| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 81 | 使用人造卫星的收费道路收费系统、收费机和收费方法 | CN02829800.4 | 2002-10-25 | CN1695171A | 2005-11-09 | 泷田佳章 |
| 一种收费道路收费系统，包括：其上安装了车载机器(11，130)的车辆(7)、人造卫星(1)和系统数据中心(20)。车载机器(11，130)从人造卫星(1)接收无线电信号，并且按照所接收的无线电信号来计算作为车辆位置的纬度、经度和高度。指示行驶车辆位置历史的纬度数据、经度数据和高度数据被存储在外部存储器件(46)中作为时间序列日志文件，并且被发送到系统数据中心(20)，其中，对于每个车辆，数据被累积在存储器件(63)中。在系统数据中心(20)中，按照收费道路路径位置数据来确定车辆(7)已经行驶的收费道路区间，所述收费道路路径位置数据包括从车辆(7)发送并在数据库中存储/累积的指示行驶车辆位置历史的纬度数据、经度数据和高度数据。按照对于每个路线区间指定的行驶费用数据来计算收费道路上行驶的每个人的行驶费用，并且通过经由由收费道路行驶人员预先设置的金融机构(25)的帐户的自动支付来收取所述费用。 | ||||||
| 82 | 人造卫星信号的接收方法、接收装置、发送方法以及信息系统 | CN03123291.4 | 2003-04-25 | CN1453186A | 2003-11-05 | 前田利秀; 岩田忠良; 石田隆张; 井上秀树 |
| 本发明向切换供服务的卫星而利用的轨道卫星的通信/广播系统，提供不使非切换时的吞吐量下降的，高效率的卫星切换装置、信号接收方法、发送方法及信息系统。(5505)是切换前的卫星1的收发模式，(5506)是切换后的卫星2的收发模式。这里，数据被分为要求短时间响应的数据(5007)和不要求的(5508)两种。在(5007)中包含数据和广播等有必要使吞吐量保持一定的数据。倒三角4和5夹着的区间是卫星切换期间。在卫星切换期间中，重叠了不要求短时间响应的数据(5508)的发送期间。能不损害数据流和广播等有必要使吞吐量保持一定的数据的通信质量，进行卫星的切换。 | ||||||
| 83 | 装有磁矩和空气动力矩发生器的人造卫星及该卫星的控制方法 | CN95193154.7 | 1995-03-29 | CN1148836A | 1997-04-30 | P·杜乔恩 |
| 低轨道人造卫星的定向方法及系统。把空气动力学导向装置与磁耦合器(1、2、3)结合起来了，空气动力学导向装置由于高层大气可引起卫星沿两个轴的转动而磁耦合器可借助地磁场产生沿三个主轴的俯仰、横滚和侧滚(偏航)的转动。人们可以达到很高的精度使卫星定向而无需消耗大量的能源。还给出了一些控制规律。 | ||||||
| 84 | 一体化热控装置、系统及人造卫星 | CN202321631291.5 | 2023-06-26 | CN220181101U | 2023-12-15 | 刘立帅; 付兴科; 徐敏; 孙承志; 吴昕颖; 刘芮; 黄泳; 赵研博; 刘彦勇; 李义飞 |
| 本实用新型提供了一种一体化热控装置、系统及人造卫星，涉及卫星热控制技术领域，本实用新型采用基于多层隔热组件的被动热控手段和基于辐射组件的间接辐射主动控温手段，有效解决了蓄电池组和光学相机的高精度控温问题，并且采用一体化设计的由石墨烯薄膜制成的第一支撑架和第二支撑架，使得辐射组件侧加热回路产生的热量和蓄电池组工作时产生的热量，可通过一体化的石墨烯薄膜实现快速高效的热交换，在保证蓄电池组和光学相机主体温度的前提下，节约了整星加热回路资源，减轻了热控装置的重量，节约了成本。 | ||||||
| 85 | 各类人造卫星自动旋转演示教具 | CN201620650186.X | 2016-06-22 | CN206021767U | 2017-03-15 | 王舒琴 |
| 本实用新型公开了一种各类人造卫星自动旋转演示教具，包括一个具有底座和立柱的支架，所述立柱的顶端分别设有同心安装的地球轴、近地卫星轴、同步卫星轴和极地卫星轴；以上轴上分别固定有一个地球仪、一个近地卫星模型、一个同步卫星模型和一个极地卫星模型；所述地球仪的赤道呈竖直，所述近地卫星环、同步卫星环和极地卫星环同心竖直分布并分别和地球仪的赤道同心。本演示教具，其使用方法分为以调节准备和演示二个步骤；采用了本实用新型的演示教具，通过不同转速的电机来带动近地、同步、极地卫星环，使固定在其上的近地、同步、极地卫星模型绕地球仪转动，直观的演示了各种人造卫星绕地球运行时的速度，使学生更易于理解与记忆。 | ||||||
| 86 | 一种空间可展结构、太阳能板及人造卫星 | CN202322980333.2 | 2023-11-03 | CN221914632U | 2024-10-29 | 游琴; 刘维海; 邢宸硕; 陈俊杰; 叶鑫欣 |
| 本申请提供一种空间可展结构、太阳能板及人造卫星，其中所述空间可展结构用于展开或收缩太阳能板，所述太阳能板为薄膜状结构；所述空间可展结构包括：直线型连杆，两根所述直线型连杆之间为一组，并围绕着所述太阳能板的中心周向均布设置有若干组，在一组所述直线型连杆中，两根所述直线型连杆的中部可转动地连接，所述折线型连杆与所述太阳能板固定通过电机带动带动轮转动，使得皮带转动，通过皮带的转动使得两个折线型连杆之间的互相靠近或远离，使得每组直线型连杆中的两根直线型连杆中部转动，以实现太阳能板的扩展与收缩，实现太阳能板的伸展与收缩，在伸展的时候不论是长度方向还是宽度方向都得以伸展，空间利用率高。 | ||||||
| 87 | Artificial satellites | US3568192D | 1966-10-24 | US3568192A | 1971-03-02 | DAWSON THOMAS WILLIAM GRANT |
| A very light, easily dispensed, efficient and durable passive radial communication satellite comprising a filamentary netlike structure of which alternate lengths of the filaments are metal coated to comprise dipoles, and in which those surfaces of the net filaments between the metal covered dipole regions are covered with a layer of metal which affords protection against damage to the net by long-wavelength ultraviolet radiation and reduces the rate of evaporation of the net material, said layer of metal being of small thickness compared to that forming the dipoles so that radio wave reflection therefrom is negligible.
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| 88 | SATELLITE ARTIFICIEL | EP16763906.1 | 2016-08-10 | EP3259188A1 | 2017-12-27 | CAEL, Philippe; WALKER, Andrew; MENA, Fabrice |
| The invention concerns an artificial satellite comprising one face from the North face and the South face supporting at least one main radiator (42, 44) having an outer face turned towards space and an inner face opposite the outer face. The satellite comprises a bearing structure carrying the North face, the South face, the East face and the West face. At least one part (54, 56) of said at least one main radiator (42, 44) protrudes from at least one face from the East face and the West face (36). The inner face of said at least one protruding part (54, 56) is covered with a high infrared emissivity material. The value of the dimension (L54,56) of said at least one protruding part (54, 56) is between 19% and 50% of the value of the distance (Lc) between the East and West faces. | ||||||
| 89 | 위성 운영 시스템 | KR1020150114474 | 2015-08-13 | KR101631856B1 | 2016-06-20 | 천이진 |
| 본발명은위성운영시스템에관한것으로, 본발명에따른시스템은인가되는제1 제어신호에따라스위칭동작하여전원공급버스를제1 전원공급라인을통해제1 컴퓨터와연결시키거나전원공급버스를백업전원공급라인을통해제1 컴퓨터와연결시키는제1 스위칭릴레이, 인가되는제2 제어신호에따라스위칭동작하여전원공급버스를제2 전원공급라인을통해제2 컴퓨터에연결시키거나전원공급버스를백업전원공급라인을통해제2 컴퓨터에연결시키는제2 스위칭릴레이, 그리고인가되는제3 제어신호에따라스위칭동작하여전원공급버스를백업전원공급라인을통해제1 컴퓨터에연결시키거나전원공급버스를백업전원공급라인을통해제2 컴퓨터에연결시키는백업스위칭릴레이를포함한다. | ||||||
| 90 | 인공위성용 힌지 장치 | KR1020080007065 | 2008-01-23 | KR100942172B1 | 2010-02-12 | 박희창; 김병인; 이성휘; 김진희; 김경원; 김선원; 김규선; 진익민; 이상률; 이주진 |
| 본 발명은 인공위성용 힌지 장치에 관한 것으로서, 더욱 상세하게는 우주공간의 극한환경(극 고온, 극저온현상)에서도 인공위성에서 태양전지판이 원활히 전개되고, 인공위성이 우주선에 실려 우주로 쏘아 올려질 때 발생되는 진동에도 잘 견디며, 상기 태양전지판의 완전 전개되어 우주공간에서 비행시, 발생되는 진동 및 충격 등에도 잘 견디는 특징이 있다. 이와 같이, 본 발명은 우주공간의 극한환경에서도 태양전지판이 전개되도록 인공위성과 태양전지판을 연결하거나 태양전지판과 태양전지판을 연결하는 힌지부에 있어서, 상기 인공위성 또는 태양전지판의 일단부에 결합부재에 의해 부착되는 제 1플레이트와; 상기 태양전지판의 일단부에 결합부재에 의해 부착되되, 상기 제 1플레이트와 끝단부가 축에 의해 결합되어 태양전지판을 전개시키는 제 2플레이트와; 상기 제 1플레이트와 제 2플레이트에 상호 연결되어 제 1플레이트와 제 2플레이트를 탄성적으로 전개되도록 형성된 인장 스프링을 포함하여 구성되는 것을 특징으로 하는 특징이 있다. 인공위성, 태양전지판, 힌지장치, 플레이트, 인장 스프링 | ||||||
| 91 | 다단계태양전지판 인공위성[크니인공위성] | KR1020000005675 | 2000-02-07 | KR1020010077700A | 2001-08-20 | 김남영 |
| PURPOSE: An artificial satellite is provided to effectively supply power, to increase the durability and to lengthen a life of the artificial satellite. CONSTITUTION: Many solar battery plates are prepared inside a sealing box to be insulated from radioactivity. In finishing a life of the initially unfolded solar battery plate, the stood-by solar battery plates are unfolded sequentially. By continuously lengthening a life of an artificial satellite, power is not lack. In leaking the power supply by reducing the efficiency of the solar battery plate, the new solar battery plate is pushed from a main body of the artificial satellite to supplement the power. | ||||||
| 92 | 인공위성용 항법 장치 | KR1020080017794 | 2008-02-27 | KR1020090092510A | 2009-09-01 | 장영근; 최영훈 |
| A navigation device for an artificial satellite is provided to improve the performance of whole system by processing the sensing data distributionally. A navigation device for an artificial satellite comprises a sensor unit(101), a main processor(102), and an interface unit(103). The sensor unit makes the sensing data by measuring the state of the location or the posture of an antibody. The main processor performs the navigation calculation using the sensing data. The interface unit provides an interface between the main processor and the sensor unit. Sensing data is filtered by the interface unit using the predetermined controller. The interface unit temporarily stores the sensing data of the sensor unit and delivers to the main processor once request. | ||||||
| 93 | 무조정 가능한 인공위성용 안테나 | KR1020010036566 | 2001-06-26 | KR1020030000539A | 2003-01-06 | 정만영 |
| PURPOSE: A non-adjustable artificial satellite antenna is provided to smoothly perform communication between the fixed or mobile station and artificial satellite by radiating, in all directions, high gain narrow band beam having angle of 45 degrees with respect to the receiving/transmitting point of receiver/transmitter equipment. CONSTITUTION: A non-adjustable artificial satellite antenna comprises a circular cone(1) having diameter(D) and length(L), and which tunes waves output from a circular reflector mirror(2) and an outer conductor in accordance with the resonance frequency and radiates beams for communication with the artificial satellite in circularly polarized waves or vertically polarized waves; the circular reflector mirror having a diameter(d), and which is disposed to be opposed to the external conductor of the circular cone, and outputs waves input through a coaxial cable(3) to the external conductor of the circular cone; and the coaxial cable having a central conductor connected to the circular cone and an outer conductor connected to the circular reflector mirror, wherein the coaxial cable is connected to a receiver/transmitter equipment arranged on the ground, and outputs waves for communication with the artificial satellite to the circular cone and the circular reflector mirror. | ||||||
| 94 | 인공위성을 이용한 인터넷 방송 시스템 | KR1020010022407 | 2001-04-25 | KR1020020082683A | 2002-10-31 | 장영삼 |
| PURPOSE: An Internet broadcasting system using an artificial satellite is provided to reduce usage of the Internet and a router by realizing a unicast using an IP multicast which uses an artificial satellite as a local server. CONSTITUTION: The first Internet site(20) includes a multicast(21), a web server(22), a hub(23), and an encoder(24). An artificial satellite(30) receives a multicast signal from the encoder(24) and outputs a corresponding signal. The second Internet site(40) includes a central distribution server(41), a web server(42), a hub(43), and a decoder(44). Telephone offices(50-70) comprise local remote distribution servers(51-53)(61-63)(71-73) which receive a multicast signal from the second Internet site(40). An ADSL router(80) receives a signal from the telephone office(50) as a unicast, performs a switching of the signal, and transmits the signal to a user(110). A cable modem(90) receives a signal from the telephone office(60) as a unicast and transmits the signal to a user(120). A private line(100) receives a signal from the telephone office(70) and transmits the signal to a user(130). | ||||||
| 95 | 인공위성 중계기내 ＲＦ 송신장치 | KR1019990047211 | 1999-10-28 | KR1020010039006A | 2001-05-15 | 이무홍; 허원혁 |
| PURPOSE: An RF transmitting apparatus in an artificial satellite repeater is provided to make a compact size of an RF transmitting apparatus by implementing a circuit by using a single temperature compensating variable amplifier, and reduce a production cost and shorten a production term as production processes are reduced by implementing the whole components in a single metal housing. CONSTITUTION: An attenuator(1000) receives a 10GHz extreme high frequency(EHF) signal from a front block, attenuates the amplitude of the signal to a proper level, and outputs it to a multiplier(2000). The multiplier(2000) receives the 10GHz EHF signal from the attenuator(1000), multiplies the frequency of the 10GHz EHF signal and outputs it to a band-pass filter(3000). The band-pass filter(3000) receives a 20GHz EHF signal from the multiplier(2000), filters it to pass only a desired frequency band of the 20GHz EHF signal and outputs it to a variable attenuator(4000). When an attenuation set level is determined according to a user's selection, the variable attenuator(4000) receives the 20GHz EHF signal from the band-pass filter(3000), attenuates the amplitude of the EHF signal corresponding to the attenuation set level, and outputs it to a three-step variable amplifier(6000). A temperature compensation driving circuit(5000) measures a temperature of an artificial satellite repeater, and outputs a corresponding temperature compensation control voltage to the three-step variable amplifier(6000). The three-step variable amplifier(6000) of which an amplification level is adjusted by the temperature compensation control voltage outputted from the temperature compensation driving circuit(5000), receives the 20GHz EHF signal from the variable attenuator(4000) and amplifies the amplitude of the 20GHz EHF signal to a proper level. | ||||||
| 96 | 一种利用和差波束天线与人造卫星信号进行方位角测量的天线姿态传感器 | CN201620567255.0 | 2016-06-12 | CN205825970U | 2016-12-21 | 张志军; 曹晓京 |
| 一种利用和差波束天线与人造卫星信号进行方位角测量的天线姿态传感器，在基站天线位置设置用于产生和波束及差波束两种形式波束的和差波束天线作为接收天线，对人造卫星的信号同时或先后进行接收，比较不同波束的输出信号强度变化，在差波束的输出信号强度与和波束的输出信号强度的差别达到最大时，差波束的接收凹点所面对的方向就是卫星的方位角，即天线的方位角；本实用新型利用和差波束天线与人造卫星信号测量方位角，利用陀螺仪持续跟踪测量天线方位角变化，利用三轴重力加速度传感器测量天线俯仰角，并利用蓄电池和外接电源为传感器供电，可精确测量基站天线姿态，结构简单，成本低，便于生产。 | ||||||
| 97 | 인공위성을 이용한 에이디에스엘 서비스 장치 | KR1020010020230 | 2001-04-16 | KR1020020080589A | 2002-10-26 | 이기영; 박성호; 주광진 |
| PURPOSE: An ADSL(Asymmetric Digital Subscriber Line) service device using an artificial satellite is provided to transmit data through a telephone line and to receive data through the artificial satellite, so that an upload speed as well as a download speed is raised. CONSTITUTION: In a subscriber device(900), a satellite receiving unit(200) receives signals of a predetermined downstream channel from a satellite(400). A filtering unit(150) filters signals in a frequency band of the downstream channel and filters signals in a frequency band of an upstream channel through a telephone line. A modem(110) demodulates the filtered downstream channel signals and modulates the upstream channel signals. The subscriber device(900) transmits upstream channel data to a telephone office(700) through the filtering unit(150). The telephone office(700) transmits downstream channel data to be transmitted to a subscriber to a satellite data station(600). The satellite data station(600) transmits the received downstream channel signals to a satellite transmission antenna(500). The downstream channel signals passes through the satellite(400) and are received to a satellite receiving antenna(300), thus being inputted to the satellite receiving unit(200). | ||||||
| 98 | 인공위성을 이용한 인터넷 서비스 시스템 | KR1020000045068 | 2000-08-03 | KR1020020011653A | 2002-02-09 | 지환국 |
| PURPOSE: An Internet service system using an artificial satellite is provided to connect various subscriber networks with television systems using a set-top box so as to enable both way communication, to allow users to be able to be provided with ultra-high-speed artificial satellite Internet service without purchasing computer systems. CONSTITUTION: An Internet service system using an artificial satellite has a main server(10) providing information services including shopping information, chatting service, mail service and network games and a variety of Internet services according to a user's choice, and a relay server(20) that is connected with a plurality of users(60) through a subscriber network(40), transmits an information request signal of each user to the main server and sends information data delivered from the main server to each user through the subscriber networks. The system further includes a satellite transmitter/receiver(31,32) that is connected to each of the main server and the relay server and transmits/receives a data information signal between the main server and the relay server using both way communication through an artificial satellite, and a set-top box(50) connected between the subscriber network and the users to enable both way communication. | ||||||
| 99 | 인공위성을 이용한 인터넷 서비스 시스템 | KR1020000021008 | 2000-04-20 | KR1020010097171A | 2001-11-08 | 지환국 |
| 사용자가 낮은 비용 부담으로 초고속의 위성 인터넷 서비스를 제공받을 수 있도록 하기 위하여, 사용자 선택에 따른 쇼핑 정보, 채팅 서비스, 메일 서비스, 네트웍 게임을 포함한 정보 서비스 및 다양한 인터넷 서비스를 제공하여 주는 메인 서버와, 다수의 사용자를 네트웍으로 연결하여 주며, 각 사용자들의 정보 요구 신호를 상기 메인 서버로 전송하여 주고, 상기 메인 서버로부터 전송되는 정보 데이터를 각 사용자측으로 전송하여 주는 중계 서버와, 상기 메인 서버와 중계 서버에 각각 접속되며, 상기 메인 서버와 중계 서버 사이의 데이터 정보 신호를 인공위성을 통한 양방향 통신으로 송수신하여 주는 위성 송수신기를 포함하여 중계 서버를 통해 다수의 사용자들을 네트웍으로 접속하도록 하고, 중계 서버와 다양한 인터넷 서비스를 제공하는 메� �� 서버 사이의 통신을 인공위성을 통해 이루어지도록 함으로써 사용자는 위성 인터넷 서비스 이용을 위한 수신기 등의 장비를 설치하지 않고도 낮은 비용 부담으로 초고속의 위성 인터넷 서비스를 이용할 수 있게 된다. | ||||||
| 100 | 인공위성용배터리감시장치 | KR1019980047236 | 1998-11-05 | KR1020000031282A | 2000-06-05 | 이상곤 |
| PURPOSE: A device for monitoring a battery is provided to automatically keep a battery without monitoring an additional worker by automatically blocking a charging current until the charging current is re-injected by removing a cause of generation of abnormality. CONSTITUTION: A battery(11) is kept inside a chamber(10), and a charging current is supplied through a relay(43). Herein, a temperature sensor for sensing a temperature inside the battery and the chamber and a voltage and a current sensor for sensing the charging voltage and current of the battery are installed in the chamber. A sending voltage of the sensor of a temperature, a voltage and a current is detected in a sensing IC(20), and a computer(30) sets up the ranges of the temperature, voltage, and current by using a general personal computer. In addition, the range of monitor of the computer set up by a user is compared with a sensor output in the sensing IC(20). That is, if the sensing output is not in the range of monitor set up in the computer, the sensing IC outputs an alarm signal. | ||||||
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