BURNER AND METHOD FOR OPERATING A GAS TURBINE

The burner has an annular premixing channel (21), into which fuel is fed radially. Feeding of fuel can be adjusted during operation. The premixing channel is made up of segments (31, 33), with radial rows of inlets (29) which alternately increase and decrease in diameter in adjacent segments. An ind...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	BLOMEYER, MALTE
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING BURNERS COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The burner has an annular premixing channel (21), into which fuel is fed radially. Feeding of fuel can be adjusted during operation. The premixing channel is made up of segments (31, 33), with radial rows of inlets (29) which alternately increase and decrease in diameter in adjacent segments. An independent claim is included for a method for operating a gas turbine using the burner.