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조한창,박정규,신현동,Cho, Han Chang,Park, Jung Kyu,Shin, Hyun Dong 대한기계학회 1999 大韓機械學會論文集B Vol.23 No.5
An experimental study was carried out in two laboratory-scale reactors to investigate the effect of heating rate on the behavior of flame front in a pulverized coal flame. Each. reactors had different heating mechanisms. For reactor A losing large heat through transparent quartz wall. pulverized coal particles were ignited by secondary air of 1050K. Flame front could be visualized through the transparent wall. Reactor B was insulated with castable refractory to minimize the heat loss through the reactor wall and accompanied with secondary air of 573K. Flame front was estimated from the gas temperature and species concentration measured using R-type thermocouple(Pt-Pt/Rh 13%) and gas chromatograph at various coal-air ratios and swirl intensities. The flame front position was closely related with the magnitude of heating rate. The heating rate for lifted flame was of the order of $10^4$ to $10^5K/s$ and for coal Ignition at least over $10^4K/s$. The heating mechanism had little impact on the extinction limits. The weak swirl number of 0.68 forced the flame front to move toward the upstream by the rapid mixing of coal and air. The primary/secondary momentum ratio was an inappropriate variable to distinct the liftoff of flame.
조한창,조길원,이용국,Cho, Han-Chang,Cho, Kil-Won,Lee, Yong-Kuk 대한기계학회 2003 大韓機械學會論文集B Vol.27 No.10
Heat regenerator occupied by regenerative materials improves thermal efficiency of combustion system through the recovery of sensible heat of exhaust gases. By using one-dimensional two-phase fluid dynamics model, the unsteady thermal flow of regenerator with spherical particles, was numerically analyzed to evaluate the heat transfer and pressure losses and to derive the design parameter for heat regenerator. It is confirmed that the computational results, such as air preheat temperature, exhausted gases outlet temperature, and pressure losses, agreed well with the experimental data. The thermal flow in heat regenerator varies with porosity, configuration of regenerator and diameter of regenerative particle. As the gas velocity increases with decreasing the cross-sectional area of the regenerator, the heat transfer between gas and particle enhances and pressure losses decrease. As particle diameter decreases, the air is preheated higher and the exhaust gases are cooled lower with the increase of pressure losses. Assuming a given exhaust gases temperature at the regenerator outlet, the regenerator need to be linearly lengthened with inlet Reynolds number of exhaust gases, which is defined as a regenerator design parameter.
분류층 석탄반응로에서 유동분포가 연소성능에 미치는 영향
조한창,신현동,CHO, Han Chang,SHIN, Hyun Dong 대한기계학회 1999 大韓機械學會論文集B Vol.23 No.8
A numerical study was carried out to analyze the effect of flow distribution of stirred part and plug flow part on combustion efficiency at the coal gasification process in an entrained bed coal reactor. The model of computation was based on gas phase eulerian balance equations of mass and momentum. The solid phase was described by lagrangian equations of motion. The $k-{\varepsilon}$ model was used to calculate the turbulence flow and eddy dissipation model was used to describe the gas phase reaction rate. The radiation was solved using a Monte-Carlo method. One-step parallel two reaction model was employed for the devolatilization process of a high volatile bituminous Kideco coal. The computations agreed well with the experiments, but the flame front was closer to the burner than the measured one. The flow distribution of a stirred part and a plug flow part in a reactor was a function of the magnitude of recirculation zone resulted from the swirl. The combustion efficiency was enhanced with decreasing stirred part and the maximum value was found around S=1.2, having the minimum stirred part. The combustion efficiency resulted from not only the flow distribution but also the particle residence time through the hot reaction zone of the stirred part, in particular for the weak swirl without IRZ(internal recirculation zone) and the long lifted flame.
구형 축열체를 사용한 축열기의 성능예측: 압력손실과 열전달의 관계
조한창,조길원,이용국 한국에너지학회 2003 에너지공학 Vol.12 No.1
본 연구에서는 배가스의 현열회수를 통해 연소기기의 열효율을 향상시키는 축열연소시스템에서 구형축열체를 이용한 축열기내 열유동을 해석할 수 있는 수치해석 코드를 개발하였다. 이를 통해 축열기내 비정상 열유동을 해석하고 축열기 길이를 포함한 축열기 형상과 축열체 구경에 따른 배열회수와 압력손실의 관계를 파악해 보았다. 수치해석은 1차원 2상 유체역학 모델을 도입하여 MacCormack방식으로 해를 얻었으며, 실험적 경향과 일치함을 알 수 있었다. 개발된 수치코드를 통해 얻은 결론은 축열기 길이가 길고 입자구경이 작으며 축열기내 유체 유속이 빠른 경우에 많은 배열을 회수할 수 있으나 압력손실이 커짐을 알 수 있었다. Heat regenerator occupied by regenerative materials improves thermal efficiency of regenerative combustion system through the recovery of heat of exhaust gaset. By using one-dimensional two-phase fluid dynamics model, the unsteady thermal flow of heat regenerator with spherical particles, was numerically simulated to evaluate the heat transfer and pressure drop and thereby to suggest the parameter for designing heat regenerator. It takes about 7 hours for the steady state of the flow field in regenerator, in which heat absorption of regenerative particle is concurrent with the same magnitude of heat desorption. The regenerative particle experiences small temperature fluctuation below 10 K during the reversing process. The performance of thermal flow in heat regenerator varies with inlet velocity of exhaust gas and air, configuration of regenerator (cross-sectional area and length) and diameter of regenerative particle. As the gas velocity increases, the heat transfer between gas and particle enhances and with the increase the pressure losses. As particle diameter decreases, the air is preheated higher and the exhaust gases are cooled more with the increase of pressure losses.
이동경계면을 갖는 연소실내에서의 입자상의 고체연료 연소장 예측
조한창,윤재건,신현동,김종욱 대한기계학회 1992 대한기계학회논문집 Vol.16 No.12
본 연구에서는 1차원, 2상 모델중 K.K.Kuo의 2상 유체역학 모델을 사용하여 유동을 수치해석하였다. Granular solid propellants having energy and fast burning rate produce great thrusts within extremely short time intervals. Thus numerical researchs prevailed rather than experimental. Using a 2-phase fluid dynamics model among 1-dimensional 2-phase models, a numerical program was set up to describe reacting flow fields, moving boundary with oscillating pressure waves and constitutive laws research. It deserves special emphasis that correlations of convective heat transfer coefficient and viscous drag force among constitutive laws are tested and discussed because slight variations of their constants make a large influence on their results. In this calculations, some of correlations make the large difference in results. Therefore constitutive laws for convective heat transfer coefficient and viscous drag force need more considerations with experiments.