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    • 2. 发明申请
    • DILUENT SHROUD FOR COMBUSTOR
    • 公司的DILUENT SHROUD
    • US20100101204A1
    • 2010-04-29
    • US12260545
    • 2008-10-29
    • Jonathan Dwight BerryJohn Joseph LipinskiGirard Albert SimonsAbhijit Som
    • Jonathan Dwight BerryJohn Joseph LipinskiGirard Albert SimonsAbhijit Som
    • F02C3/30
    • F23R3/10F23R3/28
    • Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one through baffle hole. At least one diluent shroud is affixed to the at least one baffle plate and is configured to guide a diluent flow toward a mixing chamber of the at least one fuel nozzle. Further disclosed is a method for introducing a diluent flow into a mixing chamber of a fuel nozzle including urging the diluent flow from a plenum through a baffle plate gap between a baffle plate and an outer surface of the fuel nozzle. The diluent flow is directed via at least one diluent shroud extending from the baffle plate toward a plurality of air swirler holes extending through a fuel nozzle tip. The diluent flow is flowed through the plurality of air swirler holes into the mixing chamber.
    • 公开了一种燃烧器,其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个通过挡板孔的燃料喷嘴。 至少一个稀释剂护罩固定在所述至少一个挡板上,并被构造成将稀释剂流引向所述至少一个燃料喷嘴的混合室。 进一步公开的是一种将稀释剂流引入燃料喷嘴的混合室中的方法,包括将稀释剂流从气室推压通过挡板和燃料喷嘴的外表面之间的挡板间隙。 稀释剂流经由从挡板延伸的至少一个稀释剂护罩朝向延伸穿过燃料喷嘴尖端的多个空气旋流器引导。 稀释剂流通过多个空气旋流器孔流入混合室。
    • 3. 发明授权
    • Internal manifold air extraction system for IGCC combustor and method
    • IGCC燃烧器内部歧管空气抽取系统及方法
    • US07921653B2
    • 2011-04-12
    • US11984925
    • 2007-11-26
    • Abhijit SomJonathan Dwight Berry
    • Abhijit SomJonathan Dwight Berry
    • F02C6/06F23R3/26F23R3/46
    • F01D9/023
    • A combustor for a turbine including a combustor liner; a first flow sleeve surrounding the combustor liner with a first flow annulus therebetween, the first flow sleeve having at least one cooling aperture formed about a circumference thereof for directing compressor discharge air as cooling air into the first flow annulus; a casing surrounding first flow sleeve with a second flow annulus therebetween, the first flow sleeve having at least one air extraction opening formed about a circumference thereof for directing compressor discharge air from the first flow annulus as extraction air into the second flow annulus; and an extraction port operatively coupled to the casing for extracting the extraction air from the second flow annulus.
    • 一种用于涡轮机的燃烧器,包括燃烧器衬套; 围绕所述燃烧器衬套的第一流动套筒,其间具有第一流动环空,所述第一流动套筒具有围绕其圆周形成的至少一个冷却孔,用于将压缩机排出的空气作为冷却空气引导到所述第一流动环空中; 围绕其间具有第二流动环的第一流动套管的壳体,所述第一流动套筒具有围绕其周边形成的至少一个空气抽取开口,用于将来自所述第一流动环空间的压缩机排出的空气作为抽出空气引导到所述第二流动环空中; 以及可操作地联接到所述壳体以从所述第二流动环空提取抽取空气的抽出端口。
    • 4. 发明授权
    • Diluent shroud for combustor
    • 用于燃烧器的稀释罩
    • US08454350B2
    • 2013-06-04
    • US12260545
    • 2008-10-29
    • Jonathan Dwight BerryJohn Joseph LipinskiGirard Albert SimonsAbhijit Som
    • Jonathan Dwight BerryJohn Joseph LipinskiGirard Albert SimonsAbhijit Som
    • F23C5/00
    • F23R3/10F23R3/28
    • Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one through baffle hole. At least one diluent shroud is affixed to the at least one baffle plate and is configured to guide a diluent flow toward a mixing chamber of the at least one fuel nozzle. Further disclosed is a method for introducing a diluent flow into a mixing chamber of a fuel nozzle including urging the diluent flow from a plenum through a baffle plate gap between a baffle plate and an outer surface of the fuel nozzle. The diluent flow is directed via at least one diluent shroud extending from the baffle plate toward a plurality of air swirler holes extending through a fuel nozzle tip. The diluent flow is flowed through the plurality of air swirler holes into the mixing chamber.
    • 公开了一种燃烧器,其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个通过挡板孔的燃料喷嘴。 至少一个稀释剂护罩固定在所述至少一个挡板上,并被构造成将稀释剂流引向所述至少一个燃料喷嘴的混合室。 进一步公开的是一种将稀释剂流引入燃料喷嘴的混合室中的方法,包括将稀释剂流从气室推压通过挡板和燃料喷嘴的外表面之间的挡板间隙。 稀释剂流经由从挡板延伸的至少一个稀释剂护罩朝向延伸穿过燃料喷嘴尖端的多个空气旋流器引导。 稀释剂流通过多个空气旋流器孔流入混合室。
    • 5. 发明申请
    • Internal manifold air extraction system for IGCC combustor and method
    • IGCC燃烧器内部歧管空气抽取系统及方法
    • US20090133403A1
    • 2009-05-28
    • US11984925
    • 2007-11-26
    • Abhijit SomJonathan Dwight Berry
    • Abhijit SomJonathan Dwight Berry
    • F23R3/02
    • F01D9/023
    • A combustor for a turbine including a combustor liner; a first flow sleeve surrounding the combustor liner with a first flow annulus therebetween, the first flow sleeve having at least one cooling aperture formed about a circumference thereof for directing compressor discharge air as cooling air into the first flow annulus; a casing surrounding first flow sleeve with a second flow annulus therebetween, the first flow sleeve having at least one air extraction opening formed about a circumference thereof for directing compressor discharge air from the first flow annulus as extraction air into the second flow annulus; and an extraction port operatively coupled to the casing for extracting the extraction air from the second flow annulus.
    • 一种用于涡轮机的燃烧器,包括燃烧器衬套; 围绕所述燃烧器衬套的第一流动套筒,其间具有第一流动环空,所述第一流动套筒具有围绕其圆周形成的至少一个冷却孔,用于将压缩机排出的空气作为冷却空气引导到所述第一流动环空中; 围绕其间具有第二流动环的第一流动套管的壳体,所述第一流动套筒具有围绕其周边形成的至少一个空气抽取开口,用于将来自所述第一流动环空间的压缩机排出的空气作为抽出空气引导到所述第二流动环空中; 以及可操作地联接到所述壳体以从所述第二流动环空提取抽取空气的抽出端口。