Cristian D. Avila Jimenez , Andrew Macfarlane , Felipe Campuzano , Santiago Cardona , Matthew Dunn , Thibault F. Guiberti , Assaad R. Masri , William L. Roberts
{"title":"混合燃料和二次空气喷射对两级NH3-CH4/H2旋流火焰的稳定性、形态和动力学的影响","authors":"Cristian D. Avila Jimenez , Andrew Macfarlane , Felipe Campuzano , Santiago Cardona , Matthew Dunn , Thibault F. Guiberti , Assaad R. Masri , William L. Roberts","doi":"10.1016/j.proci.2025.105817","DOIUrl":null,"url":null,"abstract":"<div><div>Ammonia (NH<sub>3</sub>) has been identified as a potential carbon-free fuel to decarbonize power generation by gas turbines. However, challenges associated with flame stabilization and emissions must be solved. Two-stage, rich-lean combustion is a promising strategy that requires fine control of the secondary stage parameters, where air is injected to oxidize the remaining unburned fuel from the rich primary stage. This study investigates the effects of the fuel blend composition (NH<sub>3</sub>-CH<sub>4</sub> and NH<sub>3</sub>-H<sub>2</sub>), NH<sub>3</sub>vol fraction (X<sub>NH3</sub>), primary (<em>ϕ<sub>primary</sub></em>) and global (<em>ϕ<sub>global</sub></em>) equivalence ratios, and geometry of the secondary air injection (number and diameter of holes) on the morphology of the lean secondary and rich-premixed primary flames, and primary flame stability and dynamics. Experiments are conducted with a lab-scale piloted burner inspired by the AE-T100’s micro gas turbine burner. By increasing the secondary air flow rate (<em>Q<sub>sec</sub></em>), <em>ϕ<sub>global</sub></em> varied from 0.91 down to a value that produces primary flame morphology changes (<em>ϕ<sub>global,FC</sub></em>), and then to a minimum value that eventually led to flame instability followed by blowout (<em>ϕ<sub>global,BO</sub></em>). These thresholds were found to depend on fuel composition and air injection geometry. High-speed chemiluminescence imaging of NH<sub>2</sub>* combined with Dynamic Mode Decomposition (DMD) revealed distinct instability mechanisms: CH₄-blended flames exhibited longitudinal pulsations, while H₂-blended flames showed a rotating inner core that reignites upstream reactants. These instabilities are linked with a combustion regime transition for the secondary combustion zone, from diffusion-like to premixed-like (or partially premixed), indicative of an optimum <em>ϕ<sub>global</sub></em> for each geometry. Finally, increasing the number of secondary air holes (while keeping diameter constant) extended flame stability to leaner <em>ϕ<sub>global</sub></em>. Data showed that the geometry of the secondary air injection is more important for stability than other varied parameters, a valuable finding for the design of future two-stage, rich-lean NH<sub>3</sub> burners.</div></div>","PeriodicalId":408,"journal":{"name":"Proceedings of the Combustion Institute","volume":"41 ","pages":"Article 105817"},"PeriodicalIF":5.2000,"publicationDate":"2025-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Fuel blend and secondary air injection effects on the stability, morphology, and dynamics of two-stage NH3-CH4/H2 swirl flames\",\"authors\":\"Cristian D. Avila Jimenez , Andrew Macfarlane , Felipe Campuzano , Santiago Cardona , Matthew Dunn , Thibault F. Guiberti , Assaad R. Masri , William L. Roberts\",\"doi\":\"10.1016/j.proci.2025.105817\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Ammonia (NH<sub>3</sub>) has been identified as a potential carbon-free fuel to decarbonize power generation by gas turbines. However, challenges associated with flame stabilization and emissions must be solved. Two-stage, rich-lean combustion is a promising strategy that requires fine control of the secondary stage parameters, where air is injected to oxidize the remaining unburned fuel from the rich primary stage. This study investigates the effects of the fuel blend composition (NH<sub>3</sub>-CH<sub>4</sub> and NH<sub>3</sub>-H<sub>2</sub>), NH<sub>3</sub>vol fraction (X<sub>NH3</sub>), primary (<em>ϕ<sub>primary</sub></em>) and global (<em>ϕ<sub>global</sub></em>) equivalence ratios, and geometry of the secondary air injection (number and diameter of holes) on the morphology of the lean secondary and rich-premixed primary flames, and primary flame stability and dynamics. Experiments are conducted with a lab-scale piloted burner inspired by the AE-T100’s micro gas turbine burner. By increasing the secondary air flow rate (<em>Q<sub>sec</sub></em>), <em>ϕ<sub>global</sub></em> varied from 0.91 down to a value that produces primary flame morphology changes (<em>ϕ<sub>global,FC</sub></em>), and then to a minimum value that eventually led to flame instability followed by blowout (<em>ϕ<sub>global,BO</sub></em>). These thresholds were found to depend on fuel composition and air injection geometry. High-speed chemiluminescence imaging of NH<sub>2</sub>* combined with Dynamic Mode Decomposition (DMD) revealed distinct instability mechanisms: CH₄-blended flames exhibited longitudinal pulsations, while H₂-blended flames showed a rotating inner core that reignites upstream reactants. 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Fuel blend and secondary air injection effects on the stability, morphology, and dynamics of two-stage NH3-CH4/H2 swirl flames
Ammonia (NH3) has been identified as a potential carbon-free fuel to decarbonize power generation by gas turbines. However, challenges associated with flame stabilization and emissions must be solved. Two-stage, rich-lean combustion is a promising strategy that requires fine control of the secondary stage parameters, where air is injected to oxidize the remaining unburned fuel from the rich primary stage. This study investigates the effects of the fuel blend composition (NH3-CH4 and NH3-H2), NH3vol fraction (XNH3), primary (ϕprimary) and global (ϕglobal) equivalence ratios, and geometry of the secondary air injection (number and diameter of holes) on the morphology of the lean secondary and rich-premixed primary flames, and primary flame stability and dynamics. Experiments are conducted with a lab-scale piloted burner inspired by the AE-T100’s micro gas turbine burner. By increasing the secondary air flow rate (Qsec), ϕglobal varied from 0.91 down to a value that produces primary flame morphology changes (ϕglobal,FC), and then to a minimum value that eventually led to flame instability followed by blowout (ϕglobal,BO). These thresholds were found to depend on fuel composition and air injection geometry. High-speed chemiluminescence imaging of NH2* combined with Dynamic Mode Decomposition (DMD) revealed distinct instability mechanisms: CH₄-blended flames exhibited longitudinal pulsations, while H₂-blended flames showed a rotating inner core that reignites upstream reactants. These instabilities are linked with a combustion regime transition for the secondary combustion zone, from diffusion-like to premixed-like (or partially premixed), indicative of an optimum ϕglobal for each geometry. Finally, increasing the number of secondary air holes (while keeping diameter constant) extended flame stability to leaner ϕglobal. Data showed that the geometry of the secondary air injection is more important for stability than other varied parameters, a valuable finding for the design of future two-stage, rich-lean NH3 burners.
期刊介绍:
The Proceedings of the Combustion Institute contains forefront contributions in fundamentals and applications of combustion science. For more than 50 years, the Combustion Institute has served as the peak international society for dissemination of scientific and technical research in the combustion field. In addition to author submissions, the Proceedings of the Combustion Institute includes the Institute''s prestigious invited strategic and topical reviews that represent indispensable resources for emergent research in the field. All papers are subjected to rigorous peer review.
Research papers and invited topical reviews; Reaction Kinetics; Soot, PAH, and other large molecules; Diagnostics; Laminar Flames; Turbulent Flames; Heterogeneous Combustion; Spray and Droplet Combustion; Detonations, Explosions & Supersonic Combustion; Fire Research; Stationary Combustion Systems; IC Engine and Gas Turbine Combustion; New Technology Concepts
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