METHOD FOR OPERATING A GAS TURBINE ASSEMBLY FOR A POWER PLANT AND GAS TURBINE ASSEMBLY FOR A POWER PLANT

A method for operating a gas turbine assembly for a power plant comprises the steps of:- providing a gas turbine assembly (1) comprising a compressor (2), a combustor assembly (4), a turbine (5) and an generator; the compressor (2), the turbine (5) and the generator being connected to a common rotor...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	SINGLA, Ghislain, GRANET, Victor, APPEL, Christoph, SMITH, Richard
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 GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A method for operating a gas turbine assembly for a power plant comprises the steps of:- providing a gas turbine assembly (1) comprising a compressor (2), a combustor assembly (4), a turbine (5) and an generator; the compressor (2), the turbine (5) and the generator being connected to a common rotor (12) rotating around an axis (A); the combustor assembly (4) comprising at least one first combustor (14) and at least one second combustor (15) arranged downstream the first combustor (14) along a gas flow direction (D);- starting-up the gas turbine assembly (1);wherein the step of starting up the gas turbine assembly (1) comprising igniting the second combustor (15) before reaching the minimum load target value and after the ignition of the first combustor (14).