Hybrid swirler

The present invention relates generally to gas turbine engines, and, more specifically, to combustors therein. A swirler includes a tubular body having a row of secondary radial swirl vanes. A tubular ferrule adjoins the body at the secondary vanes, and includes a row of primary swirl vanes. The pri...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Al-Roub, Marwan, Seto, Stanford P, Staker, John Robert, Tu, Ting-Yu
Format: Patent
Sprache:eng
Online-Zugang:Volltext bestellen
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