• 제목/요약/키워드: 극저온유체

검색결과 4건 처리시간 0.022초

액체질소에 대한 증발 열전달 촉진 및 압력강하 성능 (Performance of Evaporation Heat Transfer Enhancement and Pressure Drop for Liquid Nitrogen)

  • 남상철;이상천;박병덕
    • 대한기계학회논문집B
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    • 제24권3호
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    • pp.363-372
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    • 2000
  • An experiment was carried out to evaluate the heat transfer enhancement and the pressure drop characteristics for liquid nitrogen using wire-coil-insert technique under horizontal two-phase conditions. The tube inner diameters were 8 mm and 15 mm, respectively and the tube length was 4.7 m. The helix angle of the wire coil insert was $50^{\circ}$ and its length was 4.7 m. Heat transfer coefficients for both the plain and the enhanced test tubes were calculated from the measurements of temperatures, flow rates and pressure drops. A correlation in a power-law relationship of the Nusselt number, Reynolds number and Prandtl number for the heat transfer was proposed which can be available for design of cryogenic heat exchangers. The correlation showed that heat transfer coefficients for the wire-coil inserts were much higher than those for plain tubes, increased by more than $1.8{\sim}2.0$ times depending upon the range of the equivalent Reynolds number. The correlation was compared with other various correlations in the turbulent flow conditions.

평활관 및 열전달촉진관에서 액체질소의 관내 증발열전달 특성에 대한 연구 (Evaporation Heat Transfer Characteristics of Liquid Nitrogen in Horizontal Plain Tubes with Wire Coil Inserts)

  • 황지상;정진택;윤린;김용찬;문영준;김동혁
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.1359-1364
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    • 2004
  • An experiment was performed to study the evaporation heat transfer and the pressure drop characteristics of liquid nitrogen in a horizontal stainless steel tube with wire coil inserts. The inner diameter of test tube is 4.3mm and the length is 1.5m. Four wire coils having different pitch and thickness were inserted into the plain test tube. The wire coil length is 1.5m and the diameter is 3.65mm with thickness of 0.5mm and 0.9mm. Experiments were conducted at saturation temperature of $-191^{\circ}C$ mass flux from 200 to 370 $kg/m^{2}s$ and heat flux of 62 $kW/m^{2}$. Direct heating method was used to apply heat to the test section. Boiling heat transfer coefficients of both the plain and the enhanced tubes were calculated. Pressure drops between inlet and outlet side of test section were also measured, and they are used to estimate EPR(Enhancement Performance Ratio).

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다공성 매질에서 액화질소의 거동에 대한 연구 (STUDY ON BEHAVIOR OF LIQUID NITROGEN IN POROUS MEDIA)

  • 최성웅;이우일
    • 한국전산유체공학회지
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    • 제18권2호
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    • pp.17-25
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    • 2013
  • The process of flow through porous media is of interest a wide range of engineering fields and areas, and the importance of fluid flow with a change in phase arises from the fact that many industrial processes rely on these phenomena for materials process, energy transfer. Especially, the flow phenomena of cryogenic liquid subjected to evaporation is of interest to investigate how the cryogenic liquid behaves in the porous structure. In this study, thermo physical properties, morphological properties of the glass wool with different bulk densities in terms of its temperature-dependence and permeability behaviors under different applying pressure are discussed. Using the experimentally determined properties, characteristics of two main experimental results are investigated. In addition, simulation results are used to realize the cryogenic liquid's flow in porous media, and are compared with experimental results. By using the experimentally determined properties, more reasonable results can be suggested in dealing with porous media flow.

액체로켓 LOX 공급계의 저압 배관시스템 개발 (Development of the Low Pressure Piping System for the Liquid Rocket LOX Feed System)

  • 전상인;정진택;김우겸;박준성;권오성;김영목
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.322-325
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    • 2007
  • 본 논문은 터보펌프를 사용하는 액체로켓의 저압 LOX 공급계의 개발 프로세스를 제공한다. 대한항공은 한국항공우주연구원과 협력하여 터보펌프 공급을 위한 LOX 공급계 개발을 수행하였다. LOX 공급계는 극저온의 온도와 무게절감을 위한 얇은 배관두께가 특징이다. 본 프로젝트의 시스템은 주 배관과 LOX 온도 제어를 위한 재순환 배관으로 구성되어 있다. 각 배관시스템은 벨로우즈, 필터, 오리피스, 밸브류, 플랜지와 서포트로 구성되어 있다. 이 논문에서는 시스템 설계 및 제작, 구조 및 열 해석, 단품 시험에 대하여 설명하였다. 최종적으로, 이 시스템은 한국항공우주연구원의 PTF 시험설비에 조립되어 요구 성능을 달성하였다.

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