An Investigation of Lean Blowout of Gaseous Fuel Alternatives to Natural Gas

An Investigation of Lean Blowout of Gaseous Fuel Alternatives to Natural Gas PDF Author: Megan Karalus
Publisher:
ISBN:
Category : Combustion engineering
Languages : en
Pages : 188

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Book Description
This work examines lean premixed flame stability for multi-component fuel mixtures to support fuel flexibility for industrial combustors. A single Jet Stirred Reactor (JSR), a generic recirculation stabilized combustor, along with gaseous fuels of hydrogen, methane, and hydrogen/methane blends are chosen for the study. Experimental data on blowout are collected and a series of models are used to understand the mechanism of extinction in this recirculation-stabilized flame environment. By studying this more generic combustor, the aim is to develop generalizable results and methodologies for understanding and predicting lean blowout of multicomponent fuels. Experimental data approaching blowout are taken for fuels of pure hydrogen, pure methane, and hydrogen/methane blends in 10% by volume increments. The data relate inlet equivalence ratios to experimentally measured temperatures for each fuel approaching blowout and reveal the final blowout condition for each fuel. These blowout data are obtained by holding the air flow rate constant and decreasing the fuel flow rate until the flame is extinguished. Doing so holds the flow field and turbulence parameters approximately constant as blowout is approached. The reactor is stabilized to lower equivalence ratios and temperatures as the percentage of hydrogen in the fuel increases. In order to gain insight on the mechanism controlling blowout, two dimensional, axisymmetric computational fluid dynamic (CFD) simulations are carried out for the lean premixed combustion of both hydrogen and methane as the fuel. Hydrogen requires only 9 species to fully describe its chemistry. Therefore, the detailed mechanism of Li et al. is chosen for the hydrogen simulations. Methane combustion is described by the full GRI-3.0 chemical mechanism with 35 species. To facilitate reasonable computational times a skeletal mechanism of 22 species is developed from GRI-3.0 using the Directed Relation Graph method developed by Lu and Law. The CFD simulations for both hydrogen and methane combustion are run similarly to the experiments. The fuel flow rate is reduced until the CFD model no longer produces a burning solution. Contour plots from the CFD model illustrate the evolution of the flow-field, temperature profiles, and flame structure within the JSR as blowout is approached for both fuels. The modeling suggests that lean blowout in the JSR does not occur in a spatially homogeneous condition, but rather under a zonal structure. Analysis of the models from the perspective of a combusting fluid particle traveling through the jet, into the recirculation zone, and then entraining back into the jet suggests that the blowout condition is dependent on the development of the pool of radicals. The flame remains stable as long as the radical pool develops significantly enough to achieve ignition before the hypothetical combusting fluid particle is re-entrained. As the fuel flow decreases, the induction period increases and the ignition event is pushed further around the recirculation zone. Eventually, the induction period becomes so long that the ignition is incomplete at the point where the recirculating gas is entrained. This threshold leads to overall flame extinction. Two Chemical Reactor Network (CRN) models are developed using the flow field and reaction fields from the detailed CFD models in an attempt to capture the bulk of the physical processes responsible for flame stability. The single Plug Flow Reactor (PFR) model follows the concept of the hypothetical combusting fluid particle and assumes that only convective transport is responsible for stability. This model matches hydrogen blowout well, reproducing the ignition event and the development of the pool of radicals before re-entrainment. While the single PFR model with the UCSD chemical mechanism does predict the blowout temperature across the full range of methane/hydrogen fuel blends well, it fails to adequately predict blowout equivalence ratio for fuels with high methane concentrations. A two PFR model is subsequently developed in which the core jet region (of constant mass flow) exchanges mass with the recirculation region through turbulent diffusive transport. Entrainment of flow by jet action is confined entirely to the recirculation region, represented by the exhaust of the recirculation PFR being convectively re-entrained at its entrance. The two PFR model performs about as well as the single PFR model in predicting blowout for hydrogen in the JSR and shows significant improvement over the single PFR model in both following the experimental data approaching blowout, and predicting the blowout condition for methane. In fact the two PFR model shows good agreement with both equivalence ratio and temperature at blowout across the full range of hydrogen/methane blends. Regardless of the chemical mechanism applied, or whether we consider transport by convection only as in the single PFR model, or transport by both convection and diffusion as in the two PFR model, the story regarding the onset of blowout remains the same and is consistent with that given by CFD as well: the key to the stable operation of the reactor is the ignition event in the recirculation zone, resulting in the development of the radical pool. For pure hydrogen combustion as the fuel flow rate is reduced and the reactor moves towards blowout the destruction of the fuel slows and spreads, and the development of the radical pool moves further around the recirculation zone. The radical pool must develop (i.e. ignition must occur) before re-entrainment or the reactor will extinguish. For methane we similarly see the destruction of methane spread, and the net production of CO, and subsequently the net production of OH move further around the recirculation zone until the re-entrainment of radicals can no longer sustain the combustion. For methane, transport of the CO and radicals through turbulent diffusion appears to be a controlling process in this ignition event. The ignition event for hydrogen, on the other hand, is affected very little by the inclusion of diffusive transport of radicals. This is most likely due to the fact that the breakdown of hydrogen directly produces an H radical that feeds the chain propagating reaction, however the direct breakdown of methane has no such feedback. It is only in the destruction of methane intermediates that the H radical needed to feed the chain propagating reaction is produced.

An Investigation of Lean Blowout of Gaseous Fuel Alternatives to Natural Gas

An Investigation of Lean Blowout of Gaseous Fuel Alternatives to Natural Gas PDF Author: Megan Karalus
Publisher:
ISBN:
Category : Combustion engineering
Languages : en
Pages : 188

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Book Description
This work examines lean premixed flame stability for multi-component fuel mixtures to support fuel flexibility for industrial combustors. A single Jet Stirred Reactor (JSR), a generic recirculation stabilized combustor, along with gaseous fuels of hydrogen, methane, and hydrogen/methane blends are chosen for the study. Experimental data on blowout are collected and a series of models are used to understand the mechanism of extinction in this recirculation-stabilized flame environment. By studying this more generic combustor, the aim is to develop generalizable results and methodologies for understanding and predicting lean blowout of multicomponent fuels. Experimental data approaching blowout are taken for fuels of pure hydrogen, pure methane, and hydrogen/methane blends in 10% by volume increments. The data relate inlet equivalence ratios to experimentally measured temperatures for each fuel approaching blowout and reveal the final blowout condition for each fuel. These blowout data are obtained by holding the air flow rate constant and decreasing the fuel flow rate until the flame is extinguished. Doing so holds the flow field and turbulence parameters approximately constant as blowout is approached. The reactor is stabilized to lower equivalence ratios and temperatures as the percentage of hydrogen in the fuel increases. In order to gain insight on the mechanism controlling blowout, two dimensional, axisymmetric computational fluid dynamic (CFD) simulations are carried out for the lean premixed combustion of both hydrogen and methane as the fuel. Hydrogen requires only 9 species to fully describe its chemistry. Therefore, the detailed mechanism of Li et al. is chosen for the hydrogen simulations. Methane combustion is described by the full GRI-3.0 chemical mechanism with 35 species. To facilitate reasonable computational times a skeletal mechanism of 22 species is developed from GRI-3.0 using the Directed Relation Graph method developed by Lu and Law. The CFD simulations for both hydrogen and methane combustion are run similarly to the experiments. The fuel flow rate is reduced until the CFD model no longer produces a burning solution. Contour plots from the CFD model illustrate the evolution of the flow-field, temperature profiles, and flame structure within the JSR as blowout is approached for both fuels. The modeling suggests that lean blowout in the JSR does not occur in a spatially homogeneous condition, but rather under a zonal structure. Analysis of the models from the perspective of a combusting fluid particle traveling through the jet, into the recirculation zone, and then entraining back into the jet suggests that the blowout condition is dependent on the development of the pool of radicals. The flame remains stable as long as the radical pool develops significantly enough to achieve ignition before the hypothetical combusting fluid particle is re-entrained. As the fuel flow decreases, the induction period increases and the ignition event is pushed further around the recirculation zone. Eventually, the induction period becomes so long that the ignition is incomplete at the point where the recirculating gas is entrained. This threshold leads to overall flame extinction. Two Chemical Reactor Network (CRN) models are developed using the flow field and reaction fields from the detailed CFD models in an attempt to capture the bulk of the physical processes responsible for flame stability. The single Plug Flow Reactor (PFR) model follows the concept of the hypothetical combusting fluid particle and assumes that only convective transport is responsible for stability. This model matches hydrogen blowout well, reproducing the ignition event and the development of the pool of radicals before re-entrainment. While the single PFR model with the UCSD chemical mechanism does predict the blowout temperature across the full range of methane/hydrogen fuel blends well, it fails to adequately predict blowout equivalence ratio for fuels with high methane concentrations. A two PFR model is subsequently developed in which the core jet region (of constant mass flow) exchanges mass with the recirculation region through turbulent diffusive transport. Entrainment of flow by jet action is confined entirely to the recirculation region, represented by the exhaust of the recirculation PFR being convectively re-entrained at its entrance. The two PFR model performs about as well as the single PFR model in predicting blowout for hydrogen in the JSR and shows significant improvement over the single PFR model in both following the experimental data approaching blowout, and predicting the blowout condition for methane. In fact the two PFR model shows good agreement with both equivalence ratio and temperature at blowout across the full range of hydrogen/methane blends. Regardless of the chemical mechanism applied, or whether we consider transport by convection only as in the single PFR model, or transport by both convection and diffusion as in the two PFR model, the story regarding the onset of blowout remains the same and is consistent with that given by CFD as well: the key to the stable operation of the reactor is the ignition event in the recirculation zone, resulting in the development of the radical pool. For pure hydrogen combustion as the fuel flow rate is reduced and the reactor moves towards blowout the destruction of the fuel slows and spreads, and the development of the radical pool moves further around the recirculation zone. The radical pool must develop (i.e. ignition must occur) before re-entrainment or the reactor will extinguish. For methane we similarly see the destruction of methane spread, and the net production of CO, and subsequently the net production of OH move further around the recirculation zone until the re-entrainment of radicals can no longer sustain the combustion. For methane, transport of the CO and radicals through turbulent diffusion appears to be a controlling process in this ignition event. The ignition event for hydrogen, on the other hand, is affected very little by the inclusion of diffusive transport of radicals. This is most likely due to the fact that the breakdown of hydrogen directly produces an H radical that feeds the chain propagating reaction, however the direct breakdown of methane has no such feedback. It is only in the destruction of methane intermediates that the H radical needed to feed the chain propagating reaction is produced.

A Study of Pollutant Formation from the Lean Premixed Combustion of Gaseous Fuel Alternatives to Natural Gas

A Study of Pollutant Formation from the Lean Premixed Combustion of Gaseous Fuel Alternatives to Natural Gas PDF Author: Keith Boyd Fackler
Publisher:
ISBN:
Category : Combustion gases
Languages : en
Pages : 185

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Book Description
The goal of this research is to identify how nitrogen oxide (NOx) emissions and flame stability (blowout) are impacted by the use of fuels that are alternatives to typical pipeline natural gas. The research focuses on lean, premixed combustors that are typically used in state-of-the-art natural gas fueled systems. An idealized laboratory lean premixed combustor, specifically the jet-stirred reactor, is used for experimental data. A series of models, including those featuring detailed fluid dynamics and those focusing on detailed chemistry, are used to interpret the data and understand the underlying chemical kinetic reasons for differences in emissions between the various fuel blends. An ultimate goal is to use these data and interpretive tools to develop a way to predict the emission and stability impacts of changing fuels within practical combustors. All experimental results are obtained from a high intensity, single-jet stirred reactor (JSR). Five fuel categories are studied: (1) pure H2, (2) process and refinery gas, including combinations of H2, CH4, C2H6, and C3H8, (3) oxygen blown gasified coal/petcoke composed of H2, CO, and CO2, (4) landfill and digester gas composed of CH4, CO2, and N2, and (5) liquified natural gas (LNG)/shale/associated gases composed of CH4, C2H6, and C3H8. NOx measurements are taken at a nominal combustion temperature of 1800 K, atmospheric pressure, and a reactor residence time of 3 ms. This is done to focus the results on differences caused by fuel chemistry by comparing all fuels at a common temperature, pressure, and residence time. This is one of the few studies in the literature that attempts to remove these effects when studying fuels varying in composition. Additionally, the effects of changing temperature and residence time are investigated for selected fuels. At the nominal temperature and residence time, the experimental and modeling results show the following trends for NOx emissions as a function of fuel type: 1.) NOx emissions decrease with increasing H2 fuel fraction for combustion of CH4/H2 blends. This appears to be caused by a reduction in the amount of NO made by the prompt pathway involving the reaction of N2 with hydrocarbon radicals as the CH4 is replaced by H2. 2.) For category 2 (the process and refinery blend) and category 5 (the LNG, shale, and associated gases), NOx emissions increase with the addition of C2 and C3 hydrocarbons. This could be due to an increased production of free radicals resulting from increasing CO production when higher molecular weight hydrocarbons are broken down. 3.) For category 3 (the O2 blown gasified coal/petcoke), NOx emissions increase with increasing CO fuel fraction. The reason for this is attributed to CO producing more radicals per unit heat release than H2. When CO replaces H2, an increase in NOx emissions is seen due to an increase in the productivity of the N2O, NNH, and Zeldovich pathways. 4.) For category 4 (the landfill gas) the addition of diluents such as CO2 and N2 at constant air flow produces more NOx per kg of CH4 consumed, and N2 is more effective than CO2 in increasing the NOx emission index. The increase in emission index appears to be due to an enhancement of the prompt NOx pathway as the diluents are added and the mixture moves towards stoichiometric. In addition, the presence of CO2 as a diluent catalyzes the loss of flame radicals, leading to less NOx formation than when an equivalent amount of N2 is used as a diluent. For a selected set of fuels, detailed spacial reactor probing is carried out. At the nominal temperature and residence time, the experimental results show the following trends for flame structure as a function of fuel type: 1.) Pure H2 is far more reactive in comparison to CH4 and all other pure alkane fuels. This results in relatively flat NOx and temperature profiles; whereas, the alkane fuels drop in both temperature and NOx production in the jet, where more fresh reactor feed gases are present. 2.) For category 2 (the Process and Refinery blends), H2 addition increases reactivity in the jet while decreasing overall NOx emissions. The increased reactivity is especially evident in the CO profiles where the fuels blended with C2H6 and H2 have CO peaks on jet centerline and CO emissions for pure CH4 peaks slightly off centerline. 3.) For category 3 (the O2 blown gasified coal/petcoke), the temperature profiles for the gasification blend and pure H2 are nearly identical, which is likely due to the high reactivity of H2 dominating the relatively low reactivity of CO. Despite a small temperature difference, the addition of CO causes an increase in NOx production. 4.) For category 4 (the landfill gas), the temperature profiles are virtually indistinguishable. However, the addition of diluent decreases reactivity and spreads out the reaction zone with the CO concentration peaking at 2 mm off of centerline instead of 1 mm. Diluent addition increases NOx production in comparison to pure CH4 for reasons explained above. 5.) For category 5 (the LNG, shale, and associated gases), the temperature profiles are all very similar. The increased reactivity of C2H6 is evident from looking at the CO profiles. Increased C2H6 promotes CO production on jet centerline which is indicative of the hydrocarbon material breaking down earlier in the jet. At temperatures and residence times other than the nominal conditions, the experimental results show the following trends: 1,) The NOx emissions from LPM combustion of pure CH4, H2, C2H6, and C3H8 are shown to vary linearly with residence time and in an Arrhenius fashion with temperature. This occurs because (1) more reaction time leads to more NOx formation, and (2) NOx formation is a strong, non-linear function of temperature. 2.) The addition of both H2 and C2H6 to a LPM CH4 flame is effective at extending its lean blowout limit. The results of both two and three dimensional CFD simulations are presented to illustrate the general flow, temperature, and species structure within the reactor. Since the two dimensional model is far more computationally efficient, it is employed to study various fuel mixtures with more sophisticated chemical mechanisms. The CFD results from the LPM combustion of H2, H2/CO, and CH4 with NOx formation are presented. A three dimensional CFD simulation is run for LPM CH4 combustion that uses a global CH4 oxidation mechanism. While this model does not predict intermediate radicals and NOx, the CO contours and flow field can be used as guidelines to develop a chemical reactor network (CRN), which can incorporate detailed chemistry. In addition, this model runs quickly enough that it is a good way to initialize the temperature and flow field for simulations that do incorporate more complex chemistry. The two dimensional model is used to illustrate the difference in combustion behavior between the various fuels tested. In particular, it illustrates the geometric locations of the super-equilibrium radical fields and shows where and through which pathways NOx is formed. The pathway breakdowns show good agreement with the CRN modeling results. The main goal of the CFD modeling is to use the results of each model to develop Chemical Reactor Networks, CRNs, that are customized for a particular burner. The CRN can then be used to estimate the impacts due to fuel variation.

Stationary Gas Turbine Alternative Fuels

Stationary Gas Turbine Alternative Fuels PDF Author: J. S. Clark
Publisher: ASTM International
ISBN:
Category :
Languages : en
Pages : 363

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Book Description


Stationary Gas Turbine Alternative Fuels

Stationary Gas Turbine Alternative Fuels PDF Author: John S. Clark
Publisher: ASTM International
ISBN: 9780803102583
Category : Technology & Engineering
Languages : en
Pages : 374

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Book Description


Gas Turbine Combustion

Gas Turbine Combustion PDF Author: Arthur H. Lefebvre
Publisher: CRC Press
ISBN: 1420086049
Category : Technology & Engineering
Languages : en
Pages : 557

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Book Description
Reflecting the developments in gas turbine combustion technology that have occurred in the last decade, Gas Turbine Combustion: Alternative Fuels and Emissions, Third Edition provides an up-to-date design manual and research reference on the design, manufacture, and operation of gas turbine combustors in applications ranging from aeronautical to power generation. Essentially self-contained, the book only requires a moderate amount of prior knowledge of physics and chemistry. In response to the fluctuating cost and environmental effects of petroleum fuel, this third edition includes a new chapter on alternative fuels. This chapter presents the physical and chemical properties of conventional (petroleum-based) liquid and gaseous fuels for gas turbines; reviews the properties of alternative (synthetic) fuels and conventional-alternative fuel blends; and describes the influence of these different fuels and their blends on combustor performance, design, and emissions. It also discusses the special requirements of aircraft fuels and the problems encountered with fuels for industrial gas turbines. In the updated chapter on emissions, the authors highlight the quest for higher fuel efficiency and reducing carbon dioxide emissions as well as the regulations involved. Continuing to offer detailed coverage of multifuel capabilities, flame flashback, high off-design combustion efficiency, and liner failure studies, this best-selling book is the premier guide to gas turbine combustion technology. This edition retains the style that made its predecessors so popular while updating the material to reflect the technology of the twenty-first century.

Combustion of Gaseous Alternative Fuels in Compression Ignition Engines

Combustion of Gaseous Alternative Fuels in Compression Ignition Engines PDF Author: Mikulski Maciej
Publisher:
ISBN:
Category : Science
Languages : en
Pages :

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Book Description
The problem of alternative fuels for combustion engines has been growing in importance recently. This is connected not only with decreasing fossil fuel resources, but also with the growing concern for the natural environment and the fight against global warming. This paper discusses the possibility of utilizing alternative gaseous fuels in compression-ignition engines, using dual-fuel, gas-liquid operation strategy. Current state of the art of this technology had been introduced, along with its benefits and challenges to be countered. The discussion had been supported by authors own research experience on dual-fuel engines. The latest results of research on the impact of gas composition on combustion process in the Common Rail dual fuel engine had been presented, at the same illustrating the environmental benefits of using gaseous fuels. The Utilization of gaseous fuels with varying composition was illustrated systematically, starting with natural gas. The possibility of using fuels with lower content of methane (the so-called low-calorie gases) was shown by the impact of depleting natural gas with carbon dioxide. Industrial gases, such as syngas contain a large amount of hydrogen, carbon monoxide or higher hydrocarbons (ethane, propane). The possibility of fueling CI engines with these gasses was presented by the influence of enriching natural gas with mentioned components. The results cover engine dynamometer tests for different operating conditions with the analysis of the combustion process and detailed emission measurements discussion. The results of experimental studies were supplemented by simulation results, using mathematical models, developed by the authors for multi-fuel enginesr.

Intelligent Engine Systems

Intelligent Engine Systems PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781719375108
Category :
Languages : en
Pages : 38

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Book Description
The performance and gaseous emissions were measured for a well-stirred reactor operating under lean conditions for two fuels: JP8 and a synthetic Fisher-Tropsch fuel over a range of equivalence ratios from 0.6 down to the lean blowout. The lean blowout characteristics were determined in LBO experiments at loading parameter values from 0.7 to 1.4. The lean blowout characteristics were then explored under higher loading conditions by simulating higher altitude operation with the use of nitrogen as a dilution gas for the air stream. The experiments showed that: (1) The lean blowout characteristics for the two fuels were close under both low loading and high loading conditions. (2) The combustion temperatures and observed combustion efficiencies were similar for the two fuels. (3) The gaseous emissions were similar for the two fuels and the differences in the H2O and CO2 emissions appear to be directly relatable to the C/H ratio for the fuels. Ballal, Dilip Glenn Research Center SYNTHETIC FUELS; GAS TURBINE ENGINES; EXHAUST GASES; EXHAUST EMISSION; JP-8 JET FUEL; FUEL SYSTEMS; CARBON DIOXIDE; COMBUSTION EFFICIENCY; COMBUSTION TEMPERATURE; SIMULATION; WATER; SHOCK TUBES; IGNITION; TIME LAG; FISCHER-TROPSCH PROCESS; BLOWOUTS; AIR FLOW; DILUTION

Handbook of Alternative Fuel Technologies

Handbook of Alternative Fuel Technologies PDF Author: Sunggyu Lee
Publisher: CRC Press
ISBN: 142001451X
Category : Science
Languages : en
Pages : 542

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Book Description
In addition to enabling a clean and energy efficient future, alternative fuel sources are fast becoming a necessity for meeting today's growing demands for low-cost and convenient energy. The Handbook of Alternative Fuel Technologies offers a thorough guide to the science and available technologies for developing alternatives to petroleum fuel sour

From Oil and Gas to Alternate Fuels

From Oil and Gas to Alternate Fuels PDF Author: John Belding
Publisher:
ISBN:
Category : Direct energy conversion
Languages : en
Pages : 60

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Book Description


Alternative Fuels Guidebook

Alternative Fuels Guidebook PDF Author: Richard L. Bechtold
Publisher: SAE International
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 224

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Book Description
This book presents the fundamentals needed to understand the physical and chemical properties of alternative fuels, and how they impact refueling system design and the modification of existing garages for safety. It covers a wide range of fuels including alcohols, gases, and vegetable oils. Chapters cover: Alternative Fuels and Their Origins Properties and Specifications Materials Compatibility Storage and Dispensing Refueling Facility Installation and Garage Facility Modifications and more