Flashback Propensity of Premixed Jet Flames Operated on Synthetic Gaseous Fuel with Alternative Burner Configurations and Materials PDF Download
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Author: Zhixuan Duan
Publisher:
ISBN: 9781303612572
Category :
Languages : en
Pages : 195
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Book Description
Hydrogen enriched fuel generated from a variety of resources such as coal and biomass gasification provides an extra option for lean premixed combustion systems. Flashback is the main operability issue associated with this application. In the present work, boundary layer flashback in a jet flame configuration is investigated. Previous research is extended to more practical conditions where turbulent flows with alternative fuels are prevalent. The importance of burner rim conditions, recently revealed, is investigated systematically in the current work. To fulfill the research goals, a jet burner with interchangeable configuration and materials was built. An inline heater provided preheated air up to 810 K. Systematic studies addressing the quantitative influence of various parameters such as fuel compositions, inlet temperature, burner tip temperature, burner material, enclosure size, and burner diameter on flashback propensity were conducted. A comprehensive overview of the flashback limits for all conditions tested in the current study as well as those published previously is presented. The collective results indicate that the burner materials, tip temperature and flame confinement play significant roles for flashback propensity. A statistics based model demonstrated that better correlations arise when the tip temperature is introduced as an input, whereas a physical model revealed that the critical velocity gradient when flashback occurs is proportional to the laminar flame speed computed based on the tip temperature. The addition of multiple parameters further refined the prediction of the flashback propensity. The present work used a heat transfer analysis to show that the upstream flame propagation during flashback is affected by the burner material. The material with lower thermal conductivity yields larger flashback propensity but slower flame regression inside the tube. These observations can be potentially exploited to minimize the negative impacts of flashback in practical applications. A heat transfer model, developed to estimate burner tip temperature, was successful in demonstrating the potential of advanced heat transfer modeling in predicting flashback propensity of alternative fuels with a given burner configuration.
Author: Zhixuan Duan
Publisher:
ISBN: 9781303612572
Category :
Languages : en
Pages : 195
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Book Description
Hydrogen enriched fuel generated from a variety of resources such as coal and biomass gasification provides an extra option for lean premixed combustion systems. Flashback is the main operability issue associated with this application. In the present work, boundary layer flashback in a jet flame configuration is investigated. Previous research is extended to more practical conditions where turbulent flows with alternative fuels are prevalent. The importance of burner rim conditions, recently revealed, is investigated systematically in the current work. To fulfill the research goals, a jet burner with interchangeable configuration and materials was built. An inline heater provided preheated air up to 810 K. Systematic studies addressing the quantitative influence of various parameters such as fuel compositions, inlet temperature, burner tip temperature, burner material, enclosure size, and burner diameter on flashback propensity were conducted. A comprehensive overview of the flashback limits for all conditions tested in the current study as well as those published previously is presented. The collective results indicate that the burner materials, tip temperature and flame confinement play significant roles for flashback propensity. A statistics based model demonstrated that better correlations arise when the tip temperature is introduced as an input, whereas a physical model revealed that the critical velocity gradient when flashback occurs is proportional to the laminar flame speed computed based on the tip temperature. The addition of multiple parameters further refined the prediction of the flashback propensity. The present work used a heat transfer analysis to show that the upstream flame propagation during flashback is affected by the burner material. The material with lower thermal conductivity yields larger flashback propensity but slower flame regression inside the tube. These observations can be potentially exploited to minimize the negative impacts of flashback in practical applications. A heat transfer model, developed to estimate burner tip temperature, was successful in demonstrating the potential of advanced heat transfer modeling in predicting flashback propensity of alternative fuels with a given burner configuration.
Author: Zhi-Xuan Duan
Publisher:
ISBN: 9781267745798
Category :
Languages : en
Pages : 130
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Book Description
Various renewable gaseous fuels offer the opportunity to meet increasing energy demands and address concerns regarding global climate change. Synthetic gas generated from biomass is one such fuel that is an attractive potential substitute fuel for current combustion systems to reduce greenhouse gas emissions. Current advanced combustion systems use lean premixed strategies for minimizing criteria pollutant emissions. For the successful use of syngas in light of varying composition in lean premixed low emission combustion systems, an understanding of the role of composition on performance is required. For example, the high hydrogen content of syngas has been shown to affect the operability of combustion systems and, in particular, the risk of flashback. Hence, the focus of this thesis is on flashback in lean premixed flames under the atmospheric condition. The non-swirling jet flame configuration is chosen to isolate specific flashback mechanisms While the major focus is on the effect of fuel composition, the influence of injector diameter, diluent addition, higher hydrocarbon addition, and injector wall temperature are evaluated as well. The experimental setup consists of a quartz tube that serves as an axisymmetric injector. A quartz enclosure is used to assist with flame stabilization for the lower flame speed fuel compositions. The test procedure for approaching flashback establishes a target adiabatic flame temperature which is held constant while decreasing the mixture flow rate until flashback occurs. To add insight into the flashback mechanism, high speed schlieren imaging is employed to document the dynamic processes of flashback. Observations include 1. The schlieren images indicate the flashback in the present research typically starts in the boundary layer. 2. Different flame stabilization modes occur which have differing flashback tendencies. 3. Flashback propensity increases generally following the trend of laminar flame speed. More hydrogen and higher wall temperatures yield higher a tendency to flashback. 4. There are other factors determining the scale of flashback propensity. It is found that given a similar laminar flame speed and the same mixing ratio (1:1), the flashback propensity of H2/CO is nearly three times more prone to flashback than the mixture of H2/CH4. 5. The laminar flame speed alone cannot predict the flashback propensity. Interactions among other variables, such as wall temperature and fuel properties etc. also affect the flashback. 6. Addition of diluents over a limited range did not strongly impact flashback 7. Addition of ethane to hydrogen reduces flashback propensity more than does the addition of methane or diluents. 8.A statistical model estimates the present test result very well.
Author: Cecil J. Marek
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 18
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Book Description
Author: Omid Askari
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 271
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Book Description
This dissertation investigates the combustion and injection fundamental characteristics of different alternative fuels both experimentally and theoretically. The subjects such as lean partially premixed combustion of methane/hydrogen/air/diluent, methane high pressure direct-injection, thermal plasma formation, thermodynamic properties of hydrocarbon/air mixtures at high temperatures, laminar flames and flame morphology of synthetic gas (syngas) and Gas-to-Liquid (GTL) fuels were extensively studied in this work. These subjects will be summarized in three following paragraphs. The fundamentals of spray and partially premixed combustion characteristics of directly injected methane in a constant volume combustion chamber have been experimentally studied. The injected fuel jet generates turbulence in the vessel and forms a turbulent heterogeneous fuel-air mixture in the vessel, similar to that in a Compressed Natural Gas (CNG) Direct-Injection (DI) engines. The effect of different characteristics parameters such as spark delay time, stratification ratio, turbulence intensity, fuel injection pressure, chamber pressure, chamber temperature, Exhaust Gas recirculation (EGR) addition, hydrogen addition and equivalence ratio on flame propagation and emission concentrations were analyzed. As a part of this work and for the purpose of control and calibration of high pressure injector, spray development and characteristics including spray tip penetration, spray cone angle and overall equivalence ratio were evaluated under a wide range of fuel injection pressures of 30 to 90 atm and different chamber pressures of 1 to 5 atm. Thermodynamic properties of hydrocarbon/air plasma mixtures at ultra-high temperatures must be precisely calculated due to important influence on the flame kernel formation and propagation in combusting flows and spark discharge applications. A new algorithm based on the statistical thermodynamics was developed to calculate the ultra-high temperature plasma composition and thermodynamic properties. The method was applied to compute the thermodynamic properties of hydrogen/air and methane/air plasma mixtures for a wide range of temperatures (1,000-100,000 K), pressures (10−6-100 atm) and different equivalence ratios within flammability limit. In calculating the individual thermodynamic properties of the atomic species, the Debye-Huckel cutoff criterion has been used for terminating the series expression of the electronic partition function. A new differential-based multi-shell model was developed in conjunction with Schlieren photography to measure laminar burning speed and to study the flame instabilities for different alternative fuels such as syngas and GTL. Flame instabilities such as cracking and wrinkling were observed during flame propagation and discussed in terms of the hydrodynamic and thermo-diffusive effects. Laminar burning speeds were measured using pressure rise data during flame propagation and power law correlations were developed over a wide range of temperatures, pressures and equivalence ratios. As a part of this work, the effect of EGR addition and substitution of nitrogen with helium in air on flame morphology and laminar burning speed were extensively investigated. The effect of cell formation on flame surface area of syngas fuel in terms of a newly defined parameter called cellularity factor was also evaluated. In addition to that the experimental onset of auto-ignition and theoretical ignition delay times of premixed GTL/air mixture were determined at high pressures and low temperatures over a wide range of equivalence ratios.
Author: Nasser Shelil
Publisher: LAP Lambert Academic Publishing
ISBN: 9783659691287
Category :
Languages : en
Pages : 292
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Book Description
Lean premixed combustion is one of the new technologies of pollutants reduction in gas turbines. The main problem of premixed combustion is flashback. CFD modelling is used to simulate the combustion of premixed swirl burner that uses different types of fuels. Flashback simulation studies are performed for a wide range of fuels, operating conditions and burner design. The results show many approaches to reduce the flashback.The flashback can be reduced by lowering the turbulent intensity, adding Carbon Dioxide to the fuel, using fuel blends specially in the case of Hydrogen combustion and/or operating with lean premixed mixtures. Experiments are carried out to validate the results obtained by the CFD simulation and confirm the model validity.
Author: Bidhan Kumar Dam
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages :
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Author: Arthur H. Lefebvre
Publisher: CRC Press
ISBN: 1498736262
Category : Technology & Engineering
Languages : en
Pages : 284
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Book Description
The second edition of this long-time bestseller provides a framework for designing and understanding sprays for a wide array of engineering applications. The text contains correlations and design tools that can be easily understood and used in relating the design of atomizers to the resulting spray behavior. Written to be accessible to readers with a modest technical background, the emphasis is on application rather than in-depth theory. Numerous examples are provided to serve as starting points for using the information in the book. Overall, this is a thoroughly updated edition that still retains the practical focus and readability of the original work by Arthur Lefebvre.
Author: Tershia A. Pinder
Publisher:
ISBN:
Category :
Languages : en
Pages : 310
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Author: Christopher Eric Schneider
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
The dynamics of flame flashback were studied in a lean premixed swirl burner with central bluff-body. A range of conditions with varied flow velocities, inlet temperatures, and hydrogen/methane flow rates were investigated. Intermittent movement of the flame into the feed tube, was found over a range of conditions, with consistent trends as the system moved from stable operation to complete flashback. Statistical analysis of chemiluminescence data showed a strong link between characteristic behaviours of the system, such as the statistical frequency of upstream propagating flame protrusions, and the magnitude of the flashback, independent of the inlet conditions. Effects of conditions on the flashback magnitude and abruptness of transition are described. Existing metrics for predicting flashback were found to be inadequate for describing the observed dynamics. Laser diagnostics revealed only a slight statistical drop in axial flow velocity upstream of the flame, which appeared to strengthen as the flame moved upstream.
Author: Joe Whiteaker
Publisher:
ISBN:
Category :
Languages : en
Pages : 210
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Book Description
