CANTED COMBUSTOR FOR GAS TURBINE ENGINE

The present disclosure is directed to a combustion section for a gas turbine engine including a combustor assembly, an outer casing, a fuel injector assembly, and an inner casing. An inner liner and an outer liner are each extended at least partially along a lengthwise direction and at an acute angl...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LIND, DAVID ALBIN, KARANDE, RISHIKESH, BOARDMAN, GREGORY ALLEN, PATRA, AJOY, NAIK, PRADEEP
Format:	Patent
Sprache:	eng ; fre
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!