| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 101 | 인공위성의자세전환실험장치 | KR1019930026761 | 1993-12-07 | KR1019970005470B1 | 1997-04-16 | 강자영; 신광근; 김재한 |
| The position change test device of an artificial satellite comprises: a satellite body drum(1) having a rotating shaft(1) on the center of the upper and lower surfaces thereof; a driven gear(2) for rotating the drum(1); a position change means installed on a predetermined position of the drum(1); an internal square member(9); an external square member(11); a main supporting means for freely rotating the internal and external square members(9,11); driving means(17,18); a rotating means(15); at least one or more sensing means(8) for sensing a target position to be directed by the satellite body; a driven disc gear(13); and brake and position control means(19,20) for receiving the sensed information of the sensing means. | ||||||
| 102 | 人造衛星天線 | TW077305887 | 1988-10-11 | TW119026S | 1989-09-11 | 派崔克.坎貝爾.亨特 |
| 103 | Panel type artificial satellite and artificial satellite system therewith | EP11165796.1 | 2011-05-12 | EP2386489A2 | 2011-11-16 | Takahashi, Tadayuki; Takashima, Takeshi; Ogawa, Hiroyuki; Sakai, Shin-ichiro; Iwata, Naoko; Kuroda, Yoshikatsu; Masukawa, Kazunori |
An artificial satellite system (200) comprises at least two panel type artificial satellites (100) closely connected with a plurality kind of multi networks and the minimum necessary essential tools for one artificial satellite installed on a substrate of each panel type artificial satellites (100), wherein the multi networks(N1, N2, N3) are formed by a communicating network for communicating data among data processing tools installed on each the panel type artificial satellites (100), a heat pipe for providing thermal energy among tools installed on each the panel type artificial satellites (100) and a battery supplying line for connecting battery controlling devices installed in the each panel type artificial satellite so that the artificial satellite system (200) can maintain higher and various controlling performance with a back-up effect of the multi network in the case that any function tool is damaged in one of the panel type artificial satellite (100).
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| 104 | 태양전지판 전개모듈 및 이를 포함하는 인공위성 | KR1020120036704 | 2012-04-09 | KR101442506B1 | 2014-09-23 | 이민규; 홍주성 |
| 태양전지판 전개모듈 및 이를 포함하는 인공위성이 개시된다.
본 발명의 일 실시예에 따른 태양전지판은, 인공위성의 몸체와 연결되며, 길이 방향으로 길게 형성된 중심부재를 포함하며, 양단부에는 각각 제1전지판이 각도 조절 가능하게 연결되는 메인프레임, 상기 메인프레임의 양단부 사이에 위치되는 이동부재, 상기 이동부재에 구비되며, 외력에 의해 파단되어 상기 이동부재를 제1파트 및 제2파트로 분할하는 파단부, 상기 제1전지판과 상기 이동부재를 각각 연결하는 연결링크 및 인장된 상태로 상기 이동부재의 양측과 상기 메인프레임의 양단부를 각각 연결하며, 상기 타단부가 파단 시 상기 제1파트 및 상기 제2파트를 상기 메인프레임의 양단부 측으로 각각 이동시키는 인장탄성부재를 포함한다. 그리고 본 발명의 다른 실시예에 따른 태양전지판은, 인공위성의 몸체와 연결되며, 길이 방향으로 길게 형성된 중심전지판을 포함하며, 일단부에는 제1전지판이 각도 조절 가능하게 연결되는 제2전지판, 상기 제2전지판의 일단부로부터 이격되어 위치되며, 적어도 일부가 상기 제2전지판에 고정되는 이동부재, 상기 이동부재에 구비되며, 외력에 의해 파단되어 상기 이동부재의 고정 상태를 해제하는 파단부, 상기 태양전지판과 상기 이동부재를 연결하는 연결링크 및 인장된 상태로 상기 이동부재와 상기 제2전지판의 일단부를 각각 연결하며, 상기 타단부가 파단 시 상기 이동부재를 상기 제2전지판의 일단부 측으로 이동시키는 인장탄성부재를 포함한다. |
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| 105 | 인공위성용 광학 렌즈의 초정밀 위치 정렬 장치 | KR1020090122622 | 2009-12-10 | KR101082755B1 | 2011-11-10 | 이동우; 문상무; 임종민; 은희광; 문남진 |
| 본발명은인공위성용광학렌즈의초정밀위치정렬장치에관한것으로, 보다상세하게는인공위성에사용되는광학렌즈의위치를 5축방향으로정밀하게정렬하여상기광학렌즈의위치를제어하기위한인공위성용광학렌즈의초정밀위치정렬장치에관한것이다. 본발명에따른인공위성용광학렌즈의초정밀위치정렬장치에의하면, X축방향으로각각이동하는제 1 X축스테이지및 제 2 X축스테이지와 Y축방향으로각각이동하는제 1 Y축스테이지및 제 2 Y축스테이지의위치정렬에의하여 X축, Y축및, Z축의 3축방향의병진운동(translation) 뿐만아니라 X축중심의회전운동(elevation)과 Y축중심의회전운동(azimuth)에대하여미세하고정밀한위치정렬을제어할수 있는현저한효과가있다. | ||||||
| 106 | 태양전지판 전개장치 및 이를 포함하는 인공위성 | KR1020080070614 | 2008-07-21 | KR1020100009812A | 2010-01-29 | 김경원; 김선원; 임재혁; 이주훈; 황도순; 송운형; 최항석; 김진희; 진익민; 김학정 |
| PURPOSE: A solar cell panel unfolding device and an artificial satellite having the same are provided to improve the rigidity of the solar cell panel unfolding device by unfolding the solar panel in the artificial satellite main body. CONSTITUTION: A hinge unit connects the artificial satellite main body and a solar panel. A first unfolding unit(120) has two hinge brackets(121,124) which are mutually corresponded shape. The first unfolding unit is connected to the artificial satellite main body. A second unfolding unit(140) has third and fourth hinge brackets(141,144). The second unfolding unit is connected to the solar panel. A connecting unit(160) folds or unfolds the first and second unfolding units. | ||||||
| 107 | 인공 위성의 제어 신호 검증 장치 및 방법 | KR1020070125229 | 2007-12-05 | KR1020090058606A | 2009-06-10 | 박병하; 최종연; 권재욱; 윤영수; 조승원; 김영윤 |
| An artificial satellite control signal verification apparatus and a method are provided to verify an electromagnetic filed signal and a valve control signal selectively by assembling a control signal verify device of an artificial satellite and the artificial satellite. An interface unit(520) supplies power to an artificial satellite from a power supply unit(510), and receives more than an electromagnetic filed signal and a valve signal from the artificial satellite body. A verification unit(530) processes more than one of the received electromagnetic filed signal and a valve signal, and verifies whether a normal condition of a posture control system or not through the received valve signal, and it also verify whether a normal condition of a solar panel through the received electromagnetic filed. | ||||||
| 108 | 인공위성과 에이디에스엘을 이용한 인터넷 방송 시스템 | KR1020000027426 | 2000-05-22 | KR1020000050176A | 2000-08-05 | 한상민 |
| PURPOSE: An internet broadcasting system is provided to reduce usage amounts of internet and a router by using internet protocol(IP) multicasts using an artificial satellite as local servers to use an asymmetric digital subscriber line(ADSL) and the artificial satellite. CONSTITUTION: An internet broadcasting system using an artificial satellite and an asymmetric digital subscriber line(ADSL), comprises a first internet site(20), the artificial satellite(30), a second internet site(40), many telephone offices(50,60,70), and a signal transmitter. The first internet site including a multicast server(21), a web server(22), a hub(23), and an encoder(24) transmits a satellite signal with a multicast. The satellite receives the signal from the encoder to output corresponding data. The second internet site receives data from the satellite with a multicast, and is composed of a central distributing server(41), a web server(42), a hub(43), and a decoder(44). The telephone offices include local remote distributing servers(51,52,53,61,62,63,71,72,73). The local remote distributing servers receive signals from the second internet site with multicasts. The signal transmitter transmits the signals of the local remote distributing servers to each user through an ADSL router(80), a cable modem(90) or an exclusive line(100) with unicasts. | ||||||
| 109 | 인공위성제어용모멘텀휠조립체 | KR1019980042603 | 1998-10-12 | KR1020000025502A | 2000-05-06 | 김병진; 이현우; 이성호; 남명룡; 성단근 |
| PURPOSE: A momentum wheel assembly is provided to reliably control the position of a satellite, and to stably control the satellite in case that some of components are in trouble. CONSTITUTION: A momentum wheel assembly for controlling an artificial satellite contains three basic momentum wheels(20,22,24) arranged to rotate in each girth of three shafts formed by a roll axis(X), a pitch axis(Y) and a yaw axis(Z), and one spare momentum wheel(30) arranged to be rotated in the girth of horizontal axis with the pitch axis. When the momentum wheel(22) of the pitch axis is defected among three basic momentum wheels(20,22,24) of yaw axis, the position of the satellite is controlled with the three axes by the momentum wheels(20,24) rotated in the girths of the roll axis and the yaw axis. And when the momentum wheels(20,24) rotated in the girths of the roll axis and the yaw axis are defected, the control of position is performed with the same method as the artificial satellite contained one momentum wheel by driving the momentum wheel(22) of the pitch axis and the spare momentum wheel at the same time. | ||||||
| 110 | 人造卫星模型 | CN202130829062.4 | 2021-12-15 | CN307245567S | 2022-04-08 | 俞放; 李宗琛 |
| 1.本外观设计产品的名称：人造卫星模型。 2.本外观设计产品的用途：展示卫星结构和工作状态。 3.本外观设计产品的设计要点：在于形状。 4.最能表明设计要点的图片或照片：组合状态立体图。 | ||||||
| 111 | Improvement in artificial lecjs | US40417D | US40417A | 1863-10-27 | ||
| 112 | 人造卫星教具 | CN201930398795.X | 2019-07-25 | CN305531147S | 2020-01-03 | 宋乐; 郭安瑞; 董美涵; 冯橹源; 姚远; 李正宇; 马高峰; 刘蕊; 王林杰; 甘霖 |
| 1.本外观设计产品的名称：人造卫星教具。 2.本外观设计产品的用途：教学演示。 3.本外观设计产品的设计要点：在于形状。 4.最能表明设计要点的图片或照片：立体图。 | ||||||
| 113 | 人造卫星接收器 | CN201030213120.2 | 2010-06-18 | CN301438419S | 2011-01-12 | 汉斯-彼得·康斯丁; 阿列克塞·艾泽纳赫 |
| 1.外观设计产品名称：人造卫星接收器。2.外观设计产品用途：用于接收人造卫星发出的信号。3.设计要点：如图所示产品形状，图案或其结合。4.最能表明设计要点的图：设计1立体图1。5.设计1为基本设计。6.省略其它视图。 | ||||||
| 114 | 이벤트 기반의 위성 운영 지원 시스템 및 그 방법 | KR1020150132458 | 2015-09-18 | KR1020150118563A | 2015-10-22 | 양승은; 채동석 |
| 이벤트기반의위성운영지원시스템및 그방법이개시된다. 여기서, 이벤트기반의위성운영지원시스템은위성에서연속적으로발생하는이벤트시퀀스를저장하는이벤트시퀀스저장부, 상기이벤트시퀀스저장부에저장된이벤트시퀀스에따라지상작업을추천하는이벤트시퀀스지상활용부, 그리고상기이벤트시퀀스저장부에저장된이벤트시퀀스에따라위성운용을제어하는이벤트시퀀스위성활용부를포함한다. | ||||||
| 115 | ＮＵＩ를 이용한 위성 모니터링 장치 및 방법 | KR1020130010886 | 2013-01-31 | KR1020140098898A | 2014-08-11 | 이상철; 김해동; 조동현; 조영민; 문성태; 한상혁; 임정흠; 석진영 |
| The present invention relates to a method and an apparatus for monitoring a state of a satellite and, more specifically, to an apparatus and a method for monitoring a state of a satellite using a natural user interface (NUI), which sense a signal of an NUI possessed by a user and display a screen, which the user wants to watch, such that the state of the satellite can be easily monitored. | ||||||
| 116 | 인공위성용 광학 렌즈의 초정밀 위치 정렬 장치 | KR1020090122622 | 2009-12-10 | KR1020110065924A | 2011-06-16 | 이동우; 문상무; 임종민; 은희광; 문남진 |
| PURPOSE: An apparatus for aligning the position of a satellite optical lens is provided to control the alignment of the position with respect to the translation, the elevation, and the azimuth of an object and a telescopic sight. CONSTITUTION: A fixing frame(10) forms the Z-axis linear guide(12) on the upper side. The Z-axis stage(20) is mounted to be moved in the Z-axis direction along the Z-axis linear guide. A first X-axis stage(30) is mounted on the Z-axis stage to be moved in the X-axis direction along a first X-axis linear guide. A second X-axis stage(40) is mounted on the Z-axis stage to be moved in the Z-axis direction along a second X-axis linear guide. A first Y-axis stage(50) is mounted to be moved along the Y-axis direction along a first Y-axis linear guide(32). A second Y-axis stage(60) is mounted to be moved along the Y-axis direction along a second Y-axis linear guide(42). | ||||||
| 117 | 캠 플레이트 구동 방식의 인공위성 태양전지판 전개 장치 | KR1020020071592 | 2002-11-18 | KR1020040043358A | 2004-05-24 | 이주훈; 임창선; 김선호; 김성훈; 김진희; 황도순; 진익민; 김태경 |
| PURPOSE: A device for expanding an artificial satellite solar cell array of a cam plate drive type is provided to safely expand the solar cell array in a mission orbit, prevent breakage of the solar cell array, and securely expand the solar cell array. CONSTITUTION: A device for expanding an artificial satellite solar cell array of a cam plate drive type comprises an upper bracket(1) comprising a roller(6) to the outside of a flange part, a static body(7) to the inside, and a ratchet(11) to opposite side of the static body; a rotating shaft(4) rotatably connecting the flange parts of upper bracket and a lower bracket(2); the lower bracket connected to the upper bracket by the rotating shaft and fixed to the artificial satellite solar cell array; a driving shaft(9) in which a torsional spring(10) is inserted to the lower side of the flange part of the lower bracket, to supply rotation power; and a cam plate(3) connected to the tip of a side of the driving shaft. The cam plate has an elongated hole(3'). | ||||||
| 118 | 인공위성을 이용한 버스용 정보제공 장치 | KR1020010008381 | 2001-02-20 | KR1020020068124A | 2002-08-27 | 한상민 |
| PURPOSE: A device for supplying bus information through artificial satellite is provided to offer bus information to passengers through a speaker and an LCD(Liquid Crystal Display) monitor by receiving data transported through a GPS(Global Positioning System) satellite and a communication satellite in a moving bus. CONSTITUTION: A GPS satellite receiving antenna(100) receives a GPS signal from a GPS satellite. A communication satellite receiving antenna(200) receives a communication signal from a communication satellite. A frequency process tap(300) selects an allotted frequency from the received high-frequency signals, amplifies the selected high-frequency signal, converts the amplified high-frequency signal into a low-frequency signal, and recovers the converted spectrum diffusion signal into an original signal. A signal process tap(400) converts the recovered original signal into digital data, and converts the digital data into an analog signal. A recording unit(600) records the digital data and an application program. A processor(500) processes the digital data and the application program. A controller(700) controls a speaker unit(800) and an LCD monitor unit(900). | ||||||
| 119 | 인공위성용 배터리 전원 자동 전환 장치 | KR1020000079453 | 2000-12-21 | KR1020020050330A | 2002-06-27 | 이상곤; 장진백; 장성수 |
| PURPOSE: A device for automatically changing battery power of an artificial satellite is provided to supply power into the artificial satellite through a relay and to improve reliability. CONSTITUTION: A device for automatically changing battery power in an artificial satellite comprises a relay(30) transferring power of battery(10) into a main power bus by having a latch shape; an interface(21) supplying a control command to turn on/off the relay; a relay(31) supplying the power into a satellite main power bus; a driving circuit(40) driving the relay by detecting output of the latch shaped relay; and a voltage controller(50) supplying power into the driving circuit. The device for automatically changing the battery power in the artificial satellite automatically changes a shooting power mode. The driving circuit drives the relay while generating trouble of the latch shaped relay the power of the battery is supplied into the satellite.. Thereby, the device for automatically changing the battery power in the artificial satellite supplies the power into the artificial satellite through the relay. | ||||||
| 120 | 이벤트 기반의 위성 운영 지원 시스템 및 그 방법 | KR1020130138711 | 2013-11-15 | KR1020150056681A | 2015-05-27 | 양승은; 채동석 |
| 이벤트기반의위성운영지원시스템및 그방법이개시된다. 여기서, 이벤트기반의위성운영지원시스템은위성에서연속적으로발생하는이벤트시퀀스를저장하는이벤트시퀀스저장부, 상기이벤트시퀀스저장부에저장된이벤트시퀀스에따라지상작업을추천하는이벤트시퀀스지상활용부, 그리고상기이벤트시퀀스저장부에저장된이벤트시퀀스에따라위성운용을제어하는이벤트시퀀스위성활용부를포함한다. | ||||||
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