FUEL NOZZLE TIP ASSEMBLY

PROBLEM TO BE SOLVED: To provide a fuel nozzle tip assembly, with respect to a system and a constitution for a fuel nozzle of a gas turbine engine. SOLUTION: In one embodiment, this system includes a fuel nozzle tip retainer, and the fuel nozzle tip retainer includes structural members 62, 66, 84 ha...

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Bibliographische Detailangaben
Hauptverfasser:	BAILEY DONALD MARK, SCOTT R SIMMONS
Format:	Patent
Sprache:	eng
Schlagworte:	AIR AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a fuel nozzle tip assembly, with respect to a system and a constitution for a fuel nozzle of a gas turbine engine. SOLUTION: In one embodiment, this system includes a fuel nozzle tip retainer, and the fuel nozzle tip retainer includes structural members 62, 66, 84 having geometries 67, 88 for preventing movement of a tip insert 64 in the axial downstream direction of a fuel nozzle 12. COPYRIGHT: (C)2010,JPO&INPIT