Rich double dome combustor

The present invention relates generally to gas turbine engines, and, more specifically, to combustors therein. A gas turbine engine combustor includes outer and inner liners joined together at an annular dome. Outer and inner air swirlers and cooperating fuel injectors are mounted in two rows in the...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Danis, Allen M, Pritchard, Jr., Byron A, Taylor, Keith K, Stickles, Richard W, Dodds, Willard J, Gardner, Donald L
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!