Apparatus to facilitate decreasing combustor acoustics

A method for operating a gas turbine engine including a compressor and a combustor is provided. The method comprises channeling between about 0% to about 8% of the total airflow discharged from a compressor towards a pilot swirler coupled within the burner, wherein the burner includes a main swirler...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LI SHUII, DAI ZHONG-TAO, HELD TIMOTHY JAMES, MUELLER MARK ANTHONY, VERMEERSCH MICHAEL LOUIS
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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