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    Development of a Hydrogen Microgas Turbine Combustor: NOx Emissions and Secondary Air Injection

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 002::page 21015-1
    Author:
    Tanneberger, Tom
    ,
    Mundstock, Johannes
    ,
    Rösch, Sebastian
    ,
    Rex, Christoph
    ,
    Paschereit, Christian Oliver
    DOI: 10.1115/1.4066346
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: On the way to defossilization, green hydrogen is a promising way to substitute natural gas (NG) and oil in the gas turbine industry. In the scope of the H2mGT project, a microgas turbine (mGT) burner with 100% hydrogen firing is developed and validated. The project is funded by the German BMWK, and it is a collaboration between Technische Universität Berlin (TUB) and the manufacturer Euro-K GmbH. It consists of three phases: (1) atmospheric pressure tests with a fused silica combustion chamber; (2) atmospheric pressure tests with counterflow-cooled steel flame tube and secondary air injection; (3) validation of the burner in the mGT at elevated pressure levels. The current study will present the results of phase 2. The hydrogen burner used in the project is based on a swirl-stabilized burner of TUB and was scaled to 36 kW thermal power at atmospheric conditions. The burner design features a variable swirl intensity, additional axial momentum of air in the mixing tube, a movable central fuel lance, and pilot nozzles at the front plate. Furthermore, the steel flame tube is exchangeable, which allows the evaluation of different dilution hole patterns and, thus, the variation of the ratio of primary and secondary air. The study presents temperature, pressure, and emission measurements. It is found that the flame can be operated over a large range of equivalence ratios and preheating temperatures up to 500 °C. As expected, the NOx emissions are mainly influenced by the local equivalence ratio, which can be controlled by the fuel mass flow or the dilution hole pattern in the flame tube. Furthermore, the results show a decrease of NOx when the power density is increased at constant equivalence ratios, and a rise of NOx during the fuel transition from natural gas to hydrogen. The results indicate certain differences to the findings of phase 1.
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      Development of a Hydrogen Microgas Turbine Combustor: NOx Emissions and Secondary Air Injection

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    contributor authorTanneberger, Tom
    contributor authorMundstock, Johannes
    contributor authorRösch, Sebastian
    contributor authorRex, Christoph
    contributor authorPaschereit, Christian Oliver
    date accessioned2025-04-21T10:23:13Z
    date available2025-04-21T10:23:13Z
    date copyright9/27/2024 12:00:00 AM
    date issued2024
    identifier issn0742-4795
    identifier othergtp_147_02_021015.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306080
    description abstractOn the way to defossilization, green hydrogen is a promising way to substitute natural gas (NG) and oil in the gas turbine industry. In the scope of the H2mGT project, a microgas turbine (mGT) burner with 100% hydrogen firing is developed and validated. The project is funded by the German BMWK, and it is a collaboration between Technische Universität Berlin (TUB) and the manufacturer Euro-K GmbH. It consists of three phases: (1) atmospheric pressure tests with a fused silica combustion chamber; (2) atmospheric pressure tests with counterflow-cooled steel flame tube and secondary air injection; (3) validation of the burner in the mGT at elevated pressure levels. The current study will present the results of phase 2. The hydrogen burner used in the project is based on a swirl-stabilized burner of TUB and was scaled to 36 kW thermal power at atmospheric conditions. The burner design features a variable swirl intensity, additional axial momentum of air in the mixing tube, a movable central fuel lance, and pilot nozzles at the front plate. Furthermore, the steel flame tube is exchangeable, which allows the evaluation of different dilution hole patterns and, thus, the variation of the ratio of primary and secondary air. The study presents temperature, pressure, and emission measurements. It is found that the flame can be operated over a large range of equivalence ratios and preheating temperatures up to 500 °C. As expected, the NOx emissions are mainly influenced by the local equivalence ratio, which can be controlled by the fuel mass flow or the dilution hole pattern in the flame tube. Furthermore, the results show a decrease of NOx when the power density is increased at constant equivalence ratios, and a rise of NOx during the fuel transition from natural gas to hydrogen. The results indicate certain differences to the findings of phase 1.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDevelopment of a Hydrogen Microgas Turbine Combustor: NOx Emissions and Secondary Air Injection
    typeJournal Paper
    journal volume147
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4066346
    journal fristpage21015-1
    journal lastpage21015-10
    page10
    treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 002
    contenttypeFulltext
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