Combustion chamber, in particular for a gas turbine, with at least two resonator devices

A combustion chamber according to the invention, in particular for a gas turbine, includes at least one combustion chamber wall (3) through which cooling fluid flows and at least one resonator device (5, 6). The combustion chamber (1) according to the invention is distinguished in that the resonator...

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Bibliographische Detailangaben
1. Verfasser:	BETHKE SVEN,BUCHAL TOBIAS,GLESSNER JOHN CARL,HUTHMICHAEL,NIMPTSCH HARALD,PRADE BERND
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FORCOMBUSTION CHAMBERS, e.g. FIREBRIDGES COMBUSTION APPARATUS COMBUSTION PROCESSES DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDEDFOR DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS INCOMBUSTION CHAMBERS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTIONAPPARATUS WEAPONS
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Beschreibung
Zusammenfassung:	A combustion chamber according to the invention, in particular for a gas turbine, includes at least one combustion chamber wall (3) through which cooling fluid flows and at least one resonator device (5, 6). The combustion chamber (1) according to the invention is distinguished in that the resonator device (5, 6) is integrated into the combustion chamber wall (3) in such a way that it has the cooling fluid flow passing therethrough.