• Proceedings of the KIEE Conference
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• 2002.07b
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• pp.747-749
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• 2002

초전도 마그네트 시스템의 냉각방법 중, 액체 헬륨등의 극저온 유체를 이용한 액체냉각방식이 극저온 냉동기를 이용한 직접 전도냉각 방식에 비해 신뢰도가 높은 열적 안정성으로 인하여 현재도 많은 초전도 마그네트 시스템이 액체냉각방식을 이용하고 있다. 그러나, 고가의 극저온 액체의 재충전으로 인하여 경제성이 낮고 취급이 불편한 단점이 있다 이러한 액체냉각방식의 단점을 보완하고자 극저온 유체를 시스템 안에서 직접 응축하여 재충전을 하지 않는 재응축형 시스템을 개발하여 실험하였다. 실험에 사용한 초전도 마그네트 시스템은 상온보아 1270 mm. 최대자장 0.3 T로 설계되었고, 금속 전류도입선과 HTS 전류도입선을 복합적으로 사용하였으며, 복사차폐막 냉각용 극저온 냉동기와 헬륨 재응축용 극저온 냉동기를 사용하였다. 초전도 마그네트는 200 A에서 1600 gauss의 자장으로 운전하였고 극저온 용기에서는 0.05 bar의 압력으로 액체 헬륨이 증발하지 않고 유지되었다.

• Proceedings of the KIEE Conference
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• 2009.07a
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• pp.836_837
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• 2009

PC용 냉각장치의 일환으로 CPU의 외벽에 방열판을 달고 열전냉각모듈을 설치한 후 방열판을 냉각하기 위해서 펌프를 적용한 수냉식 냉각 시스템을 개발하고자 하였다. 먼저, 냉각 시 펌프의 부하를 설계하고 그 용량에 적절한 저소음, 고효율 BLDC 모터를 개발하고자, 상용화된 외국제품인 S사의 저효율 단상 BLDC 모터가 적용된 수냉식 펌프를 기준으로 하였다. S사의 단상 BLDC 모터에 대한 시뮬레이션과 테스트를 통해서 거의 비슷한 결과를 얻었으며, 이를 이용하여 단가가 다소 상승하더라도 효율과 성능을 향상시킬 수 있는 3상 BLDC 모터구조로 설계를 하였으며, 그 결과 효율이 거의 2배 향상되며 출력 또한 향상됨을 시뮬레이션으로 구현하였다.

• The Transactions of the Korean Institute of Power Electronics
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• v.9 no.4
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• pp.350-355
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• 2004

This paper deals with the design of a heat dissipation system, which consists of a heat source of power semiconductor devices, a heat sink ;md a fan for the forced air cooling. It suggests the method of appropriately dividing the whole heat transfer system into analytical subsystems and also presents the correspondent analytic or experimental design equations for the subsystems. The experimental results on the designed heat dissipation system for the 400kW IGBT inverter show less than 10［%］ error with respect to the design temperature and therefore verify the validity of the proposed analytical design method in the steady state.

• Journal of the Korean Society for Heat Treatment
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• v.15 no.3
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• pp.147-151
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• 2002

• The Bulletin of The Korean Astronomical Society
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• v.30 no.1
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• pp.34.1-34.1
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• 2005

• 한국항공운항학회:학술대회논문집
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• 2004.11a
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• pp.167-172
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• 2004

• Journal of Internet of Things and Convergence
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• v.10 no.2
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• pp.125-130
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• 2024

With the rapid growth of mobility technology, the industrial sector is demanding storage devices that can reliably process data from various equipment and sensors in vehicles. NAND flash memory is being utilized as a storage device in mobility environments because it has the advantages of low power and fast data processing speed as well as strong external shock resistance. However, flash memory is characterized by data corruption due to long-term exposure to high temperatures. Therefore, a dedicated system for temperature management is required in mobility environments where high temperature exposure due to weather or external heat sources such as solar radiation is frequent. This paper designs a dedicated temperature management system for managing storage device temperature in a mobility environment. The designed temperature management system is a hybrid of traditional air cooling and water cooling technologies. The cooling method is designed to operate adaptively according to the temperature of the storage device, and it is designed not to operate when the temperature step is low to improve energy efficiency. Finally, experiments were conducted to analyze the temperature difference between each cooling method and different heat dissipation materials, proving that the temperature management policy is effective in maintaining performance.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.11a
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• pp.437-438
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• 2008

To improve efficiency and allowable life of gas turbine and ram jet, the proper cooling techniques are needed. It is required not only the basic research of variable cooling techniques but also analysis of real operating conditions when we design the cooling system. From the present experimental and analytical results, we can predict the thermal stress and allowable life. This design process is for a thermal design technique that is the most foundational design technique to improve the efficiency of gas turbines and ram jets

• Journal of the Korea Institute of Information and Communication Engineering
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• v.18 no.6
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• pp.1462-1468
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• 2014

Xe gas is moved to target from GPM. It is used to feasible nuclear reaction from proton of 30MeV cyclotron being investigated by the Xe-124 gas target system. This system is divided into four parts. The hardware system was constructed by solidworks 3-D CAD and Helium supply is to cool the Havor foil. The Cooling water has the job of cooling down the temperature when Xe gas is being investigated in the target. Temperature and pressure gauges are attached to be checked easily. GPM has the part that prepares to transport Xe gas. There are storage vessel that stores Xe gas, the cold trap that filters humidity and impurity and lastly storage vessel that temporarily stores Xe gas. HCS using the helium is to clean and cool for each part. These parts are configured with SIEMENS PLC and PcVue monitoring program for more comfortable and easy maintenance.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.628-635
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• 2010

Properties of bleed air that is air source of ECS(Environmental Control System) can be rapidly changed with airplane engine operating conditions during flight. Therefore, ECS can be operated at a high performance or not during flight. So, high performance ACM has to be developed in order to flight safely. A adaptability of phase changing heat exchanger was esteemed at ACM type ECS in this study. As a result of this study, it is found that ECS outlet temperature can be controlled in a certain range with the phase changing phenomenon.