• 한국연소학회지
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• 제15권3호
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• pp.1-7
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• 2010

Edge flames have been interested as a basic structure that is concerned to flame stabilization and re-ignition of non-premixed flames. The edge flame consists of a lean premixed flame, a rich premixed flame, and a diffusion flame. In order to investigate fundamental structures of the edge flames at the conditions near the flammability limits, edge flames were stabilized within a heated narrow channel. Highly diluted partially premixed methane was used, and the flow rates of air and the partially premixed mixture were controlled. Various flame behaviors, including a transition between ordinary edge flames and premixed flames, were observed. Flame stabilization characteristics were examined as well. All flame stabilization conditions in this study showed a similar trend: characteristic time scales were inversely proportional to the equivalence ratio defined at the burner inlet. Finally, an interesting flame structure having a weak diffusion branch enveloped by a closed premixed branch was found near the flammability limits even in a fuel-air mixing layer. This structure was named as a "flame-drop" and the importance of this structure was first suggested.

• 대한기계학회논문집B
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• 제21권4호
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• pp.518-524
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• 1997

Experimental studies on combustion phenomena within a porous ceramic burner are reported. Main interest of the present work is to investigate fundamental flame behaviors and their effects on the burner operation. Due to high thermal capacity of the porous ceramic materials, the response of flame to burning condition changes is slow and thus to have a stabilized flame is quite difficult and takes much time. It is found that the temperature profile obtained at downstream of the flame zone is not much sensitive to the movement of flame and the speed of flame movement is less than 0.1 mm/sec for the conditions tested. With the premixed LPG/air flame imbedded within the porous ceramic burner, stable combustion regions and unstable combustion regions leading to blowoff or flashback phenomena are observed and mapped on flow velocity versus equivalence ratio diagram. For the development of burner operation technique which is more practical and safe, intermittent burning technique, where the fuel or/and air is supplied to the burner intermittently, is proposed as one of the flame control methods for the porous ceramic burner and tested in this study. Through the experiment, it is realized that the proposed method is acceptable in respect to burner performance and give much flexibility in the operation of porous ceramic burner.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.853-858
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• 2001

The knowledge of flame structure is essential for control of combustion instability phenomena. Some results of an experimental study on mechanism of naturally occurring combustion oscillations with a single dominant frequency are presented. Tests were conducted in a laboratory-scale dump combustor at atmospheric pressure. Sound level meter was used to track the pressure wave inside the combustor. The observed instability was a longitudinal mode with a frequency of $\sim341.8Hz$. Instability map was obtained at the condition of inlet temperature of $360^{\circ}C$, mean velocities of $8.5\sim10.8m/s$ and well premixed mixture. It showed that combustion instability was susceptible to occur in the lean conditions. In this study, unstable flame was observed from stoichiometric to 0.7 in overall equivalence ratio. At selected unstable conditions, phase-resolved OH chemiluminescence images were captured to investigate flame structure with various mean velocities. As mean velocity is increased, the flame grows and global heat release was changed. Due to these effects, combustion instability can be maintained at more lean air-fuel ratio. Also, these results give an insight to the controlling mechanism for an increasing heat release at maximum pressure.

• 청정기술
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• 제24권4호
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• pp.323-331
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• 2018

실험실 규모 기포 유동층 반응기를 이용한 하수 슬러지와 석탄 및 우드 펠렛의 혼소 실험 및 회분 분석을 통한 슬래깅 성향을 살펴보았다. 연료는 일반 건조 및 수열탄화를 통해 제작된 하수 슬러지와 아역청탄, 우드 펠렛이 적용되었다. 연소 실험은 당량비 및 산화제 유량, 초기 온도를 고정하고 2종의 하수 슬러지 연료와 석탄 또는 우드 펠렛을 발열량 기준 50 : 50 비율로 혼합한 총 4개의 조건에 대해 반응기 온도 및 배가스 조성을 측정하였다. 배가스 중 $NO_x$는 모든 조건에서 대부분 NO의 형태로 400 ~ 600 ppm 범위에서 측정되었다. $SO_2$는 원료 내 황 함량을 고려하면 하수 슬러지의 투입량이 큰 영향을 미쳤을 것으로 예상되는 가운데 수열탄화 연료가 일반 건조 연료에 비해 다소 낮은 경향을 보였다. 비산 회분 조성 분석 결과 하수 슬러지 연료가 슬래깅/파울링 가능성을 높일 것으로 생각되며, 수열탄화 연료가 일반 건조 연료에 비해 상대적으로 양호한 결과를 보일 것으로 예상되었다.

• 한국화재소방학회논문지
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• 제33권1호
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• pp.30-38
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• 2019

메탄 연료성분이 가득 찬 축소 구획실을 대상으로 개구부에서 유입된 공기와 내부 연료의 혼합특성과 백드래프트 발생특성을 규명하기 위해 대와동모사를 수행하였다. 통상의 문 형태(Door)와 가로 형태의 문이 벽면 상단($Slot_U$), 중단($Slot_M$) 및 하단($Slot_L$)에 있는 구획실의 4가지 개구부 조건들에 대해서 검토를 수행하였다. 점화원이 없을 경우 구획실 내부로 유입되는 산소의 양과 외부로 유출되는 연료의 양은 Door > $Slot_U$ ~ $Slot_M$ > $Slot_L$의 순서로 크지만 $Slot_U$의 경우가 구획실 내부에서 연료와 산소가 전체적으로 가장 잘 혼합되었고 $Slot_L$의 경우에는 연료와 산소가 층을 이루어 혼합이 가장 잘 이루어지지 않는 것으로 나타났다. 구획실 내 산소량과 연료량으로 정의되는 총괄당량비는 구획실에서 발생하는 백드래프트의 강도와 잘 연관되지 않음을 확인하였다. 백드래프트 발생 시의 구획실 내부의 최고 압력은 혼합이 가장 잘 이루어진 $Slot_U$가 가장 높게 나타났으며 $Slot_L$의 경우에는 압력상승이 낮아 백드래프트가 발생하지 않았다. 백드래프트 발생 시 Door와 $Slot_M$ 조건에서의 최고 압력값은 $Slot_U$ 다음 순서로 나타났으며, 각 조건들의 최고압력은 백드래프트 발생순간까지의 총 열발생량과 잘 연관되어 설명될 수 있었다.

• Korean Chemical Engineering Research
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• 제53권6호
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• pp.783-791
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• 2015

바이오매스 가스화 공정을 위하여 내경이 0.1 m이고 높이가 1.2 m인 유동층 반응기에서 수증기 및 촉매의 첨가가 프로듀서가스(Producer gas)에 미치는 영향을 파악하였다. 가스화 장치는 유동층 반응기, 연료공급 장치, 사이클론, 2개의 냉각기, 수증기 발생장치 및 가스분석기로 구성하였다. 층물질 및 촉매물질로 평균입자크기 $380{\mu}m$의 비구형 silica sand 와 평균입자 $356{\mu}m$ 크기의 소성된 백운석을 사용하였다. 사용된 바이오매스는 국산 우드펠릿(Korea woody pellet) 및 동남아 팜 부산물인 EFB(empty fruit bunch)를 펠릿 형태로 가공하여 사용하였다. 실험 고정 변수로는 연료공급량 50 g/min(EFB), 38 g/min(KWP) 반응 온도 $800^{\circ}C$, ER(equivalence ratio) 0.25로 설정하였다. 조업 변수로 촉매인 소성된 백운석을 층물질 0~100 wt%의 혼합비로 사용하였다. 가스화매체로 공기 또는 Air-Steam을 사용하였다. 이때 수증기 첨가량은 SBR(steam to biomass ratio) 기준 0.3으로 하였다. 생성된 가스의 조성, 타르(Tar) 및 저위발열량을 측정하였다. 실험의 결과로 소성된 백운석은 모든 실험조건에서 프로듀서가스 타르의 함량을 감소시키며 최대 67.3 wt%의 감소율을 보였다. 저위발열량은 공기가스화에서 소성된 백운석 첨가량이 증가할수록 감소하였다. 하지만 Air-steam 가스화에서 저위발열량은 변화가 적거나 오히려 소폭 증가한 경향을 보였다.

• 대한기계학회논문집B
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• 제23권9호
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• pp.1172-1177
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• 1999

Comparisons of measured turbulence properties in the unburned gas region of turbulent premixed flame stabilized by pilot flame, in cases of combusting and non-combusting flow conditions, are presented. Methane-air premixed jet at fuel equivalence ratio of 0.6 and 1.0 and Reynolds number of 7,000 was diagnosed using two-color laser velocimeter to obtain turbulence statistics. Same set of measurements was repeated at 21 locations within the unburned gas region of both combusting and non-combusting conditions. Velocity data were analyzed to evaluate the spatial distribution of turbulence properties including Reynolds stress, probability densities, joint probability densities and auto correlations. Contrary to assumptions of current theoretical models, significant influence of flame was observed in every property that was studied in the present investigation. The effective viscosity increased ten-fold when flame was on from cold flow values. The effect of mixing on joint probability as well as in turbulence intensity was suppressed by the flame. The measurements suggest that common assumptions of premixed flame model may result in sizable error in prediction of flame length and temperature distribution in near-field.

• 한국수소및신에너지학회논문집
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• 제17권3호
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• pp.255-262
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• 2006

To develop a hydrogen fueled engine with external mixture which uses in high reliability, low cost and low pressure, the single cylinder research engine with MCVVT(Mechanical Continuous Variable Valve Timing) system is developed and its basic characteristics analyzed. The MCVVT developed has high reliability and the valve timing change is possible in wide range continuously. Though the mechanical loss due to MCVVT system is increased a little, back-fire suppression research for valve overlap period is no difficulty. It's also confirmed that the hydrogen-fueled engine has lower torque and is possible high lean burn. As fuel-air equivalence ratio is high, as thermal efficiency is remarkable increasing.

• 대한기계학회논문집
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• 제19권8호
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• pp.2022-2029
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• 1995

The experiment was performed by using the condenser discharge ignition device in a constant volume combustion chamber for high pressure, equivalent to the TDC of spark ignition engine, which makes the forced turbulent field possible. The conclusions obtained under various initial pressures, initial temperatures, and turbulent conditions of the methanol-air mixture are as follows : As initial pressure, initial temperature of the mixture, and the ignition energy increase, the inflammability limit expands, but the lean inflammability limit decreases as turbulence intensity increases. Combustion duration is shorter in the case of the lower initial pressure, the higher initial temperature, an equivalence ratio of 1.1-1.2, and even though turbulence intensity increases up to optimum value. Maximum combustion pressure increases in turbulent ambience under the same mixture condition, only in the case each optimum turbulence intensity exists under every condition. As the turbulence intensity increases .tau.$_{10}$ proportion increases while the .tau.$_{pr}$ proportion decreases....

• 대한기계학회논문집B
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• 제32권9호
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• pp.659-668
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• 2008

Combustion instability has been considered as very important issue for developing gas turbine and rocket engine. There is a need for fundamental understanding of combustion instability. In this study, combustion instability was numerically and experimentally investigated in a dump combustor with bluff body. The fuel and air mixture had overall equivalence ratio of 0.9 and was injected toward dump combustor. The pressure oscillation with approximately 256Hz was experimentally obtained. For numerical simulation, the standard k-$\varepsilon$ model was used for turbulence and the hybrid combustion model (eddy dissipation model and kinetically controlled model) was applied. After calculating steady solution, unsteady calculation was performed with forcing small perturbation on initial that solution. Pressure amplitude and frequency measured by pressure sensor is nearly the same as those predicted by numerical simulation. Furthermore, it is clear that a combustion instability involving vortex shedding is affected by acoustic-vortex-combustion interaction. The phase difference between the pressure and velocity is $\pi$/2, and that between the pressure and heat release rate is in excitation range described by Rayleigh, which is obvious that combustion instability for the bluff body combustor meets thermoacoustic instability criterion.