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公开(公告)号：US20100000218A1
公开(公告)日：2010-01-07
申请号：US12498882
申请日：2009-07-07
申请人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
发明人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
IPC分类号： F02C7/22
摘要： A gas turbine combustor for mixing fuel into combustion air introduced from a compressor, burning an air-fuel mixture, and supplying produced combustion gas to a gas turbine. The combustor has a liquid fuel nozzle for jetting out liquid fuel and a pre-mixture chamber wall having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out from the liquid fuel nozzle, and defining a pre-mixture chamber therein. A plurality of gaseous fuel nozzles are disposed around the pre-mixture chamber wall in an opposing relation respectively to a plurality of air inlet holes bored through the pre-mixture chamber wall and jet out gaseous fuel substantially coaxially with the axes of the air inlet holes.
摘要翻译： 一种燃气轮机燃烧器，用于将燃料混合到从压缩机引入的燃烧空气中，燃烧空气 - 燃料混合物，并向燃气轮机供应生成的燃烧气体。 燃烧器具有用于喷出液体燃料的液体燃料喷嘴和具有中空圆锥形状的预混合室壁，该中空圆锥形状沿着从燃料喷嘴喷出的方向逐渐扩散，并且在其中限定预混合室 。 多个气体燃料喷嘴分别设置在预混合室壁周围，分别与穿过预混合室壁的多个空气入口孔相对设置，并且喷出大致与进气孔的轴线同轴的气态燃料 。
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公开(公告)号：US20080190113A1
公开(公告)日：2008-08-14
申请号：US12078218
申请日：2008-03-28
申请人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
发明人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
IPC分类号： F02C1/00
摘要： A gas turbine combustor includes a liquid fuel nozzle for jetting out liquid fuel; a pre-mixture chamber wall provided with the liquid fuel nozzle at a center thereof having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out, and defining a pre-mixture chamber therein; a plurality of air inlet holes bored through the pre-mixture chamber wall and introducing the combustion air to the pre-mixture chamber such that angles at which the combustion air is introduced to the pre-mixture chamber through the air inlet holes are deflected at least toward the circumferential direction of the pre-mixture chamber wall; and a plurality of gaseous fuel nozzles disposed around the pre-mixture chamber wall in an opposing relation respectively to the plurality of air inlet holes and jetting out gaseous fuel substantially coaxially with axes of the air inlet holes.
摘要翻译： 燃气轮机燃烧器包括用于喷出液体燃料的液体燃料喷嘴; 预混合室壁，在其中心处设置有液体燃料喷嘴，其具有在喷射燃料的方向上逐渐扩散的中空圆锥形状，并且在其中限定预混合室; 多个空气入口孔，穿过预混合室壁并将燃烧空气引入预混合室，使得燃烧空气通过进气孔引入预混合室的角度至少偏转 朝向预混合室壁的圆周方向; 以及多个气体燃料喷嘴，分别围绕所述预混合室壁以相对的关系设置在所述多个空气入口孔中，并且与所述空气入口孔的轴线大致同轴地喷出气态燃料。
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公开(公告)号：US20080190112A1
公开(公告)日：2008-08-14
申请号：US12078216
申请日：2008-03-28
申请人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
发明人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
IPC分类号： F02C1/00
摘要： A gas turbine combustor includes a liquid fuel nozzle for jetting out liquid fuel; a pre-mixture chamber wall provided with the liquid fuel nozzle at a center thereof, having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out, and defining a pre-mixture chamber therein; a plurality of air inlet holes bored through the pre-mixture chamber wall and introducing the combustion air to the pre-mixture chamber such that angles at which the combustion air is introduced to the pre-mixture chamber through the air inlet holes are deflected at least toward the circumferential direction of the pre-mixture chamber wall; and a plurality of gaseous fuel nozzles disposed around the pre-mixture chamber wall in an opposing relation respectively to the plurality of air inlet holes and jetting out gaseous fuel substantially coaxially with axes of the air inlet holes.
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公开(公告)号：US07571612B2
公开(公告)日：2009-08-11
申请号：US12078216
申请日：2008-03-28
申请人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
发明人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
摘要： A gas turbine combustor includes a liquid fuel nozzle for jetting out liquid fuel; a pre-mixture chamber wall provided with the liquid fuel nozzle at a center thereof, having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out, and defining a pre-mixture chamber therein; a plurality of air inlet holes bored through the pre-mixture chamber wall and introducing the combustion air to the pre-mixture chamber such that angles at which the combustion air is introduced to the pre-mixture chamber through the air inlet holes are deflected at least toward the circumferential direction of the pre-mixture chamber wall; and a plurality of gaseous fuel nozzles disposed around the pre-mixture chamber wall in an opposing relation respectively to the plurality of air inlet holes and jetting out gaseous fuel substantially coaxially with axes of the air inlet holes.
摘要翻译： 燃气轮机燃烧器包括用于喷出液体燃料的液体燃料喷嘴; 在其中心设置有液体燃料喷嘴的预混合室壁，其具有沿着喷射燃料的方向逐渐扩展的中空圆锥形状，并且在其中限定预混合室; 多个空气入口孔，穿过预混合室壁并将燃烧空气引入预混合室，使得燃烧空气通过进气孔引入预混合室的角度至少偏转 朝向预混合室壁的圆周方向; 以及多个气体燃料喷嘴，分别围绕所述预混合室壁以相对的关系设置在所述多个空气入口孔中，并且与所述空气入口孔的轴线大致同轴地喷出气态燃料。
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公开(公告)号：US07426833B2
公开(公告)日：2008-09-23
申请号：US10868805
申请日：2004-06-17
申请人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
发明人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
摘要： A gas turbine combustor includes a liquid fuel nozzle for jetting out liquid fuel; a pre-mixture chamber wall provided with the liquid fuel nozzle at a center thereof, having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out, and defining a pre-mixture chamber therein; a plurality of air inlet holes bored through the pre-mixture chamber wall and introducing the combustion air to the pre-mixture chamber such that angles at which the combustion air is introduced to the pre-mixture chamber through the air inlet holes are deflected at least toward the circumferential direction of the pre-mixture chamber wall; and a plurality of gaseous fuel nozzles disposed around the pre-mixture chamber wall in an opposing relation respectively to the plurality of air inlet holes and jetting out gaseous fuel substantially coaxially with axes of the air inlet holes.
摘要翻译： 燃气轮机燃烧器包括用于喷出液体燃料的液体燃料喷嘴; 在其中心设置有液体燃料喷嘴的预混合室壁，其具有沿着喷射燃料的方向逐渐扩展的中空圆锥形状，并且在其中限定预混合室; 多个空气入口孔，穿过预混合室壁并将燃烧空气引入预混合室，使得燃烧空气通过进气孔引入预混合室的角度至少偏转 朝向预混合室壁的圆周方向; 以及多个气体燃料喷嘴，分别围绕所述预混合室壁以相对的关系设置在所述多个空气入口孔中，并且与所述空气入口孔的轴线大致同轴地喷出气态燃料。
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公开(公告)号：US20080209909A1
公开(公告)日：2008-09-04
申请号：US12078217
申请日：2008-03-28
申请人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
发明人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
IPC分类号： F02C1/00
摘要： A gas turbine combustor includes a liquid fuel nozzle for jetting out liquid fuel, a pre-mixture chamber wall provided with the liquid fuel nozzle at a center thereof, having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out and defining a pre-mixture chamber therein; a plurality of air inlet holes bored through the pre-mixture chamber wall and introducing the combustion air to the pre-mixture chamber such that angles at which the combustion air is introduced to the pre-mixture chamber through the air inlet holes are deflected at least toward the circumferential direction of the pre-mixture chamber wall; and a plurality of gaseous fuel nozzles disposed around the pre-mixture chamber wall in an opposing relation respectively to the plurality of air inlet holes and jetting out gaseous fuel substantially coaxially with axes of the air inlet holes.
摘要翻译： 燃气轮机燃烧器包括用于喷出液体燃料的液体燃料喷嘴，在其中心设置有液体燃料喷嘴的预混合室壁，其具有沿喷射燃料的方向逐渐扩展的中空圆锥形状，以及 在其中限定预混合室; 多个空气入口孔，穿过预混合室壁并将燃烧空气引入预混合室，使得燃烧空气通过进气孔引入预混合室的角度至少偏转 朝向预混合室壁的圆周方向; 以及多个气体燃料喷嘴，分别围绕所述预混合室壁以相对的关系设置在所述多个空气入口孔中，并且与所述空气入口孔的轴线大致同轴地喷出气态燃料。
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公开(公告)号：US08393159B2
公开(公告)日：2013-03-12
申请号：US12498882
申请日：2009-07-07
申请人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
发明人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
摘要： A gas turbine combustor for mixing fuel into combustion air introduced from a compressor, burning an air-fuel mixture, and supplying produced combustion gas to a gas turbine. The combustor has a liquid fuel nozzle for jetting out liquid fuel and a pre-mixture chamber wall having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out from the liquid fuel nozzle, and defining a pre-mixture chamber therein. A plurality of gaseous fuel nozzles are disposed around the pre-mixture chamber wall in an opposing relation respectively to a plurality of air inlet holes bored through the pre-mixture chamber wall and jet out gaseous fuel substantially coaxially with the axes of the air inlet holes.
摘要翻译： 一种燃气轮机燃烧器，用于将燃料混合到从压缩机引入的燃烧空气中，燃烧空气 - 燃料混合物，并向燃气轮机供应生成的燃烧气体。 燃烧器具有用于喷出液体燃料的液体燃料喷嘴和具有中空圆锥形状的预混合室壁，该中空圆锥形状沿着从燃料喷嘴喷出的方向逐渐扩散，并且在其中限定预混合室 。 多个气体燃料喷嘴分别设置在预混合室壁周围，分别与穿过预混合室壁的多个空气入口孔相对设置，并且喷出大致与进气孔的轴线同轴的气态燃料 。
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公开(公告)号：US07673455B2
公开(公告)日：2010-03-09
申请号：US12078217
申请日：2008-03-28
申请人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
发明人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
摘要： A gas turbine combustor includes a liquid fuel nozzle for jetting out liquid fuel; a pre-mixture chamber wall provided with the liquid fuel nozzle at a center thereof, having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out, and defining a pre-mixture chamber therein; a plurality of air inlet holes bored through the pre-mixture chamber wall and introducing the combustion air to the pre-mixture chamber such that angles at which the combustion air is introduced to the pre-mixture chamber through the air inlet holes are deflected at least toward the circumferential direction of the pre-mixture chamber wall; and a plurality of gaseous fuel nozzles disposed around the pre-mixture chamber wall in an opposing relation respectively to the plurality of air inlet holes and jetting out gaseous fuel substantially coaxially with axes of the air inlet holes.
摘要翻译： 燃气轮机燃烧器包括用于喷出液体燃料的液体燃料喷嘴; 在其中心设置有液体燃料喷嘴的预混合室壁，其具有沿着喷射燃料的方向逐渐扩展的中空圆锥形状，并且在其中限定预混合室; 多个空气入口孔，穿过预混合室壁并将燃烧空气引入预混合室，使得燃烧空气通过进气孔引入预混合室的角度至少偏转 朝向预混合室壁的圆周方向; 以及多个气体燃料喷嘴，分别围绕所述预混合室壁以相对的关系设置在所述多个空气入口孔中，并且与所述空气入口孔的轴线大致同轴地喷出气态燃料。
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公开(公告)号：US07571609B2
公开(公告)日：2009-08-11
申请号：US12078218
申请日：2008-03-28
申请人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
发明人： Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
摘要： A gas turbine combustor includes a liquid fuel nozzle for jetting out liquid fuel; a pre-mixture chamber wall provided with the liquid fuel nozzle at a center thereof, having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out, and defining a pre-mixture chamber therein; a plurality of air inlet holes bored through the pre-mixture chamber wall and introducing the combustion air to the pre-mixture chamber such that angles at which the combustion air is introduced to the pre-mixture chamber through the air inlet holes are deflected at least toward the circumferential direction of the pre-mixture chamber wall; and a plurality of gaseous fuel nozzles disposed around the pre-mixture chamber wall in an opposing relation respectively to the plurality of air inlet holes and jetting out gaseous fuel substantially coaxially with axes of the air inlet holes.
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10.发明授权Gas turbine combustor and gaseous fuel supply method for gas turbine combustor 有权燃气轮机燃烧器的燃气轮机和气体燃料供给方法公开(公告)号：US08261529B2
公开(公告)日：2012-09-11
申请号：US12370236
申请日：2009-02-12
IPC分类号： F02C3/20
CPC分类号： F23R3/36 , F02C3/22 , F02C7/222 , F02C7/232 , F05D2220/75 , F23R2900/00002
摘要： A combustor includes two upstream parts of fuel supply system supplying gaseous fuels of two types having different heating values from each other, a three-way fuel transfer valve merging the two upstream parts of fuel supply system with each other, a plurality of gaseous fuel supply subsystems supplying a combustion chamber with the gaseous fuels supplied through the three-way fuel transfer valve and branched, and a plurality of burners injecting, corresponding to each of the gaseous fuel supply subsystems, the gaseous fuel supplied from the gaseous fuel supply subsystem into the combustion chamber.
摘要翻译： 燃烧器包括燃料供给系统的两个上游部分，其供应彼此具有不同热值的两种类型的气体燃料，三通燃料转换阀将燃料供应系统的两个上游部分彼此合并，多个气体燃料供应 向燃烧室提供通过三通燃料转移阀供应并分支的气体燃料的子系统;以及多个燃烧器，其将对应于每个气体燃料供应子系统的气态燃料喷射到从气态燃料供应子系统供给的气体燃料到 燃烧室。
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