• 한국산학기술학회논문지
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• 제21권8호
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• pp.401-406
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• 2020

자동차에서 배출되는 배기가스 중 질소산화물은 요사이 문제가 되는 미세먼지의 주요 요인 중 하나이다. 질소산화물(NOx)은 고온 조건에서 연소가 진행될 때 발생하므로 연소시 온도를 낮추는 방법으로 발생을 억제하고 있다. 자동차에서는 일반적으로 배기가스 재순환(EGR)을 사용하여 연소 온도를 낮추는 방법으로 감소시킨다. 그러나 EGR 비율이 높아질수록 NOx의 양은 저감되나 연소 안정성의 하락으로 인한 불완전연소 가능성의 증가로 일산화탄소와 미연탄화수소의 양이 증가하여 오히려 오염물질이 증가하는 문제를 발생시킬 수 있다. 여기에서는 연료 입자에 음파를 조사하여 연료 입자의 운동성을 향상시켜 연소가 원활히 진행되게 하여 연소의 안정성을 향상시키는 방안에 대하여 해석적 및 실험적 방법으로 연구하였다. 해석적 방법으로는 유동해석 소프트웨어를 사용하여 연료 입자에 다양한 주파수의 음파를 조사하여 연료 입자의 움직임 변화에 대한 연구를 진행하였다. 해석 결과, 작은 연료 입자의 조건에서는 고주파의 음파에 의해 영향을 많이 받고, 연료 입자가 큰 조건에서는 저주파의 음파에 의해 영향을 많이 받아 운동성이 증가함을 알 수 있었다. 실험적 방법으로는 연소실을 구성하여 정해진 당량비 조건에서 연소시키며 다양한 주파수의 음파를 조사하며 연소실내 압력을 측정하는 연구를 진행하였다. 측정된 압력으로부터 열방출량을 계산하면 연소의 진행 상황에 대한 정보를 얻을 수 있는데, 실험 결과 초기 연소시 상대적 저주파 조사 조건에서 열방출량이 증가한 것을 확인할 수 있었다.

• 한국연소학회지
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• 제17권1호
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• pp.22-29
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• 2012

The detachment stability characteristics of syngas $H_2$/CO jet attached flames were studied. The flame stability was observed while varying the syngas fuel composition, coaxial nozzle diameter and fuel nozzle rim thickness. The detachment stability limit of the syngas single jet flame was found to decrease with increasing mole fraction of carbon monoxide in the fuel. In hydrogen jet flames with coaxial air, the flame detachment stability was found to be independent of the coaxial nozzle diameter. However, velocities of appearance of liftoff and blowout velocities of lifted flames have dependence. At lower fuel velocity range, the critical coaxial air velocity leading to flame detachment increases with increasing fuel jet velocity, whereas at higher fuel velocity range, it decreases. This increasing-decreasing non-monotonic trend appears for all $H_2$/CO syngas compositions (50/50~100/0% $H_2$/CO). To qualitatively understand the flame behavior near the nozzle rim, $OH^*$ chemiluminescence imaging was performed near the detachment limit conditions. For all fuel compositions, local extinction on the rim is observed at lower fuel velocities(increasing stability region), while local flame extinction downstream of the rim is observed at higher fuel velocities(decreasing stability region). Maximum values of the non-monotonic trends appear to be identical when the fuel jet velocity is normalized by the critical fuel velocity obtained in the single jet cases.

• 한국항공우주학회지
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• 제34권12호
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• pp.48-58
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• 2006

횡단류에 분사되는 액체 제트의 분무 및 연소 특성에 대한 수치적 연구를 수행하였다. 수치 계산을 위해 3차원의 분무 및 화학반응 유동 해석에 유용한 KIVA 코드를 횡단류에서의 분무 해석에 적합하도록 수정하여 사용하였다. 액주의 분열과 리거먼트 및 액적의 분열 현상을 해석하기 위하여 wave 모델과 KH-RT hybrid 모델이 사용되었다. 침투길이는 유입공기의 속도가 감소하거나 분사속도가 증가함에 따라 증가하였다. 유입공기의 속도가 증가할수록 계산결과의 오차가 크게 발생함을 알 수 있었다. 연소 특성에 대한 수치 해석으로 연소실 내부의 화염전파 형상과 국부지역에서의 온도및 공해 배출량에 대한 결과를 얻었다.

• 대한기계학회논문집
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• 제13권3호
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• pp.508-516
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• 1989

본 연구는 석탄의 맥동연소과정을 비맥동연소와 빅교실험을 하여 연소특성 을 가시적으로 관찰하고 연소율 등의 연소특성을 구하며 고체연료의 맥동연소과정을 밝히고 맥동연소기 개발의 기초자료를 얻는데 목적을 두었다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.3062-3067
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• 2007

HVOF thermal spray guns are now being widely used to produce protective coatings, on the surfaces of engineering components. HVOF technology employs a combustion process to heat the gas flow and melt the coating materials which are particles of metals, alloys or cermets. Particle flow which is accelerated to high velocities and combustion gas stream are deposited on a substrate. In order to obtain good quality coatings, the analysis of torch design must be performed. The reason is that the design parameters of torch influence gas dynamic behaviors. In this study, numerical analysis is performed to predict the gas dynamic behaviors in a HVOF thermal spray gun with various torch shapes. The CFD model is used to deduce the effect of changes in nozzle geometry on gas dynamics. Using a commercial code, FLUENT which uses Finite Volume Method and SIMPLE algorithm, governing equations have been solved for the pressure, velocity and temperature distributions in the HVOF thermal spray torch.

• 한국전산유체공학회지
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• 제16권2호
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• pp.56-61
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• 2011

Numerical study is conducted to design the high temperature heat exchanger of Stirling engine by using the commercial CFD solver, FLUENT. The Fin-tube type of heat exchanger is designed as a reference model by considering the type of engine which is ${\beta}$-configuration. To find the optimal design of heat exchanger in heat transfer capacity numerical calculation is conducted by changing the shape, the number, and material of reference model in three-dimensional combustion field. Adjusted one-way constant velocity of working fluid that is helium is considered as the representative velocity of oscillating flow. The optimal design of heat exchanger considering the heat transfer capability is suggested by using the calculation results.

• Journal of Advanced Marine Engineering and Technology
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• 제24권1호
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• pp.88-93
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• 2000

In this study, the mixing process of two-phase flow generated by two jets with height difference is analyzed. The primary jet is jetted on the condition of the state mixed pulverized solid particles with air. The height difference between the main jet and the secondary jet is changed into three kinds(0, 32.5, 47.5mm). The velocity vector field, concentration field and turbulent properties of solid particles are measured by using 3-Dimensional Particles Dynamics Analyzer. As the height difference of two jets through the two nozzles increases, the solid particle recirculation zone and the dense zone in the combustion chamber become large. The solid particle concentration at the center of the combustion chamber gets dense because the particle velocity remains slow due to the existence of the solid particle recirculation zone. The particle concentration in the combustion chamber can also be influenced by the hight difference of two jets.

• 한국해양공학회지
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• 제10권3호
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• pp.117-124
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• 1996

A fluidized bed combustion chamber is widely used to incinerate waste material. The most important factor designing the incinerator is the flow characteristics in a fluidized bed, because combustion efficiency is influenced by the flow characteristics. This paper has invesitigated the flow characteristics of bubbles in fluidized bed by means of meassuring a pressure fluctuation in the fluidized bed. A pressure probe system has used to measure the pressure. The data concerned with bubble rising velocity, bubble size, distribution of bubbles and frequency of bubble generation or decay are obtained to find the flow characteristics of bubbles in the fluidized bed. The result obtained from this experimental study can be used to design the fuel feeding system of fluidized bed combustion type incinerator. And it is possible to predict the mixing of waste material and fluidizing material.

• 한국안전학회지
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• 제9권3호
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• pp.60-66
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• 1994

The purpose of this study is to compare the combustability of the formed high density polyethylene (HDPE) with the low density polyethlyene(LDPE). That is, the easiness of ignition is examined by using the methods with Oxygen Index(OI) Tester and ventilation parameter, and the combustion velocity of these polyethylenes is measured by changing the size and shape of opening area. As the result of it, the oxygen index of HDPE, in a ignition, is required more than LDPE. Then, the concentration distribution of CO by combustion is increased when the opening area is small, but, in the same opening area, LDPE tends to increase more than HDPE. In addition, as the ratio of height to width of opening area is increased, combustion velocity becomes faster relatively. In consequence, when it is generally considered, the combustability of LDPE is better than HDPE.

• 한국대기환경학회지
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• 제12권2호
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• pp.131-139
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• 1996

The developent of ceramic combustor is being increased beca- use of the excellent physical properties of ceramic material, that is, high-resistant strength, high emissivity power and high corrosin-resistance. Ceramic combustor has been interested in the application of ultra-lean combustion for low NO$_{x}$ emission and gaseuos waste incineration with good combustion. This experimental study was conducted to investigate the combustion and emission characteristics of wall recess type ceramic combustor with equivalence ratio, mixture flow velocity and wall recess depth as parameters. The results in this study are as follows: 1. Wall recess played a important role to extend flame stability region. 2. The peak temperature of gas was peoportional to equivalence ratio, mixture flow velocity and wall recess depth. 3. The static pressure of mixing chamber and inlet temperature depended on the position of flame zone. 4. NO reduction was achieved by lean mixture without lower combustibility.y.