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公开(公告)号：KR101235036B1
公开(公告)日：2013-02-21
申请号：KR1020120000254
申请日：2012-01-02
Applicant: 국방과학연구소
IPC: G01P3/64
Abstract: PURPOSE: A water speed measuring apparatus and a measuring method of a vehicle are provided to automatically measure a passage time of test vehicle, thereby reducing artificial error and improving test reliability. CONSTITUTION: A water speed measuring apparatus(100) comprises a controller(110), a sensor part(120), and a communication part(130). A sensor part comprises a transmission sensor and a receiving sensor. The communication part receives a signal from the transmission sensor of a water vehicle and a passage signal from receiving sensors. The controller measures the water speed of the water vehicle based on the received passage signal. The transmission sensor transmits a sensed signal to the receiving sensor. The Passage signal is generated based on a cut off of the sensed signal by the passage of the water vehicle. [Reference numerals] (110) Controller; (120) Sensor part; (130) Communication part; (140) Data acquisition part
Abstract translation: 目的：提供一种水速测量装置和车辆测量方法，以自动测量测试车辆的通过时间，从而减少人为误差，提高测试可靠性。 构成：水速测量装置（100）包括控制器（110），传感器部分（120）和通信部分（130）。 传感器部分包括传输传感器和接收传感器。 通信部分接收来自水车辆的传动传感器的信号和来自接收传感器的通过信号。 控制器根据接收到的通过信号测量水车的水速。 传输传感器将感测到的信号传送到接收传感器。 基于通过水车辆通过的感测信号的切断产生通道信号。 （附图标记）（110）控制器; （120）传感器部件; （130）通讯部分; （140）数据采集部分
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公开(公告)号：KR101220108B1
公开(公告)日：2013-01-11
申请号：KR1020100089681
申请日：2010-09-13
Applicant: 국방과학연구소
Abstract: 본 발명의 일 실시예에 따르는 낙하산의 리핑장치는 낙하산에 부착되고, 내부에 절단날을 구비하는 몸체부와, 상기 몸체부의 너비방향으로 상기 낙하산의 캐노피를 감싸는 리핑라인이 통관하도록 형성된 관통부 및 상기 절단날과 결합되는 구동수단을 포함하고, 상기 구동수단은 작동신호를 받은 후 일정시간이 지나 구동되어, 상기 리핑라인을 절단함으로써, 낙하산의 낙하속도를 조절함으로써, 고속으로 이동하는 피운반체에 전개충격력을 완화시키고, 피운반체의 낙하시 운동안정성을 확보할 수 있다.
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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
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。
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公开(公告)号：KR101292078B1
公开(公告)日：2013-07-31
申请号：KR1020100076030
申请日：2010-08-06
Applicant: 국방과학연구소
Abstract: 본 발명의 일 실시예에 따르는 낙하산의 전개낭은 캐노피가 내부에 수용되도록 형성되는 몸체와, 상기 몸체의 측면에 부착되고, 낙하시 항력을 받아 펼쳐지도록 형성되는 제1바람주머니 및 상기 몸체의 길이방향의 일단에 부착되고, 낙하산의 산줄과 끼움 결합되는 결합부를 포함함으로써, 낙하산의 초기 전개시 전개충격력을 감소시키고, 충격에 의한 피운반체의 동요를 줄일 수 있다.
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公开(公告)号：KR101254995B1
公开(公告)日：2013-04-17
申请号：KR1020110010341
申请日：2011-02-01
Applicant: 국방과학연구소
Abstract: 본 발명의 일 실시예에 따르는 충격장치는 대상물의 일면에 접촉하도록 형성되는 충격판과, 일단이 상기 충격판에 연결되는 가이드 로드와, 상기 가이드 로드의 타단과 기어 결합되는 엔코더와, 상기 가이드 로드의 외주면을 따라 자유 낙하하도록 형성되는 중공을 구비한 무게추와, 상기 가이드 로드를 따라 상하이동가능하게 상기 무게추의 상부에 배치되며, 자력에 의해 상기 무게추가 착탈되도록 형성되는 전자석 홀더를 포함함으로써, 장치의 자동화와 무게추의 정확한 위치제어로 인한 사용 효율성의 증대와 시험의 정확성을 향상시킬 수 있다.
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Patent Agency Ranking
公开(公告)号：KR1020110041777A
公开(公告)日：2011-04-22
申请号：KR1020090098761
申请日：2009-10-16
Applicant: 국방과학연구소
Abstract: PURPOSE: A device for measuring the strength of the ground using a servo motor is provided to enable the accurate measurement of weak soil foundation from the subsidence of the ground according to vertical load. CONSTITUTION: A device for measuring the strength of the ground using a servo motor comprises a mainframe(10), a servo motor(15), a gear-box(16), an elevating member(20), a subsidence sensing unit(30), an adapter(26) for load-settlement measurement, a pressure plate, and a controller. The mainframe comprises an excavator adapter(50). The excavator adapter is assembled with the bucket fixture of the excavator. The elevating member comprises a screw shaft(21) and a ball screw member(23). The elevating member moves up and down inside the mainframe by the servo motor. The subsidence sensing unit senses the vertical movement of the elevating member. A load cell is installed in the adapter for the load-settlement measurement. The lower end of the adapter for the load-settlement measurement is projected to the lower part of the main frame. The pressure plate is detachably assembled with the lower end of the adapter for the load-settlement measurement. The controller controls the servo motor.
Abstract translation: 目的：提供一种使用伺服电机测量地面强度的装置，以便根据垂直载荷从地面沉降中精确测量弱土基础。 构成：使用伺服电动机测量地面强度的装置包括主机（10），伺服电机（15），齿轮箱（16），升降构件（20），沉降感测单元（30） ），用于负载沉降测量的适配器（26），压力板和控制器。 主机包括挖掘机适配器（50）。 挖掘机适配器与挖掘机的铲斗固定装置组装。 升降构件包括螺杆轴（21）和滚珠丝杠构件（23）。 升降构件通过伺服马达在主机内部上下移动。 沉降感测单元感测升降构件的垂直运动。 负载传感器安装在适配器中进行负载沉降测量。 用于负载沉降测量的适配器的下端投影到主框架的下部。 压力板与适配器的下端可拆卸地组装用于负载沉降测量。 控制器控制伺服电机。
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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
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。
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公开(公告)号：KR101563217B1
公开(公告)日：2015-11-06
申请号：KR1020140086957
申请日：2014-07-10
Applicant: 국방과학연구소
IPC: H04L12/28
CPC classification number: H04L12/4015 , H04L2012/40215 , H04L2012/40273
Abstract: 본발명은차량에서출력되는 CAN신호를획득하기위한차량용 CAN 신호획득장치및 그방법에관한것으로, 계측할 CAN신호데이터를설정및 저장하는사용자운영장치; 차량의모든 CAN데이터를감지하는 CAN센서; 상기 CAN신호의이외의일반차량데이터를감지하는차량센서; 상기감지된모든 CAN데이터중에서계측할 CAN데이터를샘플링한후 상기감지된일반차량데이터와동기화하여표본화하는하드웨어처리부; 및상기하드웨어처리부에서표본화된데이터를물리적인값으로변환하여상기사용자운영장치로출력하는소프트웨어처리부;를포함한다.
Abstract translation: 本发明涉及一种用于获得用于车辆的控制器局域网（CAN）信号的装置和方法，其目的是获得由车辆输出的CAN信号，其中本发明的装置包括：用户操作装置 设置和存储要测量的CAN信号数据; CAN传感器感测车辆的所有CAN数据; 检测除CAN信号之外的一般车辆数据的车辆传感器; 硬件处理单元对所有所感测的CAN数据中的待测量的CAN数据进行采样，然后与感测到的一般车辆数据同步以进行采样; 以及软件处理单元，将在硬件处理单元中采样的数据转换为物理值，以将值输出到用户操作装置。
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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：KR101042968B1
公开(公告)日：2011-06-20
申请号：KR1020090126484
申请日：2009-12-18
Applicant: 국방과학연구소
Abstract: PURPOSE: An apparatus for measuring the shear displacement of soil using a servo motor is provided to estimate the shearing strength of soil by simultaneously applying vertical and shearing loads to the soil. CONSTITUTION: An apparatus for measuring the shear displacement of soil using a servo motor comprises a main frame(10), a servo motor(15), a gear box(16), an elevation member(20), an adapter(40) for measuring shearing displacement, and a controller. An excavator adapter(50) is formed on the top of the main frame. The servo motor and the gear box are installed in a support(14) formed in the inner top of the main frame. The elevation member has a ball screw member(23). The adapter is detachably coupled to the elevation member and measures the shearing torque of soil using a shear ring(47) protruded from the bottom of the main frame. The controller calculates the shearing force of the soil using the signal of the adapter.
Abstract translation: 目的：提供一种使用伺服电机测量土体剪切位移的装置，通过同时对土壤施加垂直和剪切载荷来估算土体的剪切强度。 一种用于使用伺服电动机测量土壤剪切位移的设备，包括主框架（10），伺服电机（15），齿轮箱（16），升降构件（20），适配器（40） 测量剪切位移和控制器。 挖掘机适配器（50）形成在主框架的顶部。 伺服电动机和齿轮箱安装在形成在主框架的内部顶部中的支撑件（14）中。 升降构件具有滚珠丝杠构件（23）。 适配器可拆卸地联接到升降构件并且使用从主框架的底部突出的剪切环（47）来测量土壤的剪切力矩。 控制器使用适配器的信号计算土壤的剪切力。
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