본 발명은, 동체의 날개를 기준으로 전단에 위치하는 전방 유닛, 동체의 날개를 기준으로 후단에 위치하는 후방 유닛, 전방 유닛 및 후방 유닛의 사이에 위치하고, 전방 유닛 및 후방 유닛과 연결되어 동체의 하중을 전달하도록 구성되는 서포트 유닛 및 서포트 유닛의 내측에 위치하고, 서포트 유닛과 연결되어 동체의 충돌시 하중을 전달하도록 구성되는 날개 유닛을 포함하고, 동체의 길이방향 하중은 전방 유닛을 거쳐 서포트 유닛을 통해 날개 유닛으로 분산되도록 구성되는 동체의 충돌 하중 분산구조를 제공한다.

    A collision load distribution structure of a fuselage includes a front unit configured to be located at front ends relative to wings attached to the fuselage, a rear unit configured to be located at rear ends relative to the wings attached to the fuselage, a support unit configured to be located between the front unit and the rear unit, and a wing unit. The support unit is configured to transfer loads applied to the fuselage in case of a crash of the fuselage. The wing unit is configured to be located in the support unit, and connected to the support unit so as to transfer the loads in case of the crash of the fuselage. Loads in a length direction of the fuselage are passed through to the front unit, and are distributed to the wing unit through the support unit.


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    Title :

    Collision load distribution structure of the fuselage


    Additional title:

    동체의 충돌 하중 분산구조


    Contributors:
    SONG WON KI (author)

    Publication date :

    2024-08-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    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 fuselage

    SONG WON KI | European Patent Office | 2024

    Free access