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

• Autorzy: Kawalec Michał , Perkowski Witold , Łukasik Borys , Bilar Adam , Wolański Piotr

Identyfikatory

DOI

10.19206/CE-145409

• 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.

Słowa kluczowe

EN

detonation; detonation engines; rotating detonation engine; RDE; experimental rocket

PL

detonacja; silniki detonacyjne; obrotowe silniki detonacyjne; RDE; rakieta eksperymentalna

• Wydawca: Polskie Towarzystwo Naukowe Silników Spalinowych
• Czasopismo: Combustion Engines
• Rocznik: 2022
• Tom: R. 61, nr 4
• Strony: 51--57
• Opis fizyczny: Bibliogr. 45 poz., il. kolor., fot., rys., wykr.

Twórcy

autor

Kawalec Michał

• Aircraft Propulsion System Department, Łukasiewicz Research Network - Institute of Aviation

• https://orcid.org/0000-0003-3147-3516

autor

Perkowski Witold

• Aircraft Propulsion System Department, Łukasiewicz Research Network - Institute of Aviation

• https://orcid.org/0000-0002-7580-5319

autor

Łukasik Borys

• Aircraft Propulsion System Department, Łukasiewicz Research Network - Institute of Aviation

• https://orcid.org/0000-0003-4512-2880

autor

Bilar Adam

• Aircraft Propulsion System Department, Łukasiewicz Research Network - Institute of Aviation

• https://orcid.org/0000-0001-9479-5075

autor

Wolański Piotr

• Łukasiewicz Research Network - Institute of Aviation

• https://orcid.org/0000-0003-3963-7722

Bibliografia

• [1] ZELDOVICH, Y.B. On the use of detonative combustion in power engineering. Journal of Technical Physics. 1940, 10, 1453-1461.
• [2] VOITSEKOVSKII, B.B. et al. Work of the Siberian Division of the Academy of Sciences of SSSR, 1958, 9.
• [3] VOITSEKHOVSKII, B.V., MITROFANOV, V.V., TOP-CHIYAN, M.E. Structure of the detonation front in gases. Izdatielstvo SO AN SSSR. Novosibirsk 1963 (in Russian).
• [4] SOLOUKHIN, R.I. Shock waves and detonations in gases. Mono Book Corp. Baltimore 1966.
• [5] NICHOLLS, J.A., WILKINSON, H.R., MORRISON, R.B. Intermittent detonation as a thrust-producing mechanism. Jet Propulsion. May 1957.
• [6] ADAMSON, T.C., OLSSON, G.R. Performance analysis of a rotating detonation wave rocket engine. Acta Astronautica. 1967, 13, 405-415.
• [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
• [9] EIDELMAN, S., GROSSMANN, W. Pulsed detonation engine: experimental and theoretical review. American Institute of Aeronautics and Astronautics Paper. 1992. https://doi.org/10.2514/6.1992-3168
• [10] KAILASANATH, K. Review of propulsion application of detonation waves. American Institute of Aeronautics and Astronautics Journal. 2000, 38(9), 1698-1708. https://doi.org/10.2514/2.1156
• [11] HINKEY, J.B., WILLIAMS, J.T., HENDERSON, S.E. et al. Rotary-valved, multiple-cycle, pulse detonation engine experimental demonstration. American Institute of Aeronautics and Astronautics Paper. 1997. https://doi.org/10.2514/6.1997-2746
• [12] GUSTAVSSON, J., NORI, V., SEGAL, C. Inlet/engine interactions in an axisymmetric pulse detonation engine system. Journal of Propulsion and Power. 2003, 19(2), 282-286. https://doi.org/10.2514/2.6109
• [13] RASHEED, A., GLASER, A., DUNTON, R.A. et al. Experimental and numerical investigation of a valved multi-tube PDE. 46th AIAA Aerospace Sciences Meeting and Exhibit. Reno 2008. https://doi.org/10.2514/6.2008-110
• [14] MATSUOKA, K., ESUMI, M., KASAHARA, J. et al. Study on valve systems for pulse detonation engines. 46th AI-AA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Nashville 2010. https://doi.org/10.2514/6.2010-6672
• [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
• [44] FLOTTAU, J., DUBOIS, T. Airbus places big bet on hydrogen propulsion as aviation’s future. Aviation Week and Space Technology. 2020, 25 September. https://aviationweek.com/aerospace/program-management/airbus-places-big-bet-hydrogen-propulsion-aviations-future
• [45] WARWICK, G., NORRIS, G., DUBOIS, T. Drive to decarbonize aviation raises green hydrogen challenges. Aviation Week and Space Technology. 2020, 8 October. https://aviationweek.com/special-topics/sustainability/drive-decarbonize-aviation-raises-green-hydrogen-challenges

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).