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31. 发明授权

US06609905B2 Catalytic burner 有权
标题翻译：催化燃烧器
公开(公告)号：US06609905B2
公开(公告)日：2003-08-26
申请号：US10132478
申请日：2002-04-26
申请人： Adnan Eroglu , Timothy Griffin , Jaan Hellat
发明人： Adnan Eroglu , Timothy Griffin , Jaan Hellat
IPC分类号： F23M300
CPC分类号： F23R3/36 , F23D2900/00008 , F23D2900/14004 , F23N2037/12 , F23R3/286 , F23R3/34 , F23R3/346 , F23R3/40
摘要： The invention relates to a catalytic burner (1) of a combuster (2), in particular of a power station installation, comprising an annular duct (4) leading to the combuster (2), a catalyzer (5) arranged in the annular duct (4), a primary injection device (7) for injecting a fuel into the annular duct (4) upstream of the catalyzer (5), a secondary injection device (3) for directly injecting a fuel into the combuster (2). To stabilize a recirculation zone (29) in the combuster (2), a swirl generation device (6) is provided, which is arranged in the annular duct (4) downstream of the catalyzer (5) and subjects a flow through the catalyzer (5) to a swirl.
摘要翻译：本发明涉及燃烧器（2）的催化燃烧器（1），特别是在电站设备中，包括通向燃烧器（2）的环形管道（4），设置在环形管道中的催化剂（5） 4），用于将燃料喷射到催化器（5）上游的环形管道（4）中的主注射装置（7），用于将燃料直接喷射到燃烧器（2）中的二次注射装置（3）。为了稳定在燃烧器（2）中的再循环区（29），设置有涡流发生装置（6），其设置在催化器（5）下游的环形管道（4）中并使流过催化剂（5）到漩涡

32. 发明授权

US5487659A Fuel lance for liquid and/or gaseous fuels and method for operation thereof 失效
标题翻译：用于液体和/或气体燃料的燃料喷枪及其操作方法
公开(公告)号：US5487659A
公开(公告)日：1996-01-30
申请号：US262454
申请日：1994-06-20
申请人： Adnan Eroglu , Franz Joos , Peter Novacek , Peter Senior
发明人： Adnan Eroglu , Franz Joos , Peter Novacek , Peter Senior
IPC分类号： B05B1/00 , F23D11/10 , F23D14/22 , F23D14/78 , F23D17/00 , F23D14/46
CPC分类号： F23D11/101 , F23D14/22 , F23D14/78 , F23D17/002
摘要： A fuel lance for liquid and/or gaseous fuels for use in a combustion chamber includes a liquid fuel pipe extending along a lance center line and defining a liquid fuel passage, a gas pipe surrounding the liquid fuel pipe and forming therebetween a gas passage, and a lance outer shell surrounding the gas pipe and forming an air passage around the gas pipe for cooling air and atomizer air. At least one air/fuel nozzle is provided in a peripheral side of the lance outer shell at a downstream end of the fuel lance for air flow out of the air passage into the combustion chamber. At least one gas nozzle is provided in the gas pipe for gas flow out of the gas passage into the air passage, the gas nozzle is positioned relative to the air/fuel nozzle so that gas from the gas nozzle flows with air from the air passage through the at least one air/fuel nozzle into the combustion chamber. At least one liquid fuel nozzle is provided in the liquid fuel pipe for liquid fuel flow out of the liquid fuel passage, the liquid fuel nozzle being positioned relative to the gas nozzle and air/fuel nozzle so that liquid fuel from the liquid fuel nozzle flows through the air passage and, with the air, through the air/fuel nozzle into the combustion chamber.
摘要翻译：用于在燃烧室中使用的用于液体和/或气体燃料的燃料喷枪包括沿喷枪中心线延伸并限定液体燃料通道的液体燃料管，围绕液体燃料管的气体管，并在其间形成气体通道;以及围绕气体管道的喷枪外壳，并且在气体管道周围形成用于冷却空气和雾化器空气的空气通道。至少一个空气/燃料喷嘴在燃料喷枪的下游端设置在喷枪外壳的周边，用于从进入燃烧室的空气通道中流出。在气体管道中设置至少一个气体喷嘴，用于气体从气体通道流入空气通道中，气体喷嘴相对于空气/燃料喷嘴定位，使得来自气体喷嘴的气体与来自空气通道的空气一起流动通过至少一个空气/燃料喷嘴进入燃烧室。在液体燃料管中设置至少一个液体燃料喷嘴，用于液体燃料流出液体燃料通道，液体燃料喷嘴相对于气体喷嘴和空气/燃料喷嘴定位，使得来自液体燃料喷嘴的液体燃料流动通过空气通道和空气通过空气/燃料喷嘴进入燃烧室。

33. 发明授权

US5423608A Mixing apparatus with vortex generating devices 失效
标题翻译：具有涡流发生装置的混合装置
公开(公告)号：US5423608A
公开(公告)日：1995-06-13
申请号：US225395
申请日：1994-04-08
申请人： Yau-Pin Chyou , Adnan Eroglu
发明人： Yau-Pin Chyou , Adnan Eroglu
IPC分类号： B01F5/00 , B01F5/06
CPC分类号： B01F5/061 , B01F2005/0621 , B01F2005/0622 , B01F2005/0623
摘要： A mixing apparatus for mixing two or more materials, includes a separating plate Upstream of a mixing zone having a plurality of vortex generators attached to the plate to create large scale longitudinal vortices in the materials as they pass the plate for rapid, controlled mixing in a short longitudinal distance. The vortex generators are arranged in a row transverse to the flow direction of the materials. The vortex generators each comprise three triangular-shaped surfaces joined to form a three sided wedge having a top surface and opposite sides surfaces that project into the flow path. The side surfaces are joined at an acute angle. The top surface is oriented at an angle to the plate. The angles may be adjusted for the type of materials to be mixed.
摘要翻译：用于混合两种或更多种材料的混合设备包括分离板上游的混合区域，其具有附接到板上的多个涡流发生器，以在材料通过该板时在材料中产生大尺度的纵向涡流，用于快速，受控混合短纵向距离。涡流发生器横向于材料的流动方向排列成一排。涡流发生器各自包括三个三角形表面，三个三角形表面被连接以形成三面楔形件，其具有突出到流动路径中的顶表面和相对的侧面。侧面以锐角连接。顶表面与板成一角度定向。可以根据要混合的材料的类型调整角度。

34. 发明授权

US09057518B2 Reheat burner 有权
标题翻译：再热燃烧器
公开(公告)号：US09057518B2
公开(公告)日：2015-06-16
申请号：US13195993
申请日：2011-08-02
申请人： Johannes Buss , Andrea Ciani , Adnan Eroglu , Urs Benz , Michael Düsing , Michael Hutapea
发明人： Johannes Buss , Andrea Ciani , Adnan Eroglu , Urs Benz , Michael Düsing , Michael Hutapea
IPC分类号： F23R3/00 , F23D11/40 , F23R3/12 , F23D14/64 , F23R3/20
CPC分类号： F23D11/402 , F23D11/408 , F23D14/64 , F23R3/002 , F23R3/12 , F23R3/20 , F23R2900/03341
摘要： A reheat burner (1) includes a channel (2) with a lance (3) protruding thereinto to inject a fuel over an injection plane (4) perpendicular to a channel longitudinal axis (15). The channel (2) and lance (3) define a vortex generation zone (6) upstream of the injection plane (4) and a mixing zone (9) downstream of the injection plane (4) in the hot gas (G) direction. The mixing zone (9) includes a high speed area (16) with a constant cross section, and a diffusion area (17) with a flared cross section downstream of the high speed area (16) in the hot gas (G) direction.
摘要翻译：再热燃烧器（1）包括具有突出于其中的喷枪（3）的通道（2），以在垂直于通道纵向轴线（15）的喷射平面（4）上喷射燃料。通道（2）和喷枪（3）在喷射平面（4）的上游限定涡流产生区（6），在热气（G）方向上限定喷射平面（4）下游的混合区（9）。混合区（9）包括具有恒定横截面的高速区域（16）和在热气体（G）方向上在高速区域（16）下游具有扩口横截面的扩散区域）。

35. 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。

36. 发明授权

US08468833B2 Burner arrangement, and use of such a burner arrangement 有权
标题翻译：燃烧器布置和使用这种燃烧器布置
公开(公告)号：US08468833B2
公开(公告)日：2013-06-25
申请号：US12876310
申请日：2010-09-07
申请人： Richard Carroni , Marcel Rieker , Adnan Eroglu , Heinz Schaer
发明人： Richard Carroni , Marcel Rieker , Adnan Eroglu , Heinz Schaer
IPC分类号： F23D11/40
CPC分类号： F23D14/02 , F23C7/002 , F23C2900/07002 , F23D14/82 , F23R3/286
摘要： A burner arrangement includes a tubular mixing tube extending along an axis and configured to mix fuel and air, the mixing tube opening into a combustion chamber in a direction of flow; and a film air ring disposed in the mixing tube and arranged concentrically to the axis, the film air ring configured to prevent a backfiring of the fuel disposed in the mixing tube and to generate or reinforce an air film near the wall, wherein the film air ring has at least one annular gap concentric to the axis and configured to inject air.
摘要翻译：燃烧器装置包括：管状混合管，其沿着轴线延伸并且构造成将燃料和空气混合，所述混合管开口沿着流动方向进入燃烧室; 以及薄膜空气环，其设置在所述混合管中并且与所述轴线同心地布置，所述薄膜空气环被配置为防止设置在所述混合管中的燃料的后燃并且产生或加强靠近所述壁的空气膜，其中所述薄膜空气环具有与轴同心的至少一个环形间隙，并且构造成喷射空气。

37. 发明授权

US08434312B2 Gas turbine with improved part load emissions behavior 有权
标题翻译：燃气轮机具有改进的部件负荷排放行为
公开(公告)号：US08434312B2
公开(公告)日：2013-05-07
申请号：US13241983
申请日：2011-09-23
申请人： Adnan Eroglu , Klaus Knapp , Peter Flohr , Hans Peter Knöpfel , Weiqun Geng
发明人： Adnan Eroglu , Klaus Knapp , Peter Flohr , Hans Peter Knöpfel , Weiqun Geng
IPC分类号： F02C7/228
CPC分类号： F02C9/26 , F02C6/003 , F23C6/042 , F23N1/022 , F23N2037/02 , F23N2041/20 , F23R7/00 , F23R2900/03341 , Y02E20/16
摘要： In a method for the low-CO emissions part load operation of a gas turbine with sequential combustion, the air ratio (λ) of the operative burners (9) of the second combustor (15) is kept below a maximum air ratio (λmax) at part load In order to reduce the maximum air ratio (λ), a series of modifications in the operating concept of the gas turbine are carried out individually or in combination. One modification is an opening of the row of variable compressor inlet guide vanes (14) before engaging the second combustor (15). For engaging the second combustor, the row of variable compressor inlet guide vanes (14) is quickly closed and fuel is introduced in a synchronized manner into the burner (9) of the second combustor (15). A further modification is the deactivating of individual burners (9) at part load.
摘要翻译：在具有顺序燃烧的燃气轮机的低CO排放部分负荷操作的方法中，第二燃烧器（15）的操作燃烧器（9）的空气比（λ）保持在最大空气比（lambdamax）以下）在部分负载下为了降低最大空气比（lambda），对燃气轮机的操作概念进行一系列修改，可单独进行或组合进行。一个变型是在接合第二燃烧器（15）之前的一排可变压缩机入口导叶（14）的开口。为了接合第二燃烧器，可变压缩机入口导叶（14）的排被快速关闭，燃料以同步的方式被引入第二燃烧器（15）的燃烧器（9）。进一步的修改是在部分负载下单个燃烧器（9）的停用。

38. 发明授权

US08375723B2 Method for operating a gas turbine 有权
标题翻译：操作燃气轮机的方法
公开(公告)号：US08375723B2
公开(公告)日：2013-02-19
申请号：US12471665
申请日：2009-05-26
申请人： Eribert Benz , Peter Flohr , Adnan Eroglu , Felix Guethe , Jaan Hellat
发明人： Eribert Benz , Peter Flohr , Adnan Eroglu , Felix Guethe , Jaan Hellat
IPC分类号： F02C6/00 , F02C1/00
CPC分类号： F02C6/003 , C10J3/00 , C10J2300/093 , C10J2300/0959 , C10J2300/1606 , C10J2300/165 , C10J2300/1671 , C10J2300/1675 , C10J2300/1678 , C10J2300/1892 , F02C3/28 , F25J3/04545 , F25J3/04575 , Y02E20/16 , Y02E20/18
摘要： In method for operating a gas turbine (11), the compressed air is fed to a combustor (18, 19) for the combustion of a coal syngas, and the resulting hot gases are expanded in a subsequent turbine (16, 17). Some of the compressed air is separated into oxygen and nitrogen, and the oxygen is used for producing the syngas. In a first combustor, (18) syngas is combusted and the resulting hot gases are expanded in a first turbine (16), and in a second combustor syngas is combusted, using the gases which issue from the first turbine (16), and the resulting hot gases are expanded in the second turbine (17). The two combustors (18, 19) are operated with undiluted syngas, and the first combustor flame temperature (TF) is lowered compared with the operation with natural gas (TNG), while the second combustor (19) is operated in the normal operation (TNG) for natural gas.
摘要翻译：在用于操作燃气轮机（11）的方法中，压缩空气被供给到用于燃烧煤合成气的燃烧器（18,19），并且所得热气体在随后的涡轮机（16,17）中膨胀。一些压缩空气被分离成氧气和氮气，氧气用于生产合成气。在第一燃烧器中，（18）合成气被燃烧，并且所得到的热气体在第一涡轮机（16）中膨胀，并且在第二燃烧器中使用从第一涡轮机（16）发出的气体燃烧合成气，所产生的热气体在第二涡轮机（17）中膨胀。两个燃烧器（18,19）与未稀释的合成气一起操作，并且与天然气（TNG）的操作相比，第一燃烧器火焰温度（TF）降低，而第二燃烧器（19）在正常操作中操作天然气）。

39. 发明授权

US07908842B2 Method for operating a gas turbine, method of operation of a combined cycle power plant, and combined cycle power plant 有权
标题翻译：操作燃气轮机的方法，联合循环发电厂的操作方法和联合循环发电厂
公开(公告)号：US07908842B2
公开(公告)日：2011-03-22
申请号：US12326519
申请日：2008-12-02
申请人： Adnan Eroglu , Jaan Hellat , Felix Guethe , Peter Flohr
发明人： Adnan Eroglu , Jaan Hellat , Felix Guethe , Peter Flohr
IPC分类号： F02C1/06 , F02C6/00
CPC分类号： F01K23/10 , F02C3/28 , F02C6/18 , F02C7/26 , F02C9/42 , Y02E20/16 , Y02E20/18
摘要： In a method for operating a gas turbine (GT) with sequential combustion, which has at least one compressor (12, 13), a first combustion chamber (14) with a first turbine (15) which is connected downstream, and a second combustion chamber (16) with a second turbine (17) which is connected downstream, the at least one compressor (12, 13) draws in air and compresses it. The compressed air is fed to the first combustion chamber (14) for combusting a first fuel, and the gas which issues from the first turbine (15) is fed to the second combustion chamber (16) for combusting a second fuel. Increased flexibility and safety in operation is achieved by different fuels being used as first and second fuel.
摘要翻译：在具有顺序燃烧的具有至少一个压缩机（12,13）的燃气轮机（GT）的操作方法中，具有连接在下游的第一涡轮（15）的第一燃烧室（14）和第二燃烧（16）与第二涡轮机（17）连接，所述第二涡轮机（17）连接在下游，所述至少一个压缩机（12,13）吸入空气并将其压缩。压缩空气被供给到第一燃烧室（14），用于燃烧第一燃料，并且从第一涡轮机（15）发出的气体被供给到用于燃烧第二燃料的第二燃烧室（16）。通过使用不同燃料作为第一和第二燃料来实现操作中增加的灵活性和安全性。

40. 发明申请

US20100330282A1 SLURRY FORMULATION FOR THE PRODUCTION OF THERMAL BARRIER COATINGS 有权
标题翻译：用于生产热障涂层的浆液配方
公开(公告)号：US20100330282A1
公开(公告)日：2010-12-30
申请号：US12826798
申请日：2010-06-30
申请人： Hans-Christoph Nienburg , Adnan Eroglu , Hartmut Haehnle
发明人： Hans-Christoph Nienburg , Adnan Eroglu , Hartmut Haehnle
IPC分类号： B05D3/12 , C04B35/16 , B05D3/02
CPC分类号： C04B35/486 , C04B35/04 , C04B35/62222 , C04B35/6316 , C04B2235/3201 , C04B2235/3225 , C04B2235/3418 , C04B2235/36 , C23C24/08 , C23C24/082 , Y10T428/249954
摘要： A slurry formulation for production of a patch or a strip of a thermal barrier coating includes 20-60 dry weight percent of alkali metal silicate binder, 40-80 dry weight percent of ceramic fillers including at least one ceramic filler selected from the group consisting of yttria-stabilized zirconia and magnesia, 0-20 dry weight percent of additives, wherein the dry weight percent of the alkali metal silicate binder, the ceramic fillers and the additives add up to 100%, and one of a solvent and suspension agent.
摘要翻译：用于生产隔热涂层的贴剂或条带的浆料制剂包括20-60干重的碱金属硅酸盐粘合剂，40-80重量％的陶瓷填料，其包括至少一种选自以下的陶瓷填料：氧化钇稳定的氧化锆和氧化镁，0-20重量％的添加剂，其中碱金属硅酸盐粘合剂，陶瓷填料和添加剂的干重百分比加起来为100％，以及溶剂和悬浮剂之一。

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