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Multiple Regime Based Fault Detection of Aircraft Piston Engine

Dubravko Miljković

Sažetak

Graphic engine monitors have a capability of setting alarm limits for particular group of engine parameters. Due to large variation of parameters during normal engine operation provided alarm limits are set to values that include large acceptable deviations during a flight. It is possible to separate engine operation to several regimes and propose tighter alarm limits for each of regimes. With these tighter limits it may be possible to detect smaller engine problems earlier.

Ključne riječi

aircraft; piston engine; engine monitor; regime switching; fault detection

Hrčak ID:

148766

URI

https://hrcak.srce.hr/148766

Datum izdavanja:

1.3.2014.

Posjeta: 1.084 *