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Gas turbine burning a gaseous fuel with the emissions of nitrogen oxides reduced.

机译:燃气轮机燃烧减少了氮氧化物排放的气体燃料。

摘要

Gas turbine including a gas circuit (1) terminated by gas burners (3) and supplied with gaseous fuel and a liquid fuel circuit (5) including a flow splitter (8) supplying the fuel injectors (9), the gas burners (3) and the fuel injectors (9) being located in compound combustion chambers (4), characterised in that the fuel circuit (5) is fed upstream of the flow splitter (8) with a water-based liquid which does not attack metals. By virtue of this very simple assembly the emissions of NOx can be greatly decreased. IMAGE
机译:燃气轮机,其包括由燃气燃烧器(3)终止并供应有气态燃料的燃气回路(1)和包括向燃料喷射器(9)提供分流器(8)的液体燃料回路(5),燃气燃烧器(3)燃料喷射器(9)位于复合燃烧室(4)中,其特征在于,在分流器(8)的上游向燃料回路(5)供给不会侵蚀金属的水基液体。通过这种非常简单的组装,可以大大减少NOx的排放。 <图像>

著录项

  • 公开/公告号FR2682161B1

    专利类型

  • 公开/公告日1995-03-31

    原文格式PDF

  • 申请/专利权人 EUROP GAS TURBINES SA;

    申请/专利号FR19910012311

  • 发明设计人 MICHEL MOLIERE;MAURICE COLAS;

    申请日1991-10-07

  • 分类号F02C3/30;F02C7/22;

  • 国家 FR

  • 入库时间 2022-08-22 04:07:17

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