• 제목/요약/키워드: Inlet-air temperature

검색결과 673건 처리시간 0.023초

반응표면분석에 의한 분유의 유동층 과립공정 최적화 (Optimization of Fluidized Bed Granulating Conditions for Powdered Milk by Response Surface Methodology)

  • 강현아;신명곤
    • 한국식품영양과학회지
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    • 제33권1호
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    • pp.225-228
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    • 2004
  • 반응표면분석법(RSM)을 활용하여 유동층과립기의 흡입공기온도, 물의 투입비율, 분무압력 등이 분유의 과립화에 미치는 영향을 분석하였다. 분유의 과립화 수율은 물의 투입 비율에 많은 영향을 받고 있음을 알 수 있었으며, 겉보기밀도 및 다짐 밀도는 분무압력에 크게 영향을 받고 있음을 보여주었다. 분유의 유동층 과립화의 최적조건은 흡입공기온도6$0^{\circ}C$, 물의 투입비율 16 mL/min, 그리고 분무압력 2.1 bar이었으며, 이때 과립화 수율은 94.0%, 겉보기밀도는 0.350 g/㎤, 그리고 다짐밀도는 0.446 g/㎤로 각각 예측되었다.

Thermal and Flow Analysis in a Proton Exchange Membrane Fuel Cell

  • Jung, Hye-Mi;Koo, Ja-Ye
    • Journal of Mechanical Science and Technology
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    • 제17권9호
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    • pp.1358-1370
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    • 2003
  • The effects of anode, cathode, and cooling channels for a Proton Exchange Membrane Fuel Cell (PEMFC) on flow fields have been investigated numerically. Continuous open-faced fluid flow channels formed in the surface of the bipolar plates traverse the central area of the plate surface in a plurality of passes such as a serpentine manner. The pressure distributions and velocity profiles of the hydrogen, air and water channels on bipolar plates of the PEMFC are analyzed using a two-dimensional simulation. The conservation equations of mass, momentum, and energy in the three-dimensional flow solver are modified to include electro-chemical characteristics of the fuel cell. In our three-dimensional numerical simulations, the operation of electro-chemical in Membrane Electrolyte Assembly (MEA) is assumed to be steady-state, involving multi-species. Supplied gases are consumed by chemical reaction. The distributions of oxygen and hydrogen concentration with constant humidity are calculated. The concentration of hydrogen is the highest at the center region of the active area, while the concentration of oxygen is the highest at the inlet region. The flow and thermal profiles are evaluated to determine the flow patterns of gas supplied and cooling plates for an optimal fuel cell stack design.

모형 가스터빈 연소기내 연소불안정성에 대한 실험적 연구 (An Experimental Study on Combustion Instability Mechanism in a Dump Gas Turbine Combustor)

  • 이연주;이종호;전충환;장영준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.853-858
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    • 2001
  • The knowledge of flame structure is essential for control of combustion instability phenomena. Some results of an experimental study on mechanism of naturally occurring combustion oscillations with a single dominant frequency are presented. Tests were conducted in a laboratory-scale dump combustor at atmospheric pressure. Sound level meter was used to track the pressure wave inside the combustor. The observed instability was a longitudinal mode with a frequency of $\sim341.8Hz$. Instability map was obtained at the condition of inlet temperature of $360^{\circ}C$, mean velocities of $8.5\sim10.8m/s$ and well premixed mixture. It showed that combustion instability was susceptible to occur in the lean conditions. In this study, unstable flame was observed from stoichiometric to 0.7 in overall equivalence ratio. At selected unstable conditions, phase-resolved OH chemiluminescence images were captured to investigate flame structure with various mean velocities. As mean velocity is increased, the flame grows and global heat release was changed. Due to these effects, combustion instability can be maintained at more lean air-fuel ratio. Also, these results give an insight to the controlling mechanism for an increasing heat release at maximum pressure.

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천연냉매인 이산화탄소의 세관 유동시 발생하는 증발 유동 현상에 대한 수치해석 연구 (Numerical Study on the Evaporation Flow Phenomena of Natural Refrigerant CO2 through Small Diameter Tubes)

  • 최인수;박병덕
    • 한국산업융합학회 논문집
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    • 제10권2호
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    • pp.89-96
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    • 2007
  • For the environment protection, carbon dioxide as a natural refrigerant has been studied to use in an automotive air conditioning system. Hence, a numerical model has been developed to describe the evaporation phenomena of carbon dioxide flowing through very small diameter tubes. The two dimensional low-Reynolds $k-{\varepsilon}$ model was used to predict the flow phenomena of carbon dioxide in the two phase during its evaporation. Furthermore, the results obtained from the model were compared with the experiments for the validation. The heat transfer coefficient is lower, as the tube inner diameter becomes smaller. However, the amount of heat absorbed by a unit mass of carbon dioxide is greater due to more surface area. Therefore, the small diameter tube has advantage in terms of compact design of evaporator. When the inlet condition of pressure and temperature is low, the heat transfer coefficient is slightly high at the same size of tube because of the thermal properties of carbon dioxide.

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200kW급 마이크로 가스터빈 시스템의 설계 변수 민감도 해석 (Design Parameter Sensitivity Analysis of a 200kW Class Micro Gas Turbine System)

  • 신현동;강도원;김동섭;최문경;박필제
    • 한국유체기계학회 논문집
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    • 제15권6호
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    • pp.39-45
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    • 2012
  • This paper describes the outcome of the design of a 200 kW class micro gas turbine and the sensitivity of its performance (efficiency and power) to the variations in major design parameters. The reference design parameters were set up based on the best available component technologies. The resulting net electricity generation efficiency of the micro gas turbine package was found to be competitive to those of other systems in the market. The sensitivities of power and efficiency to the variations in compressor and turbine efficiencies, pressure ratio, turbine inlet temperature, recuperator effectiveness, secondary air ratio, pressure loss ratios of both the cold and hot sides of the recuperator were estimated. Based on the sensitivity data, a simplified method to predict the variation in system performance responding to the combinations of small changes in all design parameters were set up and validated.

가스터빈 결빙시험용 결빙모사장치 개발 (Development of Icing Simulation Device for Gas Turbine Icing Test)

  • 이경재;양수석;이대성
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.358-361
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    • 2007
  • 대부분의 항공기는 성층권에서 순항을 하며, 이때의 온도는 지상의 그것보다 상당히 낮아 항공기 표면에 결빙이 발생할 수 있다. 기체 날개에 결빙이 발생하면 날개의 형상이 변화되어 비행특성을 저하시키며, 흡입구에서 발생한 결빙은 압축기 블레이드의 손상의 위험을 높이고 엔진의 성능에도 큰 영향을 미치게 된다. 본 논문에서는 결빙에 의한 여러 가지 상황 중 결빙으로 인한 엔진 성능 변화를 분석하기 위하여 결빙모사장치의 개발을 수행하였다. 결빙모사장치와 액체공기시스템을 이용하여 결빙모사 시험을 수행하였으며, 시험수행을 통하여 결빙이 모사가 가능함을 확인하였다.

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지열발전을 위한 칼리나 사이클의 시뮬레이션 (Simulation of the Kalina cycle for a Geothermal Power Generation)

  • 백영진;김민성;장기창;이영수;박성룡;라호상
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.782-787
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    • 2008
  • The Kalina cycle simulation study was carried out for a preliminary design of a geothermal power generation system. The Kalina cycle system can be used for the utilization of a low-temperature heat sources such as geothermal and industrial waste heat that are not hot enough to produce steam. The sea/river water can be considered as a cooling media. A steady-state simulation model was developed to analyze and optimize its performance. The model contains a turbine, a pump, an expansion valve and heat exchangers. The turbine and pump were modelled by an isentropic efficiency, while a condenser, an evaporator and a regenerative heat exchanger were modeled by UA-LMTD method with a counter-flow assumption. The simulation results show that the power generation efficiency over 10% is expected when a heat source and sink inlet temperatures are $100^{\circ}C$ and $10^{\circ}C$ respectively.

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유체의 물성치변화를 고려한 수직원형관내 고온기체유동에 관한 직접수치모사 (Direct Numerical Simulation of Strongly-Heated Internal Gas Flows with Large Variations of Fluid Properties)

  • 배중헌;유정열;최해천;유종우
    • 대한기계학회논문집B
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    • 제28권11호
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    • pp.1289-1301
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    • 2004
  • Direct numerical simulation (DNS) of strongly-heated air flows moving upward in a vertical tube has been conducted to investigate the effect of gas property variations on turbulence modification. Three heating conditions(q$_1$$^{+}$=0.0045, 0.0035 and 0.0018) are selected to reflect the experiment of Shehata and McEligot (1998) at the inlet bulk Reynolds numbers of 4300 and 6000. At these conditions, the flow inside the heated tube remains turbululent or undergoes a transition to subturbulent or laminarizing flow. Consequently, a significant impairment of heat transfer occurs due to the reduction of flow turbulence. The predictions of integral parameters and mean profiles such as velocity and temperature distributions are in excellent agreement with the experiment. The computed turbulence data indicate that a reduction of flow turbulence occurs mainly due to strong flow acceleration effects for strongly-heated internal gas flows. Thus, buoyancy influences are secondary but not negligible especially for turbulent flow at low heating condition. Digital flow visualization also shows that vortical structures rapidly decay as the heating increases.s.

이산화탄소의 마이크로 핀관 내 상향유동 증발열전달 특성에 관한 연구 (An experimental study on heat transfer characteristics in a vertical micro-fin tube during evaporation process of carbon dioxide flowing upward)

  • 김용진;조진민;김민수
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2007년도 동계학술발표대회 논문집
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    • pp.247-251
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    • 2007
  • Because of the ozone layer depletion and global warming, new alternative refrigerants are being developed. In this study, evaporation heat transfer characteristics of carbon dioxide flowing upward in a vertical micro-fin tube have been investigated by experiment. Before a test section, a pre-heater is installed to adjust the inlet quality of the refrigerant to a desired value. The micro-fin tube with outer diameter of 5 mm and length of 1.44 m was selected as the test section. The test was conducted at mass fluxes of 318 to $530\;kg/m^2s$, saturation temperature of -5 to $5^{\circ}C$, and heat fluxes of 15 to $30\;kW/m^2$. As the vapor quality increases, the heat transfer coefficients of carbon dioxide are increased, and the heat transfer coefficients increase when the heat fluxes and saturation temperatures increase, and there was not much of influence of mass flux on the heat transfer coefficients.

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Effect of Different Carrier Agents on Physicochemical Properties of Spray-dried Pineapple (Ananas comosus Merr.) Powder

  • Quoc, Le Pham Tan
    • 대한화학회지
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    • 제64권5호
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    • pp.259-266
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    • 2020
  • The main purpose of this study is to examine the different physicochemical properties of spray-dried products. The carrier agents and powders after the spray-drying process were analyzed for encapsulation yield, moisture content, color parameters, total polyphenol content (TPC), antioxidant capacity (AC), bulk density, flowability, wettability, hygroscopicity, water solubility index (WSI), particle size and microstructure. The spray-drying process was carried out with different carrier agents including maltodextrin (MD) and the combination of maltodextrin and gum arabic (MD-GA) with MA/GA ratio of 70/30, dried at the inlet/outlet air temperature of 160 ℃/70 ℃, 4 bar, airflow rate of 70 ㎥·h-1 and feed flow rate of 750 mL·h-1. The results showed that the different carrier agents have significant influences on the physicochemical properties of the powder produced by the spray-drying method. In there, while the values of recovery efficiency and flowability of spray-dried products from MD are higher than those of spray-dried products from MD-GA combination, the opposite is true for the values of TPC, AC, bulk density and wettability, whereas hygroscopicity and WSI values are equally represented in both products.