COMBUSTION CHAMBER, AND METHOD OF OPERATING COMBUSTION CHAMBER
PROBLEM TO BE SOLVED: To provide a combustion chamber (10) for a gas turbine, having a plurality of first and second premixed fuel supply devices (11, 12) connected to a combustion device (13), which has a first zone (14) connected with the first premixed fuel supply devices (11) and a second zone (...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Patent |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | PROBLEM TO BE SOLVED: To provide a combustion chamber (10) for a gas turbine, having a plurality of first and second premixed fuel supply devices (11, 12) connected to a combustion device (13), which has a first zone (14) connected with the first premixed fuel supply devices (11) and a second zone (15) connected with the second premixed fuel supply devices (12).SOLUTION: The second premixed fuel supply devices (12) are shifted along a longitudinal axis (16) of a combustion device with respect to the first premixed fuel supply devices (11). The first zones (14) are disposed at the upstream of the second premixed fuel supply devices (12) with respect to the longitudinal axis of the combustion device. |
---|