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    Effect of Inert Species on the Static and Dynamic Stability of a Piloted, Swirl-Stabilized Flame

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 006::page 61021-1
    Author:
    Rodriguez Camacho, Javier
    ,
    Akiki, Michel
    ,
    Blust, James
    ,
    O'Connor, Jacqueline
    DOI: 10.1115/1.4064048
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Carbon sequestration and utilization has been proposed as a method for decarbonizing high-efficiency industrial gas turbines operating on natural gas fuels for power generation and industrial markets. To increase the efficiency of the carbon removal process from the exhaust stream of the turbine, exhaust gas recirculation (EGR) can be used. EGR recycles a portion of the engine exhaust into the inlet, increasing the concentration of inert species in the exhaust stream to improve the performance and cost-effectiveness of CO2 separation systems. This strategy can, however, reduce the oxygen concentration in the air, leading to changes in flame stabilization in the combustor. In this study, we investigate the effect of air diluted with inert gases of different compositions and the impact that these mixtures have on flame static and dynamic stability. A swirl-stabilized flame in a single-nozzle, variable-length combustor is used to measure the flame behavior for oxygen concentrations of 15–21% by volume. A constant adiabatic flame temperature test matrix is conducted to mimic operation in an industrial gas turbine. High-speed chemiluminescence imaging is used to determine the change in flame shape and dynamics for each gas composition. As the oxygen concentration decreases, the flame lifts from the centerbody, resulting in an aerodynamically stabilized flame at the lowest O2 concentrations. Different compositions of gases result in different flame shapes, where higher levels of N2 in the diluents result in more flame stabilization in the outer recirculation zone as compared to those with higher levels of CO2. The flame oscillation mechanisms also change with oxygen concentration, where the lifted flames at low O2 levels exhibit an ignition/extinction oscillation mode as compared to a vortex-shedding-coupled oscillation mode at high O2 levels where the flame is stabilized on the centerbody. Companion chemical kinetics simulations are used to explain changes in the flame's shape and behavior.
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      Effect of Inert Species on the Static and Dynamic Stability of a Piloted, Swirl-Stabilized Flame

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4295241
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    contributor authorRodriguez Camacho, Javier
    contributor authorAkiki, Michel
    contributor authorBlust, James
    contributor authorO'Connor, Jacqueline
    date accessioned2024-04-24T22:27:02Z
    date available2024-04-24T22:27:02Z
    date copyright1/12/2024 12:00:00 AM
    date issued2024
    identifier issn0742-4795
    identifier othergtp_146_06_061021.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295241
    description abstractCarbon sequestration and utilization has been proposed as a method for decarbonizing high-efficiency industrial gas turbines operating on natural gas fuels for power generation and industrial markets. To increase the efficiency of the carbon removal process from the exhaust stream of the turbine, exhaust gas recirculation (EGR) can be used. EGR recycles a portion of the engine exhaust into the inlet, increasing the concentration of inert species in the exhaust stream to improve the performance and cost-effectiveness of CO2 separation systems. This strategy can, however, reduce the oxygen concentration in the air, leading to changes in flame stabilization in the combustor. In this study, we investigate the effect of air diluted with inert gases of different compositions and the impact that these mixtures have on flame static and dynamic stability. A swirl-stabilized flame in a single-nozzle, variable-length combustor is used to measure the flame behavior for oxygen concentrations of 15–21% by volume. A constant adiabatic flame temperature test matrix is conducted to mimic operation in an industrial gas turbine. High-speed chemiluminescence imaging is used to determine the change in flame shape and dynamics for each gas composition. As the oxygen concentration decreases, the flame lifts from the centerbody, resulting in an aerodynamically stabilized flame at the lowest O2 concentrations. Different compositions of gases result in different flame shapes, where higher levels of N2 in the diluents result in more flame stabilization in the outer recirculation zone as compared to those with higher levels of CO2. The flame oscillation mechanisms also change with oxygen concentration, where the lifted flames at low O2 levels exhibit an ignition/extinction oscillation mode as compared to a vortex-shedding-coupled oscillation mode at high O2 levels where the flame is stabilized on the centerbody. Companion chemical kinetics simulations are used to explain changes in the flame's shape and behavior.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Inert Species on the Static and Dynamic Stability of a Piloted, Swirl-Stabilized Flame
    typeJournal Paper
    journal volume146
    journal issue6
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4064048
    journal fristpage61021-1
    journal lastpage61021-10
    page10
    treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 006
    contenttypeFulltext
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