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A turbomachine includes a compressor, a turbine operatively connected to the compressor, and a combustion assembly fluidly connected between the compressor and the turbine. The combustion assembly includes an end cover including a plurality of fuel circuits, a fuel distributing flange fluidly connec

A turbomachine includes a compressor, a turbine operatively connected to the compressor, and a combustion assembly fluidly connected between the compressor and the turbine. The combustion assembly includes an end cover including a plurality of fuel circuits, a fuel distributing flange fluidly connected to at least one of the plurality of fuel circuits, a nozzle assembly fluidly linked to the at least one of the plurality of fuel circuits, and a fuel distribution system configured and disposed to deliver fuel to the fuel distributing flange. The fuel distribution system is selectively activated to stage fuel delivery to the at least one of the plurality of fuel circuits at a pressure sufficient to achieve atomization at the nozzle assembly without requiring a supplemental atomization air flow prior to delivering fuel to others of the plurality of fuel circuits at a pressure to achieve atomization without requiring a supplemental atomization air flow.

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1. A turbomachine comprising: a compressor;a turbine operatively connected to the compressor;a combustion assembly fluidly connected between the compressor and the turbine, the combustion assembly including: a combustor end cover including a plurality of fuel circuits;a fuel distributing flange moun

1. A turbomachine comprising: a compressor;a turbine operatively connected to the compressor;a combustion assembly fluidly connected between the compressor and the turbine, the combustion assembly including: a combustor end cover including a plurality of fuel circuits;a fuel distributing flange mounted to an outer surface of the combustor endcover and fluidly connected to at least one of the plurality of fuel circuits;a nozzle assembly fluidly linked to the at least one of the plurality of fuel circuits;another fuel distributing flange fluidly connected to at least one other of the plurality of fuel circuits;another nozzle assembly fluidly connected to the at least one other of the plurality of fuel circuits; anda fuel distribution system configured and disposed to deliver fuel to the fuel distributing flange, the fuel distribution system being selectively activated to stage fuel delivery to the at least one of the plurality of fuel circuits at a pressure sufficient to achieve atomization without requiring a supplemental atomization air flow at the nozzle assembly prior to delivering fuel to others of the plurality of fuel circuits at a pressure sufficient to achieve atomization without requiring a supplemental atomization air flow at the nozzle. 2. The turbomachine according to claim 1, wherein the fuel distributing system is configured and disposed to direct fuel to the at least one other of the plurality of fuel circuits only when fuel pressure is sufficient to achieve atomization at the another nozzle without requiring a supplemental atomization air flow. 3. The turbomachine according to claim 2, wherein the endcover includes at least five fuel circuits, each of the at least five fuel circuits being fluidly connected to an associated nozzle assembly. 4. The turbomachine according to claim 3, wherein the fuel distributing flange is connected to one of the at least five fuel circuits. 5. The turbomachine according to claim 3, wherein the fuel distributing flange is connected to only two of the plurality of fuel circuits. 6. The turbomachine according to claim 2, wherein the fuel delivery system is configured and disposed to stage delivery of liquid fuel to each of the fuel distributing flange and the another fuel distributing flange. 7. The turbomachine according to claim 6, wherein the fuel delivery system passes fuel to the another fuel distributing flange only after fuel flow at the fuel distributing flange is above at least one lbs/sec (0.45 kg/sec). 8. The turbomachine according to claim 6, wherein the fuel delivery system passes fuel to the another fuel distributing flange only after fuel flow at the fuel distributing flange is between at least one lbs/sec (0.45 kg/sec) and about 2 lbs/sec (0.907 kg/sec). 9. A turbomachine comprising: a compressor;a turbine operatively connected to the compressor;a combustion assembly fluidly connected between the compressor and the turbine, the combustion assembly including: a combustor end cover including a plurality of fuel circuits;a fuel distributing flange mounted to an outer surface of the combustor endcover and fluidly connected to at least one of the plurality of fuel circuits;a nozzle assembly fluidly linked to the at least one of the plurality of fuel circuits;another fuel distributing flange fluidly connected to at least one other of the plurality of fuel circuits;another nozzle assembly fluidly connected to the at least one other of the plurality of fuel circuits; anda fuel distribution system configured and disposed to deliver fuel to the fuel distributing flange, the fuel distribution system being selectively activated to stage fuel delivery to the at least one of the plurality of fuel circuits prior to delivering fuel to others of the plurality of fuel circuits. 10. The turbomachine according to claim 9, wherein wherein the fuel distributing system is configured and disposed to direct fuel to the at least one other of the plurality of fuel circuits only when fuel pressure is sufficient to achieve atomization at the another nozzle without requiring a supplemental atomization air flow. 11. The turbomachine according to claim 10, wherein the endcover includes at least five fuel circuits, each of the at least five fuel circuits being fluidly connected to an associated nozzle assembly. 12. The turbomachine according to claim 11, wherein the fuel distributing flange is connected to one of the at least five fuel circuits. 13. The turbomachine according to claim 11, wherein the fuel distributing flange is connected to only two of the plurality of fuel circuits. 14. The turbomachine according to claim 10, wherein the fuel delivery system is configured and disposed to stage delivery of liquid fuel to each of the fuel distributing flange and the another fuel distributing flange.