Investigations of the working processes in a gas turbine low-emission combustor operating on the synthesis gas, in which the\nprinciple of RQL (Rich-Burn, Quick-Mix, and Lean-Burn) combustion technology is realized, have been performed. Selected\nconcept of a gas turbine combustor can provide higher performance and lower emission of nitrogen oxides and demonstrates\nsatisfactory major key parameters. Obtained results and recommendations can be used for the gas turbine combustor operation\nmodes modeling, geometry optimization, and prospective power generation units design and engineering.
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