Weitere Titelangaben:

    机身的碰撞载荷分布结构


    Beteiligte:
    SONG WON KI (Autor:in)

    Erscheinungsdatum :

    21.05.2024


    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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