{"title":"轴向分级富预混氨燃烧系统中活性氮排放和燃烧动力学","authors":"Jun Lee , Ukhwa Jin , Kyu Tae Kim","doi":"10.1016/j.combustflame.2025.114133","DOIUrl":null,"url":null,"abstract":"<div><div>The key technical problems associated with ammonia-fueled gas turbine combustion are well established in terms of flame-stabilization mechanisms for the less reactive ammonia and the overwhelming tendency to produce excessive nitrogen oxides through the fuel-NOx pathways. Recent studies suggest that these problems can be alleviated by chemical-kinetics-controlled fuel/air injection strategies, particularly those involving spatially separated reaction zones. The mechanistic role of axially staged secondary air and lean-premixed fuel/air jets injected into a high-temperature vitiated crossflow is, however, relatively underexplored; our knowledge of the effectiveness and relative importance of these strategies with regard to exhaust gas emissions and combustion dynamics is limited. Here, we undertake reduced-order kinetic modeling and comprehensive measurements of reactive nitrogen compounds (NOx, N<sub>2</sub>O, NH<sub>3</sub>) and unreacted hydrogen concentrations using an axial-staging-enhanced fuel-flexible test facility. We show that an increase in the primary equivalence ratio to 1.25 under non-staged rich-premixed conditions causes the total NOx emissions to be reduced substantially from 3030 to 57 ppmvd while producing unreacted ammonia and hydrogen emissions. When the rich-premixed ammonia condition is kept unchanged for the primary reaction zone, the second-stage reaction volume sequentially created by transverse air or lean-premixed H<sub>2</sub>/air injection is revealed to mitigate unburned ammonia and hydrogen emissions effectively by reinitiating related elementary reactions. The existence of a second-stage reaction region, however, tends to augment NH-related NO production and thermal NO reactions, potentially nullifying or strongly reducing the effective gains. This apparent drawback is found to be much less pronounced in the H<sub>2</sub>/air axial staging situations, as the production of the ammonia-derived fuel NO through <em>N</em> + OH → NO + <em>H</em> is relatively reduced, in close connection with the enhanced OH depletion reaction, H<sub>2</sub> + OH → H + H<sub>2</sub>O. As well as achieving the minimum NOx concentration of about 367 ppmvd with no unreacted ammonia and nitrous oxide emissions, we demonstrate that high-amplitude low-frequency pressure fluctuations are largely suppressed under the investigated H<sub>2</sub>/air-staged conditions.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"277 ","pages":"Article 114133"},"PeriodicalIF":5.8000,"publicationDate":"2025-04-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Reactive nitrogen emissions and combustion dynamics in an axially staged rich-premixed ammonia combustion system\",\"authors\":\"Jun Lee , Ukhwa Jin , Kyu Tae Kim\",\"doi\":\"10.1016/j.combustflame.2025.114133\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The key technical problems associated with ammonia-fueled gas turbine combustion are well established in terms of flame-stabilization mechanisms for the less reactive ammonia and the overwhelming tendency to produce excessive nitrogen oxides through the fuel-NOx pathways. Recent studies suggest that these problems can be alleviated by chemical-kinetics-controlled fuel/air injection strategies, particularly those involving spatially separated reaction zones. The mechanistic role of axially staged secondary air and lean-premixed fuel/air jets injected into a high-temperature vitiated crossflow is, however, relatively underexplored; our knowledge of the effectiveness and relative importance of these strategies with regard to exhaust gas emissions and combustion dynamics is limited. Here, we undertake reduced-order kinetic modeling and comprehensive measurements of reactive nitrogen compounds (NOx, N<sub>2</sub>O, NH<sub>3</sub>) and unreacted hydrogen concentrations using an axial-staging-enhanced fuel-flexible test facility. We show that an increase in the primary equivalence ratio to 1.25 under non-staged rich-premixed conditions causes the total NOx emissions to be reduced substantially from 3030 to 57 ppmvd while producing unreacted ammonia and hydrogen emissions. When the rich-premixed ammonia condition is kept unchanged for the primary reaction zone, the second-stage reaction volume sequentially created by transverse air or lean-premixed H<sub>2</sub>/air injection is revealed to mitigate unburned ammonia and hydrogen emissions effectively by reinitiating related elementary reactions. The existence of a second-stage reaction region, however, tends to augment NH-related NO production and thermal NO reactions, potentially nullifying or strongly reducing the effective gains. This apparent drawback is found to be much less pronounced in the H<sub>2</sub>/air axial staging situations, as the production of the ammonia-derived fuel NO through <em>N</em> + OH → NO + <em>H</em> is relatively reduced, in close connection with the enhanced OH depletion reaction, H<sub>2</sub> + OH → H + H<sub>2</sub>O. As well as achieving the minimum NOx concentration of about 367 ppmvd with no unreacted ammonia and nitrous oxide emissions, we demonstrate that high-amplitude low-frequency pressure fluctuations are largely suppressed under the investigated H<sub>2</sub>/air-staged conditions.</div></div>\",\"PeriodicalId\":280,\"journal\":{\"name\":\"Combustion and Flame\",\"volume\":\"277 \",\"pages\":\"Article 114133\"},\"PeriodicalIF\":5.8000,\"publicationDate\":\"2025-04-30\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Combustion and Flame\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0010218025001713\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENERGY & FUELS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Combustion and Flame","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0010218025001713","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENERGY & FUELS","Score":null,"Total":0}
Reactive nitrogen emissions and combustion dynamics in an axially staged rich-premixed ammonia combustion system
The key technical problems associated with ammonia-fueled gas turbine combustion are well established in terms of flame-stabilization mechanisms for the less reactive ammonia and the overwhelming tendency to produce excessive nitrogen oxides through the fuel-NOx pathways. Recent studies suggest that these problems can be alleviated by chemical-kinetics-controlled fuel/air injection strategies, particularly those involving spatially separated reaction zones. The mechanistic role of axially staged secondary air and lean-premixed fuel/air jets injected into a high-temperature vitiated crossflow is, however, relatively underexplored; our knowledge of the effectiveness and relative importance of these strategies with regard to exhaust gas emissions and combustion dynamics is limited. Here, we undertake reduced-order kinetic modeling and comprehensive measurements of reactive nitrogen compounds (NOx, N2O, NH3) and unreacted hydrogen concentrations using an axial-staging-enhanced fuel-flexible test facility. We show that an increase in the primary equivalence ratio to 1.25 under non-staged rich-premixed conditions causes the total NOx emissions to be reduced substantially from 3030 to 57 ppmvd while producing unreacted ammonia and hydrogen emissions. When the rich-premixed ammonia condition is kept unchanged for the primary reaction zone, the second-stage reaction volume sequentially created by transverse air or lean-premixed H2/air injection is revealed to mitigate unburned ammonia and hydrogen emissions effectively by reinitiating related elementary reactions. The existence of a second-stage reaction region, however, tends to augment NH-related NO production and thermal NO reactions, potentially nullifying or strongly reducing the effective gains. This apparent drawback is found to be much less pronounced in the H2/air axial staging situations, as the production of the ammonia-derived fuel NO through N + OH → NO + H is relatively reduced, in close connection with the enhanced OH depletion reaction, H2 + OH → H + H2O. As well as achieving the minimum NOx concentration of about 367 ppmvd with no unreacted ammonia and nitrous oxide emissions, we demonstrate that high-amplitude low-frequency pressure fluctuations are largely suppressed under the investigated H2/air-staged conditions.
期刊介绍:
The mission of the journal is to publish high quality work from experimental, theoretical, and computational investigations on the fundamentals of combustion phenomena and closely allied matters. While submissions in all pertinent areas are welcomed, past and recent focus of the journal has been on:
Development and validation of reaction kinetics, reduction of reaction mechanisms and modeling of combustion systems, including:
Conventional, alternative and surrogate fuels;
Pollutants;
Particulate and aerosol formation and abatement;
Heterogeneous processes.
Experimental, theoretical, and computational studies of laminar and turbulent combustion phenomena, including:
Premixed and non-premixed flames;
Ignition and extinction phenomena;
Flame propagation;
Flame structure;
Instabilities and swirl;
Flame spread;
Multi-phase reactants.
Advances in diagnostic and computational methods in combustion, including:
Measurement and simulation of scalar and vector properties;
Novel techniques;
State-of-the art applications.
Fundamental investigations of combustion technologies and systems, including:
Internal combustion engines;
Gas turbines;
Small- and large-scale stationary combustion and power generation;
Catalytic combustion;
Combustion synthesis;
Combustion under extreme conditions;
New concepts.