• Title/Summary/Keyword: 응축온도

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CFD Analysis to Suppress Condensate Water Generated in Gas Sampling System of HANARO (하나로 기체시료채취계통에서 생성된 응축수 억제를 위한 CFD 해석)

  • Cho, SungHwan;Lee, JongHyeon;Kim, DaeYoung
    • Journal of Nuclear Fuel Cycle and Waste Technology(JNFCWT)
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    • v.18 no.2_spc
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    • pp.327-336
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    • 2020
  • The high-flux advanced neutron application reactor (HANARO) is a research reactor with thermal power of 30 MW applied in various research and development using neutrons generated from uranium fission chain reaction. A degasifier tank is installed in the ancillary facility of HANARO. This facility generates gas pollutants produced owing to internal environmental factors. The degasifier tank is designed to maintain the gas contaminants below acceptable levels and is monitored using an analyzer in the gas sampling panel. If condensate water is generated and flows into the analyzer of the gas sampling panel, corrosion occurs inside the analyzer's measurement chamber, which causes failure. Condensate water is generated because of the temperature difference between the degasifier tank and analyzer when the gas flows into the analyzer. A heating system is installed between the degasifier tank and gas sampling panel to suppress condensate water generation and effectively remove the condensate water inside the system. In this study, we investigated the efficiency of the heating system. In addition, the variations in the pipe temperature and the amount of average condensate water were modeled using a wall condensation model based on the changes in the fluid inlet temperature, outside air temperature, and heating cable-setting temperature.

Prediction on Maximum Performance of Cascade Refrigeration System Using R717 and R744 (R718-R744용 캐스케이드 냉동시스템의 최대 성능 예측)

  • Roh, Geun-Sang;Son, Chang-Hyo
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.10 no.10
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    • pp.2565-2571
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    • 2009
  • In this paper, cycle performance analysis of cascade refrigeration system using $NH_3-CO_2$(R717-R744) is presented to offer the basic design data for the operating parameters of the system. The operating parameters considered in this study include subcooling and superheating degree and condensing and evaporating temperature in the ammonia(R717) high temperature cycle and the carbon dioxide low temperature cycle. The COP of cascade refrigeration system increases with the increasing superheating degree, but decreases with the increasing subcooling degree. The COP of cascade refrigeration system increases with the increasing condensing temperature, but decreases with the increasing evaporating temperature. Therefore, superheating and subcoolng degree, evaporating and condensing temperature of cascade refrigeration system using $NH_3-CO_2$ have an effect on the COP of this system. A multilinear regression analysis was employed in terms of subcooling, superheating, evaporating, condensing, and cascade heat exchanger temperature difference in order to develop mathematical expressions for maximum COP and an optimum evaporating temperature.

Themodynamic Characteristics of a Two-Stage Binary Absorption Cycle (2단(段) 2원(元) 흡수(吸收)사이클의 특성(特性)에 관(關)한 연구(硏究))

  • Lee, Y.H.;Rie, D.H.;Kashiwagi, T.;Seo, J.Y.
    • Solar Energy
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    • v.15 no.1
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    • pp.29-38
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    • 1995
  • This paper concerns the study of a two-stage binary absorption cycle employing the refrigerant/absorbent combinations of $LiBr/H_2O$ and $NH_3/H_2O$. This cycle consists of coupling two single-effect absorption cycles so that the first stage absorber and condenser produces heating water to evaporate refrigerant in the evaporator of the second stage. The effect of operating variables such as evaporator temperature, condenser and absorber temperature, and generator temperature on the coefficient of performance and temperature lift have been studied for two-stage binary absorption heat pump systems. It is found that this cycle has a large temperature lift at $105^{\circ}C$ of optimum generator temperature to obtain $50^{\circ}C$ of condenser temperature.

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수직한 벽면에서 혼합증기(수증기/공기)의 막응축 열전달

  • 박수기;김무환;유건중
    • Proceedings of the Korean Nuclear Society Conference
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    • 1996.11a
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    • pp.217-223
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    • 1996
  • 혼합증기(수증기/공기)의 막응축 열전달 계수를 수직한 벽면에서 측정하고 상관식을 개발하였다. 열전달 상관식은 액막측과 증기측으로 구분하여 만들었고, 액막측 전열계수의 상관식은 액막의 Reynolds수와 Prandtl수의 함수로 나타냈으며, 증기측 전열계수의 상관식은 증기의 Reynolds수, Prandtl수, Schmidt수 및 공기의 질량분율, 액막 Reynolds수의 함수로 제안하였다. 응축 액막의 두께와 확산층의 순간온도 측정결과로부터 액막의 파형 계면이 확산층에서의 열 및 물질전달에 큰 영향을 끼치고 있음을 확인하였고, 증기측 전열계수의 상관식에 포함된 액막 Reynolds수가 파형 계면의 영향을 반영하고 있다.

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화학기상응축공정(CVC)을 이용하여 제조한 Fe/N 나노분말의 TEM 미세조직

  • 김택수;이병택;최철진
    • Proceedings of the Korean Powder Metallurgy Institute Conference
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    • 2003.04a
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    • pp.38-38
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    • 2003
  • 나노입자는 일반적인 크기의 입자에서 볼 수 없는 특성을 나타내므로 촉매, 광학, 자성기록매체, 자성유체로의 자유로운 응용이 기대되어지고 있으며, 다양한 조성의 나노재료 및 제조공정에 관한 연구개발이 활발히 이루어지고 있는 추세이다. 이중 나노재료제조공정은 기상응축, 열분해법, 플라즈마법 및 볼밀링법 등이 상용화되어 있으며, 본 연구에서는 화학적균일성과 다양한 조성으로의 응용이 용이한 화학기상응축공정을 이용하여 Fe/N나노분말을 제조하였다. 제조된 Fe/N 나노 분말의 분해온도 ($50^{\circ}C$~$1100^{\circ}C$)에 따른 미세조직의 변화를 고분해능전자현미경(HRTEM)을 이용하여 관찰하였다. 그 결과 분해온도에 따라 Amorphous +$\alpha$-Fe nanocrystallites $\rightarrow$ Amorphous +$\alpha$-Fe nanocrystallites + $Fe_3N$ nanocrystallites $\rightarrow$ $Fe_3N$ nanocrystallites로 상태변이가 일어났으며, $1100^{\circ}C$의 경우 약 5-6nm크기의 산화막이 형성되어 있으며, 이는 코어두RP의 약 28%를 차지하고 있다.

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Flow Characteristics of R600a in an Adiabatic Capillary Tube (단열 모세관내 R600a의 유동 특성)

  • Ku, Hak-Geun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.11 no.2
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    • pp.449-454
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    • 2010
  • In this paper, flow characteristics of R600a in an adiabatic capillary tube were investigated employing the homogeneous flow model. The model is based on fundamental equations of mass, energy and momentum which are solved simultaneously. Two friction factors(Churchill) and viscosity(McAdams) are comparatively used to investigate the flow characteristics. Thermodynamic and transport properties of R600a are calculated employing EES property code. Flow characteristics analysis of R600a in an adiabatic capillary tube is presented to offer the basic design data for the operating parameters. The operating parameters considered in this study include condensation temperature, evaporation temperature, subcooling degree and inner diameter tube of the adiabatic capillary tube. The main results were summarized as follows: condensation and evaporation temperature, inlet subcooling degree and inner diameter tube of an adiabatic capillary tube using R600a have an effect on length of an adiabatic capillary tube. The length of an adiabatic capillary tube using R600a is expressed to the correlation shown in Eq. (15).

Analytical Modeling of a Loop Heat Pipe with a Flat Evaporator by Applying Thin-Film Theory (평판형 증발부를 갖는 루프히트파이프에 대해 박막이론을 적용한 해석적 모델링)

  • Jung, Eui-Guk;Boo, Joon-Hong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.12
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    • pp.1079-1085
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    • 2010
  • A steady-state analytical model was presented for a loop heat pipe (LHP) with an evaporator that has a flat geometry. On the basis of a series of reviews of the relevant literature, a sequence of calculations was proposed to predict the temperatures and pressures at each important part of the LHP: the evaporator, liquid reservoir (compensation chamber), liquid line, vapor line, and condenser. The analysis of the evaporator, which is the only part in the LHP that has a capillary structure, was emphasized. Thin-film theory is applied to account for the pressure and temperature in the region adjacent to the liquid-vapor interface in the evaporator. The present study introduced a unique method to estimate the liquid temperature at the interface. Relative freedom was assumed in the configuration of a condenser with a simplified liquid-vapor interface. Our steady-state model was validated by experimental results available in the literature. The relative error was within 3% on the absolute temperature scale, and reasonable agreement was obtained.

Performance Analysis of 2-Stage Compression and 1-Stage Expansion Refrigeration System using Alternative Natural Refrigerants (암모니아 대체 자연냉매를 이용하는 2단압축 1단팽창 냉동시스템의 성능예측)

  • Roh, Geon-Sang
    • Journal of the Korean Institute of Gas
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    • v.16 no.3
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    • pp.42-47
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    • 2012
  • In this paper, alternative natural refrigerant R290(Propane), R600(Butane), R717(Ammonia), R1270(Propylene) for freon refrigerant R22 were used working fluids for 2-stage compression and 1-stage expansion refrigeration system. The operating parameters considered in this study included evaporation temperature, condensation temperature, subcooling degree, superheating degree, mass flow rate ratio of inter-cooler. The main results were summarized as follows : The COP of 2-stage compression and 1-stage expansion refrigeration system increases with the increasing subcooling degree and mass flow rate ration of inter-cooler, but decreases with the increasing evaporating temperature, condensing temperature and superheating degree. Therefore, subcooling degree, mass flow rate ratio of inter-cooler of 2-stage compression and 1-stage expansion refrigeration system using natural refrigerants have an effect on COP of this system. The COP of natural refrigerants was higher than the COP of freon R22 in this study, so points to be considered are the security, the attached facilities for natural refrigerants than COP.

Condensation Heat Transfer Characteristics of Hydrocarbon Refrigerants in Horizontal Tubes of 7.73 mm and 5.80 mm (7.73 mm와 5.80 mm 수평관내 탄화수소 냉매의 응축 열전달 특성)

  • Son, Chang-Hyo
    • Journal of Hydrogen and New Energy
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    • v.19 no.4
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    • pp.331-339
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    • 2008
  • 본 논문은 내경 7.73 mm와 5.80mm의 수평관내 프레온계 냉매 R-22와 탄화수소계 냉매 R-290과 600a의 응축 열전달 계수의 실험적 결과를 나타내었다. 실험장치는 압축기, 응축기, 팽창밸브, 증발기 등으로 구성된다. 응축 실험은 질량유속 $35.5{\sim}210.4\;kg/m^2s$이고, 응축온도 40$^{\circ}C$인 조건에서 수행하였다. 주요 결과를 요약하면 다음과 같다. 탄화수소계 냉매 R-290과 R-600a의 평균 열전달 계수는 프레온계 냉매 R-22보다 높게 나타났으며, R-600a의 평균 열전달 계수가 모든 관경에 대해 가장 높게 나타났다. 실험결과와 종래의 상관식을 비교한 결과, 모든 관경과 냉매에 대해 Haraguchi 등의 상관식이 가장 좋은 일치를 보였다. 그 중에서 Cavallini-Zecchin의 상관식은 7.73 mm 관경의 실험데이터와, Dobson 등의 상관식은 내경 5.80 mm 관경의 데이터와 좋은 일치를 보였다.

Research on Gas-phase Condensation of Cryogenic Propellant in Pipelines of a Liquid Rocket Engine (로켓엔진의 극저온 연료 공급관내에서 기체상 응축에 관한 연구)

  • Bershadskiy, Vitaly A.;Phyrsov, Valery P.;Cho, Kie-Joo;Oh, Seung-Hyub;Kim, Cheul-Woong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.3
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    • pp.248-252
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    • 2007
  • This article is related to the possibility for continuous operation of a liquid rocket engine when a portion of cryogenic propellant in the pipeline is vaporized. As a result of experimental studies imitating the formation of vapors in the flow, we confirmed the possibility of full gas-phase condensation in case temperature of cryogenic liquid is lower than it's saturation temperature in the pipeline. Empirical equation allowing to calculate a nonequilibrium condensation region in the steady flow of cryogenic liquid was obtained as a non-dimensional form and the fields of practical application were suggested.