System comprising a sector nozzle for a gas turbine

Systems are provided for mounting sector nozzles (34) within gas turbine combustors (12). In one embodiment, a sector nozzle (34) includes a nozzle portion (48) configured to mix fuel and air to produce a fuel-air mixture and a shell (56) coupled to the nozzle portion (48). The sector nozzle (34) al...

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Bibliographische Detailangaben
Hauptverfasser:	Berry, Jonathan Dwight, Simons, Derrick Walter, Stewart, Jason Thurman
Format:	Patent
Sprache:	eng ; fre ; ger
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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Beschreibung
Zusammenfassung:	Systems are provided for mounting sector nozzles (34) within gas turbine combustors (12). In one embodiment, a sector nozzle (34) includes a nozzle portion (48) configured to mix fuel and air to produce a fuel-air mixture and a shell (56) coupled to the nozzle portion (48). The sector nozzle (34) also includes a first longitudinal strut (60) and a second longitudinal strut (60) coupled to a first surface (78) of the shell (56) on opposite sides of a window (67) within the first surface (78). A third longitudinal strut (62) is coupled to a second surface (84) of the shell, and the second surface (84) is disposed opposite of the first surface (78).