METHOD FOR OPERATING A COMBUSTOR FOR A GAS TURBINE AND COMBUSTOR FOR A GAS TURBINE

The invention provides a new path of combustion technology for gas turbine operation with multifuel capability, low emissions of NO x and CO and high thermal efficiency. According to the present invention a method for operating a combustor for a gas turbine and a combustor for a gas turbine are disc...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	FREITAG, EWALD, DOEBBELING, KLAUS
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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