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公开(公告)号:US20090158702A1
公开(公告)日:2009-06-25
申请号:US12332520
申请日:2008-12-11
申请人: Giovanni TONNO , Mariateresa PACI , Michele D'ERCOLE , Alessandro RUSSO , Jesse F. STEWART , Ya-Tien CHIU , Marco ULIVI , Antonio BALDASSARRE
发明人: Giovanni TONNO , Mariateresa PACI , Michele D'ERCOLE , Alessandro RUSSO , Jesse F. STEWART , Ya-Tien CHIU , Marco ULIVI , Antonio BALDASSARRE
CPC分类号: F02C9/46 , F02C9/52 , F02C9/54 , F05D2270/091
摘要: A method is described for controlling load variations in a gas turbine. The method comprises reducing the flow of gaseous fuel entering the combustor to a predefined minimum value, if an increase is observed in the rotation regime of said turbine above a predefined maximum value and a total reduction in the load, activating a selective feeding sequence of the burners if the turbine is operating in normal functioning or premixed flame mode, modifying the angulation of the adjustable stator vanes, in order to reduce the speed rate of the compressor, and opening one or more anti-surge valves and one or more overboard bleeds, in order to reduce the air flow at the inlet of the combustor.
摘要翻译: 描述了一种用于控制燃气轮机中的负载变化的方法。 如果在所述涡轮机的旋转状态中观察到的增加高于预定的最大值并且负载的总的减小,则该方法包括将进入燃烧器的气态燃料的流量减少到预定的最小值,激活 燃烧器,如果涡轮机正常运行或预混火焰模式,改变可调节定子叶片的角度,以便降低压缩机的速度,以及打开一个或多个防喘振阀和一个或多个外侧流出物, 以便减少燃烧器入口处的气流。