COMBUSTER ASSEMBLY FOR A TURBINE ENGINE

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

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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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Beschreibung
Zusammenfassung: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 annular dome (118). A mounting assembly (144) attaches the forward end (112) of the liner (108) to the annular dome (118). The mounting assembly (144) includes a pin (162) extending through the slot (122) and the forward end (128) of the annular dome (118). The mounting assembly (144) also includes a grommet (172) positioned in an opening (174) in the forward end (112) of the liner (108). The grommet (172) is also positioned around the pin (162) to protect the liner (108) during operation of the gas turbine engine.