-
公开(公告)号：KR101430581B1
公开(公告)日：2014-08-18
申请号：KR1020140026008
申请日：2014-03-05
Applicant: 국방과학연구소
Abstract: The present invention relates to a shock sensor using a crush switch (100) with a flexible printed circuit board (FPCB) and an insulation sheet. A gap between a disconnected wire or a connected wire and a cut unit for cutting the wire is filled with polycarbonate containing 40% of glass or is empty. Only one line from each wire is connected so as to be small and easily installed compared to an existing method which is impossible to check the shock sensor after assembly. Further, the present invention has excellent safety and operation reliabilities and facilitates function checks in an electrically conductive state on an interface by ensuring the same output signals after a guided missile is assembled.
Abstract translation: 本发明涉及使用具有柔性印刷电路板（FPCB）和绝缘片的压碎开关（100）的冲击传感器。 断线或连接线之间的间隙和用于切割线的切割单元填充有包含40％玻璃的聚碳酸酯或为空。 与现有的方法相比，每根电线只有一条线连接成小而易于安装，这在组装后无法检查冲击传感器。 此外，本发明具有优异的安全性和操作可靠性，并且通过在组装导弹之后确保相同的输出信号，便于在接口上的导电状态下的功能检查。
-
公开(公告)号：KR101392223B1
公开(公告)日：2014-05-08
申请号：KR1020130141405
申请日：2013-11-20
Applicant: 국방과학연구소
CPC classification number: F42C21/00
Abstract: The present invention relates to an ignition test device and a method for the same. The ignition test device includes a mounting device for mounting a fuse; a cable electrically connecting the fuse and an initiating pipe in order to transmit an ignition signal from the fuse to the initiating pipe; and a safety device which accommodates the initiating pipe and includes a safety device with a case on which a hole which the cable passes through is arranged and which forms a sealed space in order for the initiating pipe to be detonated in the sealed space.
Abstract translation: 点火试验装置及其方法技术领域本发明涉及一种点火试验装置及其方法。 点火测试装置包括用于安装保险丝的安装装置; 将熔断器与起动管电连接以将点火信号从保险丝传输到起动管的电缆; 以及安装装置，其容纳起动管，并且包括具有壳体的安全装置，所述电缆穿过所述壳体，并且形成密封空间，以使所述起动管在所述密封空间中被引爆。
-
公开(公告)号：KR101360108B1
公开(公告)日：2014-02-11
申请号：KR1020130154145
申请日：2013-12-11
Applicant: 국방과학연구소
CPC classification number: F42C21/00
Abstract: The present invention relates to a fuse tester for checking a detonating function of an electronic fuse. As a fuse tester for testing a fuse which a groove is formed for a member to be inserted in one side and which generates a current in order to perform a detonating function when a predetermined condition is satisfied, the present invention comprises: a connecting unit which is formed to engage in the groove, is detachable from the groove, forms a closed circuit with a circuit prepared in the fuse when it is attached, and receives a current generated from the fuse; and a lamp unit which is formed at one end of the connecting unit, is connected to a handle unit made of an insulating material and the connecting unit, and functions when a current is transmitted through the connecting unit.
Abstract translation: 本发明涉及一种用于检查电子保险丝的引爆功能的保险丝测试器。 作为用于测试保险丝的保险丝测试器，其中，当满足预定条件时，形成用于插入一侧的构件的槽并且产生电流以便执行引爆功能的保险丝，本发明包括：连接单元， 形成为接合在凹槽中，可从凹槽拆卸，当熔丝被安装时，利用制备在熔丝中的电路形成闭合电路，并且接收从熔丝产生的电流; 并且形成在连接单元的一端的灯单元连接到由绝缘材料制成的手柄单元和连接单元，并且当电流通过连接单元传输时起作用。
-
公开(公告)号：KR101343422B1
公开(公告)日：2013-12-20
申请号：KR1020120093266
申请日：2012-08-24
Applicant: 국방과학연구소
Abstract: A fuse system according to an embodiment of the present invention comprises: a step of transmitting information about firing timing to a control circuit when a firing detection sensor inside the fuse operates; a step of operating a timing device to count flight time and measuring a flight altitude by the control circuit when the information about firing timing is received: a step of obtaining an altitude change rate from the measured flight altitude and flight time and calculating the firing range of a bullet from the altitude change rate; a step of determining whether or not the bullet falls down based on the calculated firing range and setting an altitude measuring range when the bullet falls down; and a step of determining a final firing range from the measured flight altitude when the bullet reaches the altitude measuring section and determining the explosion altitude of the bullet based on the final firing range and firing tables stored in a memory. [Reference numerals] (100) Operation mode and explosion altitude charger;(110) Operation mode and explosion altitude displayer;(120) Communication interface (Transmission/Reception);(130) Operation mode/Explosion altitude input and data generator;(200) Fuse system;(210) Communication interface (Reception/Transmission);(220) Power conversion circuit;(230) Battery for fuses or power generator;(240) Control circuit unit;(241) Control a transmitter;(242) Detect altitude information;(243) Memory (firing table/explosion altitude);(244) Calculation and control, Bullet flight altitude calculation/Firing range determination/Detonation altitude determination/Detonation command generation;(250) Bullet firing sensor;(260) Transceiving unit;(261) Transmitting unit;(262) Reception unit;(263) Transmission antenna;(264) Receiving antenna;(270) Oscillator circuit;(280) Detonator circuit;(290) Safe loading device (Explosive type);(291) Fuse check circuit
Abstract translation: 根据本发明实施例的保险丝系统包括：当保险丝内部的点火检测传感器工作时，向控制电路发送关于点火时间的信息的步骤; 当接收到关于点火时间的信息时，操作定时装置来计算飞行时间并由控制电路测量飞行高度的步骤：从所测量的飞行高度和飞行时间获得高度变化率并计算起飞范围的步骤 从高度变化率的一个子弹; 基于所计算的击发范围来确定子弹是否下降并且在子弹落下时设置高度测量范围的步骤; 以及当子弹到达高度测量部分时根据测量的飞行高度确定最终射击范围并基于存储在存储器中的最终射击范围和击发表确定子弹的爆炸高度的步骤。 （100）操作模式和爆炸高度充电器;（110）操作模式和爆炸高度显示器;（120）通信接口（发送/接收）;（130）操作模式/爆炸高度输入和数据发生器;（200 保险丝系统;（210）通信接口（接收/发送）;（220）电源转换电路;（230）保险丝或发电机电池;（240）控制电路单元;（241）控制发射机;（242） 高度信息;（243）记录（发射台/爆炸高度）;（244）计算和控制，子弹飞行高度计算/射击范围确定/爆轰高度确定/爆震命令生成;（250）子弹击发传感器;（260）收发 单元;（261）发送单元;（262）接收单元;（263）发送天线;（264）接收天线;（270）振荡电路;（280）雷管电路;（290）安全加载装置（爆炸型） 291）保险丝检查电路
-
-
-
Search Results
14
records
(took 0.02 seconds)
