• 제목/요약/키워드: Micro-Cooler

검색결과 34건 처리시간 0.024초

마이크로 채널내 박막영역에서의 증발 모델링 (Evaporative Modeling in n Thin Film Region of Micro-Channel)

  • 박경우;노관중;이관수
    • 대한기계학회논문집B
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    • 제27권1호
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    • pp.17-24
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    • 2003
  • A mathematical model of the hydrodynamic and heat transfer performances of two-phase flow (gas-liquid) in thin film region of micro channel is proposed. For the formulation of modeling, the flow of the vapor phase and the shear stress at the liquid-vapor interface are considered. In this work, disjoining pressure and capillary force which drive the liquid flow at the liquid-vapor interface in thin film region are adopted also. Using the model, the effects of the variations of channel height and heat flux on the flow and heat transfer characteristics are investigated. Results show that the influence of variation of vapor pressure on the liquid film flow is not negligible. The heat flux in thin-film region is the most important operation factor of micro cooler system.

혹서기(酷暑期) 환경요인(環境要因)에 의한 전통주거건축(傳統住居建築)의 공간구성(空間構成)에 관한 연구 - 전북지방 농촌주택(農村住宅)을 중심으로 - (A Study on the Chracter of Spatial Organization in traditional House by hot Weather environmental Factors - Focused on the rural house in Chonbuk province -)

  • 김용집
    • 건축역사연구
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    • 제7권2호
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    • pp.49-62
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    • 1998
  • The character of spatial organization in rtaditional house is found through the analysis of field survey and measure of its micro climate in hot weather period of summer. The mean temperature of interior space is higher than outside space of the house. In the point of structural conditions, inside of Choga in caustal and mountain area is cooler than any other houses. In inland area, slate roof house is cooler than Choga. In mountain area, the thermal difference of inside and outside in Kyubjib is higher than Hotjib. In the point of spatial conditions, kitchen is the coolest space and very suitable for spatial organization. Anbang is the hottest space because of its centeral position in the house. In wind condition, mountain area is windy and caustal area is calm. Around the house the rear side of the house is windy and left side is calm.

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Design and Fabrication of a Micro PZT Cantilever Array Actuator for Applications in Fluidic Systems

  • Kim Hyonse;In Chihyun;Yoon Gilho;Kim Jongwon
    • Journal of Mechanical Science and Technology
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    • 제19권8호
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    • pp.1544-1553
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    • 2005
  • In this article, a micro cantilever array actuated by PZT films is designed and fabricated for micro fluidic systems. The design features for maximizing tip deflections and minimizing fluid leakage are described. The governing equation of the composite PZT cantilever is derived and the actuating behavior predicted. The calculated value of the tip deflection was 15 ${\mu}m$ at 5 V. The fabrication process from SIMOX (Separation by oxygen ion implantation) wafer is presented in detail with the PZT film deposition process. The PZT films are characterized by investigating the ferroelectric properties, dielectric constant, and dielectric loss. Tip deflections of 12 ${\mu}m$ at 5 V are measured, which agreed well with the predicted value. The 18 ${\mu}l/s$ leakage rate of air was observed at a pressure difference of 1000 Pa. Micro cooler is introduced, and its possible application to micro compressor is discussed.

형상기억합금 메쉬 와셔를 이용한 우주용 냉각기 진동절연기의 발사 진동 및 충격 저감 성능검증 (Verification of Launch Vibration and Shock Isolation Performance for Spaceborne Compressor Vibration Isolator with SMA Mesh Washer)

  • 이명재;한제헌;오현웅
    • 한국소음진동공학회논문집
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    • 제24권7호
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    • pp.517-524
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    • 2014
  • Micro-vibration induced by on-board equipments such as fly-wheel and cryogenic cooler with mechanical moving parts affects the image quality of high-resolution observation satellite. Micro-vibration isolation system has been widely used for enhancing the pointing performance of observation satellites. In general, the micro-vibration isolation system requires a launch locking mechanism additionally to guarantee the structural safety of mission payloads supported by the isolation system with low stiffness under launch environment. In this study, we propose a passive launch and on-orbit vibration isolation system using shape memory alloy mesh washers for the micro-vibration isolation of spaceborne compressor, which does not require the additional launch locking mechanism. The basic characteristics of the isolator were measured in static and free vibration tests of the isolator, and a simple equivalent model of the isolator was proposed. The effectiveness of the isolator design in a launch environment was demonstrated through sine vibration, random vibration and shock tests.

의탄성 형상기억합금 메쉬 와셔가 적용된 수동형 진동절연기의 수학적 등가모델 도출 (Derivation of Numerical Equivalent Model of Vibration Isolator using Pseudoelastic SMA Mesh Washer)

  • 권성철;전수현;오현웅
    • 항공우주시스템공학회지
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    • 제8권3호
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    • pp.6-13
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    • 2014
  • A passive launch and on-orbit vibration isolator using SMA(Shape Memory Alloy) washer for both the structural safety of the micro-vibration source by attenuating the transmitted force under launch loads and the micro-vibration isolation during their on-orbit operation has been proposed, which does not require the additional launch locking mechanism. To measure the characteristics of SMA mesh washer, we performed compressive loading tests with a single SMA mesh washer and a vibration isolator using SMA mesh washer. The numerical equivalent model of vibration isolator using SMA mesh washer composed of two spring and viscous damping elements has been verified that both stiffness and viscous damping varied with respect to compressed deformations. In addition, the effectiveness of launch loads and micro-vibration reduction has been investigated through the dynamic characteristics measurement test of cooler assembly combined with passive vibration isolator.

자동차용 이산화탄소 냉방 시스템의 정상상태 및 동적 특성에 관한 연구 (Studies on the Steady State and Dynamic Characteristics of a Carbon Dioxide Air-Conditioning System for Vehicles)

  • 박민수;김성철;김달원;김민수
    • 대한기계학회논문집B
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    • 제31권6호
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    • pp.531-538
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    • 2007
  • In this study, an air conditioning system using carbon dioxide as a refrigerant was developed for automotive cabin cooling. Experiments have been carried out to examine the steady state and dynamic characteristics of this system. The system consists of a compressor, a gas cooler, an evaporator, an expansion device, an internal heat exchanger and an accumulator. The compressor is a variable displacement type, driven by the electric motor, and the gas cooler and the evaporator are aluminum extruded heat exchangers of micro channel type. The $CO_2-refrigerant$ charge, the compressor speed, the air inlet temperature of the gas cooler, the air inlet temperature and the air flow rate of the evaporator and the cooling load are varied and the performance of the system is experimentally investigated. As the compressor speed increased, cooling capacity increased, but the coefficient of performance was deteriorated. As the cabin air temperature or the air flow rate to the cabin was set high, both the cooling capacity and the COP increased. In the cool down experiment with 1.0 or 2.0 kW of heat load, the dynamic characteristics of the air-conditioning system were investigated. For a given capacity of compressor, cool down speed was monitored, and the temperature change was acceptable fur low heat load condition.

박막형 열전 냉각 모듈 제작을 위한 디자인 모델 소개 (Introduction to the Thin Film Thermoelectric Cooler Design Theories)

  • 전성재;장봉균;송준엽;현승민;이후정
    • 한국정밀공학회지
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    • 제31권10호
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    • pp.881-887
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    • 2014
  • Peltier 효과를 이용한 박막형 열전 냉각 모듈은 열전 재료에 의한 열 출입의 방향에 따라서 수직형 구조와 수평구조로 나누어진다. 이와 같은 박막형 열전 냉각 모듈의 성능은 기존의 벌크 형태의 냉각 모듈을 평가하기 위해 사용하는 모델을 이용하여 측정할 수 있다. 우리가 제조한 열전 박막을 모델에 적용하여 열전재료의 길이 변화에 따른 열 방출 성능을 평가 하여 보았다. 재료의 성능이 향상됨에 따라서 동일한 열 전기적 저항에서 최대 열 방출 성능은 $73.9W/cm^2$에서 $131.2W/cm^2$으로 크게 증가하는 것을 알 수 있었다. 또한 방사 형태로 $10{\mu}m$ 두께의 열전 재료와 전극들이 두께가 각기 다른 기판 위에 형성된 수평형 냉각 모듈을 설계하여 $10{\mu}m$ 두께의 $SiO_2$ 멤브레인 위에 열전재료가 형성된 열전 모듈에서 22 K의 온도 차를 해석결과로부터 알 수 있었다. 이와 같은 결과로부터 열전 재료의 특성과 모듈의 열 전기적 저항은 필연적으로 짧은 열전 재료의 길이와 두께를 갖는 박막형 열전 모듈을 높은 효율의 모듈로 설계하기 위해 반드시 고려되어 되어야 할 요소임을 확인 할 수 있다.

마이크로 채널 디자인에 따른 온 칩 액체 냉각 연구 (Study of On-chip Liquid Cooling in Relation to Micro-channel Design)

  • 원용현;김성동;김사라은경
    • 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.

Development of Micro Tensile Test of CVD-SiC coating Layer for TRISO Nuclear Fuel Particles at elevated temperature

  • Lee, Hyun-Min;Park, Kwi-Il;Kim, Do-Kyung
    • 한국재료학회:학술대회논문집
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    • 한국재료학회 2012년도 춘계학술발표대회
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    • pp.95.1-95.1
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    • 2012
  • Very High Temperature gas cooler Reactor (VHTR) has been considered as one of the most promising nuclear reactor because of many advantages including high inherent safety to avoid environmental pollution, high thermal efficiency and the role of secondary energy source. The TRISO coated fuel particles used in VHTR are composed of 4 layers as OPyC, SiC, IPyC and buffer PyC. The significance of CVD-SiC coatings used in tri-isotropic(TRISO) nuclear coated fuel particles is to maintain the strength of the whole particle. Various methods have been proposed to evaluate the mechanical properties of CVD-SiC film at room temperature. However, few works have been attempted to characterize properties of CVD-SiC film at high temperature. In this study, micro tensile system was newly developed for mechanical characterization of SiC thin film at elevated temperature. Two kinds of CVD-SiC films were prepared for micro tensile test. SiC-A had [111]-preferred orientation, while SiC-B had [220]-preferred orientation. The free silicon was co-deposited in SiC-B coating layer. The fracture strength of two different CVD-SiC films was characterized up to $1000^{\circ}C$.The strength of SiC-B film decreased with temperature. This result can be explained by free silicon, observed in SiC-B along the columnar boundaries by TEM. The presence of free silicon causes strength degradation. Also, larger Weibull-modulus was measured. The new method can be used for thin film material at high temperature.

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이산화탄소 냉매 시스템용 내부 열교환기의 냉방성능에 관한 실험적 연구 (Experimental Study on Cooling Performance of Internal Heat Exchanger for CO2 Refrigerant System)

  • 김대훈;권영철
    • 한국산학기술학회논문지
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    • 제9권3호
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    • pp.587-592
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    • 2008
  • 이산화탄소 냉매 시스템용 내부 열교환기의 성능을 조사하기 위하여 4종류의 내부 열교환기를 사용하여 냉방운전조건에서 실험을 수행하였다. 내부 열교환기의 길이, 관 개수, 운전조건, 형상 변화에 대한 영향이 연구되었다. 내부 열교환기 길이가 증가할수록 능력과 효율은 향상되었다. 압력강하는 고압측보다 저압측에서 더 크게 나타났다. 가스쿨러의 온도가 높아질수록 능력과 효율은 선형적으로 증가하였으며, 증발기의 운전조건은 과열도보다는 이상영역을 설정하면 효율증대 효과 측면에서 유리하였다. 마이크로 채널의 경우가 튜브보다 능력과 효율이 크게 우수하였지만 압력강하 측면에서는 크게 불리하였다.