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System and method for diffusion combustion with fuel-diluent mixing in a stoichiometric exhaust gas recirculation gas turbine system

机译:在化学计量的废气再循环燃气轮机系统中利用燃料-稀释剂混合进行扩散燃烧的系统和方法

摘要

A system is provided with a turbine combustor having a first diffusion fuel nozzle (554), wherein the first diffusion fuel nozzle has first (722) and second passages (724) that separately inject respective first and second flows into a chamber (494) of the turbine combustor to produce a diffusion flame. The first flow includes a first fuel and a first diluent, and the second flow includes a first oxidant. The system includes a turbine driven by combustion products from the diffusion flame in the turbine combustor. The system also includes an exhaust gas compressor, wherein the exhaust gas compressor is configured to compress and route an exhaust gas from the turbine to the turbine combustor along an exhaust recirculation path.
机译:一种系统,其具有具有第一扩散燃料喷嘴(554)的涡轮燃烧器,其中,第一扩散燃料喷嘴具有第一通道(722)和第二通道(724),所述第一通道和第二通道分别将各自的第一和第二流注入到腔室(494)中。涡轮燃烧器产生扩散火焰。第一流包括第一燃料和第一稀释剂,第二流包括第一氧化剂。该系统包括由来自涡轮机燃烧器中的扩散火焰的燃烧产物驱动的涡轮机。该系统还包括排气压缩机,其中,排气压缩机被构造成沿着排气再循环路径压缩排气并将其从涡轮机引导至涡轮机燃烧器。

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