Invention Grant
US08495881B2 System and method for thermal control in a cap of a gas turbine combustor 有权
在燃气轮机燃烧器的盖中进行热控制的系统和方法

System and method for thermal control in a cap of a gas turbine combustor
Abstract:
A system comprises a turbine combustor cap. The turbine combustor cap includes a plurality of segments. Each segment of the plurality of segments has edges abutting at least two fuel nozzle receptacles. Moreover, each segment of the plurality of segments does not completely surrounding any one fuel nozzle receptacle.
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