Method for operating a burner of a gas turbine and a power plant

The gas turbine burner operating process involves dividing the synthetic gas (SG) into first and second part flows (SG1, SG2). These are led separately to the burner for combustion. The process is applied in a power generation system with gas and steam turbines with a carburation device for a fossil...

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Bibliographische Detailangaben
Hauptverfasser:	FRANK HANNEMANN, ANDREAS HEILOS, BERTHOLD KOSTLIN, MICHAEL HUTH
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIR SUPPLY BLASTING BURNERS COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS DRAUGHT-INDUCING ENGINE PLANTS IN GENERAL ENGINE PLANTS NOT OTHERWISE PROVIDED FOR ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING STEAM ACCUMULATORS STEAM ENGINE PLANTS STEAM ENGINES SUPPLYING NON-COMBUSTIBLE LIQUID OR GAS WEAPONS
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Beschreibung
Zusammenfassung:	The gas turbine burner operating process involves dividing the synthetic gas (SG) into first and second part flows (SG1, SG2). These are led separately to the burner for combustion. The process is applied in a power generation system with gas and steam turbines with a carburation device for a fossil fuel.