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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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