System and method for detecting failure in gas turbine

Certain embodiments of the invention may include systems, methods, and apparatus for detecting failure in gas turbine hardware. According to an example embodiment of the invention, a method 400 for detecting a failure in a gas turbine is provided. The method can include monitoring 402 a parameter as...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	Nirmalan, Nirm Velumylum, Peczka, Daniel Joseph, Carey, Bradley Steven, Intile, John Charles, Szepek, Scott William, John, Justin V
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	Certain embodiments of the invention may include systems, methods, and apparatus for detecting failure in gas turbine hardware. According to an example embodiment of the invention, a method 400 for detecting a failure in a gas turbine is provided. The method can include monitoring 402 a parameter associated with the turbine, wherein the monitored parameter comprises at least one turbine bucket temperature, detecting an event 404 associated with operation of the turbine, wherein the event is based at least in part on the monitored parameter, and initiating shutdown 406 of the turbine upon detection of the event wherein the monitored parameter is above a predetermined value for at least a predetermined time duration.