• Title/Summary/Keyword: Flame Response

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제트확산화염과 예혼합화염의 다양한 속도 섭동에 대한 응답 특성 (A Study on Response Characteristics of Jet-diffusion Flame and Premixed Flame with Various Velocity Perturbations)

  • 안명근;김태성;김희동;윤영빈
    • 한국연소학회지
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    • 제22권2호
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    • pp.19-26
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    • 2017
  • An experimental study investigates the flame response characteristics of jet-diffusion flame and premixed flame. The experiment was conducted while varying the amplitude. Flame lengths were quantified for OH chemiluminescence measurement and compared with the result of the flame transfer function. Flame length and flame velocity perturbation were normalized and compared with the result of the flame transfer function. The comparison results appear that velocity perturbation and flame length oscillation of premixed flame show linear behaviors on the other hand jet-diffusion flame, amplitudes are more thant 0.20, shows nonlinear behaviors of flame velocity perturbation and flame length oscillation.

전개확산제트화염과 정체점 확산화염과의 유사성 (Similarity between a stagnant point diffusion flame and an evolving jet diffusion flame)

  • 박정;신현동
    • 대한기계학회논문집B
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    • 제21권4호
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    • pp.494-502
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    • 1997
  • Experiments on corresponding jet flames with stagnant point diffusion flames have been carried out in initial injection periods. A compensated measurement of maximum flame temperature, which is based on the ion signal, has been employed to inspect flame responses to time-varying strain rates. The flame responses are obtained at two conditions for the slowly time-varying strain rate and the case of flame extinction, and analyzed to confirm similarity between a stagnant point diffusion flame and an evolving jet diffusion flame. Nonsteady effects are addressed via the comparison between several time scales. The time variation with low strain rates, in which illustrates the flame behavior of the upper branch far from extinction in the well-known S-curve, is confirmed to produce a quasi-steady flame response through the nonsteady experiments. The time variation with strain rates in the case of flame extinction indicates an unsteady effect of flame response. It is therefore found that the flame responses near jet tip depend on time histories of characterized strain rates in the developing process.

난류 예혼합 연소기에서의 흡입 유동 섭동에 대한 화염의 동적 거동 (Flame Dynamic Response to Inlet Flow Perturbation in a Turbulent Premixed Combustor)

  • 김대식
    • 한국연소학회지
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    • 제14권4호
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    • pp.48-53
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    • 2009
  • This paper describes the forced flame response in a turbulent premixed gas turbine combustor. The fuel was premixed with the air upstream of a choked inlet to avoid equivalence ratio fluctuations. To impose the inlet flow velocity, a siren type modulation device was developed using an AC motor, rotating and static plates. Measurements were made of the velocity fluctuation in the nozzle using hot wire anemometry and of the heat release fluctuation in the combustor using chemiluminescence emission. The test results showed that flame length as well as geometry was strongly dependent upon modulation frequency in addition to operating conditions such as inlet velocity. Convection delay time between the velocity perturbation and heat release fluctuations was calculated using phase information of the transfer function, which agreed well with the results of flame length measurements. Also, basic characteristics of the flame nonlinear response shown in the current test conditions were introduced.

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외부압력 교란에 의한 연소반응 연구 고찰 (Study of Flame Response Characteristics to External Acoustic Perturbations)

  • 서성현
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제37회 추계학술대회논문집
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    • pp.415-418
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    • 2011
  • 비선형적인 연소불안정 현상 이해를 위해서는 압력 섭동에 대한 화염 반응 특성 파악이 중요하다. 이전 연구는 스피커에 의한 연료와 공기 혼합체 섭동에 대한 난류, 층류 예혼합 화염의 반응, 그리고 화염에 직접 축 방향 압력파를 가진하는 경우로 나뉜다. 본 연구에서는 액체로켓엔진 연소환경을 모사한 연소화염의 횡 방향 가진파에 대한 화염 응답 함수 파악을 위한 실험 장치를 고안하여 제시하였다.

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유동 섭동에 의한 난류예혼합화염의 열발생 모델에 관한 연구 (A Heat Release Model of Turbulent Premixed Flame Response to Acoustic Perturbations)

  • 조주형;백승욱
    • 대한기계학회논문집B
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    • 제32권6호
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    • pp.413-420
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    • 2008
  • The unsteady heat release characteristics play a significant role in combustion instabilities observed in low emissions gas turbine combustors. Such combustion instabilities are often caused by coupling mechanisms between unsteady heat release rates and acoustic perturbations. A generalized model of the turbulent flame response to acoustic perturbations is analytically formulated by considering a distributed heat release along a curved mean flame front and using the flame's kinematic model that incorporates the turbulent flame development. The effects of the development of flame speed on the flame transfer functions are examined by calculating the transfer functions with a constant or developing flame speed. The flame transfer function due to velocity fluctuation shows that, when a developing flame speed is used, the transfer function magnitude decreases faster with Strouhal number than the results with a constant flame speed at low Strouhal numbers. The flame transfer function due to mixture ratio fluctuation, however, exhibits the opposite results: the transfer function magnitude with a developing flame speed increases faster than that with a constant flame speed at low Strouhal numbers. Oscillatory behaviors of both transfer function magnitudes are shown to be damped when a developing flame speed is used. Both transfer functions also show similar behaviors in the phase characteristics: The phases of both transfer functions with a developing flame speed increase more rapidly than those with a constant flame speed.

예혼합 연소기에서의 화염 전달 함수 측정 (Flame Transfer Function Measurement in a Premixed Combustor)

  • 김대식;김기태;전승배;이종근
    • 한국연소학회지
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    • 제13권2호
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    • pp.1-6
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    • 2008
  • An experimental study of the flame response in a turbulent premixed combustor has been conducted with room temperature, atmospheric pressure inlet conditions using premixed natural gas. The fuel is premixed with the air upstream of a choked inlet to avoid equivalence ratio fluctuations. Therefore the observed flame response is only the result of the imposed velocity fluctuations, which are produced using a variable speed siren. Measurements are made of the velocity fluctuation in the nozzle using hot wire anemometry and of the heat release fluctuation in the combustor using chemiluminescence emission. The results are analyzed to determine the phase and gain of the flame transfer function as a function of the modulation frequency. Of particular interest is the effect of flame structure on the flame response predictions and measurements. The results show that both the gain and the phase of flame transfer function are closely associated with the flame length and structure, which is dependent upon the upstream flow perturbation as well as equivalence ratio in the current study.

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비예혼합화염과 예혼합화염의 속도 섭동에 따른 응답 특성 (How to Prepare the Manuscript for Submission to the Proceedings of KSPE Conference)

  • 안명근;김태성;윤영빈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.612-616
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    • 2017
  • 비예혼합합화염과 예혼합화염의 화염응답특성을 속도섭동을 다양하게 변경하며 실험하였다. 연료로는 수소($H_2$)/메탄($CH_4$)을 50/50 %로 혼합한 혼합연료를 사용하였으며 산화제로는 공기를 사용하였다. OH 자발광(OH fluorescence)을 이용하여 화염이미지를 계측하였으며 PMT(Photo Multiplier Tube)를 이용하여 열 방출량을 계측하였다. 계측된 이미지는 MatLab 코드를 이용하여 수치화하였다. 예혼합화염의 결과에서는 진폭이 증가할수록 화염섭동이 증가하는 경향성을 보았으며 진폭에 따라서 화염전달 함수의 게인 값이 선형적인 거동을 하는 것을 관찰하였다. 비예혼합화염의 화염길이는 진폭이 증가할수록 짧아지는 것을 관찰하였고 게인 값은 진폭에 비선형적인 거동을 하는 것을 확인하였다.

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압력섭동에 따른 비정상 화염편 응답특성 해석 (Flamelet Analysis for Transient Response to Pressure Oscillations)

  • 배준경;김용모;김성구
    • 한국연소학회지
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    • 제16권1호
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    • pp.30-35
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    • 2011
  • This study has been mainly motivated to numerically investigate the transient flame response to pressure oscillations in the gaseous hydrogen - liquid oxygen flames at supercritical pressures. The present analysis is based on the real-fluid transient flamlet model and the flame field is acoustically perturbed only by the sinewave oscillations in the frequency range from 1,000 Hz to 5,000 Hz. Based on numerical results, the detailed discussions are made for the flame response characteristics and the transient flamelet response associated with the high-frequency combustion instability in the liquid propellant rocket engines.

THE DEVELOPMENT OF A UV FLAME DETECTOR FOR THE AUTOMATIC FIRE SUPPRESSION SYSTEM FOR ENGINE COMPARTMENT FIRES

  • Lim, Sung-Mook;Jung, Ki-Chang;Kim, Eung-Sik;Kim, Hong
    • 한국화재소방학회:학술대회논문집
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    • 한국화재소방학회 1997년도 International Symposium on Fire Science and Technology
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    • pp.590-597
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    • 1997
  • In this work, a new type of UV flame detection system was developed. In order to measure the performance of UV flame detector, various kinds of experiments was performed. The results show that the maximum response time of the UV flame detector is 0.2 seconds when the detection distance is one meter The advantages of this system include wide area, high speed response and high sensitivity. After testing the W flame detector in engine compartment it detected fire within 0.09 seconds and extinguished within 5 seconds. Hence, the UV flame detector can be applied in automatic fire suppression system for automobiles.

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Evolution of Flame Shape to a Vortex Pair

  • Rhee, Chang-Woo
    • Journal of Mechanical Science and Technology
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    • 제15권5호
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    • pp.623-629
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    • 2001
  • The PSC (Propagation of Surfaces under Curvature) algorithm is adapted to the simulation of a flame propagation in a premixed medium including the effect of volume expansion across the flame front due to exothermicity. The algorithm is further developed to incorporate the flame anchoring scheme. This methodology is successfully applied to numerically simulate the response of an anchored V-flame to two strong free stream vortices, in accord with experimental observations of a passage of Karman vortex street through a flame. The simulation predicts flame cusping when a strong vortex pair interacts with flame front. In other words, this algorithm handles merging and breaking of the flame front and provides an accurate calculation of the flame curvature which is needed for flame propagation computation and estimation of curvature-dependent flame speeds.

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