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Prethodno priopćenje
https://doi.org/10.17818/NM/2016/SI2

A Hybrid Diagnostic System for a Small Turbojet Engine

Rudolf Andoga ; Faculty of Aeronautics Technical University of Košice Slovakia
František . Adamčík jr ; Faculty of Aeronautics Technical University of Košice Slovakia
Ján Hrabovský ; Faculty of Aeronautics Technical University of Košice Slovakia
Tomáš Vaispacher ; Faculty of Aeronautics Technical University of Košice Slovakia

Puni tekst: engleski, pdf (3 MB) str. 86-92 preuzimanja: 265* citiraj
APA 6th Edition
Andoga, R., Adamčík jr, F., Hrabovský, J. i Vaispacher, T. (2016). A Hybrid Diagnostic System for a Small Turbojet Engine. NAŠE MORE, 63 (3 Special Issue), 86-92. https://doi.org/10.17818/NM/2016/SI2
MLA 8th Edition
Andoga, Rudolf, et al. "A Hybrid Diagnostic System for a Small Turbojet Engine." NAŠE MORE, vol. 63, br. 3 Special Issue, 2016, str. 86-92. https://doi.org/10.17818/NM/2016/SI2. Citirano 24.01.2020.
Chicago 17th Edition
Andoga, Rudolf, František . Adamčík jr, Ján Hrabovský i Tomáš Vaispacher. "A Hybrid Diagnostic System for a Small Turbojet Engine." NAŠE MORE 63, br. 3 Special Issue (2016): 86-92. https://doi.org/10.17818/NM/2016/SI2
Harvard
Andoga, R., et al. (2016). 'A Hybrid Diagnostic System for a Small Turbojet Engine', NAŠE MORE, 63(3 Special Issue), str. 86-92. https://doi.org/10.17818/NM/2016/SI2
Vancouver
Andoga R, Adamčík jr F, Hrabovský J, Vaispacher T. A Hybrid Diagnostic System for a Small Turbojet Engine. NAŠE MORE [Internet]. 2016 [pristupljeno 24.01.2020.];63(3 Special Issue):86-92. https://doi.org/10.17818/NM/2016/SI2
IEEE
R. Andoga, F. Adamčík jr, J. Hrabovský i T. Vaispacher, "A Hybrid Diagnostic System for a Small Turbojet Engine", NAŠE MORE, vol.63, br. 3 Special Issue, str. 86-92, 2016. [Online]. https://doi.org/10.17818/NM/2016/SI2

Sažetak
A diagnostic system is one of the key components securing the safety of operation of a turbojet engine. There are many different engineering approaches how to design engine diagnostic systems applied in real-world conditions. We propose a novel approach for a diagnostic system design to be applied on the object of a small turbojet engine using thermal diagnostics combined with a more traditional model based approach. The combination of these two approaches together with application of methods from the area of computational intelligence create a hybrid diagnostic system, which can be integrated with a control system of the engine. The article also deals with experimental validation of the designed diagnostic system on the object of a small turbojet engine iSTC-21v in laboratory conditions.

Ključne riječi
turbojet engines; diagnostics; computational intelligence; hybrid systems

Hrčak ID: 162525

URI
https://hrcak.srce.hr/162525

Posjeta: 357 *