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公开(公告)号：KR1020140052347A
公开(公告)日：2014-05-07
申请号：KR1020120118365
申请日：2012-10-24
Applicant: 한국항공우주연구원
CPC classification number: Y02A40/252 , Y02A40/266 , Y02A40/268 , Y02E10/46 , Y02P60/124 , A01G9/24 , A01G9/14 , A01G9/1438 , A01G9/241 , F03G6/00 , F24S50/20 , Y02E10/52
Abstract: Disclosed are a ventilation window and a photovoltaic greenhouse having the same. According to an embodiment of the present invention, multiple ventilation holes though which internal air and external air pass are formed on the ventilation window, to enable easy ventilation. In addition, the multiple ventilation holes can have a downward slope in the direction of the outside. According to an embodiment of the present invention, the photovoltaic greenhouse can include the described ventilation window and a solar cell module which converts sunlight to electric power. Multiple cylinders are provided with piston rods which are joined to each corner of a back side of the solar cell module to be able to rotate in any direction. The solar cell module is able to trace the sun by the rotations of the multiple cylinders in any direction (upward, downward, left and right).
Abstract translation: 公开了一种通风窗和具有该通风窗的光伏温室。 根据本发明的一个实施例，通风窗上形成有内部空气和外部空气通过的多个通风孔，以便于通风。 此外，多个通风孔可以在外部的方向上具有向下的倾斜。 根据本发明的实施例，光伏温室可以包括所描述的通风窗和将太阳光转换为电力的太阳能电池模块。 多个气缸设置有活塞杆，活塞杆连接到太阳能电池模块的后侧的每个角以能够在任何方向上旋转。 太阳能电池模块能够通过多个气缸在任何方向（向上，向下，向左和向右）的转动来追踪太阳。
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公开(公告)号：KR101282558B1
公开(公告)日：2013-07-04
申请号：KR1020110093337
申请日：2011-09-16
Applicant: 한국항공우주연구원
Abstract: 달 및 행성 탐사차에서 운행 시 바퀴에 전달되는 압력을 전기에너지로 변환시키는 에너지 수확형 바퀴를 구비하는 달 및 행성 탐사차가 개시된다. 달 및 행성 탐사차의 바퀴는, 탐사차의 회전축에 연결되는 림(rim)부, 상기 림부 외측에 구비되는 타이어부 및 상기 림부와 상기 타이어부 사이에서 상기 림부 외주면을 둘러싸도록 구비되며 유연성 있는 압전 폴리머 재질로 형성된 에너지 변환부를 포함하여 구성된다.
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公开(公告)号：KR100400977B1
公开(公告)日：2003-10-10
申请号：KR1020000079452
申请日：2000-12-21
Applicant: 한국항공우주연구원
IPC: G01M99/00
Abstract: PURPOSE: An apparatus is provided to allow a user to observe, on the earth, the explosion of solar cell panel mounted to an artificial satellite, in the cosmos, through the apparatus with simplified structure and reduced cost, while improving reliability for test. CONSTITUTION: An apparatus comprises a solar cell panel(3); an explosion structure connected to the solar cell panel; a bungee cable arranged to a guide beam(12) for implementing gravity-free state on the earth, and which explodes the solar cell panel; an adiabatic box for providing a low temperature environment by supplying a low temperature nitrogen gas(20) through a nitrogen liquid tank(17), an evaporator(18) and a nitrogen gas supply pump(19); and a power controller(22) and a power supply(21) connected to a heater so as to operate an extra small friction bearing.
Abstract translation: 目的：提供一种装置，使得用户能够通过该设备在地球上观察安装在人造卫星上的太阳能电池板的爆炸，其结构简化且成本降低，同时提高了测试的可靠性。 构成：一种装置包括太阳能电池板（3）; 连接到太阳能电池板的爆炸结构; 布置在引导梁（12）上的用于在地球上实现无重力状态并且使太阳能电池板爆炸的蹦极电缆; （17），蒸发器（18）以及氮气供给泵（19）供给低温氮气（20）来提供低温环境的绝热箱。 以及连接到加热器的电源控制器（22）和电源（21），以便操作额外的小摩擦轴承。
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公开(公告)号：KR1020020080564A
公开(公告)日：2002-10-26
申请号：KR1020010020194
申请日：2001-04-16
Applicant: 한국항공우주연구원
IPC: G01F23/18
Abstract: PURPOSE: A water level control apparatus is provided to prevent contamination by using a pure water in humidity control, while achieving improved accuracy for water level control. CONSTITUTION: A water level control apparatus for controlling water level through a relay(2) and a driving unit(3), comprises a pump(6) connected to an electronic valve(7) and a water reservoir(5); an electrode rod(4) having a resistance value; and a float(9) connected to the electrode rod, and which moves in accordance with the water level. The water level is measured by the resistance value obtained from the resistance sensed by sensors arranged at a low water level(11), an intermediate water level(12) and a high water level(13), and measured by a multi-meter(1). The electrode rod is made of a conductive material including nichrome and tungsten.
Abstract translation: 目的：提供水位控制装置，通过使用纯水进行湿度控制来防止污染，同时提高水位控制的精度。 构成：用于通过继电器（2）和驱动单元（3）控制水位的水位控制装置包括连接到电子阀（7）和储水器（5）的泵（6）; 具有电阻值的电极棒（4）; 以及连接到电极棒的浮子（9），并且根据水位移动。 水位由通过布置在低水位（11），中间水位（12）和高水位（13）的传感器感测到的电阻获得的电阻值来测量，并由多米 1）。 电极棒由包括镍铬合金和钨的导电材料制成。
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公开(公告)号：KR1020020042109A
公开(公告)日：2002-06-05
申请号：KR1020000071869
申请日：2000-11-30
Applicant: 한국항공우주연구원
IPC: F28D15/02
CPC classification number: F28D15/0233 , F28D15/0275
Abstract: PURPOSE: A method for arranging heat pipe with identical shape using line contact is provided to form uniform distribution of temperature by efficiently dispersing concentrated heat load. CONSTITUTION: Heat pipes(10) contacts with each other on lines to form regular polygons such as hexagons and quadrangles to exchange heat. The heat pipes layered upon another to contact with each other on lines. The heat pipes are manufactured by same process as the shape thereof is identical. The weight of needed heat pipes is reduced in comparison with usual method when the heat pipes are to be densely used so as to be applied to a communication satellite.
Abstract translation: 目的：提供一种使用线接触排列具有相同形状的热管的方法，通过有效地分散集中热负荷来形成均匀的温度分布。 构成：热管（10）在线上彼此接触以形成正六边形和四边形的常规多边形以交换热量。 层叠在另一个上的热管在线上彼此接触。 热管通过与其形状相同的相同工艺制造。 当热管被密集使用以便应用于通信卫星时，与常规方法相比，所需热管的重量减少。
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Patent Agency Ranking
公开(公告)号：KR100292788B1
公开(公告)日：2001-06-15
申请号：KR1019980063937
申请日：1998-12-31
Applicant: 한국항공우주연구원
IPC: G06F11/00
Abstract: 본 발명은 MASS 메모리나 디지털 데이터 프로세싱에 16bit 데이터를 처리하는데 있어 modified Hamming code를 이용하여 1bit 에러정정과 2bit 에러를 검출하도록 하는 에러검출 및 정정회로에 관한 것이다.
이러한 본 발명은 16bit 데이타 입력을 받아 패리티비트를 생성하는 체크비트 생성기와, 전송데이터에 오류를 발생시키기 위해 선택된 데이터비트의 값을 역으로 변환시키는 오류발생회로와, 체크비트와 입력데이터에서 생성된 체크비트를 비교하여 오류코드를 발생시키는 오류코드 발생기와, 체크비트의 값에 따라 오류비트의 위치를 찾아주는 오류위치 감지기와, 오류가 감지된 위치의 데이터를 정정하는 오류정정기와, 오류발생 여부를 감지하는 오류발생 감지기를 구비시킴으로써 이루어진다.-
公开(公告)号：KR101346062B1
公开(公告)日：2013-12-31
申请号：KR1020130011313
申请日：2013-01-31
Applicant: 한국항공우주연구원
Abstract: The present invention relates to a rotational GPS electronic compass capable of accurately measuring a location using correction information provided from a ground base station by simply correcting reception errors using one GPS receiver and capable of confirming a direction through information measured by a receiver including the GPS receiver combined with a rotation unit. [Reference numerals] (AA) Calculation unit;(BB) Output unit
Abstract translation: 本发明涉及一种旋转GPS电子罗盘，其能够使用一个GPS接收机简单地校正接收错误，并且能够通过由包括GPS接收机的接收机测量的信息来确认方向，来精确地测量从地面基站提供的校正信息的位置 结合旋转单元。 （附图标记）（AA）计算单元;（BB）输出单元
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公开(公告)号：KR1020130029925A
公开(公告)日：2013-03-26
申请号：KR1020110093337
申请日：2011-09-16
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A piezoelectricity energy gathering type wheel for a moon and planet discovery vehicle is provided to supplement electric power to drive mount equipment and the discovery vehicle by additionally supplying the electric power. CONSTITUTION: A piezoelectricity energy gathering type wheel for a planet discovery vehicle comprises a rim unit(15), a tire unit(11), and an energy conversion unit(13). The rim unit is connected to a rotary shaft of the planet discovery vehicle. The tire unit is included in a left side of the rim unit. The energy conversion unit warps a surface of the rim unit between the tire unit and the rim unit and is formed in a piezoelectric element material in order to convert energy, which is transferred from a wheel(10) in driving of the planet discovery vehicle, into electric energy.
Abstract translation: 目的：提供一种用于月球和行星发现车辆的压电能聚集型轮，用于补充电力，通过额外提供电力来驱动安装设备和发现车辆。 构成：用于行星发现车辆的压电能聚集型轮包括轮辋单元（15），轮胎单元（11）和能量转换单元（13）。 轮辋单元连接到行星发现车辆的旋转轴。 轮胎单元包括在轮辋单元的左侧。 能量转换单元在轮胎单元和轮辋单元之间扭曲轮辋单元的表面，并且形成为压电元件材料，以便转换在行星发现车辆的驾驶中从车轮（10）传递的能量， 进入电能。
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公开(公告)号：KR1020020050329A
公开(公告)日：2002-06-27
申请号：KR1020000079452
申请日：2000-12-21
Applicant: 한국항공우주연구원
IPC: G01M99/00
CPC classification number: B64G7/00 , B64G1/44 , G01N17/002
Abstract: PURPOSE: An apparatus is provided to allow a user to observe, on the earth, the explosion of solar cell panel mounted to an artificial satellite, in the cosmos, through the apparatus with simplified structure and reduced cost, while improving reliability for test. CONSTITUTION: An apparatus comprises a solar cell panel(3); an explosion structure connected to the solar cell panel; a bungee cable arranged to a guide beam(12) for implementing gravity-free state on the earth, and which explodes the solar cell panel; an adiabatic box for providing a low temperature environment by supplying a low temperature nitrogen gas(20) through a nitrogen liquid tank(17), an evaporator(18) and a nitrogen gas supply pump(19); and a power controller(22) and a power supply(21) connected to a heater so as to operate an extra small friction bearing.
Abstract translation: 目的：提供一种装置，使用户能够在地球上观察安装在宇宙中的人造卫星的太阳能电池板的爆炸，通过设备以简化的结构和降低的成本，同时提高测试的可靠性。 构成：装置包括太阳能电池板（3）; 连接到太阳能电池板的爆炸结构; 引导梁（12）布置成用于在地球上实现无重力状态并且爆炸太阳能电池板的蹦极缆绳; 一个用于通过向氮液罐（17），蒸发器（18）和氮气供应泵（19）供应低温氮气（20）来提供低温环境的绝热箱; 以及连接到加热器以便操作额外的小摩擦轴承的功率控制器（22）和电源（21）。
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公开(公告)号：KR1020020049433A
公开(公告)日：2002-06-26
申请号：KR1020000078602
申请日：2000-12-19
Applicant: 한국항공우주연구원
IPC: G05D23/30
Abstract: PURPOSE: A thermal control device using a PID(Proportional Integral Differential) feedback current control method is provided to control accurately temperature by improving accuracy in a process for controlling power of a heater. CONSTITUTION: A control computer(1) includes a software executing a PID control loop. The control computer(1) is used for processing and storing all data. A GPIB card is mounted in the control computer(1). A master rack(2) is formed with a command control unit(3), a data acquisition module(4), and an interface unit(5). The command control unit(3) distributes commands of the control computer(1) to sub-modules. The data acquisition module(4) measures temperature, voltage, and current. The interface unit(5) assigns a command value to a power supply(10). A fuse/switch module(6) is formed with a fuse(7) and a toggle switch(8). A power supply rack(9) includes a multitude of power supply. The number of power supply corresponds to the number of heater(13). A shunt box module(11) includes a shunt register. The heater(13) and a thermocouple(14) are adhered to a thermal control portion(12).
Abstract translation: 目的：提供使用PID（比例积分微分）反馈电流控制方法的热控制装置，通过提高加热器功率的控制过程中的精度来精确控制温度。 构成：控制计算机（1）包括执行PID控制回路的软件。 控制计算机（1）用于处理和存储所有数据。 GPIB卡安装在控制计算机（1）中。 主机架（2）形成有指令控制单元（3），数据采集模块（4）和接口单元（5）。 命令控制单元（3）将控制计算机（1）的命令分配给子模块。 数据采集模块（4）测量温度，电压和电流。 接口单元（5）向电源（10）分配命令值。 保险丝/开关模块（6）形成有保险丝（7）和拨动开关（8）。 电源机架（9）包括多个电源。 电源数量相当于加热器的数量（13）。 分路盒模块（11）包括分路寄存器。 加热器（13）和热电偶（14）粘附到热控制部分（12）。
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