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1. 发明公开

KR1020160068460A 다연장 발사장치 有权
标题翻译：发射多个箭头的装置
公开(公告)号：KR1020160068460A
公开(公告)日：2016-06-15
申请号：KR1020140174255
申请日：2014-12-05
申请人： 엘아이지넥스원 주식회사
发明人： 송철호
IPC分类号： F41F1/08 , F41A23/42
CPC分类号： F41F1/08 , F41A23/42 , F41F1/085
摘要： 본발명은동일방향배치되는복수개의발사관을수용하며상기발사관과정렬되는발사구를포함하는몸체부; 상기발사구를덮는덮개부;및상기발사구둘레를따라상기덮개부와접촉하여상기몸체부에결합하는플랜지부와, 상기플랜지부에서상기발사관의길이방향을기준으로발사방향으로돌출형성되며상기발사구의둘레를따라형성되는화염차단부를포함하는덮개클램프부를포함하는다연장발사장치를제공하여, 인접하는발사관에서발사되는발사체의화염에의해해당발사구의덮개부가파손되는것을방지하는유리한효과를제공한다.
摘要翻译：本发明涉及一种多扩展发射装置。多发射发射装置包括：身体单元，其存储沿相同方向布置的多个发射管，并且包括设置有发射管的发射开口; 覆盖所述发射开口的盖单元; 凸缘单元，其沿着所述发射开口的圆周与所述盖单元接触以联接到所述主体单元; 以及盖体单元，其形成为相对于所述凸缘单元相对于所述发射管的长度方向在发射方向突出，并且包括沿所述发射开口的圆周形成的防火部。多延伸发射装置具有防止由于从相邻的发射管发射的发射物体的火焰而损坏对应的发射开口的盖单元的优点。

2. 发明公开

KR1020100007264A 차량용 하역 장치 및 이를 구비한 다연장 로켓 시스템 无效
标题翻译：装载和卸载装置，用于车辆和包括装置的多个发射摇篮系统
公开(公告)号：KR1020100007264A
公开(公告)日：2010-01-22
申请号：KR1020080067826
申请日：2008-07-11
申请人： 한화테크윈 주식회사
发明人： 박수진 , 이강일
IPC分类号： F41A23/26 , F41A9/78
CPC分类号： F41A23/42 , F41A9/87 , F41H7/00
摘要： PURPOSE: A loading and unloading device for a vehicle and a multiple rocket launching system including the same are provided to easily load and unload objects using a simple structure. CONSTITUTION: Loading objects are placed on a base(210). A rotatable first actuator(220) is installed on the base. A rotatable first link member(230) is installed on the base. The rotatable first link member is positioned in order to receive the power from the first actuator. A rotatable second link member(240) is installed on the base. A third link member(250) connects the rotatable first link member and the rotatable second link member. A rotatable fourth link member(260) is installed and connected the second link member. One part of a second actuator(270) is installed on the rotatable second link member, and the other part of the second actuator is installed on the rotatable fourth link member.
摘要翻译：目的：提供一种用于车辆的装卸装置和包括其的多重火箭发射系统，以使用简单的结构容易地加载和卸载物体。构成：将物体放置在基座（210）上。可旋转的第一致动器（220）安装在基座上。可旋转的第一连杆构件（230）安装在基座上。可旋转的第一连杆构件被定位成为从第一致动器接收动力。可旋转的第二连杆构件（240）安装在基座上。第三连杆构件（250）连接可旋转的第一连杆构件和可旋转的第二连杆构件。可旋转的第四连杆构件（260）安装并连接在第二连杆构件上。第二致动器（270）的一部分安装在可旋转的第二连杆构件上，并且第二致动器的另一部分安装在可旋转的第四连杆构件上。

3. 发明公开

KR1020150022203A 발화가스 제거부재가 구비된 발사장치 有权
标题翻译：投入使用的气体供应
公开(公告)号：KR1020150022203A
公开(公告)日：2015-03-04
申请号：KR1020130099695
申请日：2013-08-22
申请人： 한국항공우주연구원
发明人： 고주용
IPC分类号： F41F3/04 , F41A23/42 , B64G1/22
CPC分类号： F41F3/04 , B64G1/22 , F41A23/42
摘要： 발사체용 발화가스 제거장치가 개시되어 있다.
개시된 발사체용 발화가스 제거장치는, 발사체의 후방동체 벽면에 설치되는 인터페이스부; 상기 인터페이스부의 외측에 연결되며, 비활성가스가 공급되는 공급관; 상기 인터페이스부의 내측에 연결되며, 상기 공급관으로 유입되는 비활성가스가 유입되는 유입관; 및 상기 유입관에 연결된 채 상기 후방동체의 챔버 내에 설치되며, 상기 유입관을 통해 유입되는 비활성가스를 챔버 내부를 향해 고압으로 분사하기 위한 다수의 분사공이 형성되어, 상기 챔버 내부의 발화가스를 챔버 벽면에 형성된 배출구를 통해 외부로 배출하는 매니폴드를 포함하는 것이다.
摘要翻译：公开了一种用于射弹的点火气体去除装置。用于射弹的点火气体去除装置包括：安装在射弹后部机身的壁上的接口部分; 连接到供应惰性气体的界面部分的外侧的供给管; 连接到所述接口部分的内侧的入口管，供给到所述供给管的惰性气体流入所述入口管; 以及安装在后机身的室内的歧管，连接到入口管，入口管具有多个注入孔，用于将通过入口管流入的惰性气体以高压注入到室中，并且将内部的点燃气体通过室的壁上的出口将室通向外部。

4. 发明授权

KR101138154B1 로켓 포드 탑재 시스템 有权
标题翻译： Roket Pod装载系统
公开(公告)号：KR101138154B1
公开(公告)日：2012-04-23
申请号：KR1020080128961
申请日：2008-12-18
申请人： 한화디펜스 주식회사
发明人： 구자상
IPC分类号： F41A23/42 , F41A23/26
CPC分类号： F41A9/82 , F41A23/42 , F41F3/042
摘要： PURPOSE: A rocket pod loading system is provided to reduce the transfer distance of the center beam transfer method for transferring the rocket pod carriage. CONSTITUTION: A rocket pod mount system comprises a launcher housing(10), a fixed beam(20), a center beam(30), a center beam transfer unit(40), a rocket pod carriage(50), a roller, and a wire. The fixed beam is inserted and fixed inside the launcher housing. The center beam is transferred to backward and forward in the fixed beam inside. The center beam transfer unit transfers the center beam to backward and forward. The rocket pod carriage transfers a rocket pod to the inner and outer launch station housing. The roller is installed in the front-end or the back-end of the center beam. The one end of the wire is fixed to the fixed beam. The other end of the wire is fixed to the rocket pod carriage.

5. 发明公开

KR1020100070425A 로켓 포드 탑재 시스템 有权
标题翻译： ROKET POD装载系统
公开(公告)号：KR1020100070425A
公开(公告)日：2010-06-28
申请号：KR1020080128961
申请日：2008-12-18
申请人： 한화디펜스 주식회사
发明人： 구자상
IPC分类号： F41A23/42 , F41A23/26
CPC分类号： F41A9/82 , F41A23/42 , F41F3/042
摘要： PURPOSE: A rocket pod loading system is provided to reduce the transfer distance of the center beam transfer method for transferring the rocket pod carriage. CONSTITUTION: A rocket pod mount system comprises a launcher housing(10), a fixed beam(20), a center beam(30), a center beam transfer unit(40), a rocket pod carriage(50), a roller, and a wire. The fixed beam is inserted and fixed inside the launcher housing. The center beam is transferred to backward and forward in the fixed beam inside. The center beam transfer unit transfers the center beam to backward and forward. The rocket pod carriage transfers a rocket pod to the inner and outer launch station housing. The roller is installed in the front-end or the back-end of the center beam. The one end of the wire is fixed to the fixed beam. The other end of the wire is fixed to the rocket pod carriage.
摘要翻译：目的：提供一种火箭炮垛装载系统，以减少用于传送火箭炮垛托架的中心射束传送方法的传送距离。构成：火箭炮座安装系统包括发射器壳体（10），固定梁（20），中心梁（30），中心梁传递单元（40），火箭舱托架（50），滚子和电线固定梁插入并固定在发射器壳体内。中心梁在内侧的固定梁中向后前进。中心光束传输单元将中心光束向后前进。火箭筒托架将一个火箭筒传送到内部和外部发射台壳体。辊安装在中心梁的前端或后端。线的一端固定在固定梁上。电线的另一端固定在火箭筒托架上。

6. 发明公开

KR1020100005543A 차량용 하역 장치 및 이를 구비한 다연장 로켓 시스템 无效
标题翻译：装载和卸载装置，用于车辆和包括装置的多个发射摇篮系统
公开(公告)号：KR1020100005543A
公开(公告)日：2010-01-15
申请号：KR1020080065631
申请日：2008-07-07
申请人： 한화테크윈 주식회사
发明人： 박인규
IPC分类号： F41A23/26 , F41A23/42 , B66C23/36
CPC分类号： F41A9/87 , F41A23/42 , F41H7/02 , F41H7/00
摘要： PURPOSE: A loading and unloading device for a vehicle and an MLRS(Multiple Launch Rocket System) using the same are provided to reduce the number of manufacturing steps and the manufacturing cost by simplifying the inner structure of the device. CONSTITUTION: A loading and unloading device(100) for a vehicle is composed of a base(110), first and second actuators(121,122), lower, middle, and upper link members(130,140,180), a protruded fixed unit(150), a parallel link member(160), one or more connection link member(170). The first actuator is rotatably installed on the base. The lower link member is rotated by operation of the first actuator. The middle link member is rotatably mounted on the lower link member. One end of the second actuator is mounted on the lower link member and the other end is mounted on the middle link member. The parallel link member is rotatably mounted on the middle link member. The connection link member connects the parallel link member and the protruded fixed unit each other. The upper link member applies force to loaded articles. One end of the third actuator is mounted on the middle link member and the other end is mounted on the upper link member.
摘要翻译：目的：提供一种用于车辆的装卸装置和使用其的MLRS（多发射火箭系统），以通过简化装置的内部结构来减少制造步骤的数量和制造成本。构成：用于车辆的装载和卸载装置（100）由基座（110），第一和第二致动器（121,122），下部，中部和上部连接构件（130,140,180），突出的固定单元（150），平行连杆构件（160），一个或多个连接构件（170）。第一致动器可旋转地安装在基座上。下连杆构件通过第一致动器的操作而旋转。中间连杆构件可旋转地安装在下连杆构件上。第二致动器的一端安装在下连杆构件上，另一端安装在中间连杆构件上。平行连杆构件可旋转地安装在中间连杆构件上。连接连杆构件将平行连杆构件和突出的固定单元彼此连接。上连杆构件对加载的物品施加力。第三致动器的一端安装在中间连杆构件上，另一端安装在上连杆构件上。

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