• Title/Summary/Keyword: 연소 가시화

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An Experimental Study on the combustion Characteristics in the Helmholtz-Type Pulsating Combustor (헬름홀쯔형 맥동연소기의 연소 및 작동특성에 관한 실험적 연구)

  • 길상인;신현동
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.15 no.5
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    • pp.1727-1736
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    • 1991
  • 본 연구에서는 자체 제작된 헬름홀쯔형 맥동 연소기를 이용하여 작동원리와 연소특성을 조사함으로써 맥동연소현상을 물리적으로 이해하는 것이다. 주기적 화염 의 직접가시화, 연소장의 시간평균 온도 및 농도분포, 변동압력의 크기와 공기흡입량 을 조사함으로써 맥동에 영향을 미치는 요인이 무엇인지 그리고 이것이 어떠한 변화를 야기시키는가를 살펴보고자 한다. 이렇게 얻어진 결과의 종합을 통해 장치의 형상이 결정된 일반적인 맥동연소기가 자발적인 상태에서 작동될 때 작동결정인자가 무엇인가 를 알수가 있을 것으로 사료된다.

The Visualization of Unstable Combustion in Hybrid Rocket (하이브리드 로켓의 불안정 연소 특성 가시화)

  • Koo, Won-Mo;Lee, Chang-Jin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.4
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    • pp.46-51
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    • 2007
  • The irregular fuel surface was observed by the visualization of hybrid rocket combustion. Even though the test condition maintained oxidizer rich environment, the irregular dark fuel surface was formed as the result of incomplete combustion. In order to investigate the correlation of the characteristics of oxidizer flow and the irregular fuel surface, various flow conditions were imposed such as swirl flow, induced swirl flow by helical fuel configuration and straight flow. Test results revealed no correlation was found between oxidizer flow condition and irregular fuel surface. And this can be a commonly observed phenomena in the tests with different fuel/oxidizer combination. Thus, the irregular fuel surface can be a result of the interaction of blowing flow of vaporized fuel and the boundary layer of oxidizer flow. A further study will be required to confirm the assumption for the formation of irregular fuel surface.

Effect of Swirl Angles and Combustion Characteristics of Low Swirl Model Combustor (저선회 모델 연소기의 연소특성 및 선회각도 영향)

  • Jeong, Hwanghui;Lee, Keeman
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.4
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    • pp.40-49
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    • 2016
  • This study aims to confirm the characteristics of low swirl combustion at our low swirl model combustor. To do it, it is experimentally conducted by evaluating the flame shape, stability region and emissions according to the swirl angle. The most significant feature of low swirl combustion is a occurrence of lifted flame. Such lifted flames happen to combine exquisitely propagating feature of premixed flame with diverging flow. This feature of lifted flame was confirmed through a velocity flow field and visualized the flame in this model combustor. The visualized flame was classified according to the thermal power and equivalence ratio. The variation study in swirl angles showed that the lean flammable limit could be extended only by swirl angles. Also, as the swirl angle increased, it was confirmed that the NOx and CO emissions were decreased due to the mixing enhancement and shorter resident time.

Flame Interaction with Shear Layer Flow in the Post Chamber of Hybrid Rocket (하이브리드 로켓 후연소실 전단유동과 연소반응의 상호 간섭)

  • Moon, Young Joo;Lee, Changjin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.7
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    • pp.585-592
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    • 2016
  • Visualization was done by using $CH^*$ chemiluminescence images and PMT measurements in order to understand the origin of fluctuating pressure and chemical luminosity at about 500 Hz frequency even in stable combustion, which was observed in recent experimental tests, and to find the physical correlation leading to Low Frequency Instability(LFI) in terms of phase angle. In stable combustion, chemical reactions are distributed along the shear layer flow showing a negative coupling(about 180 degree in phase angle) with combustion pressure. However, phase difference is shifted to a positive coupling showing less than 90 degree in unstable case. Also a periodic change in the distribution of chemical reactions is observed along with local flame extinction and the appearance of big scale vortex flow. In the transition to LFI, local flame extinction and small vortex flow start to appear in a row. As seen in the bluff body wake in reactive flow, the periodic appearance of vortex flow seems to share the same physical process of BVK(Bernard Von Karman) instability generation. Thus, the appearance of local extinction in 500 Hz fluctuations is gradually amplified to complete extinctions of about 20 Hz, and it leads into LFI.

Flame Propagation Characteristics in a Heavy Duty Liquid Phase LPG Injection SI Engine by Flame Visualization (대형 액상 LPG 분사식 SI 엔진에서 화염 가시화를 이용한 희박영역에서의 화염 전파특성 연구)

  • 김승규;배충식;이승목;김창업;강건용
    • Transactions of the Korean Society of Automotive Engineers
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    • v.10 no.4
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    • pp.23-32
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    • 2002
  • Combustion and flame propagation characteristics of the liquid phase LPG injection (LPLI) engine were investigated in a single cylinder optical engine. Lean bum operation is needed to reduce thermal stress of exhaust manifold and engine knock in a heavy duty LPG engine. An LPLI system has advantages on lean operation. Optimized engine design parameters such as swirl, injection timing and piston geometry can improve lean bum performance with LPLI system. In this study, the effects of piston geometry along with injection timing and swirl ratio on flame propagation characteristics were investigated. A series of bottom-view flame images were taken from direct visualization using an W intensified high-speed CCD camera. Concepts of flame area speed, In addition to flame propagation patterns and thermodynamic heat release analysis, was introduced to analyze the flame propagation characteristics. The results show the correlation between the flame propagation characteristics, which is related to engine performance of lean region, and engine design parameters such as swirl ratio, piston geometry and injection timing. Stronger swirl resulted in foster flame propagation under open valve injection. The flame speed was significantly affected by injection timing under open valve injection conditions; supposedly due to the charge stratification. Piston geometry affected flame propagation through squish effects.

Measurments of 2-D Image Soot Distribution in Late Combustion Stage Using Elastic Scattering, Laser-Induced Incandescence and Flame Luminosity (레이저 탄성산란법, 여기적열법, 자발광을 이용한 가시화 디젤엔진의 후기연소의 2차원 soot 분포 측정)

  • Noh, S.M.;Won, Y.H.;Park, J.G.;Choi, I.Y.;Chun, K.M.
    • Proceedings of the KSME Conference
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    • 2000.11b
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    • pp.162-167
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    • 2000
  • Soot formation and oxidation is closely related to the combustion phenomena inside a diesel engine. Laser-based diagnostics provide a means for improving our understanding of diesel combustion, because they have highly temporal and spatial ability. To understand the soot behavior we did preliminary study by taking flame luminosity photographs and 2-D imaging soot distribution using Laser Elastic Scattering(LIS) and Laser-Induced Incandescence(LII). From the data we found that soot concentration was high in the bowl and disappeared from the central region in the late combustion stage.

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Self-ignition of high-pressure hydrogen gas released into tube (튜브내 고압수소가스 누출에 따른 자발점화 현상 유동가시화 연구)

  • Kim, Yeong Ryeon;Lee, Hyoung Jin;Kim, Sei Hwan;Jeung, In Seuck
    • 한국연소학회:학술대회논문집
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    • 2012.04a
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    • pp.247-248
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    • 2012
  • Unidentified self-ignitions were reported when the high-pressure hydrogen gas suddenly leaked out. This paper presents a flow visualization study to investigate the self-ignition mechanism in a test tube how the ignition process is initiated and the flame propagates with measurement of a number of pressure and light sensors installed in the tube supported the analysis of the self-ignition. The test result showed the location of the self-ignition taken place and critical static pressure at the boundary layer for self-ignition.

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A study on the spray combustion characteristics of D.I. diesel engine using visualization engine system (가시화 엔진을 이용한 직분식 디젤 엔진의 분무 연소 특성에 관한 연구)

  • Chung, J.W.;Lee, K.H.;Choi, S.W.;Kim, B.S.
    • Journal of ILASS-Korea
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    • v.4 no.4
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    • pp.17-23
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    • 1999
  • Recently, many researchers have been studied a D.I. diesel engine because of the exhaust gas restriction and fuel consumption performance. It is well known that the fuel injection characteristics are the key factors on the diesel combustion and exhaust emission. In this study, the fuel injection characteristics of 5-hole injector and the combustion characteristics are investigated with the amount of fuel by means of the visualization method and visualization D.I. diesel engine system. As the results of the experiments, the spray pattern of the fuel injection and the diffusion flame of a D.I. diesel engine are clarified. In addition, combustion phenomena with operation conditions such as engine speed and engine load are made clear.

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A Hybrid Technique for Fire Animation (불의 애니메이션을 위한 복합적 기법)

  • Min, Kyung-Ha
    • Journal of Korea Game Society
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    • v.7 no.3
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    • pp.77-88
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    • 2007
  • In this paper, we present a new fire animation and visualization scheme. The most difficult problem in creating fire animation is how to simulate the mechanism of emitting lighting and heat of fire. We attack the difficulty by presenting a hybrid scheme that combines the simulation scheme and the combustion process in voxelized space where the numerical solution of the classical fluid equations is implemented. Therefore, the combustion process is simulated at each voxel and the amount of heat generated at the voxel is estimated. The generated heat will increase the temperature at the voxel, where results in the increase of turbulent motion of fire. We also propose a visualization scheme that modifies the photon mapping algorithm in order to render fire and various lighting effects of fire to the environments.

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Conditional Sampling Measurement to Identify Flame Structures in Turbulent Combustion (난류 화염 구조 규명을 위한 조건 평균 측정법)

  • Huh Kang Y.
    • Journal of the Korean Society of Visualization
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    • v.2 no.1
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    • pp.8-11
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    • 2004
  • Conditional sampling measurement is required for conditional averages as well as unconditional Favre averages to resolve different flame structures of turbulent combustion. A Favre average can be obtained as an integral of conditional average and Favre PDF in terms of the mixture fraction, which is a preferred choice as a sampling variable in diffusion controlled turbulent combustion. MILD combustion data are presented as an example for a conditionally averaged data set and comparison with CMC calculation results.

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