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1. 发明授权

US08607572B2 Low NOx combustor for hydrogen-containing fuel and its operation 有权
标题翻译：用于含氢燃料的低NOx燃烧器及其操作
公开(公告)号：US08607572B2
公开(公告)日：2013-12-17
申请号：US12857265
申请日：2010-08-16
申请人： Hiromi Koizumi , Satoshi Dodo , Hirokazu Takahashi , Tomohiro Asai , Tomomi Koganezawa , Shohei Yoshida
发明人： Hiromi Koizumi , Satoshi Dodo , Hirokazu Takahashi , Tomohiro Asai , Tomomi Koganezawa , Shohei Yoshida
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/346 , F23C2900/9901 , Y02E20/18
摘要： 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.
摘要翻译：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. 发明授权

US08261529B2 Gas turbine combustor and gaseous fuel supply method for gas turbine combustor 有权
标题翻译：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
申请人： Hiromi Koizumi , Tomohiro Asai , Hiroshi Inoue , Tsunemasa Nishijima , Hidetaro Murata
发明人： Hiromi Koizumi , Tomohiro Asai , Hiroshi Inoue , Tsunemasa Nishijima , Hidetaro Murata
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。

3. 发明申请

US20110094239A1 Low NOx Combustor for Hydrogen-Containing Fuel and its Operation 有权
标题翻译：含氢燃料的低NOx燃烧器及其操作
公开(公告)号：US20110094239A1
公开(公告)日：2011-04-28
申请号：US12857265
申请日：2010-08-16
申请人： Hiromi KOIZUMI , Satoshi Dodo , Hirokazu Takahashi , Tomohiro Asai , Tomomi Koganezawa , Shohei Yoshida
发明人： Hiromi KOIZUMI , Satoshi Dodo , Hirokazu Takahashi , Tomohiro Asai , Tomomi Koganezawa , Shohei Yoshida
IPC分类号： F02C7/22
CPC分类号： F23R3/346 , F23C2900/9901 , Y02E20/18
摘要： 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.
摘要翻译：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。

4. 发明申请

US20090223226A1 GAS TURBINE COMBUSTOR AND GASEOUS FUEL SUPPLY METHOD FOR GAS TURBINE COMBUSTOR 有权
标题翻译：气体涡轮机燃气轮机和气体燃料供应方法
公开(公告)号：US20090223226A1
公开(公告)日：2009-09-10
申请号：US12370236
申请日：2009-02-12
申请人： Hiromi Koizumi , Tomohiro Asai , Hiroshi Inoue , Tsunemasa Nishijima , Hidetaro Murata
发明人： Hiromi Koizumi , Tomohiro Asai , Hiroshi Inoue , Tsunemasa Nishijima , Hidetaro Murata
IPC分类号： F02C7/224
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。

5. 发明申请

US20080190113A1 Gas turbine combustor and fuel supply method for same 有权
标题翻译：燃气轮机燃烧器和燃油供应方法相同
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
CPC分类号： F23R3/286 , F23R3/343
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。

6. 发明申请

US20080190112A1 Gas turbine combustor and fuel supply method for same 有权
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
CPC分类号： F23R3/286 , F23R3/343
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.

7. 发明授权

US08143413B2 Polycationized phospholipid derivatives 有权
标题翻译：聚阳离子磷脂衍生物
公开(公告)号：US08143413B2
公开(公告)日：2012-03-27
申请号：US12550196
申请日：2009-08-28
申请人： Takehisa Dewa , Tomohiro Asai , Mamoru Nango , Naoto Oku
发明人： Takehisa Dewa , Tomohiro Asai , Mamoru Nango , Naoto Oku
IPC分类号： C07F9/06 , C07F9/02 , C07C69/34
CPC分类号： C07F9/2408 , C07F9/2458
摘要： The present invention provides novel phospholipid derivatives. Furthermore, the present invention provides lipid membrane structures excellent in gene/nucleic acid introduction efficiency into a cell.
摘要翻译：本发明提供新型磷脂衍生物。此外，本发明提供了将细胞的基因/核酸导入效率优异的脂质膜结构。

8. 发明申请

US20090317455A1 REVERSE TARGETING LIPID VESICLE 审中-公开
标题翻译：反向定向脂肪VESICLE
公开(公告)号：US20090317455A1
公开(公告)日：2009-12-24
申请号：US12377868
申请日：2007-08-31
申请人： Naoto Oku , Tomohiro Asai , Takeo Urakami
发明人： Naoto Oku , Tomohiro Asai , Takeo Urakami
IPC分类号： A61K9/127 , A61P37/02
CPC分类号： A61K39/385 , A61K9/0019 , A61K39/35 , A61K2039/55555 , A61K2039/6018 , A61K2300/00
摘要： The present invention provides an immunomodulating agent and a therapeutic agent for a immune disease, which comprise a lipid vesicle encapsulating a drug capable of suppressing or damaging an immunocyte that expresses or binds to an antibody, the lipid vesicle having an antigen for the antibody bound to the outer surface thereof. Hence, there is provided means for effectively treating an immune disease such as an allergic diseases or an autoimmune disease.
摘要翻译：本发明提供免疫调节剂和免疫疾病治疗剂，其包含包封能够抑制或损伤表达或结合抗体的免疫细胞的药物的脂质囊泡，所述脂质囊泡具有与抗体结合的抗体的抗原其外表面。因此，提供了有效治疗免疫疾病如过敏性疾病或自身免疫性疾病的手段。

9. 发明授权

US08393159B2 Gas turbine combustor and fuel supply method for same 有权
标题翻译：燃气轮机燃烧器和燃油供应方法相同
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
IPC分类号： F23R3/12 , F23R3/28
CPC分类号： F23R3/286 , F23R3/343
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。

10. 发明授权

US07673455B2 Gas turbine combustor and fuel supply method for same 有权
标题翻译：燃气轮机燃烧器和燃油供应方法相同
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
IPC分类号： F23R3/14 , F02C7/22
CPC分类号： F23R3/286 , F23R3/343
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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