METHOD FOR OPERATING A GAS TURBINE ASSEMBLY COMPRISING A SEQUENTIAL COMBUSTOR

A gas turbine for power plant; the gas turbine having an axis and comprising: a compressor (3,30) for compressing air; a feeding of a high reactive fuel (69); a sequential combustor (22,31,33) for mixing and combusting the compressed air with at least a high reactive fuel; at least a turbine (5,7,21...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DUESING, Michael Klaus, CIANI, Andrea
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS 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 MECHANICAL ENGINEERING WEAPONS
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