公开(公告)号：US06216644B1

公开(公告)日：2001-04-17

申请号：US09431179

申请日：1999-11-01

申请人： Adnan Eroglu ,  Franz Joos ,  Bettina Paikert ,  Cristian Oliver Paschereit ,  Jakob J. Keller

发明人： Adnan Eroglu ,  Franz Joos ,  Bettina Paikert ,  Cristian Oliver Paschereit ,  Jakob J. Keller

IPC分类号： F15D5504

CPC分类号： F15D1/0045 ,  F15D1/06 ,  F23D2209/20 ,  F23R3/045 ,  F23R2900/00014

摘要： In heat generators and burners, it is frequently necessary to realize discontinuous cross-sectional expansions of a flow duct. When the flow (U) passes over the step (10) formed in the wall (8) of the flow duct, coherent lateral separation vortices form which are propagated almost undamped downstream of the step and frequently represent the cause of thermo-acoustic vibrations of high amplitude. In accordance with the invention, vortex-generating elements (20) with a lateral pitch dimension (t) are arranged on a line transverse to the main flow (U) a distance (s) upstream of the step (10). Given an expedient selection of the pitch dimension (t), the lateral coherence of the separation vortex is enduringly destroyed.

摘要翻译： 在发热体和燃烧器中，通常需要实现流路的不连续的横截面扩展。 当流动（U）通过形成在流动管道的壁（8）中的台阶（10）时，形成相干侧向分离涡流，其在步骤的下游几乎无阻尼地传播，并且经常表示热声振动的原因 高振幅。 根据本发明，具有横向间距尺寸（t）的涡流产生元件（20）在横向于主流（U）的线上布置在步骤（10）上游的距离（s）处。 考虑到桨距尺寸（t）的适当选择，分离涡流的横向相干性被持续地破坏。

公开(公告)号：US06572366B2

公开(公告)日：2003-06-03

申请号：US10145044

申请日：2002-05-15

申请人： Adnan Eroglu ,  Klaus Knapp ,  Bettina Paikert

发明人： Adnan Eroglu ,  Klaus Knapp ,  Bettina Paikert

IPC分类号： F23D1446

CPC分类号： F23C7/002 ,  F23C2900/07002 ,  F23D11/402 ,  F23D14/70 ,  F23D17/002 ,  F23D2210/00 ,  F23R2900/03341

摘要： What is described is a burner system with a premix burner (1), in which is provided at least one vortex generator (2), through which passes an air-containing gaseous main flow (ZL) which flows axially through the premix burner (1) and into which gaseous and/or liquid fuel is injected, downstream of the vortex generator (2), as a secondary flow for generating a fuel/air mixture, and with a combustion chamber (5) which adjoins the premix burner (1) downstream of the latter and has a combustion chamber cross section (C2) which is larger than the flow cross section (C1), delimited by the premix burner (1), directly upstream of the combustion chamber (5). The invention is distinguished in that, between the premix burner (1) and the combustion chamber (5), a flow duct (10) is provided, delimited by side walls which create a gradual transition between the flow cross section (C1) and the combustion chamber cross section (C2), and in that upstream, within and/or downstream of the flow duct (10) is provided at least one flow stall structure (11), by means of which the fuel/air mixture passing through the flow duct (10) is separated locally from the side wall of the flow duct (10).

公开(公告)号：US06672863B2

公开(公告)日：2004-01-06

申请号：US10145780

申请日：2002-05-16

申请人： Klaus Doebbeling ,  Bettina Paikert ,  Christian Oliver Paschereit

发明人： Klaus Doebbeling ,  Bettina Paikert ,  Christian Oliver Paschereit

IPC分类号： F23D1446

CPC分类号： F23C9/00 ,  F23C7/002 ,  F23C2900/07002 ,  F23D11/402 ,  F23D17/002

摘要： In a premixing burner (1) for a gas turbine or hot-gas generation for the combustion of liquid or gaseous fuel, in which fuel is mixed with combustion air (9a, 9b) in a burner interior (14), is fed to a combustion chamber (3) and is burnt in this combustion chamber (3), stabilization in the part-load model is achieved in a simple and efficient way in that means (15) are provided which make it possible to recirculate hot exhaust gas (17) out of the combustion chamber (3) into the burner interior (14) and to stabilize the flame by means of selfignition processes. The means (15) are preferably a recirculation line which picks up hot exhaust gas (17) from the outer backflow zone (10) and feeds it to the burner interior (14) in the region of a burner tip (2) facing away from the combustion chamber (3), additional fuel (pilot fuel 21) being admixed with the exhaust gas (17) in the recirculation line upstream of the feed to the burner interior (14).

摘要翻译： 在用于燃气轮机或用于燃烧液体或气体燃料的燃气的预混合燃烧器（1）中，其中燃料与燃烧器内部（14）中的燃烧空气（9a，9b）混合，被供给到 燃烧室（3），并且在该燃烧室（3）中燃烧，部件负荷模型中的稳定性以简单有效的方式实现，因为提供了使得可以再循环热废气（17）的装置（15） ）从燃烧室（3）进入燃烧器内部（14）并通过自燃过程来稳定火焰。 装置（15）优选地是从外部回流区（10）拾取热废气（17）并在燃烧器尖端（2）的远离燃烧器端部（2）的区域中将其供给到燃烧器内部（14）的再循环管线。 燃烧室（3），附加燃料（引燃燃料21）与在燃烧器内部（14）的进料上游的再循环管线中的废气（17）混合。

公开(公告)号：US06277340B1

公开(公告)日：2001-08-21

申请号：US09002539

申请日：1998-01-02

申请人： Bettina Paikert ,  Jonathan Lloyd ,  Timothy Albert Griffin

发明人： Bettina Paikert ,  Jonathan Lloyd ,  Timothy Albert Griffin

IPC分类号： B01J802

CPC分类号： B01J19/32 ,  B01J2219/3221 ,  B01J2219/32213 ,  B01J2219/32227 ,  B01J2219/32237 ,  B01J2219/32248 ,  B01J2219/32255 ,  B01J2219/32408

摘要： A low pressure drop, highly efficient structured packing comprises sheet material formed into vertical preferably square channels containing vortex generators formed from the sheet material. The channels, while vertically linear, are periodically interrupted by the vortex generators providing tortuous fluid paths along the channels. The thus formed vortex generators form openings between adjacent channels providing fluid communication between and uniform flow within the different channels. The packing can be utilized in fluid mixing or those operations that require multiphase mass transfer, such as absorption or distillation. The addition of a catalyst makes the structure suitable for catalytic distillation. Turbulence is provided the fluids by the tortuous vertical path with low pressure drops transversely and vertically, with optimum liquid holdup.

摘要翻译： 低压降，高效率的结构填料包括形成垂直的优选方形通道的片材，其包含由片材形成的涡流发生器。 垂直线性的通道被涡流发生器周期性地中断，该涡流发生器沿通道提供曲折的流体路径。 如此形成的涡流发生器在相邻通道之间形成开口，从而提供不同通道内的流体连通和均匀的流动。 填料可用于流体混合或需要多相传质的操作，如吸收或蒸馏。 加入催化剂使该结构适合于催化蒸馏。 湍流通过弯曲的垂直路径以低压降横向和垂直地提供流体，具有最佳的液体滞留。

公开(公告)号：US20070207425A1

公开(公告)日：2007-09-06

申请号：US11678182

申请日：2007-02-23

申请人： Andreas Brautsch ,  Hanspeter Hardegger ,  Daniel Burri ,  Bettina Paikert

发明人： Andreas Brautsch ,  Hanspeter Hardegger ,  Daniel Burri ,  Bettina Paikert

IPC分类号： F23D11/00

CPC分类号： F23D17/002 ,  F23D11/108 ,  F23R3/36

摘要： A lance for a hybrid burner of a combustor of a gas turbine, includes an inner passage for a liquid fuel, an outer passage coaxially enclosing the inner passage for a gaseous fuel, a plurality of star like arranged outer nozzles branching off radially from the outer passage, a plurality of inner nozzles, which branch off radially from the inner passage and which each extend coaxially inside one of the outer nozzles, and a distributor section, which is arranged upstream of the outer nozzles n the outer passage and has a plurality of star like arranged, coaxially extending through-openings for the gaseous fuel. In order to reduce the flow resistance in the gas path of the lance, the through-openings each have an opening width which is larger in the circumferential direction than in the radial direction.

摘要翻译： 一种用于燃气轮机燃烧器的混合燃烧器的喷枪，包括用于液体燃料的内部通道，同轴地包围用于气体燃料的内部通道的外部通道，多个星形布置的外部喷嘴，从外部径向分支 多个内部喷嘴，其从所述内部通道径向分支并且在所述外部喷嘴之一内同轴地延伸;以及分配器部分，其设置在所述外部通道的外部喷嘴的上游，并且具有多个 星形排列，同轴延伸用于气态燃料的通孔。 为了减小喷枪的气体路径中的流动阻力，通孔各自具有在圆周方向上比径向方向更大的开口宽度。

公开(公告)号：US06055813A

公开(公告)日：2000-05-02

申请号：US141585

申请日：1998-08-28

申请人： Jakob Keller ,  Hugh Jackson ,  Ulf Muller ,  Bettina Paikert ,  Khawar Syed

发明人： Jakob Keller ,  Hugh Jackson ,  Ulf Muller ,  Bettina Paikert ,  Khawar Syed

IPC分类号： F23R3/16 ,  F23C7/00 ,  F23R3/12 ,  F02C9/16

CPC分类号： F23R3/12 ,  F23C7/00 ,  F23C2900/07002

摘要： Described is a plenum, in particular the air plenum of a gas-turbine combustion chamber, having at least two flow inlets, for introducing gas flows into the plenum, in which the gas flows are guided essentially along the inner wall of the plenum and are directed toward one another in such a way that the gas flows, after coinciding, are directed as a free gas flow away from the inner wall.The invention is distinguished by the fact that at least one flow obstacle (11) oriented in interaction with the direction of flow of the gas flows (1, 2) guided on the inner wall (3) is provided on the inner wall (3).

摘要翻译： 描述了一种气室，特别是具有至少两个流入口的燃气轮机燃烧室的空气增压室，用于将气流引入到气室中，其中气体基本上沿着气室的内壁被引导，并且分别是 以这样的方式彼此指向，使得气体在重合之后流动，以自由气体流动远离内壁。 本发明的特征在于，在内壁（3）上设置有与在内壁（3）上引导的气体流动（1,2）相互作用的至少一个流动障碍物（11） 。

公开(公告)号：US06241479B1

公开(公告)日：2001-06-05

申请号：US09391400

申请日：1999-09-08

申请人： Klaus Döbbeling ,  Bettina Paikert

发明人： Klaus Döbbeling ,  Bettina Paikert

IPC分类号： F04F1100

CPC分类号： F04F5/06 ,  B01F5/0406 ,  B01F5/041 ,  B01F5/0416 ,  B01F2013/1052

摘要： In a method of compressing a gas, a compression which is simple to realize is achieved in that, in a first step, a foam (21) is formed from the gas and a liquid, in which foam (21) the sonic velocity is markedly lower than in the gas and in the liquid taken by themselves, in that, in a second step, the foam is directed at supersonic velocity through a nozzle (19, 20) and the gas located in the foam is thereby compressed, and in that, in a third step, the compressed gas and the liquid are separated from one another behind the nozzle (19, 20).

摘要翻译： 在压缩气体的方法中，实现简单实现的压缩是因为在第一步骤中，泡沫（21）由气体和液体形成，其中泡沫（21）的声速显着地 低于在气体中和在自身中采集的液体中，因为在第二步骤中，泡沫以超声速度通过喷嘴（19,20），并且位于泡沫中的气体被压缩，并且因此 在第三步骤中，压缩气体和液体在喷嘴（19,20）之后彼此分离。

公开(公告)号：US5573392A

公开(公告)日：1996-11-12

申请号：US496190

申请日：1995-06-28

申请人： Bettina Paikert ,  Peter Senior

发明人： Bettina Paikert ,  Peter Senior

IPC分类号： F23D11/40 ,  F23D11/10 ,  F23D17/00 ,  F23Q9/00

CPC分类号： F23D17/002 ,  F23D11/107 ,  F23C2900/07002 ,  F23D2900/11101

摘要： In order to improve the combustion of the liquid fuel (4) in such a burner (1) without influencing that of the gaseous fuel (7), the liquid fuel (4) is directed at high flow and swirl velocity into the settling chamber (13) of the airblast nozzle (2). Then the flow and swirl velocity is reduced and a thin fluid film is formed on the prefilming lip (15). The blast air (15) is directed with a quantity ratio of less than 1:1 to the liquid fuel (4) into the airblast nozzle (2) and separates small fuel droplets at the tip (27) of the prefilming lip (15).In a double-cone burner (1), the combustion mixture (28) is injected against the swirl of its main air flow (8) and at a spray angle (26) of less than or equal to 30.degree..

摘要翻译： 为了改善这种燃烧器（1）中的液体燃料（4）的燃烧而不影响气态燃料（7）的燃烧，液体燃料（4）以高流量和旋转速度被引导到沉降室 喷气喷嘴（2）的13）。 然后减小流动和旋转速度，并在预制唇缘（15）上形成薄的流体膜。 鼓风空气（15）以与液体燃料（4）的数量比小于1:1的比例引导到喷气喷嘴（2）中，并且在预制嘴唇（15）的尖端（27）处分离小的燃料液滴， 。 在双锥形燃烧器（1）中，燃烧混合物（28）以其主空气流（8）的涡流和小于或等于30°的喷雾角（26°）注入。

公开(公告)号：US08459985B2

公开(公告)日：2013-06-11

申请号：US12876508

申请日：2010-09-07

申请人： Richard Carroni ,  Bettina Paikert

发明人： Richard Carroni ,  Bettina Paikert

IPC分类号： F23D14/62

CPC分类号： F23D14/02 ,  F23C7/002 ,  F23C2900/07002 ,  F23C2900/9901 ,  F23D14/62 ,  F23R3/286 ,  F23R2900/00014

摘要： A method for producing hot gas for operating a turbomachine fired with at least one combustion chamber includes premixing a fuel with a plurality of operating gases by introducing fuel into the plurality of operating gases in a mixing chamber disposed upstream of the combustion chamber using a burner arrangement, wherein the fuel includes at least one of a combustible gas and a H2-rich fuel; and introducing the premixed fuel into the combustion chamber.

摘要翻译： 一种生产用于操作用至少一个燃烧室燃烧的涡轮机的热气体的方法包括：通过使用燃烧器装置将设置在燃烧室上游的混合室内的燃料引入到多个操作气体中来预燃燃料与多个操作气体 ，其中所述燃料包括可燃气体和富H2燃料中的至少一种; 并将预混燃料引入燃烧室。

公开(公告)号：US07520745B2

公开(公告)日：2009-04-21

申请号：US11689655

申请日：2007-03-22

申请人： Gijsbertus Oomens ,  Bettina Paikert ,  Peter Flohr ,  Christian Steinbach

发明人： Gijsbertus Oomens ,  Bettina Paikert ,  Peter Flohr ,  Christian Steinbach

IPC分类号： F23D14/62 ,  F23D14/46

CPC分类号： F23C7/002 ,  F23C2900/07002 ,  F23D11/24 ,  F23D11/38 ,  F23R3/343

摘要： A premix burner, for example for a gas turbine, having a conical swirl generator (1) and a cylindrical mixing section (2) which follows it in the direction of flow, includes a high-pressure atomizer nozzle (10) with one or more fuel feed passages. The high-pressure atomizer nozzle (10) includes at least two outlet passages, through which liquid fuel enters the swirl generator (1), these passages being arranged off-center with respect to the longitudinal axis of the nozzle and being configured in such a way that the spray cone (11) of the fuel is oriented at an angle (β) with respect to the longitudinal axis of the swirl generator (1) which is smaller than the cone half-angle (α) of the swirl generator (1). The outlet passages in particular have an internal geometry with a conically narrowed section.

摘要翻译： 包括具有锥形涡流发生器（1）的燃气轮机的预混合燃烧器和在流动方向上沿其流动的圆柱形混合部分（2）包括具有一个或多个的高压雾化喷嘴（10） 燃料供给通道。 高压雾化器喷嘴（10）包括至少两个出口通道，液体燃料通过该出口通道进入涡流发生器（1），这些通道相对于喷嘴的纵向轴线偏离中心，并被配置在 燃料的喷雾锥体（11）相对于涡流发生器（1）的纵向轴线以与旋流发生器（1）的锥形半角（α）小的角度（β）定向的方式， ）。 出口通道特别具有内部几何形状，具有锥形变窄的部分。