PZL-10 turboshaft engine : system design review

• Autorzy: Czarnecki Michał , Olsen John , Ma Ruixian

Identyfikatory

DOI

10.2478/kones-2019-0003

• Języki publikacji: EN

Abstrakty

EN

The PZL – 10-turboshaft gas turbine engine is straight derivative of GTD-10 turboshaft design by OKMB (Omsk Engine Design Bureau). Prototype engine first run take place in 1968. Selected engine is interested platform to modify due gas generator layout 6A+R-2, which is modern. For example axial compressor design from successful Klimov designs TB2-117 (10A-2-2) or TB3-117 (12A-2-2) become obsolete in favour to TB7-117B (5A+R-2-2). In comparison to competitive engines: Klimov TB3-117 (1974 – Mi-14/17/24), General Electric T-700 (1970 – UH60/AH64), Turbomeca Makila (1976 – H225M) the PZL-10 engine design is limited by asymmetric power turbine design layout. This layout is common to early turboshaft design such as Soloview D-25V (Mil-6 power plant). Presented article review base engine configuration (6A+R+2+1). Proposed modifications are divided into different variants in terms of design complexity. Simplest variant is limited to increase turbine inlet temperature (TIT) by safe margin. Advanced configuration replace engine layout to 5A+R+2-2 and increase engine compressor pressure ratio to 9.4:1. Upgraded configuration after modification offers increase of generated power by 28% and SFC reduction by 9% – validated by gas turbine performance model. Design proposal corresponds to a major trend of increasing available power for helicopter engines – Mi-8T to Mi-8MT – 46%, H225M – Makila 1A to 1A2 – 9%, Makila 1A2 to Makila 2-25%.

Słowa kluczowe

EN

gas turbine; design; topology; turbo shaft; performance

• 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: 2019
• Tom: Vol. 26, No. 1
• Strony: 23--29
• Opis fizyczny: Bibliogr. 12 poz., rys.

Twórcy

autor

Czarnecki Michał

• Rzeszow University of Technology, Department of Aircraft and Aircraft Engines Powstancow Warszawy Av. 8, 35-959 Rzeszow, Poland tel.: [phone], fax: [phone]

autor

Olsen John

• School of Mechanical and Manufacturing Engineering The University of New South Wales, Sydney, Ainsworth Building, N.S.W. 2052, Sydney, Australia tel.: [phone], fax: [phone]

autor

Ma Ruixian

• School of Energy Science and Engineering Harbin Institute of Technology Harbin, 150001, Heilongjiang, China

Bibliografia

• [1] Lozitskiy, L. P., Vetrov, A. N., Doroshko, S. M., Ivanov, V. P., Konyaev, Konstruktsiya i prochnost' aviatsionnykh gazoturbinnykh, Vozdushnyy, Moskva 1992.
• [2] Zrelov, V. A, Otechestvennye gazoturbinnye dvigateli, Osnovnye parametry i konstruktivnye skhemy, Mashinostroenie 2005.
• [3] Vzlyot, Natsional'nyy aerokosmicheskiy zhurnal, ISSN 1819-1754, 4, pp. 9-29, Moskva 2006.
• [4] Brophy, F., Mah, S., Turcotte, J. Preliminary Multi-Dysciplinary Optimisation (PMDO) an Example at Engine Level, RTO-EN-AVT-167, 2009.
• [5] Dixon, S. L., Fluid Mechanics, Thermodynamics of Turbomachinery, Pergamon Press Ltd., 1998.
• [6] Panchenko, Y., Patel, K., Moustapha, H., Dowhan, M. J., Mah, S., Hall, D., Preliminary Multi-Dysciplinary Optimisation in Turbomachinery Design, Defense Technical Information Center, ADP014195, 2002.
• [7] Schobeiri, M., Turbomachinery Flow Physics and Dynamic Performance, Springer-Verlag, Berlin 2005.
• [8] Shmyrov, V. F, Tsukanov, R. U, Ryzhenko, A. I., Pehterev, V. D, Airplane power plant systems designing, Kharkov aviation institute, 2010.
• [9] Dżygadło, Z., Łyżwiński, M., Otyś, J., Szczeciński, S., Wiatrek, R., Zespoły wirnikowe silników turbinowych, Wydawnictwa Komunikacji i Łączności, Warszawa 1982.
• [9] Dżygadło, Z., Łyżwiński, M., Otyś, J., Szczeciński, S., Wiatrek, R., Zespoły wirnikowe silników turbinowych, Wydawnictwa Komunikacji i Łączności, Warszawa 1982.
• [10] Jakubowski, R., Modeling and analysis of jet engine with cooling turbine, Journal of KONES Powertrain and Transport, Vol. 24 , No. 1 , 2017.
• [11] Stieczkin, B., Kazandżan, P., Aleksiejew, Ł., Goworow, A., Konowałow, N., Nieczajew, J., Fiedorow, R., Teoria silników odrzutowych, MON, 1961.
• [12] PZL-10W- Instrukcja użytkowania i obsługi technicznej 19.02.208, WSK, Rzeszow 1987.

Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).