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11. 发明专利

JP2011074802A Gas turbine combustor 审中-公开
标题翻译：气体涡轮搅拌机
公开(公告)号：JP2011074802A
公开(公告)日：2011-04-14
申请号：JP2009225888
申请日：2009-09-30
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： ASAI TOMOHIRO , KOIZUMI HIROMI , YOSHIDA SHOHEI , KOGANEZAWA TOMOKI
IPC分类号： F02C3/24 , F02C6/08 , F02C7/22 , F02C9/00 , F02C9/18 , F02C9/40 , F02C9/52 , F23R3/06 , F23R3/14 , F23R3/26 , F23R3/28
摘要： PROBLEM TO BE SOLVED: To solve a problem that the reliability of a burner is deteriorated because the metal temperature of a swirler surface drastically changes due to non-evaporation fuel or soot accumulating on the swirler surface, in a low quality oil fuel burning gas turbine combustor.
SOLUTION: The combustor includes a liquid fuel nozzle 20 jetting liquid fuel into a combustion chamber, a spray air nozzle 21 positioned on an outer peripheral side of the liquid fuel nozzle 20 and spraying spray air for atomizing the liquid fuel, and a swirler 17 supplying combustion air from the outer peripheral side of the spray air nozzle 21 to the combustion chamber. A purge air hole 50 for supplying purge air 104 is provided between a spray air hole 21a and a combustion air hole 24a on a swirler surface 18.
COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题为了解决由于旋流器表面的金属温度由于积聚在旋流器表面上的非蒸发燃料或烟灰而急剧变化的燃烧器的可靠性恶化的问题，在低质量的油燃料燃烧燃气轮机燃烧器。解决方案：燃烧器包括将液体燃料喷射到燃烧室中的液体燃料喷嘴20，位于液体燃料喷嘴20的外周侧的喷雾空气喷嘴21，喷射用于使液体燃料雾化的喷射空气，旋流器17将燃烧空气从喷雾空气喷嘴21的外周侧供给到燃烧室。在旋流器表面18上的喷射空气孔21a和燃烧空气孔24a之间设置有用于供给吹扫空气104的吹扫空气孔50.（C）2011，JPO＆INPIT

12. 发明专利

JP2010230287A Coal gasification power-generating plant and combustion method for coal gasification power-generating plant 审中-公开
标题翻译：燃煤发电厂的燃煤发电厂和燃烧方法
公开(公告)号：JP2010230287A
公开(公告)日：2010-10-14
申请号：JP2009080847
申请日：2009-03-30
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： KOIZUMI HIROMI , MOMO SATOSHI , TAKAHASHI HIROKAZU , YOSHIDA SHOHEI
IPC分类号： F23L7/00 , F23C99/00
CPC分类号： Y02E20/344
摘要： PROBLEM TO BE SOLVED: To further reduce NOx by disposing a partitioning wall having an injection hole for injecting nitrogen produced by an air separator to the outer periphery sidewall surface of an inner cylinder, on the inner side of an outer cylinder. SOLUTION: This coal gasification power-generating plant includes the air separator for separating the air into oxygen and nitrogen, a gasification furnace for producing a coal gasification gas by coal and oxygen produced by the air separator, a gas turbine combustor producing a combustion gas by the coal gasification gas produced by the gasification furnace, and a turbine driven by the combustion gas. On the inner side of the an outer cylinder of the gas turbine combustor, the partitioning wall is provided having the injection hole for injecting nitrogen produced by the air separator to the outer periphery sidewall surface of an inner cylinder of the gas turbine combustor. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：解决问题：为了进一步减少NOx，通过在外筒的内侧设置具有用于将由空气分离器产生的氮注入的注入孔的分隔壁设置在内筒的外周侧壁面上。解决方案：该煤气化发电厂包括用于将空气分离成氧和氮的空气分离器，用于由空气分离器产生的煤和氧产生煤气化气体的气化炉，产生由气化炉产生的煤气化气体的燃烧气体和由燃烧气体驱动的涡轮。在燃气轮机燃烧器的外筒的内侧，设置有分隔壁，其具有用于将由空气分离器产生的氮气喷射到燃气轮机燃烧器的内筒的外周侧壁面的喷射孔。版权所有（C）2011，JPO＆INPIT

13. 发明专利

JP2010065579A Fuel supply method of gas turbine 有权
标题翻译：燃油供应方法
公开(公告)号：JP2010065579A
公开(公告)日：2010-03-25
申请号：JP2008231618
申请日：2008-09-10
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： KOIZUMI HIROMI , ASAI TOMOHIRO , KOGANEZAWA TOMOKI , MIURA KEISUKE , YOSHIDA SHOHEI , NISHIJIMA YASUMASA
IPC分类号： F02C7/232 , F01K25/14 , F02C3/28 , F02C7/22 , F02C7/26 , F02C9/40
CPC分类号： Y02E20/18
摘要： PROBLEM TO BE SOLVED: To safely start a gas turbine without using starting fuel, even when hydrogen-including fuel is used for the gas turbine.
SOLUTION: A fuel supply method of a gas turbine combustor includes a fuel system for supplying the hydrogen-including fuel, a burner connected to the fuel system and jetting the hydrogen-including fuel to a combustion chamber, and a system for supplying purge gas to the fuel system, and includes a first process of supplying the purge gas in a pipe of the fuel system, and a second process of supplying the hydrogen-including fuel and the purge gas to the burner up to completing ignition from when starting the ignition of the gas turbine combustor.
COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：即使使用含氢燃料用于燃气轮机，也可以不使用起动燃料来安全地启动燃气轮机。解决方案：燃气轮机燃烧器的燃料供给方法包括用于供应含氢燃料的燃料系统，连接到燃料系统并将含氢燃料喷射到燃烧室的燃烧器和用于供给燃料的系统向燃料系统吹扫气体，并且包括在燃料系统的管道中供应吹扫气体的第一过程，以及将第二过程向燃烧器供应直到完成点火的燃料和净化气体从起动燃气轮机燃烧器的点火。版权所有（C）2010，JPO＆INPIT

14. 发明专利

JP2009002535A Diffusing combustion type gas turbine combustor 有权
标题翻译：扩散式燃气式燃气轮机
公开(公告)号：JP2009002535A
公开(公告)日：2009-01-08
申请号：JP2007161347
申请日：2007-06-19
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： HIRATA YOSHITAKA , YOSHIDA SHOHEI , INOUE HIROSHI , SASAO TOSHIBUMI , KOIZUMI HIROMI , SEKIGUCHI TATSUYA
IPC分类号： F23R3/12 , F23R3/04 , F23R3/18
摘要： PROBLEM TO BE SOLVED: To provide a diffusing combustion type gas turbine combustor capable of reducing NOx emission in a case when at least one of a gas fuel and a liquid fuel is burned.
SOLUTION: This diffusing combustion type gas turbine combustor comprises a combustion liner 7 for mixing the combustion air 13 from a compressor 1 with the fuels 16, 17 and burning the same, a liquid fuel nozzle 12 disposed at an upstream-side position on a shaft center line X of the combustion liner 7 for atomizing the liquid fuel 17 and injecting the same into the combustion liner 7, a swirler 11 circularly disposed at an outer peripheral side of the liquid fuel nozzle 12 and having a plurality of air holes 19, a plurality of gas fuel nozzles 15 injecting the gas fuel 16 toward the air holes 19 of the swirler 11, and a combustion liner cap 10 disposed at an outer peripheral side of the swirler 11, having a plurality of slit holes 23, and forming a low-velocity circulation flow 100 at an outer peripheral side of the swirler 11, and the air holes 19 are formed in parallel with the axis X in a sectional view including the shaft center line X so that the circulation flow 101 jetted from the air holes 19 into the combustion liner 7 is mixed with the circulation flow 100.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种在气体燃料和液体燃料中的至少一种燃烧的情况下能够减少NOx排放的扩散燃烧式燃气轮机燃烧器。解决方案：该扩散燃烧型燃气轮机燃烧器包括用于将来自压缩机1的燃烧空气13与燃料16,17混合的燃烧衬套7，并燃烧燃料衬套7，设置在上游侧位置的液体燃料喷嘴12 在用于雾化液体燃料17并将其注入燃烧衬套7的燃烧衬套7的轴心线X上，设置在液体燃料喷嘴12的外周侧的旋流器11，具有多个气孔如图19所示，多个气体燃料喷嘴15将气体燃料16喷射到旋流器11的气孔19，以及设置在旋流器11的外周侧的燃烧衬套帽10，具有多个狭缝孔23，在旋流器11的外周侧形成低速循环流100，并且在包括轴心线X的截面图中，气孔19与轴线X平行地形成，使得循环流101喷射进入燃烧衬套7的气孔19与循环流100混合。版权所有：（C）2009，JPO＆INPIT

15. 发明专利

JP2008275189A Gas turbine combustor and combustion method of gas turbine combustor 有权
标题翻译：气体涡轮机燃烧器燃烧器燃烧方法
公开(公告)号：JP2008275189A
公开(公告)日：2008-11-13
申请号：JP2007115651
申请日：2007-04-25
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： HIRATA YOSHITAKA , YOSHIDA SHOHEI , INOUE HIROSHI , SASAO TOSHIBUMI
IPC分类号： F23R3/30 , F23R3/06 , F23R3/12
摘要： PROBLEM TO BE SOLVED: To provide a gas turbine combustor capable of achieving stable combustion and reduction of NOx emission even when a liquid fuel of low quality is used.
SOLUTION: This gas turbine combustor 3 comprises a premixer having a fuel nozzle 105 for jetting the liquid fuel of low quality as fine liquid droplets, a mixing chamber 14 provided with the fuel nozzle at its head portion, formed along the fuel jetting direction, and mixing the fuel liquid droplets jetted from the fuel nozzle with a part of the compressed air, and an evaporation chamber 15 disposed between the mixing chamber 14 and the combustion chamber 3, and evaporating the fuel liquid droplets jetted from the fuel nozzle and mixed with a part of the compressed air in the mixing chamber, by the heat of a part of the compressed air, and a plurality of air introduction holes 18-20 are formed on a wall surface of the mixing chamber in a state of being separated from each other in the axial direction of the mixing chamber 14, to introduce a part of the compressed air into the mixing chamber 14 formed at an inner peripheral side.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：即使使用低质量的液体燃料，提供能够实现稳定的燃烧和NOx排放的降低的燃气轮机燃烧器。解决方案：该燃气轮机燃烧器3包括具有燃料喷嘴105的预混合器，用于喷射作为细小液滴的低质量液体燃料，混合室14在其头部设有燃料喷嘴，沿燃料喷射形成方向，并将从燃料喷嘴喷射的燃料液滴与一部分压缩空气混合，以及设置在混合室14和燃烧室3之间的蒸发室15，并蒸发从燃料喷嘴喷射的燃料液滴，通过一部分压缩空气的热量与混合室中的一部分压缩空气混合，并且在分离的状态下在混合室的壁表面上形成多个空气引入孔18-20 在混合室14的轴向上彼此之间，将一部分压缩空气引入形成在内周侧的混合室14中。版权所有（C）2009，JPO＆INPIT

16. 发明专利

JP2008170059A Gas turbine combustor and its modifying method 审中-公开
标题翻译：燃气轮机及其改造方法
公开(公告)号：JP2008170059A
公开(公告)日：2008-07-24
申请号：JP2007003281
申请日：2007-01-11
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： YOSHIDA SHOHEI , HIRATA YOSHITAKA , INOUE HIROSHI , SASAO TOSHIBUMI
IPC分类号： F23R3/34 , F02C7/00 , F02C7/232 , F02C9/26 , F23R3/14 , F23R3/30
摘要： PROBLEM TO BE SOLVED: To provide a gas turbine combustion and its modifying method capable of reducing an exhaust amount of NOx by a simple and inexpensive composition.
SOLUTION: The gas turbine combustor is provided with: a low load fuel nozzle 9; a high load fuel nozzle 11; a fuel supply device 19 being a supply source of fuel injected by the fuel nozzles 9, 11; a low load fuel pipe 20 leading fuel from the fuel supply device 19 to the low load fuel nozzle 9; a high load fuel pipe 21 leading fuel from the fuel supply device 19 to the high load fuel nozzle 11; a low load fuel flow regulating valve 22 provided in the low load fuel pipe 20, increasing a fuel supply amount following rising of a fuel supply pressure, and reducing the fuel supply amount when the fuel supply pressure becomes a set value or more; and a high load fuel flow regulating valve 23 provided in the high load fuel piping 21, and starting supply of fuel when the fuel supply pressure becomes a set value or more.
COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够通过简单且廉价的组合物来减少NOx的排气量的燃气轮机燃烧及其改进方法。燃气轮机燃烧器设置有：低负荷燃料喷嘴9; 高负荷燃料喷嘴11; 作为由燃料喷嘴9,11喷射的燃料的供给源的燃料供给装置19; 将燃料从燃料供给装置19引导到低负荷燃料喷嘴9的低负荷燃料管20; 将燃料从燃料供给装置19引导到高负荷燃料喷嘴11的高负荷燃料管21; 设置在低负荷燃料管20中的低负荷燃料流量调节阀22，在燃料供给压力升高之后增加燃料供给量，并且在燃料供给压力成为设定值以上时，减少燃料供给量; 以及设置在高负荷燃料管路21中的高负荷燃料流量调节阀23，当燃料供给压力成为设定值以上时开始供给燃料。版权所有（C）2008，JPO＆INPIT

17. 发明专利

JP2008031847A Gas turbine combustor, its operating method, and modification method of gas turbine combustor 审中-公开
标题翻译：气体涡轮搅拌机，其运行方法和气体涡轮搅拌机的改造方法
公开(公告)号：JP2008031847A
公开(公告)日：2008-02-14
申请号：JP2006202717
申请日：2006-07-26
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： YOSHIDA SHOHEI , HIRATA YOSHITAKA , INOUE HIROSHI , SASAO TOSHIBUMI , MOMO SATOSHI
IPC分类号： F02C3/30 , F23R3/00
摘要： PROBLEM TO BE SOLVED: To suppress a generation amount of dust under a low load condition of a gas turbine.
SOLUTION: The gas turbine combustor comprises: an inner cylinder mixing combustion air with fuel so as to generate combustion gas; a swirler 10 positioned upstream of the inner cylinder so as to give a swirl component to the combustion air flowing into the inner cylinder; and a combustion chamber arranged in the inner cylinder so as to burn the fuel and the air. A pressure spraying type fuel nozzle 9 is arranged in the center of the axis of the swirler, and has a pilot injection hole blowing pilot fuel and a main injection hole blowing main fuel and arranged on an outer peripheral side of the pilot injection hole, and a means for supplying water to the pilot fuel or main fuel is provided. Therefore, the generation amount of dust is suppressed under the low load condition of the gas turbine.
COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：为了抑制在燃气轮机的低负载条件下的灰尘的产生量。燃气轮机燃烧器包括：内燃机，其将燃烧空气与燃料混合以产生燃烧气体; 旋转器10位于内筒的上游，以便向流入内筒的燃烧空气产生旋流分量; 以及设置在内筒中以燃烧燃料和空气的燃烧室。喷射型燃料喷嘴9配置在旋流器的轴心的中央，并且具有向先导喷射孔喷射先导燃料的主喷射孔和主喷射主喷射孔，并且配置在引燃喷射孔的外周侧，提供了向先导燃料或主燃料供水的方法。因此，在燃气轮机的低负荷状态下，能够抑制灰尘的产生量。版权所有（C）2008，JPO＆INPIT

18. 发明专利

JP2007205215A Control method for gas turbine, and control device for gas turbine 有权
标题翻译：用于气体涡轮机的控制方法和用于气体涡轮机的控制装置
公开(公告)号：JP2007205215A
公开(公告)日：2007-08-16
申请号：JP2006024048
申请日：2006-02-01
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： HIRATA YOSHITAKA , YOSHIDA SHOHEI , TAKAHASHI YASUO , SASAO TOSHIBUMI , INOUE HIROSHI , MURATA EITARO , ITO KAZUYUKI
IPC分类号： F02C7/042 , F01D17/00 , F02C7/18 , F04D27/00 , F04D29/56
CPC分类号： F02C9/54 , F02C7/22 , F02C7/2365 , F02C9/20 , F05D2270/08 , F05D2270/083 , F05D2270/303 , F05D2270/304 , F23N2035/06 , F23N2041/20 , F23R3/26
摘要： PROBLEM TO BE SOLVED: To suppress an amount of generation of soot and dust in a partial load area, while enjoying an advantage of a pressure spraying type liquid fuel nozzle.
SOLUTION: A combustor is provided with a pressure spraying type liquid fuel nozzle. A working fluid flow rate of a compressor is reduced with respect to a working fluid flow rate of a compressor set so that the performance of the compressor becomes the highest in the partial load area of the gas turbine. The amount of generation of soot and dust in the partial load area is thereby suppressed, while enjoying the advantage of the pressure spraying type liquid fuel nozzle.
COPYRIGHT: (C)2007,JPO&INPIT
摘要翻译：解决问题：在享受压力喷射型液体燃料喷嘴的优点的同时，抑制部分负荷区域中的烟灰和灰尘的产生量。解决方案：燃烧器设置有压力喷射型液体燃料喷嘴。相对于压缩机组的工作流体流量，压缩机的工作流体流量减小，使得压缩机的性能在燃气轮机的部分负载区域中变得最高。由此，能够在享受压力喷射式液体燃料喷嘴的优点的同时，抑制部分负荷区域中的烟尘的产生量。版权所有（C）2007，JPO＆INPIT

19. 发明专利

JP2007064625A Gas turbine combustor and its fuel supply method 有权
标题翻译：燃气轮机及其燃油供应方法
公开(公告)号：JP2007064625A
公开(公告)日：2007-03-15
申请号：JP2006332911
申请日：2006-12-11
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： YOSHIDA SHOHEI , HIRATA YOSHITAKA , ITO KAZUYUKI , MUROTA TOMOYA , INOUE HIROSHI , ASAI TOMOHIRO
IPC分类号： F23R3/10 , F02C7/22 , F23R3/28 , F23R3/34 , F23R3/36
摘要： PROBLEM TO BE SOLVED: To provide a gas turbine combustor and its fuel supply method capable of preventing backfire, while reducing an NOx generation quantity. SOLUTION: This combustor 2 for mixing a fuel with combustion air introduced from a compressor 1 and burning it, and supplying generated combustion gas to a gas turbine 3 is equipped with a liquid fuel nozzle 13 for blowing out the fuel; a mixing chamber wall 5 equipped with the liquid fuel nozzle 13 in the center, having a hollow circular-cone shape enlarged toward the blowout direction, and forming a mixing chamber 4 inside; a plurality of air introduction holes 14, 15, 16 bored on the mixing chamber wall 5 so that the combustion air is introduced into the mixing chamber 4, and that simultaneously its introduction angle is deflected at least toward the circumferential direction of the mixing chamber wall 5; and each gas fuel nozzle 17 provided respectively oppositely to the plurality of air introduction holes 14, 15, 16 on the peripheral side of the mixing chamber wall 5, for blowing out the fuel approximately in the same axial direction as axial lines L1, L2, L3 of the air introduction holes 14, 15, 16. COPYRIGHT: (C)2007,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够在减少NOx生成量的同时防止回火的燃气轮机燃烧器及其燃料供给方法。解决方案：用于将燃料与从压缩机1引入的燃烧空气混合并将其燃烧并将生成的燃烧气体供应到燃气轮机3的燃烧器2配备有用于吹出燃料的液体燃料喷嘴13; 在中央配备有液体燃料喷嘴13的混合室壁5，具有朝向吹出方向扩大的中空圆锥形状，在内部形成混合室4; 在混合室壁5上钻出的多个空气导入孔14,15,16，使得燃烧空气被引入到混合室4中，同时其引入角度至少朝向混合室壁的圆周方向偏转 5; 以及与混合室壁5的周边侧的多个空气导入孔14,15,16分别相对地设置的各气体燃料喷嘴17，用于沿与轴线L1，L2相同的轴线吹出燃料，空气导入孔14,15,16的L3。版权所有（C）2007，JPO＆INPIT

20. 发明专利

JP2007024357A Gas turbine combustor, method of preventing carbonization of fuel, and purging method 有权
标题翻译：气体燃烧器，燃烧碳化方法和清洗方法
公开(公告)号：JP2007024357A
公开(公告)日：2007-02-01
申请号：JP2005204615
申请日：2005-07-13
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： YOSHIDA SHOHEI , HIRATA YOSHITAKA , INOUE HIROSHI , SASAO TOSHIBUMI
IPC分类号： F23R3/28 , F02C3/30 , F02C7/232 , F23R3/12 , F23R3/34
摘要： PROBLEM TO BE SOLVED: To provide a gas turbine combustor, a method of preventing carbonization of fuel, and a purging method capable of preventing accumulation of carbon inside of a fuel nozzle and fuel piping regardless of an operating state of a gas turbine without enlarging gas turbine equipment.
SOLUTION: This gas turbine combustor 4 having a pilot burner 6 and a main burner 8, further comprises pilot piping 17 for supplying fuel to the pilot burner 6, main piping 18 for supplying fuel to the main burner 8, and communication piping 21 connecting the pilot piping 17 and the main piping 18, and guiding a part of the fuel supplied to the pilot burner 6, to the main burner 8 during the stop of the main burner 8.
COPYRIGHT: (C)2007,JPO&INPIT
摘要翻译：要解决的问题：提供一种燃气轮机燃烧器，防止燃料碳化的方法以及能够防止燃料喷嘴和燃料管道内部的碳积聚的吹扫方法，而不管燃气轮机的运行状态如何没有扩大燃气轮机设备。解决方案：具有引燃燃烧器6和主燃烧器8的燃气轮机燃烧器4还包括用于向引燃燃烧器6供给燃料的先导配管17，向主燃烧器8供给燃料的主配管18，以及连通配管 21，在主燃烧器8的停止期间，连接先导管道17和主管道18，并将供给到先导燃烧器6的燃料的一部分引导到主燃烧器8.版权所有（C）2007， JPO＆INPIT

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