This paper gives the idea and builds a sample test bench that allows for full testing and checking of new heat and anti-wear layers used in small plane piston engines. It explains the design idea, tech answers, and ways to watch the most key params like temp, load, spin speed, and forces of friction. The bench makes a copy of the running state usual for plane engines, making it easy to check the rubbing and heat features of the picked coats and how they act under set conditions.
This includes sample test results as well as the ability to read specific engine parameters by standard engine components without any need for specialized anti-wear coatings. The novelty of this work lies in the development of a unique measurement and control system for real-time tracking of all critical engine parameters and for adaptive proper conditions to different scenarios. Therefore, the test stand should not only accurately repeat the loads typical of small aviation engines, but also permit the preparation and study of multi-layer anti-wear and thermal coatings with drastically extended service life and reduced operation costs for such power units.
REFERENCES(26)
1.
Balicki W, Chachurski R, Głowacki P, Godzimirski J, Kawalec K, Kozakiewicz A et al. Lotnicze silniki turbinowe. Konstrukcja, eksploatacja, diagnostyka (in Polish). Wydawnictwa Naukowe Instytutu Lotnictwa. Warszawa 2010.
Balicki W, Korczewski Z, Szczeciński S. Possibilities of the performance improvement of the aero- and marine propulsion units equipped with combustion piston engines. Journal of Polish CIMEEAC. 2010;5(1):7-22.
Chachurski R, Omen Ł, Panas AJ, Zalewski P. Mobilne stanowisko przygotowania i obsługi miniaturowych turbinowych silników odrzutowych – Zestaw odrzutowych celów powietrznych ZOCP-JET2. Biuletyn WAT. 2020;LXIX(4). https://doi.org/10.5604/01.300....
Chachurski R. Zdarzenia lotnicze związane z oblodzeniem silników turbinowych (in Polish). XIII Ogólnopolska Konferencja Mechanika w Lotnictwie; Kazimierz Dolny2008.
Dziubak S, Dziubak T. Experimental study of an axial flow cyclone with ongoing dust removal from a settling tank. Chem Eng Process–Process Intensif. 2025;209:110167. https://doi.org/10.1016/j.cep.....
Dziubak T, Dziubak S, Tomaszewski M. Numerical study of the effect of axial cyclone inlet velocity and geometrical parameters on separation efficiency and pressure drop. Powder Technol. 2023;427:118692. https://doi.org/10.1016/j.powt....
Frant M, Kachel S, Maślanka W. Gust modeling with state-of-the-art computational fluid dynamics (CFD) software and its influence on the aerodynamic characteristics of an unmanned aerial vehicle. Energies. 2023;16:6847. https://doi.org/10.3390/en1619....
Johnson RO, O’Neil M. Unmanned aerial vehicles in perspective: effects, capabilities, and technologies. United States Air Forces Scientific Advisory Board. 2003.
Kozakiewicz A, Jóźwiak S, Jóźwiak P, Kachel S. Material origins of the accelerated operational wear of RD-33 engine blades. Materials. 2021;14:336. https://doi.org/10.3390/ma1402....
Olejnik A, Kachel S, Rogólski R. Techniques for adjusting qualities of aircraft structural models for more effective aeroelastic flutter analyses. J Phys Conf Ser. 2023;2526:012040. https://doi.org/10.1088/1742-6....
Olejnik A, Kiszkowiak Ł, Rogólski R, Chmaj G, Radomski M, Majcher M et al. The use of unmanned aerial vehicles in remote sensing systems. Sensors. 2020;20:2003. https://doi.org/10.3390/s20072....
Oszczypała M, Ziółkowski J, Małachowski J. Reliability analysis of military vehicles based on censored failures data. Appl Sci. 2022;12:2622. https://doi.org/10.3390/app120....
Panas AJ, Chachurski RZ, Jakielaszek Z. In-flight testing of the susceptibility to icing of the induction system of the Rotax 582 engine. Journal of KONES. 2016;23(4).
Świątek P. Porównanie parametrów eksploatacyjnych samochodowych silników spalinowych i do samolotów ultralekkich. TTS Technika Transportu Szynowego. 2015;22(12):2159-2162.
Wróblewski P, Iskra A. Problems of reducing friction losses of a piston-ring-cylinder configuration in a combustion piston engine with an increased isochoric pressure gain. SAE Technical Paper 2020-01-2227. 2020. https://doi.org/10.4271/2020-0....
Wróblewski P, Koszalka G. An experimental study on frictional losses of coated piston rings with symmetric and asymmetric geometry. SAE Int J Engines. 2021;14(6):853-866. https://doi.org/10.4271/03-14-....
Wróblewski P, Świątek P, Kachel S, Zyska T. Development and research of a hybrid power unit for ultralight aircraft: an innovative approach to energy efficiency and operational flexibility. Combustion Engines. 2024;197(2):83-96. https://doi.org/10.19206/CE-17....
Ziółkowski J, Małachowski J, Oszczypała M, Szkutnik-Rogoż J, Lęgas A. Modelling of the military helicopter operation process in terms of readiness. Defence Sci J. 2021;71(5):602-611.
Żurek J, Małachowski J, Ziółkowski J, Szkutnik-Rogoż J. Reliability analysis of technical means of transport. Appl Sci. 2020;10:3016. https://doi.org/10.3390/app100....
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.