• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1998년도 춘계학술대회논문집; 용평리조트 타워콘도, 21-22 May 1998
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• pp.492-497
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• 1998

Thermoacoustic oscillation is a significant problem in cylindrical-type combustors such as common internal combustion engines, industrial furnaces, gas turbine, etc. This kind of low frequency oscillation can give rise to serious troubles such as the destruction of system or producing of a strong noise. Accurate numerical simulation of thermoacoustic phenomena is a complex and challenging problem. Especially, considering the reaction of mixture intensifies the difficulty of analysis. Like as other simulations of the aerodynamics and aeroacoustics, direct computation of thermoacoustic phenomena requires that the Navier-Stokes equations be solved using accurate numerical differentiation and time-marching schemes, with non-reflecting boundary conditions. In this study,, numerical approach aims at qualitative analysis and efficient prediction of problem, not at the development of an accurate scheme. Overally speaking, numerical prediction is reasonably matched with experimental result.

• 한국음향학회지
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• 제18권7호
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• pp.56-66
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• 1999

일반 내연기관이나 산업용로, 로켓 엔진 등의 기본적인 형상이라고 할 수 있는 관형 연소기에서 발생하는 연소 소음은 열-음향 되먹임 현상에 의해 야기되는 형태가 지배적이며. 심할 경우 시스템의 파괴를 야기할 수도 있는 중요한 문제이다. 본 연구에서는 열-음향 진동중에서도 열-기인 음향 진동으로 분류될 수 있는 현상에 초점을 맞추어 유동장, 음향장 및 연소 반응을 수치적으로 해석하여 여러 주어진 조건에 따른 정상적인 해석뿐만 아니라 음압 수준이나 기본 주파수 예측과 같은 정량적인 결과 도출을 효과적으로 수행할 수 있는 수치적 기법의 개발을 목적으로 하였다. 다양한 당량비를 가진 혼합기에 대해 수치 해석을 수행한 결과 실험 측정치의 경향과 잘 일치할 뿐만 아니라 정량적인 면에서도 상당히 정확한 예측을 할 수 있음을 확인하였다.

• 한국수소및신에너지학회논문집
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• 제19권3호
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• pp.217-225
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• 2008

A new micro reformer system consisted of a micro reformer, a microcombustor and a micro evaporator was studied experimentally and computationally. In order to satisfy the primary requirements for designing the microcombustor integrated with a micro evaporator, i.e. stable burning in a small confinement and maximum heat transfer through a wall, the present microcombustor is simply cylindrical to be easily fabricated but two-staged (expanding downstream) to feasibly control ignition and stable burning. Results show that the aspect ratio and wall thickness of the microcombustor substantially affect ignition and thermal characteristics. For the optimized design conditions, a premixed microflame was easily ignited in the expanded second stage combustor, moved into the smaller first stage combustor, and finally stabilized therein. A micro reformer system integrated with a modified microcombustor based on the optimized design condition was fabricated. For a typical operating condition, the designed micro reformer system produced 22.3 sccm hydrogen (3.61 W in LHV) in an overall efficiency of 12%.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.466-471
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• 2004

In gas turbines, excess air for combustion is available and therefore lean premixed combustion is the most promising approach to the significant reduction of thermal NOx emissions. At lean conditions, however, flame stability is inherently worse and hence combustion tends to be incomplete. Efforts have been devoted toward extending the operating range of complete combustion at leaner conditions. One of them is the lean-lean two-stage combustion where lean to ultra-lean secondary mixtures are mixed with the hot burned gas from the primary stage. Conventional flame combustion or flameless reaction are initiated depending on the conditions of the secondary zone. In the first part of the present study, the effects of fuel injection on the emissions and flame stability were investigated for a single tubular flame, In the second part, the emissions and flame stability were studied for a two-stage combustor with secondary mixture injected through the tangential slots on a cylindrical combustor wall. The effects of the ratio of air flow rates to the primary and secondary zones on the emissions and combustion characteristics were investigate.

• 한국연소학회지
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• 제18권2호
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• pp.1-7
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• 2013

Flame stabilization characteristics of premixed flames in narrow annular coaxial tubes (NACT) were investigated experimentally. The NACT burner was proposed as a model of a cylindrical refractory burner, and it was made of quartz tubes. Flame stabilization conditions affected by the characteristic length of the burner was investigated with the variation of the equivalence ratio and the flow rates. Flame behaviors in narrow spaces could be directly observed. Conclusively, more wide flame stabilization conditions could be obtained at the case of the decreased channel scale. A flame instability, such as combustion noise was detected concerned with the flame oscillation observed at the surface of multi channel stage. Some flame propagation characteristics had complicated tendencies that may exist in practical porous-media combustors. Therefore, this NACT burner can be a basic configuration for the development of flame stabilization model in porous media combustor, and it will enhance our understanding about the behavior of flames in meso-scale combustion spaces.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년도 제30회 춘계학술대회논문집
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• pp.168-172
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• 2008

추진제 유량 변화와 분사기 배열에 따른 특성속도를 연구하기 위해 축소형 연소기를 이용하여 연소시험을 수행하였다. 그 결과 유사한 압력과 혼합비 조건에서 효과적인 비 단위 면적당 유량 범위가 존재함을 알 수 있었고 최외곽 분사기로부터 막 냉각이 적용된 연소실 벽면까지의 거리 증가는 연소실 내 저 혼합비 영역을 증가시키고 특성속도를 저감시키는 기능을 하는 것으로 해석결과 나타났다. 즉, 이 2가지 설계요소는 주어진 연소압력에서 액체로켓엔진 연소기의 성능을 향상시킬 수 있는 중요한 인자임을 확인하였다.

• 한국수소및신에너지학회논문집
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• 제21권4호
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• pp.286-294
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• 2010

According to the propagation of fuel cell system, the importance of that system efficiency is being magnified. Thus, the efficiency improvement of reformer which is the important part of fuel cell system will be required. In structural aspect, the reformer is classified into cylindrical and plate type. Plate type reformer features better maintenance and space efficiency compared with cylindrical type. In this study, we changed the shape of combustion chamber to improve the reforming efficiency. And then we performed the CFD simulation to predict the spacial distribution of temperature. Analysis cased contains with baffles, fins, baffles and fins, and without those. In case of only with-baffle, temperature distributions were uneven because the high temperature stream was concentrated near the baffle end. In case of with-fin, the temperature distributions were relatively even than other cases.

• 대한환경공학회지
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• 제34권2호
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• pp.103-108
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• 2012

연소과정 중에 발생하는 질소산화물을 저감하는 기술인 MILD 연소로는 연소용 공기 및 연료로 고온의 배기가스가 유입되는 양에 따라 질소산화물 저감 특성이 많은 영향을 받는다. 일반적인 MILD 연소로는 연료와 연소용 공기는 수직 상향방향이고 배기가스는 수직하향 방향으로 흐르면서 배기가스가 유입되는데 이러한 형태보다 더욱 배기가스의 유입량을 증가시키기 위한 방법으로 동심원관형태의 MILD 연소로를 사용하고 있다. 본 연구에서는 바깥 원통의 배기가스 통로에서 안쪽 원통의 연소통로 사이에 연결관을 설치하고 배기가스를 유입하기 위한 공기노즐을 동심원관 형태로 설치하여 공기분사속도, 노즐 직경, 배기가스측 압력과 연소로측 압력 차이의 변화에 따른 유입량 특성을 수치해석을 통해 살펴봄으로써 MILD 연소로에서 더욱 적극적인 배기가스의 유입량 특성을 파악하는 것을 연구하였다. 공기노즐 분사속도의 증가에 따라 유입량은 속도의 제곱근에 비례하는 것을 알았고 배기가스 측과 연소로 측의 압력차의 크기에 선형적으로 감소하는 것을 관찰하였다. 공기노즐 출구 위치의 변화는 유입량 변화에 큰 영향이 없음을 알 수 있었다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1998년도 춘계학술대회논문집; 용평리조트 타워콘도, 21-22 May 1998
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• pp.678-683
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• 1998

Combustion instability by thermoacoustic feedback incite strong low frequency noise and vibration which damage the system and provoke the environmental problems. Therefore, it is necessary to control the thermoacoustic oscillation. In the way of controlling the instability, active control method using adaptive algorithm is applied. In this study, active noise control method using anti-sound technique is selected, whose principle is cancelling the noise with the addition of opposite phase sound. At first, simulation is performed to confirm the stability of controller, and after that control of combustion instability is carried out to get cancellation of 20-30dB SPL.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2001년도 제17회 학술발표회 논문초록집
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• pp.50-53
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• 2001

Flame propagation during the initial stages of ignition in a non-premixed swirl, having some of characteristics of the primary zone of an aero gas turbine combustor, has been investigated. Nd:YAG laser was adopted as the principal ignition source to allow arbitrary placing of the ignition site i subsequent flame development was monitored using a natural light high speed filming technique for many ignition site at two different swirl ratios and an overall equivalence ratio of 0.9. For ignition offset from the burner centreline, buoyancy force associated with radial pressure gradient produced a strong inward movement of the flame kernel. At the burner exit. flame kernels invariably developed into cylindrical form and a 'radial confinement /axia expansion' (RCAE) process was observed.