Hybrid rich- and lean-premixed ammonia-hydrogen combustion for mitigation of NOx emissions and thermoacoustic instabilities

被引:8
|
作者
Jin, Ukhwa [1 ]
Kim, Kyu Tae [1 ]
机构
[1] Korea Adv Inst Sci & Technol KAIST, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea
基金
新加坡国家研究基金会;
关键词
Ammonia; Carbon neutrality; Combustion instability; Gas turbine combustion; Hydrogen; Fuel staging; LAMINAR BURNING VELOCITY; STABILITY LIMITS; SWIRL FLAMES; AIR FLAMES; METHANE; REDUCTION; PLASMA;
D O I
10.1016/j.combustflame.2024.113366
中图分类号
O414.1 [热力学];
学科分类号
摘要
The large-scale direct utilization of two carbon-free fuels, ammonia and hydrogen, is currently attracting significant interest in the context of the development of new gas turbine combustion technologies, with paying close attention to the reduction of nitrogen oxides and unburned ammonia emissions. Motivated by recent observations that rich-premixed conditions tend to mitigate excessive NOx emissions from ammonia combustion, and that uniformly blended ammonia-hydrogen fuel/air mixtures tend to increase NOx production exponentially, here we propose a hybrid configuration of hydrogen -doped rich-premixed ammonia-air flames (inner stage) and lean-premixed pure hydrogen -air flames (outer stage) in a radially stratified primary reaction zone. This fuel staging scheme offers a possible mechanism for chemical kinetics-controlled NOx abatement and asymmetryinduced thermoacoustic instability suppression. The relevance and feasibility of the unconventional premixing approach are rigorously evaluated based on detailed measurements of exhaust gas concentrations and selfexcited pressure fluctuations, in conjunction with OH*/NH2*/NH* chemiluminescence and OH PLIF imaging measurements. We observe that drastically different non-homogeneous reaction regions can be stably established in a comparatively compact combustion volume without producing negative flame stabilization effects - such as blowoff of less reactive ammonia flames and flashback of more reactive hydrogen flames. As compared with the uniform-blend baseline condition, the hybrid staging method is shown to significantly mitigate total nitrogen oxides emissions, from 7764 to 310 ppmvd (96 % reduction), and achieving an approximately two-fold reduction in dynamic pressure amplitude. Interestingly, hydrogen-enriched rich-premixed ammonia flames are revealed to exhibit anomalous oscillatory states originating from the preferential diffusion of hydrogen molecules and reaction rate-dependent separation of reactive layers, enabling interacting non-homogeneous reaction zones with markedly different characteristic time scales to resist the growth of intense pressure perturbations.
引用
收藏
页数:11
相关论文
共 20 条
  • [1] Intrinsic combustion instabilities in ammonia-hydrogen/methane non-premixed flames
    Antar, Elie
    Robert, Etienne
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2024, 40 (1-4)
  • [2] Experimental investigation of lean-premixed hydrogen combustion instabilities in a can-annular combustion system
    Moon, Kihun
    Choi, Yongseok
    Kim, Kyu Tae
    [J]. COMBUSTION AND FLAME, 2022, 235
  • [3] Preliminary study on lean premixed combustion of ammonia-hydrogen for swirling gas turbine combustors
    Valera-Medina, A.
    Pugh, D. G.
    Marsh, P.
    Bulat, G.
    Bowen, P.
    [J]. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2017, 42 (38) : 24495 - 24503
  • [4] Effect of CO2 Opposing Multiple Jets on Thermoacoustic Instability and NOx Emissions in a Lean-Premixed Model Combustor
    ZHOU Hao
    HU Liubin
    [J]. Journal of Thermal Science, 2024, 33 (01) : 207 - 221
  • [5] Effect of CO2 Opposing Multiple Jets on Thermoacoustic Instability and NOx Emissions in a Lean-Premixed Model Combustor
    Zhou, Hao
    Hu, Liubin
    [J]. JOURNAL OF THERMAL SCIENCE, 2024, 33 (01) : 207 - 221
  • [6] Effect of CO2 Opposing Multiple Jets on Thermoacoustic Instability and NOx Emissions in a Lean-Premixed Model Combustor
    Hao Zhou
    Liubin Hu
    [J]. Journal of Thermal Science, 2024, 33 : 207 - 221
  • [7] Dual-fuel, dual-swirl burner for the mitigation of thermoacoustic instabilities in turbulent ammonia-hydrogen flames
    Katoch, Amit
    Guiberti, Thibault F.
    de Campos, Daniel V.
    Lacoste, Deanna A.
    [J]. COMBUSTION AND FLAME, 2022, 246
  • [8] High-frequency transverse combustion instabilities of lean-premixed multislit hydrogen-air flames
    Lee, Taesong
    Kim, Kyu Tae
    [J]. COMBUSTION AND FLAME, 2022, 238
  • [9] Mitigation of Combustion Instability and NOx Emissions by Microjets in Lean Premixed Flames with Different Swirl Numbers
    ZHOU Hao
    HU Liubin
    [J]. Journal of Thermal Science, 2023, 32 (04) : 1697 - 1709
  • [10] Mitigation of Combustion Instability and NOx Emissions by Microjets in Lean Premixed Flames with Different Swirl Numbers
    Zhou, Hao
    Hu, Liubin
    [J]. JOURNAL OF THERMAL SCIENCE, 2023, 32 (04) : 1697 - 1709