公开(公告)号：US09121611B2

公开(公告)日：2015-09-01

申请号：US13552723

申请日：2012-07-19

申请人： Hiromi Koizumi ,  Shohei Yoshida ,  Satoshi Dodo

发明人： Hiromi Koizumi ,  Shohei Yoshida ,  Satoshi Dodo

IPC分类号： F23R3/28 ,  F23R3/10 ,  F23R3/34 ,  F23R3/54

CPC分类号： F23R3/28 ,  F23R3/10 ,  F23R3/343 ,  F23R2900/00002 ,  F23R2900/00004

摘要： A combustor is provided that can ensure combustion stability even when operated on low BTU gas without needing any equipment for preventing back-flow of fuel gas during operation on pilot fuel. The combustor includes a first perforated plate disposed upstream of a combustion chamber, the first plate having a plurality of nozzle holes and air holes; a second perforated plate disposed on the upstream side of the first plate; and a plurality of gas nozzles each of which is inserted into corresponding nozzle holes. The gas nozzle has a leading end located inside the corresponding one of the nozzle holes. Each of the gas nozzles includes a jet hole portion having a diameter smaller than that of a gas jet hole of the gas nozzle; and a passage portion designed to form an air passage on the outer circumference of the leading end portion of the gas nozzle.

摘要翻译： 提供了一种燃烧器，即使在低BTU气体下运行时也能确保燃烧稳定性，而不需要任何设备来防止燃油在运行过程中逆流。 燃烧器包括设置在燃烧室上游的第一多孔板，第一板具有多个喷嘴孔和气孔; 设置在所述第一板的上游侧的第二多孔板; 以及各自插入相应的喷嘴孔中的多个气体喷嘴。 气体喷嘴具有位于对应的一个喷嘴孔内的前端。 每个气体喷嘴包括直径小于气体喷嘴的气体喷射孔的直径的喷射孔部分; 以及设计成在气体喷嘴的前端部的外周形成空气通路的通路部。

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。

公开(公告)号：US20130029277A1

公开(公告)日：2013-01-31

申请号：US13552723

申请日：2012-07-19

申请人： Hiromi Koizumi ,  Shohei Yoshida ,  Satoshi Dodo

发明人： Hiromi Koizumi ,  Shohei Yoshida ,  Satoshi Dodo

IPC分类号： F23D14/62

CPC分类号： F23R3/28 ,  F23R3/10 ,  F23R3/343 ,  F23R2900/00002 ,  F23R2900/00004

摘要： A combustor is provided that can ensure combustion stability even when operated on low BTU gas without needing any equipment for preventing back-flow of fuel gas during operation on pilot fuel. The combustor includes a first perforated plate disposed upstream of a combustion chamber, the first plate having a plurality of nozzle holes and air holes; a second perforated plate disposed on the upstream side of the first plate; and a plurality of gas nozzles each of which is inserted into corresponding nozzle holes. The gas nozzle has a leading end located inside the corresponding one of the nozzle holes. Each of the gas nozzles includes a jet hole portion having a diameter smaller than that of a gas jet hole of the gas nozzle; and a passage portion designed to form an air passage on the outer circumference of the leading end portion of the gas nozzle.

摘要翻译： 提供了一种燃烧器，即使在低BTU气体下运行时也能确保燃烧稳定性，而不需要任何设备来防止燃油在运行过程中逆流。 燃烧器包括设置在燃烧室上游的第一多孔板，第一板具有多个喷嘴孔和气孔; 设置在所述第一板的上游侧的第二多孔板; 以及各自插入相应的喷嘴孔中的多个气体喷嘴。 气体喷嘴具有位于对应的一个喷嘴孔内的前端。 每个气体喷嘴包括直径小于气体喷嘴的气体喷射孔的直径的喷射孔部分; 以及设计成在气体喷嘴的前端部的外周形成空气通路的通路部。

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。

公开(公告)号：US20070256416A1

公开(公告)日：2007-11-08

申请号：US10582954

申请日：2003-12-16

申请人： Satoshi Dodo ,  Susumu Nakano ,  Kuniyoshi Tsubouchi ,  Shohei Yoshida ,  Yoshitaka Hirata

发明人： Satoshi Dodo ,  Susumu Nakano ,  Kuniyoshi Tsubouchi ,  Shohei Yoshida ,  Yoshitaka Hirata

IPC分类号： F02C7/00

CPC分类号： F23R3/44 ,  F23R3/045 ,  F23R3/06 ,  F23R3/14 ,  F23R3/34 ,  F23R3/346

摘要： A combustor for a gas turbine capable of performing stable combustion even by using high temperature air, comprising a first burner (5) jetting fuel and air into a combustion chamber (2) and a second burner (8) causing the circulating jet of the fuel and air installed at a position corresponding to the tip part of a flame caused by the first burner (5).

摘要翻译： 一种用于燃气轮机的燃烧器，其能够通过使用高温空气来执行稳定的燃烧，包括将燃料和空气喷射到燃烧室（2）中的第一燃烧器（5）和引起燃料循环喷射的第二燃烧器（8） 和空气安装在与由第一燃烧器（5）引起的火焰的尖端部分对应的位置。

公开(公告)号：US08397510B2

公开(公告)日：2013-03-19

申请号：US10582954

申请日：2003-12-16

申请人： Satoshi Dodo ,  Susumu Nakano ,  Kuniyoshi Tsubouchi ,  Shohei Yoshida ,  Yoshitaka Hirata

发明人： Satoshi Dodo ,  Susumu Nakano ,  Kuniyoshi Tsubouchi ,  Shohei Yoshida ,  Yoshitaka Hirata

IPC分类号： F02C1/00

CPC分类号： F23R3/44 ,  F23R3/045 ,  F23R3/06 ,  F23R3/14 ,  F23R3/34 ,  F23R3/346

摘要： A combustor for a gas turbine capable of performing stable combustion even by using high temperature air, comprising a first burner (5) jetting fuel and air into a combustion chamber (2) and a second burner (8) causing the circulating jet of the fuel and air installed at a position corresponding to the tip part of a flame caused by the first burner (5).

摘要翻译： 一种用于燃气轮机的燃烧器，其能够通过使用高温空气来执行稳定的燃烧，包括将燃料和空气喷射到燃烧室（2）中的第一燃烧器（5）和引起燃料循环喷射的第二燃烧器（8） 和空气安装在与由第一燃烧器（5）引起的火焰的尖端部分对应的位置。

公开(公告)号：US5836164A

公开(公告)日：1998-11-17

申请号：US593087

申请日：1996-01-29

申请人： Satoshi Tsukahara ,  Shohei Yoshida ,  Masahiko Yamagishi ,  Kazumi Iwai ,  Hiromi Koizumi ,  Yoichi Yoshinaga

发明人： Satoshi Tsukahara ,  Shohei Yoshida ,  Masahiko Yamagishi ,  Kazumi Iwai ,  Hiromi Koizumi ,  Yoichi Yoshinaga

IPC分类号： F23C6/04 ,  F23R3/28 ,  F23R3/34 ,  F02C1/00

CPC分类号： F23R3/286 ,  F23C6/047 ,  F23R3/34 ,  F23R3/346 ,  F23D2900/00008

摘要： A gas turbine combustor includes a diffusion combustor arranged at an axis portion of a combustion chamber for effecting diffusion combustion, a plurality of first premixing combustors arranged at an outer periphery of the diffusion combustor for effecting premixed combustion, each of the plurality of first premixing combustors being formed so that a mixture outlet end thereof projects more downstream than a fuel outlet end of the diffusion combustor, and a plurality of second premixing combustors each formed so that a mixture outlet thereof projects more downstream than the mixture outlet end of the first combustor, wherein the first premixing combustors and the second premixing combustors are arranged alternately at the outer periphery of the diffusion combustor, and wherein a swirler is provided on the first premixing combustor in the vicinity of the mixture outlet end thereof for swirling mixture.

摘要翻译： 燃气轮机燃烧器包括布置在燃烧室的轴线部分以进行扩散燃烧的扩散燃烧器，多个第一预混合燃烧器，其布置在扩散燃烧室的外周处以实现预混合燃烧;多个第一预混合燃烧器 形成为使得其混合物出口端比扩散燃烧器的燃料出口端更下游突出，并且多个第二预混合燃烧器各自形成为使得其混合物出口比第一燃烧器的混合物出口端更下游突出， 其中所述第一预混合燃烧器和所述第二预混合燃烧器交替地布置在所述扩散燃烧器的外周，并且其中在所述第一预混合燃烧器的混合物出口端附近设置旋流器以进行旋转混合。

公开(公告)号：US09353951B2

公开(公告)日：2016-05-31

申请号：US13047227

申请日：2011-03-14

申请人： Daisuke Hayashi ,  Shohei Yoshida

发明人： Daisuke Hayashi ,  Shohei Yoshida

IPC分类号： F02C7/00 ,  F23R3/34 ,  F23D14/64 ,  F23R3/10 ,  F23R3/28

CPC分类号： F23R3/343 ,  F23D14/64 ,  F23D2900/00008 ,  F23R3/10 ,  F23R3/286 ,  F23R2900/00002

摘要： A combustor with a burner maintains combustion stability. The burner includes an air hole member 31 with a plurality of air holes 34, 35 provided at an upstream side of the combustion gases generated by a combustion chamber 1. A first fueling nozzle 33 jets fuel in a direction crossing a central axis of the burner towards at least two of air holes 35. A plurality of second fueling nozzles 32, one for each of the remaining air holes 34, are provided to jet the fuel in a direction routed along the burner axis towards the corresponding air hole 34. A fuel header 30 distributes the fuel to the first fueling nozzle 33 and each of the second fueling nozzles 32. A fuel header storage unit 70 shrouds the fuel header 30, fueling nozzles 32, 33, and has an air inflow hole 71.

摘要翻译： 具有燃烧器的燃烧器保持燃烧稳定性。 燃烧器包括一个气孔构件31，其具有设置在由燃烧室1产生的燃烧气体的上游侧的多个气孔34,35。第一燃料喷嘴33沿与燃烧器的中心轴线交叉的方向喷射燃料 至少两个气孔35.多个第二燃料喷嘴32，一个用于每个剩余的空气孔34，以沿着燃烧器轴线向着相应的气孔34喷射燃料。燃料 集管30将燃料分配到第一加燃料喷嘴33和每个第二加燃料喷嘴32.燃料头存放单元70覆盖燃料集管30，燃料喷嘴32,33，并具有空气流入孔71。

公开(公告)号：US08252672B2

公开(公告)日：2012-08-28

申请号：US12267040

申请日：2008-11-07

申请人： Tomokatsu Watanabe ,  Sunao Aya ,  Naruhisa Miura ,  Keiko Sakai ,  Shohei Yoshida ,  Toshikazu Tanioka ,  Yukiyasu Nakao ,  Yoichiro Tarui ,  Masayuki Imaizumi

发明人： Tomokatsu Watanabe ,  Sunao Aya ,  Naruhisa Miura ,  Keiko Sakai ,  Shohei Yoshida ,  Toshikazu Tanioka ,  Yukiyasu Nakao ,  Yoichiro Tarui ,  Masayuki Imaizumi

IPC分类号： H01L21/265

CPC分类号： H01L29/7802 ,  H01L21/046 ,  H01L21/0485 ,  H01L29/1608 ,  H01L29/66068 ,  H01L29/7828

摘要： A method of manufacturing a silicon carbide semiconductor device having a silicon carbide layer, the method including a step of implanting at least one of Al ions, B ions and Ga ions having an implantation concentration in a range not lower than 1E19 cm−3 and not higher than 1E21 cm−3 from a main surface of the silicon carbide layer toward the inside of the silicon carbide layer while maintaining the temperature of the silicon carbide layer at 175° C. or higher, to form a p-type impurity layer; and forming a contact electrode whose back surface establishes ohmic contact with a front surface of the p-type impurity layer on the front surface of the p-type impurity layer.

摘要翻译： 一种制造具有碳化硅层的碳化硅半导体器件的方法，该方法包括以下步骤：注入注入浓度在1E19cm-3以上的Al离子，B离子和Ga离子中的至少一种，而不是 高于1E21cm-3，从碳化硅层的主表面朝向碳化硅层的内部，同时将碳化硅层的温度保持在175℃以上，形成p型杂质层; 以及形成其背面与p型杂质层前表面上的p型杂质层的前表面欧姆接触的接触电极。

公开(公告)号：US07844128B2

公开(公告)日：2010-11-30

申请号：US12385702

申请日：2009-04-16

申请人： Takashi Toyooka ,  Shohei Yoshida

发明人： Takashi Toyooka ,  Shohei Yoshida

IPC分类号： G06K9/36

CPC分类号： G09G3/2092 ,  G09G2320/02 ,  G09G2320/0261 ,  G09G2320/10

摘要： An image display method includes dividing one frame into a plurality of sub-frames by multiplying a frame frequency of an input image signal, reducing a high-spatial frequency component of an image signal which is used for image display in at least one predetermined sub-frame among the plurality of sub-frames in comparison with that of an image signal which is used for image display in another sub-frame, and displaying an image in each sub-frame.

摘要翻译： 一种图像显示方法包括：通过将输入图像信号的帧频相乘来将一帧划分成多个子帧，减少用于至少一个预定子帧中的图像显示的图像信号的高空间频率分量， 与在另一子帧中用于图像显示的图像信号的帧相比，并且在每个子帧中显示图像。