• 제목/요약/키워드: Initial Pressure Ratio

검색결과 343건 처리시간 0.029초

엔진실린더 모형 연소실내의 메탄-공기 예혼합기의 화염전파속도 특성 (Propagation Speed Characteristics of Premixed Methane-Air Flame in a Combustion Chamber with Model of Engine Cylinder)

  • 전충환
    • Journal of Advanced Marine Engineering and Technology
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    • 제22권2호
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    • pp.225-231
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    • 1998
  • Flame propagation speed characteristics of methante-air mixtures were experimentally investigated in combustion chamber modelled engine. Flame propagation process was known as a funtion of equivalence ratio initial pressure and initial temperature. Ion probe and schlieren photograph were applied to measure the local flame speed and flame radius in quiescent mixtures. Pressure was also measured to make sure of the reproducibility and to apply combustion analysis. Burning velocity was calculated from the flame propagation speed and combustion analysis. Flames were developed faster with higher initial pressure and initial temperature but showed maximum propagation speed at equivalence ratio 1.1 regardless of initial pressure and temperature. Local flame speed was maximum values at near midpoint between center and wall.

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COMBUSTION CHARACTERISTICS OF INHOMOGENEOUS METHANE-AIR MIXTURE IN A CONSTANT VOLUME COMBUSTION CHAMBER

  • Choi, S.H.;Jeon, C.H.;Chang, Y.J.
    • International Journal of Automotive Technology
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    • 제5권3호
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    • pp.181-188
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    • 2004
  • A cylindrical constant-volume combustion chamber was used to investigate the flow characteristics at the spark electrode gap and the combustion characteristics of an inhomogeneous charge methane-air mixture under several parameters such as stratified pattern, initial charge pressure, ignition time and the excess air ratio of the initial charge mixture. Flow characteristics including mean velocity and turbulence intensity were analyzed by a hot-wire anemometer. The combustion pressure development, measured by a piezo-electric pressure transducer, was used to investigate the effect of initial charge pressure, excess air ratio and ignition times on combustion pressure and combustion duration. It was found that the mean velocity and turbulence intensity had the maximum value around 200-300 ms and then decreased gradually to near-zero value at 3000 ms. For the stratified patterns, the combustion rate under the rich injection (RI) condition was the fastest. Under the initial charge conditions, the second mixture was accompanied by an increase in the combustion rate, and that the higher the mass which is added in the second stage injection, the faster the combustion rate.

정적연소기에서의 메탄-공기 혼합기의 연소특성(1) : 균질급기 (Combustion Characteristics of Methane-Air Mixture in a Constant Volume Combustion Chamber(1): Homogeneous Charge)

  • 최승환;전충환;장연준
    • 한국자동차공학회논문집
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    • 제11권3호
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    • pp.48-57
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    • 2003
  • A cylindrical constant volume combustion chamber was used to investigate the flow characteristics at spark plug and the combustion characteristics of homogeneous charge methane-air mixture under various initial pressure, excess air ratio and ignition times in quiescent mixture. The flow characteristics such as mean velocity and turbulence intensity was analyzed by hot wire anemometer. Combustion pressure development measured by piezoelectric pressure transducer and flame propagation acquired by ICCD camera were used to investigate the effect of initial pressure, excess air ratio and ignition times on pressure, combustion duration, flame speed and burning velocity. Mean velocity and turbulence intensity had the maximum value at 200 or 300ms and then decreased to near 0 value gradually after 3 seconds. Combustion duration, flame speed and burning velocity were observed to be promoted with excess air ratio of 1.1, lower initial pressure and ignition time of 300ms.

핀틀 로켓의 초기 최적 노즐 팽창비 결정 방법 연구 (The stydy on determination method of initial optimal nozzle expansion ratio in pintle solid rocket motor)

  • 김중근;이영원
    • 한국항공우주학회지
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    • 제39권8호
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    • pp.744-749
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    • 2011
  • 본 논문에서는 핀틀 로켓의 초기 최적 노즐 팽창비를 결정하는 방법에 대해서 제시하였다. 초기 최적 노즐 팽창비는 최대/최소 압력의 추력 계수로부터 계산되는 질량 가중 추력 계수를 최대화시켜 결정하였으며 이는 주어진 임무를 수행함에 있어 소요되는 추진제무게가 최소화되는 조건과 일치한다. 초기 최적 노즐 팽창비 결정에 영향을 주는 인자는 최대 압력, 추력조절비 그리고 총추력비이며 이중에서 총추력비가 가장 큰 영향을 준다.

정적연소기에서의 메탄-공기 균질혼합기의 연소특성 분석 (Combustion Characteristics Analysis of Methane-Air Homogeneous Mixture in a Constant Volume Combustion Chamber)

  • 이석영;김상진;전충환
    • 한국연소학회지
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    • 제13권3호
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    • pp.9-16
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    • 2008
  • In this study, a cylindrical constant volume combustion chamber is used to investigate the flow and combustion characteristics of methane-air homogeneous mixture under various initial charge pressure, excess air ratios and ignition times. The flame and burning speed, mean gas speed are calculated by numerical analysis to analyze the combustion characteristics. It is found that the mean gas velocity during combustion has the maximum value around 300 ms and then decreased gradually on the condition of 10000 ms, and that the combustion duration is shorten and flame speed and burning velocity have the highest value under the conditions of an excess air ratio 1.1, an initial charge pressure of 0.2 MPa and an ignition time of 300 ms in the present study. And, the initial pressure and burning speed are in inverse proportion, so that it is in agreement with Strehlow who presented that the initial pressure and burning speed are in inverse proportion when the burning speed is under 50cm/s.

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밀폐 연소실내의 메탄-공기 예혼합기의 연소 및 라디칼 특성에 관한 연구 (1) (A Study on the Characteristics of Methane-Air Premixture Combustion and Combustion Radicals (1))

  • 전충환;장영준
    • 대한기계학회논문집B
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    • 제20권2호
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    • pp.659-669
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    • 1996
  • To clarify the effects of equivalence ratio, initial pressure and temperature on the flame propagation and radicals characteristics, a series of the experimental study were conducted in a quiescent methane-air premixture using a constant volume chamber. The development of the flame was visualized following the start of ignition using high speed schlieren photo and radical images by intensified CCD camera. Combustion pressure and ion current were recorded simultaneously according to the experimental conditions which were equivalence ratio with 0.7 to 1.2, initial pressure with 0.08 MPa to 0.40 MPa and initial premixture temperature with 3l3.2K to 403.2K. The results showed that the flame speed by ion current and mass fraction burned by combustion pressure characterized the effects of flame propagation very well. And increased combustion duration due to lean combustion condition that was below equivalence ratio, 0.8 caused cycle variation and decreasing the power of engine.

와류형 고압인젝터의 초기분무의 분열 과도현상 (Transient Breakup Phenomena of Initial Spray from High-Pressure Swirl Injector)

  • 최동석;김덕줄;고장권
    • 대한기계학회논문집B
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    • 제22권8호
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    • pp.1132-1140
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    • 1998
  • The disintegration process of initial spray from high-pressure swirl injector was investigated at different injection pressures. The transient breakup phenomena that were difficult to observe at high injection pressure were easily observed at the low injection pressure of 0.4MPa. The effect of fuel remained inside a nozzle hole volume on the penetration of initial spray was also investigated. The disintegration process of initial spray could be classified four regions: the formation of mushroom shape, the first collision, the second collision, and the development of spray, The liquid film of cup shape was particularly found in the second collision region, and the growth ratio of its length and width at low and high injection pressures were compared.

고 표면적-체적 비를 가지는 소형 연소실 환경에서의 연소특성 (Combustion characteristics in small combustion chamber that has high surface to volume ratio)

  • 이대훈;최권형;권세진
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2000년도 제21회 KOSCO SYMPOSIUM 논문집
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    • pp.212-216
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    • 2000
  • Combustion phenomenon in scale-downed combustor is investigated. As the combustor volume decreases surface to volume ratio increases. for increased surface to volume ratio means increased heat loss and this increased heat loss affects reaction in combustion chamber. Plastic mini combustor is made. Stoichiometricaly premixed Hydrogen I air gas is used as fuel. Initial chamber pressure and chamber size are varied and the effects are evaluated. Peak pressure decreases with the decrease in chamber height. As initial chamber pressure decreases peak pressure decreases. And this change is more important than scale down effect till the chamber height of 1mm. With this result and further information following the experiments design parameter for micro engine can be established.

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정적연소실에서 메탄-공기 예혼합화염의 CO, $CO_2$ 및 NOx 배출 특성 (CO, $CO_2$ and NOx Emission Characteristics of Methane-Air Premixed Flame in Constant Volume Combustion Chamber)

  • 김태권;김성훈;장준영
    • 한국자동차공학회논문집
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    • 제8권2호
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    • pp.19-26
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    • 2000
  • This paper presents the effects of initial pressure of mixture on CO, $CO_2$ and NOx emissions in constant volume combustion chamber. The CO, $CO_2,O_2,N_2$ concentrations in the chamber are determined by thermal conductivity detection (Gas-chromatograph) wile the NOx concentration is measured by chemiluminescent detection (NOx Analyser). Methane-air mixture is used as premixed fuel and the measurements are taken with equivalence ratios($\phi$) varing from 0.6 to 1.3, and initial pressures of methane-air mixture varing from 0.1MPa to 0.8MPa in constant volume combustion chamber. The NOx concentration steadily increases with increasing equivalence ratio, peaks in lean flame ($\phi$=0.85~0.9), and then rapidly decreases. However, as the initial pressure of mixture is increased, the equivalence ratio corresponding to the point of peak [NOx] shifts towards leaner conditions. This is caused by a similar shift in the peak [CH], which is caused by the variation with pressure and equivalence ratio of the rate of CH production from $CH_2$ and OH. The maximum combustion pressure peaks at $\phi$ =1.05 and the $CO_2$ concentration peaks at $\phi$=0.95~1.0 while the CO concentration rises sharply at the condition of fuel-rich mixtures. This is caused by complete combustion at $\phi$=0.95.

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反復三軸壓縮試驗에 의한 砂質土의 液狀化 評價에 관한 硏究 (A Study on the Evaluation of Liquefaction of Sandy Soils by the Cyclic Triaxial Compression Test)

  • 고재만;도덕현
    • 한국농공학회지
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    • 제33권3호
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    • pp.51-62
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    • 1991
  • A comprehensive laboratory investigation of the liquefaction characteristics of Jumunjin standard sand. Seoul sand and Hongsung sand was peformed by the undrained cyclic triaxial compression test under different relative densities, confining pressures and cyclic deviator stresses. The results obtained are as follows ; 1. Liquefaction potential was dominated by the stress ratio at a given number of cycle. That is, the number of cycle required to cause initial liquefaction became samller as the stress ratio increased. 2. Liquefaction potential of a sand was infliuenced by initial relative density or void ratio. Under a given relative density. liquefaction potential of Jumunjin standard sand and Seoul sand was smaller than that of Hongsung sand. 3. The pore pressure ratio of Hongsung sand was the smallest three under a given relative density and stress ratio, and it showed higher value when the cyclic stress and the shear strain were high. 4. An excessive pore pressure ratio not found when initial shear was smaller than 0.01%, and the pore pressure ratio started to increase when initial shear became greater than 0.01%. 5. Soil texture is an important factor to cause liquefaction, and liquefaction potential decreased a the mean grain size decreased. however the sand having fine grain such as Hongsung sand showed somewhat higher liquefaction potential. 6. Based on the analysis of the specimens whose number of the cycles to cause liquefaction was 8~12, it was found that the relationship between density and stress ratio was linear. The curves for Hongsung sand was steeper than the other. 7. From the above results and the method suggested by Seed-Idriss, it may be considered that the damages by Hongsung earthquake was not directly caused by liquefaction.

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