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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
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。
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公开(公告)号：KR1020010105034A
公开(公告)日：2001-11-28
申请号：KR1020000026688
申请日：2000-05-18
Applicant: 국방과학연구소
Inventor： 김인학
IPC: F16B2/08
Abstract: 본 발명은 비행기나 선박 등에 보관되어 운반되는 물품을 용이하면서도 안전하게 장착할 수 있고, 안전하게 분리할 수 있는 서스펜션 밴드 유니트에 관한 것이다. 상기 서스펜션 밴드 유니트는 러그에 의하여 항공기와 용이하게 체결할 수 있다. 또한, 상부판의 양단에 밴드를 회동가능하게 설치하기 때문에 물품을 용이하게 착탈할 수 있다. 또한, 시간지연장치가 마련되므로, 소정의 시간이 경과한 후에 서스펜션 밴드 유니트가 분리된다. 그러므로, 서스펜션 밴드 유니트와 물품 사이에는 간섭이 발생하지 않는 효과가 있다.
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公开(公告)号：KR1020120058335A
公开(公告)日：2012-06-07
申请号：KR1020100120064
申请日：2010-11-29
Applicant: 국방과학연구소
Inventor： 김인학
Abstract: PURPOSE: A shell assembly, a guided missile therewith, and a shock reducing method of the guided missile are provided to securely protect the front body of the guided missile when the shell assembly is launched. CONSTITUTION: A shell assembly(130) comprises a shell(134), a first support(131), and a second support(132). One end of the shell has a mounting surface, and the other end is formed in a hollow cylindrical shape. The first support is attached on the inner surface of the shell and supports an axial load. The second support is coupled to the first support and is separated from the first support by lateral expansion pressure. And the second support transfers the lateral expansion pressure to the shell.
Abstract translation: 目的：提供一种外壳组件，导弹及其导弹的减震方法，以便在外壳组件启动时可靠地保护导弹的前身。 构成：壳体组件（130）包括壳体（134），第一支撑件（131）和第二支撑件（132）。 壳的一端具有安装表面，另一端形成为中空圆柱形。 第一支撑件附接在壳体的内表面并且支撑轴向载荷。 第二支撑件联接到第一支撑件并且通过横向膨胀压力与第一支撑件分离。 第二支撑将侧向膨胀压力传递到壳体。
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公开(公告)号：KR1020120021544A
公开(公告)日：2012-03-09
申请号：KR1020100076030
申请日：2010-08-06
Applicant: 국방과학연구소
Abstract: PURPOSE: A deploying bag, parachute assembly comprising the same, and method of assembling a parachute assembly are provided to reduce impact in the initial deploying of a parachute and reduce the fluctuation of a target due to impact. CONSTITUTION: A deploying bag(10) comprises a body(13), a first wind bag(12), and a coupling unit(15). The body holds the canopy of a parachute, and the body is separated while the canopy gets out when the parachute is deployed. The first wind bag is attached to the side of the body and is opened by drag when falling. The coupling unit is attached to one end of the body and is coupled to the wire of the parachute.
Abstract translation: 目的：提供一种包括该降落伞组件的部署袋，降落伞组件以及组装降落伞组件的方法，以减少降落伞初始部署中的影响并减少由于冲击引起的目标的波动。 构成：展开袋（10）包括主体（13），第一风袋（12）和联接单元（15）。 身体保持降落伞的冠层，当降落伞被部署时，身体被分开，而伞顶则出来。 第一个风袋附着在身体的侧面，并在下落时被拖动打开。 联接单元连接到主体的一端，并连接到降落伞的导线上。
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公开(公告)号：KR100503634B1
公开(公告)日：2005-07-26
申请号：KR1020010020821
申请日：2001-04-18
Applicant: 국방과학연구소
Inventor： 김인학
IPC: B64D1/02
Abstract: 본 발명은 항공기 투하용 물체의 감속력을 이용한 추출장치에 관한 것으로, 더욱 상세하게는 상, 하부가 개방되고, 상부에서 하부로 갈수록 좁아지는 원뿔형으로 형성되며, 상기 투하 물체의 전면부에 장착되며, 하단부의 내측에 스톱퍼가 형성된 장착부와, 상기 장착부의 스톱퍼에 고정 가능한 걸림부가 내측면에서 상부로 연장 형성되고, 상기 장착부로부터 연장 형성되어 원뿔을 이루는 추출부와, 상기 추출부의 내측 저면에 길이 방향으로 고정 설치되는 샤프트와, 상기 추출부의 걸림부와 결합된 상태에서 상기 물체에 감속력이 발생하면, 상기 샤프트를 따라 이동되어 상기 추출부에 충격을 가해 상기 추출부를 상기 물체에서 이탈시키는 이동부 및 상기 장착부와 추출부 및 이동부를 고정하는 안전핀을 포함하는 것을 특징으로 한다.
따라서 상기와 같이 구성된 본 발명에 따르면 항공기 투하용 물체의 공기 마찰을 줄이도록 전면부에 부착되어, 물체가 항공기에서 투하될 시 낙하산에 의해 감속력이 발생되면 감속력에 의해 물체의 전면부에서 이탈되도록 할 수 있다.-
Patent Agency Ranking
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
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。
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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
IPC: F41F3/06
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。
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公开(公告)号：KR1020020065995A
公开(公告)日：2002-08-14
申请号：KR1020010006148
申请日：2001-02-08
Applicant: 국방과학연구소
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：提供用于轻型鱼雷的水上飞机的降落伞组件，以便通过快速，准确地部署降落伞，在射击后连续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）; 固定在鱼雷管中的拉绳（5）连接到顶篷以在降落伞上点燃鱼雷; 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; 组装单元，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）。 使用降落伞组件进行射击后，可以稳定地控制鱼雷的姿势。
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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
Abstract: 본발명의일 실시예에따르는보호덮개는복수의지지체를포함하며, 일단은밀폐면을형성하고, 타단은개구된중공의원통으로형성되는쉘조립체와, 상기쉘조립체의내부에수용되는완충공및 상기쉘조립체의밀폐면과결합하여, 유체의유입을막는밀폐판을포함함으로써, 발사및 비행시에는견고하게유도탄의전방체를보호하고, 입수시에는충격을완충하도록파열됨으로써, 정밀타격을목표로하는유도탄의기계또는전자장치들이신뢰성을유지하도록보호할수 있다.
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公开(公告)号：KR1020120027870A
公开(公告)日：2012-03-22
申请号：KR1020100089681
申请日：2010-09-13
Applicant: 국방과학연구소
CPC classification number: F42B10/56 , B64D17/343 , B64D17/62
Abstract: PURPOSE: A ripping device, a parachute, and a guided missile therewith are provided to improve the movement stability of an object when the object falls down. CONSTITUTION: A ripping device(10) for a parachute comprises a body(11), a perforated part(16), and an actuating unit. The body is attached on a parachute and has a cutting knife. The perforated part is formed in the width direction of the body. Ripping lines(23,24) covering the canopy of the parachute penetrate through the perforated part. The actuating unit is coupled to the cutting knife and controls the falling speed of the parachute by cutting the ripping lines through the cutting knife.
Abstract translation: 目的：提供翻录装置，降落伞和导弹，以提高对象跌落时物体的运动稳定性。 构成：用于降落伞的撕裂装置（10）包括主体（11），穿孔部分（16）和致动单元。 身体附在降落伞上，并有切刀。 穿孔部分沿主体的宽度方向形成。 覆盖降落伞顶盖的折叠线（23,24）穿过穿孔部分。 致动单元联接到切割刀，并通过切割刀切割撕裂线来控制降落伞的下落速度。
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