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41. 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。

42. 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。

43. 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。

44. 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。

45. 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）。

46. 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。

47. 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。

48. 发明申请

US20100175382A1 GAS TURBINE BURNER 有权
标题翻译：燃气涡轮燃烧器
公开(公告)号：US20100175382A1
公开(公告)日：2010-07-15
申请号：US12684187
申请日：2010-01-08
申请人： Adnan Eroglu
发明人： Adnan Eroglu
IPC分类号： F02C7/22
CPC分类号： F23R3/34 , F23C6/047 , F23C2900/07002 , F23C2900/07021 , F23D11/105 , F23D11/12 , F23D11/402 , F23D14/58 , F23D14/64 , F23D17/002 , F23D2900/00015 , F23D2900/11101 , F23R3/12 , F23R3/286 , F23R3/343 , F23R3/346 , F23R3/36 , F23R2900/03341
摘要： The burner (1) of a gas turbine includes a swirl generator (2) and, downstream of it, a mixing tube (3). The swirl generator (2) is defined by at least two walls facing one another to define a conical swirl chamber (5) and is provided with nozzles (6) arranged to inject a fuel and apertures (7) arranged to feed an oxidiser into the swirl chamber (5). The burner (1) includes a lance (9) which extends along a longitudinal axis of the swirl generator (2) and is provided with side nozzles (11) for ejecting a fuel within the burner (1). The side nozzles (11) have their axes (12) inclined with respect to the axis of the lance (9) and can be positioned along the axis of the burner.
摘要翻译：燃气轮机的燃烧器（1）包括涡流发生器（2），并在其下游设置有混合管（3）。漩涡发生器（2）由至少两个彼此面对的壁限定，以限定锥形旋流室（5），并且设置有喷嘴（6），该喷嘴布置成喷射燃料和孔（7），其布置成将氧化剂进料到旋流室（5）。燃烧器（1）包括沿着涡流发生器（2）的纵向轴线延伸的喷枪（9），并且设置有用于在燃烧器（1）内喷射燃料的侧喷嘴（11）。侧喷嘴（11）具有相对于喷枪（9）的轴线倾斜的轴线（12），并且可以沿着燃烧器的轴线定位。

49. 发明申请

US20080115497A1 Premix Burner for a Gas Turbine Combustion Chamber 有权
标题翻译：燃气轮机燃烧室预混燃烧器
公开(公告)号：US20080115497A1
公开(公告)日：2008-05-22
申请号：US11860581
申请日：2007-09-25
申请人： Adnan Eroglu , Majed Toqan
发明人： Adnan Eroglu , Majed Toqan
IPC分类号： F02C1/00 , F23C1/08 , F23C5/00 , F23D11/40
CPC分类号： F23D17/002 , F23C7/002 , F23R3/286
摘要： A burner (1) for a combustion chamber of a gas turbine, especially in a power plant, includes an oxidator feed device (10) for feeding a gaseous oxidator into a mixer chamber (3) of the burner (1), a gaseous fuel feed device (11) for feeding a gaseous fuel into the mixer chamber (3), and a liquid fuel feed device (12) for feeding a liquid fuel into the mixer chamber (3). In order to improve the operation of the burner (1) with liquid fuel, the liquid fuel feed device (12) has a main feed line (13) which feeds liquid fuel to a plurality of injection orifices (14). Some of these injection orifices (14), with regard to a main outflow direction (9) of the burner (1), which has an oxidator-fuel mixture, which flows from the mixer chamber (3), at an outlet opening (5) of the mixer chamber (3), are arranged in series. Some or all of these injection orifices (14) are designed so that a main injection direction (15) of the respective injection orifice (14) has a radial component which extends radially to the main outflow direction (9).
摘要翻译：一种用于燃气轮机的燃烧室的燃烧器（1），特别是在动力装置中，包括用于将气态氧化剂进料到燃烧器（1）的混合室（3）中的氧化剂进料装置（10）用于将气体燃料供给到混合室（3）中的进料装置（11）和用于将液体燃料供给到混合室（3）中的液体燃料供给装置（12）。为了通过液体燃料来改善燃烧器（1）的操作，液体燃料供给装置（12）具有向多个喷射孔（14）供给液体燃料的主供给管线（13）。关于燃料器（1）的主要流出方向（9），其中一些喷射孔（14）具有从混合室（3）流出的氧化剂 - 燃料混合物的出口（5））混合室（3）串联布置。这些注入口（14）中的一些或全部被设计成使得各个喷射孔（14）的主喷射方向（15）具有径向分量，其径向延伸到主流出方向（9）。

50. 发明申请

US20050175948A1 Burner with staged fuel injection 有权
标题翻译：燃烧器分阶段燃油喷射
公开(公告)号：US20050175948A1
公开(公告)日：2005-08-11
申请号：US11006809
申请日：2004-12-08
申请人： Douglas Pennell , Adnan Eroglu
发明人： Douglas Pennell , Adnan Eroglu
IPC分类号： F23D11/12 , F23D14/22 , F23R3/12 , F23R3/28 , F23R3/34 , F23D14/46
CPC分类号： F23R3/286 , F23R3/12
摘要： A burner with staged fuel injection includes at least two separate stages (4a, 4b) for fuel injection arranged along the swirl body (1). The burner is distinguished in that, between the first and the second stage (4a, 4b), a separating element (8) is provided, which extends in the direction of the combustion chamber (3) and separates the combustion air flow which enters in the region of the first stage (4a) from the combustion air flow which enters in the region of the second stage (4b). The burner can be operated with low combustion pulsations even in the case of low burner powers.
摘要翻译：具有分级燃料喷射的燃烧器包括沿着涡流体（1）布置的用于燃料喷射的至少两个分离的台阶（4a，4b）。燃烧器的特征在于，在第一和第二阶段（4a，4b）之间，设置有分离元件（8），其沿着燃烧室（3）的方向延伸并分离燃烧空气流从进入第二级（4b）的区域的燃烧空气流进入第一级（4a）的区域。即使在低燃烧器功率的情况下，燃烧器也可以以低燃烧脉动操作。

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