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This investigation is devoted to an analysis of the working process in a dual-fuel low-emission combustion chamber for a floating vessel’s gas turbine. The low-emission gas turbine combustion chamber with partial pre-mixing of fuel and air inside the outer and inner radial-axial swirlers was chosen as the object of research. When modelling processes in a dualflow low-emission gas turbine combustion chamber, a generalized method is used, based on the numerical solution of the system of conservation and transport equations for a multi-component chemically reactive turbulent system, taking into consideration nitrogen oxides formation. The Eddy-Dissipation-Concept model, which incorporates Arrhenius chemical kinetics in a turbulent flame, and the Discrete Phase Model describing the interfacial interaction are used in the investigation. The obtained results confirmed the possibility of organizing efficient combustion of distillate liquid fuel in a low-emission gas turbine combustion chamber operating on the principle of partial preliminary formation of a fuel-air mixture. Comparison of four methods of liquid fuel supply to the channels of radial-axial swirlers (centrifugal, axial, combined, and radial) revealed the advantages of the radial supply method, which are manifested in a decrease in the overall temperature field non-uniformity at the outlet and a decrease in nitrogen oxides emissions. The calculated concentrations of nitrogen oxides and carbon monoxide at the flame tube outlet for the radial method of fuel supply are 32 and 9.1 ppm, respectively. The results can be useful for further modification and improvement of the characteristics of dual-fuel gas turbine combustion chambers operating with both gaseous and liquid fuels.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
89--99
Opis fizyczny
Bibliogr. 35 poz., rys.
Twórcy
autor
- Admiral Makarov National University of Shipbuilding Geroes of Ukraine Ave., 9, 54025 Mikolayiv, Ukraine
autor
- Admiral Makarov National University of Shipbuilding Geroes of Ukraine Ave., 9, 54025 Mikolayiv, Ukraine
autor
- Gdańsk University of Technology, 11/12 Gabriela Narutowicza Street, 80-233 Gdańsk, Poland
Bibliografia
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- 8. Burunsuz К.S., Kuklinovsky V.V., Serbin S.I. (2019): Investigations of the Emission Characteristics of a Gas Turbine Combustor with Water Steam Injection. Refrigeration Engineering and Technology, Vol. 55(2), 77–83.
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- 14. Ibrahim I.A., Shabaan M.M., Shehata M.A., Farag T.M. (2014): Investigation of Dual-Fuel Combustion Characteristics inside a Gas Turbine. Combustor International Conference on Machine Learning, Electrical and Mechanical Engineering (ICMLEME’2014). Dubai (UAE). Retrieved from: http://iieng. org/images/proceedings_pdf/2853E0114035.pdf.
- 15. Kurji H. (2017): Fuel Flexibility with Low Emissions for Gas Turbine Engines, PhD thesis, Cardiff University.
- 16. Matveev I., Serbin S., Mostipanenko A. (2007): Numerical Optimization of the “Tornado” Combustor Aerodynamic Parameters. Collection of Technical Papers – 45th AIAA Aerospace Sciences Meeting, Reno, Nevada, AIAA 2007-391, Vol. 7, 4744–4755.
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- 28. Abou-Taouk A., Sigfrid I.R., Whiddon R., Eriksson L.E. (2012): A Four-Step Global Reaction Mechanism for CFD Simulations of Flexi-Fuel Burner for Gas Turbines. Proceedings of the 17th International Symposium on Turbulence, Heat and Mass Transfer Palermo, Italy, 1–12.
- 29. Novosselov I.V., Malte P.C. (2007): Development and Application of an Eight-Step Global Mechanism for CFD and CRN Simulations of Lean-Premixed Combustors. Proceedings of GT2007 ASME Turbo Expo 2007: Power for Land, Sea and Air, 1–11.
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- 32. Romanovsky G.F., Serbin S.I., Patlaychuk V.M. (2005): Modern Gas Turbine Units of Russia and Ukraine. Vol. 1, Mikolayiv: NUK, 344 (in Ukrainian).
- 33. Gatsenko N.A., Serbin S.I. (1995): Arc Plasmatrons for Burning Fuel in Industrial Installations. Glass and Ceramics, Vol. 51(11/12), 383–386.
- 34. Serbin S.I., Matveev I.B., Goncharova N.A. (2014): Plasma Assisted Reforming of Natural Gas for GTL. Part I. IEEE Transactions on Plasma Science, Vol. 42(12), 3896–3900.
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Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-7095aa77-9a82-4ccb-8231-b344dd6e93c4