GAS TURBINE ENGINE WITH RESONATOR RINGS

A gas turbine engine has a resonator ring (10) that is formed by two circumferentially extending rings. The first and second circumferentially extending rings (30, 31) have located within them baffles (20). Both the first ring (30) and the second ring (31) are able to mitigate acoustic frequencies g...

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Bibliographische Detailangaben
Hauptverfasser:	DYSZKIEWICZ, Wojciech, CASSAR, Daniel, CRANE, John M, RAJARAM, Rajesh, TERDALKAR, Sachin
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A gas turbine engine has a resonator ring (10) that is formed by two circumferentially extending rings. The first and second circumferentially extending rings (30, 31) have located within them baffles (20). Both the first ring (30) and the second ring (31) are able to mitigate acoustic frequencies generated by the gas turbine engine.