BUNDLED TUBE FUEL NOZZLE ASSEMBLY FOR GAS TURBINE COMBUSTOR

A bundled tube fuel nozzle assembly for a gas turbine combustor includes: a forward plate facing a head end air plenum, an aft plate facing a combustion chamber, and premixing tubes extending from the forward plate to the aft plate. An interior side wall extends circumferentially around the first pl...

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Bibliographische Detailangaben

Hauptverfasser:	McConnaughhay, Johnie Franklin, Berry, Jonathan Dwight, Chila, Ronald James, Hughes, Michael John, Ostebee, Heath Michael
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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