• 자원리싸이클링
• /
• 제15권1호
• /
• pp.46-57
• /
• 2006

폐기물고형연료(RDF : Resused Derived Fuel)를 연료로 하는 연소기술의 개발을 위하여 기포유동층 연소로와 순환유동층 연소로, 연속연소식 연소로, 회분식 연소로 등 다양한 연소장치를 이용하여 연소 특성실험을 하였다. 여러 종류의 연소설비에서 RDF의 연소 및 배출가스 특성을 비교, 분석하였으며 RDF 전용 연소설비에 대하여 보다 깊은 연구의 기초 자료로 활용하자고 하였다. 기포 유동층 및 순환유동층연소로에서는 적정투입량과 가스공탑속도등 적정운전조건에 따라 안정적인 연소가 이루어지는 것을 확인할 수 있었다. 순환유동층 연소로에서 연소조건에 따라 연료 중의 질소성분과 연소공기 중의 산소와의 반응이 커져서 NOx의 농도가 높아지는 것을 알 수 있었으며 $SO_2$는 매우 낮은 농도로 측정되어 RDF의 유동층 연소시 거의 발생하지 않는 것으로 판단되었으며, HCl의 경우 평균 36.4ppm으로 배출허용기준치보다는 낮으나 저감대책이 필요한 것으로 판단되었다. 연속연소식 연소로와 회분식 연소로의 경우 성형 RDF와 fluff RDF를 비교 실험한 결과 높은 밀도를 가진 성형 RDF의 연소가 안정적인 열회수 측면에서 더 유리한 것을 알 수 있었으며 배가스 특성은 비슷한 값을 나타내었으며 배출가스 특성은 비슷하였다.

• 대한기계학회논문집
• /
• 제18권2호
• /
• pp.389-396
• /
• 1994

It is very important to clarify the ignition and flame propagation processes of methanol fuel in the Spark-ignition engine. High speed Schlieren photography and pressure trace analyses were used to study on combustion characteristics of methanol fuel in a constant volume chamber. Methanol-air mixtures equivalence rations from lean limit to 1.4 were ignited at initial pressure (0.1, 0.3, 0.5 MPa), temperature (313 343, 373 K) and ignition energy (40, 180 mJ). As the result of this study, we verified the characteristics such as ignition delay, effective thermal efficiency, flame propagation velocity, lean limit, ignitability and combustion duration. Obatained results are as follows. (1) The time to 10% reach of maximum pressure was 40-50% of the total combustion duration for this experimental condition hardly affected by equivalence ratio. (2) The Effective thermal efficiency, as calculated from maximum pressure was the highest when the mixture was slightly lean $({\phi} 0.8-0.9)$ and maximum pressure was the highest when the mixiture was slightly rich $({\phi} 1.2-1.2).$

• International Journal of Automotive Technology
• /
• 제8권1호
• /
• pp.19-25
• /
• 2007

This experimental study was carried out to obtain both low emissions and high thermal efficiency by rapid bulk combustion. Two kinds of experiments were conducted to obtain fundamental data on the operation of a RI engine by a radical ignition method. First, the basic experiments were conducted to confirm rapid bulk combustion by using a radical ignition method in a constant volume chamber (CVC). In this experiment, the combustion velocity was much higher than that of a conventional method. Next, to investigate the desirable condition of engine operation using radical ignition, an applied experiment was conducted in an actual engine based on the basic experiment results obtained from CVC condition. A sub-chamber-type diesel engine was reconstructed using a SPI type engine with controlled injection duration and spark timing, and finally, converted to a RI engine. In this study, the operation characteristics of the RI engine were examined according to the sub-chamber's specifications such as the sub-chamber volume and the diameter and number of passage holes. These experimental results showed that the RI engine operated successfully and was affected by the ratio of the passage hole area to the sub-chamber volume.

• 에너지공학
• /
• 제6권1호
• /
• pp.34-40
• /
• 1997

자동차 촉매인 Pd/cordierite 촉매상에서 메탄의 연소시험을 통하여 천연가스 이용기술 활용가능성에 대해서 고찰하였다. 중고온 연소에서 알맞은 비표면적 18.7$m^2$/g 을 갖으며 안정한 구조를 확인하였다. 메탄 연소 반응시 활성화에너지는 19.2 kcal/mol로써 비교적 우수한 활성을 보여주었으며, 메탄 연소 반응의 승온과 온도를 내리면서 촉매의 비활성 특성을 보여주는 활성 히스테리시스 현상을 관찰하였다. Pd/cordierite 촉매상에서 반응온도 $700^{\circ}C$이하에서 공간속도와 공연비를 변화시키면서 메탄 연소특성을 수행하였다.

• 설비공학논문집
• /
• 제15권10호
• /
• pp.835-842
• /
• 2003

A three dimensional numerical analysis has been conducted for a stoker type incinerator which has the capacity of 1.5 ton/hr. The objective of the present study is to predict the effects of swirl induced by secondary air and to find an optimal operating condition of the incinerator. In this study, combustion characteristics such as distributions of temperature, velocity and concentration of each species have been examined with various injection types of secondary air and with different flow rates of secondary air in the incinerator. It is found that the secondary air injection on the combustion process makes the path of fluid particle longer in the combustor and enhances the mixing between air and combustion gas by arousing a swirl. Therefore, the injection type of secondary air can be an important key in the design process of incinerator.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
• /
• pp.129-132
• /
• 2012

본 연구에서는 과산화수소와 케로신을 추진제로 사용하는 동축 스월형 다중 인젝터 로켓 엔진의 혼합비에 따른 연소 특성을 확인하기 위하여 설계 혼합비인 7.6을 기준으로 6.0~9.0까지 변화시켜가며 연소 실험을 수행하였다. 연소성능은 특성배기속도와 압력 섭동 값을 계산하여 평가하였다. 설계점 연소 실험을 포함하여 총 6번의 연소 실험을 수행하였고, 실험 결과 90%이상의 연소 효율을 보였으며, 압력 섭동 값은 1% 이내로 매우 안정적인 것으로 확인되었다.

• 한국분무공학회지
• /
• 제4권4호
• /
• pp.30-37
• /
• 1999

The breakup characteristics of liquid sheet formed by the liquid rocket injector has a close relation with the combustion efficiency. In this paper, basic characteristics of droplet size and velocity distribution were measured with PDPA for the Like Doublet Impinging Injector. Test variables were the angle of impact, the diameter of orifice and jet velocity. Water was used as test fluid. As a result, for impingement angle less than 90 degree, following correlations were obtained between drop size and design parameters : $D_{32}({\mu}m)=295.0{\times}V^{-0.09}\times(2\theta)^{-0.1}{\times}d^{0.072}$. For impingement angle greater than 100 degree, drop sizes were increased but eventually converged to a certain limiting value.

• 오토저널
• /
• 제14권6호
• /
• pp.39-47
• /
• 1992

The engine combustion is one of the most important process affecting performance and emissions. One effective way to improve the engine combustion is to control motion of the charge inside a cylinder by means of optimum induction system design, because the flame speed is mainly determined by the turbulence in a gasoline engine. This paper describes the measurement and characterization of mean velocity and turbulence intensity inside the cylinder of a 4-valve gasoline engine using laser Doppler velocimeter(LDV) under motoring(non-firing) conditions. Since the measured LDV data in each cycle show small cycle variation during compression stroke in the tested engine, the mean velocity and turbulence intensity are calculated by ensemble averaging method neglecting cycle variation effects. In the ensemble averaging method, the effects of the calculation window, in which velocities are assumed as the same crank angle, on mean velocity and turbulence intensity are fully investigated. In addition, the effects of measuring point on the flow characteristics are studied. With large calculation window, the mean velocity is shown to be less sensitive with respect to crank angle and turbulence intensity decrease in its absolute amplitude. When the piston approch to the top dead center of compression, the turbulence intensity is found to be homogeneous in the cylinder.

• 한국자동차공학회논문집
• /
• 제11권2호
• /
• pp.96-103
• /
• 2003

In this paper, the heat loss to the constant volume vessel wall was investigated using instantaneous heat flux sensor, schlieren visualization, pressure rise curve. And the heat loss characteristics of plasma jet ignition were compared with conventional spark ignition. In case of plasma jet ignition, the flame kernel moves toward the center of combustion vessel in the initial period of combustion, and the flame surface spread out to the vessel wall. However, in case of conventional spark ignition, the flame surface contact with combustion vessel wall in the initial period of combustion. As a result, heat loss in the combustion duration for conventional spark ignition increase faster than that of plasma jet ignition. And the combustion enhancement rate of plasma jet ignition is higher than that of conventional spark ignition, and it was found that the heat loss rate is inversely proportional to the combustion enhancement rate.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2001년도 춘계학술대회논문집D
• /
• pp.459-464
• /
• 2001

A mathematical model has been developed to describe the turbulent and reversed flow with convective heat transfer in a cylindrical combustion chamber. By using the mathematical model for high temperature flow enables the trends in overall heat transfer rates to be predicted. The model was applied to the design of the combustion chamber. The influences of the size of air inlet and inlet velocity were investigated for process optimization. Through modelling work it is found that the heat transfer rate to the chamber wall may be enhanced by adjusting the air flow and heat transfer pattern through selecting the air inlet condition. Internal plate has less influence to the heat transfer characteristics.