Proposed is a collision load distribution structure of a fuselage, wherein the structure includes a support unit positioned between a front unit and a rear unit of the fuselage and configured to allow a collision load of the fuselage to be transferred by being connected to the front unit and the rear unit, a wing unit positioned at the inside of the support unit and connected to the support unit to transfer the collision load of the fuselage, and a seat unit coupled to a connection frame mounted in a second-row passenger space of a floor frame constituting the front unit and fastened to a first rear frame extending in a height direction from the floor frame toward the support unit.


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    Title :

    Collision Load Distribution Structure of Fuselage


    Contributors:
    SONG WON KI (author)

    Publication date :

    2024-05-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Fuselage collision load distribution structure

    SONG WON KI | European Patent Office | 2024

    Free access

    Collision load distribution structure of fuselage

    SONG WON KI | European Patent Office | 2024

    Free access

    Collision Load Distribution Structure of Fuselage

    SONG WON KI | European Patent Office | 2024

    Free access

    Collision load distribution structure of fuselage

    SONG WON KI | European Patent Office | 2024

    Free access

    Collision load distribution structure of the fuselage

    SONG WON KI | European Patent Office | 2024

    Free access