• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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• pp.254-257
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• 2010

본 연구에서는 로켓엔진 연소기의 음향 불안정 억제를 위해 헬름홀츠 공명기의 음향학적 최적 설계 조건을 해석/실험적으로 연구하였다. 질량-스프링-댐퍼 시스템과의 유사성을 이용한 모델 식의 풀이를 통해 감쇠 성능을 정량화하였다. 헬름홀츠 공명기의 기하학적 형상 인자로 목의 길이와 공동의 크기, 목 및 공동의 직경을 선택하였다. 목의 길이가 짧아지고, 공동의 길이가 길어짐에 따라 흡음성능이 증가하고, 목과 공동의 직경비가 증가함에 따라 흡음성능은 감소하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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• pp.259-264
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• 2005

연소불안정과 밀접한 관련이 있는 열방출의 측정은 연소불안정을 제어하는데 매우 중요하다. 따라서 본 연구에서는 희박예혼합연소에서 반응영역의 위치와 전체, 국소 열방출률의 지표로 많이 사용되는 $OH^{\ast}$ 이미지를 ICCD를 이용해 취득하였다. 본 연구의 목적은 당량비가 전체 열방출률과 국소 레일라이 지수 분포에 미치는 영향을 알아보는 것이다. 국소 레일라이 지수 분포는 선적분된 이미지를 아벨 역변환 시켜서 화염의 중앙 단면 정보를 통해 얻을 수 있었다. 각 당량비 조건에서, 한 주기 동안의 열방출의 평균값은 당량비가 증가함에 따라 지수 함수적으로 증가하였다. 국소 레일라이 지수 분포 결과로부터, 연소불안정을 증폭시키거나 소멸시키는 영역을 분명히 알 수 있었다. 이것은 넓은 당량비 조건에 대한 화염구조와 연소불안정 영역에 대한 통찰력을 제공한다.

• 한국연소학회지
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• 제15권1호
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• pp.12-21
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• 2010

The main objective of this study was investigation of combustion instability characteristics in a lean partially premixed gas turbine dump combustor. Dynamic pressure transducers were located on combustor and inlet section to observe combustion pressure oscillation and difference at each measurement places. Also flame shape and $CH^*$ chemiluminescence were measured using a high speed ICCD camera. The combustor length was varied in order to have different acoustic characteristics from 800 to 1090 mm. The first section of this paper shows the stability map in model gas turbine combustor. And the effects of combustor length, mixture velocity in the mixing section and equivalence ratio were studied by the pressure perturbation and heat release oscillation. Also, the instability frequency and mode analysis were studied in last two sections. We observed two dominant instability frequencies in this study. Lower frequencies were obtained at lower equivalence ratio region and it was associated with a fundamental longitudinal mode of combustor length. Higher frequencies were observed in higher equivalence ratio conditions. It was related to secondary longitudinal mode of combustor and mixing section. In this instability characteristics, pressure oscillation of mixing section part was larger than pressure oscillation of combustor. As a result, combustion instability was strongly affected by acoustic characteristics of combustor and mixing section geometry.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.59-60
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• 2017

가스터빈 연소기의 연소불안정성을 평가하기 위해 동적모드분해(dynamic mode decomposition, DMD) 기법을 적용하였다. DMD 기법으로 도출된 감쇠계수(damping coefficient)와 FFT 결과를 비교 분석 하였다. 또한 화염전달함수 (flame transfer function, FTF)를 도출하는 실험적 방법에 DMD 기법을 적용하여 분석을 시도하였다. 기존에 제시된 열방출 섭동을 추출하는 방법에서 개선된, OH PLIF 이미지를 이용하여 열방출 섭동을 추출하는 방법을 사용하였다. 분석 결과, 열방출 섭동의 추출 위치에 따라 화염전달함수의 이득(gain)이 변하는 것을 확인하였다.

• 한국연소학회지
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• 제22권1호
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• pp.39-45
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• 2017

Combustion instability analysis of partially premixed model gas turbine combustor was conducted with 1D lumped method. Flame Transfer Function(FTF) was obtained with variation of fuel composition by Photo Multiplier Tube(PMT) and Hot Wire Anemometry(HWA). Decreasing instability frequency was observed when combustor length increased and multi-mode instability was confirmed. Instability frequency mode was changed while $H_2$ composition rate was increased and had agreement with experimental value. This work confirms that prediction of longitudinal combustion instability mode of partially premixed combustor is possible using 1D lumped method.

• 대한기계학회논문집B
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• 제33권9호
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• pp.658-665
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• 2009

Lean premixed combustors are used for significant NOx reduction which one of issues in current gas turbine combustor. This study was investigated to estimate the effects of the unmixedness of fuel-air, equivalence ratio on the instability mechanism, NOx emission and combustion oscillation in a lean premixed combustor. The experiments were conducted in a dump combustor at atmospheric pressure conditions using methane as fuel. The swirler angle was $45^{\circ}$, the degrees of fuel-air mixing were 0, 50 and 100 and inlet temperature was 650K. The equivalence ratio was ranging from 0.5 to 0.8. This paper shows that NOx emission was increased when the degree of fuel-air mixing is increased in same equivalence ratio and when equivalence ratio is increased. And the range of the combustion instability was enlarged as a function of increasing of the degree of fuel-air mixing.

• Journal of Advanced Marine Engineering and Technology
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• 제22권2호
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• pp.225-231
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• 1998

Flame propagation speed characteristics of methante-air mixtures were experimentally investigated in combustion chamber modelled engine. Flame propagation process was known as a funtion of equivalence ratio initial pressure and initial temperature. Ion probe and schlieren photograph were applied to measure the local flame speed and flame radius in quiescent mixtures. Pressure was also measured to make sure of the reproducibility and to apply combustion analysis. Burning velocity was calculated from the flame propagation speed and combustion analysis. Flames were developed faster with higher initial pressure and initial temperature but showed maximum propagation speed at equivalence ratio 1.1 regardless of initial pressure and temperature. Local flame speed was maximum values at near midpoint between center and wall.

• 한국연소학회지
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• 제18권3호
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• pp.9-23
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• 2013

A rotary kiln furnace is one of the most widely used gas-solid reactors in the industrial field. Although the rotary kiln is a versatile system and has different size, approach to the reactor modeling can be generalized in terms of flow motion of the solid and gas phases, heat transfer, and chemical reactions on purpose. In this paper, starting from a zero-dimensional model and extending to higher dimension and comprehensive models, overall procedure of the design development of rotary kiln reactors and considerations are presented. The approaches to performance analysis of the reactors are introduced and examples of application cases are presented.

• 대한기계학회논문집B
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• 제32권8호
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• pp.574-581
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• 2008

The characteristics of combustion and flow for a lean premixed flame in lab-scale gas turbine combustor was studied through experiment and numerical analysis. From the experiment, flame structure and heat release rate were obtained from OH emission spectroscopy. Qualitative comparisons were made line-integrated OH chemiluminescence image and abel-transformed one. NOx analyzer was implemented to get the characteristic of NOx exhaust from the combustor. From the numerical analysis, the thermal distribution and characteristic of recirculation zone with the change of fuel-air mixing degree, the characteristic of methane distribution with equivalence ratio in the combustor respectively. Total heat release rate is increased with increasing equivalence ratio. Thermal Nox is reduced with increasing fuel-air mixing degree. Increasing equivalence ratio results in the decrease of the size of reaction zone and alteration of the position of the reaction zone into the entrance of the combustor.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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• pp.274-280
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• 2005

광학적 접근이 가능한 대기압, 실험용 덤프 연소기에서 실험적 연구를 수행하였다. 본 연구의 목적은 불안정 연소 동안 주기적으로 변하는 압력 사이클의 위상에 따른 온도를 측정함에 있다. 특히, 연소 불안정에 영향을 미치는 연료/공기의 혼합정도가 온도특성에 미치는 효과를 살펴보기 위해 반 스톡스 라만 분광학을 이용하였다. 본 논문에서는 위상에 따른 평균온도, 표준 오차, 확률 밀도함수 및 1900K 이상의 고온이 발생할 확률에 대한 결과가 제시되어있다. 실험결과에 대해 간략히 살펴보면, 압력위상에 따른 평균온도는 압력위상과 거의 동일 위상을 가짐을 확인할 수 있었고, 평균온도의 최대-최소 차이는 연료/공기 혼합이 양호할수록 작아지는 것을 발견할 수 있었다. 온도 확률밀도 함수는 화염 거동과 질소산화물 배출 특성에 대한 기본 자료를 제시해 주었다. 이러한 결과들은 궁극적으로 연소 불안정 발생 메커니즘과 열-음향학적 상호작용을 이해함에 있어 중요한 역할을 할 것으로 기대된다 하겠다.