• 제목/요약/키워드: Cold Exit

검색결과 74건 처리시간 0.025초

간헐식 폭기형 수체순환장치 모델링 (A Modeling of Intermittent-Hydraulic-Gun-Aerator)

  • 송무석;서동일
    • 대한조선학회논문집
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    • 제42권3호
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    • pp.183-189
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    • 2005
  • A modeling of a hydraulic-gun-aerator is proposed to set up a design procedure for such devices. The aerators are used to destroy any thermal stratification that are responsible for the degradation of water qualify of lakes. The aerator produces ascending flow by using air bubbies released instantly near the bottom of the lake into a cylindrical pipe installed vertically. Differently form the diffuser-aerators, they can pull up the cold, oxygen depleted water directly to the region of the free surface, and they are believed to work effectively especially for relatively deeper lakes. Their design procedure has not been established yet though, and we propose a model focusing on the exit flow velocity at the top of the aerator through the examination of presently operating devices.

충돌형 분사기 형태의 액체로켓엔진용 가스발생기 연소성능시험 (Combustion Performance Tests of Fuel-Rich Gas Generator for Liquid Rocket Engine Using an Impinging Injector)

  • 한영민;김승한;문일윤;김홍집;김종규;설우석;이수용;권순탁;이창진
    • 한국추진공학회지
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    • 제8권2호
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    • pp.10-17
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    • 2004
  • 본 논문에서는 액체로켓엔진용 160 kW급 터보펌프의 터빈을 구동하고, 액체산소와 케로신을 추진제로 사용하는 연료 과잉 가스발생기의 설계점 연소성능시험 결과에 대해 논의하였다. 충돌형 F-O-F 분사기로 구성된 헤드부, 물냉각 채널 연소실, torch igniter, turbulence ring 그리고 측정 링을 갖는 가스발생기에 대해 기술하였고, 설계점에서의 연소시험 및 turbulence ring 장착여부. 연소실 길이 변화에 따른 연소시험의 결과들에 대해 기술하였다. 연소시험 결과 가스발생기는 설계점에서 안정된 작동성을 보여주었고. 연소압력 및 온도 등의 성능은 예측치에 근접하는 결과였다. Turbulence ring은 출구에서의 가스온도를 균일하게 분포시켜 효과적인 혼합 장치임을 보여 주었고, 4∼6msec 정도에서의 연소가스 잔류시간은 연소효율에 큰 영향을 주지 않았다. 가스발생기 출구에서의 온도는 공급되는 추진제의 O/F ratio에 따라 매우 민감하게 변화하였다.

축류형터빈 전효율에 파급된 불확도에 관한 실험적연구 (An Experimental Study on the Propagated Uncertainties on the Total-to-total Efficiency of an Axial Turbine)

  • 조수용;김은종
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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    • pp.123-126
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    • 2003
  • 실험에서 측정변수에 발생되는 불확도가 터빈 전효율의 불확도에 미치는 영향을 실험을 통하여 분석하였다. 단단 축류형 3차원 터빈이 실험에 사용되었으며 평균반경에서 반동도가 0.373이며 상온 저압 상태에서 실험이 수행되었다. 입구/출구전압력에 의하여 발생되는 불확도는 터빈 전효율의 불확도로 전파되는 영향이 상당히 크게 나타나므로 상온저압시험에서는 높은 정밀도를 갖는 압력계가 필요하게 된다. 측정변수의 불확도가 전효율의 불확도에 차지하는 영향은 토오크에 의하여 발생되는 불확도가 가장 크게 나타났으며 회전수에 의한 불확도가 가장 적었다. 토오크의 불확도 영향은 회전수의 증가에 따라 증가하는 경향이 있다. 전압력의 경우는 출구측에서의 불확도가 입구측에 비하여 영향력이 크게 나타났다.

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폐쇄형 해양온도차발전 사이클에 관한 연구 (A Study of Closed OTEC Power Plants)

  • 신상호;정동수;김종보;서태범;천원기;오정무
    • 태양에너지
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    • 제17권4호
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    • pp.23-33
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    • 1997
  • 본 연구에서는 Rankine 사이클을 이용한 해양 온도차 발전 시스템을 컴퓨터로 모사했고 작동유체를 변화시켜 가면서 그 성능을 비교하였다. 증발기와 응축기는 UA(총괄열전달계수$\times$전열면적)와 LMTD(대수평균온도차) 방법으로 모사하였으며 터빈과 펌프는 등엔트로피 효율로 모사하였다. 작동유체로는 R22, R290, R1270, R134a, R125, R143a, R32, R410A 그리고 암모니아 등을 사용하였다. 모사 결과 OTEC 발전 시스템의 효율은 작동유체에 상관없이 거의 일정한 것으로 드러났다. 한편 증발기 출구에서의 과열도와 응축기 출구에서의 과냉도는 시스템의 성능에 거의 영향을 미치지 않는 것으로 나타났지만 터빈의 효율과 열교환기의 크기는 시스템 성능에 큰 영향을 미치는 것으로 나타났다. 마지막으로 따뜻한 표층수와 차가운 심해수 사이의 온도차가 $20^{\circ}C$이상일 때 실제로 전기를 생산할 수 있다는 사실을 확인했다.

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A FLOW AND PRESSURE DISTRIBUTION OF APR+ REACTOR UNDER THE 4-PUMP RUNNING CONDITIONS WITH A BALANCED FLOW RATE

  • Euh, D.J.;Kim, K.H.;Youn, Y.J.;Bae, J.H.;Chu, I.C.;Kim, J.T.;Kang, H.S.;Choi, H.S.;Lee, S.T.;Kwon, T.S.
    • Nuclear Engineering and Technology
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    • 제44권7호
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    • pp.735-744
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    • 2012
  • In order to quantify the flow distribution characteristics of APR+ reactor, a test was performed on a test facility, ACOP ($\underline{A}$PR+ $\underline{C}$ore Flow & $\underline{P}$ressure Test Facility), having a length scale of 1/5 referring to the prototype plant. The major parameters are core inlet flow and outlet pressure distribution and sectional pressure drops along the major flow path inside reactor vessel. To preserve the flow characteristics of prototype plant, the test facility was designed based on a preservation of major flow path geometry. An Euler number is considered as primary dimensionless parameter, which is conserved with a 1/40.9 of Reynolds number scaling ratio. ACOP simplifies each fuel assembly into a hydraulic simulator having the same axial flow resistance and lateral cross flow characteristics. In order to supply boundary condition to estimate thermal margins of the reactor, the distribution of inlet core flow and core exit pressure were measured in each of 257 fuel assembly simulators. In total, 584 points of static pressure and differential pressures were measured with a limited number of differential pressure transmitters by developing a sequential operation system of valves. In the current study, reactor flow characteristics under the balanced four-cold leg flow conditions at each of the cold legs were quantified, which is a part of the test matrix composing the APR+ flow distribution test program. The final identification of the reactor flow distribution was obtained by ensemble averaging 15 independent test data. The details of the design of the test facility, experiment, and data analysis are included in the current paper.

초음속 노즐 출구에 대칭적으로 설치한 추력방향제어장치인 램프 탭의 연구 (An study on the ramp tabs for thurst vector control symmetrically installed at the supersonic nozzle exit)

  • 김경련;고재명;박종호
    • 한국유체기계학회 논문집
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    • 제10권6호
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    • pp.32-37
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    • 2007
  • Aerodynamic forces and moments have been used to control rocket propelled vehicles. If control is required at very low speed, Those systems only provide a limited capability because aerodynamic control force is proportional to the air density and low dynamic pressure. But thrust vector control(TVC) can overcome the disadvantages. TVC is the method which generates the side force and roll moment by controlling exhausted gas directly in a rocket nozzle. TVC is classified by mechanical and fluid dynamic methods. Mechanical methods can change the flow direction by several objects installed in a rocket nozzle exhaust such as tapered ramp tabs and jet vane. Fluid dynamic methods control the flight direction with the injection of secondary gaseous flows into the rocket nozzle. The tapered ramp tabs of mechanical methods are used in this paper. They installed at the rear in the rocket nozzle could be freely moved along axial and radial direction on the mounting ring to provide the mass flow rate which is injected from the rocket nozzle. In this paper, the conceptual design and the study on the tapered ramp tabs of the thurst vector control has been carried out using the supersonic cold flow system and schlieren system. This paper provides the thrust spoilage, three directional forces and moments and distribution of surface pressure on the region enclosed by the tapered ramp tabs.

300MW급 Shell형 1단 분류층 가스화기 성능에 대한 전산수치해석 : 석탄·바이오매스 혼합비에 따른 CO2 가스화 반응 (Numerical Study on 300 MW Shell-Type One-Stage Entrained Flow Bed Gasifier : Effect of Coal·Biomass Blending Ratio on CO2 Gasification)

  • 홍정우;박상신;송지훈;황정호
    • 한국수소및신에너지학회논문집
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    • 제23권3호
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    • pp.274-284
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    • 2012
  • Recently, gasification technology for coal blended with biomass has been an issue. Especially, An advantages of coal blended with biomass are 1) obtaining high cold gas efficiency, 2) obtaining syn-gas of high-high heating value (HHV), and 3) controlling occurrence of $CO_2$. In this study, the efficiency and characteristic of 300 MW Shell type gasifier were predicted using CFD simulation. The CFD simulation was performed for biomass coal blending ratios of 0~0.2, 0.5, 1 and $O_2$/fuel ratios of 0.5~0.84. Kinetic parameters (A, $E_a$) obtained by $CO_2$ gasification experiment were used as inputs for the simulation. In results of CFD simulation, residence times of particle in 300MW Shell type gasifer presented as 7.39 sec ~ 13.65 sec. Temperature of exit increased with $O_2$/fuel ratio as 1400 K ~ 2800 K, while there is not an effects of biomass coal blending ratios. Considering both aspects of temperature for causing wall slagging and high cold gas efficiency, the optimal $O_2$/fuel ratio and blending ratio were found to be 0.585 and 0.05, respectively.

CFD 해석을 통한 4종의 건식 분류층 석탄가스화기 설계개념 비교 (Comparison of Design Concepts for Four Different Entrained-Bed Coal Gasifier Types with CFD Analysis)

  • 윤용승;주지선;이승종
    • 공업화학
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    • 제22권5호
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    • pp.566-574
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    • 2011
  • 석탄가스화기는 석탄가스화복합발전과 석탄간접액화 공정에서 고효율을 얻기 위한 중요한 설비 중 하나이다. 현재 여러 종류의 석탄가스화기가 성공적으로 사용되고 있지만, 간단하면서도 신뢰도를 높일 수 있는 다양한 설계 변경이 가능하다. 건식 분류층 가스화기 4종류의 형태를 제시하고 이들을 체류시간, 가스화기 출구 합성가스의 온도, 합성가스 조성을 중점으로 비교하였다. 설계개념이 적정한지를 우선 파악하고자 반응을 배제한(cold-flow) CFD 해석을 먼저 수행하였고, 실제 가스화기 조건을 반영한 화학반응이 고려된(hot-flow) 해석을 수행하여 비교하였다. 가스화기 설계에 CFD를 적용하는 데는 슬랙의 거동과 슬랙탭 설계 등 측면에서 제한적이기는 하지만, 다양한 설계개념 중에서 가능성이 높은 가스화기 형태의 범위를 좁히는 데 매우 유용하게 사용될 수 있다.

유동상 반응로 조건에서 목재와 RDF 부분 산화의 영향 (Effect of Partial Oxidation of Wood and RDF in a Fluidized Bed)

  • 김태현;최상민
    • 한국연소학회지
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    • 제13권2호
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    • pp.23-32
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    • 2008
  • Gasification characteristics in the fluidized bed reactor are essential for the design of a gasification furnace to optimize the operation condition. Moisture content of the solid fuel is one of the important factors to influence directly the gasification characteristics. So it is necessary to investigate the effect of moisture content of solid fuel in partial oxidation condition. Gasification characteristics are investigated with results from thermogravimetric analyzer and lab-scale fluidized bed reactor for wood and RDF samples along with changing moisture contents. Additionally lab-scale fluidized bed reactor was run continuously and gas concentrations at the exit were measured. It is observed that the rate of reaction in partial oxidation condition is between the results from the combustion environment and from the inert condition. Moisture content in a particle slows down the heating rate of a particle. So, reaction is delayed by the moisture content. However, RDF samples those are easy to break-up don't show the effect of moisture content. The result of continuous operation condition shows that proper moisture content promotes gasification because steam from the particles helps gasification of the solid fuel. A simulation to predict the syn-gas composition was conducted by the Aspen Plus process simulator. The cold gas efficiency of the experiment was compared with results from the simulation.

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축열조를 이용한 냉매과냉각 시스템의 전력수요관리 효과에 대한 연구 (A Study on the DSM Effect of a Refrigerant-Subcooling Refrigeration System with an Ice Storage Tank)

  • 김정배;이은지;이동원
    • 설비공학논문집
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    • 제22권12호
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    • pp.845-851
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    • 2010
  • This study was experimentally performed to find the effects of refrigerant subcooling in the refrigeration system and to propose how to get the efficient use of energy. A refrigerant-subcooling refrigeration system consisted of a typical single vapor-compression refrigeration cycle, a subcooler, and an ice storage tank. The degree of subcooling at the exit of the condenser can be increased by the heat transfer between the subcooler and the ice storage tank. The cold heat in the ice storage tank was stored by using the refrigeration cycle during night time and then used to absorb the heat from the subcooler during daytime. The cooling capacity and COP of this system were higher than those of the conventional system due to the increase in the degree of subcooling. Typically, the refrigerant-subcooling system showed superior performance to the conventional refrigeration system and would also contribute to load leveling.