• 마이크로전자및패키징학회지
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• 제23권2호
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• pp.73-78
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• 2016

집적회로(Integrated Circuit) 소자의 트랜지스터(transistor) 밀도 증가는 소자에서 발생하는 열 방출(heat dissipation)의 급격한 상승을 초래하여 열 문제를 발생시키고, 이는 소자의 성능과 열적 신뢰성에 영향을 크게 미친다. 열문제의 해결방안 중 본 연구에서는 냉매를 이용한 액체 냉각방법을 연구하였으며, 실리콘 웨이퍼에 관통실리콘비아(through Si via)와 마이크로 채널(microchannel)을 딥 반응성 이온 애칭(deep reactive ion etching)로 구현한 후 유리기판과 어노딕본딩을 통하여 액체 냉각 구조를 제작하였다. 제작된 마이크로 채널 위에 Ag, Cu 또는 Cr/Au/Cu bump를 스크린프린팅(screen printing) 방법으로 형성하였고, 범프의 유무를 통해 액체 냉각 전후의 냉각 모듈의 실리콘 표면온도의 변화를 적외선현미경으로 분석하였다. Cr/Au/Cu bump가 탑재된 액체 냉각 모듈의 경우 가열온도 $200^{\circ}C$에서 냉각 전후의 실리콘 표면 온도 차이는 약 $45.2^{\circ}C$이고, 전력밀도 감소는 약 $2.8W/cm^2$ 이었다.

• 마이크로전자및패키징학회지
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• 제22권4호
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• pp.31-36
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• 2015

전자소자의 다기능, 고밀도, 고성능, 그리고 소형화는 전자 패키지 기술에 초미세 피치 플립 칩, 3D 패키지, 유연 패키지, 등 새로운 기술 패러다임 전환을 가져왔으며, 이로 인해 패키지 된 칩의 열 관리는 소자의 성능을 좌우하는 중요한 요소로 대두되고 있다. Heat sink, heat spreader, TIM, 열전 냉각기, 등 많은 소자 냉각 방법들 중 본 연구에서는 냉매를 이용한 on-chip 액체 냉각 모듈을 Si 웨이퍼에 제작하고, 마이크로 채널 디자인에 따른 냉각 효과를 분석하였다. 마이크로 채널은 딥 반응성 이온 에칭을 이용하여 형성하였고, 3 종류 디자인(straight MC, serpentine MC, zigzag MC)으로 제작하여 마이크로 채널 디자인이 냉각 효율에 미치는 영향을 관찰하였다. 가열온도 $200^{\circ}C$, 냉매 유동속도 150 ml/min의 경우에서 straight MC가 약 $44^{\circ}C$의 높은 냉각 전후의 온도 차를 보였다. 냉매의 흐름과 상 변화는 형광현미경으로 관찰하였으며, 냉각 전후의 온도 차는 적외선현미경을 이용하여 분석하였다.

• Design & Manufacturing
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• 제17권4호
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• pp.63-71
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• 2023

In order to increase the extrusion production speed of aluminum, extrusion die cooling technology using liquid nitrogen has recently attracted a lot of attention. Increasing the extrusion speed increases the temperature of the bearing area of extrusion dies and the extrusion profile, which may cause defects on the surface of extruded profile. Extrusion die cooling technology is to directly inject liquid nitrogen through a cooling channel formed between the die and the backer inside the die-set. The liquid nitrogen removes heat from the die-set, and gaseous nitrogen at the exit of the channel, covers the extrusion profile of an inert atmosphere reducing the oxidation and the profile temperature. The aim of this study is to evaluate the cooling capacity by applying die cooling to extrusion of Al-Mn-based aluminum alloy flat tubes, and to investigate the effects of die cooling on the change in extrusion characteristics of flat tubes. Cooling capacity was confirmed by observing the temperature change of the extrusion profile depending on whether or not die cooling is applied. To observe changes in material characteristics due to die cooling, surface observation is conducted and microstructure and precipitate analysis are performed by FE-SEM on the surface and longitudinal cross section of the extruded flat tubes.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제29회 추계학술대회논문집
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• pp.170-173
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• 2007

본 연구에서는 액체로켓엔진 내부에 라이너를 설치하고 기체 질소를 이용한 막냉각 방법을 사용하여, 라이너의 막냉각 특성을 살펴보았다. 고온 가스는 액체로켓 연소가스와 액체질소를 혼합하여 사용하였다. 기존의 액체로켓엔진 시험 설비에 추가적으로 라이너 냉각 기체를 공급 설비를 구축하였으며, 라이너 및 냉각 기체 공급부를 제작하였다. 10초 연소 실험을 통해 라이너 내부 고온 가스의 온도와 라이너 외부 벽면 온도를 측정하였으며, 기체 질소에 의한 라이너 냉각 특성을 확인하였다.

• 한국초전도ㆍ저온공학회논문지
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• 제19권2호
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• pp.1-8
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• 2017

Recently, Research and development activity of HTS (High Temperature Superconducting) power application is very progressive worldwide. Especially, HTS cable system and HTSFCL (HTS Fault current limiter) system are proceeding to practical stages. In such system and equipment, cryogenic cooling system, which makes HTS equipment cooled lower than critical temperature, is one of crucial components. In this article, cryogenic cooling system for HTS application, mainly cable, is reviewed. Cryogenic cooling system can be categorized into conduction cooling system and immersion cooling system. In practical HTS power application area, immersion cooling system with sub-cooled liquid nitrogen is preferred. The immersion cooling system is besides grouped into open cycle system and closed cycle system. Turbo-Brayton refrigerator is a key component for closed cycle system. Those two cooling systems are focused in this article. And, each design and component of the cooling system is explained.

• 한국추진공학회지
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• 제10권4호
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• pp.85-92
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• 2006

액체로켓엔진의 막냉각 성능 예측을 위한 설계 프로그램을 개발하였다. 저혼합비 가스층이 가지는 열차단 효과를 CFD를 적용하여 해석하였다. CFD 해석 결과에 기반한 1차원 막냉각 모델을 기존의 재생냉각 프로그램에 적용하였다. 축소형 calorimetric 연소기와 실물형 연소실의 열유속 시험 데이터비교를 통하여, 비록 과다예측 특성을 보이기는 하지만 만족할만한 결과를 얻었다. 이로서 막냉각이 로켓엔진의 노즐목의 열하중 감소에 효과적임이 확인되었다.

• 설비공학논문집
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• 제18권1호
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• pp.24-30
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• 2006

Three liquid cooling heat exchangers for cooling of telecommunication equipment were designed and their cooling performances were tested. The liquid cooling heat exchangers had twelve rectangular channels $(5\times3 mm)$ with different flow paths of 1, 4, and 12. Silicon rubber heaters were used to provide heat flux to the test section. Heat input was varied from 75 to 400 W, while flow rate and inlet temperature of working fluid were altered from 1.2 to 4.0 liter/fin and from 15 to 3$30^{\circ}C$, respectively. The 4-path heat exchanger showed lower and more uniform average inner temperatures between heaters and the surface of heat exchanger than those of the others. To obtain optimal distribution of working fluid to each channels of liquid cooling heat exchangers, 2-3-2 and 4-3 type tube distributors were designed, and their distribution performances of working fluid were numerically and experimentally investigated. The distributor of the 2-3-2 type showed superior distribution performance compared with those of the 4-3 type distributor.

• Membrane and Water Treatment
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• 제8권4호
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• pp.355-367
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• 2017

In India, the current operation of condenser cooling system & effluent disposal system in existing power plants aims to reduce drawal of seawater and to achieve Zero Liquid Discharge to meet the demands of statutory requirements, water scarcity and ecological system. Particularly in the Steam-Electric power plants, condenser cooling system adopts Once through cooling (OTC) system which requires more drawal of seawater and effluent disposal system adopts sea outfall system which discharges hot water into sea. This paper presents an overview of closed-loop technology for condenser cooling system and to achieve Zero Liquid Discharge plant in Steam-Electric power plants making it lesser drawal of seawater and complete elimination of hot water discharges into sea. The closed-loop technology for condenser cooling system reduces the drawal of seawater by 92% and Zero Liquid Discharge plant eliminates the hot water discharges into sea by 100%. Further, the proposed modification generates revenue out of selling potable water and ZLD free flowing solids at INR 81,97,20,000 per annum (considering INR 60/Cu.m, 330 days/year and 90% availability) and INR 23,760 per annum (considering INR 100/Ton, 330 days/year and 90% availability) respectively. This proposed modification costs INR 870,00,00,000 with payback period of less than 11 years. The conventional technology can be replaced with this proposed technique in the existing and upcoming power plants.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2002년도 추계 학술대회논문집
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• pp.1-7
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• 2002

Liquid rocket regenerative cooling design procedure is introduced with the example of the 250 kg thrust, LOx/kerocine experimental test rocket system. The presentation may be useful for numerical analysists who have limited experiences with real rocket system.

• 한국수소및신에너지학회논문집
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• 제30권6호
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• pp.490-498
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• 2019

The intermittent electric power supply of renewable energy can have extremely negative effect on power grid, so long-term and large-scale storage for energy released from renewable energy source is required for ensuring a stable supply of electric power. Power to gas which can convert and store the surplus electric power as hydrogen through water electrolysis is being actively studied in response to increasing supply of renewable energy. In this paper, we proposed the novel concept of hydrogen liquefaction process combined with pre-cooling process using the liquid air. It is that hydrogen converted from surplus electric power of renewable energy was liquefied through the hydrogen liquefaction process and vaporization heat of liquid hydrogen was conversely recovered to liquid air from ambient air. Moreover, Comparisons of specific energy consumption (kWh/kg) saved for using the liquid air pre-cooling was quantitatively conducted through the performance analysis. Consequently, about 12% of specific energy consumption of hydrogen liquefaction process was reduced with introducing liquid air for pre-cooling and optimal design point of helium Brayton cycle was identified by sensitivity analysis on change of compression/expansion ratio.