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公开(公告)号：US20120192568A1
公开(公告)日：2012-08-02
申请号：US13358227
申请日：2012-01-25
申请人： Keisuke MIURA , Tomomi Koganezawa , Satoshi Dodo , Takeo Saito
发明人： Keisuke MIURA , Tomomi Koganezawa , Satoshi Dodo , Takeo Saito
CPC分类号： F23R3/286 , F23R3/343 , F23R2900/00014
摘要： A combustor of the prior art that defines the outlet position and direction of an air hole and suppresses adhesion of flame to an air hole outlet can reduce a discharge amount of NOx by increasing a distance over which fuel and air are mixed with each other. However, such a combustor is not sufficiently discussed for measures to suppress the occurrence of combustion oscillation resulting from the variation of a flame surface.A combustor 2 according to the present invention includes a combustion chamber 5 to which fuel and air are supplied; air holes 32 adapted to supply air to the combustion chamber 5; fuel nozzles 25 adapted to supply gaseous fuel to the air holes 32; and orifices 24 adapted to allow the gaseous fuel supplied to the air holes 32 to cause a pressure drop.
摘要翻译： 限定空气孔的出口位置和方向并且抑制火焰与空气孔出口的粘附的现有技术的燃烧器可以通过增加燃料和空气彼此混合的距离来减少NOx的排放量。 但是，为了抑制由火焰表面的变化引起的燃烧振动的发生的措施，这种燃烧器没有充分的讨论。 根据本发明的燃烧器2包括供应燃料和空气的燃烧室5; 适于向燃烧室5供应空气的气孔32; 适于向气孔32供应气体燃料的燃料喷嘴25; 以及适于允许供应到气孔32的气体燃料引起压降的孔口24。
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公开(公告)号：US20110076628A1
公开(公告)日：2011-03-31
申请号：US12893879
申请日：2010-09-29
申请人： Keisuke MIURA , Satoshi Dodo , Kazuki Abe , Tomomi Koganezawa
发明人： Keisuke MIURA , Satoshi Dodo , Kazuki Abe , Tomomi Koganezawa
CPC分类号： F23R3/10 , F23R3/286 , F23R3/343 , Y02T50/675
摘要： This invention is directed to supply a combustor having a structure that reduces NOx emissions while maintaining combustion stability. The combustor has a chamber into which fuel and air are supplied. An air hole plate having a plurality of air holes upstream of the chamber is also disclosed, and fuel nozzles supplying fuel to the air holes of the air hole plate are further disclosed. In the combustor, a center of a chamber-side of the air hole plate is closer to the chamber than exits of outermost peripheral air holes.
摘要翻译： 本发明旨在提供具有减少NOx排放的结构的燃烧器，同时保持燃烧稳定性。 燃烧器具有供应燃料和空气的室。 还公开了一种在腔室上游具有多个气孔的气孔板，并且还公开了向空气孔板的气孔供给燃料的燃料喷嘴。 在燃烧器中，气孔板的室侧的中心比最外周气孔的出口更靠近室。
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23.发明申请HUMID AIR TURBINE, HUMID AIR TURBINE CONTROL SYSTEM, AND HUMID AIR TURBINE CONTROL METHOD 有权湿度空气涡轮机，湿度空气涡轮机控制系统和湿度空气涡轮机控制方法公开(公告)号：US20080229755A1
公开(公告)日：2008-09-25
申请号：US12018574
申请日：2008-01-23
CPC分类号： F02C3/22 , F01D25/305 , F01D25/32 , F02C1/005 , F02C3/305 , F23L2900/00001 , F23N2041/20
摘要： The present invention provides a humid air turbine having a compressor, a humidificator for generating humid air by adding moisture to compressed air supplied from the compressor, a combustor, a turbine, a recuperator for effecting heat exchange between exhaust from the turbine and the humid air, an economizer for effecting heat exchange between exhaust from the recuperator and water, and a system for supplying the water heated by the economizer to the humidificator. The humid air turbine includes a temperature measurement device for measuring the temperature of gas discharged from the economizer, and a control device for adjusting the amount of moisture to be supplied to the humidificator in accordance with a temperature signal from the temperature measurement device. The present invention assures low NOx of combustor and flame stability before and after water addition to the humid air turbine.
摘要翻译： 本发明提供一种湿空气涡轮机，其具有压缩机，加湿器，用于通过向从压缩机供应的压缩空气增加水分产生潮湿空气，燃烧器，涡轮机，用于实现来自涡轮机的排气与湿空气之间的热交换的换热器 ，用于实现来自换热器的排气与水之间的热交换的节能器，以及用于将由节能器加热的水供应到加湿器的系统。 湿式空气涡轮机包括：温度测量装置，用于测量从节能器排出的气体的温度;以及控制装置，用于根据来自温度测量装置的温度信号调节供给到加湿器的水分量。 本发明确保在加入湿空气涡轮机之前和之后的燃烧器的低NOx和火焰稳定性。
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公开(公告)号：US07343745B2
公开(公告)日：2008-03-18
申请号：US11136554
申请日：2005-05-25
IPC分类号： F02C7/22
摘要： A gas turbine combustor has a combustion chamber into which fuel and air are supplied, wherein the fuel and the air are supplied into said combustion chamber as a plurality of coaxial jets.
摘要翻译： 燃气轮机燃烧器具有供给燃料和空气的燃烧室，其中燃料和空气作为多个同轴喷嘴供应到所述燃烧室中。
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公开(公告)号：US07340881B2
公开(公告)日：2008-03-11
申请号：US10730088
申请日：2003-12-09
CPC分类号： F01D9/023 , F02C3/145 , F02C7/08 , F05D2260/212
摘要： The invention provides a gas turbine combustor in which the size of a combustor outer casing can be reduced. A transition inner duct and a transition outer duct are disposed in a main housing, inlet openings for a fluid to cool the transition inner duct are formed at ends of the transition outer duct on both sides nearer to the combustor liner and the turbine, and the transition outer duct is formed as an extraction flow passage for extracting the cooling fluid having flown in through the inlet openings to a recuperator. A partition member is also provided to prevent the fluid in the main housing and the fluid in the combustor outer casing from mixing with each other.
摘要翻译： 本发明提供一种燃气轮机燃烧器，其中可以减小燃烧器外壳的尺寸。 过渡内管道和过渡外管道设置在主壳体中，用于冷却过渡内管道的流体的入口开口形成在过渡外管道的靠近燃烧器衬套和涡轮机的两侧的端部，并且 过渡外管形成为用于将通过入口开口流入的冷却流体提取到换热器的提取流路。 还设置有分隔构件以防止主壳体中的流体和燃烧器外壳体中的流体彼此混合。
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公开(公告)号：US07188476B2
公开(公告)日：2007-03-13
申请号：US11136573
申请日：2005-05-25
IPC分类号： F02C7/228
摘要： A gas turbine combustor has a combustion chamber into which fuel and air are supplied, wherein the fuel and the air are supplied into said combustion chamber as a plurality of coaxial jets.
摘要翻译： 燃气轮机燃烧器具有供给燃料和空气的燃烧室，其中燃料和空气作为多个同轴喷嘴供应到所述燃烧室中。
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27.发明授权Gas turbine combustor with fuel-air pre-mixer and pre-mixing method for low nox combustion 有权燃气轮机燃烧器采用燃油预混合器和预混合方式进行低NOx燃烧公开(公告)号：US06871503B1
公开(公告)日：2005-03-29
申请号：US10088114
申请日：1999-10-20
申请人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Masaya Ohtsuka , Kazuyuki Ito , Isao Takehara
发明人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Masaya Ohtsuka , Kazuyuki Ito , Isao Takehara
摘要： The purpose is to improve the mixture ratio of a pre-mixer by a simple arrangement to form a more uniform premixed gases so as to materialize low NOx combustion. Two fuel nozzles disposed circumferentially of a pre-mixer are combined with a single air intake window to make a set, which set is used to produce swirls in a pair, thereby expediting mixing. Further, the inlet window is shaped such that its circumferential width is changed axially of the combustor, thereby changing the strength and size of the swirls to achieve the greatest effect. By reducing both the pre-mixer inlet windows and the partition walls in number, the manufacturing cost can be reduced, and by strengthening and optimizing the swirls, a combustor with superior low NOx performance can be provided, while it is possible to reduce the length of the pre-mixer necessary to obtain the same mixture ratio, leading to a cost reduction.
摘要翻译： 目的是通过简单的布置提高预混合器的混合比，以形成更均匀的预混合气体，以实现低NOx燃烧。 将预混合器周向设置的两个燃料喷嘴与单个进气窗口组合以制成一组，该组用于产生一对涡流，从而加速混合。 此外，入口窗口的形状使得其周向宽度沿着燃烧器的轴向改变，从而改变了涡流的强度和尺寸以达到最大的效果。 通过减少预混合器入口窗口和隔壁，可以降低制造成本，并且通过强化和优化涡流，可以提供具有优异的低NOx性能的燃烧器，同时可以减小长度 的预混合器，以获得相同的混合比，导致成本降低。
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28.发明授权Combustor and the method of fuel supply and converting fuel nozzle for advanced humid air turbine 有权燃烧器和燃料供应和转换燃料喷嘴用于先进湿润空气涡轮机的方法公开(公告)号：US09334808B2
公开(公告)日：2016-05-10
申请号：US13197953
申请日：2011-08-04
申请人： Kazuki Abe , Tomomi Koganezawa
发明人： Kazuki Abe , Tomomi Koganezawa
摘要： A fuel control device and method of a gas turbine combustor, for advanced humid air turbines, in which plural combustion units comprising plural fuel nozzles for supplying fuel and plural air nozzles for supplying air for combustion are provided. A part of the plural combustion units are more excellent in flame stabilizing performance than the other combustion units. A fuel ratio, at which fuel is fed to the part of the combustion units is set on the basis of internal temperature of the humidification tower and internal pressure of the humidification tower to control a flow ratio of the fuel fed to the plural combustion units.
摘要翻译： 提供一种用于先进湿式空气涡轮机的燃气轮机燃烧器的燃料控制装置和方法，其中包括用于供应燃料的多个燃料喷嘴和用于供给燃烧空气的多个空气喷嘴的多个燃烧单元。 多个燃烧单元的一部分在火焰稳定性方面优于其它燃烧单元。 基于加湿塔的内部温度和加湿塔的内部压力来设定向燃烧单元的一部分供给燃料的燃料比，以控制供给到多个燃烧单元的燃料的流量比。
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公开(公告)号：US09074772B2
公开(公告)日：2015-07-07
申请号：US12893879
申请日：2010-09-29
申请人： Keisuke Miura , Satoshi Dodo , Kazuki Abe , Tomomi Koganezawa
发明人： Keisuke Miura , Satoshi Dodo , Kazuki Abe , Tomomi Koganezawa
CPC分类号： F23R3/10 , F23R3/286 , F23R3/343 , Y02T50/675
摘要： This invention is directed to supply a combustor having a structure that reduces NOx emissions while maintaining combustion stability. The combustor has a chamber into which fuel and air are supplied. An air hole plate having a plurality of air holes upstream of the chamber is also disclosed, and fuel nozzles supplying fuel to the air holes of the air hole plate are further disclosed. In the combustor, a center of a chamber-side of the air hole plate is closer to the chamber than exits of outermost peripheral air holes.
摘要翻译： 本发明旨在提供具有减少NOx排放的结构的燃烧器，同时保持燃烧稳定性。 燃烧器具有供应燃料和空气的室。 还公开了一种在腔室上游具有多个气孔的气孔板，并且还公开了向空气孔板的气孔供给燃料的燃料喷嘴。 在燃烧器中，气孔板的室侧的中心比最外周气孔的出口更靠近室。
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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
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。
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