According to one embodiment of the present invention, a pneumatic launching device comprises: a gun barrel having one or more pressure holes; a pressure providing part which can be in fluid communication with the gun barrel through the pressure hole; a gas supply port formed in the pressure providing part and receiving gas from the outside; a sealing member fixed to the gun barrel to block a gap between a loaded projectile and the gun barrel; and a first trigger port connected to one end of the gun barrel to apply a pneumatic pressure to the loaded projectile. Therefore, an objective of the present invention is to provide the pneumatic launching device for reducing friction between the projectile and the gun barrel.

    본 발명의 일 실시예에 따른 공압 발사 장치는, 하나 이상의 압력 구멍을 가지는 총신, 상기 압력 구멍을 통해 상기 총신과 유체 연통할 수 있는 압력 제공부, 상기 압력 제공부에 형성되어 외부로부터 가스를 주입받는 가스 공급 포트, 상기 총신에 고정되어 장전된 투사체와 상기 총신 사이의 틈을 막는 실링 부재 및 상기 총신의 일단과 연결되어 상기 장전된 투사체에 공압을 가할 수 있는 제1 트리거 포트를 포함한다.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Pneumatic launcher


    Weitere Titelangaben:

    공압 발사 장치


    Beteiligte:
    JEONG JUWON (Autor:in) / KIM KYUNG WON (Autor:in) / LEE JUNGJU (Autor:in) / LIM JAE HYUK (Autor:in)

    Erscheinungsdatum :

    13.06.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64G Raumfahrt , COSMONAUTICS



    Pneumatic launcher

    Europäisches Patentamt | 2019

    Freier Zugriff

    Pneumatic Launcher System

    L. Dragonuk | NTIS | 1982


    ROTARY WING UNMANNED AERIAL VEHICLE AND PNEUMATIC LAUNCHER

    ZHANG HANHUI | Europäisches Patentamt | 2018

    Freier Zugriff

    Rotary wing unmanned aerial vehicle and pneumatic launcher

    ZHANG HANHUI | Europäisches Patentamt | 2019

    Freier Zugriff