Multiple Zone Pilot For Low Emission Combustion System
AssigneeGeneral Electric Company
InventorsAbdul Rafey Khan, Thomas Edward Johnson
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AssigneeGeneral Electric Company
InventorsAbdul Rafey Khan, Thomas Edward Johnson
Estimating the term…
A method of operating a combustor includes delivering a primary fuel flow through a plurality of primary fuel nozzles toward a primary combustion zone and combusting the primary fuel flow in the primary combustion zone. A secondary fuel flow is delivered through a secondary fuel nozzle toward a secondary combustion zone and combusted therein. The secondary fuel is located such that the plurality of primary fuel nozzles are arrayed around the secondary fuel nozzle. An outer swirler is located between the plurality of primary fuel nozzles and the secondary fuel nozzle and includes a plurality of outer swirler channels extending therethrough. A flow of swirler fuel is delivered through the plurality of outer swirler channels into the combustor substantially between the primary combustion zone and the secondary combustion zone to stabilize combustion in the primary combustion zone and/or the secondary combustion zone.
A combustor for a turbomachine comprising:
A method of operating a combustor comprising:
Dependencies are inferred from the claim text.