FUEL NOZZLE AND ASSOCIATED METHOD OF ASSEMBLY

The fuel nozzle (20) can have a proximal member (26) having a first mating portion (36) defined around an assembly axis (28), a first fluid conduit (50) internal to the proximal member (26) and spaced apart from the assembly axis (28), and a first stop (58) facing a first circumferential direction;...

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Bibliographische Detailangaben
1. Verfasser:	SWABY, Nadia
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING BURNERS 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:	The fuel nozzle (20) can have a proximal member (26) having a first mating portion (36) defined around an assembly axis (28), a first fluid conduit (50) internal to the proximal member (26) and spaced apart from the assembly axis (28), and a first stop (58) facing a first circumferential direction; and a distal member (24) having a second mating portion (34) configured for axial engagement with the first mating portion (36) along the assembly axis (28), a second stop (60) facing a second circumferential direction, the second circumferential direction opposite the first circumferential direction and configured to abut against the first stop (58) when the distal member (24) and proximal member (26) are axially engaged to one another in a predetermined relative circumferential alignment.