Overview of low emission combustors of aircraft turbine drive units
| 1 | Department of Mechanics, Machines and Energy Processes; Faculty of Mechanical and Power Engineering, Wroclaw University of Science and Technology, Poland |
CORRESPONDING AUTHOR
Jean-Marc Fąfara
Department of Mechanics, Machines and Energy Processes; Faculty of Mechanical and Power Engineering, Wroclaw University of Science and Technology, Wybrzeże Wyspiańskiego, 50-370, Wrocław, Poland
Department of Mechanics, Machines and Energy Processes; Faculty of Mechanical and Power Engineering, Wroclaw University of Science and Technology, Wybrzeże Wyspiańskiego, 50-370, Wrocław, Poland
Submission date: 2020-09-04
Final revision date: 2020-11-03
Acceptance date: 2020-11-04
Publication date: 2020-12-15
Combustion Engines 2020,183(4), 45–49
KEYWORDS
TOPICS
ABSTRACT
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.
REFERENCES (11)
1.
Les oxydes d’azote – Polluant atmosphérique surveillé en Nouvelle-Calédonie: origines, impacts et surveillance. New Caledonia, Printer SCAL’AIR, 2015.
2.
OCDE. Études de l'OCDE sur l'innovation environnementale – Invention et transfert de technologies envi-ronnementales. 2012. Printer OCDE, Paris. https://doi.org/10.1787/207435....
3.
GŁOWACKI, P., SZCZECIŃSKI, S. Turbinowy silnik odrzutowy jako źródło zagrożeń ekologicznych. Prace In-stytutu 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 combus-tion chamber. Russian Aeronautics (Iz VUZ). 2014, 56(4), 59-62.
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....
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 Ex-position. 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.
RELATED ARTICLE
The scientific journal is financed under the Agreement 185/WCN/2019/1 from the funds of the Minister of Science and Higher Education
We process personal data collected when visiting the website. The function of obtaining information about users and their behavior is carried out by voluntarily entered information in forms and saving cookies in end devices. Data, including cookies, are used to provide services, improve the user experience and to analyze the traffic in accordance with the Privacy policy. Data are also collected and processed by Google Analytics tool (more).
You can change cookies settings in your browser. Restricted use of cookies in the browser configuration may affect some functionalities of the website.
You can change cookies settings in your browser. Restricted use of cookies in the browser configuration may affect some functionalities of the website.