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公开(公告)号：KR1020150066795A
公开(公告)日：2015-06-17
申请号：KR1020130152287
申请日：2013-12-09
Applicant: 한국항공우주연구원
IPC: H02G11/02
CPC classification number: H02G11/02
Abstract: 본발명은케이블권취장치및 방법에관한것이다. 본발명에따른케이블권취방치는상호결합되는상부케이스와하부케이스로이루어진케이스와; 상기상부케이스의일측면에형성되며, 케이블이인입/인출되는개구와; 상기하부케이스의내부에회전가능하도록장착되어케이블이권취되며, 상면에케이블삽입홈이형성되어있는릴; 및상기릴의상면에형성되어상기상부케이스외측으로돌출되며, 상기릴을회전또는정지시키는릴구동부를포함하는것을특징으로한다.
Abstract translation: 本发明涉及一种用于缠绕电缆的装置和方法。 根据本发明的实施例的用于缠绕电缆的方法包括：包括上壳体和下壳体的壳体; 形成在上壳体的一侧的开口，用于插入或拔出电缆; 能够在下壳体中旋转的卷轴，卷绕电缆，并且在上侧具有插入槽; 以及向上壳体的外侧突出并旋转或停止卷轴的旋转的卷轴驱动部。
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公开(公告)号：KR101514569B1
公开(公告)日：2015-04-24
申请号：KR1020130142320
申请日：2013-11-21
Applicant: 한국항공우주연구원
CPC classification number: B64G5/00
Abstract: 본발명은높이조절및 회전잠금이가능한위성체조립치구에관한것으로, 더욱상세하게는승강장치및 가이드부를구비함으로써상부프레임이승강이원활하게이루어질수 있으며, 상부프레임을원하는각도로기울인상태에서회전잠금장치를통해손쉽게회전된상태로고정할수 있는높이조절및 회전잠금이가능한위성체조립치구에관한것이다.
Abstract translation: 本发明涉及一种能够进行高度调节和旋转锁定的卫星组合装置，更具体地涉及能够调节高度和旋转锁定的卫星组合装置，并且包括：上升和体面的装置和导向件 部分; 上架顺利运行; 并且上框架能够在上框架以期望的角度倾斜的状态下通过旋转锁定装置容易地以旋转状态固定。
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公开(公告)号：KR101129345B1
公开(公告)日：2012-03-26
申请号：KR1020090115248
申请日：2009-11-26
Applicant: 한국항공우주연구원
IPC: G01M99/00
Abstract: 본 발명은 복수의 태양전지패널이 절첩되어 형성된 태양전지판의 전개시험시, 그 상부에 형성되는 것으로서, 평행하게 형성되는 한 쌍의 레일과, 상기 레일을 따라 슬라이드 이동 가능하도록 각 레일에 설치되는 제1 슬라이드 부재와, 상기 각 제1 슬라이드 부재를 상호 연결하도록 설치되는 가이드 레일과, 상기 가이드 레일을 따라 슬라이드 이동 가능하도록 설치되는 제2 슬라이드 부재와, 상기 제2 슬라이드 부재에 연결된 채, 태양전지판에 연결되어 태양전지판의 자중을 지지하는 지지케이블을 포함하는 것을 특징으로 한다.
본 발명에 의하면, 태양전지판의 자중을 지지하는 지지케이블을 2축을 따라 슬라이드 이동가능하게 함으로써, 태양전지판 전개시험 시 완벽한 무중력 상태를 구현할 수 있는 효과가 있다.
인공위성, 태양전지판, 전개시험, 무중력상태 제공장치-
公开(公告)号：KR101081605B1
公开(公告)日：2011-11-08
申请号：KR1020090100852
申请日：2009-10-22
Applicant: 한국항공우주연구원
IPC: H04W24/02
Abstract: 본발명은버스트의채널품질추정을향상시키는방법에관한것으로서, 수신된버스트의데이터구간신호를등화시에최적의경로로부터계산되는 BPM(Best Path Metric) 값들을합하여 BPMS(Best Path Metric Sum) 값을획득하는 BPMS 획득단계; 및, 변조방식에따라실험적으로얻어지는다수의 BPMS 값과상기 BPMS 값에각각대응하는 uncoded BER 값의상관관계로부터, 상기 BPMS 획득단계에서획득되는 BPMS 값에대응하는 BEP 값을추정하는 BEP 추정단계를포함하는것을특징으로하여, 훈련신호의양단의데이터를등화하여얻을수 있는 BPMS 값을이용하여 BEP를추정함으로써, 각각의버스트마다실제데이터의정확한채널품질을추정하여채널상태를신뢰성있게예측할수 있는현저한효과가있다.
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公开(公告)号：KR101074533B1
公开(公告)日：2011-10-17
申请号：KR1020090097969
申请日：2009-10-15
Applicant: 한국항공우주연구원
IPC: G01R29/10
Abstract: 고출력 RF 신호를방출하는안테나시스템의통신기능을테스트하기위하여구비되는안테나햇에있어서, 상기안테나시스템으로부터방출되는 RF 신호가유입되어외부로방출되는것을차폐하기위하여일면이개방되고, 내부에는공간부가형성되는본체부; 상기안테나시스템과대향하는방향으로상기본체부의내벽에설치되어, 상기안테나시스템으로부터출력되고상기공간부를통하여전송되는 RF 신호를감지하는수신안테나; 및, 상기수신안테나의전 측면을차폐하도록상기본체부의내부로돌출하여형성되어, 상기본체부의내벽으로부터반사되는다중경로를통한 RF 신호를차단하는도파관부를포함하는것을특징으로하여안테나햇의내벽으로부터반사되는다중반사파의영향을최소화하여고출력안테나시스템의통신기능을테스트하기위한고출력 RF 안테나시스템검증용안테나햇에관한것이다.
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Patent Agency Ranking
公开(公告)号：KR1020110074016A
公开(公告)日：2011-06-30
申请号：KR1020090130848
申请日：2009-12-24
Applicant: 한국항공우주연구원
CPC classification number: B64G1/222 , B64G2001/224
Abstract: PURPOSE: An opening and holding apparatus of the body panel of a satellite is provided to open the body panel of the satellite by the change of an opening angle freely without operation of a crane and maintain the opened state. CONSTITUTION: An opening and holding apparatus of the body panel of a satellite comprises a strong back(100), a frame(200), an interface bracket(300) and a rotating device(400). The strong back is mounted by fastening of a fixing bolt(101) to an interface hole, which is formed on the front of the body panel(1). The frame is mounted on a rotating shaft on one side of the body panel through fixing pieces(210). The interface bracket connects the strong back and the frame. The interface bracket is installed so that the height and gap of the strong back to the frame are corrected. The rotate device comprises a fixing unit(410) and a hinge unit(420). The fixing unit is coupled to the handling point(10) of the satellite and fixes the rotating shaft.
Abstract translation: 目的：提供卫星身体面板的开放保持装置，通过自由地改变开放角度来打开卫星的身体面板，而不需要起重机的操作，并保持打开状态。 构成：卫星的身体面板的开放保持装置包括强背部（100），框架（200），接口支架（300）和旋转装置（400）。 通过将固定螺栓（101）紧固到形成在车身板（1）的前部上的接口孔来安装坚固的后背。 框架通过固定件（210）安装在主体面板一侧的旋转轴上。 接口支架连接强背和框架。 安装接口支架，使得强回到框架的高度和间隙得到纠正。 旋转装置包括固定单元（410）和铰链单元（420）。 固定单元联接到卫星的操作点（10）并固定旋转轴。
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公开(公告)号：KR1020100022760A
公开(公告)日：2010-03-03
申请号：KR1020080081434
申请日：2008-08-20
Applicant: 한국항공우주연구원
IPC: B64G1/44
CPC classification number: B64G1/443 , B64G7/00 , B64G2001/224
Abstract: PURPOSE: A satellite solar inflating testing device is provided to simplify the structure of the device for analyzing the inflating procedure of an artificial satellite solar battery plane in advance. CONSTITUTION: A satellite solar inflating testing device which analyzes the inflating procedure of an artificial satellite solar battery plane comprises target parts(131,132), a record part(130) and a detection part(135). The target part indicates the location of the solar panel and is mounted on the solar panel. The record part takes a photograph of the inflating procedure of the solar panel in which the target part is attached. The record part extracts inflating procedure data of the solar panel using the recorded image. The target part is included of a fluorescent body or a luminous body. The target part is composed of a chemilight. A fixing part is formed on one side of the solar panel in order to support and fix the solar panel.
Abstract translation: 目的：提供一种卫星太阳能充气试验装置，用于简化用于分析人造卫星太阳能电池飞机充气程序的装置的结构。 构成：分析人造卫星太阳能电池平面的充气程序的卫星太阳能充气试验装置包括目标部件（131,132），记录部件（130）和检测部件（135）。 目标部分表示太阳能电池板的位置并安装在太阳能电池板上。 记录部分拍摄目标部分附着的太阳能电池板的充气过程的照片。 记录部分使用记录图像提取太阳能电池板的充气程序数据。 目标部分包括荧光体或发光体。 目标部分由化学物质组成。 为了支撑和固定太阳能电池板，在太阳能电池板的一侧形成固定部。
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公开(公告)号：KR1020100018839A
公开(公告)日：2010-02-18
申请号：KR1020080077534
申请日：2008-08-07
Applicant: 한국항공우주연구원
Abstract: PURPOSE: An NEA unit and the deployment test device of a satellite solar array including the same are provided to manufacture the NEA unit simply with a low cost by manufacturing the NEA unit fixing and releasing the solar array with an electromagnet. CONSTITUTION: A fixing part is included on the side of a hinged solar array. A electromagnet part(152) fixes and releases the hinged solar array by optionally combining to the fixing part. A housing(151) receives the electromagnet part. The electromagnet part includes a controller and a rectifier for supplying power. A part of the side of the housing is opened to forms a first opening part(512). A cover plate(153) is formed to close the first opening.
Abstract translation: 目的：提供NEA单元和包括其的卫星太阳能阵列的部署测试装置，通过制造NEA单元来简单地以低成本制造NEA单元，并用电磁铁固定和释放太阳能阵列。 构成：固定部件包括在铰接太阳能阵列的一侧。 电磁铁部件152通过可选地组合到固定部件来固定和释放铰接的太阳能电池阵列。 壳体（151）接收电磁体部分。 电磁铁部件包括用于供电的控制器和整流器。 壳体侧面的一部分被打开以形成第一开口部分（512）。 形成盖板（153）以封闭第一开口。
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公开(公告)号：KR1020100018826A
公开(公告)日：2010-02-18
申请号：KR1020080077516
申请日：2008-08-07
Applicant: 한국항공우주연구원
Abstract: PURPOSE: An L-shaped fixture for a thermal vacuum test and a satellite supporting apparatus having the same are provided to support a satellite in a horizontal position and minimize affects on the satellite during the thermal vacuum test. CONSTITUTION: An upper support(111) is provided on one side of a satellite(10) in order to secure the satellite in a horizontal position. A lower support(112) is coupled with the upper support to form an L-shaped feature and supports the upper support and the satellite. A reflector(113) is provided on a part of the lower support which is opposite to the satellite and reflects heat to outside. The upper and lower supports and the reflector is formed out of an aluminum material with a polished surface.
Abstract translation: 目的：提供用于热真空测试的L形夹具和具有该L形固定装置的卫星支撑装置，用于将卫星支撑在水平位置，并且在热真空测试期间最小化对卫星的影响。 构成：为了将卫星固定在水平位置，在卫星（10）的一侧设置有上支撑（111）。 下支撑件（112）与上支撑件联接以形成L形特征并支撑上支架和卫星。 反射器（113）设置在下卫星的与卫星相对的一部分上并将热量反射到外部。 上部和下部支撑件和反射器由具有抛光表面的铝材料形成。
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公开(公告)号：KR1020090126501A
公开(公告)日：2009-12-09
申请号：KR1020080052619
申请日：2008-06-04
Applicant: 한국항공우주연구원
IPC: B64F5/00
Abstract: PURPOSE: A trolley for the assembly work of a medium and large-sized satellite is provided to make the free pose change of an artificial satellite possible, thereby improving the accessibility of a worker. CONSTITUTION: A trolley(100) for the assembly work of a medium and large-sized satellite comprises a rotating unit(110), a side plate(120), a plurality of erecting units(130), and a lower platform(140). The rotating unit supports one end of an artificial satellite(10). The rotating unit implements the rolling rotation of the artificial satellite. The rotating unit is fixed in one side of the side plate. The erecting unit rotates the side plate to implement the erecting exercise. The lower platform supports the erecting unit.
Abstract translation: 目的：提供中型和大型卫星组装工作台的手推车，使人造卫星的自由姿势变化，从而提高工人的可及性。 构成：用于中型和大型卫星的组装工作的手推车（100）包括旋转单元（110），侧板（120），多个竖立单元（130）和下平台（140） 。 旋转单元支撑人造卫星（10）的一端。 旋转单元实现人造卫星的滚动旋转。 旋转单元固定在侧板的一侧。 竖立单元旋转侧板以实施竖立运动。 下部平台支撑架设单元。
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