RESONATORS WITH INTERCHANGEABLE METERING TUBES FOR GAS TURBINE ENGINES

The present disclosure provides a gas turbine combustor including a combustion structure (10) having a combustor liner (14) and a flow sleeve (12). The combustor liner (14) includes inner and outer surfaces (31, 30) and defines a combustion zone (15). The gas turbine combustor further includes a plu...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	YOU, Danning, SCHIAVO, Anthony L, KREBS, Werner, PRADE, Bernd, CRANE, John M
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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