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公开(公告)号：KR1020110008666A
公开(公告)日：2011-01-27
申请号：KR1020090066128
申请日：2009-07-21
Applicant: 국방과학연구소
IPC: H02P1/28
CPC classification number: H02P1/28 , H02P25/062 , H02P25/18
Abstract: PURPOSE: A soft start device and a method thereof are provided to prevent the voltage drop of a power supply device by using a contactless power device with a Y-connection state. CONSTITUTION: One side junction part(304a) of a first on/off state switch(304) is connected to the output terminal of a three-phase induction motor(303). One side junction part(305a) of a second on/off state switch(305) is connected to the output terminal of the three-phase induction motor. A contactless power device(302) supplies a voltage to the induction motor and softly starts the motor. A control part(301) outputs a control signal for a Y-connection to the first on/off state switch. The control part outputs a control signal for a delta connection to the second on/off state switch.
Abstract translation: 目的：提供软启动装置及其方法，以通过使用具有Y连接状态的非接触式电力装置来防止电源装置的电压下降。 构成：第一开关状态开关（304）的一侧接合部（304a）与三相感应电动机（303）的输出端子连接。 第二开关状态开关（305）的一侧接合部（305a）与三相感应电动机的输出端子连接。 非接触式电力设备（302）向感应电动机提供电压并轻轻启动电动机。 控制部件（301）向第一开/关状态开关输出用于Y连接的控制信号。 控制部分输出用于与第二开/关状态开关的增量连接的控制信号。
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公开(公告)号：KR101310087B1
公开(公告)日：2013-09-23
申请号：KR1020110094271
申请日：2011-09-19
Applicant: 국방과학연구소
Inventor： 변영철
Abstract: 본 발명은 장기간 유도탄이 탑재되어 보관, 취급 및 운용되는 캐니스터 내에서 유도탄의 엔진 혹은 구동장치 등의 유도탄 부품으로부터 누출될 수 있는 연료 및 오일을 감시할 수 있도록 하는 누유감시장치에 관한 것이다.
이에 본 발명은, 유도탄의 장착/이탈 상태를 확인하는 유도탄 커넥터; 유도탄 캐니스터 내부의 누유 여부를 감시하는 누유감시회로; 누유된 액체감지신호를 상기 누유감시회로에 전달하는 액체레벨센서; 및 상기 누유 여부에 따라 유도탄의 발사를 제어하는 발사플랫폼 제어장치;를 포함하고, 유도탄 장착/이탈 신호를 이용하여 유도탄 장착 상태 및 유도탄 발사 상태에서 유도탄 캐니스터 내부의 누유 여부를 감시할 수 있는 유도탄 캐니스터 누유감시장치를 제공한다.-
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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：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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Patent Agency Ranking
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公开(公告)号：KR1020130030657A
公开(公告)日：2013-03-27
申请号：KR1020110094271
申请日：2011-09-19
Applicant: 국방과학연구소
Inventor： 변영철
Abstract: PURPOSE: A monitoring device of guided missile canister oil leakage is provided to monitor the oil leakage when installing the guided missile and to stably control launch by blocking error signal of sensor output when separating the guided missile. CONSTITUTION: A monitoring device(1) of guided missile canister oil leakage comprises a guided missile connector(5), an oil leakage monitoring circuit(12), a liquid level sensor(11), and a launching platform control device(3). The guided missile connector checks installation and separation of the guided missile. The oil leakage monitoring circuit monitors the oil leakage whether or not inside the guided missile canister. The liquid level sensor delivers a liquid monitoring signal which is oil-leaked to oil leakage monitoring circuit. [Reference numerals] (1) Oil leakage monitoring device; (12) Oil leakage monitoring circuit; (3) Launching platform control device; (5) Guided missile umbilical connector; (AA) Guided missile canister; (BB) Liquid sensing signal; (CC) Guided missile mounting/removal signal
Abstract translation: 目的：提供导弹罐漏油监测装置，监控导弹安装时的漏油情况，分离导弹时，通过阻挡传感器输出的误差信号稳定控制发射。 构成：导弹油泄漏监控装置（1）包括导弹连接器（5），漏油监测电路（12），液位传感器（11）和发射平台控制装置（3）。 导弹连接器检查导弹的安装和分离。 漏油监控电路监控导弹罐内是否漏油。 液位传感器提供液体监测信号，该信号被漏油到漏油监测电路。 （附图标记）（1）漏油监视装置; （12）漏油监控电路; （3）启动平台控制装置; （5）导弹脐带连接器; （AA）导弹罐; （BB）液体检测信号; （CC）引导导弹安装/拆卸信号
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公开(公告)号：KR101210289B1
公开(公告)日：2012-12-10
申请号：KR1020100070646
申请日：2010-07-21
Applicant: 국방과학연구소
Abstract: 본발명은로터리안전스위치및 이를구비하는유도탄발사장치에관한것으로, 상기로터리안전스위치는, 잠금상태에서잠금해제상태로전환되면, 발사관에동작신호가전달되는동작스위치부와, 상기동작스위치부와결합되며, 회전에의하여상기동작스위치부의잠금및 잠금해제상태가스위칭되는스위치노브와, 상기스위치노브를통관하며하부에형성되는핀부재를구비하는작동버튼와, 동작스위치부의잠금및 잠금해제상태에서각각상기스위치노브의움직임을구속시키며, 상기핀부재와맞닿도록형성되어상기작동버튼이가압되면스위치노브의구속을해제시키도록형성되는래치핀및 상기래치핀이지지되며, 상기동작스위치부가통관하는고정판을포함한다. 이에의하여본 발명은강한진동이나충격에도로타리스위치가비정상적으로작동하지않도록고정시켜주며, 버튼을연동시켜운용자가쉽게고정을해제시킬수 있도록하여로터리안전스위치를제공한다.
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公开(公告)号：KR101794762B1
公开(公告)日：2017-11-07
申请号：KR1020160030482
申请日：2016-03-14
Applicant: 국방과학연구소
Abstract: 본발명은유도탄의날개지지대에관한것으로, 유도탄동체; 상기유도탄동체에구비되어상기유도탄동체로부터멀어지는방향으로전개되는다수의날개; 및상기날개의단부에구비되어상기날개를지지하는지지대를포함하고, 상기지지대는상기유도탄을수용하는원통형상의발사관에접촉하도록형성되는것을특징으로하는유도탄날개지지구조에대한것이다.
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