The present invention relates to an aircraft door locking device capable of omnidirectional location adjustment which allows a relative location of a roller to be variable wherein the roller is coupled to the hook formed in a body of the aircraft, thereby solving an existing problem that an air accident is followed when connection of the hook and the roller is not easy.

    본 발명은 전 방향 위치 조절이 가능한 항공기 도어 잠금장치에 관한 것으로서, 항공기의 몸체에 형성된 훅과 결합되는 롤러의 상대적 위치를 가변 가능하게 형성하여, 훅과 롤러의 결합이 용이하지 않을 경우 항공 사고로 이어지던 종래의 문제점을 해결한, 전 방향 위치 조절이 가능한 항공기 도어 잠금장치에 관한 것이다.


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    Titel :

    Aircraft door locking system of omnidirectional centering control


    Weitere Titelangaben:

    전 방향 위치 조절이 가능한 항공기 도어 잠금장치


    Beteiligte:
    CHOI SEOK SOON (Autor:in) / NAM GOO HYUN (Autor:in) / BAEK SEUNG JIN (Autor:in)

    Erscheinungsdatum :

    2018-01-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    E05B LOCKS , Schlösser / B64C AEROPLANES , Flugzeuge



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