• 제목/요약/키워드: combustion zone

검색결과 386건 처리시간 0.022초

Slit-jet 노즐을 통과한 초음파 무화 에어로졸 화염에 정상초음파가 미치는 영향 (Effects of Ultrasonic Standing Wave on the Ultrasonically-atomized Aerosol Flame Injected through a Slit-jet Nozzle)

  • 안현종;강윤형;김정수
    • 한국추진공학회지
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    • 제24권6호
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    • pp.53-60
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    • 2020
  • 액체연료 분무 연소에서 화염 외부에 정상초음파 가진을 통해 압력장을 조절함으로써 초음파 무화액체연료 화염에 미치는 초음파 가진의 영향을 관찰하는 실험을 수행하였다. 초음파에 의해 미립화된 케로신 에어로졸화염은 초고속카메라, DSLR 그리고 슐리렌 촬영기법을 이용하여 가시화하였다. 연소시 소모된 연료량은 정밀유량측정법으로 계측하였고, 이를 통해 수송기체 공연비를 구할 수 있었다. 실험결과, 2차화염영역에 정상초음파를 가함에 따라 액체연료 에어로졸의 연소반응률이 증대되는 것을 관찰할 수 있었다.

Characteristics Evaluation on Welding Metal Zones Welded with Inconel 625 Filler Metal to Cast Steel for Piston Crown Material

  • Jeong, Jae-Hyun;Moon, Kyung-Man;Lee, Sung-Yul;Lee, Myeong-Hoon;Baek, Tae-Sil
    • Journal of Advanced Marine Engineering and Technology
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    • 제39권5호
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    • pp.542-547
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    • 2015
  • Since the oil price has been significantly jumped for several years, a heavy oil of low quality has been mainly used in the diesel engine of the merchant ship. Thus, a combustion chamber of the engine has been often exposed to severely corrosive environment more and more because temperature of the exhaust gas of the combustion chamber has been getting higher and higher with increasing of using the heavy oil of low quality. As a result, wear and corrosion of the engine parts such as exhaust valve, piston crown and cylinder head surrounded with combustion chamber are more serious compared to the other parts of the engine. Therefore, an optimum repair welding for these engine parts is very important to prolong their lifetime in a economical point of view. In this study, Inconel 625 filler metal were welded with GTAW method in the cast steel which would be generally used with piston crown material. And the corrosion properties of weld metal, heat affected and base metal zones were investigated using electrochemical methods such as measurement of corrosion potential, anodic polarization curves, cyclic voltammogram and impedance etc. in 35% $H_2SO_4$ solution. The weld metal and base metal zones exhibited the highest and lowest values of hardness respectively. Furthermore, the corrosion current density of the weld metal zone revealed the lowest value, having the highest value of hardness. The corrosive products with red color and local corrosion like as a pitting corrosion were considerably observed at the base metal zone, while these morphologies were not wholly observed in the weld metal zone. In particular, the polarization characteristics such as impedance, polarization curve and cyclic voltammogran associated with corrosion resistance property were well in good agreement with each other. Consequently, it is suggested that the mechanical and corrosion characteristics of the piston crown can be predominantly improved by repair welding method using the Inconel 625 electrode.

희박연소를 이용한 가스터빈 연소기의 저 $NO_{x}$ 특성 (The Low $NO_{x}$ Characteristics of a Lean Premixed Gas Turbine Combustor)

  • 손민규;안국영;김한석;김용모
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.66-70
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    • 2001
  • The combustion characteristics have been investigated to develop the low $NO_{x}$ gas turbine combustor. The lean premixed combustion technology was applied to reduce the $NO_{x}$ emission. Also, the conventional combustor was designed and tested for the baseline of low $NO_{x}$ combustor performance. The test was conducted at the condition of high temperature and ambient pressure. The combustion air which has the temperature of 500K were supplied to the combustor through the air preheater. The temperature and emissions of $NO_{x}$ and CO were measured at the exit of combustor. The premixing chamber can be operated very lean condition of equivalence ratio around 0.35. The $NO_{x}$ was decreased with decreasing the equivalence ration. The CO was decreased with decreasing the equivalence ratio, but the CO was increased with decreasing the equivalence ratio below 0.45. But, at the very lean condition of equivalence ratio below 0.35 both NOx and CO were increased because of the flame unstability. The $NO_{x}$ was decreased slightly and CO was increased with increasing inlet air flowrate. This results can be used to determine the size of combustor. The low $NO_{x}$ combustor has lower values of $NO_{x}$ and CO compared with conventional one. Consequently the performance of combustor shows the possibility of the application to the gas turbine system.

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자체반응열 고온합성법을 이용한 Titanium Carbonitride의 합성에 관한 연구 (A Study on the Synthesis of Titanium Carbonitride by SHS(Self-propagating High-temperature Synthesis) Method)

  • 하호;황규민;이희철
    • 한국세라믹학회지
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    • 제31권6호
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    • pp.637-642
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    • 1994
  • Using SHS(Self-propagating High-temperature Synthesis) method, the optimum synthetic condition of titanium carbonitride was established by controlling the parameters such as relative density of mixture (Ti+C), nitrogen pressure, additive amounts of titanium hydride(TiH1.924) and protecting heat loss. Under 1 atm nitrogen pressure, nitridation ratio with changing relative density of the sample compacts has a maximum (87.2%) at about 55%, and in the case of enveloping the pellet with a quartz tube, the highest nitridation ratio of 90% was obtained at about 68%. At relative density of 55%, nitridation ratio with the nitrogen pressure has a miximum (87.3%) at 7 atm. As the amounts of additive titanium hydride increased, nitridation ratio decreased at below 7 atm nitrogen pressure and, increased at above this pressure until percent of addition percent reached 15 wt% and decreased abruptly upon futher increases in titanium hydride. In the synthesis of TiCxNy by combustion reaction, heat transfer from combustion zone to preheating zone and nitrogen gas penetration into the compact were found to be important factors affecting the TiCxNy formation. It was difficult to obtain high nitridation ratio when the conbustion temperature was either too high or too low, and it seems that the retention of high temperature after a combustion wave sweeped through the reactant mixture pellet is critical to obtain a satisfactory nitridation ratio.

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모형 가스터빈 연소기의 입구 형상변화에 따른 연소 불안정성에 관한 LES 연구 (LES Studies on the Combustion Instability with Inlet Configurations in a Model Gas Turbine Combustor)

  • 황철홍;이창언
    • 대한기계학회논문집B
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    • 제32권5호
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    • pp.342-350
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    • 2008
  • The effects of combustion instability on flow structure and flame dynamics with the inlet configurations in a model gas turbine combustor were investigated using large eddy simulation (LES). A G-equation flamelet model was employed to simulate the unsteady flame behaviors. As a result of mean flow field, the change of divergent half angle($\alpha$) at combustor inlet results in variations in the size and shape of the central toroidal recirculation (CTRZ) as well as the flame length by changing corner recirculation zone (CRZ). The case of ${\alpha}=45^{\circ}$ show smaller size and upstream location of CTRZ than those of $90^{\circ}$ and $30^{\circ}$ by the development of higher swirl velocity. The flame length in the case of ${\alpha}=45^{\circ}$ is shorter than other cases, while the case of ${\alpha}=30^{\circ}$ yields the longest flame length due to the decrease of effective reactive area with the absence of CRZ. Through the analysis of pressure fluctuation, it was identified that the case of ${\alpha}=45^{\circ}$ shows the largest damping effect of pressure oscillation in all configurations and brings in the noise reduction of 2.97dB, compared to that of ${\alpha}=30^{\circ}$ having the largest pressure oscillation. These reasons were discussed in detail through the analysis of unsteady phenomena related to recirculation zone and flame surface. Finally the effects of flame-acoustic interaction were evaluated using local Rayleigh parameter.

이중 콘형 부분 예혼합 GT 노즐의 다단 연소특성 (Characteristics of Multi staged Combustion on a Double-cone Partial Premixed Nozzle)

  • 김한석;조주형;김민국;황정재;이원준
    • 한국가스학회지
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    • 제24권1호
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    • pp.49-55
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    • 2020
  • 산업용 혹은 발전용 가스터빈에 사용되는 이중 콘형 예혼합 연소기의 다단 연소 특성을 이해하기 위하여 실험적연구를 수행하였다. 이를 위하여 기존에 모두 경사면에 공급되는 연료를 콘부분으로 일부 할애하는 방식으로 다단연소 방식을 구성하였으며 콘에서 분사되는 연료공급은 축방향과 콘 경사면 방향으로 하였다. 다단연소 연소특성을 이해하기 위하여 콘에서의 연료 분사 방향과 연료 분배율 변화에 대한 NOx와 CO의 배출 농도 그리고 벽면 온도분포를 측정하였다. 그 결과 총 연료에 대한 콘으로의 분배율이 3%인 경우 콘에서의 연료 분사방향에 관계없이 노즐내의 예혼합 영역에서 연료가 공기와 균일하게 혼합됨으로서 연소영역의 고온점 감소에 의하여 NOx 배출 농도가 감소된다. 그러나 콘에서 축방향으로 분사되는 연료분배율이 8%로 증가하는 경우 노즐 내부 예혼합 영역으로의 화염 역화로 인하여 NOx의 배출농도가 오히려 증가하게 된다.

모형 가스터빈 연소기에서 스월수에 따른 유동 특성에 관한 실험적 연구 (Experimental Study of Flow Characteristics with Swirl Number on Dump Combustor)

  • 박재영;한동식;김한석;송주헌;장영준;전충환
    • 에너지공학
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    • 제20권4호
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    • pp.338-345
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    • 2011
  • 희박예혼합 가스터빈 연소기에 적용되는 스월 유동은 연소효율증가와 배기가스저감을 목적으로 적용된 것로 연소기 내 유동장의 전단층생성에 의한 재순환영역이 생성되게 한다. 이러한 재순환영역은 연소가스 재순환에 의한 화염온도와 화염길이를 낮추는 효과를 가지고 있다. 또한 희박연소에서 연소불안정성 억제효과도 있다. 본 연구에서는 모형가스터빈연소기에서 스월러를 이용하여 스월유동을 유도하고, 연소기 노즐에서 평균속도가 일정 할 때의 스월수 증가에 따른 유동장의 속도분포 특성을 분석하였으며 이때 PIV 계측 실험과 난류통계기법을 이용하여 난류인자들을 도출하였다. 스월수의 증가는 연소기 내부 유동장의 형태가 바뀌게 되고, 재순환영역의 위치가 연소기 노즐방향으로 이동하게 되어 화염길이를 줄여 주며, 난류강도와 난류길이 스케일이 감소하게 되어 에디의 크기가 작아짐을 확인하였다.

디젤 연소 전략에 따른 배기가스 및 탄화수소 종 분석 (Diesel Combustion Strategies Effect on Exhaust Emissions and Hydrocarbon Species)

  • 한만배
    • 대한기계학회논문집B
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    • 제36권7호
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    • pp.759-765
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    • 2012
  • 1.7L 커먼레일 직접분사 디젤 엔진을 이용하여 1500rpm 3.9bar BMEP 조건에서 세가지 연소 전략에 따른 배기가스 배출 특성 및 탄화수소 종 분석을 수행하였다. 첫째 전략은 EGR 을 사용하지 않고 연료 분할 분사를 이용하는 방법(split injection), 둘째는 적절한 EGR 적용 및 단일 연료분사 방법(single-1)이며 셋째는 다량의 EGR 및 레일 압력 증대 등을 통한 저온디젤연소(single-2)이다. 본 실험 조건으로부터 split injection 방법과 single-1 방법은 PM-NOx 상반 관계를 보였고, single-2 방법은 PM-NOx 상관관계에서 벗어나 PM 및 NOx 동시 저감이 가능하였다. 탄화수소 종 분석 결과, THC 배출 경향과 동일하게 탄소번호에 관계없이 split injection 이 가장 적은 배출을 보였고, single-1 그리고 single-2 의 순서로 많이 배출하였다. 메탄, 아세틸렌 및 CO 의 THC 에 대한 비율은 공연비가 농후해 짐에 따라서 증가하였고 이는 공연비가 농후에 따른 연소 영역에서 산소 농도 감소로 열해리가 증가하였기 때문이다.

Computational Analysis of the Effects of Spray Parameters and Piston Shape on Syngas-Diesel Dual-Fuel Engine Combustion Process

  • Ali, Abubaker Ahmed M.M.;Kabbir, Ali;Kim, Changup;Lee, Yonggyu;Oh, Seungmook;Kim, Ki-seong
    • 한국분무공학회지
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    • 제23권4호
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    • pp.192-204
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    • 2018
  • In this study, a 3D CFD analysis method for the combustion process was established for a low calorific value syngas-diesel dual-fuel engine operating under very lean fuel-air mixture condition. Also, the accuracy of computational analysis was evaluated by comparing the experimental results with the computed ones. To simulate the combustion for the dual-fuel engine, a new dual-fuel chemical kinetics set was used that was constituted by merging two verified chemical kinetic sets: n-heptane (173 species) for diesel and Gri-mech 3.0 (53 species) for syngas. For dual-fuel mode operations, the early stage of combustion was dominated by the fuel burning inside or near the spray plume. After which, the flame propagated into the syngas in the piston bowl and then proceeded toward the syngas in the squish zone. With the baseline injection system and piston shape, a significant amount of unburned syngas was discharged. To solve this problem, effects of the injection parameters and piston shape on combustion characteristics were analyzed by calculation. The change in injection variables toward increasing the spray plume volume or the penetration length were effective to cause fast burning in the vicinity of TDC by widening the spatial distribution of diesel acting as a seed of auto-ignition. As a result, the unburned syngas fraction was reduced. Changing the piston shape with the shallow depth of the piston bowl and 20% squish area ratio had a significant effect on the combustion pattern and lessened the unburned syngas fraction by half.

선회연소기를 이용한 산소부화연소화염의 연소 특성 연구 (Characteristics of Oxygen-Enhanced Flame in Swirl Burner)

  • 이윤원;안국영;김한석;이창언
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.149-154
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    • 2001
  • The emission characteristics, flame stability, the composition of the flame zone and temperature profile were studied experimentally. The compositions of oxydant were varied by substituting $N_2$ with $CO_2$ at the constant $O_2$ concentration. Results showed that flame became unstable due to the high heat capacity, low transport rate and strong radiation effect of $CO_2$ in comparison with those of $N_2$. The reaction zone was cooled, broadened, as the conversion ratio of $CO_2$ to $N_2$ was increased. Temperature has a large effect on the NOx emission. The concentration of NOx in flue gas decreased due to the decreased temperature of reaction zone. It was also shown that the reaction was delayed by the cooling effect. As the conversion ratio of $CO_2$ to $N_2$ was increased, the emission of CO and the higher temperature zone increased due to the decrease of reaction rate by the cooling effect.

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