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1. 发明申请

US20140102257A1 COPPER ANODE REFINING SYSTEM AND METHOD 审中-公开
标题翻译：铜阳极精炼系统和方法
公开(公告)号：US20140102257A1
公开(公告)日：2014-04-17
申请号：US14109474
申请日：2013-12-17
申请人： David B. George , Arsenio Enriquez , Adrian Christian Denys , William John Mahoney , Ian Francis Masterson , Stephen Manley , Jesse Cates , Kevin Albrecht
发明人： David B. George , Arsenio Enriquez , Adrian Christian Denys , William John Mahoney , Ian Francis Masterson , Stephen Manley , Jesse Cates , Kevin Albrecht
IPC分类号： C22B15/00
CPC分类号： C22B15/006 , C21C5/4606 , C22B9/05 , C22B15/0036 , F23C2900/07022 , F23D14/22 , F23D14/32 , F23D14/56 , Y02P10/212
摘要： A method and system for the copper anode refining is provided in which coherent jet technology is employed to heat the molten blister copper and/or melt scrap copper charges using a melting flame, oxidize the sulfur in the molten blister copper, and reduce the oxygen in the molten blister copper using top-blown coherent jet gas streams from one or more multi-functional, coherent jet lance assemblies. The present system and method employs a microprocessor-based controller operatively controlling the flow of an oxygen-containing gas, an inert gas, a reducing agent and a fuel to the coherent jet lance. The disclosed copper anode refining system and method greatly improves copper production while lowering oxidation /reduction cycle times and minimizing NOx emissions.
摘要翻译：提供了一种用于铜阳极精炼的方法和系统，其中使用相干喷射技术来使用熔融火焰加热熔融的铜泡铜和/或熔融废铜电荷，氧化熔融的铜铜中的硫，并且减少氧气中的氧使用来自一个或多个多功能，相干喷射枪组件的顶吹相干射流气流的熔融起泡铜。本系统和方法采用基于微处理器的控制器，可操作地控制含氧气体，惰性气体，还原剂和燃料到相干射流喷枪的流动。所公开的铜阳极精炼系统和方法极大地改善了铜的生产，同时降低了氧化/还原循环时间并最大限度地减少了NOx排放。

2. 发明授权

US08621870B2 Fuel injection method 有权
标题翻译：燃油喷射法
公开(公告)号：US08621870B2
公开(公告)日：2014-01-07
申请号：US12816112
申请日：2010-06-15
申请人： Richard Carroni , Adnan Eroglu
发明人： Richard Carroni , Adnan Eroglu
IPC分类号： F02C7/22 , F02C7/26
CPC分类号： F23R3/36 , F23C2900/07002 , F23C2900/07021 , F23C2900/07022 , F23C2900/9901 , F23L7/00 , F23R3/286 , F23R3/34 , F23R2900/00002 , F23R2900/03341
摘要： A method is provided for fuel injection in a sequential combustion system comprising a first combustion chamber and downstream thereof a second combustion chamber, in between which at least one vortex generator is located, as well as a premixing chamber having a longitudinal axis downstream of the vortex generator, and a fuel lance having a vertical portion and a horizontal portion, being located within said premixing chamber. The fuel injected is an MBtu-fuel. In said premixing chamber the fuel and a gas contained in an oxidizing stream coming from the first combustion chamber are premixed to a combustible mixture. The fuel is injected in such a way that the residence time of the fuel in the premixing chamber is reduced in comparison with a radial injection of the fuel from the horizontal portion of the fuel lance.
摘要翻译：提供了一种用于在顺序燃烧系统中进行燃料喷射的方法，所述顺序燃烧系统包括第一燃烧室，并且在其下游具有第二燃烧室，其中至少一个涡流发生器位于该第二燃烧室之间，以及具有在涡流下游的纵向轴线的预混合室发电机和具有垂直部分和水平部分的燃料喷枪，位于所述预混合室内。注入的燃料是一种MBtu燃料。在所述预混合室中，燃料和包含在来自第一燃烧室的氧化物流中的气体被预混合到可燃混合物中。与燃料喷枪的水平部分的燃料的径向喷射相比，燃料以这样的方式被喷射，使得燃料在预混合室中的停留时间减小。

3. 发明申请

US20100186417A1 USE OF INERT GASES FOR SHIELDING OXIDIZER AND FUEL 审中-公开
标题翻译：使用用于屏蔽氧化剂和燃料的惰性气体
公开(公告)号：US20100186417A1
公开(公告)日：2010-07-29
申请号：US12665970
申请日：2008-07-03
申请人： Malte Blomeyer , Olga Deiss , Andre Kluge , Thomas Kunadt , Berthold Köstlin , Martin Lenze , Paul Pixner , Uwe Sieber
发明人： Malte Blomeyer , Olga Deiss , Andre Kluge , Thomas Kunadt , Berthold Köstlin , Martin Lenze , Paul Pixner , Uwe Sieber
IPC分类号： F02C7/22 , B05B7/04 , F23D11/38
CPC分类号： F23D11/36 , F23C2900/07022 , F23D14/78 , F23D2214/00 , F23L2900/07002 , F23R3/283
摘要： A method for protecting a burner from being heated excessively during the combustion of a fuel in a combustion chamber is provided. The fuel is injected through a fuel nozzle at the same time as an inert gas in the surroundings of the injected fuel is injected into the combustion chamber in such a manner that the fuel is separated spatially from an oxidizer by the inert gas until an ignitable mixture of the fuel is produced.
摘要翻译：提供一种用于在燃烧室内的燃料燃烧期间保护燃烧器不被过度加热的方法。燃料通过燃料喷嘴喷射，同时惰性气体在注入的燃料的周围注入到燃烧室中，使得燃料在空间上与氧化剂被惰性气体分离直到可点燃的混合物的燃料产生。

4. 发明申请

US20080098994A1 Method and apparatus for isolating inactive fuel passages 有权
标题翻译：用于隔离惰性燃料通道的方法和装置
公开(公告)号：US20080098994A1
公开(公告)日：2008-05-01
申请号：US11978241
申请日：2007-10-26
申请人： Matthew Innes , Walter Omielan , Richard Hamby
发明人： Matthew Innes , Walter Omielan , Richard Hamby
IPC分类号： F02M19/06
CPC分类号： F02C7/22 , F02M21/042 , F05D2260/607 , F23C2900/07022 , F23D2206/10 , F23D2209/30 , F23K2301/203 , F23N5/203 , F23N2027/04 , F23N2027/06 , F23N2037/08 , F23R3/34 , F23R3/36
摘要： One aspect relates to an apparatus having a combustion chamber and a duct in fluid flow communication with the combustion chamber. The apparatus includes at least one opening adapted for delivering a liquid fuel into the duct. The apparatus further includes at least one passage adapted for delivery of a gas upstream of the at least one opening for minimizing the entrance of a fluid other than the gas into the fuel delivery opening.
摘要翻译：一个方面涉及一种具有燃烧室和与燃烧室流体连通的管道的设备。该装置包括适于将液体燃料输送到管道中的至少一个开口。该装置还包括至少一个通道，其适于在至少一个开口的上游输送气体，以最小化除气体之外的流体进入燃料输送口。

5. 发明授权

US09121612B2 System and method for reducing combustion dynamics in a combustor 有权
标题翻译：用于减少燃烧器中的燃烧动力学的系统和方法
公开(公告)号：US09121612B2
公开(公告)日：2015-09-01
申请号：US13409309
申请日：2012-03-01
申请人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
发明人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
IPC分类号： F23R3/28 , F23R3/00 , F02C3/30 , F23R3/54 , F23R3/32 , F23D14/62
CPC分类号： F23R3/286 , F02C3/30 , F23C2900/07022 , F23D14/62 , F23R3/002 , F23R3/32 , F23R3/54 , F23R2900/00013
摘要： A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface axially separated from a downstream surface, and tube bundles extend from the upstream surface through the downstream surface. A divider inside a tube bundle defines a diluent passage that extends axially through the downstream surface, and a diluent supply in fluid communication with the divider provides diluent flow to the diluent passage. A method for reducing combustion dynamics in a combustor includes flowing a fuel through tube bundles, flowing a diluent through a diluent passage inside a tube bundle, wherein the diluent passage extends axially through at least a portion of the end cap into a combustion chamber, and forming a diluent barrier in the combustion chamber between the tube bundle and at least one other adjacent tube bundle.
摘要翻译：用于减少燃烧器中的燃烧动力学的系统包括具有从下游表面轴向分离的上游表面的端盖，并且管束从上游表面延伸穿过下游表面。管束内的分隔器限定了一个沿轴向延伸穿过下游表面的稀释剂通道，与分隔器流体连通的稀释剂供应器提供稀释剂流向稀释剂通道。一种用于减少燃烧动力学的方法，包括使燃料通过管束流动，使稀释剂流过管束内的稀释剂通道，其中稀释剂通道轴向延伸通过端盖的至少一部分进入燃烧室，以及在管束与至少一个其它相邻管束之间的燃烧室中形成稀释剂阻挡层。

6. 发明授权

US08443607B2 Coaxial fuel and air premixer for a gas turbine combustor 失效
标题翻译：用于燃气轮机燃烧器的同轴燃料和空气预混合器
公开(公告)号：US08443607B2
公开(公告)日：2013-05-21
申请号：US12389994
申请日：2009-02-20
申请人： William D. York , Willy S. Ziminsky , Benjamin P. Lacy
发明人： William D. York , Willy S. Ziminsky , Benjamin P. Lacy
IPC分类号： F02C3/22 , F02C7/22
CPC分类号： F23R3/286 , F23C2900/07022 , F23D14/64 , F23L2900/07002 , F23L2900/07009
摘要： An air/fuel premixer comprising a peripheral wall defining a mixing chamber, a nozzle disposed at least partially within the peripheral wall comprising an outer annular wall spaced from the peripheral wall so as to define an outer air passage between the peripheral wall and the outer annular wall, an inner annular wall disposed at least partially within and spaced from the outer annular wall, so as to define an inner air passage, and at least one fuel gas annulus between the outer annular wall and the inner annular wall, the at least one fuel gas annulus defining at least one fuel gas passage, at least one air inlet for introducing air through the inner air passage and the outer air passage to the mixing chamber, and at least one fuel inlet for injecting fuel through the fuel gas passage to the mixing chamber to form an air/fuel mixture.
摘要翻译：一种空气/燃料预混合器，其包括限定混合室的外围壁，至少部分地设置在所述周壁内的喷嘴，其包括与所述周壁隔开的外环形壁，以便在所述周壁和外环之间限定外部空气通道壁，内环形壁，其至少部分地设置在外环形壁内并与外环壁相隔开，以便限定内空气通道，以及在外环形壁与内环形壁之间的至少一个燃料气体环，至少一个限定至少一个燃料气体通道的燃料气体环，用于将空气通过内部空气通道引导空气的至少一个空气入口和到混合室的外部空气通道，以及至少一个燃料入口，用于通过燃料气体通道将燃料喷射到混合室以形成空气/燃料混合物。

7. 发明申请

US20120080022A1 MULTI STAGE COMBUSTION FURNACE AND PROCESS FOR THE THERMAL EXPANSION OF MINERAL PARTICLES 有权
标题翻译：多级燃烧炉和矿物颗粒热膨胀过程
公开(公告)号：US20120080022A1
公开(公告)日：2012-04-05
申请号：US13253411
申请日：2011-10-05
申请人： Michael SPINO
发明人： Michael SPINO
IPC分类号： F24C1/00
CPC分类号： F23C99/005 , F23C5/08 , F23C7/02 , F23C7/06 , F23C2900/07022 , Y02E20/348
摘要： The present document describes a multistages combustion furnace system for thermal expansion of mineral particles which comprises: a furnace having an expansion chamber for receiving the mineral particles; a burner head to be connected at a distance for an atmospheric coupling of the furnace and for operating the multistages combustion furnace system; a furnace device to be connected at a distance for an atmospheric coupling of the burner head to offset the quenching effect of ambient air normally drawn in the furnace; and a tuyere for thermal expansion of mineral particles to be connected between the expansion chamber and the furnace device; wherein the multistage combustion furnace system is to be connected with an inlet of preheated air.
摘要翻译：本文件描述了一种用于矿物颗粒热膨胀的多级燃烧炉系统，其包括：具有用于接收矿物颗粒的膨胀室的炉; 燃烧器头连接一段距离，用于炉的大气耦合和操作多级燃烧炉系统; 要连接燃烧器头的大气耦合的一段距离的炉装置，以抵消通常在炉中吸入的环境空气的淬火作用; 以及用于在膨胀室和炉装置之间连接的矿物颗粒的热膨胀的风口; 其中多级燃烧炉系统与预热空气入口连接。

8. 发明申请

US20100281876A1 FUEL BLANKETING BY INERT GAS OR LESS REACTIVE FUEL LAYER TO PREVENT FLAME HOLDING IN PREMIXERS 审中-公开
标题翻译：燃油通过惰性气体或无反应性燃料层进行燃烧以预防火焰燃烧
公开(公告)号：US20100281876A1
公开(公告)日：2010-11-11
申请号：US12435651
申请日：2009-05-05
申请人： Abdul Rafey Khan , Balachandar Varatharajan , Gilbert Otto Kraemer , Ertan Yilmaz , Benjamin Lacy , William David York
发明人： Abdul Rafey Khan , Balachandar Varatharajan , Gilbert Otto Kraemer , Ertan Yilmaz , Benjamin Lacy , William David York
IPC分类号： F02C7/22 , F02C3/20
CPC分类号： F23R3/286 , F23C2900/07022 , F23L2900/07002 , F23L2900/07009
摘要： A premixer for a gas turbine combustor includes a first passage configured to inject a highly reactive fuel; and a second passage configured to inject an inert gas or a less reactive fuel or a mixture of both. The second passage is configured to form a layer of the inert gas or less reactive fuel or the mixture of both that blankets a layer of the highly reactive fuel. Another premixer includes a plurality of nozzles, each nozzle including a pair of concentric tubes, the pair of concentric tubes including a first tube configured to inject a highly reactive fuel and a second tube surrounding the first tube and configured to dispense an inert gas or a less reactive fuel or a mixture of both that blankets the highly reactive fuel.
摘要翻译：燃气轮机燃烧器的预混合器包括：第一通道，其构造成喷射高反应性燃料; 以及构造成喷射惰性气体或较少反应性燃料或二者的混合物的第二通道。第二通道被配置成形成一层惰性气体或较少的反应性燃料或两者的混合物，这些层覆盖高反应性燃料层。另一个预混合器包括多个喷嘴，每个喷嘴包括一对同心管，该对同心管包括构造成喷射高反应性燃料的第一管和围绕第一管的第二管，并且构造成分配惰性气体或较少的反应性燃料或两者的混合物，其覆盖高反应性燃料。

9. 发明申请

US20070289305A1 Fuel spraying apparatus of gas turbine engine 有权
标题翻译：燃气轮机发动机喷油装置
公开(公告)号：US20070289305A1
公开(公告)日：2007-12-20
申请号：US11637060
申请日：2006-12-12
申请人： Takeo Oda , Hiroyuki Ninomiya , Hideki Ogata
发明人： Takeo Oda , Hiroyuki Ninomiya , Hideki Ogata
IPC分类号： F23R3/14
CPC分类号： F23R3/14 , F23C2900/07022 , F23D11/383 , F23D2900/00008 , F23D2900/11101 , F23R3/283 , F23R3/286 , F23R3/343 , F23R2900/00017 , F23R2900/00019 , Y02T50/675
摘要： A fuel spraying apparatus of a gas turbine engine includes a first fuel spraying section configured to spray fuel for diffusion combustion and a second fuel spraying section configured to spray fuel for premixed combustion. The second fuel spraying section is disposed so as to surround the first fuel spraying section. The apparatus further includes an air curtain generating section disposed between the first fuel spraying section and the second fuel spraying section. The air curtain generating section configured to generate an air curtain which defines an outer edge of a diffusion combustion area in a combustion chamber.
摘要翻译：燃气涡轮发动机的燃料喷射装置包括构造成喷射用于扩散燃烧的燃料的第一燃料喷射部和被配置为喷射用于预混燃烧的燃料的第二燃料喷射部。第二燃料喷射部设置成围绕第一燃料喷射部。该装置还包括设置在第一燃料喷射部分和第二燃料喷射部分之间的气帘产生部分。所述气帘产生部构造成产生限定燃烧室内的扩散燃烧区域的外缘的气帘。

10. 发明授权

US5370529A Low NO.sub.x combustion system for fuel-fired heating appliances 失效
标题翻译：燃油加热设备的低NOx燃烧系统
公开(公告)号：US5370529A
公开(公告)日：1994-12-06
申请号：US111297
申请日：1993-08-24
申请人： Lin-Tao Lu , Larry R. Mullens , Keith M. Grahl
发明人： Lin-Tao Lu , Larry R. Mullens , Keith M. Grahl
IPC分类号： F23D14/70 , F24H3/06 , F23D14/62 , F24H9/00
CPC分类号： F24H3/065 , F23D14/70 , F23C2900/07022
摘要： A fuel-fired, forced air draft induced heating furnace is provided with NO.sub.x reduction apparatus associated with a plurality of combustor tubes forming a portion of its heat exchanger structure. In-shot type fuel burners are spaced apart from and face the open inlet ends of horizontal combustion sections of the combustor tubes. The NO.sub.x reduction apparatus includes a plurality of metal mesh tubes having diameters substantially less than the internal diameters of the combustion tubes. The mesh tubes are coaxially supported within the combustor tubes, adjacent their inlet ends, by elongated support members longitudinally passing through the mesh tubes and having first ends anchored to the combustor tube inlet ends, and second ends slidably resting on internal side surface portions of the combustor tubes. During burner operation the burner flames injected into the combustor tubes are forced through the mesh tubes which operate to laterally reduce the cross-sections of the flames, increase their axial velocity through the combustor tubes, and substantially diminish the intimate contact of secondary combustion with the maximum temperature zones of the flames within the combustor tubes.
摘要翻译：燃料燃烧的强制通风引风加热炉设置有与形成其热交换器结构的一部分的多个燃烧器管相关联的NOx还原装置。喷射型燃料燃烧器与燃烧器管的水平燃烧部分的开放入口端相隔开并面对。 NOx还原装置包括多个金属网管，其直径基本上小于燃烧管的内径。网管连接在燃烧器管内，靠近其入口端，细长的支撑件纵向通过网管并具有固定到燃烧器管入口端的第一端，第二端可滑动地搁置在燃烧器管的内侧表面部分上燃烧器管。在燃烧器操作期间，喷射到燃烧器管中的燃烧器火焰被迫通过网管，其操作以横向地减小火焰的横截面，增加其通过燃烧器管的轴向速度，并且基本上减少二次燃烧与燃烧器管内火焰的最高温度区。

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