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1. 发明授权

US08275231B2 Optical waveguide 有权
标题翻译：光波导
公开(公告)号：US08275231B2
公开(公告)日：2012-09-25
申请号：US12310411
申请日：2007-08-16
申请人： Gilbert Braun , Volker Ertle , Christian Henke , Gülsen Kisaboyun , Andreas Pahl , Bernd Prade , Uwe Scheuer , Wolfgang Stammen , Edmund Zastrozny
发明人： Gilbert Braun , Volker Ertle , Christian Henke , Gülsen Kisaboyun , Andreas Pahl , Bernd Prade , Uwe Scheuer , Wolfgang Stammen , Edmund Zastrozny
IPC分类号： G02B6/10 , G02B6/00 , G02B6/32
CPC分类号： G02B23/2407 , F23M11/045 , F23M2900/11041 , F23N5/08 , F23N2900/05005 , G02B23/2492
摘要： An optical waveguide with a tubular or hose-like housing is provided, which is used in a high-temperature environment, such as, for example, in a burner. The housing has an input opening, an output opening and a center line extending from the input opening to the output opening. In the interior of the housing, transparent spheres are lined up along with center line. The light is guided on account of the refraction of a light beam upon entering and exiting from the transparent spheres.
摘要翻译：提供具有管状或软管状壳体的光波导，其用于例如在燃烧器中的高温环境中。壳体具有从输入开口延伸到输出开口的输入开口，输出开口和中心线。在房屋的内部，透明球体与中心线一起排列。由于在从透明球体进入和离开时光束的折射而引导光。

2. 发明申请

US20100031659A1 Method and Device for Monitoring the Formation of Deposits of Solid Particles, Particularly in a Fuel Line and in the Fuel Valves of a Gas Turbine 有权
标题翻译：用于监测固体颗粒沉积物形成的方法和装置，特别是在燃料管线和燃气轮机的燃料阀中
公开(公告)号：US20100031659A1
公开(公告)日：2010-02-11
申请号：US12083032
申请日：2006-10-05
申请人： Andreas Diebels , Bernd Prade
发明人： Andreas Diebels , Bernd Prade
IPC分类号： F02C7/22 , G01N7/00
CPC分类号： F23K5/147 , F02C7/30 , F05D2260/607 , F05D2260/80 , F23K2900/05001 , F23N2035/16 , F23N2041/20 , Y10T137/7759
摘要： A process is disclosed for monitoring the formation of deposits of solid particles in a fuel line having a valve. A measure for the deposits of solid particles in the fuel line is determined by determining the degree of opening of the valve passage and the quantity of fuel flowing through the valve, and by comparing them with a previously determined control value which characterizes the deposit-free line. Also disclosed is a device for monitoring the formation of deposits of solid particles in a fuel line having a valve, the device having a measurement system for determining the current fuel flow and a measurement system for determining the current valve position, as well as an evaluation system connected to the measurement systems. Also disclosed is a combustion chamber comprising a device and operated by a process according to the invention, and a gas turbine with said combustion chamber.
摘要翻译：公开了一种用于监测具有阀的燃料管中固体颗粒沉积物形成的方法。通过确定阀通道的开度和流过阀的燃料量来确定燃料管线中固体颗粒沉积物的量度，并将其与预先确定的控制值进行比较，其特征在于无沉积线。还公开了一种用于监测具有阀的燃料管线中的固体颗粒沉积物的形成的装置，该装置具有用于确定当前燃料流量的测量系统和用于确定当前阀位置的测量系统，以及评估系统连接到测量系统。还公开了一种燃烧室，其包括通过根据本发明的方法操作的装置和具有所述燃烧室的燃气轮机。

3. 发明授权

US07080515B2 Gas turbine can annular combustor 有权
标题翻译：燃气轮机可以环形燃烧器
公开(公告)号：US07080515B2
公开(公告)日：2006-07-25
申请号：US10667263
申请日：2003-09-19
申请人： Samer P. Wasif , Udo Schmitz , Robert Bland , Karsten Jordan , John Carl Glessner , J. Scott Markovitz , Bernd Prade , David Kargetta , Stephen Ramier , Stefan Dahlk
发明人： Samer P. Wasif , Udo Schmitz , Robert Bland , Karsten Jordan , John Carl Glessner , J. Scott Markovitz , Bernd Prade , David Kargetta , Stephen Ramier , Stefan Dahlk
IPC分类号： F02C3/00 , F23R3/04 , F23R3/14
CPC分类号： F23R3/14 , F23R3/286 , F23R3/343 , F23R3/54 , F23R3/60 , F23R2900/00014 , F23R2900/03044
摘要： A gas turbine engine (120) includes a cylindrical basket (146) having an axis (14) and a single main burner assembly (12) disposed within the basket. A burner insert (34) is disposed in an annular space between the burner assembly and the basket. The insert includes a face perpendicular to the axis of the basket. A plurality of passageways (114) are formed in the basket, positioned proximate to and downstream of the burner insert for allowing passage of a portion of an oxidizer flow (42) into a combustion chamber (30). A fluid flow path (38), defined between a combustion chamber liner portion (32) of the basket and a casing (40) spaced radially outward from the combustion liner portion, discharges a fluid into a flow reversal region (118) proximate an inlet (20) of the burner assembly. A fuel outlet (44) is disposed in the flow reversal region.
摘要翻译：燃气涡轮发动机（120）包括具有轴线（14）的圆柱形篮（146）和设置在篮内的单个主燃烧器组件（12）。燃烧器插入件（34）设置在燃烧器组件和篮子之间的环形空间中。插入件包括垂直于筐轴线的面。多个通道（114）形成在篮中，其位于燃烧器插入件附近和下游，以允许一部分氧化剂流（42）通入燃烧室（30）。限定在筐的燃烧室衬套部分（32）和与燃烧衬套部分径向向外间隔开的壳体（40）之间的流体流动路径（38）将流体排放到靠近入口的流动反向区域（118）（20）。燃料出口（44）设置在流动反转区域中。

4. 发明授权

US06832481B2 Turbine engine fuel nozzle 有权
标题翻译：涡轮发动机燃油喷嘴
公开(公告)号：US06832481B2
公开(公告)日：2004-12-21
申请号：US10255892
申请日：2002-09-26
申请人： Michael Herbert Koenig , Bernd Prade
发明人： Michael Herbert Koenig , Bernd Prade
IPC分类号： F23R330
CPC分类号： F23R3/286 , F23C2900/07001 , F23D2900/14004 , F23R3/14
摘要： A performance-enhancing fuel nozzle is disclosed. The nozzle suitable for use in combustors which combine high-swirl-number combustion in a pilot zone with low-swirl-number combustion in a main combustion zone. The nozzle includes a fuel delivery member adapted for fluid communication with a fuel source and a flow conditioning member having a fuel exit port. The fuel exit port is in fluid communication with the fuel supply and is adapted to ensure that the recirculation region adjacent the nozzle tip remains flame free. In one aspect of the invention, the fuel concentration profile of the nozzle is characterized by a radially-outward region that is flammable and a radially-inward region that is substantially non-flammable. In another aspect of the invention, the fuel exit port being is disposed a radially-outward portion of the flow conditioning member. In another aspect of the invention, the flow conditioning member is characterized by a swirl number lower than about 0.5. In another aspect of the invention, the exit are high-momentum jets, having a design ratio pressure of greater than about 1.1. In another aspect of the invention, the nozzle is part of a combustor which has a high-swirl-number combustion in a pilot zone and low-swirl-number combustion in a main combustion zone.
摘要翻译：公开了一种性能增强的燃料喷嘴。该喷嘴适用于在主燃烧区内将先导区域的高涡数燃烧与低涡数燃烧相结合的燃烧器。喷嘴包括适于与燃料源流体连通的燃料输送构件和具有燃料出口的流量调节构件。燃料出口与燃料供应流体连通，并且适于确保与喷嘴尖端相邻的再循环区域保持无火焰状态。在本发明的一个方面，喷嘴的燃料浓度分布特征在于可燃的径向向外区域和基本上不可燃的径向向内区域。在本发明的另一方面，燃料出口端口设置在流量调节构件的径向向外的部分。在本发明的另一方面，流量调节构件的特征在于低于约0.5的涡旋数。在本发明的另一方面，出口是具有大于约1.1的设计比压力的高动量射流。在本发明的另一方面，喷嘴是燃烧器的一部分，其在先导区域中具有高涡流数量的燃烧，并且在主燃烧区域中具有低漩涡数量的燃烧。

5. 发明授权

US6038864A Burner with annular gap and gas flow with constant meridional velocity through the annular gap and gas turbine having the burner 失效
标题翻译：具有环形间隙的气体和具有恒定子午速度的气流通过环形间隙和具有燃烧器的燃气轮机
公开(公告)号：US6038864A
公开(公告)日：2000-03-21
申请号：US047164
申请日：1998-03-23
申请人： Bernd Prade , Bernhard Schetter , Holger Streb
发明人： Bernd Prade , Bernhard Schetter , Holger Streb
IPC分类号： F23D14/82 , F23C7/00 , F23D14/24 , F23D14/26 , F23R3/14 , F23Q9/00
CPC分类号： F23D14/24 , F23C7/004 , F23D14/26
摘要： A burner includes an axis and a configuration which is rotationally symmetrical relative to the axis and includes an outer casing and an inner casing coaxial thereto. The configuration defines an annular gap extending from an inlet to an outlet for guiding a stream of oxygen-containing gas. A multiplicity of nozzles for supplying a fuel to the stream and a swirl lattice are disposed in the annular gap. The configuration including the outer and inner casings is constructed in such a way that the stream flows through the annular gap between the swirl lattice and the outlet at an essentially constant meridional velocity. The burner is particularly suitable for use in a gas turbine.
摘要翻译：燃烧器包括轴线和相对于轴线旋转对称的构造，并且包括外壳体和与其同轴的内壳体。该构造限定了从入口延伸到出口的环形间隙，用于引导含氧气体流。在环形间隙中设置有多个用于向流体供给燃料的喷嘴和旋转晶格。包括外壳体和内壳体的构造被构造成使得流以基本上恒定的子午速度流过旋流晶格和出口之间的环形间隙。燃烧器特别适用于燃气轮机。

6. 发明授权

US09523288B2 Hydraulic bearing for a stationary gas turbine 有权
标题翻译：用于固定燃气轮机的液压轴承
公开(公告)号：US09523288B2
公开(公告)日：2016-12-20
申请号：US14129953
申请日：2012-06-11
申请人： Uwe Lohse , Bernd Prade
发明人： Uwe Lohse , Bernd Prade
IPC分类号： F01D25/18 , F01D25/16 , F01M11/04 , F16C33/10
CPC分类号： F01D25/16 , F01D25/18 , F01M11/04 , F05D2240/127 , F16C33/1045 , F16C2360/23
摘要： A hydraulic bearing is provided for a stationary gas turbine that has an oil sump with an outflow for hydraulic oil, wherein the outflow has an outflow opening which is arranged in the oil sump and an outflow line which is connected to the outflow opening. The hydraulic bearing is adapted to bring about an annular flow with a central air column when hydraulic oil flows out in the outflow line.
摘要翻译：为固定式燃气轮机提供液压轴承，该固定式燃气轮机具有用于液压油的流出口的油底壳，其中流出口具有布置在油底壳中的流出口和连接到流出口的流出管线。当液压油在流出管路中流出时，液压轴承适于带有中央空气柱的环形流。

7. 发明授权

US09217569B2 Burner and method for operating a burner 有权
标题翻译：燃烧器和操作燃烧器的方法
公开(公告)号：US09217569B2
公开(公告)日：2015-12-22
申请号：US13121955
申请日：2009-09-14
申请人： Bernd Prade
发明人： Bernd Prade
IPC分类号： F02C3/20 , F23R3/14 , F23R3/26 , F23R3/36
CPC分类号： F23R3/14 , F23R3/26 , F23R3/36 , F23R2900/00002
摘要： A burner and a method for operating a burner are provided. The burner includes a channel having a mixing zone and having a feed for an oxidation means, particularly an air feed, and at least one fuel feed for injecting fuel, wherein a separating means which divides the channel over a wide range of the channel into at least two separated channels, namely a first channel and a second channel, is provided in the channel. The method for operating a burner having a channel includes a mixing zone into which an oxidation mass flow and fuel are injected, wherein two substantially separate flow paths are formed by means of a separating means in the channel and the at least two separated first and second channels, formed by the separating means.
摘要翻译：提供了一种用于操作燃烧器的燃烧器和方法。燃烧器包括具有混合区并具有用于氧化装置的进料，特别是空气进料的通道和用于喷射燃料的至少一种燃料进料，其中分离装置将通道的宽范围分成通道在通道中设置了至少两个分离的通道，即第一通道和第二通道。用于操作具有通道的燃烧器的方法包括：混合区，其中注入有氧化质量流和燃料，其中通过通道中的分离装置形成两个基本上分离的流动路径，并且所述至少两个分离的第一和第二通道由分离装置形成。

8. 发明申请

US20130125550A1 GAS TURBINE COMBUSTION CHAMBER 有权
标题翻译：气体涡轮搅拌室
公开(公告)号：US20130125550A1
公开(公告)日：2013-05-23
申请号：US13813494
申请日：2011-06-15
申请人： Bernd Prade
发明人： Bernd Prade
IPC分类号： F23R3/28
CPC分类号： F23R3/28 , F23R3/343
摘要： A gas turbine combustion chamber is provided including a pilot fuel nozzle arranged in the central section of a cylinder that opens at one end towards a combustion chamber. The pilot fuel nozzle includes a fuel nozzle and a cylindrical outer casing around the outer circumference of the fuel nozzle. A pilot swirl element is arranged between fuel nozzle and outer casing, including a plurality of main burners which are arranged around the pilot fuel nozzle, and including a pilot cone having an inner side and an outer side. The pilot cone is arranged on the pilot fuel nozzle and an opening, such that a pilot flame is formed in the pilot cone by mixing air and pilot fuel in order to ignite a fuel injected by the main burners, wherein the pilot cone has turbulence generators on the inner side and/or outer side thereof.
摘要翻译：提供一种燃气轮机燃烧室，其包括引导燃料喷嘴，该引燃燃料喷嘴布置在气缸的中心部分中，该气缸的一端朝向燃烧室开口。导向燃料喷嘴包括燃料喷嘴和围绕燃料喷嘴外圆周的圆柱形外壳。在燃料喷嘴和外壳之间设置有一个先导涡流元件，包括设置在引燃燃料喷嘴周围的多个主燃烧器，并且包括具有内侧和外侧的先导锥体。先导锥体布置在先导燃料喷嘴和开口上，使得先导火焰通过混合空气和引燃燃料而形成在先导锥体中，以点燃由主燃烧器喷射的燃料，其中先导锥具有湍流发生器在其内侧和/或外侧。

9. 发明授权

US08020387B2 Method of operating a burner, including a combustion chamber with a low nitrous oxide emission 有权
标题翻译：操作燃烧器的方法，包括具有低一氧化二氮排放的燃烧室
公开(公告)号：US08020387B2
公开(公告)日：2011-09-20
申请号：US11665101
申请日：2005-09-30
申请人： Bernd Prade
发明人： Bernd Prade
IPC分类号： F02C1/00
CPC分类号： F02C3/20 , F02C9/40 , F23L7/00 , F23L2900/07002 , F23L2900/07008 , F23L2900/07009 , F23N2021/10 , F23N2041/20
摘要： There is described a method for operation of a burner, whereby a fuel is supplied to the burner, sprayed into the combustion air, mixed with the combustion air to give a fuel/air mixture and burnt in a combustion chamber. With regard to a combustion particularly low in pollutants and, in order to reduce the nitrogen oxide emissions with relation to achieving a given nitrogen oxide emission level, a change in parameters characterizing the fuel is determined. Such a parameter may, for example, be the Wobbe index. There is further described a device for carrying out said method, comprising a fuel treatment device, with an analytical device for the analysis of the current fuel composition and a monitoring and control system.
摘要翻译：描述了一种操作燃烧器的方法，由此将燃料供应到燃烧器，喷射到燃烧空气中，与燃烧空气混合以产生燃料/空气混合物并在燃烧室中燃烧。关于特别低的污染物的燃烧，为了相对于达到给定的氮氧化物排放水平而减少氮氧化物的排放，确定了表征燃料的参数的变化。这样的参数可以例如是Wobbe索引。进一步描述了用于执行所述方法的装置，其包括燃料处理装置，具有用于分析当前燃料组成的分析装置和监视和控制系统。

10. 发明申请

US20100183991A1 Premixing burner and method for operating a premixing burner 审中-公开
标题翻译：预混燃烧器和操作预混燃烧器的方法
公开(公告)号：US20100183991A1
公开(公告)日：2010-07-22
申请号：US12669971
申请日：2008-07-23
申请人： Berthold Köstlin , Martin Lenze , Bernd Prade
发明人： Berthold Köstlin , Martin Lenze , Bernd Prade
IPC分类号： F23D14/24 , F23C7/00 , F23C5/08 , F23L7/00
CPC分类号： F23C7/004 , F23C2900/07001 , F23D11/383 , F23D2900/14021 , F23L7/00 , F23L2900/07002 , F23L2900/07009 , F23R3/14 , F23R3/286
摘要： A method for operating a premixing burner is provided. The premixing burner includes a premixing zone. An air mass flow and fuel may be injected into the premixing zone, and a potential hot gas backflow area may form. A fluid containing no fuel is injected downstream from the fuel injection into the premixing zone in order that a hot gas backflow area does not form. A premixing burner including a premixing zone is also provided.
摘要翻译：提供了一种操作预混合燃烧器的方法。预混合燃烧器包括预混合区。空气质量流量和燃料可以注入预混合区域，并且可能形成潜在的热气回流区域。将不含燃料的流体从燃料喷射下游注入预混合区域，以便不形成热气体回流区域。还提供了包括预混合区域的预混合燃烧器。

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