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1. 发明申请

US20060035188A1 Burner 有权
标题翻译：刻录机
公开(公告)号：US20060035188A1
公开(公告)日：2006-02-16
申请号：US10525779
申请日：2003-08-20
申请人： Peter Berenbrink , Malte Blomeyer , Wener Krebs , Bernd Prade , Holger Streb
发明人： Peter Berenbrink , Malte Blomeyer , Wener Krebs , Bernd Prade , Holger Streb
IPC分类号： F23D14/46
CPC分类号： F23R3/343 , F23R3/14 , F23R3/286 , F23R2900/00014
摘要： Burners in prior art exhibit combustion instabilities in certain ranges. The operating range of burners is restricted by said instabilities. In an inventive burner, the combustible has a concentration distribution, whereby the concentration of the combustible reduces in a radial direction from the interior to the exterior.
摘要翻译：现有技术中的燃烧器在某些范围内表现出燃烧不稳定性。燃烧器的运行范围受到不稳定性的限制。在本发明的燃烧器中，可燃物具有浓度分布，由此可燃物的浓度在径向方向上从内部到外部减小。

2. 发明授权

US07753677B2 Burner 有权
标题翻译：刻录机
公开(公告)号：US07753677B2
公开(公告)日：2010-07-13
申请号：US10525779
申请日：2003-08-20
申请人： Peter Berenbrink , Malte Blomeyer , Werner Krebs , Bernd Prade , Holger Streb
发明人： Peter Berenbrink , Malte Blomeyer , Werner Krebs , Bernd Prade , Holger Streb
IPC分类号： F23D14/26 , F23D14/62
CPC分类号： F23R3/343 , F23R3/14 , F23R3/286 , F23R2900/00014
摘要： Burners in prior art exhibit combustion instabilities in certain ranges. The operating range of burners is restricted by said instabilities. In an inventive burner, the combustible has a concentration distribution, whereby the concentration of the combustible reduces in a radial direction from the interior to the exterior.
摘要翻译：现有技术中的燃烧器在某些范围内表现出燃烧不稳定性。燃烧器的运行范围受到不稳定性的限制。在本发明的燃烧器中，可燃物具有浓度分布，由此可燃物的浓度在径向方向上从内部到外部减小。

3. 发明授权

US07472540B2 Method and device for compensating variations in fuel composition in a gas turbine system 有权
标题翻译：用于补偿燃气轮机系统中燃料组成变化的方法和装置
公开(公告)号：US07472540B2
公开(公告)日：2009-01-06
申请号：US10575516
申请日：2004-10-11
申请人： Peter Berenbrink , Malte Blomeyer
发明人： Peter Berenbrink , Malte Blomeyer
IPC分类号： F02C9/26
CPC分类号： F02C9/34 , F05D2270/08 , F05D2270/081
摘要： The invention relates to a method for compensating variations in fuel composition in a gas turbine system consisting of at least two parallel-operated burner stages, wherein the fuel supply to at least two of the burner stages is adjusted in response to variations in fuel composition, wherein the fuel split between the burner stages, i.e. the relative increase in speed of the fuel supplied to the burner stages, is adjusted to a target value or maintained at a target value during adjustment of the fuel supply. The target value can, for example be a constant or a function of one or several variables. More particularly, the gas turbine system can comprise a pilot burner stage and a main burner stage. When the fuel supply is adjusted, the fuel split between the pilot burner stage and the main burner stage is adjusted to a target value or maintained at a target value.
摘要翻译：本发明涉及一种用于补偿由至少两个平行操作的燃烧器级构成的燃气轮机系统中的燃料组成变化的方法，其中至少两个燃烧器级的燃料供应是根据燃料组成的变化进行调节的，其中在燃料级之间分配的燃料，即供应到燃烧器级的燃料的速度的相对增加在调节燃料供应期间被调整到目标值或维持在目标值。目标值例如可以是一个或多个变量的常数或函数。更具体地，燃气轮机系统可以包括引燃燃烧器级和主燃烧器级。当调节燃料供应时，将引燃燃烧器级和主燃烧器级之间的燃料分配调节到目标值或维持在目标值。

4. 发明申请

US20070119178A1 Method and device for compensating variations in fuel composition in a gas turbine system 有权
标题翻译：用于补偿燃气轮机系统中燃料组成变化的方法和装置
公开(公告)号：US20070119178A1
公开(公告)日：2007-05-31
申请号：US10575516
申请日：2004-10-11
申请人： Peter Berenbrink , Malte Blomeyer
发明人： Peter Berenbrink , Malte Blomeyer
IPC分类号： F02C9/26
CPC分类号： F02C9/34 , F05D2270/08 , F05D2270/081
摘要： The invention relates to a method for compensating variations in fuel composition in a gas turbine system consisting of at least two parallel-operated burner stages, wherein the fuel supply to at least two of the burner stages is adjusted in response to variations in fuel composition, wherein the fuel split between the burner stages, i.e. the relative increase in speed of the fuel supplied to the burner stages, is adjusted to a target value or maintained at a target value during adjustment of the fuel supply. The target value can, for example be a constant or a function of one or several variables. More particularly, the gas turbine system can comprise a pilot burner stage and a main burner stage. When the fuel supply is adjusted, the fuel split between the pilot burner stage and the main burner stage is adjusted to a target value or maintained at a target value.
摘要翻译：本发明涉及一种用于补偿由至少两个平行操作的燃烧器级构成的燃气轮机系统中的燃料组成变化的方法，其中至少两个燃烧器级的燃料供应是根据燃料组成的变化进行调节的，其中在燃料级之间分配的燃料，即供应到燃烧器级的燃料的速度的相对增加在调节燃料供应期间被调整到目标值或维持在目标值。目标值例如可以是一个或多个变量的常数或函数。更具体地，燃气轮机系统可以包括引燃燃烧器级和主燃烧器级。当调节燃料供应时，将引燃燃烧器级和主燃烧器级之间的燃料分配调节到目标值或维持在目标值。

5. 发明申请

US20140209044A1 BYPASS STEAM LINE 审中-公开
标题翻译：旁路蒸汽管线
公开(公告)号：US20140209044A1
公开(公告)日：2014-07-31
申请号：US14239140
申请日：2012-08-02
申请人： Peter Berenbrink , Frank Deidewig , Holger Gedanitz , Dirk Huckriede , Mario Koebe , Bernd Prade , Horst Uwe Rauh , Stephan Schestag
发明人： Peter Berenbrink , Frank Deidewig , Holger Gedanitz , Dirk Huckriede , Mario Koebe , Bernd Prade , Horst Uwe Rauh , Stephan Schestag
IPC分类号： F22G5/12
CPC分类号： F22G5/123 , B01F3/04056 , B01F5/0421 , B01F5/0428 , B01F15/063 , B01F2015/061 , F01D25/12 , F02C3/30 , F02C7/1435 , F02C7/16 , F05D2220/31 , F05D2260/20 , F05D2260/601 , F05D2260/96 , F22G5/126
摘要： A mixing unit for mixing water with steam in a bypass station is provided. The mixing unit has a plurality of Laval nozzles arranged in the mixing unit, which Laval nozzles are displaced axially with respect to one another in a water steam direction, with the result that the noise emissions are reduced overall.
摘要翻译：提供了一种用于在旁路站中混合水和蒸汽的混合单元。混合单元具有布置在混合单元中的多个拉瓦尔喷嘴，其中拉瓦尔喷嘴在水蒸汽方向上相对于彼此轴向位移，结果是噪声排放总体上降低。

6. 发明授权

US6052986A Method and device for burning fuel with air 有权
标题翻译：用空气燃烧燃料的方法和装置
公开(公告)号：US6052986A
公开(公告)日：2000-04-25
申请号：US272748
申请日：1999-03-16
申请人： Stefan Hoffmann , Peter Berenbrink , Hans Judith
发明人： Stefan Hoffmann , Peter Berenbrink , Hans Judith
IPC分类号： F23R3/28 , F23C15/00 , F23D23/00 , F23M99/00 , F02C7/00
CPC分类号： F23D23/00 , F23M20/005 , F23R2900/00014
摘要： A method and a device for burning fuel with air in a combustion chamber. The air is fed to the combustion chamber through at least one air inlet and the fuel is fed to the combustion chamber through a plurality of burners. Each burner has an associated delay time corresponding to a period of time after which an acoustic impulse in the combustion chamber causes a thermal impulse during combustion of the fuel fed through the burner. The feeding of the fuel through the burner is controlled in such a way that the delay times of the burners are substantially different from one another. The invention can be used on a combustion chamber of a gas turbine.
摘要翻译：燃烧室内用燃烧燃料的方法和装置。空气通过至少一个空气入口进入燃烧室，燃料通过多个燃烧器供给到燃烧室。每个燃烧器具有对应于一段时间的相关联的延迟时间，此后燃烧室中的声脉冲在通过燃烧器供给的燃料的燃烧期间引起热脉冲。通过燃烧器供给燃料以这样的方式进行控制，使得燃烧器的延迟时间基本上彼此不同。本发明可用于燃气轮机的燃烧室。

7. 发明授权

US06632084B2 Burner configuration with primary and secondary pilot burners 有权
标题翻译：燃烧器配置与主要和次要驾驶燃烧器
公开(公告)号：US06632084B2
公开(公告)日：2003-10-14
申请号：US09794662
申请日：2001-02-27
申请人： Peter Berenbrink
发明人： Peter Berenbrink
IPC分类号： F23Q300
CPC分类号： F23D17/002 , F23D2206/10 , F23D2209/10 , F23D2209/20 , F23D2900/00014 , F23D2900/00015 , F23R3/343
摘要： A burner configuration with primary and secondary pilot burners is described. The burner configuration is used in a firing installation, in particular a gas turbine combustion chamber, and has a main burner and, disposed centrally within it, a primary pilot burner used for igniting and/or for stabilizing the combustion of the main burner. For additional stabilization, for reducing rumble noises in the firing installation and for avoiding the possible flashback of the flame in a partial region of the burner, which can then sometimes occur, a plurality of outlet openings, which together form a secondary pilot burner, are disposed in the outlet region of the main burner. The flames of the secondary pilot burner surround the main flame like a ring and additionally stabilize the operation under different load conditions.
摘要翻译：描述了具有主要和次要先导燃烧器的燃烧器配置。燃烧器配置用于燃烧装置，特别是燃气轮机燃烧室，并具有主燃烧器，并且设置在其内部，用于点燃和/或稳定主燃烧器燃烧的主引燃燃烧器。为了进一步的稳定化，为了减少点火装置中的隆隆声，并且为了避免在燃烧器的局部区域中可能发生的火焰的闪回，这可能会有时会发生，多个出口开口一起形成次级引燃燃烧器设置在主燃烧器的出口区域。次级引燃燃烧器的火焰围绕主火焰像环，并且另外在不同的负载条件下稳定操作。

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