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Zastosowanie płynnego wodoru jako paliwa do samolotów pasażerskich
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Abstrakty
The paper briefly reviews a recent initiative on the application of hydrogen as a fuel for future commercial aircraft. Special attention is paid to the benefits of using liquid hydrogen (LH2) to power aircraft engines. A comparison of LH2 to other fuels is presented, as well as a comparison of LH2 hazard to hazard imposed by typical jet fuel. Major attention is focused on the combustion of hydrogen benefits in turbine engines with classic deflagrative combustion chamber and engines utilizing detonative combustion of the hydrogen-air mixture. Benefits and problems with the utilization of LH2 are discussed in this paper.
W artykule dokonano przeglądu niedawnej inicjatywy dotyczącej zastosowania wodoru jako paliwa do przyszłych statków komercyjnych. Szczególną uwagę zwrócono na korzyści z zastosowania ciekłego wodoru (LH2) do zasilania silników lotniczych. Porównano LH2 z innymi paliwami oraz przedstawiono zagrożenia z zastosowania LH2 z zagrożeniami stosowania tradycyjnego silnika odrzutowego. Ponadto, skupiono się również na spalaniu wodoru w silnikach turbinowych z klasyczną deflagracyjną komorą spalania oraz silnikach z detonacyjną komorą spalania mieszanki wodorowo-powietrznej. W artykule omówiono także zalety i problem związane z wykorzystaniem LH2.
Czasopismo
Rocznik
Tom
Strony
157--175
Opis fizyczny
Bibliogr. 50 poz., rys., tab.
Twórcy
autor
- Łukasiewicz Research Network – Institute of Aviation (Sieć Badawcza Łukasiewicz – Instytut Lotnictwa)
Bibliografia
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- 17. Kawalec M., Perkowski W., Łukasik B., Bilar A., Wolański P.: Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz – Institute of Aviation. Combustion Engines, 191(4), 2022, DOI 10.19206/CE-145409.
- 18. Kawalec M., Perkowski W., Wolański P.: Development of Rocket Engines with Detonation Combustion Chamber. In: Research on detonative propulsion in Poland, ed. Wolański P., pp. 163-181, Institute of Aviation Scientific Publication, Warsaw 2021.
- 19. Kawalec M., Wolański P.: Development of Rocket Engine with Continuously Rotating Detonation supplied by Liquid Propellants. Proceeding of EUCASS, Lille, France, 27 June-1 July, 2022.
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- 35. Voitsekhovskii B.V.: Stationary spin detonation. Soviet Journal of Applied mechanics and Technical Physics, vol. 3, 1960.
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- 37. Wolański P. (ed.): Research on detonative propulsion in Poland. Institute of Aviation Scientific Publication No. 60, Łukasiewicz Research Network – Institute of Aviation, Warsaw 2021.
- 38. Wolański P., Balicki W., Perkowski W., Bilar A.: Experimental Research of Liquid Fueled Continuously Rotating Detonation Chamber. Shock Waves, 2021, DOI 10.1007/s00193-021-01014.
- 39. Wolański P., Kalina P., Balicki W., Rowiński A., Perkowski A., Kawalec M., Łukasik B.: Development of gasturbine with detonation chamber. Detonation Control for Propulsion, Pulse Detonation and Rotating Detonation Engines, Springer: Cham, Switzerland, 2018, pp. 23-37.
- 40. Wolański P., Kindracki J., Fujiwara T., Oka Y., Shima-uchi K.: An Experimental Study of Rotating Detonation Engine. In Proceedings of the 20th ICDERS, Minsk 2005.
- 41. Wolanski P., Kindracki J., Fujiwara T.: An Experimental Study of Small Rotating Detonation Engine. Proceedings of the Fifth International Colloquium on Pulsed and Continuous Detonations, Moscow, Russia, July 3-7, 2006.
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- 43. Wolański P.: Detonation Engines. Journal of KONES, Vol. 18 (2011), No.3 pp.515-521.
- 44. Wolański P.: Detonative Propulsion. Proceedings of the Combustion Institute, 34, pp.125-158, Elsevier, 2013.
- 45. Wolanski P.: Development of the continuous rotating detonation engines. In: Progress in Pulsed and Continuous Detonations, ed. by G.D. Roy and S.M. Frolov, Moscow, Torus Press, 2010.
- 46. Wolański P.: RDE research and development in Poland. Shock Waves, 2021, DOI 10.1007/s00193-021-01038-2.
- 47. Wolański P.: Rotating Detonation Wave Stability. In: Research on detonative propulsion in Poland, ed. Wolański P., pp. 71-92, Institute of Aviation Scientific Publication, Warsaw 2021.
- 48. Yi T.-H., Lou J., Turangan C., Choi J.-Y., Wolanski P.: Propulsive performance of a continuously rotating detonation engine. Journal of Propulsion and Power, vol. 27, 2011.
- 49. Yi T.H., Lou J., Wolanski P., Turangan C., Khoo B.C.: Effect of nozzle shapes on the performance of continuously rotating detonation engine. AIAA paper 2010-0152, 2010, DOI: 10.2514/6.2010-152.
- 50. Yi T.-H., Turangan C., Lou J., Wolanski P., Kindracki J.: A three-dimensional numerical study of rotational detonation in an annular chamber. AIAA 2009-0634. 2009.
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-90fb3030-2b00-4155-b38b-0d545c5a3f93