Overview of low emission combustors of aircraft turbine drive units

• Autorzy: Fąfara Jean-Marc

Identyfikatory

DOI

10.19206/CE-2020-407

• Języki publikacji: EN

Abstrakty

EN

It is important to notice that aircraft turbine drive units are commonly used in the modern aviation. The piston engines are often reserved for small and/or sportive aircraft. The turbine drive units are also combustion engine. This paper presents the most popular combustors used in the aeronautical turbine engines. Firstly there are listed the requirements that a combustor has to achieve. Then are presented the combustor designs that permit to achieve the firstly presented requirements. In this work are presented the LPP, TAPS, RQL, graduated combustion zone, VGC, exhaust recirculation system combustors. For each combustor design is enlighten its principle of work, described the etymology of the given name to this design and shown a scheme. The work is closed by a briefly conclusion about the described combustor.

Słowa kluczowe

EN

aircraft; engine; low emission; combustor; design

PL

samolot; silnik; niska emisja; komory spalania; projekt

• Wydawca: Polskie Towarzystwo Naukowe Silników Spalinowych
• Czasopismo: Combustion Engines
• Rocznik: 2020
• Tom: R. 59, nr 4
• Strony: 45--49
• Opis fizyczny: Bibliogr. 11 poz., il. kolor., wykr.

Twórcy

autor

Fąfara Jean-Marc

• Department of Mechanics, Machines and Energy Processes, Faculty of Mechanical and Power Engineering, Wroclaw Unversity of Science and Technology

Bibliografia

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• [3] GŁOWACKI, P., SZCZECIŃSKI, S. Turbinowy silnik odrzutowy jako źródło zagrożeń ekologicznych. Prace Instytutu Lotnictwa. 2011, 4(213), 252-257.
• [4] MARKUSHIN, A., BAKLANOV, A., TSYGANOV, N. Improvement of aircraft GTE emission characteristics by using the microflame fuel combustion in a shortened combustion chamber. Russian Aeronautics (Iz VUZ). 2014, 56(4), 59-62.
• [5] Royce Rolls. The jet engine. Derby, 1986. Printer Royce Rolls plc.
• [6] GUELLOUH, N., SZAMOSI, Z., SIMENFALVI, Z. Combustors with low emission levels for aero gas turbine engines. International Journal of Engineering and Management Sciences. 2019, 4(1), 503-514. https://doi.org/10.21791/IJEMS.2019.1.62.
• [7] TEMME, J.E., ALLISON, P.M., DRISCOLL, J.F. Low frequency combustion instabilities imaged in a gas turbine combustor flame tube. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 2012, Nashville, Tennessee.
• [8] HERBON, J., AICHOLTZ, J., HSIEH, S.Y. et al. N+2 Advanced low NOx combustor technology – Final Report. 2017NASA/CR-2017-219410, E-19298, GRC-E-DAA-TN35615.
• [9] KHOSRAVY EL_HOSSAINI, M. Review of the new combustion technologies in modern gas turbines. In: BENINI, E. Progress in gas turbine performance. Printer IntechOpen, London 2013, 145-164. https://doi.org/10.5772/54403
• [10] BAUDOIN, C., COMMARET, P., LE LETTY, E. et al. Canadian patent no 2 398 669. 2002, Canadian Intellectual Property Office.
• [11] GIERAS, M. Miniaturowe silniki turboodrzutowe. Oficyna Wydawnictwa Politechniki Warszawskiej. Warszawa 2016.

Uwagi

Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2021).