APPARATUS FOR ASSEMBLING GAS TURBINE ENGINE COMBUSTORS

A method for assembling a gas turbine engine combustor facilitates reducing costs and time required for assembly. The combustor includes a spectacle plate, a plurality of swirlers, and a plurality of deflector plates. The method includes coupling an assembly fixture to at least one swirler, coupling...

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Bibliographische Detailangaben
Hauptverfasser: KASTRUP DAVID A, FURBISH STEPHEN C
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A method for assembling a gas turbine engine combustor facilitates reducing costs and time required for assembly. The combustor includes a spectacle plate, a plurality of swirlers, and a plurality of deflector plates. The method includes coupling an assembly fixture to at least one swirler, coupling the assembly fixture to the spectacle plate such that the swirler is maintained in alignment with respect to the spectacle plate during assembly of the combustor, and attaching the swirler to the spectacle plate.