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 (...

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Bibliographische Detailangaben
Hauptverfasser: EROGLU ADNAN, KNOEPFEL HANS PETER
Format: Patent
Sprache:eng
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