-
公开(公告)号：KR1020110074015A
公开(公告)日：2011-06-30
申请号：KR1020090130845
申请日：2009-12-24
Applicant: 한국항공우주연구원
CPC classification number: B64G5/00
Abstract: PURPOSE: A device for holding a satellite loading body is provided to enhance the adjustability of a worker by compensating the weight of a loading body to raise the efficiency and stability of mounting work of the satellite loading body. CONSTITUTION: A device for holding a satellite loading body comprises a horizontal frame(10), a vertical frame(20), a connecting unit(30), a first adjusting unit(40), a second adjusting unit(50) and a handle unit(60). The satellite loading body is installed on one side of the horizontal frame. The vertical frame is connected to the horizontal frame and can be lifted using a crane. The connecting unit is installed on the upper end of the vertical frame and is connected to the crane. The first adjusting unit connects the horizontal frame to the vertical frame and slopes at a predetermined angle. The second adjusting unit is installed on one side of the horizontal frame and thus the loading body is installed to be able to move up and down and to the left and right.
Abstract translation: 目的：提供一种用于保持卫星装载体的装置，以通过补偿装载体的重量来提高工作人员的可调性，以提高卫星装载体的安装工作的效率和稳定性。 构成：用于保持卫星装载体的装置包括水平框架（10），垂直框架（20），连接单元（30），第一调节单元（40），第二调节单元（50）和手柄 单元（60）。 卫星装载体安装在水平框架的一侧。 垂直框架连接到水平框架，并可以使用起重机提升。 连接单元安装在垂直框架的上端，并连接到起重机。 第一调节单元将水平框架连接到垂直框架并以预定角度倾斜。 第二调节单元安装在水平框架的一侧，因此装载体能够上下移动，左右移动。
-
公开(公告)号：KR1020110041000A
公开(公告)日：2011-04-21
申请号：KR1020090097969
申请日：2009-10-15
Applicant: 한국항공우주연구원
IPC: G01R29/10
CPC classification number: G01R29/10 , G01R29/0878 , G01R29/105
Abstract: PURPOSE: An antenna hat for high power RF antenna system verification is provided to solve the deterioration of communications quality by limiting the attenuation of an RF signal which is reflected from the inner wall of the antenna through a multi path. CONSTITUTION: A device includes a main body(20), an RX-antenna(30), and a waveguide unit(40). One side of the main body is opened to prevent an RF signal from being discharged outside and the main body has a space therein. The RX antenna is installed in the interior of the main body in opposite to an antenna system. The RF signal is outputted from the antenna system and is transmitted through the space. The waveguide unit is protruded into the interior of the main body to shield the front side of the RX antenna. The waveguide blocks the RF signal which is reflected from the interior of the main body through a multi-path.
Abstract translation: 目的：提供一种用于大功率射频天线系统验证的天线帽，通过限制通过多路径从天线的内壁反射的RF信号的衰减来解决通信质量的恶化。 构成：装置包括主体（20），RX-天线（30）和波导单元（40）。 主体的一侧被打开以防止RF信号被排出到外部，并且主体在其中具有空间。 RX天线安装在与天线系统相对的主体内部。 RF信号从天线系统输出并通过该空间传输。 波导单元突出到主体的内部以屏蔽RX天线的前侧。 波导通过多路径阻挡从主体内部反射的RF信号。
-
公开(公告)号：KR100986002B1
公开(公告)日：2010-10-06
申请号：KR1020080077534
申请日：2008-08-07
Applicant: 한국항공우주연구원
CPC classification number: B64G7/00
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.
-
公开(公告)号：KR101679633B1
公开(公告)日：2016-11-25
申请号：KR1020150111726
申请日：2015-08-07
Applicant: 한국항공우주연구원
CPC classification number: B64C39/024 , B60L11/1824 , B60L2200/10 , B60L2230/22 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/122 , B64C2201/18 , B64D1/00 , B64D17/00 , B64F1/005 , H04B7/18504 , Y02T10/7005 , Y02T10/7088 , Y02T90/12 , Y02T90/121 , Y02T90/14 , Y02T90/16
Abstract: 드론을이용한원격탐사장치가개시되어있다.개시된드론을이용한원격탐사장치는인공위성을매개로서버와송수신이가능하며, 상부에는격납부, 하부에는말뚝부를갖는드론스테이션; 및상기드론스테이션의격납부에탑재된채, 드론스테이션에마련된충전시설에의해전력이공급되며, 상기드론스테이션의제어명령에따라비행하면서탐사현장을탐사하는드론을포함하되, 상기드론스테이션에마련된말뚝부는하단으로갈수록예리한형상으로되고, 다른부위에비해무거운중량으로갖도록하여, 공중에서지면을향해투하했을때 드론스테이션이지면에수직상으로박히도록한 것을특징으로한다.
-
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-
Patent Agency Ranking
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.
-
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。
-
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。
-
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。
-
-
-
-
-
-
-
-
-
Search Results
18
records
(took 0.023 seconds)
