• 제목/요약/키워드: Fuel Nozzle

검색결과 625건 처리시간 0.033초

메탄 분류 화염에서의 연소 조건에 따른 NOx 배출 특성 (NOx Emission Characteristics in Parametrically Varied Methane-Air Coflow Flames)

  • 이상한;오창보;이창언
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2000년도 제20회 KOSCO SYMPOSIUM 논문집
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    • pp.35-44
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    • 2000
  • It was numerically studied that NOx emission characteristics of confined $CH_{4}$ jet flames with the variation of the diameter of inner fuel nozzle, the flow rate of $CH_{4}$ and equivalence ratio. Parabolic type equations were adopted in the calculation and GRI-2.1I mechanism was used for the chemical reaction. NOx emission index (EINOx) was introduced to evaluate NOx emission quantitatively in parametrically varied flames and the contribution of Thermal and Prompt NO mechanism was discussed. The results showed that Total EINOx varied sensitively with the variation of the flow rate of$CH_{4}$ but it was not sensitive to the variation of the diameter of inner fuel nozzle. Thermal EINOx showed the similar tendency to total EINOx and Prompt EINOx showed insensitivity to the variation of the diameter of inner fuel nozzle and the flow rate of $CH_{4}$.

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스크램제트 연소기 모델의 고공시험 연구 (The high altitude test method of Scramjet engine combustor model)

  • 우관제;김영수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.271-274
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    • 2002
  • This paper is investigated construction of the Scramjet test facility and test method of Scramjet engine combustor model. Scramiet engine combustor model test was performed at Lab C-16BK CIAM (Central Institute of Aviation Motors) at Tyraevo in Moscow. The velocity of flow in the combustion chamber equal to Mach number 2.49 with single hole fuel spray nozzle injector and test duration equal to 7 seconds. Therefore In this paper is showed high altitude test method of Scramjet combustor model and the proper structure of combustor with single hole fuel spray nozzle.

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직접 분사식 디젤 기관 인젝터의 연료 분무 특성 (Spray Characteristics of Fuel Injector in DI Diesel Engine)

  • 이창식;김민규;전원식;진다시앙
    • 한국자동차공학회논문집
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    • 제9권5호
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    • pp.75-81
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    • 2001
  • This paper presents the atomization characteristics of single hole injector in the direct injection type diesel engine. The spray characteristics of fuel injector such as the droplet size and velocity were measured by phase Doppler particle analyzer. In this paper, the atomization characteristics of fuel spray are investigated for the experimental analysis of the measuring data by the results of mean diameter and mean velocity of droplet. The effect of fuel injection pressure on the droplet size shows that the higher injection pressure results in the decrease of mean droplet diameter in the fuel spray. The minimum size of fuel spray droplet appears on the location of 40mm axial distance from nozzle exit of diesel injector. Based on the experimental results, the correlation between the droplet diameter and mean velocity of the diesel spray due to the change of axial and radial distance from the nozzle tip were investigated.

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다단 연소기를 이용한 LNG 화염의 NOx 발생에 관한 실험적 연구 (An Experimental Study on the NOx Formation of LNG Flame in Fuel Staged Combustor)

  • 정진도;한지웅;안국영
    • 대한기계학회논문집B
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    • 제28권4호
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    • pp.389-394
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    • 2004
  • An experimental study on the NOx formation of LNG flame in fuel staged combustor has been studied. The design concept of multi fuel/air staged combustor is creation of two separate flame, a primary flame is a act as a pilot flame for the secondary combustion stage combustion zone, where most of fuel bums. Experiments were performed on a semi-industrial scale (thermal input 0.233 MW) in a laboratory furnace and Liquefied Natural Gas(LNG) was used as a primary and secondary fuels. This study included parametric study to identify the optimum operating conditions which are primary/secondary fuel ratio, and primary/secondary air ratio for reducing NOx emission with two types of nozzle. The test demonstrated that NOx emission can be reduced by >70% in accordance with operating conditions.

유화연료의 특성에 관한 연구 (A Study on Characteristics of Emulsified Fuel)

  • 정진수;김종진;이금배
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 1999년도 제19회 KOSCO SYMPOSIUM 논문집
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    • pp.105-110
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    • 1999
  • The elementary experiment was performed to develop the emulsified fuel production system using pressure injection nozzle in this study. The stabilities and characteristics of emulsified fuel which is produced through direct spray of water via pressure injection nozzle into oil are examined. To understand performance of emulsion production, stabilities of emulsified fuel which is made by adding water to the mixed fuel of Bunker-C and 10 $^{\sim}$ 50 vol% of heating oil were investigated. According to volume ratios of surfactant in heating oil the stability and SMDs were measured

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디젤연소에 미치는 노즐 형상 및 분사시기의 효과에 관한 연구 (A Study on Effects of the Nozzle Shape and Injection Timing in a Diesel Combustion)

  • 윤천한;김경훈
    • 한국분무공학회지
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    • 제6권3호
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    • pp.32-37
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    • 2001
  • The characteristics of engine performance with fuel injection system in D.I. diesel engine were studied in this paper. A fuel injection system has an important role in the performance and emission gas in a diesel engine. In this paper, an experimental study has been performed to verify the effect of the performance and the emission gas with the factors such as diameters of an injection nozzle hole, diameters of an injection pipe and injection timing in the fuel injection system. The authors have obtained the results that optimizing the factors of fuel injection system is significant to enhance the performance of the engine system and consumption ratio of fuel, smoke, and NOx.

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다단 연소기를 이용한 LNG 화염의 NOx 발생에 관한 실험적 연구 (An Experimental study on the NOx Formation of LNG Flame in Fuel Staged Combustor)

  • 한지웅;안국영;김한석;정진도;박경진
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.161-166
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    • 2001
  • An Experimental study on the NOx formation of LNG flame in fuel staged combustor has been studied. The design concept of multi fuel/air staged combustor is creation of two separate flame, a primary flame is act as a pilot flame for the secondary combustion stage combustion zone, where most of fuel burns. Experiments were performed on a semi-industrial scale (thermal input 0.233 MW) in a laboratory furnace and Liquefied Natural Gas(LNG) was used as primary and secondary fuels. The study included parametric study to identify the optimum operating conditions which are primary/secondary fuel ratio, and primary/secondary air ratio for reducing NOx emission with two types of nozzle. The test demonstrated that NOx emission can be reduced by >70% in accordance with operating conditions.

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직접 디젤 연료분사계의 분사 특성과 기관 성능 개선에 관한 연구 (Injection Feature and Engine Performance Improvement of the Direct Diesel Fuel Injection System)

  • 윤천한;김경훈
    • 한국분무공학회지
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    • 제7권1호
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    • pp.1-6
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    • 2002
  • This study has focused on using fuel injections as variables for measuring performance and reducing exhaust gas in turbo-charger diesel engine. In experiments, we changed nozzle hole diameter, diameter of an injection pipe, and injection timing as variable. The results show that torque. fuel consumption and smoke are reduced as nozzle hole diameter decreases, while NOx increases. When the diameter of injector is reduced, torque, fuel consumption and smoke are deteriorated, but NOx is decreased. In addition, when the time for injection is advanced. torque, fuel consumption and smoke are improved, but the density of NOx is increased.

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상호작용하는 부상화염의 특성에 관한 연구 (Characteristics of Interacting Lifted Flames)

  • 이승;이병준
    • 대한기계학회논문집B
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    • 제25권4호
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    • pp.461-466
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    • 2001
  • The characteristics of nonpremixed interacting flames are investigated in the parameter of nozzle configuration and nozzle separation distane, s. Three nozzle arrangements - diamond 4 nozzle, linear 5 nozzle and cross 5 nozzle- are used. When s is about 10 nozzle diameter, flames lift from the nozzle at the highest fuel flowrate compared with the other s cases. Normally flames are extinguished at the lifted states. Flowrates when blowout occurs are affected by the nozzle configuration, nozzle seperation distance. Blowout flowrates for the diamond- or cross-shaped nozzle cases are parabolic function of s. For 5 cross nozzle case, flames extinguished at 3.3 times higher flowrate than that of single equivalent area nozzle. Turbulent liftoff heights are not function of flowrates for these cases.

로켓 노즐 유동의 열/화학적 특징 및 해석 기법 (Thermochemcial Characteristics of Rocket Nozzle Flow and Methods of Analysis)

  • 최정열
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2001년도 춘계 학술대회논문집
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    • pp.144-148
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    • 2001
  • Characteristics of high temperature rocket nozzle flow is discussed along with the aspects of computational analysis. Three methods of nozzle flow analysis, frozen-equilibrium, shifting-equilibrium and non-equilibrium approaches, were discussed those were coupled with the methods of computational fluid dynamics. A chemical equilibrium code developed for the analysis of general hydrocarbon fuel was coupled with three approaches of nozzle flow analysis, and a test was made for a bell nozzle at typical operation condition. As a results, the characteristics of the approaches were discussed in aspects of rocket performance, thermal analysis and computational efficiency.

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