Invention Grant
US08820087B2 Method and system for controlling fuel to a dual stage nozzle 有权
用于将燃料控制到双级喷嘴的方法和系统

Method and system for controlling fuel to a dual stage nozzle
Abstract:
A method and system for controlling delivery of fuel to a dual stage nozzle in the combustor of a gas turbine. A liquid fuel is conveyed from a single stage fuel supply through a plurality of primary fuel supply lines to a first nozzle stage including a plurality of primary nozzles. A predetermined operating condition of the gas turbine is identified and a signal is produced in response to the identified operating condition. The signal effects actuation of valves located on secondary fuel supply lines extending from each of the primary fuel supply lines to supply fuel to respective secondary nozzles.
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