The study of the continuously rotating detonation combustion chamber supplied with different types of fuel

• Autorzy: Łukasik B. , Czyż S. , Irzycki A. , Rowiński A.
• Języki publikacji: EN

Abstrakty

EN

The paper summarizes research that was conducted last year as part of the project of “Turbine engine with detonation combustion chamber”. In this project, throughout 2012 and early 2013, tests were carried out on a test stand connected to the compressed air system. Research, of the rotating detonation phenomena, was carried out for a number of detonation chambers with different interior channel geometry. In addition, for each geometry configuration, tests were carried out for different levels of choking of the chamber outlet and hence for different pressures conditions inside the detonation chamber. This article presents the results of tests carried out for gaseous (hydrogen), hybrid (hydrogen + kerosene) and liquid (Jet-A) fuels, using different types of fuel injectors and for different fuel injection configuration settings (inside the chamber, or in front of the chamber). During these tests, parameters such as pressure behind the detonation wave (using piezoelectric sensors), the static pressure in front of and inside the detonation chamber and temperature: before, inside and at the outlet of the chamber, were measured. Research was performed for the various mass flow rates of air and fuel injected into the chamber that means for the different air-fuel equivalence ratios (Lambda). The main achievement of this study was to obtain a stable and reproducible rotating detonation of air and heated kerosene (Jet-A) mixture, thus the results presented in this paper presents mainly these tests as the most interesting to the reader

Słowa kluczowe

EN

rotating detonation; air/Jet-A detonation; detonation combustion chamber; internal combustion engine

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2013
• Tom: Vol. 20, No. 3
• Strony: 259--266
• Opis fizyczny: Bibliogr. 4 poz., rys.

Twórcy

autor

Łukasik B.

• Institute of Aviation Krakowska Avenue 110/114, 02-256 Warszawa tel.: [phone] ext. 426, fax: [phone]

autor

Czyż S.

• Institute of Aviation Krakowska Avenue 110/114, 02-256 Warszawa tel.: [phone] ext. 426, fax: [phone]

autor

Irzycki A.

• Institute of Aviation Krakowska Avenue 110/114, 02-256 Warszawa tel.: [phone] ext. 426, fax: [phone]

autor

Rowiński A.

• Institute of Aviation Krakowska Avenue 110/114, 02-256 Warszawa tel.: [phone] ext. 426, fax: [phone]

Bibliografia

• [1] Bykovski, F. A., Verdernikov, E. F, Polozov, S. V., Golubev, Yu. V., Initiation of Detonation in Flows of Fuel-Air Mixtures, Combustion, Explosion and Shock Waves, Vol. 43, No. 3, 2007.
• [2] Kailasanath, K., Review of Propulsion Applications of Detonation Waves, AIAA Journal 2000, Vol. 38, No. 9, 2000.
• [3] Kindracki, J., Badania eksperymentalne i symulacje numeryczne procesu inicjacji wirującej detonacji gazowej, PhD dissertation, MEiL, Politechnika Warszawska, Warszawa 2008.
• [4] Kuo, K., Principles of Combustion, Wiley, New York 1986.