| 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 | 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. | ||||||
| 102 | 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. | ||||||
| 103 | Ergonomically designed check-out counter system for supermarket and merchandising industries | EP90300123.8 | 1990-01-05 | EP0396218A1 | 1990-11-07 | Vrooman, Carll DeWitt; Taylor, Dennis Ray |
An ergonomically designed check-out counter system for supermarket and merchandising industries is characterised by provisions for differences in human heights, hand and position of operators and for ease in handling of merchandise to reduce fatigue and injury to the operators while providing maximum productivity under both light and heavy through put requirements. The check-out counter system includes one or more of the features of a housing defining the overall shape of the check-out counter system, a movable floor device (27) for receiving the cashier and for moving vertically up and down to position the cashier at a desired height regardless of the human height of the cashier, a movable chair device (40) positioned in the intermediate opening (24) for receiving the cashier and including adjustment devices (41,43) for moving the chair vertically and horizontally to desired positions thereby providing the cashier with the option of sitting or standing, a keyboard device (50) for entering price data of the merchandise which may be moved back and forth to accommodate right-handed and left-handed cashiers, and merchandise bagging devices (60,61,70,73) for easy handling and bagging of the merchandise after checking-out by the cashier and providing for direct bagging by the cashier or bagging by a bagger. |
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| 104 | 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。 | ||||||
| 105 | 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。 | ||||||
| 106 | 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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| 107 | 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. | ||||||
| 108 | 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. | ||||||
| 109 | 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). | ||||||
| 110 | 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'). | ||||||
| 111 | 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). | ||||||
| 112 | 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. | ||||||
| 113 | 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. | ||||||
| 114 | 태양전지판 전개장치 및 이를 포함하는 인공위성 | KR1020080070614 | 2008-07-21 | KR101008047B1 | 2011-01-13 | 김경원; 김선원; 임재혁; 이주훈; 황도순; 송운형; 최항석; 김진희; 진익민; 김학정 |
| 높은 전개강성을 가지며 열적으로 우수한 태양전지판 전개장치 및 이를 포함하는 인공위성이 개시된다. 개시된 본 발명에 의한 인공위성은, 인공위성 본체, 인공위성 본체와 연결되어, 태양광을 받아 인공위성 본체의 전력을 발생시키는 태양전지판, 그리고, 태양전지판을 인공위성 본체에 대해 전개시키는 전개장치를 포함한다. 여기서, 전개장치는, 인공위성 본체와 태양전지판을 상호 연결시키는 힌지유닛, 상호 대응되는 형상의 제 1 및 제 2 힌지브라켓을 가지고 인공위성 본체와 연결되는 제 1 전개유닛, 상호 대응되는 형상의 제 3 및 제 4 힌지브라켓을 가지고 태양전지판에 연결되는 제 2 전개유닛, 그리고, 제 1 및 제 2 전개유닛을 상호 접힘/전개 가능하게 연결하는 연결유닛을 포함한다. 이러한 구성에 의하면, 태양전지판이 인공위성 본체로부터 전개될 때 고강성을 가짐으로써, 인공위성의 빠른 안정화를 도모할 수 있다. 인공위성, 태양전지, 전개, 접힘, 펼쳐짐, 강성. | ||||||
| 115 | Panel type artificial satellite and artificial satellite system therewith | US13096078 | 2011-04-28 | US08702040B2 | 2014-04-22 | Tadayuki Takahashi; Takeshi Takashima; Hiroyuki Ogawa; Shin-ichiro Sakai; Naoko Iwata; Yoshikatsu Kuroda; Kazunori Masukawa |
| An artificial satellite system includes at least two panel type artificial satellites 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 satellite, wherein the multi networks are formed by a communicating network for communicating data among data processing tools installed on each of the panel type artificial satellites, a heat pipe for providing thermal energy among tools installed on each of the panel type artificial satellites and a battery supplying line for connecting battery controlling devices installed in the each panel type artificial satellite so that the artificial satellite system 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. | ||||||
| 116 | PANEL TYPE ARTIFICIAL SATELLITE AND ARTIFICIAL SATELLITE SYSTEM THEREWITH | US13096078 | 2011-04-28 | US20110278399A1 | 2011-11-17 | Tadayuki TAKAHASHI; Takeshi Takashima; Hiroyuki Ogawa; Shin-ichiro Sakai; Naoko Iwata; Yoshikatsu Kuroda; Kazunori Masukawa |
| 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 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. | ||||||
| 117 | アンテナ内蔵型人工衛星 | PCT/JP2012/078134 | 2012-10-31 | WO2013065722A1 | 2013-05-10 | 森口 達次 |
人工衛星は、そのデッドスペースに接する当該人工衛星の壁に形成された少なくとも１つのハッチと、ハッチを開くハッチ開閉機構と、を備え、ハッチにアンテナが取付けられている。 |
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| 118 | ERGONOMIC SEATING ASSEMBLIES AND METHODS | PCT/US2012/049599 | 2012-08-03 | WO2013020088A2 | 2013-02-07 | CHRISTIANSON, Nicholas, M.; GOMREE, Jean Francois; SCHOENFELDER, Rodney, C.; WEBER, Jeffrey; MONITOR, Shawn |
Seating assemblies and methods are disclosed. A seating assembly can comprise a seat, a back support, and a frame component. The frame component can extend from a bottom portion, positioned near an underside of the seat, to a top portion, configured to maintain the back support at a position above the seat. The back support can laterally extend from a left edge portion to a right edge portion and can include a spring member at or near each of the left and right edge portions. The spring member can include at least one undulation or arc providing integrated compression adaptation to a user. The seating assembly can further comprise a tilt mechanism, engaged with the frame component, including one or more leaf springs and a spring contact assembly. The spring contact assembly can be positioned on a top side of the one or more leaf springs. |
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| 119 | PROPULSION SYSTEM FOR SMALL ARTIFICIAL SATELLITES | PCT/EP2016/067680 | 2016-07-25 | WO2017021191A1 | 2017-02-09 | ROSSETTINI, Luca; ALBANO LOPES, Gonçalo Daniel |
A propulsion system for small artificial satellites comprises a plurality of engines (2) fixable to a frame (101) of a satellite (100); a control unit (3) connected functionally to the engines (2) for sending at least one activation signal (AS) for activating at least one engine (2); the system is selectively configurable at least between a first configuration in which at least one of the engines (2) is activated for correcting the orbit of the satellite (100) and a second configuration in which at least one of the engines (2) is activated for dispersing said satellite (100) relative to another adjacent satellite. |
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| 120 | Procédé de traitement du signal de réception d'un radar SAR à rampés de fréquence | EP98401088.4 | 1998-05-05 | EP0877260A1 | 1998-11-11 | Normant, Eric |
L'invention concerne l'utilisation d'un radar de type Deramp en radar à synthèse d'ouverture pour de l'imagerie radar. Un radar de type Deramp émet des impulsions modulées linéairement en fréquence répétées de manière cohérente et réalise une sorte de compression d'impulsion en réception par démodulation des signaux d'écho reçus au moyen d'une rampe de fréquence reproduisant tout ou partie d'une impulsion émise et par une transformée de Fourier en distance. Avec ce type de compression d'impulsion, il apparaît sur le signal délivré par un radar de type Deramp une modulation de phase parasite perturbant les traitements SAR classiques de construction d'image radar. Le procédé proposé permet d'éliminer les effets néfastes de cette modulation de phase parasite sur la construction d'une image radar. Il consiste à adopter un support temporel particulier pour la démodulation et à corriger la modulation de phase parasite apparaissant avec ce support temporel particulier principalement par une correction de phase au niveau de la réponse impulsionnelle du filtre de focalisation image et accessoirement par une autre correction de phase au niveau des coefficients complexes de réflexion obtenus pour les points de l'image en fin de traitement SAR. |
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