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公开(公告)号：US07457710B2
公开(公告)日：2008-11-25
申请号：US11279421
申请日：2006-04-12
IPC分类号： F23N5/00
CPC分类号： G01N33/2829 , F23M20/005 , F23N5/16 , F23R2900/00013 , G01N25/50 , G01N2291/02872
摘要： A sensor 11 detects the acoustic pressure at a first location in a combustion chamber 7 of a test rig 1 and produces an input signal which is a function of the acoustic pressure. A controller 13 receives the input signal and produces an output signal which is a function of the input signal. An acoustic actuator (16-18) receives the output signal and introduces into the combustion chamber 7 at a second location an acoustic pressure which is a function of the output signal. The acoustic actuator may comprise a fuel injector 18 or a loudspeaker. By using an appropriate control algorithm, acoustic boundary conditions corresponding to a particular gas turbine combustion chamber may be produced, at least in a certain frequency range.
摘要翻译： 传感器11检测试验台1的燃烧室7中的第一位置处的声压，并产生作为声压的函数的输入信号。 控制器13接收输入信号并产生作为输入信号的函数的输出信号。 声学致动器（16-18）接收输出信号，并在第二位置处将作为输出信号的函数的声压引入燃烧室7。 声学致动器可以包括燃料喷射器18或扬声器。 通过使用适当的控制算法，可以至少在一定的频率范围内产生对应于特定燃气轮机燃烧室的声学边界条件。
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公开(公告)号：US08029273B2
公开(公告)日：2011-10-04
申请号：US11540636
申请日：2006-10-02
CPC分类号： F23R3/28 , F23C7/002 , F23D2210/00
摘要： A burner is disclosed which includes a vortex generator for a combustion air stream, means for the admission of fuel into the combustion air stream and air inlet ducts, the combustion air stream enters a vortex chamber of the vortex generator via air inlet ducts. The fuel is injected into the combustion air asymmetrically via the injection means.
摘要翻译： 公开了一种燃烧器，其包括用于燃烧空气流的涡流发生器，用于将燃料进入燃烧空气流和空气入口管道的装置，燃烧空气流经由空气入口管进入涡流发生器的涡流室。 燃料通过注射装置不对称地注入燃烧空气中。
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公开(公告)号：US07198483B2
公开(公告)日：2007-04-03
申请号：US10470556
申请日：2002-01-30
申请人： Dirk Bueche , Rolf Dornberger , Petros Koumoutsakos , Christian Oliver Paschereit , Bruno Schuermans , Peter Stoll
发明人： Dirk Bueche , Rolf Dornberger , Petros Koumoutsakos , Christian Oliver Paschereit , Bruno Schuermans , Peter Stoll
CPC分类号： F23D14/02 , F02C7/222 , F23C2900/07002 , F23K5/005 , F23K2401/201 , F23N5/16 , F23N2037/02 , F23N2037/20 , F23N2041/20 , F23R2900/00014
摘要： Arranged upstream of each swirl-stabilized premix burner (1) of a burner system there is respectively an adjustable distributing device (5) with control valves (V1, . . . , V8) and/or on/off valves (V″1, . . . , V″16), by means of which various axial mass flow distributions of the fuel introduced can be set. Preferably, those which have particularly favorable values with respect to characteristics such as NOx emission and maximum amplitudes of pulsations occurring are chosen. For this purpose, Pareto solutions are determined with respect to the said characteristics, in that a distributing device (5) is represented by a tree structure with distributing parameters, and values for the distributing parameters on the basis of which the distributing device (5) is set by means of a control unit are iteratively generated in a data-processing system by an evolutionary algorithm. On the basis of the values determined by a measuring unit, solutions which are especially favorable with respect to the characteristics mentioned, especially Pareto-optimal, are selected. The distributing devices are then set during operation on the basis of the solutions of this type corresponding to respective requirements.
摘要翻译： 在燃烧器系统的每个涡旋稳定的预混合燃烧器（1）的上游布置有分别具有控制阀（V 1，...，V 8）的可调节分配装置（5） 和/或开/关阀（V“1”，...，V“16”），借助于各种轴向质量流量分布 的燃油可以设定。 优选地，选择对于发生的特性如NO x发射和最大的脉动振幅具有特别有利的值的那些。 为此，相对于所述特征确定帕累托解，其中分配装置（5）由具有分布参数的树结构表示，并且分配参数的值基于分配装置（5）， 通过控制单元进行设置，通过进化算法在数据处理系统中迭代生成。 基于由测量单元确定的值，选择对于所提及的特性尤其有利的解决方案，特别是帕累托最优。 然后在操作期间基于对应于各种要求的这种类型的解决方案来设置分配设备。
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公开(公告)号：US07424804B2
公开(公告)日：2008-09-16
申请号：US11214919
申请日：2005-08-31
CPC分类号： F23R3/286 , F23M20/005 , F23R3/002 , F23R2900/00014
摘要： A premix burner has a swirl generator and two perforated through flow elements are arranged at a defined distance from one another in the inflow region for the combustion air. The through flow elements are preferably arranged in such a way that substantially the entire combustion airstream has to flow through the through flow elements. The degree of perforation of the through flow elements and the distance between these elements are preferably adapted to one another in such a way that a reflection free condition for combustion pulsation frequencies which may be expected is present at the exit from the burner into the combustion chamber.
摘要翻译： 预混燃烧器具有涡流发生器，并且两个穿孔的流动元件在用于燃烧空气的流入区域中以彼此限定的距离布置。 通流元件优选地布置成使得基本上整个燃烧气流必须流过通过流动元件。 通过流动元件的穿孔程度和这些元件之间的距离优选地彼此适配，使得可以预期的燃烧脉动频率的无反射条件存在于从燃烧器进入燃烧室的出口 。
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公开(公告)号：US07137809B2
公开(公告)日：2006-11-21
申请号：US10470557
申请日：2002-01-30
申请人： Dirk Bueche , Rolf Dornberger , Petros Koumoutsakos , Christian Oliver Paschereit , Bruno Schuermans , Peter Stoll
发明人： Dirk Bueche , Rolf Dornberger , Petros Koumoutsakos , Christian Oliver Paschereit , Bruno Schuermans , Peter Stoll
CPC分类号： F23N5/16 , F23C2900/07002 , F23D14/02 , F23K5/002 , F23N2023/44 , F23N2035/18 , F23N2037/02 , F23N2041/20 , F23R2900/00013
摘要： In the case of swirl-stabilized premix burners (1), an axial mass flow distribution of the fuel introduced which has especially favorable values with respect to characteristics such as NOx emission and maximum amplitudes of pulsations occurring is used. For this purpose, Pareto solutions are determined with respect to the said characteristics, in that a distributing device (5) with control valves is represented by a tree structure with distributing parameters, and values for the distributing parameters on the basis of which the distributing device (5) is set by means of a control unit (10) are iteratively generated in a data-processing system (9) by an evolutionary algorithm. On the basis of the values determined by a measuring unit (11), solutions which are especially favorable with respect to the characteristics mentioned, espectially Pareto-optimal, are selected. The distributing devices or the premix burners of the burner system are then formed in a way corresponding to such a solution.
摘要翻译： 在涡流稳定的预混燃烧器（1）的情况下，引入的燃料的轴向质量流量分布相对于诸如NO x x发射的特性和最大的脉动幅度具有特别有利的值， 用过的。 为此，相对于所述特性确定帕累托解决方案，其中具有控制阀的分配装置（5）由具有分配参数的树形结构表示，并且分配参数的值基于该分配参数 （5）通过控制单元（10）设置在数据处理系统（9）中通过进化算法迭代生成。 基于由测量单元（11）确定的值，选择对于所述特征特别有利的解决方案，具有帕累托优化。 然后以与这种解决方案相对应的方式形成燃烧器系统的分配装置或预混燃烧器。
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公开(公告)号：US06981358B2
公开(公告)日：2006-01-03
申请号：US10460363
申请日：2003-06-13
申请人： Valter Bellucci , Peter Flohr , Christian Oliver Paschereit , Bruno Schuermans , Daniele Tabacco
发明人： Valter Bellucci , Peter Flohr , Christian Oliver Paschereit , Bruno Schuermans , Daniele Tabacco
CPC分类号： F23D11/402 , F23M20/005 , F23R3/286 , F23R2900/00014 , F23R2900/03341
摘要： A reheat combustion system for a gas turbine comprises a mixing tube adapted to be fed by products of a primary combustion zone of the gas turbine and by fuel injected by a lance; a combustion chamber fed by the said mixing tube; and at least one perforated acoustic screen. The or each said acoustic screen is provided inside the mixing tube or the combustion chamber, at a position where it faces, but is spaced from, a perforated wall thereof. In use, the perforated wall experiences impingement cooling as it admits air into the combustion system for onward passage through the perforations of the said acoustic screen, and the acoustic screen damps acoustic pulsations in the mixing tube and combustion chamber.
摘要翻译： 用于燃气轮机的再热燃烧系统包括适于由燃气轮机的主燃烧区的产物和由喷枪喷射的燃料供给的混合管; 由所述混合管供给的燃烧室; 和至少一个穿孔声屏。 所述或每个所述声屏被设置在所述混合管或所述燃烧室内部，所述位于与所述混合管或所述燃烧室相对的位置，但与其穿孔壁相对。 在使用中，穿孔壁经受冲击冷却，因为它允许空气进入燃烧系统，以便先前通过所述声屏幕的穿孔，并且声屏蔽物阻止混合管和燃烧室中的声脉冲。
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公开(公告)号：US20060228658A1
公开(公告)日：2006-10-12
申请号：US11279421
申请日：2006-04-12
IPC分类号： F23N5/00
CPC分类号： G01N33/2829 , F23M20/005 , F23N5/16 , F23R2900/00013 , G01N25/50 , G01N2291/02872
摘要： A sensor 11 detects the acoustic pressure at a first location in a combustion chamber 7 of a test rig 1 and produces an input signal which is a function of the acoustic pressure. A controller 13 receives the input signal and produces an output signal which is a function of the input signal. An acoustic actuator (16-18) receives the output signal and introduces into the combustion chamber 7 at a second location an acoustic pressure which is a function of the output signal. The acoustic actuator may comprise a fuel injector 18 or a loudspeaker. By using an appropriate control algorithm, acoustic boundary conditions corresponding to a particular gas turbine combustion chamber may be produced, at least in a certain frequency range,
摘要翻译： 传感器11检测试验台1的燃烧室7中的第一位置处的声压，并产生作为声压的函数的输入信号。 控制器13接收输入信号并产生作为输入信号的函数的输出信号。 声学致动器（16-18）接收输出信号，并在第二位置处将作为输出信号的函数的声压引入燃烧室7。 声学致动器可以包括燃料喷射器18或扬声器。 通过使用适当的控制算法，可以至少在一定频率范围内产生对应于特定燃气轮机燃烧室的声学边界条件，
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公开(公告)号：US09285123B2
公开(公告)日：2016-03-15
申请号：US11693951
申请日：2007-03-30
CPC分类号： F23R3/346 , F02C7/228 , F02C9/34 , F02C9/40 , F23N5/022 , F23N2025/04 , F23N2025/06 , F23N2025/26 , F23N2037/02 , F23R3/36
摘要： A burner system with staged fuel injection includes at least one burner with a mixing zone. A combustion chamber is disposed downstream of the mixing zone and a first fuel introduction device is provided upstream of the mixing zone. Furthermore, a second fuel introduction device for the direct injection of fuel into the combustion chamber, is disposed downstream of the mixing zone. In addition, at least one sensor for determining combustion parameters is connected to a control device. The control device is designed to control the second fuel introduction device as a function of the parameters determined by the sensors.
摘要翻译： 具有分级燃料喷射的燃烧器系统包括具有混合区域的至少一个燃烧器。 燃烧室设置在混合区的下游，并且第一燃料引入装置设置在混合区的上游。 此外，用于将燃料直接喷射到燃烧室中的第二燃料引入装置设置在混合区的下游。 此外，用于确定燃烧参数的至少一个传感器连接到控制装置。 控制装置被设计成根据由传感器确定的参数来控制第二燃料引入装置。
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公开(公告)号：US20070238059A1
公开(公告)日：2007-10-11
申请号：US11693951
申请日：2007-03-30
CPC分类号： F23R3/346 , F02C7/228 , F02C9/34 , F02C9/40 , F23N5/022 , F23N2025/04 , F23N2025/06 , F23N2025/26 , F23N2037/02 , F23R3/36
摘要： A burner system with staged fuel injection includes at least one burner with a mixing zone. A combustion chamber is disposed downstream of the mixing zone and a first fuel introduction device is provided upstream of the mixing zone. Furthermore, a second fuel introduction device for the direct injection of fuel into the combustion chamber, is disposed downstream of the mixing zone. In addition, at least one sensor for determining combustion parameters is connected to a control device. The control device is designed to control the second fuel introduction device as a function of the parameters determined by the sensors.
摘要翻译： 具有分级燃料喷射的燃烧器系统包括具有混合区域的至少一个燃烧器。 燃烧室设置在混合区的下游，并且第一燃料引入装置设置在混合区的上游。 此外，用于将燃料直接喷射到燃烧室中的第二燃料引入装置设置在混合区的下游。 此外，用于确定燃烧参数的至少一个传感器连接到控制装置。 控制装置被设计成根据由传感器确定的参数来控制第二燃料引入装置。
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公开(公告)号：US20110027732A1
公开(公告)日：2011-02-03
申请号：US12846087
申请日：2010-07-29
申请人： Pirmin SCHIESSEL , Bruno Schuermans , Zdenko Papa , Norbert Emberger , Adnan Eroglu , Rainer Conzelmann , Luca Tentorio
发明人： Pirmin SCHIESSEL , Bruno Schuermans , Zdenko Papa , Norbert Emberger , Adnan Eroglu , Rainer Conzelmann , Luca Tentorio
IPC分类号： F23C7/00
CPC分类号： F23D11/38 , F23C2900/07002 , F23C2900/07021 , F23D17/002 , F23R3/286 , F23R2900/00014
摘要： The burner of a gas turbine includes two or more part cone shells arranged offset with respect to one another and defining a cone shaped chamber with longitudinal tangential slots for feeding air therein. A lance carrying a liquid fuel nozzle arranged centrally in the cone shaped chamber is also provided. A portion of the nozzle facing the cone shaped chamber is divergent in shape. A diffuser angle (α) between the wall of the nozzle and a longitudinal axis of the cone shaped chamber is less than 5°. A diverging portion of the nozzle has a diffuser length to nozzle diameter ratio comprised between 2-6. The nozzle diameter is the smaller diameter of the diverging portion.
摘要翻译： 燃气涡轮机的燃烧器包括相对于彼此偏移设置的两个或多个锥形壳体，并且限定具有用于在其中进给空气的纵向切向槽的锥形室。 还提供了一种携带液体燃料喷嘴的喷枪，其中心地配置在锥形室中。 面对锥形腔的喷嘴的一部分的形状是发散的。 喷嘴壁与锥形腔的纵向轴线之间的扩散角（α）小于5°。 喷嘴的发散部分的扩散器长度与喷嘴直径之比在2-6之间。 喷嘴直径是发散部分的较小直径。
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