Fuel nozzle assembly for a gas turbine engine
A technology of fuel nozzles and gas turbines, which is applied to engine components, turbine/propulsion fuel delivery systems, machines/engines, etc., and can solve problems such as low cycle, high cycle fatigue, and fuel hole structure rupture
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[0083] figure 1is a schematic diagram of an exemplary gas turbine engine 100 . In the exemplary embodiment, engine 100 includes compressor 102 and combustor 104 . Combustor 104 includes a combustion zone 105 and a fuel nozzle assembly 106 . Engine 100 also includes turbine 108 and common compressor / turbine shaft 110 (sometimes referred to as rotor 110 ). Compressor 102 is also rotatably coupled to rotor 110 . In the exemplary embodiment, there are multiple combustors 104 and fuel nozzle assemblies 106 . In the following discussion, only one of the components will be discussed unless otherwise indicated. In one embodiment, gas turbine engine 100 is a PG93719FBA heavy-duty gas turbine engine commercially available from General Electric Company of Greenville, Southern California. It is worth noting that the present invention is not limited to any one particular engine, and that the present invention may be used in conjunction with other gas turbine engines, such as, for exam...
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