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    • 1. 发明授权
    • Low NOx combustor for hydrogen-containing fuel and its operation
    • 用于含氢燃料的低NOx燃烧器及其操作
    • US08607572B2
    • 2013-12-17
    • US12857265
    • 2010-08-16
    • Hiromi KoizumiSatoshi DodoHirokazu TakahashiTomohiro AsaiTomomi KoganezawaShohei Yoshida
    • Hiromi KoizumiSatoshi DodoHirokazu TakahashiTomohiro AsaiTomomi KoganezawaShohei Yoshida
    • F02C1/00F02G3/00
    • F23R3/346F23C2900/9901Y02E20/18
    • An object of the present invention is to provide a gas turbine combustor that supports hydrogen-containing gas having a high burning velocity and is capable of performing low NOx combustion without reducing reliability of a burner. A first fuel nozzle is provided upstream of a combustion chamber and supplies fuel for activation and hydrogen-containing gas. The combustor has a primary combustion zone, a reduction zone and a secondary combustion zone. In the primary combustion zone, the fuel supplied from the first fuel nozzle is combusted under a fuel rich condition to form a burned gas containing a low concentration of oxygen. In the reduction zone, a hydrogen-containing gas is injected into the combustion chamber through a second fuel injection hole from a second fuel nozzle so that NOx generated in the primary combustion zone is reduced by an oxygen reaction of the hydrogen. In the secondary combustion zone, air for lean combustion is supplied into the combustion chamber so that unburned part of fuel is combusted under a fuel lean condition.
    • 本发明的目的是提供一种燃气轮机燃烧器,其支撑具有高燃烧速度的含氢气体并且能够进行低NOx燃烧而不降低燃烧器的可靠性。 第一燃料喷嘴设置在燃烧室的上游,并供应用于活化的燃料和含氢气体。 燃烧器具有主燃烧区,还原区和二次燃烧区。 在主燃烧区域中,从第一燃料喷嘴供给的燃料在富燃状态下燃烧,形成含有低浓度氧气的燃烧气体。 在还原区中,通过来自第二燃料喷嘴的第二燃料喷射孔将含氢气体注入燃烧室,使得在一次燃烧区中产生的NOx通过氢的氧反应而被还原。 在二次燃烧区域,用于稀薄燃烧的空气被供应到燃烧室中,使得燃料的未燃烧部分在燃料稀薄状态下燃烧。
    • 2. 发明申请
    • Low NOx Combustor for Hydrogen-Containing Fuel and its Operation
    • 含氢燃料的低NOx燃烧器及其操作
    • US20110094239A1
    • 2011-04-28
    • US12857265
    • 2010-08-16
    • Hiromi KOIZUMISatoshi DodoHirokazu TakahashiTomohiro AsaiTomomi KoganezawaShohei Yoshida
    • Hiromi KOIZUMISatoshi DodoHirokazu TakahashiTomohiro AsaiTomomi KoganezawaShohei Yoshida
    • F02C7/22
    • F23R3/346F23C2900/9901Y02E20/18
    • An object of the present invention is to provide a gas turbine combustor that supports hydrogen-containing gas having a high burning velocity and is capable of performing low NOx combustion without reducing reliability of a burner. A first fuel nozzle is provided upstream of a combustion chamber and supplies fuel for activation and hydrogen-containing gas. The combustor has a primary combustion zone, a reduction zone and a secondary combustion zone. In the primary combustion zone, the fuel supplied from the first fuel nozzle is combusted under a fuel rich condition to form a burned gas containing a low concentration of oxygen. In the reduction zone, a hydrogen-containing gas is injected into the combustion chamber through a second fuel injection hole from a second fuel nozzle so that NOx generated in the primary combustion zone is reduced by an oxygen reaction of the hydrogen. In the secondary combustion zone, air for lean combustion is supplied into the combustion chamber so that unburned part of fuel is combusted under a fuel lean condition.
    • 本发明的目的是提供一种燃气轮机燃烧器,其支撑具有高燃烧速度的含氢气体并且能够进行低NOx燃烧而不降低燃烧器的可靠性。 第一燃料喷嘴设置在燃烧室的上游,并供应用于活化的燃料和含氢气体。 燃烧器具有主燃烧区,还原区和二次燃烧区。 在主燃烧区域中,从第一燃料喷嘴供给的燃料在富燃状态下燃烧,形成含有低浓度氧气的燃烧气体。 在还原区中,通过来自第二燃料喷嘴的第二燃料喷射孔将含氢气体注入燃烧室,使得在一次燃烧区中产生的NOx通过氢的氧反应而被还原。 在二次燃烧区域,用于稀薄燃烧的空气被供应到燃烧室中,使得燃料的未燃烧部分在燃料稀薄状态下燃烧。
    • 3. 发明申请
    • Combustor and Method for Modifying the Same
    • 燃烧器及其修改方法
    • US20100251725A1
    • 2010-10-07
    • US12751503
    • 2010-03-31
    • Satoshi DodoHiromi KoizumiKeisuke MiuraHirokazu Takahashi
    • Satoshi DodoHiromi KoizumiKeisuke MiuraHirokazu Takahashi
    • F02C7/22F02C7/04
    • F23R3/286F23R3/343
    • This invention is intended to maintain combustor reliability.The invention provides a combustor that includes: a fueling nozzle that jets a fuel towards a combustion chamber located downstream; and a flat-plate-shaped air blowhole plate facing the upstream side of the combustion chamber and disposed between the fueling nozzle and the combustion chamber, the air blowhole plate having a plurality of air blowholes arranged at equal intervals in a circumferential direction relative to the center of the air blowhole plate, in order to jet towards the combustion chamber a flow of fuel and a flow of air that is formed at the outer circumferential side of the fuel flow; wherein, in a phase that the fuel flow and the air flow reach an inner wall of the combustion chamber after being jetted from each of a plurality of independently operable burners and from part of the circumferentially arrayed air blowholes, or in a phase that the fuel flow and the air flow interfere with two of the adjacent burners, a spacing between air blowholes that are the part of the circumferentially arrayed air blowholes, is greater than in other phases of the air blowholes.According to the invention, combustor reliability can be maintained.
    • 本发明旨在维持燃烧器的可靠性。 本发明提供了一种燃烧器,其包括:燃料喷嘴,其将燃料喷射到位于下游的燃烧室; 以及面对所述燃烧室的上游侧并且设置在所述加燃料喷嘴和所述燃烧室之间的平板状空气孔板,所述空气孔板具有多个相对于所述燃烧室的圆周方向等间隔排列的空气孔 空气孔板的中心,为了向燃烧室喷射形成在燃料流的外周侧的燃料流和空气流; 其特征在于,在燃料流和空气流从多个可独立操作的燃烧器中的每一个喷射并从周向排列的空气孔的一部分喷射到燃烧室的内壁的阶段中,或者燃料 气流和空气流干扰两个相邻的燃烧器,作为周向排列的空气孔的一部分的空气孔之间的间距大于空气孔的其它阶段。 根据本发明,可以保持燃烧器的可靠性。