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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 2.785 Kb

str. 86-92

preuzimanja: 556

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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

Datum izdavanja:

27.7.2016.

Posjeta: 1.027 *