초록 ▼

A method for operating a gas turbine engine facilitates reducing an amount of emissions from a combustor. The combustor includes a mixer assembly including a pilot mixer, a main mixer, and a centerbody that extends therebetween. The pilot mixer includes a pilot fuel nozzle and a plurality of axial s

A method for operating a gas turbine engine facilitates reducing an amount of emissions from a combustor. The combustor includes a mixer assembly including a pilot mixer, a main mixer, and a centerbody that extends therebetween. The pilot mixer includes a pilot fuel nozzle and a plurality of axial swirlers. The main mixer includes a main swirler and a plurality of fuel injection ports. The method comprises injecting fuel into the combustor through the pilot mixer, such that the fuel is discharged downstream from the pilot mixer axial swirlers, and directing flow exiting the pilot mixer with a lip extending from the centerbody into a pilot flame zone downstream from said pilot mixer.

대표청구항 ▼

What is claimed is: 1. A method for operating a gas turbine engine to facilitate reducing an amount of emissions from a combustor including a mixer assembly including a pilot mixer, a main mixer, and a centerbody extending therebetween, the pilot mixer including a pilot fuel nozzle and a plurality

What is claimed is: 1. A method for operating a gas turbine engine to facilitate reducing an amount of emissions from a combustor including a mixer assembly including a pilot mixer, a main mixer, and a centerbody extending therebetween, the pilot mixer including a pilot fuel nozzle and a plurality of main swirlers, the main mixer including a main swirler and a plurality of fuel injection ports, said method comprising: injecting fuel into the combustor through the pilot mixer, such that the fuel is discharged downstream from the pilot mixer axial swirlers; and directing flow exiting the pilot mixer with a lip extending from the centerbody into a pilot flame zone downstream from said pilot mixer; wherein the centerbody includes a divergent portion, a radial aft portion, and a lip that projects therebetween, directing flow exiting the pilot mixer further comprises directing flow into the pilot flame zone with the centerbody lip. 2. A method in accordance with claim 1 wherein directing flow into the pilot flame zone with the centerbody lip further comprises directing flow with the lip to facilitate reducing deposit formation along the centerbody radially inner surface. 3. A method in accordance with claim 1 wherein directing flow into the pilot flame zone with the centerbody lip further comprises directing flow with the lip to facilitate isolating flows exiting the pilot mixer from flows exiting the main mixer. 4. A method in accordance with claim 1 wherein directing flow into the pilot flame zone with the centerbody lip further comprises directing flow into the pilot flame zone with a lip including an extension, a corner, and a back approach including a radius. 5. A method in accordance with claim 1 wherein directing flow into the pilot flame zone with the centerbody lip further comprises directing flow with the lip to facilitate preventing fuel from filming against said centerbody inner surface aft portion.