The present invention provides a connecting device for a projectile, comprising: a first connector part inserted into and coupled to an insertion hole formed in an outer wall of a projectile; a second connector part insertable into the first connector part and having a hollow interior to provide a flow path for gas supplied to the projectile; and a lever part rotatably coupled to the second connector part and fixed in position by being in contact with the inner circumferential surface of the first connector part as rotating relative to the second connector part.

    본 발명은 발사체의 외벽에 형성되는 삽입공에 삽입 결합되는 제1커넥터부와, 제1커넥터부에 삽입 가능하며 발사체로 공급되는 기체의 유동 경로를 제공하도록 내부가 중공으로 형성되는 제2커넥터부 및 제2커넥터부에 회전가능하게 결합되며, 제2커넥터부에 대해 상대 회전함에 따라 제1커넥터부의 내주면에 접촉되어 위치 고정되는 레버부를 포함하는 발사체용 커넥팅 장치를 제공한다.


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    Titel :

    Connecting apparatus for projectile


    Weitere Titelangaben:

    발사체용 커넥팅 장치


    Beteiligte:
    KO JU YONG (Autor:in)

    Erscheinungsdatum :

    08.07.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F16L PIPES , Rohre / F17D Rohrleitungssysteme , PIPE-LINE SYSTEMS



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