• Title/Summary/Keyword: Fuel Flow

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Numerical Study on Flow Distribution in PEMFC with Metal foam Bipolar Plate (다공성 분리판을 적용한 고분자 전해질 연료전지의 유동 분포에 관한 전산해석 연구)

  • SONG, MYEONGHO;KIM, KYOUNGYOUN
    • Transactions of the Korean hydrogen and new energy society
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    • v.27 no.1
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    • pp.29-35
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    • 2016
  • It is important to uniformly supply the fuel gas into the reaction activity area in polymer electrolyte membrane fuel cell (PEMFC). Recent studies have shown that the cell performance can be significantly improved by employing metal foam gas distributor as compared with the conventional bipolar plate types. The metal foam gas distributor has been reported to be more efficient to fuel transport. In this study, three-dimensional computational fluid dynamics (CFD) simulations have been performed to examine the effects of metal foam flow field design on the fuel supply to the reaction site. Darcy's law is used for the flow in the porous media. By solving additional advection equation for fluid particle trajectory, the gas transport has been visualized and examined for various geometrical configuration of metal foam gas distributor.

Preliminary Design on Jet Pump for Fuel Transfer and Analysis of Flow Distribution (연료 이송용 제트펌프 기본 설계 및 유동장 해석)

  • Kong Chang-Duk;Park Jong-Ha;Kim Young-Kwang;Han Dong-Joo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.125-129
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    • 2006
  • In the present study, preliminary design and analysis of flow distribution for a jet pump, which is able to transfer fuel from the tank to the engine, were performed as an aerospace component technology development project. The jet pump is a core part, which is normally installed in the fuel tank, to supply the fuel from the tank to the engine feed pump, or to transfer the feed between tanks. In order to design preliminarily installed in the jet pump, equations for design were modelled using SIMULINK, and the design was carried out based on the simulation model.

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Flame Stabilization Mechanism of a Micro Cyclone Combustor (마이크로 사이클론 연소기의 화염 안정화 기구)

  • Oh, Chang-Bo;Choi, Byung-Il;Han, Yong-Shik;Kim, Myung-Bae;Hwang, Cheol-Hong
    • 한국연소학회:학술대회논문집
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    • 2007.05a
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    • pp.139-144
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    • 2007
  • A micro cyclone combustor was developed to be used as a component of mobile power generator (MPG). The cyclone combustor was designed so that fuel and air were supplied to the combustion chamber separately to prevent a flash-back. The flame shape stabilized inside the micro cyclone combustor was visualized experimentally and the flow field and the combustion characteristics of the combustor were investigated numerically. The global equivalence ratio (${\Phi}$), defined using the fuel and air flow rates, was introduced to examine the overall flow and flame features of the combustor. The flame stabilization mechanism could be well understood using the velocity distribution inside the combustor. For only non-reacting case, it was found that a weak recirculating zone was formed upper the fuel-supplying tube in case of ${\Phi}$ < 1.0. It was also found that small regions that have a negative axial velocity exist near the fuel injection ports for both of non-reacting and reacting case. It was identify that a flame front was stabilized at the negative axial velocity regions near the fuel injection ports.

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Experimental Study on the Unsteady Flow Characteristics of Propellant in the Satellite (인공위성에 사용되는 추진연료의 비정상 유동특성에 관한 실험적 연구)

  • 최진철;윤효철;강신재
    • Journal of the Korean Society of Propulsion Engineers
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    • v.4 no.2
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    • pp.39-45
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    • 2000
  • A Thruster valve operates to supply fuel into thruster chamber. Very quick on-off operation of thruster valve results in unsteady flow of fuel in the propellant supplying system. Then fuel kinetic force, elastic material of propellant line, compressibility of fuel cause the flow field to pulsate. The pressure oscillation arising from resonance would damage the weak part of the thruster valve and other propellant supplying equipment. Pressure drop and fuel flowrate through propellant suppling system were measured, and pressure oscillation were triggered at the thruster valve inlet.

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Power upgrading of WWR-S research reactor using plate-type fuel elements part I: Steady-state thermal-hydraulic analysis (forced convection cooling mode)

  • Alyan, Adel;El-Koliel, Moustafa S.
    • Nuclear Engineering and Technology
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    • v.52 no.7
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    • pp.1417-1428
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    • 2020
  • The design of a nuclear reactor core requires basic thermal-hydraulic information concerning the heat transfer regime at which onset of nucleate boiling (ONB) will occur, the pressure drop and flow rate through the reactor core, the temperature and power distributions in the reactor core, the departure from nucleate boiling (DNB), the condition for onset of flow instability (OFI), in addition to, the critical velocity beyond which the fuel elements will collapse. These values depend on coolant velocity, fuel element geometry, inlet temperature, flow direction and water column above the top of the reactor core. Enough safety margins to ONB, DNB and OFI must-emphasized. A heat transfer package is used for calculating convection heat transfer coefficient in single phase turbulent, transition and laminar regimes. The main objective of this paper is to study the possibility of power upgrading of WWR-S research reactor from 2 to 10 MWth. This study presents a one-dimensional mathematical model (axial direction) for steady-state thermal-hydraulic design and analysis of the upgraded WWR-S reactor in which two types of plate fuel elements are employed. FOR-CONV computer program is developed for the needs of the power upgrading of WWR-S reactor up to 10 MWth.

Combustion Test of a Mach 5 Scramjet Engine Model (마하 5 스크램젯 엔진 모델의 연소 시험)

  • Yang, Inyoung;Lee, Yang-Ji;Kim, Young-Moon;Lee, Kyung-Jae
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.3
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    • pp.9-14
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    • 2013
  • Combustion tests were conducted for a hydrogen-fueled Mach 5 scramjet engine model using a blow-down facility. No fuel and two fuel flow rate cases were tested for two different model configurations. Time history of the wall static pressures inside the model and their time-averaged spatial distribution were used for the analysis of the flow and combustion characteristics. For shorter model, supersonic combustion was occurred for both of the fuel flow rate cases. For longer model, supersonic combustion was occurred for less fuel case, whereas thermal choking and subsonic combustion were occurred for more fuel case. Intake started even for this subsonic combustion case.

Fundamental Study on Effect of Preceding Vehicle Information on Fuel Consumption Reduction of a Vehicle Group

  • Matsumoto, Shuichi;Kawashima, Hironao
    • Journal of Communications and Networks
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    • v.15 no.2
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    • pp.173-178
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    • 2013
  • It is a concern that eco-driving vehicles, because their driving behavior differs from other vehicles due to e.g. e-start, may inhibit smooth traffic flow. Therefore, it is necessary to study the cooperative eco-driving done by a vehicle group, putting "vehicle-to-vehicle communication" and "road-to-vehicle communication" into perspective. Based on these factors, this study aimed to: 1) Analyze fuel consumption rates and driving behaviors of more than one vehicle following an Eco-Driving vehicle. 2) Examine the effect of information on the fuel consumption rate of the preceding vehicles on the following vehicles. As a result, the following findings were obtained: 1) By providing information to multiple following vehicles, the fuel consumption rate of the second vehicle was not lowered, while that of the third one was. 2) It is possible that, when information on fuel consumption of a preceding vehicle is provided to the following one, an inter-vehicular distance is shortened during deceleration to contribute to smooth traffic flow. From the above results, it is suggested that, when targeting a vehicle group, sharing the information on preceding vehicles is effective.

Flow Control of a Solenoid Gas Injector and Its Application on a Natural Gas Engine (솔레노이드 가스 인젝터의 유량제어와 천연가스엔진에서의 응용)

  • Sim, Han-Sub
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.8 no.2
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    • pp.83-89
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    • 2009
  • An air-fuel ratio control is essential in reducing hazardous exhaust emissions from a compressed natural gas(CNG) engine, and can be accomplished by accurate control of gas injection flow. In this study, theoretical research was conducted on injection characteristics of a solenoid gas injector, and injection experiments for calibration and analysis were performed. Various factors for gas injection flow such as injection pressure, gas temperature, and supply voltage are studied. A dynamic flow equation of the natural gas was proposed on the basis of flow dynamics theories and results of the injection experiment. The verification of the dynamic flow equation of the solenoid injector was carried out with a large CNG-engine applied to an urban bus. Air-fuel ratio control experiments were conducted in both steady and transient state. Results of injection experiments for the solenoid injector and the CNG-engine was proved the control method proposed herein to be effective.

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Hydraulic Design and Performance Evaluation of a Fuel Pump for a High Pressure Turbopump System (고압 터보펌프용 연료펌프의 수력설계 및 성능 평가)

  • Choi, Bum-Seog;Yoon, Eui-Soo;Oh, Hyoung-Woo
    • The KSFM Journal of Fluid Machinery
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    • v.8 no.2 s.29
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    • pp.31-38
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    • 2005
  • A low NPSH and high pressure fuel pump has been designed for a turbopump system. The fuel pump has an axial inducer and a centrifugal impeller. A meanline method has been established for the preliminary design and performance prediction of pumps at design or off-design points. KeRC(Kelyish Research Center) carried out a model testing of the fuel pump with water as a working fluid at the reduced speed. Predicted performances by the method are shown to be in good agreement with experimental results for cavitating and non-cavitating conditions. The established meanline method can be used for the performance prediction and preliminary design of high speed pumps which have a inducer, impeller and volute. In the current study, the three dimensional viscous flow in the fuel pump was investigated through numerical computation. A modified design of the fuel pump was generated to improve pump performance by utilizing CFD results. The modified fuel pump was experimentally tested by ROTEM and KARI(Korea Aerospace Research Institute). The measured non-cavitating and cavitating performance showed a good agreement with designed performance.

Effects of environmental temperature on the performance of direct methanol fuel cell for vehicles (외부온도가 수송용 메탄올연료전지 성능에 미치는 영향)

  • Han, Chang-Hwa;Jung, Dae-Seung;Choi, Ji-Sun;Han, Sang-Hun;Lee, Joong-Hee
    • 한국신재생에너지학회:학술대회논문집
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    • 2009.11a
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    • pp.176-179
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    • 2009
  • The performance of direct methanol fuel cells is affected by operating conditions such as, methanol feeding temperatures, methanol concentrations, and methanol flow rates during the operation in different environmental conditions. In this study, effects of the environmental temperature on performance of direct methanol fuel cells have been investigated in order to test a applicability of direct methanol fuel cell to the vehicle. The environmental temperature (ET) was varied from $-20^{\circ}C$ to $+30^{\circ}C$. The inside fuel cell temperature (CT) during test at various operating conditions was monitored and the performance of fuel cell was measured in the I-V polarization curve. With increasing the ET, the performance of the fuel cell was significantly improved and the CT also almost linearly increased. However, at below $0^{\circ}C$ ET, the DMFC showed very poor performance and needed to control CT or methanol feeding temperature (MFT), methanol flow rate(MFR) to obtain enough power of the vehicle.

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