Canted combustor for gas turbine engine

The present disclosure is directed to a combustion section (26) for a gas turbine engine. The combustion section (26) includes a combustor assembly (50), an outer casing (110), a fuel injector assembly (70), and an inner casing (120). The combustor assembly (50) includes an inner liner (52) and an o...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KARANDE, Rishikesh, LIND, David Albin, NAIK, Pradeep, BOARDMAN, Gregory Allen, PATRA, Ajoy
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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