Narzędzia help

Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
first last
cannonical link button


Combustion Engines

Tytuł artykułu

Measurement of exhaust gas emissions from miniature turbojet engine

Autorzy Gawron, B.  Białecki, T. 
Treść / Zawartość
Warianty tytułu
Języki publikacji EN
EN This paper presents a methodology developed to measure exhaust gas emissions during operation of a miniature turbojet engine, using a laboratory test rig. The rig has been built for research and development works aimed at modelling and investigating processes and phenomena occurring in jet engines. The miniature jet engines, similarly to full–scale ones used commonly in air transport, are characterized by variable exhaust gas emissions, depending on engine operating parameters. For this reason, an attempt has been made to determine the characteristic features of miniature engine operation modes and to define the variability of operation parameters and exhaust gas emissions as a function of time. According to the authors, the preliminary tests allowed for defining specific profile of engine test, which enables proper measurement regarding exhaust gas emissions using the miniature jet engine. The paper also presents test results for Jet A-1 fuel, according to the used methodology.
Słowa kluczowe
PL proces spalania   wpływ na środowisko   emisja spalin   miniaturowe silniki turboodrzutowe  
EN combustion process   effect on environment   exhaust gas emission   miniature turbojet engine  
Wydawca Polskie Towarzystwo Naukowe Silników Spalinowych
Czasopismo Combustion Engines
Rocznik 2016
Tom R. 55, nr 4
Strony 58--63
Opis fizyczny Bibliogr. 16 poz., wykr.
autor Gawron, B.
autor Białecki, T.
[1] Gawron, B., Kaźmierczak, U. Hydrocarbon biocomponents use in aviation fuels – preliminary analysis of issues, Journal of KONBIN. 2013, 27/28, 63-72.
[2] Kinsey, S.J. et al. Characterization of Emissions from Commercial Aircraft Engines during the Aircraft Particle Emissions eXperiment (APEX) 1 to 3, 2009.
[3] Lobo, P., Whitefield, P.D., Hagen, D.E. et al. The development of exhaust speciation profiles for commercial jet engines, 2007.
[4] Fleuti, E., Maraini, S. Air Quality Assessment Sensitivities, Zurich Airport Case Study. 2012.
[5] International Civil Aviation Organization, ICAO Annex 16: Environmental Protection, Volume II – Aircraft Engine Emissions. 2008.
[6] Badami, M., Nuccio, P., Signoretto, A. Experimental and numerical analysis of a small-scale turbojet engine, Energy Conversion and Management. 2013, 76, 225-233.
[7] Benini, E., Giacometti, S. Design, manufacturing and operation of a small turbojet-engine for research purposes. Applied Energy. 2007, 84, 1102-1116.
[8] Badami, M., Nuccio, P., Pastrone, D., Signoretto, A. Performance of a small-scale turbojet engine fed with traditional and alternative fuels. Energy Conversion and Management. 2014, 82, 219-228.
[9] Habib, Z., Parthasarathy, R., Gollahalli, S. Performance and emission characteristic of biofuel in a small-scale gas turbine engine. Applied Energy. 2010, 87, 1701-1709.
[10] Ibrahim, M.N., Ali, A.H.H., Ookawara, S. Experimental Study on Performance and Emissions of Turbojet Engine Fueled by Alternative Biodiesel. The 23 International Conference On: Environmental Protection is a Must.2013.
[11] Mendez, C.J., Parthasatathy, R.N., Gollahalli, S.R. Performance and emission characteristic of butanol/Jet A blends in a gas turbine engine. Applied Energy. 2014, 118, 135-140.
[12] Chmielewski. M., Gieras. M. Small Gas Turbine GTM-120 bench testing with emission measurements. Journal of KONES. 2015, 22, 47-54.
[13] Gawron, B., Białecki, T. The laboratory test rig with miniature jet engine to research aviation fuels combustion process. Journal of KONBIN. 2015, 36, 79-90.
[14] website of engine manufacturer -
[15] Walsh, P.P., Fletcher, P. Gas Turbine Performance. Second Edition. 2004.
[16] Lefebvre, A.H., Ballal, D.R. Gas Turbine Combustion. Alternative Fuels and Emissions, Third Edition, 2010.
Kolekcja BazTech
Identyfikator YADDA bwmeta1.element.baztech-578640fc-787b-418e-ab67-9d175c001a5f
DOI 10.19206/CE-2016-406