公开(公告)号：KR101262696B1

公开(公告)日：2013-05-15

申请号：KR1020100117683

申请日：2010-11-24

Applicant: 국방과학연구소

Inventor： 김인학 ,  김형렬 ,  독고욱

IPC: F42B15/20 ,  F42B12/02 ,  F42B17/00 ,  F42B12/76

Abstract: 본발명의일 실시예에따르는보호덮개는복수의지지체를포함하며, 일단은밀폐면을형성하고, 타단은개구된중공의원통으로형성되는쉘조립체와, 상기쉘조립체의내부에수용되는완충공및 상기쉘조립체의밀폐면과결합하여, 유체의유입을막는밀폐판을포함함으로써, 발사및 비행시에는견고하게유도탄의전방체를보호하고, 입수시에는충격을완충하도록파열됨으로써, 정밀타격을목표로하는유도탄의기계또는전자장치들이신뢰성을유지하도록보호할수 있다.

公开(公告)号：KR100416213B1

公开(公告)日：2004-01-31

申请号：KR1020010006148

申请日：2001-02-08

Applicant: 국방과학연구소

Inventor： 전완수 ,  독고욱 ,  김인학 ,  신용재 ,  김찬기 ,  박정기

IPC: B64D17/00

Abstract: PURPOSE: A parachute assembly for a light torpedo of a hydroplane is provided to stabilize the torpedo by controlling the posture of the torpedo continuously after firing with deploying the parachute promptly and accurately. CONSTITUTION: A parachute assembly for a light torpedo is composed of a parachute having a canopy(1a) and a rope(1b); a parachute container(2) assembled with the lower part of the rope to contain the parachute, and opened in the upper part; a cover(4) closing the upper part of the parachute container; a pulling rope(5) fixed in a torpedo tube and connected to the canopy to pull the parachute in firing the torpedo; an opening unit opening the cover; a pulling rope cutting unit cutting the parachute from the pulling rope; an assembling unit installed in the lower part of the parachute container to restrict rotation of the container, and to assemble with the light torpedo for separating by moving back and forth; and a sleeve(9) fixed in the lower part of the parachute container. The posture of the torpedo is controlled stably after firing with the parachute assembly.

Abstract translation: 目的：提供一种用于轻型鱼雷的降落伞组件，用于通过迅速和准确地部署降落伞并在发射后连续控制鱼雷的姿态来稳定鱼雷。 一种用于轻型鱼雷的降落伞组件，包括一个具有顶盖（1a）和绳索（1b）的降落伞; 降落伞容器（2），其与绳子的下部组装在一起以容纳降落伞，并在上部开口; 一个封闭降落伞容器上部的盖子（4） （5）固定在鱼雷管中并连接到天篷以拉动降落伞以发射鱼雷; 打开盖的打开单元; 牵引绳切割单元，用于从牵引绳切割降落伞; 组装单元，所述组装单元安装在所述降落伞容器的下部以限制所述容器的旋转，并且与所述轻型鱼雷组装以通过前后移动来分离; 和固定在降落伞容器下部的套筒（9）。 用降落伞组件发射后，鱼雷的姿态稳定可控。

公开(公告)号：KR100840995B1

公开(公告)日：2008-06-24

申请号：KR1020070017975

申请日：2007-02-22

Applicant: 국방과학연구소

Inventor： 김인학 ,  김형렬 ,  독고욱

IPC: G01M7/08 ,  G01M10/00

Abstract: A device for testing impact of launching into the water is provided to obtain reliable test results at low cost by simulating various water entry conditions and repeatedly performing a test. A device for testing impact of launching into the water includes a test object, a launch tube(120), a high pressure vessel(130), a measuring unit, and a launch tube support unit. The test object has an impact pressure sensor and an impact acceleration sensor at a head. The launch tube launches the test object. The high pressure vessel is installed in the rear of the launch tube and selectively applies air pressure to the launch tube to launch the test object. The measuring unit has a signal cable to connect sensors of the test object and measuring equipment and measures impact data when the test object enters the water. The launch tube support unit supports the launch tube to rotate the launch tube within a predetermined range.

Abstract translation: 提供了一种用于测试发射到水中的影响的装置，通过模拟各种进水条件并重复进行测试，以低成本获得可靠的测试结果。 用于测试发射到水中的影响的装置包括测试对象，发射管（120），高压容器（130），测量单元和发射管支撑单元。 测试对象在头部具有冲击压力传感器和冲击加速度传感器。 发射管启动测试对象。 高压容器安装在发射管的后部，并且选择性地向发射管施加空气压力以发射测试对象。 测量单元具有连接测试对象和测量设备的传感器的信号电缆，并在测试对象进入水中时测量影响数据。 发射管支撑单元支撑发射管以将发射管旋转在预定范围内。

公开(公告)号：KR1020040056109A

公开(公告)日：2004-06-30

申请号：KR1020020082657

申请日：2002-12-23

Applicant: 국방과학연구소

Inventor： 전완수 ,  독고욱 ,  정현기 ,  빈재구 ,  박태조

IPC: F16H13/14

Abstract: PURPOSE: A preload fixing apparatus of an orbital friction driving mechanism is provided to reduce noise and backlash by transmitting power from the input shaft to the output shaft without passing the gear train, to improve power transmission efficiency by restricting slip between the inner periphery of the ring roller and the outer periphery of the orbital roller with applying preload, and to prevent wear from friction by forming the lubrication film with injecting lubricant. CONSTITUTION: An orbital friction driving mechanism comprises a body casing(10) having a space part; an input shaft(20) inserted to the body casing; a sun roller(30) combined with the input shaft in the space part; a ring roller(40) mounted outside the sun roller in the space part; plural orbital rollers(50) rolled and contacted to the outer periphery of the sun roller and the inner periphery of the ring roller with revolving and rotating; and an output shaft(60) inserted to the body casing and extended in the same axis of the input shaft to rotate in revolving the orbital roller. The ring roller is divided into a right separation body having a fixing part fastened in the body casing and a roller part covering the right of the roller groove, and a left separation body having an assembling part and a roller part covering the left of the roller groove. A preload bolt combines the assembling part of the left separation body with the fixing part of the right separation body.

Abstract translation: 目的：提供一种轨道摩擦驱动机构的预载固定装置，通过在不通过齿轮系的情况下将动力从输入轴传递到输出轴，以减小噪音和间隙，通过限制滑轮的内周边之间的滑动来提高动力传递效率 环形辊和轨道滚子的外周边施加预载荷，并通过用注入润滑剂形成润滑膜来防止摩擦磨损。 构成：轨道摩擦驱动机构包括具有空间部分的主体壳体（10） 插入到所述主体壳体中的输入轴（20） 与空间部分中的输入轴组合的太阳辊（30）; 安装在太阳辊外部的空间部分中的环形滚轮（40） 多个轨道滚子（50）旋转并旋转而卷绕并接触太阳辊的外周和环形滚筒的内周; 以及输入轴（60），其插入到主体壳体中并且在输入轴的同一轴线上延伸以在旋转滚动辊中旋转。 环形滚筒分为具有紧固在主体壳体中的固定部分和覆盖滚子槽右侧的滚子部分的右侧分离体，以及具有组装部分和覆盖辊子左侧的滚子部分的左侧分离体 槽。 预紧螺栓将左分离体的组装部分与右分离体的固定部分组合。

公开(公告)号：KR1020120056123A

公开(公告)日：2012-06-01

申请号：KR1020100117683

申请日：2010-11-24

Applicant: 국방과학연구소

Inventor： 김인학 ,  김형렬 ,  독고욱

IPC: F42B15/20 ,  F42B12/02 ,  F42B17/00 ,  F42B12/76

CPC classification number: F42B19/005 ,  F42B17/00 ,  F42B19/46

Abstract: PURPOSE: A protection cover of a guided missile and a shock relieving method of the guided missile are provided to protect machines or electric devices of a guided missile with added reliability because a protection cover fractures to buffer an impact when the guided missile flies into water. CONSTITUTION: A protection cover of a guided missile(100) comprises a shell assembly(130), a shock absorbing ball(150), and a closing plate(120). The shell assembly comprises a plurality of supporters. One end of the shell assembly forms a closed plane and the other end of the shell assembly is formed into a shape of an opened hollow cylinder. The shock absorbing ball is housed inside the shell assembly. The closing plate is joined to the closed plane of the shell assembly and blocks the inflow of fluid.

Abstract translation: 目的：提供导弹的保护盖和导弹的减震方法，以保护导弹的机器或电气设备，增加可靠性，因为当导弹飞入水中时，保护盖破裂以缓冲冲击。 构成：导弹（100）的保护盖包括壳体组件（130），减震球（150）和封闭板（120）。 壳体组件包括多个支撑件。 壳体组件的一端形成一个闭合平面，并且壳体组件的另一端形成一个打开的中空圆柱体的形状。 减震球容纳在壳体内。 闭合板连接到壳组件的封闭平面并阻止流体流入。

公开(公告)号：KR100515027B1

公开(公告)日：2005-09-15

申请号：KR1020020002051

申请日：2002-01-14

Applicant: 국방과학연구소

Inventor： 김인학 ,  독고욱 ,  전완수

IPC: F41F3/06

CPC classification number: F42B19/46

Abstract: 본 발명은 초계기와 어뢰가 탑재된 밴드 어셈블리가 분리될 때 작동 케이블이 투하되는 어뢰에 영향을 미치지 않도록 하여 어뢰의 초기 투하자세를 안전하게 유지할 수 있고, 밴드 어셈블리와 어뢰가 분리될 때 밴드 어셈블리가 어뢰로부터 일정 거리만큼 이탈되기 때문에 어뢰에서 전개되는 낙하산과 밴드 어셈블리 사이의 간섭을 피할 수 있어 안정성 및 작동 신뢰성을 향상시킬 수 있는 어뢰 탑재용 밴드 어셈블리를 제공하기 위한 것으로, 어뢰에 감싸지는 한 쌍의 밴드와, 상기 밴드의 일측이 회전 가능하게 연결되고 초계기에 고정되는 파이론에 탑재되는 탑재부와, 상기 밴드의 타측에 탑재되고 어뢰에 감싸진 밴드를 잠금 및 잠금해제 작용을 하는 개폐부와, 상기 개폐부의 일측에 설치되어 개폐부의 록킹이 해제될 때 록킹 해제작용을 일정 시간� ��안 지연시키는 시간 지연장치와, 상기 밴드의 일측에 연결되어 상기 밴드에서 어뢰가 분리될 때 탄성력을 부여하는 탄성수단과, 상기 파이론의 지지대에 연결되고, 상기 시간 지연장치에 끼워지는 장전핀이 연결되어 상기 어뢰가 초계기로부터 분리될 때 시간 지연장치에서 장전핀을 이탈시켜 시간 지연장치를 작동시키는 케이블을 포함하여 구성된다.

公开(公告)号：KR1020020065996A

公开(公告)日：2002-08-14

申请号：KR1020010006150

申请日：2001-02-08

Applicant: 국방과학연구소

Inventor： 전완수 ,  독고욱 ,  김인학 ,  신용재 ,  김찬기 ,  박정기

IPC: B64D17/00

Abstract: PURPOSE: A parachute assembly for a light torpedo of an aircraft is provided to stabilize the torpedo by controlling the posture of the torpedo continuously after firing with deploying the parachute promptly and accurately. CONSTITUTION: A parachute assembly for a light torpedo is composed of a parachute having a canopy(1a) and a rope(1b); a parachute container(2) assembled with the lower part of the rope to contain the parachute, and opened in the upper part; a cover(4) closing the upper part of the parachute container; a pulling rope(5) fixed in an aircraft, and connected to the canopy to pull the parachute in falling the torpedo; an opening unit opening the cover; a pulling rope cutting unit cutting the parachute from the pulling rope; a rotation preventive assembling unit installed in the lower part of the parachute container to restrict rotation of the container, and to assemble with the light torpedo for separating by moving back and forth; and a sleeve(9) fixed in the lower part of the parachute container. The torpedo is controlled stably after firing with deploying the parachute promptly.

Abstract translation: 目的：提供用于飞机轻型鱼雷的降落伞组件，通过快速准确地部署降落伞，在射击后不间断地控制鱼雷的姿势来稳定鱼雷。 构成：用于轻型鱼雷的降落伞组件由具有顶篷（1a）和绳索（1b）的降落伞组成。 与绳索的下部组装以包含降落伞并在上部开口的降落伞容器（2）; 关闭降落伞容器的上部的盖（4）; 固定在飞机上的拉绳（5），并连接到伞架以在落下的鱼雷上拉降伞; 打开盖子的打开单元; 牵引绳切割单元从牵引绳切割降落伞; 旋转防止组装单元，其安装在降落伞容器的下部，以限制容器的旋转，并与轻型鱼雷组装以通过前后移动进行分离; 以及固定在降落伞容器的下部的套筒（9）。 射击后，鱼雷迅速地部署在降落伞上。

公开(公告)号：KR1020120056315A

公开(公告)日：2012-06-04

申请号：KR1020100117685

申请日：2010-11-24

Applicant: 국방과학연구소

Inventor： 김원제 ,  박성운 ,  독고욱

IPC: F42B19/38 ,  F42B8/12

CPC classification number: F42B19/38 ,  F42B8/28

Abstract: PURPOSE: A floating device, a floating system having the same, an underwater moving object, and a method for collecting the underwater moving object are provided to reduce operational costs by collecting expensive underwater moving bodies when underwater moving objects stop driving or abnormally stop operating. CONSTITUTION: A floating device comprises a high pressure vessel(10), a manifold, an air supply pipe(30), and a floating air bladder(40). The high pressure vessel stores air in a compressed state over a predetermined air pressure. The manifold is coupled with one end of the high pressure vessel and comprises a conduit line and a regulating unit. The air in the high pressure vessel is received or discharged through the conduit line. The regulating unit controls the flow of the air passing through the conduit line. The air supply pipe is connected with one end of an inner conduit line of the manifold. The floating air bladder is connected with the air supply pipe and receives the air from the air supply pipe to float underwater moving objects.

Abstract translation: 目的：提供一种浮动装置，具有该浮动装置的浮动系统，水下运动物体和用于收集水下运动物体的方法，以在水下运动物体停止行驶或异常停止运行时通过收集昂贵的水下移动体来降低运行成本。 构成：浮动装置包括高压容器（10），歧管，空气供应管（30）和浮动气囊（40）。 高压容器在预定的空气压力下存储处于压缩状态的空气。 歧管与高压容器的一端连接并且包括导管线和调节单元。 高压容器中的空气通过导管接收或排出。 调节单元控制通过导管线的空气的流动。 供气管与歧管内管道的一端连接。 浮动气囊与供气管连接，并从供气管接收空气，以浮动水下运动物体。

公开(公告)号：KR100420932B1

公开(公告)日：2004-03-04

申请号：KR1020010006150

申请日：2001-02-08

Applicant: 국방과학연구소

Inventor： 전완수 ,  독고욱 ,  김인학 ,  신용재 ,  김찬기 ,  박정기

IPC: B64D17/00

Abstract: PURPOSE: A parachute assembly for a light torpedo of an aircraft is provided to stabilize the torpedo by controlling the posture of the torpedo continuously after firing with deploying the parachute promptly and accurately. CONSTITUTION: A parachute assembly for a light torpedo is composed of a parachute having a canopy(1a) and a rope(1b); a parachute container(2) assembled with the lower part of the rope to contain the parachute, and opened in the upper part; a cover(4) closing the upper part of the parachute container; a pulling rope(5) fixed in an aircraft, and connected to the canopy to pull the parachute in falling the torpedo; an opening unit opening the cover; a pulling rope cutting unit cutting the parachute from the pulling rope; a rotation preventive assembling unit installed in the lower part of the parachute container to restrict rotation of the container, and to assemble with the light torpedo for separating by moving back and forth; and a sleeve(9) fixed in the lower part of the parachute container. The torpedo is controlled stably after firing with deploying the parachute promptly.

Abstract translation: 目的：提供一种用于飞机的轻型鱼雷的降落伞组件，通过迅速和准确地部署降落伞并在发射后连续控制鱼雷的姿态来稳定鱼雷。 一种用于轻型鱼雷的降落伞组件，包括一个具有顶盖（1a）和绳索（1b）的降落伞; 降落伞容器（2），其与绳子的下部组装在一起以容纳降落伞，并在上部开口; 一个封闭降落伞容器上部的盖子（4） 固定在飞机上的牵引绳（5），并连接到天篷以拉落伞降落鱼雷; 打开盖的打开单元; 牵引绳切割单元，用于从牵引绳切割降落伞; 防旋组装单元，其安装在降落伞容器的下部以限制容器的旋转，并且通过来回移动而与轻型鱼雷组装以进行分离; 和固定在降落伞容器下部的套筒（9）。 发射后迅速部署降落伞，鱼雷控制稳定。

公开(公告)号：KR1020030061522A

公开(公告)日：2003-07-22

申请号：KR1020020002051

申请日：2002-01-14

Applicant: 국방과학연구소

Inventor： 김인학 ,  독고욱 ,  전완수

IPC: F41F3/06

CPC classification number: F42B19/46 ,  F41F3/08

Abstract: PURPOSE: A band assembly for mounting a torpedo is provided to stably keep the early dropping position of the torpedo by preventing a cable from influencing the torpedo when the band assembly is separated from a patrol plane. CONSTITUTION: A couple of bands(4) are covered with a torpedo(2). A mounting unit(6) is connected to one side of the bands, and is mounted on a pylon fixed on a patrol plane. An opening/closing unit(8) is mounted on the other side of the bands, and locks/unlocks the bands. A delaying unit(10) is installed at one side of the opening/closing unit, and delays the unlocking of the opening/closing unit when the opening/closing unit is unlocked. An elastic unit is connected to one side of the bands, and applies elasticity to the bands when the torpedo is separated from the bands. A cable(12) is connected to a loading pin fit into the delaying unit, and separates the loading pin from the delaying unit and operates the delaying unit when the torpedo is separated from the patrol plane.

Abstract translation: 目的：提供用于安装鱼雷的带组件，以便当带组件与巡视平面分离时，通过防止电缆对鱼雷的影响来稳定地保持鱼雷的早期落下位置。 构成：几个乐队（4）被鱼雷（2）覆盖。 安装单元（6）连接到带的一侧，并安装在固定在巡视平面上的挂架上。 开/关单元（8）安装在带的另一侧，并锁定/解锁带。 延迟单元（10）安装在打开/关闭单元的一侧，并且当打开/关闭单元被解锁时，延迟打开/关闭单元的解锁。 弹性单元连接到带的一侧，并且当鱼雷与带分离时，弹性单元对带施加弹性。 电缆（12）连接到装配到延迟单元中的装载销，并将装载销与延迟装置分离，并且当鱼雷与巡逻平面分离时，操作延迟装置。