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doi: 10.17586/2226-1494-2024-24-4-645-653

Configurable combustion models of combustion chamber of microturbine engine with possibility of connecting various physico-chemical processes

P. V. Bulat, L. O. Vokin, K. N. Volkov, A. B. Nikitenko, N. V. Prodan, M. E. Renev


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Article in Russian

For citation:
Bulat P.V., Vokin L.O., Volkov K.N., Nikitenko A.B., Prodan N.V., Renev M.E. Configurable combustion models of combustion chamber of microturbine engine with possibility of connecting various physico-chemical processes. Scientific and Technical Journal of Information Technologies, Mechanics and Optics, 2024, vol. 24, no. 4, pp. 645–653 (in Russian). doi: 10.17586/2226-1494-2024-24-4-645-653


Abstract
Mathematical and numerical models of the combustion of a fuel mixture in the combustion chamber of a microturbine engine have been developed. Complexity of the models can vary, which gives developers a fairly convenient calculation and design tool. Models allow to take into account the required design tasks by considering and not taking into account various physical processes, and create an optimal complexity model for each specific case. The development of the required configuration begins with the consideration of a simple model of the global kerosene in air combustion reaction without conjugate heat exchange with solids. Step by step, models of extended kinetics, swirling flow, radiation, heat exchange with walls, and the presence of lubricant oil in kerosene are added to the calculation methodology. The results of calculating the wall temperature and combustion completeness were compared with those of JetCat P100-RX and P550-PRO turbojet engines, the integral characteristics of which are well known. In the course of the performed computational and experimental studies, a comparison of the run-off spots on the walls of the combustion chamber with the calculated temperature distributions was performed. A good agreement of the results was obtained for the complete mathematical model. The effect of better cooling of the combustion chamber and increasing the completeness of combustion by twisting the flow behind the compressor is revealed. The effect of the addition of oil to kerosene on an increase in specific fuel consumption by 1–4 % has been determined. The significance of the results obtained lies in the possibility of applying the proposed calculation methodology in engineering practice. The considered modifications of the model represent an important stage in the creation and verification of a mathematical model of in-chamber processes.

Keywords: micro gas turbine engine, combustion chamber, numerical simulation, validation

Acknowledgements. This work was financially supported by the Ministry of Science and Higher Education of the Russian Federation during the implementation of the project “Development of fundamental and applied principles of promising methods for increasing the efficiency of small-sized gas turbine engines of unmanned aerial vehicles and aerospace transport systems, as well as ground-based power plants”, No. FZWF-2024-0004.

References
  1. Starikovskaia S.M. Plasma assisted ignition and combustion. Journal of Physics D: Applied Physics, 2006, vol. 39, no. 16, pp. R265–R299. https://doi.org/10.1088/0022-3727/39/16/R01
  2. Bulat M.P., Bulat P.V., Denissenko P.V., Esakov I.I., Grachev L.P., Lavrov P.V., Volkov K.N., Volobuev I.A. Plasma-assisted ignition and combustion of lean and rich air/fuel mixtures in low- and high-speed flows. Acta Astronautica, 2020, vol. 176, pp. 700–709. https://doi.org/10.1016/j.actaastro.2020.04.028
  3. Zhdanov I.A., Staudacher S., Falaleev S.V. Problems and prospect of microgasturbines development for unmanned aerial vehicle propulsion. Vestnik of Samara State Aerospace University named after academician S.P. Korolev (National Research University), 2011, no. 3-1(27), pp. 345–353. (in Russian)
  4. Kuznetsov A.V., Makaryants G.M. Micro gas turbine engine imitation model. Vestnik of Samara University. Aerospace and Mechanical Engineering, 2017, vol. 16, no. 2, pp. 65–74. (in Russian). https://doi.org/10.18287/2541-7533-2017-16-2-65-74
  5. Sychenkov V.A., Limanskii A.S., Yousef W.M., Ankudimov V.V., Seyid Jafari S.S. Micro gas turbine engine for unmanned aerial vehicles. Russian Aeronautics, 2019, vol. 62, no. 4, pp. 651–660. https://doi.org/10.3103/S1068799819040160
  6. Hosseinalipour S.M., Abdolahi M., Razaghi E., Static and dynamic mathematical modeling of a micro gas turbine. Journal of Mechanics, 2013, vol. 29, no. 2, pp. 327–335. https://doi.org/10.1017/jmech.2013.3
  7. Asgari H., Chen X.Q., Morini M., Pinelli M., Sainudiin R., Spina P.R., Venturini M. NARX models for simulation of the start-up operation of a single-shaft gas turbine. Applied Thermal Engineering, 2016, vol. 93, pp. 368–376. https://doi.org/10.1016/j.applthermaleng.2015.09.074
  8. Erario M.L., De Giorgi M.G., Przysowa R. Model-based dynamic performance simulation of a microturbine using flight test data. Aerospace, 2022, vol. 9, no. 2, pp. 60. https://doi.org/10.3390/aerospace9020060
  9. Teixeria M., Romagnosi L., Mezine M., Baux Y., Anker J., Claramunt K., Hirsch C. A methodology for fully-coupled CFD engine simulations, applied to a micro gas turbine engine. Proceedings of the ASME Turbo Expo2C-2018, 2018, pp. GT2018-76870. https://doi.org/10.1115/GT2018-76870
  10. Romagnosi L., Li Y., Mezine M., Teixeira M., Vilmin S., Anker J.E., Claramunt K., Baux Y., Hirsch C. A methodology for steady and unsteady full-engine simulations. Proceedings of the ASME Turbo Expo 2C-2019, 2019, pp. GT2019-90110. https://doi.org/10.1115/GT2019-90110
  11. Briones A.M., Caswell A.W., Rankin B.A. Fully coupled turbojet engine computational fluid dynamics simulations and cycle analyses along the equilibrium running line. Journal of Engineering for Gas Turbines and Power, 2021, vol. 143, no. 6, pp. 061019. https://doi.org/10.1115/1.4049410
  12. Tikhonov A.S., Borovkov A.I., Tamm A.Yu. Numerical and experimental investigation of the main parameters of a small gas turbine engine. IOP Conference Series: Materials Science and Engineering, 2020, vol. 986, pp. 012052. https://doi.org/10.1088/1757-899X/986/1/012052
  13. Wang T.-S. Thermophysics characterization of kerosene combustion. Journal of Thermophysics and Heat Transfer, 2001, vol. 15, no. 2, pp. 140–147. https://doi.org/10.2514/2.6602
  14. Tuccillo R., Cameretti M.C., De Robbio R., Reale F., Chiariello F. Methane-Hydrogen Blends in Micro Gas Turbines: Comparison of Different Combustor Concepts. Proceedings of the ASME Turbo Expo 8, 2019. https://doi.org/10.1115/GT2019-90229
  15. Reale F., Calabria R., Chiariello F., Pagliara R., Massoli P. A micro gas turbine fuelled by methane-hydrogen blends. Applied Mechanics and Materials, 2012, vol. 232, pp. 792–796. https://doi.org/10.4028/www.scientific.net/AMM.232.792
  16. Bazooyar B., Gohari Darabkhani H. The design strategy and testing of an efficient microgas turbine combustor for biogas fuel. Fuel, 2021, vol. 294, pp. 120535. https://doi.org/10.1016/j.fuel.2021.120535
  17. Gómez-Rico M.F., Martı́n-Gullón I., Fullana A., Conesa F.A., Font R. Pyrolysis and combustion kinetics and emissions of waste lube oils. Journal of Analytical and Applied Pyrolysis, 2003, vol. 68–69, pp. 527–546. https://doi.org/10.1016/S0165-2370(03)00030-5
  18. Cadorin M., Pinelli M., Vaccari A., Calabria R., Chiariello F., Massoli P., Bianchi E. Analysis of a Micro gas turbine fed by natural gas and synthesis gas: MGT test bench and combustor CFD analysis. Journal of Engineering for Gas Turbines and Power, 2012, vol. 134, no. 7, pp. 071401. https://doi.org/10.1115/1.4005977
  19. Calabria R., Chiariello F., Massoli P., Reale F. Part load behavior of a micro gas turbine fed with different fuels. Proceedings of the ASME Turbo Expo 1B, 2014, pp. GT2014-26631. https://doi.org/10.1115/GT2014-26631
  20. Meziane S., Bentebbiche A. Numerical study of blended fuel natural gas-hydrogen combustion in rich/quench/lean combustor of a micro gas turbine. International Journal of Hydrogen Energy, 2019, vol. 44, no. 29, pp. 15610–15621. https://doi.org/10.1016/j.ijhydene.2019.04.128
  21. Reale F., Sannino R. Numerical modeling of energy systems based on micro gas turbine: a review. Energies, 2022, vol. 15, no. 3, pp. 900. https://doi.org/10.3390/en15030900
  22. Banihabib R., Assadi M. The role of micro gas turbines in energy transition. Energies, 2022, vol. 15, no. 21, pp. 8084. https://doi.org/10.3390/en15218084


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