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

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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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Beschreibung
Zusammenfassung:	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 disclosed, at least comprising a first combustion chamber 1 with a wide operating range, a subsequent deflection unit 2 for deflecting the hot gas flow of the first combustion chamber 1 at least in circumferential direction and including components 11, 12, 13, 14 for injecting and mixing additional air 9 and/or fuel 10, and a sequential combustion chamber 3 with a short residence time, where the temperature of the hot gases reaches its maximum.