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公开(公告)号：KR101804044B1
公开(公告)日：2017-12-01
申请号：KR1020160032610
申请日：2016-03-18
Applicant: 국방과학연구소
Abstract: 본발명은중량물과용이하게조립또는분해할수 있으면서인양시중량물과분리되는것을방지하도록한 중량물인양용후크어셈블리에관한것이다.본발명에따른중량물인양용후크어셈블리는, 중량물(1)을인양하는중량물인양기구에상단이체인(31)으로연결되는 T형후크(10)와, 중량물(1)에체결되고, 상기 T형후크(10)의하단을내부에수용하여, 상기 T형후크(10)에연결되는후크고정구(20)를포함하고, 상기 T형후크(10)는상기후크고정구(20)로삽입된후, 정해진각도로회전시킨후, 중량물이인양되는것을특징으로한다.
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公开(公告)号：KR1020170106834A
公开(公告)日：2017-09-22
申请号：KR1020160030482
申请日：2016-03-14
Applicant: 국방과학연구소
Abstract: 본발명은유도탄의날개지지대에관한것으로, 유도탄동체; 상기유도탄동체에구비되어상기유도탄동체로부터멀어지는방향으로전개되는다수의날개; 및상기날개의단부에구비되어상기날개를지지하는지지대를포함하고, 상기지지대는상기유도탄을수용하는원통형상의발사관에접촉하도록형성되는것을특징으로하는유도탄날개지지구조에대한것이다.
Abstract translation: 本发明涉及一种被引导车辆的机翼支架， 多个叶片，其设置在所述引导车体中并沿远离所述引导车体的方向展开; 以及设置在所述叶片的端部以支撑所述叶片的支撑基座，其中所述支撑基座形成为接触容纳所述引导车的圆柱形发射管。
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公开(公告)号：KR101644520B1
公开(公告)日：2016-08-01
申请号：KR1020140111059
申请日：2014-08-25
Applicant: 국방과학연구소
Abstract: 본발명은유도탄횡방향고정장치에관한것으로서, 보다상세하게는유도탄수송및 운용시 유도탄과고정부의간극을제거하여유도탄이발사관내부에서횡방향운동을하지못하도록하는유도탄횡방향고정장치에관한것이다. 이를위해, 본발명은중공의관으로형성되는발사관, 상기발사관의외주면에관통되어설치되고, 회전가능하도록설치되는회전스터드및 상기회전스터드의단부를감싸도록설치됨과동시에상기회전스터드의회전에의해발사관의길이방향의수직방향을따라이동가능한직선이동스터드를포함하는것을특징으로하는스터드를이용한유도탄횡방향고정장치를제공한다.
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公开(公告)号：KR1020160024418A
公开(公告)日：2016-03-07
申请号：KR1020140111059
申请日：2014-08-25
Applicant: 국방과학연구소
Abstract: 본발명은유도탄횡방향고정장치에관한것으로서, 보다상세하게는유도탄수송및 운용시 유도탄과고정부의간극을제거하여유도탄이발사관내부에서횡방향운동을하지못하도록하는유도탄횡방향고정장치에관한것이다. 이를위해, 본발명은중공의관으로형성되는발사관, 상기발사관의외주면에관통되어설치되고, 회전가능하도록설치되는회전스터드및 상기회전스터드의단부를감싸도록설치됨과동시에상기회전스터드의회전에의해발사관의길이방향의수직방향을따라이동가능한직선이동스터드를포함하는것을특징으로하는스터드를이용한유도탄횡방향고정장치를제공한다.
Abstract translation: 本发明涉及一种用于在横向固定导弹的装置，更具体地涉及一种用于在横向上固定导弹的装置，其防止导弹在发射管内沿横向移动，通过去除 在导弹运输和导弹运行期间导弹与固定装置之间的差距。 因此，本发明提供了一种用于使用螺柱固定导向件在横向上的装置，包括：形成为中空管的发射管; 旋转螺柱，穿透并安装在发射管的外周表面上，并安装成可旋转; 以及通过旋转螺柱的旋转沿着发射管的纵向的垂直方向可移动的直线运动螺柱，并且安装成覆盖旋转螺柱的端部单元。
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公开(公告)号：KR101558434B1
公开(公告)日：2015-10-07
申请号：KR1020130159683
申请日：2013-12-19
Applicant: 국방과학연구소
Abstract: 본발명은발사관용힌지클램프형중량물고정장치에관한것으로서, 보다상세하게는구조를간소화함과동시에신뢰성을향상시킬수 있는발사관용힌지클램프형중량물고정장치에관한것이다. 이를위해, 본발명은발사관에플랜지결합되는원통형구조물, 상기구조물의내주면에밀착하여장입되는중량물및 상기구조물과중량물의외주면을동시에감싸도록힌지를중심으로회동하는클램프를포함하고, 상기클램프의분리가능한부분에형성되는체결부가결합또는분리됨으로써선택적으로상기구조물과중량물을고정지지하는것을특징으로하는발사관용힌지클램프형중량물고정장치를제공한다.
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Patent Agency Ranking
公开(公告)号：KR1020150072245A
公开(公告)日：2015-06-29
申请号：KR1020130159683
申请日：2013-12-19
Applicant: 국방과학연구소
Abstract: 본발명은발사관용힌지클램프형중량물고정장치에관한것으로서, 보다상세하게는구조를간소화함과동시에신뢰성을향상시킬수 있는발사관용힌지클램프형중량물고정장치에관한것이다. 이를위해, 본발명은발사관에플랜지결합되는원통형구조물, 상기구조물의내주면에밀착하여장입되는중량물및 상기구조물과중량물의외주면을동시에감싸도록힌지를중심으로회동하는클램프를포함하고, 상기클램프의분리가능한부분에형성되는체결부가결합또는분리됨으로써선택적으로상기구조물과중량물을고정지지하는것을특징으로하는발사관용힌지클램프형중량물고정장치를제공한다.
Abstract translation: 本发明涉及一种用于发射管的铰链式夹具的重量固定装置，更具体地，涉及一种用于发射管的铰链式夹具的重量固定装置，以简化结构并提高可靠性。 为了实现这一点，用于发射管的铰链式夹具的重量固定装置包括：通过凸缘连接到发射管的圆柱形结构; 附着于要插入的结构的内周的重量; 以及夹具围绕铰链旋转以同时覆盖结构的外周和重量。 紧固部件与夹具的可拆卸部分接合或分离，以选择性地固定和支撑结构和重物。
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公开(公告)号：KR1020150033083A
公开(公告)日：2015-04-01
申请号：KR1020130112616
申请日：2013-09-23
Applicant: 국방과학연구소
Abstract: 본발명은내측벽에발사체에서분사된화염이발사체로역류하는것을방지할수 있도록내측벽에화염역류방지판이설치된화염역류방지판을가진발사관에관한것이다. 본발명에따른화염역류방지판을가진발사관은, 내부에발사체(1)가장전되도록상기발사체(1)의길이방향을따라중공으로형성되고, 상기발사체(1)가발사되면서상기발사체(1)로부터배출된화염이그 후단에형성된토출구(11)를통하여배출되는발사관에있어서, 상기발사관(10)의내부에는상기발사관(10)의내측벽으로부터상기발사관(10)의중심을향하도록연장되게형성되어, 그내측둘레가상기발사체(1)의둘레에인접하게형성되는화염역류방지판(12)이설치되는것을특징으로한다.
Abstract translation: 本发明涉及一种具有防反火防止板的发射管，其具有内壁上的阻焰防止板，以防止火焰从发射体喷射，并且火焰向后流向发射体 在内墙上 根据本发明，具有防回火防止板的发射管沿着发射体（1）的纵向方向中空地形成，以使发射体（1）装载在内部; 并且作为发射体（1）发射的从发射体（1）排出的火焰通过形成在后端的排出孔（11）排出。 其内周形成为靠近发射体（1）的圆周的防焰反流板（12）通过从发射管（10）的内壁朝向发射管（10）的中心大范围地形成 发射管（10）在发射管（10）内。
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公开(公告)号：KR101405261B1
公开(公告)日：2014-06-10
申请号：KR1020140021440
申请日：2014-02-24
Applicant: 국방과학연구소
Abstract: The present invention relates to a launching tube having a function of preventing counterflow of flame which can prevent the flame jetted from a projectile from counterflow to the projectile at the moment when the projectile is launched. The launching tube according to the present invention is formed in a tubular shape, and a projectile (1) is loaded in the launching tube. The flame discharged from the projectile (1) when the projectile is launched is discharged from an outlet port (11) formed at the rear end of the launching tube. The launching tube is provided with a flame counterflow reducing part (30) at a portion at which a rear end of the projectile (1) is positioned, and an inner cross sectional area of the flame counterflow reducing part (30) is larger than that of other portion. An outer launching tube (10) is connected to an inner launching tube (20) which is disposed in the outer launching tube (10) and is formed adjacent to the outer peripheral surface of the projectile (1) at a predetermined interval, and the lower end of the inner launching tube is connected to the flame counterflow reducing part (30).
Abstract translation: 本发明涉及具有防止火焰逆流的功能的发射管，其能够防止在发射抛射体时从射弹喷射的火焰与射弹反流。 根据本发明的发射管形成为管状，射出管（1）装载在发射管中。 当发射弹时从射弹（1）排出的火焰从形成在发射管后端的出口（11）排出。 发射管在射弹（1）的后端所在的部分处设置有火焰逆流减少部（30），火焰逆流减少部（30）的内横截面面积大于 的其他部分。 外部发射管（10）连接到设置在外部发射管（10）中并以预定间隔邻近射弹（1）的外周表面形成的内部发射管（20），并且 内部发射管的下端连接到火焰逆流减少部分（30）。
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公开(公告)号：KR1020140016103A
公开(公告)日：2014-02-07
申请号：KR1020120083464
申请日：2012-07-30
Applicant: 국방과학연구소
Abstract: The canister connector of a launching tube according to an embodiment of the present invention is a canister connector of a launching tube, which is formed on the outer periphery of the launching tube where a guide missile is contained, and connects an inner connector connected to a canister connector of the guided missile on one end so as to transmit an electric signal to the canister connector of the guided missile, and an outer cable connected to launching equipment of a guided missile on one end. The canister connector of a launching tube comprises multiple pins projected toward outside from one side to be electrically connected to the outer cable, a coupling part covering one side to limit a domain where the pins are formed, and an insertion part coupled with the coupling part and having multiple holes corresponding to the pins to protect the pins.
Abstract translation: 根据本发明实施例的发射管的罐连接器是发射管的罐连接器，其形成在发射管的外周上，其中容纳有导弹，并且连接到连接到 一端的导弹连接器，以便将电信号发送到导弹的罐连接器，以及一端连接到导弹发射装置的外线缆。 发射管的罐连接器包括从一侧向外侧突出以与外部电缆电连接的多个销，连接部分，其覆盖一侧以限制销形成的区域，以及与耦合部分耦合的插入部分 并且具有对应于销的多个孔以保护销。
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公开(公告)号：KR100659303B1
公开(公告)日：2006-12-20
申请号：KR1020060031137
申请日：2006-04-05
Applicant: 국방과학연구소
Abstract: A missile fixing mechanism of a missile shooting apparatus is provided to basically prevent an impact between a shooting pipe and the missile before the missile is shoot by stably fixing the missile in the shooting pipe. A missile fixing mechanism of a missile shooting apparatus includes a missile support(110), an inner stub(120), and an outer stub(140). A penetration hole is formed in the radial direction of the missile and the missile support is positioned on the outer peripheral surface of the missile. The inner stub is inserted into the penetration hole. One end of the inner stub makes contact with the outer peripheral surface of the missile. The outer stub is fixed to the shooting pipe so as to make contact with the tip end surface of the inner stub.
Abstract translation: 本发明提供了一种导弹射击装置的导弹固定机构，通过将导弹稳定地固定在射击管内，基本上防止了导弹射击前射击管与导弹之间的撞击。 一种导弹射击装置的导弹固定机构，包括导弹支架（110），内支杆（120）和外支杆（140）。 在导弹的径向上形成穿透孔，导弹支架位于导弹的外围表面上。 内短棒插入穿孔。 内桩的一端与导弹的外周表面接触。 外柱固定在射出管上以便与内柱的尖端表面接触。
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