Methods and apparatus for fabricating gas turbine engine combustors

A method facilitates fabricating a gas turbine engine combustor. The method comprises coupling a venturi to a primary swirler, and coupling the venturi to a secondary swirler such that a gap is defined between a portion of the venturi and a portion of one of the primary swirler and the secondary swi...

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Bibliographische Detailangaben
Hauptverfasser: COOPER JAMES N, HELD TIMOTHY J, MARTINI JEFFREY M, KASTRUP DAVID A, DE VANE SHAUN M, FORTUNA DOUGLAS M
Format: Patent
Sprache:eng
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Zusammenfassung:A method facilitates fabricating a gas turbine engine combustor. The method comprises coupling a venturi to a primary swirler, and coupling the venturi to a secondary swirler such that a gap is defined between a portion of the venturi and a portion of one of the primary swirler and the secondary swirler.