• Title/Summary/Keyword: Fuel Flow

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튜브진동 시 판스프링 지지부의 미끄럼변위와 마멸 분석 (Analysis of Slip Displacement and Wear in Oscillating Tube supported by Plate Springs)

  • 김형규;이영호;송주선
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 2003년도 학술대회지
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    • pp.41-49
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    • 2003
  • Tube oscillation behaviour is experimentally investigated for the study on the fuel rod fretting that is caused by the flow-induced vibration in nuclear reactor. The experiment was conducted in all at room temperature. The specimen of tube assembly was supported by plate springs which simulated the spacer grids and fuel rods of a fuel assembly. To investigate the influence of contact condition between the grids and rods, normal load of 10 and 5 N, gaps of 0.1 and 0.3 mm were applied. The range of the oscillation at the center of the fuel rod specimen was varied as 0.2, 0.3 and 0.4 mm to simulate the fuel rod vibration due to flow. Displacements near the contact were measured with four displacement sensors during the tube oscillation. As results, the shape of oscillation (phase) varied depending on the contact condition. The oscillation displacement increased considerably from the contact to gap condition. The displacement increased further as the gap size increased. It is regarded that the spring shape influences the tube oscillation behaviour. Simple calculation showed that the slip displacement was very small. Therefore, cumulative damage concept is necessary for the fuel rod wear. The mechanism of plowing is thought required to explain the severe wear in the case of gap existence.

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용융 탄산염 연료전지의 분리판 내 연료 분배 해석 (A study for gas distribution in separators of molten carbonate fuel cell)

  • 박준호;차석원
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2011년도 추계학술대회 초록집
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    • pp.82.2-82.2
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    • 2011
  • A channel design which is closely related with the mass transport overpotential is one of the most important procedures to optimize the whole fuel cell performance. In this study, three dimensional results of a numerical study for gas distribution in channels of a molten carbonate fuel cell (MCFC) unit cell for a 1kW class stack was presented. The relationship between the fuel and air distribution in the anode and cathode channels of the unit cell and the electric performance was observed. A charge balance model in the electrodes and the electrolyte coupled with a heat transfer model and a fluid flow model in the porous electrodes and the channels was solved for the mass, momentum, energy, species and charge conservation. The electronic and ionic charge balance in the anode and cathode current feeders, the electrolyte and GDEs were solved for using Ohm's law, while Butler-Volmer charge transfer kinetics described the charge transfer current density. The material transport was described by the diffusion and convection equations and Navier-Stokes equations govern the flow in the open channel. It was assumed that heat is produced by the electrochemical reactions and joule heating due to the electrical currents.

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고온 고분자전해질 연료전지 박판형 분리판의 유로 설계 및 스택 성능 평가 (Flow Field Design and Stack Performance Evaluation of the Thin Plate Separator for High Temperature Polymer Electrolyte Membrane Fuel Cell)

  • 김지홍;김민진;김진수
    • 한국수소및신에너지학회논문집
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    • 제29권5호
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    • pp.442-449
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    • 2018
  • Research on High temperature polymer electrolyte fuel cell (HT-PEMFC) has actively been conducted all over the world. Since the HT-PEMFC can be operated at a high temperature of $120-180^{\circ}C$ using phosphoric acid-doped polybenzimidazole (PBI) electrolyte membrane, it has considerable advantages over conventional PEMFC in terms of operating conditions and system efficiency. However, If the thermal distribution is not uniform in the stack unit, degradation due to local reaction and deterioration of lifetime are difficult to prevent. The thin plate separator reduces the volume of the fuel cell stack and improves heat transfer, consequently, enhancing the cooling effect. In this paper, a large area flow field of thin plate separator for HT-PEMFC is designed and sub-stack is fabricated. We have studied stack performance evaluation under various operating conditions and it has been verified that the proposed design can achieve acceptable stack performance at a wide operating range.

End-Burning 하이브리드 로켓의 스월 강도 변화에 따른 연료 후퇴율에 관한 연구 (A Study on Regression Rate in End-Burning Hybrid rocket with Variation of Swirl Intensity)

  • 최원준;우경진;문희장;성홍계;김진곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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    • pp.70-75
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    • 2012
  • 본 연구는 End-Burning 하이브리드 로켓 연소에서 연료직경과 인젝터 형상 변화, 인젝터 각도 변화를 통한 스월강도 변화에 따른 연소특성의 변화을 알아보기 위해 수행하였다. 연료직경이 커지면 연료의 연소량이 증가하고, 인젝터 직경이 커질수록 후퇴율이 낮아졌다. 그리고 본 연구의 End-Burning 연소기는 고체연료의 연소율에 미치는 영향이 산화제 유동의 Impinging 효과 보다는 Swirl 효과가 더 큼을 확인했다. 스월상수를 적용한 후퇴율식을 도출하여, 스월상수가 서로 다른 경우들에 대한 후퇴율 관계식을 하나의 식으로 표현할 수 있었다.

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화염 구조에 미치는 연료 및 당량비에 관한 연구 (A Study on the Influence of Equivalence Ratio and Kinds of fuel in Flame Structure)

  • 박상규;최낙정;산하박사
    • 한국분무공학회지
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    • 제3권4호
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    • pp.43-49
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    • 1998
  • In order to clarify the effect of equivalence ratio and kinds of fule in flame structure, a numerical simulation of triple flame developed in a co-flowing methane-air and air stream was carried out by the elementary chemical reaction mechanism. The following conclusions were obtained. Equivalence ratio at which the apparent burning velocity is maximum is a little larger than that of the one-dimensional premixed flame. Apparent burning velocities are two times higher than that of the one-dimensional premixed flame for the methane-air. The flame thrusts out forward in the downstream of the boundary between mixture and air stream, and a part of the flow is bent and forks out in this protruding flame so that a triple flame is originated; this triple flame is composed of fuel rich and lean premixed flame branches and a diffusion flame branch. Near the equivalence ratio at which the burning velocity of rule-dimensional premixed flame is the largest the effect of one-dimensional premixed flame becomes large and the fuel rich premixed flame advances and becomes vertical to the flow direction.

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축열식 저 NOx 연소기의 배기가스 내부 재순환 유동에 대한 연구 (A Study on the Self Flue Gas Recirculating Flow of the Regenerative Low NOx Burner)

  • 김종규;강민욱;윤영빈
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2001년도 제23회 KOSCO SYMPOSIUM 논문집
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    • pp.17-26
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    • 2001
  • Self flue gas recirculation flow is an effective method for low NOx emission in the regenerative low NOx burner. The object of this study is to analyze the self flue gas recirculating flow by varying jet velocity of the combustion air. Fuel and air flow rates are fixed and combustion air jet nozzle diameters are 13, 6.5 and 5mm. The stoichiometric line is obtained from the concentration of the fuel using an acetone PLIF technique. It is found that the self flue gas recirculating flow is entrained into that line using a two color PIV technique. As the jet velocity of combustion air is increased, the flue gas entrainment rate into the stoichiometric line is increased. This result suggests that NOx emission can be reduced due to the effects of flue gas which is lowering the flame temperatures.

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가변형 음속/초음속 이젝터 시스템에 관한 실험적 연구 (An Experimental Study of the Variable Sonic/supersonic Ejector Systems)

  • 이준희;김희동
    • 대한기계학회논문집B
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    • 제29권5호
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    • pp.554-560
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    • 2005
  • A new method to improve the efficiency of a hydrogen fuel cell system was introduced by using variable sonic/supersonic ejectors. To obtain the variable area ratio of the nozzle throat to ejector throat which controls the mass flow rate of the suction flow, the ejectors used a movable cylinder inserted into a conventional ejector-diffuser system. Experiments were carried out to understand the flow characteristics inside the variable ejector system. The secondary mass flow rates of subsonic and supersonic ejectors were examined by varying the operating pressure ratio and area ratio. The results showed that the variable sonic/supersonic ejectors could control the recirculation ratio by changing the throat area ratio, and also showed that the recirculation ratio increased fur the variable sonic ejector and decreased for the variable supersonic ejector, as the throat area ratio increases.

HVOF 용사총의 기체역학에 관한 연구 (A Study of Gas Dynamics of the High-Velocity Oxy-Fuel Thermal Spray Gun)

  • 조필재;김희동
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.574-579
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    • 2003
  • The present study addresses an analytical investigation to understand the characteristics of gas flow in the High-Velocity Oxy-Fuel(HVOF) thermal spray gun. One-dimensional analysis is extended to involve the effects of the wall friction and powder particle diameter. From the present analysis it is well known that the flow characteristics inside and outside the thermal spray gun is varied depending on the combustion chamber pressure. The thermal spray gun flow is characterized by six different patterns. The powder particle size and wall friction significantly influence the powder particle velocity. The particle velocity decreases with an increase in the powder particle size. This implies that the combustion chamber pressure should be increased to achieve a higher velocity of the powder particle.

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SCV에 의한 스윌 유동이 직분식 디젤 엔진의 연소에 미치는 영향에 관한 연구 (A Study on the Effects of Swirl Flow Generated by SCV on the Combustion Characteristics of the D.I. Diesel Engine)

  • 정재우;이기형;이창식
    • 한국자동차공학회논문집
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    • 제10권2호
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    • pp.31-39
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    • 2002
  • Recently, many researches have been performed to improve the performance of the combustion and emission in a D.I.Diesel engine. One of the main factors effect on the characteristics of combustion is the characteristic of air-fuel mixing. Thus, swirl flow has been used widely to improve the air-fuel mixing in a D.I.Diesel engine. Since this swirl flow has interaction with other factors, in this study, the characteristics of the combustion and the flame effected by the swirl flow generated by SCV was investigated. From this experiment, the interactions of the swirl flow and the injection timing made clear. In addition, the effects of swirl and injection timing on the diffusion flame were clarified.

반응과 비반응 제트유동에서 단일 와동의 동적 거동에 대한 수치해석적 연구 (A Numerical Investigation on the Dynamic Behaviors of Single Vortex in a Reacting and Non-reacting Jet Flow)

  • 황철홍;오창보;이대엽;이창언
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2002년도 춘계 학술대회논문집
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    • pp.35-40
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    • 2002
  • The dynamic behaviors of the single vortex in a reacting and non-reacting methane-air jet flow were investigated numerically. The numerical method was based on a predictor-corrector for low Mach number flow A two-step global reaction mechanism was adopted as a combustion model. After fuel and air were developed entirely in computational domain, the single vortex was generated by an axisymmetric jet that was impulsed to emit a cold fuel. Through comparisons of single vortex in reacting and non-reacting jet flow, it was found that global dynamic behaviors and the mechanisms leading to the formation, transport processes of vortex ring were influenced significantly by heat release from reaction. In addition, the interaction between a single vortex and flame bulge generated by buoyance effect in a reacting jet flow was found.

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