DIFFUSER-DESWIRLER FOR A GAS TURBINE ENGINE

A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer...

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Bibliographische Detailangaben
Hauptverfasser: Parker, David Vickery, King, Christopher David, Williams, Megan Lynn, Berhe, Awot Michael, Surprenant, Matthew Brian, Manteiga, John Alan, Ollove, Jesse Jacob
Format: Patent
Sprache:eng
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Zusammenfassung:A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer shell to define a plurality of fluid passageways and a splitter extends along the circumferential direction between adjacent vanes to split the flow of compressed air passing through the each fluid passageway. All of these components are manufactured as a single monolithic piece and are configured for diffusing and deswirling compressor air before passing it to a combustor for an improved combustion process.