COMBUSTOR
    1.
    发明申请

    公开(公告)号:US20110076628A1

    公开(公告)日:2011-03-31

    申请号:US12893879

    申请日:2010-09-29

    IPC分类号: F23N1/02 F23D14/62

    摘要: This invention is directed to supply a combustor having a structure that reduces NOx emissions while maintaining combustion stability. The combustor has a chamber into which fuel and air are supplied. An air hole plate having a plurality of air holes upstream of the chamber is also disclosed, and fuel nozzles supplying fuel to the air holes of the air hole plate are further disclosed. In the combustor, a center of a chamber-side of the air hole plate is closer to the chamber than exits of outermost peripheral air holes.

    摘要翻译: 本发明旨在提供具有减少NOx排放的结构的燃烧器,同时保持燃烧稳定性。 燃烧器具有供应燃料和空气的室。 还公开了一种在腔室上游具有多个气孔的气孔板,并且还公开了向空气孔板的气孔供给燃料的燃料喷嘴。 在燃烧器中,气孔板的室侧的中心比最外周气孔的出口更靠近室。

    Combustor and operating method thereof
    2.
    发明授权
    Combustor and operating method thereof 有权
    燃烧器及其操作方法

    公开(公告)号:US09074772B2

    公开(公告)日:2015-07-07

    申请号:US12893879

    申请日:2010-09-29

    摘要: This invention is directed to supply a combustor having a structure that reduces NOx emissions while maintaining combustion stability. The combustor has a chamber into which fuel and air are supplied. An air hole plate having a plurality of air holes upstream of the chamber is also disclosed, and fuel nozzles supplying fuel to the air holes of the air hole plate are further disclosed. In the combustor, a center of a chamber-side of the air hole plate is closer to the chamber than exits of outermost peripheral air holes.

    摘要翻译: 本发明旨在提供具有减少NOx排放的结构的燃烧器,同时保持燃烧稳定性。 燃烧器具有供应燃料和空气的室。 还公开了一种在腔室上游具有多个气孔的气孔板,并且还公开了向空气孔板的气孔供给燃料的燃料喷嘴。 在燃烧器中,气孔板的室侧的中心比最外周气孔的出口更靠近室。

    Combustor and the method of fuel supply and converting fuel nozzle for advanced humid air turbine
    3.
    发明授权
    Combustor and the method of fuel supply and converting fuel nozzle for advanced humid air turbine 有权
    燃烧器和燃料供应和转换燃料喷嘴用于先进湿润空气涡轮机的方法

    公开(公告)号:US09334808B2

    公开(公告)日:2016-05-10

    申请号:US13197953

    申请日:2011-08-04

    摘要: A fuel control device and method of a gas turbine combustor, for advanced humid air turbines, in which plural combustion units comprising plural fuel nozzles for supplying fuel and plural air nozzles for supplying air for combustion are provided. A part of the plural combustion units are more excellent in flame stabilizing performance than the other combustion units. A fuel ratio, at which fuel is fed to the part of the combustion units is set on the basis of internal temperature of the humidification tower and internal pressure of the humidification tower to control a flow ratio of the fuel fed to the plural combustion units.

    摘要翻译: 提供一种用于先进湿式空气涡轮机的燃气轮机燃烧器的燃料控制装置和方法,其中包括用于供应燃料的多个燃料喷嘴和用于供给燃烧空气的多个空气喷嘴的多个燃烧单元。 多个燃烧单元的一部分在火焰稳定性方面优于其它燃烧单元。 基于加湿塔的内部温度和加湿塔的内部压力来设定向燃烧单元的一部分供给燃料的燃料比,以控制供给到多个燃烧单元的燃料的流量比。