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公开(公告)号：KR101336738B1
公开(公告)日：2013-12-04
申请号：KR1020130082197
申请日：2013-07-12
Applicant: 국방과학연구소
Abstract: The present invention relates to a propulsion unit for high-speed driving on an underwater track. Disclosed is the propulsion unit for high-speed driving on the underwater track comprising: a main body in which components are built in, a hollow unit is formed in a shaft direction inside the center, a front end part is sealed, and a rear end part is opened; a fuel chamber formed at the inner front end of the main body and in which the propulsion unit is built; a nozzle assembly for covering the rear end of the main body and increasing the fluid speed of discharged combustion gas; and a pipe exposed to the outside by penetrating through the center of the hollow unit and the nozzle assembly.
Abstract translation: 本发明涉及一种用于在水下轨道上高速行驶的推进单元。 公开了用于在水下轨道上进行高速行驶的推进单元，其特征在于，包括：内置有部件的主体，中心部的轴向形成中空部，密封前端部，后端部 部分打开 燃料室，形成在主体的内前端，其中构建有推进单元; 用于覆盖主体的后端并提高排出的燃烧气体的流体速度的喷嘴组件; 以及通过穿过中空单元和喷嘴组件的中心而暴露于外部的管。
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公开(公告)号：KR101347166B1
公开(公告)日：2014-01-03
申请号：KR1020130094641
申请日：2013-08-09
Applicant: 국방과학연구소
Abstract: A support device for the underwater vehicle, according to an embodiment of the invention, comprises of: a fixed part of the first and second spaced apart from each other; a rope part which connects the fixed part of the first and second in the water and which passes through the hollow formed in the underwater vehicle; and an extension loader which pulls one side of the rope part in order for the rope part to maintain the tension above a certain level.
Abstract translation: 根据本发明的实施例的用于水下航行器的支撑装置包括：第一和第二间隔开的固定部分; 绳索部分，其连接第一和第二在水中的固定部分，并穿过形成在水下航行器中的中空; 以及拉伸装置，其拉动绳索部分的一侧，以使绳索部分将张力保持在一定水平以上。
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公开(公告)号：KR101292079B1
公开(公告)日：2013-07-31
申请号：KR1020110120316
申请日：2011-11-17
Applicant: 국방과학연구소
Inventor： 이도형
Abstract: 본 발명의 일 실시예에 따르는 일면이 개구된 개구부를 구비하는 하우징과, 상기 하우징 내에 일정 압력으로 충진되고, 제1 온도이상으로 가열되면 발화되도록 형성되는 신호 화약 충진부와, 상기 신호 화약 충진부를 덮도록 상기 하우징에 배치되는 제1 보조 화약부와, 보론 나이트라이드(Boron Nitride) 분말을 포함하고, 상기 제1 보조 화약부를 덮도록 형성되는 제1 덮개부 및 상기 제1 덮개부를 덮으며, 상기 하우징을 밀폐시키는 제2 덮개부를 포함함으로써, 화재(온도)를 독자적으로 감지하고 자동 점화되어 추진제를 정상 연소시킬 수 있다.
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公开(公告)号：KR1020130054744A
公开(公告)日：2013-05-27
申请号：KR1020110120316
申请日：2011-11-17
Applicant: 국방과학연구소
Inventor： 이도형
Abstract: PURPOSE: A heat sensing igniter, a heat sensing automatic lighter, and a flight vehicle including the same are provided to mitigate a danger by sensing fire for automatically igniting and normally combusting a propellant ahead of the intense reaction of the propellant in the event of fire. CONSTITUTION: A heat sensing igniter comprises a housing, a signal gunpowder filler, a first sub gunpowder part, a first cover part, and a second cover part. The signal gunpowder filler is filled into the housing at a regular pressure and is ignited when being heated to a first or higher temperature. The first temperature indicates 130-150 degrees Celsius. The heat sensing automatic lighter comprises first and second bodies, a fire gunpowder part, an electric initiator, and a heat sensing igniter. The first and second bodies are joined to a propulsion unit in order to ignite a solid propeller. The ignition temperature of the first and second bodies is 220-240 degrees Celsius.
Abstract translation: 目的：提供热敏点火器，热敏自动打火机和包括该热敏感点火器的飞行器，以通过感测火灾来自动点燃和正常燃烧推进剂，以防止在发生火灾时推进剂的强烈反应之前发生危险 。 构成：热敏点火器包括壳体，信号火药填料，第一子火药部分，第一盖部分和第二盖部分。 信号火药填料以常规压力填充到壳体中，并且当被加热到第一或更高温度时被点燃。 第一个温度表示130-150摄氏度。 热敏自动打火机包括第一和第二主体，火焰火药部分，电引发器和感热点火器。 第一和第二主体连接到推进单元以点燃固体螺旋桨。 第一机体和第二机体的点火温度为220-240摄氏度。
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