Technology of low-emission fuel combustion and conceptual structure of the combustion chamber of a gas-turbine power plant

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Currently, the priority for improvement of the combustion chambers of aircraft gas turbine engines and ground-based gas turbine plants is associated with a decrease in the concentration of harmful substances in the exhaust gases while ensuring fuel economy and operational efficiency. Pride of place in the design of a gas turbine power plant goes to solving the problem of organizing the combustion process, i.e. the development of a low-emission combustion system that provides high efficiency and environmental safety. Thus, ecology today determines not only the appearance of a combustion chamber, but also that of a gas turbine power plant as a whole. Below, an attempt is made to summarize the results of developing a low-emission combustion system for various types of combustion chambers of convertible gas turbine power plants and to present a unified approach to the problem  of designing a conceptual structure of a low-emission combustion chamber.

About the authors

Yu. I. Tsybizov

Samara National Research University

Author for correspondence.

Doctor of Science (Engineering),
Professor of the Department of Thermal Engineering and Thermal Engines

Russian Federation

D. D. Tyulkin

Samara National Research University

ORCID iD: 0000-0001-6575-6691

Postgraduate Student

Russian Federation

I. E. Vorotyntsev

Samara National Research University

ORCID iD: 0000-0002-8887-1438

Postgraduate Student

Russian Federation


  1. Frolov S.M. Combustion science and problems of contemporary power engineering. Russian Journal of General Chemistry. 2009. V. 79, Iss. 11. P. 2556-2561. doi: 10.1134/S1070363209110437
  2. Arutyunov V.S., Shmelev V.M., Rakhmetov A.N., Shapovalova O.V., Zakharov A.A., Roschin A.A. New approaches to development of low-emission combustion chambers for gas turbine engines. Alternative Energy and Ecology. 2013. No. 6 (128), part 2. P. 105-120. (In Russ.)
  3. Lavrov V.N., Posthikov A.M., Tsibizov Yu.I., Malchikov G.D., Grebnev V.V., Morozov A.V. Developing of low emission fuel burning system in gas turbine engines. Vestnik of the Samara State Aerospace University. 2007. No. 2 (13). P. 118-127. (In Russ.)
  4. Lavrov V.N., Postnikov A.M., Tsererin N.V., Tsybizov Yu.I., Belyaev V.V. Experience of design and lines of further improvement of gas turbine engine low-emission combustion chambers. Vestnik of the Samara State Aerospace University. 2002. No. 2 (2). P. 65-70. (In Russ.)
  5. Postnikov A.M. Snizhenie oksidov azota v vykhlopnykh gazakh GTU [Reducing the content of nitrogen oxides in gas turbine exhaust]. Samara: Samarskiy Nauchnyy Tsentr RAN Publ., 2002. 286 p.
  6. Matveev S.G., Lukachev S.V., Orlov M.Yu., Chechet I.V., Krasovskaya Yu.V. Raschet obrazovaniya CO i NOX v kamerakh sgoraniya GTD: elektron. ucheb. posobie [Calculation of CO and NOX formation in gas turbine engine combustion chambers. Electronic resource]. Samara: Samara State Aerospace University Publ., 2012. 41 p.
  7. Mingazov B.G. Kamery sgoraniya gazoturbinnykh dvigateley [Combustion chambers of gas turbine engines]. Kazan: Kazan State Technical University Publ., 2006. 220 p.
  8. Bantikov D.Yu., Yeliseev Yu.S., Lavrov V.N., Pchelyakov A.A., Fedorchenko D.G., Tsybizov Yu.I. Results of primary operation of NK-37 engine low emission combustion system. Vestnik of the Samara State Aerospace University. 2013. No. 3 (41), part 2. P. 9-14. (In Russ.). doi: 10.18287/1998-6629-2013-0-3-2(41)-9-14
  9. Gritsenko E.A., Danil'chenko V.P., Lukachev S.V., Reznik V.E., Tsybizov Yu.I. Konvertirovanie aviatsionnykh GTD v gazoturbinnye ustanovki nazemnogo primeneniya [Conversion of aircraft gas turbine engines into ground-application gas turbine units]. Samara: Samarskiy Nauchnyy Tsentr RAN Publ., 2004. 266 p.
  10. Biryuk V.V., Gorshkalev A.A., Lukachev S.V., Tsybizov Yu.I. Multi-nozzle combustion chamber of aviation gas turbine engines as basis of environmental safety. Review. Modern Science: Research, Ideas, Results, Technologies. 2016. No. 1 (17). P. 89-99. (In Russ.). doi: 10.23877/MS.TS.25.009
  11. Yeliseev Yu.S., Fedorchenko D.G., Golanov S.P., Tsibisov Yu.I., Tyulkin D.D., Vorotyntsev I.E., Ivchenko A.V. Application of additive technology of selective laser melting (SLM) in designing a low emission combustion chamber of a gas turbine plant. Vestnik of Samara University. Aerospace and Mechanical Engineering. 2019. V. 18, no. 1. P. 174-183. (In Russ.). doi: 10.18287/2541-7533-2019-18-1-174-183

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