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Author

  • Harald H.-W. Funke (10)
  • Karsten Kusterer (10)
  • Atsushi Horikawa (7)
  • Kunio Okada (6)
  • Anis Haj Ayed (5)
  • Jan Keinz (5)
  • Manfred Wirsum (3)
  • Masahide Kazari (3)
  • Constantin J. D. Striegan (2)
  • Masato Yamaguchi (2)
  • Shigeki Aoki (2)
  • Anis Haji Ayed (1)
  • Benjamin Struth (1)
  • D. Bohn (1)
  • Dieter Bohn (1)
  • Jens Dickhoff (1)
  • Junichi Kitajima (1)
  • M. Kazari (1)
  • Mitsugu Ashikaga (1)
  • Takahiro Uto (1)
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Year of publication

  • 2022 (1)
  • 2021 (1)
  • 2019 (2)
  • 2017 (2)
  • 2016 (2)
  • 2015 (2)

Document Type

  • Conference Proceeding (7)
  • Article (3)

Keywords

  • combustor development (2)
  • fuels (2)
  • hydrogen (2)
  • industrial gas turbine (2)
  • Dry-low-NOx (DLN) combustion (1)
  • High hydrogen combustion (1)
  • Hydrogen combustion (1)
  • Hydrogen gas turbine (1)
  • Micromix combustion (1)
  • emission (1)
  • engine demonstration (1)

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Developments of Hydrogen Dry Low Emission Combustion Technology (2015)
Atsushi Horikawa ; Masahide Kazari ; Kunio Okada ; Harald H.-W. Funke ; Jan Keinz ; Karsten Kusterer ; Anis Haji Ayed
Application of Low NOx Micro-Mix Hydrogen Combustion to Industrial Gas Turbine Combustor and Conceptual Design (2015)
Atsushi Horikawa ; Kunio Okada ; Masahide Kazari ; Harald H.-W. Funke ; Jan Keinz ; Karsten Kusterer ; Anis Haj Ayed
Experimental and Numerical Study on Optimizing the Dry Low NOₓ Micromix Hydrogen Combustion Principle for Industrial Gas Turbine Applications (2016)
Harald H.-W. Funke ; Jan Keinz ; Karsten Kusterer ; Anis Haj Ayed ; Masahide Kazari ; Junichi Kitajima ; Atsushi Horikawa ; Kunio Okada
Combined with the use of renewable energy sources for its production, hydrogen represents a possible alternative gas turbine fuel for future low-emission power generation. Due to the difference in the physical properties of hydrogen compared to other fuels such as natural gas, well-established gas turbine combustion systems cannot be directly applied to dry low NOₓ (DLN) hydrogen combustion. The DLN micromix combustion of hydrogen has been under development for many years, since it has the promise to significantly reduce NOₓ emissions. This combustion principle for air-breathing engines is based on crossflow mixing of air and gaseous hydrogen. Air and hydrogen react in multiple miniaturized diffusion-type flames with an inherent safety against flashback and with low NOₓ emissions due to a very short residence time of the reactants in the flame region. The paper presents an advanced DLN micromix hydrogen application. The experimental and numerical study shows a combustor configuration with a significantly reduced number of enlarged fuel injectors with high-thermal power output at constant energy density. Larger fuel injectors reduce manufacturing costs, are more robust and less sensitive to fuel contamination and blockage in industrial environments. The experimental and numerical results confirm the successful application of high-energy injectors, while the DLN micromix characteristics of the design point, under part-load conditions, and under off-design operation are maintained. Atmospheric test rig data on NOₓ emissions, optical flame-structure, and combustor material temperatures are compared to numerical simulations and show good agreement. The impact of the applied scaling and design laws on the miniaturized micromix flamelets is particularly investigated numerically for the resulting flow field, the flame-structure, and NOₓ formation.
CFD Based Improvement of the DLN Hydrogen Micromix Combustion Technology at Increased Energy Densities (2016)
Anis Haj Ayed ; Karsten Kusterer ; Harald H.-W. Funke ; Jan Keinz
Combined with the use of renewable energy sources for its production, Hydrogen represents a possible alternative gas turbine fuel within future low emission power generation. Due to the large difference in the physical properties of Hydrogen compared to other fuels such as natural gas, well established gas turbine combustion systems cannot be directly applied for Dry Low NOx (DLN) Hydrogen combustion. Thus, the development of DLN combustion technologies is an essential and challenging task for the future of Hydrogen fuelled gas turbines. The DLN Micromix combustion principle for hydrogen fuel has been developed to significantly reduce NOx-emissions. This combustion principle is based on cross-flow mixing of air and gaseous hydrogen which reacts in multiple miniaturized diffusion-type flames. The major advantages of this combustion principle are the inherent safety against flash-back and the low NOx-emissions due to a very short residence time of reactants in the flame region of the micro-flames. The Micromix Combustion technology has been already proven experimentally and numerically for pure Hydrogen fuel operation at different energy density levels. The aim of the present study is to analyze the influence of different geometry parameter variations on the flame structure and the NOx emission and to identify the most relevant design parameters, aiming to provide a physical understanding of the Micromix flame sensitivity to the burner design and identify further optimization potential of this innovative combustion technology while increasing its energy density and making it mature enough for real gas turbine application. The study reveals great optimization potential of the Micromix Combustion technology with respect to the DLN characteristics and gives insight into the impact of geometry modifications on flame structure and NOx emission. This allows to further increase the energy density of the Micromix burners and to integrate this technology in industrial gas turbines.
CFD based exploration of the dry-low-NOx hydrogen micromix combustion technology at increased energy densities (2017)
Anis Haj Ayed ; Karsten Kusterer ; Harald H.-W. Funke ; Jan Keinz ; D. Bohn
Automated design space exploration of the hydrogen fueled "Micromix" combustor technology (2017)
Anis Haj Ayed ; Constantin J. D. Striegan ; Karsten Kusterer ; Harald H.-W. Funke ; M. Kazari ; Atsushi Horikawa ; Kunio Okada
Combined with the use of renewable energy sources for its production, Hydrogen represents a possible alternative gas turbine fuel for future low emission power generation. Due to its different physical properties compared to other fuels such as natural gas, well established gas turbine combustion systems cannot be directly applied for Dry Low NOx (DLN) Hydrogen combustion. This makes the development of new combustion technologies an essential and challenging task for the future of hydrogen fueled gas turbines. The newly developed and successfully tested “DLN Micromix” combustion technology offers a great potential to burn hydrogen in gas turbines at very low NOx emissions. Aiming to further develop an existing burner design in terms of increased energy density, a redesign is required in order to stabilise the flames at higher mass flows and to maintain low emission levels. For this purpose, a systematic design exploration has been carried out with the support of CFD and optimisation tools to identify the interactions of geometrical and design parameters on the combustor performance. Aerodynamic effects as well as flame and emission formation are observed and understood time- and cost-efficiently. Correlations between single geometric values, the pressure drop of the burner and NOx production have been identified as a result. This numeric methodology helps to reduce the effort of manufacturing and testing to few designs for single validation campaigns, in order to confirm the flame stability and NOx emissions in a wider operating condition field.
Combined heat and power supply demonstration of Micro-Mix Hydrogen Combustion Applied to M1A-17 Gas Turbine (2022)
Atsushi Horikawa ; Mitsugu Ashikaga ; Masato Yamaguchi ; Tomoyuki Ogino ; Shigeki Aoki ; Manfred Wirsum ; Harald H.-W. Funke ; Karsten Kusterer
Kawasaki Heavy Industries, Ltd. (KHI), Aachen University of Applied Sciences, and B&B-AGEMA GmbH have investigated the potential of low NOx micro-mix (MMX) hydrogen combustion and its application to an industrial gas turbine combustor. Engine demonstration tests of a MMX combustor for the M1A-17 gas turbine with a co-generation system were conducted in the hydrogen-fueled power generation plant in Kobe City, Japan. This paper presents the results of the commissioning test and the combined heat and power (CHP) supply demonstration. In the commissioning test, grid interconnection, loading tests and load cut-off tests were successfully conducted. All measurement results satisfied the Japanese environmental regulation values. Dust and soot as well as SOx were not detected. The NOx emissions were below 84 ppmv at 15 % O2. The noise level at the site boundary was below 60 dB. The vibration at the site boundary was below 45 dB. During the combined heat and power supply demonstration, heat and power were supplied to neighboring public facilities with the MMX combustion technology and 100 % hydrogen fuel. The electric power output reached 1800 kW at which the NOx emissions were 72 ppmv at 15 % O2, and 60 %RH. Combustion instabilities were not observed. The gas turbine efficiency was improved by about 1 % compared to a non-premixed type combustor with water injection as NOx reduction method. During a total equivalent operation time of 1040 hours, all combustor parts, the M1A-17 gas turbine as such, and the co-generation system were without any issues.
Application of Low NOx Micro-mix Hydrogen Combustion to 2MW Class Industrial Gas Turbine Combustor (2019)
Atsushi Horikawa ; Kunio Okada ; Takahiro Uto ; Yuta Uchiyama ; Manfred Wirsum ; Harald H.-W. Funke ; Karsten Kusterer
Numerical Simulations of the Micromix DLN Hydrogen Combustion Technology with LES and Comparison to Results of RANS and Experimental Data (2019)
Constantin J. D. Striegan ; Benjamin Struth ; Jens Dickhoff ; Karsten Kusterer ; Harald H.-W. Funke ; Dieter Bohn
Combustor development and engine demonstration of micro-mix hydrogen combustion applied to M1A-17 gas turbine (2021)
Atsushi Horikawa ; Kunio Okada ; Masato Yamaguchi ; Shigeki Aoki ; Manfred Wirsum ; Harald H.-W. Funke ; Karsten Kusterer
Kawasaki Heavy Industries, LTD. (KHI) has research and development projects for a future hydrogen society. These projects comprise the complete hydrogen cycle, including the production of hydrogen gas, the refinement and liquefaction for transportation and storage, and finally the utilization in a gas turbine for electricity and heat supply. Within the development of the hydrogen gas turbine, the key technology is stable and low NOx hydrogen combustion, namely the Dry Low NOx (DLN) hydrogen combustion. KHI, Aachen University of Applied Science, and B&B-AGEMA have investigated the possibility of low NOx micro-mix hydrogen combustion and its application to an industrial gas turbine combustor. From 2014 to 2018, KHI developed a DLN hydrogen combustor for a 2MW class industrial gas turbine with the micro-mix technology. Thereby, the ignition performance, the flame stability for equivalent rotational speed, and higher load conditions were investigated. NOx emission values were kept about half of the Air Pollution Control Law in Japan: 84ppm (O2-15%). Hereby, the elementary combustor development was completed. From May 2020, KHI started the engine demonstration operation by using an M1A-17 gas turbine with a co-generation system located in the hydrogen-fueled power generation plant in Kobe City, Japan. During the first engine demonstration tests, adjustments of engine starting and load control with fuel staging were investigated. On 21st May, the electrical power output reached 1,635 kW, which corresponds to 100% load (ambient temperature 20 °C), and thereby NOx emissions of 65 ppm (O2-15, 60 RH%) were verified. Here, for the first time, a DLN hydrogen-fueled gas turbine successfully generated power and heat.
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