• 한국연소학회:학술대회논문집
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• 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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• pp.407-408
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• 2014

• 한국수소및신에너지학회논문집
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• 제28권2호
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• pp.181-189
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• 2017

This paper describes experimental results on combustion characteristics with hydrogen contents of synthetic natural gas (SNG) in low swirl combustor. To investigate the effect of hydrogen contents for premixed SNG flame, stability map, CH chemiluminescence images, flame spectrum analysis and emission performances were measured. In the results, as the hydrogen content was increased, the lean flammable limit was expanded and the flame length was decreased. The hydrogen contents affected the flame liftoff height, and it has different tendency according to the equivalence ratio and flame shape. The change of height and length of flame according to hydrogen contents is caused by the fast burning velocity of hydrogen, which can be confirmed by GRI 3.0 reaction mechanism in PREMIX code. The intensity of $OH^*$, $CH^*$ and $C_2^*$ was confirmed by spectrum analysis of flame. As a result, the $CH^*$ intensity was not significantly different according to hydrogen content. The increase of hydrogen contents influenced positively CO and NOx emission performances.

• 센서학회지
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• 제13권5호
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• pp.335-341
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• 2004

A light collecting probe named Multi-colored Integrated Receiving Optics (MICRO) is experimentally examined to verify its performance. For these purposes, the time-series signals of MICRO probe is compared with those of electrostatic probe and light-guided probe by monitoring, for example, such as OH radical chemiluminescence, CH radical band and droplet Mie scattering. In addition, the experiment was conducted by using laminar premixed Bunsen flame, turbulent premixed Bunsen flame and premixed spray flame, respectively. It was confirmed that the performance of MICRO probe was very useful and convenient to obtain the chemiluminescence signals from local regions in turbulent premixed Bunsen flame and premixed spray flame.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.1116-1121
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• 2004

In this study, the effect of central fuel injection on a coaxial laminar $CH_{4}/air$ flame was experimented at the defined premixing condition(${\Phi}=1.90$, ${\sigma}=50/75/100%$, x/D=10). The partial premixing parameter are the equivalence ratio that total fuel is fixed at 200cc/min, the fuel split degree which means the percentage of fuel entering the outer tube to the total amount, and the mixing distance indicating the nonreactant mixture's homogeneity between inner tube top and burner exit. The object is to investigate the flame structure and chemiluminescence characteristics of laminar partial premixed flame as changing mixing parameters. The radical signal was acquired from ICCD camera and PMT. Each intensity was compared with Abel inverted value for measuring the effect of background light on the peak signal location and the intensity at central preheat zone. The results show that the peak location of each radical was broaden as the fuel split degree increasing because the mixing quality was enhanced. and $OH^{\ast}$ is a good indicator for flame front between reaction and preheat zone. At last $CH_{2}^{\ast}$ has the same tendency with $CH^{\ast}$ but a thinner reaction zone than $CH^{\ast}$ due to a rapid decay on the burned gas side.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2015년도 제51회 KOSCO SYMPOSIUM 초록집
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• pp.139-141
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• 2015

• 한국연소학회:학술대회논문집
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• 한국연소학회 제26회 KOSCO SYMPOSIUM 논문집
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• pp.159-165
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• 2003

Self-excited noise generation from laminar flames in thin annular jets of methane/air premixture has been investigated experimentally. Various flames were observed in this flow configuration, including conical shape flames, ring shape flames, steady crown shape flames, and oscillating crown shape flames. Self-excited noise with the total sound pressure level of about 70dB was generated from the oscillating crown shape flames for the equivalence ratio larger than 0.95. Sound pressure and $CH^{\ast}$ chemiluminescence were measured by using a microphone and a photomultiplier tube. The frequency of generated noise was measured as functions of equivalence ratio and premixture velocity. A frequency doubling phenomena have also been observed. The measured $CH^{\ast}$ chemiluminescence data were analyzed from which the corresponding sound pressure has been calculated. By comparing the data with those of measured ones, the noise source can be attributed to the flame front fluctuation near the edge of the oscillating crown-shape flames. The flame stability regime was influenced sensitively to the supplying air through the inner tube.

• 한국연소학회지
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• 제19권1호
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• pp.29-38
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• 2014

This paper described an experimental investigations of combustion instability mode in a lean premixed dual swirl combustor for micro-gasturbine system. When such the instability occurs, a strong coupling between pressure oscillations and unsteady heat release excites a self-sustained acoustic wave which results in a loud, annoyed sound and may also lead a structural damage to the combustion chamber. The detailed period of flame behavior and heat release in combustion instability mode have been examined with high speed OH and CH-PLIF system and $CH^*$ chemiluminescence measurement, flame tomography with operated at 10 kHz and 6 kHz each. Experiment results suggest that unstable flame behavior has a specific frequency with 200 Hz and this frequency is accords with about 1/2 sub-harmonic of combustor resonance frequency, not fundamental frequency. This is very interesting phenomenon that have not reported yet from other previous works. Therefore, when a thermo-acoustic instability with Rayleigh criterion occurs, the fact that the period of heat release and flame behavior are different each other was proposed for the first time through this work.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제23회 추계학술대회 논문집
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• pp.137-140
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• 2004

주기적인 와류화염과 열방출 진동의 연관성에 대한 실험적인 연구가 수행되었다. 난류제트화염은 덤프 연소기에서 재순환 되는 뜨거운 생성물에 의해서 안정화되며, 큰 스케일의 주기적 와류가 음파에 의해서 제트화염에 부가되었다. 실제적인 연소기에서의 불안정 현상을 모사하기 위해 가진주파수와 실험변수들을 조절하였다. 본 연구의 목적은 원치 않는 열방출의 진동을 유도시키는 와류-열방출의 연관성을 분석하여, 연소불안정의 능동제어를 위해 사용될 수 있는 알맞은 연료분사 패턴을 조사하는 것이다. 주기적인 패턴을 측정할 수 있는 슐리렌 기법과 CH* chemiluminescence 기법이 사용되었으며, 실험결과는 와류 생성 사이클의 위상에 따라서 서로 비교되었다.

• 한국추진공학회지
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• 제16권5호
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• pp.10-19
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• 2012

연소불안정 현상을 제거하거나 효과적으로 제어하기 위해서는 화염구조에 대한 이해가 매우 중요하다. 이에 본 연구에서는 OH 자발광 및 He-Ne 레이저 광흡수 계측기법을 이용하여 연소불안정과 화염 구조사이의 상관관계에 대한 실험적 연구를 다양한 실험조건에서 수행하였다. 실험에서는 673 K로 가열된 swirl 형태로 공급되는 건조한 공기와 LNG($CH_4$) 연료를 사용하였으며 전체 당량비는 1.2 조건에서 속도를 25 ~ 70 m/s까지 바꾸어가며 실험을 수행하였다. 이를 통하여 연소불안정 현상이 낮은 속도조건과 높은 속도조건에서 발생하는 것을 확인할 수 있었고, 낮은 속도조건의 불안정에서는 화염의 와동구조가 연소불안정현상에 영향을 끼친다는 것을 확인할 수 있었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.367-376
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• 2012

연소불안정 현상을 제거하거나 효과적으로 제어하기 위해서는 화염구조에 대한 이해가 매우 중요하다. 이에 본 연구에서는 OH 자발광 및 He-Ne 레이저 광흡수 계측기법을 이용하여 연소불안정과 화염구조사이의 상관관계에 대한 실험적 연구를 다양한 실험조건에서 수행하였다. 실험에서는 673K로 가열되어진 swirl 형태로 공급되는 건조한 공기와 LNG(CH4) 연료를 사용하였으며 전체 당량비는 1.2 조건에서 속도를 25 ~ 70 m/s까지 바꾸어가며 실험을 수행하였다. 이를 통하여 연소불안정 현상이 낮은 속도조건과 높은 속도조건에서 발생하는 것을 확인할 수 있었고, 낮은 속도조건의 불안정에서는 화염의 와동구조가 연소불안정현상에 영향을 끼친다는 것을 알 수 있었다.