COMBUSTER ASSEMBLY FOR A TURBINE ENGINE

A combustor assembly (100) for a gas turbine engine is provided. The combustor assembly (100) generally includes an annular dome (118) and a liner (108). The liner (108) at least partially defines a combustion chamber and includes the forward end (112) received within a slot (122) defined by the ann...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	STIEG, Michael Alan, TOWLE, Brian Christopher, BLOOM, Nicholas John
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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