首页> 外国专利> METHOD FOR OPERATING A GAS TURBINE WITH SEQUENTIAL COMBUSTION AND A GAS TURBINE FOR THE PERFORMANCE OF THE SPECIFIED METHOD

METHOD FOR OPERATING A GAS TURBINE WITH SEQUENTIAL COMBUSTION AND A GAS TURBINE FOR THE PERFORMANCE OF THE SPECIFIED METHOD

机译:顺序燃烧操作燃气轮机的方法和性能指定方法的燃气轮机

摘要

1. The method of operation of a gas turbine (10) with sequential combustion (14, 15, 17, 19), while the gas turbine (10) contains a compressor (13), a first combustion chamber (14, 17) with the first chamber (14) combustion and the first burners (17), which receives compressed air from the compressor (13), the second combustion chamber (15, 19) proper with the second combustion chamber (15) and the second burners (19), which receives hot gas from the first chamber (14) , 17) a combustion with a predetermined temperature (T) at the inlet of the second combustion chamber, and a turbine (16) that receives hot gas from the second chamber (15, 19) of combustion, characterized in that the temperature (T) at the inlet of the second combustion chamber is lowered to operate the gas turbine (10) with the base load, and the temperature (T) at the inlet of the second combustion chamber is increased with decreasing load (RL) by gas turbine from base load to partial load. 2. A method according to claim 1, characterized in that diluting air is mixed with hot gases from the first combustion chamber (14, 17) to achieve a reduced temperature (T) at the inlet of the second combustion chamber. The method according to claim 2, characterized in that the mass flow rate of the dilution air is changed to achieve large changes in temperature (T) at the inlet of the second combustion chamber. The method according to claim 1, characterized in that the temperature at the outlet of the first combustion chamber (14, 17) or the temperature (T) at the inlet of the second combustion chamber, respectively, is controlled depending on the load (LS) on the gas turbine. The method according to claim 1, characterized in that the temperature at the outlet of the first combustion chamber (14, 17) or the temperature (T) at the inlet of the second combustion chamber, respectively, is controlled depending on the combustion pressure, in particular in
机译:1.具有顺序燃烧(14、15、17、19)的燃气轮机(10)的运行方法,而燃气轮机(10)包括压缩机(13),具有第一燃烧室(14、17)的第一燃烧室(14)。第一燃烧室(14)和第一燃烧器(17)从压缩机(13)接收压缩空气,第二燃烧室(15、19)和第二燃烧室(15)和第二燃烧器(19) )从第一室(14)接收热气,)在第二燃烧室的入口处以预定温度(T)燃烧,涡轮(16)从第二室(15)接收热气,(19)的燃烧,其特征在于,降低第二燃烧室的入口处的温度(T)以使燃气轮机(10)以基本负荷运转,并且降低第二燃烧室的入口处的温度(T)。随着燃气轮机的负荷(RL)从基本负荷降低到部分负荷,燃烧室会增加。 2.根据权利要求1所述的方法,其特征在于,将稀释空气与来自所述第一燃烧室(14、17)的热气体混合,以在所述第二燃烧室的入口处实现降低的温度(T)。 3.根据权利要求2所述的方法,其特征在于,改变所述稀释空气的质量流量以在所述第二燃烧室的入口处实现大的温度(T)变化。 2.根据权利要求1所述的方法,其特征在于,根据负荷(LS)分别控制第一燃烧室(14、17)出口处的温度或第二燃烧室入口处的温度(T)。 )在燃气轮机上。 2.根据权利要求1所述的方法,其特征在于,根据燃烧压力分别控制第一燃烧室(14、17)出口处的温度或第二燃烧室入口处的温度(T),特别是在

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号