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公开(公告)号：US09685770B2
公开(公告)日：2017-06-20
申请号：US13851089
申请日：2013-03-26
Applicant: KOREA ASTRONOMY AND SPACE SCIENCE INSTITUTE
Inventor： Chan Park , Moo-Young Chun , Jae Sok Oh , Jakyoung Nah
Abstract: Disclosed is a vacuum wall-through structure to be installed in a hole formed in a wall of a vacuum chamber. The vacuum wall-through structure includes a cable holder that holds a cable at the center thereof and a cable holder cover installed outside the cable holder.
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公开(公告)号：US20130276300A1
公开(公告)日：2013-10-24
申请号：US13845658
申请日：2013-03-18
Applicant: KOREA ASTRONOMY AND SPACE SCIENCE INSTITUTE
Inventor： Sang Mok Cha , In-Soo Yuk , Chan Park , Moo Young Chun
IPC: B23P19/04
CPC classification number: B23P19/04 , B25B27/023 , B25B27/04 , Y10T29/53
Abstract: Provided is a miniature pin extracting device for extracting a miniature pin inserted into a part. The miniature pin extracting device includes a coupling having a polygonal pillar shape, the coupling having a lower end coupled to the locating pin, a retainer mounted outside the coupling, and a screw part supported by the retainer, the screw part being coupled to an upper end of the coupling. Thus, a rotation force of the screw part may be converted into a vertical axial motion through the retainer to safely extract the locating pin without lateral force and rotation, thereby minimizing damage of the part.
Abstract translation: 提供了一种用于提取插入到部件中的微型销的微型引脚提取装置。 微型销提取装置包括具有多边形柱形的联接器，联接器具有联接到定位销的下端，安装在联接器外部的保持器和由保持器支撑的螺钉部分，螺钉部分联接到上部 耦合端。 因此，可以通过保持器将螺钉部分的旋转力转换成垂直的轴向运动，以安全地提取定位销而无需侧向力和旋转，从而最小化零件的损坏。
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Patent Agency Ranking
公开(公告)号：US10948610B2
公开(公告)日：2021-03-16
申请号：US15675304
申请日：2017-08-11
Inventor： Junga Hwang
IPC: G01T1/02
Abstract: An analysis system for an aviation radiation dose includes: a proton spectrum generator which generates a galactic cosmic ray incident on the Earth's atmosphere and a proton spectrum corresponding to a solar proton event; a global radiation dose map producer which generates-particle transport and produces a radiation dose map; a global radiation dose map converter which converts the radiation dose map based on a standard atmosphere into a radiation dose map corresponding to current atmosphere conditions in real time; and a database in which data necessary for operations of the proton spectrum generator, the global radiation dose map producer and the global radiation dose map converter is previously calculated and stored, thereby having an effect on estimating any radiation route dose if information about an arbitrary path and time is given.
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公开(公告)号：US20180045836A1
公开(公告)日：2018-02-15
申请号：US15675304
申请日：2017-08-11
Inventor： Junga HWANG
IPC: G01T1/02
CPC classification number: G01T1/02
Abstract: An analysis system for an aviation radiation dose according to the present invention includes: a proton spectrum generator which calculates a galactic cosmic ray incident on the Earth's atmosphere and a proton spectrum corresponding to a solar proton event; a global radiation dose map producer which calculates particle transport based on the proton spectrum and produces a radiation dose map; a global radiation dose map converter which converts the radiation dose map produced based on a standard atmosphere into a radiation dose map corresponding to current atmosphere conditions in real time; and a database in which data necessary for operations of the proton spectrum generator, the global radiation dose map producer and the global radiation dose map converter is previously calculated and stored, thereby having an effect on estimating a radiation dose of another route if another piece of information about an arbitrary path and time is given besides a previous given path.
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公开(公告)号：US09541673B2
公开(公告)日：2017-01-10
申请号：US14709997
申请日：2015-05-12
Applicant: Korea Astronomy and Space Science Institute
Inventor： Ji-Hye Baek , Jaejin Lee , Seonghwan Choi , Eunmi Hwang , Young-Deuk Park
CPC classification number: G01W1/02 , G01W1/10 , G08G5/0004 , G08G5/0013 , G08G5/0021 , G08G5/0052 , G08G5/0091
Abstract: A space weather monitoring system for polar routes includes: a satellite which flies over polar routes; a route-information providing server which receives data collected by the satellite monitoring the polar routes and generates various pieces of information about space weather; a flight vehicle which makes a request for information about the polar routes of the flight to the route-information providing server, and flies over the polar routes based on the received information; and a network which relays data among the satellite, the route-information providing server and the flight vehicle, so that an aurora-distribution map needed for an aircraft flight, an electromagnetic wave absorption map based on the ionosphere, information about space weather, and the situation and forecast of the space weather can be provided to an airline, thereby having effects on allowing the airline to check the information about the space weather in real time and fully considering a user who is unfamiliar to the space weather.
Abstract translation: 极地航路的空间气象监测系统包括：飞越极地航路的卫星; 路线信息提供服务器，接收卫星收集的数据，监测极地路线，并产生有关空间天气的各种信息; 向飞行信息提供服务器请求关于飞行极地路线的信息的飞行器，并基于接收的信息飞越极地路线; 以及在卫星，路线信息提供服务器和飞行车辆之间中继数据的网络，使得飞机飞行所需的极光分布图，基于电离层的电磁波吸收图，关于空间天气的信息，以及 可以向航空公司提供空间天气的情况和预测，从而影响航空公司实时检查有关空间天气的信息，充分考虑到空间天气不熟悉的用户。
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公开(公告)号：US08976341B2
公开(公告)日：2015-03-10
申请号：US13967204
申请日：2013-08-14
Applicant: Korea Astronomy and Space Science Institute
Inventor： Seung Cheol Bang , Hyung Chul Lim , Jong Uk Park
CPC classification number: G01S7/484 , G01S7/4865 , G01S17/105
Abstract: An optoelectric control apparatus for a satellite laser ranging system comprises a communication controller for externally receiving optoelectric control data. Memory is connected to the communication controller and stores a round trip distance to a satellite. A laser generation control unit is connected to the communication controller and outputs a laser fire signal. A signal measurement unit receives a laser start time. A real-time conversion unit is connected to the signal measurement unit and the communication controller, and converts a predicted laser arrival time into real time. A Lagrange interpolation processor is connected to the real-time conversion unit and the memory, and calculates a time at which laser light fired by a laser transmission unit returns back to a laser reception unit (laser arrival time). The clock unit is connected to a time measurement unit, the real-time conversion unit, a register unit, and a delay unit, and outputs time information.
Abstract translation: 一种用于卫星激光测距系统的光电控制装置，包括用于外部接收光电控制数据的通信控制器。 存储器连接到通信控制器并存储到卫星的往返距离。 激光产生控制单元连接到通信控制器并输出激光火焰信号。 信号测量单元接收激光开始时间。 实时转换单元连接到信号测量单元和通信控制器，并将预测的激光到达时间实时转换。 拉格朗日内插处理器连接到实时转换单元和存储器，并且计算由激光传输单元发射的激光返回激光接收单元（激光到达时间）的时间。 时钟单元连接到时间测量单元，实时转换单元，寄存器单元和延迟单元，并输出时间信息。
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公开(公告)号：US20140118717A1
公开(公告)日：2014-05-01
申请号：US13967204
申请日：2013-08-14
Applicant: KOREA ASTRONOMY AND SPACE SCIENCE INSTITUTE
Inventor： Seung Cheol Bang , Hyung Chul Lim , Jong Uk Park
IPC: G01C3/08
CPC classification number: G01S7/484 , G01S7/4865 , G01S17/105
Abstract: An optoelectric control apparatus for a satellite laser ranging system comprises a communication controller for externally receiving optoelectric control data. Memory is connected to the communication controller and stores a round trip distance to a satellite. A laser generation control unit is connected to the communication controller and outputs a laser fire signal. A signal measurement unit receives a laser start time. A real-time conversion unit is connected to the signal measurement unit and the communication controller, and converts a predicted laser arrival time into real time. A Lagrange interpolation processor is connected to the real-time conversion unit and the memory, and calculates a time at which laser light fired by a laser transmission unit returns back to a laser reception unit (laser arrival time). The clock unit is connected to a time measurement unit, the real-time conversion unit, a register unit, and a delay unit, and outputs time information.
Abstract translation: 一种用于卫星激光测距系统的光电控制装置，包括用于外部接收光电控制数据的通信控制器。 存储器连接到通信控制器并存储到卫星的往返距离。 激光产生控制单元连接到通信控制器并输出激光火焰信号。 信号测量单元接收激光开始时间。 实时转换单元连接到信号测量单元和通信控制器，并将预测的激光到达时间实时转换。 拉格朗日内插处理器连接到实时转换单元和存储器，并且计算由激光传输单元发射的激光返回激光接收单元（激光到达时间）的时间。 时钟单元连接到时间测量单元，实时转换单元，寄存器单元和延迟单元，并输出时间信息。
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