• Title/Summary/Keyword: Fuel nozzle

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5kW 용융탄산염 연료전지 이젝터 설계 및 시험 (The Ejector Design and Test for 5kW Molten Carbonate Fuel Cell)

  • 김범주;김도형;이정현;정상천;이성윤;강승원;임희천
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2008년도 춘계학술대회 논문집
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    • pp.53-56
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    • 2008
  • An ejector is a fluid machinery to be utilized for mixing fluids, maintaining vacuum, and transporting them. The Ejector is applied for a variety of industrial fields such as refrigerators and power plants. It is adopted to recycle anode off gas safely in 5kW Molten Carbonate Fuel Cell system of KEPRI(Korea Electric Power Research Institute). The ejector is placed at mixing point between the anode off gas and the cathode off gas or the fresh air. In this study, the entrainment ratio is measured according to the diametrical ratio of nozzle to throat. In addition, the performance curve of the ejector and the differential pressure in diffuser is observed.

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동축류 마일드 연소기를 적용한 마일드 연소 형성 연구 (Formation of MILD Combustion using Co-flow MILD Combustor)

  • 이필형;황상순
    • 한국연소학회지
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    • 제22권3호
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    • pp.8-16
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    • 2017
  • MILD combustion was first developed to suppress thermal NOx formation in combustor for heating industrial furnaces. In this paper, the effect of co-flow MILD combustor geometry and operating conditions on the formation of MILD combustion was analyzed using 3 dimensional numerical simulation. The numerical simulations were carried out using ANSYS Fluent. The combustion and turbulence flow was modeled using the Eddy Dissipation Concept(EDC) model and realizable $k-{\varepsilon}$ model respectively. The results show that the high temperature region and average temperature decreased due to an increase in the air velocity and decrease the wall thickness of fuel nozzle. In particular, the MILD combustion flame was found to be stable with a combustion flame region at fuel velocity 10 m/s, air velocity 20 m/s, fuel nozzle thickness 1.0 mm, equivalence ratio 0.9, and outlet area ratio 40%.

Carbon Contained Ammonium Diuranate Gel Particles Preparation in Mid-process of High-temperature Gas-cooled Reactor Fuel Fabrication

  • Jeong, Kyung Chai;Cho, Moon Sung
    • Nuclear Engineering and Technology
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    • 제48권1호
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    • pp.175-181
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    • 2016
  • This study investigates the dispersibility of carbon in carbon contained ammonium diuranate (C-ADU) gel particles and the characteristics of C-ADU gel liquid droplets produced by the vibrating nozzle and integrated aging-washing-drying equipment. It was noted that the excellent stability of carbon dispersion was only observed in the C-ADU gel particle that contained carbon black named CB 10. ADU gel liquid droplets containing carbon particles with the excellent sphericity of approximately 1,950 mm were then obtained using an 80-100-Hz vibrating nozzle system. Dried C-ADU gel particles obtained by the aging-washing-drying equipment were thermal decomposed until $500^{\circ}C$ at a rate of $1^{\circ}C/min$ in an air or in 4% $H_2$ gas atmosphere. The thermally decomposed C-ADU gel particles showed 24% weight loss and a more complicated profile than that of ADU gel particles.

이중 콘형 부분 예혼합 GT 노즐의 연료 분사구 형상 변화에 대한 연소특성 (Combustion Characteristics of a Double-cone Partial Premixed Nozzle with Various Fuel hole Patterns)

  • 김한석;조주형;김민국;황정재;이원준
    • 한국가스학회지
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    • 제24권4호
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    • pp.25-31
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    • 2020
  • 산업용 혹은 발전용 가스터빈에 사용되는 이중 콘형 예혼합 연소기의 연소 특성을 이해하기 위하여 실험적 연구를 수행하였다. 노즐의 여러 연료 분사 방식에 대하여 NOx와 CO의 배출 특성, 화염 안정성 및 연소실 온도 분포에 대한 연소특성을 비교하였다. 주 연구 결과로는 연료홀 개수가 동일하고 연료 홀 직경이 감소하는 경우와 연료 홀면적이 동일하고 연료 홀 수가 감소되는 경우 연료의 연소용 공기층 침투가 커지기 때문에 NOx의 배출은 감소하지만 화염 안정성은 감소하게 된다. 그리고 동일 연료 홀 면적을 이용하는 분사방식에 있어서 연료 홀을 교차 변경하는 경우 연료의 평균 침투거리 증가로 NOx의 배출이 감소되며 연료 침투거리가 적은 연료가 화염을 안정화시키는 역할을 한다.

고온가스로용 핵연료 UO2 Kernel 입자제조 ( UO2 Kernel Particle Preparation for HTGR Nuclear Fuel)

  • 정경채;김연구;오승철;조문성
    • 한국세라믹학회지
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    • 제44권8호
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    • pp.437-444
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    • 2007
  • The broth solution was prepared by the mixing of an uranyl nitrate, THFA, PVA, and water. The uranium concentration of the broth solution was $0.5{\sim}0.8$ mole-U/L and the viscosity of it was $30{\sim}80cSt$. The droplets of this broth solution were farmed in air and ammonia by the vibrating nozzle with the frequency of 100 Hz at the amplitude of $100{\sim}130V$. The diameter of the droplet was about $1900{\mu}m$ from using the nozzle diameter of 1 mm. The diameter of the aged gel was about $1400{\mu}m$ after aging in ammonia solution at $60{\sim}80^{\circ}C$, and the dried gel with the diameter of about $900{\mu}m$ was obtained after drying at room temperature or partially vacuum condition. The diameter of the calcined $UO_3$ microsphere after calcination at $600^{\circ}C$ appeared about $800{\mu}m$ in air atmosphere. Although the droplets of the same sizes were formed, the calcined microspheres of different sizes were manufactured in the case of the broth solutions of the different uranium concentration. The droplets of the desired diameters were obtained by the change of the nozzle diameters and the broth flow rates.

공연비 변화가 MILD 연소 특성에 미치는 영향에 관한 해석적 연구 (A numerical study of the air fuel ratio effect on the combustion characteristics in a MILD combustor)

  • 하지수;김태권;심성훈
    • 대한환경공학회지
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    • 제32권6호
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    • pp.587-592
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    • 2010
  • 연소과정 중에 발생하는 질소산화물을 저감하는 기술인 MILD 연소에 대하여 공연비를 변화시키면서 나타나는 연소 특성을 수치해석을 통하여 연구하였다. 작은 크기의 공기분출속도(10 m/s)에서는 공기가 연소로 내 상부영역까지 침투하지 못한다. 반면에 공기분출속도가 30 m/s인 경우에는 공기유동이 연료유동을 억제하고 상부영역까지 흘러간다. 이론공기량에 해당하는 공기분출속도 18 m/s에서는 10 m/s 보다 상대적으로 상부영역까지 침투하였다. 이러한 유동 양상으로 공기분출속도가 작은 10 m/s에서는 연소반응대가 공기노즐 측에 치우쳐 나타나고 30 m/s에서는 연료노즐 측에 형성되었다. 공기분출속도 16, 18, 20 m/s에서는 공기노즐과 연료노즐 중간 영역에서 연소반응대가 형성되었다. 연소로 내 최대온도와 NOx 생성은 공기분출속도가 10 m/s, 30 m/s인 경우 보다 이론공기량이거나 이에 가까운 16, 18, 20 m/s에서 낮게 나타났다. 본 연구로부터 MILD 연소로에서 이론공기량 조건이 NOx를 저감하는 최적의 조건이라는 것을 밝혔다.

동축류 버너에서 질소 희석된 연료의 부상 특성 (Characteristics of Lifted Flame in Coflow Jets for Highly Diluted Fuel)

  • 원상희;차민석;이병준;정석호
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2000년도 제20회 KOSCO SYMPOSIUM 논문집
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    • pp.9-15
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    • 2000
  • Characteristics of lifted flames for highly diluted propane and methane with nitrogen in coflowing air is experimentally investigated. In case of propane, for various fuel mole fractions and jet velocities, three distinctive types of flames are observed; nozzle attached flames, stationary lifted flames, and oscillating lifted flames. When fuel jet velocity is much smaller than coflow velocity, the base of nozzle attached flame has a tribrachial structure unlike usual coflow difusion flames. Based on the balance mechanism of the propagation speed of tribrachial flame with flow velocity, jet velocity is scaled with stoichiometric laminar burning velocity. Results show that there exists two distinctive lifted flame stabilization; stabilization in the developing region and in the developed region of jets depending on initial fuel mole fraction. It has been found that lifted flame can be stabilized for fuel velocity even smaller than stoichiometric laminar burning velocity. This can be attributed to the buoyancy effect and flow visualization supports it. Lifted flames are also observed for methane diluted with nitrogen. The lifted flames only exist in the developing region of jet.

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연료 활성화를 위한 디젤 미립화 장치의 수치해석 연구 (Numerical Study of Diesel Atomization Device for Fuel Activation)

  • 최상인;;서호석;김상범;조영민
    • 한국대기환경학회지
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    • 제33권4호
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    • pp.306-318
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    • 2017
  • Heavy diesel vehicles are one of major sources of urban fine dust in Korea and other developing countries. In this study, an auxiliary device assisting fuel atomization, which is called FAD (Fuel Activation Device), was closely reviewed through numerical simulation. As calculated, the diesel flow velocity passing across FAD increased up to 1.68 times, and it enhanced the cavitation effect which could improve the injected fuel atomization. Super cavitation phenomenon, which is the most important effect on nozzle injection, has occurred until the cavitation number (${\sigma}$) decreased from 1.15 to 1.09, and atomized droplets via a nozzle of which opening was $500{\mu}m$ distributed less than $200{\mu}m$ in sauter mean diameter (SMD).

空氣밸브型 脈動燃燒器의 特性에 관한 實驗的 硏究 (An experimental study of the overall characteristics in an aero-valved pulsating combustor)

  • 오상헌;최병륜;임광열
    • 대한기계학회논문집
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    • 제11권2호
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    • pp.271-278
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    • 1987
  • 본 논문에서는 공기밸브형 진동연소기에 관한 이해를 더 증진시키기 위해서 기본적인 공기밸브형 진동연소기를 제작해서 압력진동 및 발생되는 소음특성, 작동주 파수, 그리고 연소특성에 관해 실험적 고찰을 행했다.

노즐분공내 유체충돌이 있는 디젤노즐의 유동 및 분무특성 연구 (Characterization of the internal flow and fuel spray from an impinging flow nozzle)

  • 하성업;김흥열;구자예;류구영
    • 대한기계학회논문집B
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    • 제21권12호
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    • pp.1635-1646
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    • 1997
  • The nozzle length to diameter ratio of real diesel nozzles is about 2-8 which is not long enough for a fully developed and stabilized flow. The characteristics of the flow such as turbulence at the nozzle exit which affect the development of the spray can be enhanced by impinging the flow inside nozzle. The flow details inside the impinging nozzles have been investigated both experimentally and numerically. The mean velocities, the fluctuating velocities, and discharge coefficients in the impinging inlet nozzles, round inlet nozzle, and sharp inlet nozzle were obtained at various Reynolds number. The developing feature of the external spray were photographed by still camera and the droplet sizes and velocities were also measured by laser Doppler technique. The spray angle was greater and the droplet sizes near the spray axis were smaller with the impinging flow inside nozzle.