COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE

A combustor assembly for a gas turbine engine is provided. The combustor assembly generally includes an annular dome and a liner that at least partially define a combustion chamber. The annular dome defines a plurality of circumferentially spaced fuel injection ports and a plurality of mounting asse...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	VENTURATO MARCO, TURNER DOUGLAS DOWNEY, STEFFENS STEVEN CRAIG, PROANO CADENA VALERIA, ROYER BRIAN MICHAEL
Format:	Patent
Sprache:	chi ; eng
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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