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International Journal of Chemical Engineering
Volume 2017, Article ID 6146984, 14 pages
Research Article

Investigations of a Gas Turbine Low-Emission Combustor Operating on the Synthesis Gas

Admiral Makarov National University of Shipbuilding, Mykolaiv, Ukraine

Correspondence should be addressed to Serhiy Serbin; ur.xednay@nibresis

Received 3 November 2016; Revised 24 February 2017; Accepted 12 March 2017; Published 5 April 2017

Academic Editor: Nandkishor Nere

Copyright © 2017 Serhiy Serbin and Nataliia Goncharova. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


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