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Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz - Institute of Aviation

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In the paper short information about advantages of introduction of detonation combustion to propulsion systems is briefly discussed and then research conducted at the Łukasiewicz - Institute of Aviation on development of the rotating detonation engines (RDE) is presented. Special attention is focused on continuously rotating detonation (CRD), since it offers significant advantages over pulsed detonation (PD). Basic aspects of initiation and stability of the CRD are discussed. Examples of applications of the CRD to gas turbine and rocket engines are presented and a combine cycle engine utilizing CRD are also evaluated. The world's first rocket flight powered by liquid propellant detonation engine is also described.
Czasopismo
Rocznik
Strony
51--57
Opis fizyczny
Bibliogr. 45 poz., il. kolor., fot., rys., wykr.
Twórcy
  • Aircraft Propulsion System Department, Łukasiewicz Research Network - Institute of Aviation
  • Aircraft Propulsion System Department, Łukasiewicz Research Network - Institute of Aviation
  • Aircraft Propulsion System Department, Łukasiewicz Research Network - Institute of Aviation
autor
  • Aircraft Propulsion System Department, Łukasiewicz Research Network - Institute of Aviation
  • Łukasiewicz Research Network - Institute of Aviation
Bibliografia
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  • [7] SHEN, P.I.-W., ADAMSON, T.C. Theoretical analysis of a rotating two-phase detonation in liquid rocket motors. Acta Astronautica. 1972, 17, 715-728.
  • [8] EIDELMAN, S., GROSSMANN, W., LOTTATI, I. Review of propulsion applications and numerical simulations of the pulsed detonation engine concept. Journal of Propulsion and Power. 1991, 7(6), 857-865. https://doi.org/10.2514/3.23402
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  • [15] SHIMO, M., HEISTER, S.D. Multicyclic-detonation-initiation studies in valveless pulsed detonation combustors. Journal of Propulsion and Power. 2008, 24(2), 336-344. https://doi.org/10.2514/1.29546
  • [16] PENG, C., FAN, W., ZHENG, L. et al. Experimental investigation on valves air-breathing dual-tube pulse detonation engines. Applied Thermal Engineering. 2012, 51(1-2), 1116-1123. https://doi.org/10.1016/j.applthermaleng.2012.10.026
  • [17] LU, J., ZHENG, L., WANG, Z. et al. Operating characteristics and propagation of back-pressure waves in a multi-tube two-phase valveless air-breathing pulse detonation combustor. Experimental Thermal and Fluid Science. 2015, 61, 12-23. https://doi.org/10.1016/j.expthermflusci.2014.10.010
  • [18] LU, J. Investigations on key technologies of the pulse detonation turbine engine. Northwestern Polytechnical University.
  • [19] RASHEED, A., TANGIRALA, V.E., VANDERVORT, C.L. et al. Interactions of a pulsed detonation engine with a 2D blade cascade. 42nd AIAA Aerospace Sciences Meeting and Exhibit. Reno 2004. https://doi.org/10.2514/6.2004-1207
  • [20] FROLOV, S.M. (ed.) Pulsed Detonation Engines. Torus Press. Moscow 2006.
  • [21] FROLOV, S.M., AKSENOV, V., IVANOV, V. et al. Catapult launching tests of an unmanned aerial vehicle with a ramjet pulsed detonation engine. European Conference for Aeronautics and Space Sciences. 2008. https://doi.org/10.13009/EUCASS2019-178
  • [22] DEAN, A.J., RASHEED, A., TANGIRALA, V.E. et al. Operation and noise transmission of an axial turbine driven by a pulse detonation combustor. Proceedings of International Gas Turbine Institute. ASME Turbo Expo 2005, 6, 1275-1284. https://doi.org/10.1115/GT2005-69141
  • [23] NORRIS, G. Pulse power: pulse detonation engine-powered flight demonstration marks milestone in Mojave. Aviation Week & Space Technology. 2008, 168(7), 60.
  • [24] WOLAŃSKI, P. Detonation engines. Journal of KONES. 2011, 18(3), 515-521.
  • [25] WOLAŃSKI, P. Detonative propulsion. Proceedings of the Combustion Institute. 2013, 34(1), 125-158. https://doi.org/10.1016/j.proci.2012.10.005
  • [26] XIE, Q., JIA, Z., WENA, H. et al. Review on the rotating detonation engine and typical problems. Transaction on Aerospace Research. 2020, 4(261), 107-163. https://doi.org/10.2478/tar-2020-0024
  • [27] WOLAŃSKI, P. (ed.) Research on detonative propulsion in Poland. Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa. Warsaw 2021.
  • [28] NETTLETON, M.A. Gaseous Detonations: Their Nature, Effects and Control. Butterworths. London 1987.
  • [29] WOLAŃSKI, P. Rotating detonation wave stability. 23rd International Colloquium on the Dynamics of Explosions and Reactive Systems. Irvine 2011. http://www.icders.org/ICDERS2011/abstracts/ICDERS2011-0211.pdf
  • [30] XIE, Q., WEN, H., LI, W. et al. Analysis of operating diagram for H2/air rotating detonation combustors under lean fuel condition. Energy. 2018, 151, 408-419. https://doi.org/10.1016/j.energy.2018.03.062
  • [31] SUCHOCKI, J., YU, S.T., HOKE, J. et al. Rotating detonation engine operation. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Nashville 2012. https://doi.org/10.2514/6.2012-119
  • [32] YI, T-H., JING, L., TURANGAN, C. et al. Numerical study of detonation processes in rotating detonation engine and its propulsive performance. Transaction on Aerospace Research. 2020, 3(260), 30-48. https://doi.org/10.2478/tar-2020-0015
  • [33] KAWALEC, M., PERKOWSKI, W., WOLANSKI, P. Development of rocket engines with detonation combustion chamber. [In] Wolański, P. (ed.): Research on detonative propulsion in Poland. Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa. Warsaw 2021.
  • [34] BYKOVSKII, F.A., ZHDAN, S.A., VEDERNIKOV, E.F. Continuous spin detonations. Journal of Propulsion and Power. 2006, 22(6), 1204-1216. https://doi.org/10.2514/1.17656
  • [35] ANAND, V., GEORGE, A.S., DRISCOLL, R. et al. Characterization of instabilities in a rotating detonation combustor. International Journal of Hydrogen Energy. 2015, 40(46), 16649-16659. https://doi.org/10.1016/j.ijhydene.2015.09.046
  • [36] TANG, X.M., WANG, J.P., SHAO, Y.T. Three-dimensional numerical investigations of the rotating detonation engine with a hollow combustor. Combustion and Flame. 2015, 162(4), 997-1008. https://doi.org/10.1016/j.combustflame.2014.09.023
  • [37] FOTIA, M. Update on air breathing detonation driven propulsion research. International Workshop on Detonation for Propulsion. 2015.
  • [38] FOTIA, M., HOKE, J., SCHAUER, F. Experimental performance scaling of rotating detonation engines operated on gaseous fuels. Journal of Propulsion and Power. 2017, 33(5), 1-10. https://doi.org/10.2514/1.B36213
  • [39] HEISTER, S., SLABAUGH, C. et al. Advancing pressure gain combustion in terrestrial turbine systems. University Turbine Systems Research Workshop. 1004. 2016. https://www.netl.doe.gov/sites/default/files/2017-11/utsr-25343-kickoff-presentation.pdf
  • [40] EUDE, Y., DAVIDENKO, D., FALEMPIN, F. et al. Use of the adaptive mesh refinement for 3D simulations of a CDWRE (continuous detonation wave rocket engine). 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco 2011. https://doi.org/10.2514/6.2011-2236
  • [41] DAVIDENKO, D., EUDE, Y., FALEMPIN, F. Numerical study on the annular nozzle optimization for rocket application. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Bremen 2009. https://doi.org/10.2514/6.2009-7390
  • [42] WOLAŃSKI, P., KALINA, P., BALICKI, W. et al. Development of Gasturbine with Detonation Chamber. Detonation Control for Propulsion, Pulse Detonation and Rotating Detonation Engines. Springer, Cham 2018. https://doi.org/10.1007/978-3-319-68906-7_2
  • [43] WOLAŃSKI, P., BALICKI, W., PERKOWSKI, W. et al. Experimental research of liquid-fueled continuously rotating detonation chamber. Shock Waves. 2021, 31, 807-812. https://doi.org/10.1007/s00193-021-01014-w
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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-1275e681-4de0-4a08-9810-91c0c03ab4be
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