According to the present invention, an apparatus for absorbing shocks of a cockpit can include: a plurality of supports having a plate shape, mounted on a structure supporting the cockpit, and spaced apart from each other by a predetermined distance to face each other; a friction pad mounted on a surface facing the plurality of supports; and a distance control part installed on the supports and controlling a distance between the supports. Therefore, a user can easily verify the performance of the apparatus for absorbing shocks.

    본 발명에 따른 조종석 충격흡수 장치는 판 형상이고 조종석을 지지하는 구조물에 장착되며 일정거리 이격되어 서로 마주하는 복수의 지지대; 상기 복수의 지지대의 마주하는 면에 장착되는 마찰패드; 및 상기 지지대에 설치되며 상기 지지대 간의 거리를 조절하는 거리조절부;를 포함할 수 있다.


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    Titel :

    SHOCK ABSORBER OF COCKPIT FOR HELICOPTER


    Weitere Titelangaben:

    조종석 충격흡수 장치


    Beteiligte:
    SHIN SEOK NAM (Autor:in) / CHANG WOO CHUL (Autor:in)

    Erscheinungsdatum :

    27.04.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16F SPRINGS , Federn



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