Co-Firing Hydrogen With Natural Gas for 9 MW Siemens Energy Dry Low Emissions Combustor: High-Pressure Rig Test
Abstract To validate 30% H2 (by volume) capability for the Siemens Energy's 9 MW SGT-300-2S engine, high-pressure rig testing was conducted. The dry low emissions (DLE) combustor was initially operated with natural gas to establish a baseline operation. Subsequently, it was fueled with a 30% H2 (by volume) blend under various ambient temperatures. To evaluate operational margins, tests were extended to 35% and 40% H2. Finally, the combustion system's robustness was rigorously tested under various overfiring conditions. The impact of H2 concentration on combustor performance was investigated, focusing on factors such as burner metal temperature, NOx and CO emissions, combustion dynamics, and combustor wall temperatures. Test results indicate that burner metal temperatures and NOx emissions increase with increasing H2 concentration. The turbine entry temperature (TET) at which CO emissions begin to rise is lowered with increasing H2 concentration. This suggests that adding H2 to the fuel can lower the turndown temperature for controlling CO emissions, thereby improving the engine's part load thermal efficiency. Combustion dynamic pressure amplitudes remained low for H2 concentrations up to 40%. Combustor wall temperatures for H2 operation up to 40% were comparable to those for natural gas. Test results demonstrate that the combustion system can safely operate with up to 40% H2 by volume in the fuel. The effect of pilot split on combustion was investigated for natural gas and the fuel blends with 30% and 40% H2. A key finding is that different fuel compositions may require different pilot split and turndown control temperature for optimal operation.
Authors
- Jadeed Beita (ORCID: https://orcid.org/0009-0008-1309-150X)
- Suresh Sadasivuni
- Kexin Liu (ORCID: https://orcid.org/0000-0002-7150-2820)
Institutions
- EA Technology (GB)
- Siemens Healthcare (United States) (US)
- Orion Corporation (United Kingdom) (GB)
Publication Details
- Journal
- Journal of Engineering for Gas Turbines and Power
- Published
- 2025-09-01
- DOI
- https://doi.org/10.1115/1.4069616
- Primary Topic
- Advanced Combustion Engine Technologies
- Type
- article
- Field-Weighted Citation Impact
- 0.00