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 the 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; a lever unit coupled to the second connector part and connecting the first connector part and the second connector part; a block unit installed on the outer wall of the projectile; and a lock unit coupled to the lever unit and insertable into the block unit.

    본 발명은 발사체의 외벽에 형성되는 삽입공에 삽입 결합되는 제1커넥터부와, 제1커넥터부에 삽입 가능하며 발사체로 공급되는 기체의 유동 경로를 제공하도록 내부가 중공으로 형성되는 제2커넥터부 및 제2커넥터부에 결합되며, 제1커넥터부와 제2커넥터부를 연결하는 레버부 및 발사체의 외벽에 설치되는 블록부와, 레버부와 결합되며 블록부에 삽입 가능한 잠금부를 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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