• Title/Summary/Keyword: Global equivalence ratio

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Determination of Laminar Burning Velocity in Premixed Oxy-Methane Flames (메탄-산소 층류화염전파속도 측정)

  • Oh, Jeong-Seog;Noh, Dong-Soon;Lee, Eun-Gyeong;Hong, Seong-Kook
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.258-262
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    • 2011
  • The laminar burning velocity in premixed Oxy-CH4 flames was studied in a lab-scale Bunsen burner. $CH^*$ chemiluminescence method and Schliren photography were used. Experimental results were compared with numerical prediction which was calculated with a CHEMKIN 3.7 package with a PREMIX code. Global equivalence ratio of oxy-CH4 mixture was varied from 0.5 to 2.0 in a laminar flow region. The laminar burning velocity was measured as 3.1 m/s for Schlieren photograph and 2.9 m/s for $CH^*$ chemiluminescence technique (angle method).

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Flame Stabilization Mechanism of a Micro Cyclone Combustor (마이크로 사이클론 연소기의 화염 안정화 기구)

  • Oh, Chang-Bo;Choi, Byung-Il;Han, Yong-Shik;Kim, Myung-Bae;Hwang, Cheol-Hong
    • 한국연소학회:학술대회논문집
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    • 2007.05a
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    • pp.139-144
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    • 2007
  • A micro cyclone combustor was developed to be used as a component of mobile power generator (MPG). The cyclone combustor was designed so that fuel and air were supplied to the combustion chamber separately to prevent a flash-back. The flame shape stabilized inside the micro cyclone combustor was visualized experimentally and the flow field and the combustion characteristics of the combustor were investigated numerically. The global equivalence ratio (${\Phi}$), defined using the fuel and air flow rates, was introduced to examine the overall flow and flame features of the combustor. The flame stabilization mechanism could be well understood using the velocity distribution inside the combustor. For only non-reacting case, it was found that a weak recirculating zone was formed upper the fuel-supplying tube in case of ${\Phi}$ < 1.0. It was also found that small regions that have a negative axial velocity exist near the fuel injection ports for both of non-reacting and reacting case. It was identify that a flame front was stabilized at the negative axial velocity regions near the fuel injection ports.

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Numerical Simulation of the Mixing and Flow Characteristics in a Micro Cyclone Combustor (마이크로 사이클론 연소기의 혼합 및 유동특성에 관한 수치해석 연구)

  • Choi, Byung-ll;Han, Yong-Shik;Kim, Myung-Bae;Hwang, Cheol-Hong;Oh, Chang-Bo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.31 no.12
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    • pp.1042-1047
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    • 2007
  • A micro cyclone combustor was developed to be used as a heat source of thermoelectric power generator (TPG). The cyclone combustor was designed so that fuel and air were supplied to the combustion chamber separately. The mixing and flow characteristics in the combustor were investigated numerically. The global equivalence ratio ($\Phi$), defined using the fuel and air flow rates, was introduced to examine the flow features of the combustor. The mixing of fuel and air inside the combustor could be well understood using the fuel concentration distribution. It was found that the weak recirculating zone was formed upper the fuel-supplying tube in case of ${\Phi}$<1.0. In addition, it was found that small regions that have a negative axial velocity exist near the fuel injection ports. It is assumed that these negative axial velocity regions can stabilize a flame inside the micro cyclone combustor.

3D RANS Simulation and the Prediction by CRN Regarding NOx in a Lean Premixed Combustion in a Gas Turbine Combustor (희박 예혼합 가스터빈 연소기 3 차원 전산 해석 및 화학반응기 네트워크에 의한 NOx 예측)

  • Yi, Jae-Bok;Jeong, Dae-Ro;Huh, Kang-Yul;Jin, Jae-Min;Park, Jung-Kyu;Lee, Min-Chul
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.12
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    • pp.1257-1264
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    • 2011
  • This paper presents 3D simulation by STAR-CCM+ for lean premixed combustion in a stationary gas turbine combustor with separate pilot and main nozzles. The constant for the source term in the flame area density transport equation was modified to account for a low global equivalence ratio and validated against measurement data. A Partially-premixed Coherent Flame Model(PCFM) involves propagation of a laminar premixed flame with the predicted flame surface density and equilibrium assumption in the burned gas with spatial inhomogeneity. The conditions for cooling by radiation and convection are considered for accurate determination of the heat flux on the wall. A parametric study is of the pilot-fuel-to-total-fuel-ratio is carried out. A chemical reactor network (CRN) was constructed on the basis of the 3D simulation results and compared against measurements of NOx.

On the Reliability of the Computational Fire Model Based on the Yield Rate Concept of Combustion Gases (생성율 개념에 기초한 화재모델의 신뢰성에 대한 연구)

  • Kim, Sung-Chan;Ko, Gwon-Hyun;Lee, Seong-Hyuk
    • Fire Science and Engineering
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    • v.23 no.4
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    • pp.130-136
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    • 2009
  • The present study has been performed to evaluate the reliability of the fire field model (FDS version 5.2) with yield rate concept of combustion products. The CO and smoke density predicted by FDS model was directly compared with measurement in a reduced scale ISO-9705 room. The GER (global equivalence ratio) concept was used to characterize the CO and smoke density with ventilation condition in the fire compartment. The FDS model tends to under-predict CO concentration and smoke density than those of measurement for the under-ventilated conditions. Also, the discrepancy between predicted and measured result increases as GER increases. In order to improve the reliability of the fire model for performance evaluation of fire safety, the fire model is necessary to be validated in various fire cases as well as develop detailed physical model.

Effects of Ventilation Condition on the Fire Characteristics in Compartment Fires (Part I: Performance Estimation of FDS) (구획화재에서 환기조건의 변화가 화재특성에 미치는 영향(Part I: FDS의 성능평가))

  • Hwang, Cheol-Hong;Park, Chung-Hwa;Ko, Gwon-Hyun;Lock, Andrew
    • Fire Science and Engineering
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    • v.24 no.3
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    • pp.131-138
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    • 2010
  • Experimental and numerical studies were conducted to investigate the thermal and chemical characteristics of heptane fires in a full-scale ISO 9705 room. Representative fire conditions were considered for over-ventilated fire (OVF) and under-ventilated fire (UVF). Fuel flow rate and doorway width were changed to create OVF and UVF conditions. Detailed comparisons of temperature and species concentrations between experimental and numerical data were presented in order to validate the predictive performance of FDS (Fire Dynamic Simulator). The OVF and UVF were explicitly characterized with distributions of temperature and product formation measured in the upper layer, as well as combustion efficiency and global equivalence ratio. It was shown that the numerical results provided a quantitatively realistic prediction of the experimental results observed in the OVF conditions. For the UVF, the numerically predicted temperature showed reasonable agreement with the measured temperature. The predicted steady-state volume fractions of $O_2$, $CO_2$, CO and THC also agreed quantitatively with the experimental data. Although there were some limitations to predict accurately the transient behavior in terms of CO production/consumption in the UVF condition, it was concluded that the current FDS was very useful tool to predict the fire characteristics inside the compartment for the OVF and UVF.

Geometric Effects of Compartment Opening on Fuel-Air Mixing and Backdraft Behavior (개구부의 기하학적 형상이 구획실의 연료-공기 혼합특성 및 백드래프트 거동에 미치는 영향)

  • Ha, Suim;Oh, Chang Bo
    • Fire Science and Engineering
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    • v.33 no.1
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    • pp.30-38
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    • 2019
  • Mixing characteristics and backdraft dynamics were investigated using large eddy simulation for compartments initially filled with methane fuel. Four different opening geometries, i.e. conventional door opening case (Door) and the cases where horizontal door was implemented on the upper ($Slot_U$), middle ($Slot_M$) and lower part ($Slot_L$) of side wall, were considered in the simulations. For cases without ignition, the amounts of inflow oxygen and outflow fuel from the compartment opening were, from largest to smallest, Door > $Slot_U$ ~ $Slot_M$ > $Slot_L$. However, the fuel and oxygen were the best mixed for the $Slot_U$ case while the fuel and oxygen were not well mixed and in relatively separated two layers for the $Slot_L$ case. The global equivalence ratio defined by the amounts of fuel and oxygen in the compartment was not correlated reasonably with the peak pressure of backdraft. The peak pressure during backdraft was the highest for the $Slot_U$ case, a well mixed condition of fuel and air, and backdraft was not found for the $Slot_L$ where the pressure rise was not so high due to the mixing status. The peak pressures for the Door and $Slot_M$ cases were in between Door and $Slot_L$ cases. The peak pressure during backdraft was well correlated with the total amount of heat release until the instance of backdraft occurrence.