Combustion Characterization in a Diffusive Gas Turbine Burner for Hydrogen-Compliant Applications

The target of net-zero emissions set by the 2015 Paris Agreement has strongly commissioned the energy production sector to promote decarbonization, renewable sources exploitation, and systems efficiency. In this framework, the utilization of hydrogen as a long-term energy carrier has great potential...

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Main Authors: Salvatore Carusotto, Prashant Goel, Mirko Baratta, Daniela Anna Misul, Simone Salvadori, Francesco Cardile, Luca Forno, Marco Toppino, Massimo Valsania
Format: Article
Language:English
Published: MDPI AG 2022-06-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/15/11/4117
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author Salvatore Carusotto
Prashant Goel
Mirko Baratta
Daniela Anna Misul
Simone Salvadori
Francesco Cardile
Luca Forno
Marco Toppino
Massimo Valsania
author_facet Salvatore Carusotto
Prashant Goel
Mirko Baratta
Daniela Anna Misul
Simone Salvadori
Francesco Cardile
Luca Forno
Marco Toppino
Massimo Valsania
author_sort Salvatore Carusotto
collection DOAJ
description The target of net-zero emissions set by the 2015 Paris Agreement has strongly commissioned the energy production sector to promote decarbonization, renewable sources exploitation, and systems efficiency. In this framework, the utilization of hydrogen as a long-term energy carrier has great potential. This paper is concerned with the combustion characterization in a non-premixed gas turbine burner, originally designed for natural gas, when it is fed with NG-H2 blends featuring hydrogen content from 0 to 50% in volume. The final aim is to retrofit a 40 MW gas turbine. Starting from the operational data of the engine, a CFD model of the steady-state combustion process has been developed, with reference to the base load NG conditions, by reducing the fuel mass-flow rate by up to 17% to target the baseline turbine inlet temperature. When the fuel is blended with hydrogen, for a given temperature at turbine inlet, an increase in the peak temperature up to 800 K is obtained, if no countermeasures are taken. Furthermore, the flame results are more intense and closer to the injector in the case of hydrogen blending. The results of this work hint at the necessity of carefully analyzing the possible NOx compensation strategies, as well as the increased thermal stresses on the injector.
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spelling doaj.art-c9ab677c7ddd4b719dd672d43a8924972023-11-23T14:00:38ZengMDPI AGEnergies1996-10732022-06-011511411710.3390/en15114117Combustion Characterization in a Diffusive Gas Turbine Burner for Hydrogen-Compliant ApplicationsSalvatore Carusotto0Prashant Goel1Mirko Baratta2Daniela Anna Misul3Simone Salvadori4Francesco Cardile5Luca Forno6Marco Toppino7Massimo Valsania8Dipartimento Energia DENERG, Politecnico di Torino, Corso Duca degli Abruzzi 24, 10129 Torino, ItalyDipartimento Energia DENERG, Politecnico di Torino, Corso Duca degli Abruzzi 24, 10129 Torino, ItalyDipartimento Energia DENERG, Politecnico di Torino, Corso Duca degli Abruzzi 24, 10129 Torino, ItalyDipartimento Energia DENERG, Politecnico di Torino, Corso Duca degli Abruzzi 24, 10129 Torino, ItalyDipartimento Energia DENERG, Politecnico di Torino, Corso Duca degli Abruzzi 24, 10129 Torino, ItalyEthos Energy Italia S.p.A., Corso Romania 661, 10156 Torino, ItalyEthos Energy Italia S.p.A., Corso Romania 661, 10156 Torino, ItalyEthos Energy Italia S.p.A., Corso Romania 661, 10156 Torino, ItalyEthos Energy Italia S.p.A., Corso Romania 661, 10156 Torino, ItalyThe target of net-zero emissions set by the 2015 Paris Agreement has strongly commissioned the energy production sector to promote decarbonization, renewable sources exploitation, and systems efficiency. In this framework, the utilization of hydrogen as a long-term energy carrier has great potential. This paper is concerned with the combustion characterization in a non-premixed gas turbine burner, originally designed for natural gas, when it is fed with NG-H2 blends featuring hydrogen content from 0 to 50% in volume. The final aim is to retrofit a 40 MW gas turbine. Starting from the operational data of the engine, a CFD model of the steady-state combustion process has been developed, with reference to the base load NG conditions, by reducing the fuel mass-flow rate by up to 17% to target the baseline turbine inlet temperature. When the fuel is blended with hydrogen, for a given temperature at turbine inlet, an increase in the peak temperature up to 800 K is obtained, if no countermeasures are taken. Furthermore, the flame results are more intense and closer to the injector in the case of hydrogen blending. The results of this work hint at the necessity of carefully analyzing the possible NOx compensation strategies, as well as the increased thermal stresses on the injector.https://www.mdpi.com/1996-1073/15/11/4117hydrogenCFDnon-premixed combustionretrofittinggas turbines
spellingShingle Salvatore Carusotto
Prashant Goel
Mirko Baratta
Daniela Anna Misul
Simone Salvadori
Francesco Cardile
Luca Forno
Marco Toppino
Massimo Valsania
Combustion Characterization in a Diffusive Gas Turbine Burner for Hydrogen-Compliant Applications
Energies
hydrogen
CFD
non-premixed combustion
retrofitting
gas turbines
title Combustion Characterization in a Diffusive Gas Turbine Burner for Hydrogen-Compliant Applications
title_full Combustion Characterization in a Diffusive Gas Turbine Burner for Hydrogen-Compliant Applications
title_fullStr Combustion Characterization in a Diffusive Gas Turbine Burner for Hydrogen-Compliant Applications
title_full_unstemmed Combustion Characterization in a Diffusive Gas Turbine Burner for Hydrogen-Compliant Applications
title_short Combustion Characterization in a Diffusive Gas Turbine Burner for Hydrogen-Compliant Applications
title_sort combustion characterization in a diffusive gas turbine burner for hydrogen compliant applications
topic hydrogen
CFD
non-premixed combustion
retrofitting
gas turbines
url https://www.mdpi.com/1996-1073/15/11/4117
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