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http://yadda.icm.edu.pl:80/baztech/element/bwmeta1.element.baztech-bd4621e9-e594-4d37-9308-4035f03bc725

Czasopismo

Combustion Engines

Tytuł artykułu

Performance analysis of turbofan engine with additional combustion chamber fueled by alternative fuel

Autorzy Marszałek, Natalia 
Treść / Zawartość
Warianty tytułu
Języki publikacji EN
Abstrakty
EN Presented paper is focused on the performance analysis of turbofan engine with additional combustion chamber fueled by alternative fuel. Additional combustion chamber was situated between high pressure turbine and low pressure turbine. Such configuration is also know under the name inter turbine burner (ITB). As an alternative fuels burn in additional combustion chamber were selected cryogenics fuels: liquid hydrogen and liquid methane. The main combustion chamber was supplied by conventional aviation fuel - kerosene. Thermodynamic model of turbofan engine with ITB was implemented in MATLAB environment. The problem of modeling an additional combustion chamber was presented. Analysis was carried out for take-off conditions. Obtained results indicate that implementation of ITB exert a positive influence on engine performance result in thrust increase.
Słowa kluczowe
PL paliwa alternatywne   ciekły wodór   ciekły metan   ITB   silnik turbowentylatorowy  
EN alternative fuels   liquid hydrogen   liquid methane   inter turbine burner   ITB   turbofan engine  
Wydawca Polskie Towarzystwo Naukowe Silników Spalinowych
Czasopismo Combustion Engines
Rocznik 2019
Tom R. 58, nr 4
Strony 249--253
Opis fizyczny Bibliogr. 10 poz., rys., wykr.
Twórcy
autor Marszałek, Natalia
Bibliografia
[1] BUFFI, M.,CHIARAMONTI, D., VALERA-MEDINA, A. Strategies toward experimental assessments of new aviation renewable fuels and blends: the BIOREFLY project, Energy Procedia. 2017, 105, 433-438.
[2] DAGGETT, D.L., HENDRICKS, R.C.,WALTHER, R.C., CORPORAN, E. Alternative fuels for use in commercial aircraft. 2007.
[3] DAGGETT, D.L., HADALLER, O., HENDRICKS, R.C., WALTHER, R.C. Alternative fuels and their potential impact on aviation, NASA/TM-2006-214365, 2006.
[4] EL-SAYED, A.F. Aircraft propulsion and gas turbine engines. CRC Press. 2017.
[5] JAKUBOWSKI, R. Analysis of chosen fuels influence on turboprop engine work performance. Journal of KONES Powertrain and Transport. 2016, 23(2). DOI: 10.5604/ 12314005.1213586.
[6] LIU, F., SIRIGNANO, W.A. Turbojet and turbofan engine performance increase through turbine burners. Journal of Propulsion and Power. 2001, 17(3).
[7] LEFEBVRE, A.H., BALLAL, D.R. Gas turbine combustion - alternative fuels and emissions, 3rd edition. CRC Press. 2010.
[8] ŁAPUCHA, R. Komory spalania silników turbinowo-odrzutowych. Procesy, obliczenia, badania. Wydawnictwa Naukowe Instytutu Lotnictwa. Warszawa 2004.
[9] SARAVANAMUTTO, H., ROGERS, G., COHEN, H., STRAZNICKY, P. Gas turbine theory. Pearson Prenticle Hall. 2009.
[10] Air Transport Action Group (ATAG), Beginner’s Guide to Aviation Biofuels, 2nd, Geneva 2011.
Kolekcja BazTech
Identyfikator YADDA bwmeta1.element.baztech-bd4621e9-e594-4d37-9308-4035f03bc725
Identyfikatory
DOI 10.19206/CE-2019-441