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Rotating combustion chambers as a key feature of effective timing of turbine engine working according to Humphrey cycle – CFD analysis

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper presents a concept of a new turbine engine with the use of rotating isochoric combustion chambers. In contrast to previously analyzed authors’ engine concepts, here rotating combustion chambers were used as a valve timing system. As a result, several practical challenges could be overcome. An effective ceramic sealing system could be applied to the rotating combustion chambers. It can assure full tightness regardless of thermal conditions and related deformations. The segment sealing elements working with ceramic counter-surface can work as self-alignment because of the centrifugal force acting on them. The isochoric combustion process, gas expansion, and moment generation were analyzed using the CFD tool (computational fluid dynamics). The investigated engine concept is characterized by big energy efficiency and simple construction. Finally, further improvements in engine performance are discussed.
Rocznik
Strony
art. no. e143100
Opis fizyczny
Bibliogr. 19 poz., rys., tab.
Twórcy
  • Institute of Machine Design Fundamentals, Warsaw University of Technology, Narbutta 84, 02-524 Warsaw, Poland
  • Institute of Machine Design Fundamentals, Warsaw University of Technology, Narbutta 84, 02-524 Warsaw, Poland
Bibliografia
  • [1] P. Tarnawski, “Analytical performance evaluation of Humphrey for turbine engine application,” Mach. Dyn. Res., vol. 41, no 3, 27–37, 2017.
  • [2] K. Kamiuto, “Comparison of basic gas cycles under the restriction of constant heat addition,” Appl. Energy, vol.83, no. 6, 2006, pp. 583–593, 2005, doi: 10.1016/j.apenergy.2005.05.008.
  • [3] P. Stathopoulos, “Comprehensive thermodynamic analysis of the Humphrey cycle for gas turbines with pressure gain combustion,” Energies, 11, p. 3521, 2018, doi: 10.3390/en11123521.
  • [4] C. Brophy and G. Roy, “Benefits and challenges of pressure-gain combustion systems for gas turbines,” Mech. Eng., vol. 131, no. 3, pp. 54–55, 2009, doi: 10.1115/1.2009-MAR-8.
  • [5] F. Walraven, “Operational Behavior of a Pressure Wave Machine with Constant Volume Combustion,” ABB Technical Report CHCRC 94–10, 1994.
  • [6] K. Kurec, J. Piechna, and K. Gumowski, “Investigations on unsteady flow within a stationary passage of a pressure wave exchanger by means of PIV measurements and CFD calculations,” Appl. Therm. Eng., vol. 112, no. 5 , pp. 610–620, 2017, doi: 10.1016/j.applthermaleng.2016.10.142.
  • [7] P. Akbari and M.R. Nalim, “Review of recent developments in wave rotor combustion technology,” J. Propul. Power, vol. 25, no. 4, pp. 833–844, 2009, doi: 10.2514/1.34081.
  • [8] P. Tarnawski and W. Ostapski, “Pulse powered turbine engine concept – Numerical analysis of influence of different valve timing concepts on thermodynamic performance,” Bull. Pol. Acad. Sci. Tech. Sci., vol. 66, no. 3, pp. 373–382, 2018, doi: 10.24425/123444.
  • [9] P. Tarnawski, “Pulse powered turbine engine concept,” Ph.D. dissertation, Poland:Warsaw University of Technology,Warsaw, 2018.
  • [10] P. Tarnawski, and W. Ostapski, “Pulse powered turbine engine concept implementing rotating valve timing system: Numerical CFD analysis,” J. Aerosp. Eng., vol. 32, no. 3, p. 04019017, 2018.
  • [11] P. Tarnawski andW. Ostapski, “Turbine engine concept realizing Humphrey cycle,” in Materials, Technologies, Constructions – Constructions and Design, vol. 4. A. Mazurkow, Ed., Poland: Rzeszow University of Technology, 2019, pp 23–43.
  • [12] Turbo Tech 103 Expert, “Compressor Mapping”, Garret Advancing Motion. [Online]. Available: https://www.garrettmotion.com/wp-content/uploads/ 2019/10/GAM_Turbo-Tech-103_Expert-1.pdf. [Accessed:10 Dec. 2020].
  • [13] P. Tarnawski and W. Ostapski, “A concept of a pulse-powered turbine engine with application of self-acting displacement valves- 3D numerical analysis,” SAE Int. J. Engines, vol. 14, no. 3, pp. 419–437, 2021, doi: 10.4271/03-14-03-0025.
  • [14] ANSYS® Academic Associate CFD, ANSYS Fluent User Guide, Release 18.1. Canonsburg, PA,USA, ANSYS Inc., 2016.
  • [15] D. Derlukiewicz, “Method of modeling of thermo-elastic phenomena in layered ceramic coatings”. Ph.D. dissertation, Poland: Wroclaw University of Technology, Wroclaw, 2006.
  • [16] J. Li, E. Gong, W. Li, K. Zhang, and L. Yuan, “Investigation on combustion properties in simplified wave rotor constant volume combustor,” 21st AIAA International Space Planes and Hypersonics Technologies Conference, 2017, doi: 10.2514/6.2017-2384.
  • [17] L. Labarrere, T. Poinsot, A. Dauptain, F. Duchaine, M. Bellenoue, and B. Boust, “Exparimental and numerical study of cyclic variations in a constant volume combustion chamber,” Combust. Flame, vol. 172, pp. 49–61, 2016, doi: 10.1016/j.combustflame.2016.06.027.
  • [18] H. Kato, H. Mashiko, K. Funazaki, and J. Takida, “Multiobjective aerodynamic optimization of a supersonic turbine for higher efficiency and smaller load fluctuation,” 10th World Congress on Structural and Multidisciplinary Optimization, 2013.
  • [19] Gas Turbine Engines, “Aviation week and space technology,” Geocities. [Online]. Available: http://www.geocities.jp/nomonomo2007/AircraftDatabase/AWdata/AviationWeekPages/GTEnginesAWJan2008.pdf. [Accessed: 28 Jan. 2018].
Uwagi
Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2022-2023).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-dd5364d9-af72-42d1-871f-5df02ea37365
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