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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：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：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：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：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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公开(公告)号：US20060101825A1
公开(公告)日：2006-05-18
申请号：US11214919
申请日：2005-08-31
IPC分类号： F23R3/30
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：US20050084811A1
公开(公告)日：2005-04-21
申请号：US10470557
申请日：2002-01-30
申请人： Dirk Bueche , Rolf Dornberger , Petros Koumoutsakos , Christian Paschereit , Bruno Schuermans , Peter Stoll
发明人： Dirk Bueche , Rolf Dornberger , Petros Koumoutsakos , Christian 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是 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：US08931589B2
公开(公告)日：2015-01-13
申请号：US13152499
申请日：2011-06-03
IPC分类号： F01N13/02
CPC分类号： F23M99/005 , F23M20/005 , F23R2900/00014
摘要： A damper arrangement (10) has a first Helmholtz damper (11) connected in series to a second Helmholtz damper (12). The resonance frequency of the first Helmholtz damper (11) and the resonance frequency of the second Helmholtz damper (12) are shifted from one another in an amount producing a synergic damping effect.
摘要翻译： 阻尼器装置（10）具有与第二亥姆霍兹阻尼器（12）串联连接的第一亥姆霍兹阻尼器（11）。 第一亥姆霍兹阻尼器（11）的共振频率和第二亥姆霍兹阻尼器（12）的共振频率以产生协同阻尼效应的量相互偏移。
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9.发明授权Helmholtz damper and method for regulating the resonance frequency of a Helmholtz damper 有权亥姆霍兹阻尼器和用于调节亥姆霍兹阻尼器谐振频率的方法公开(公告)号：US08727070B2
公开(公告)日：2014-05-20
申请号：US13158896
申请日：2011-06-13
申请人： Andreas Huber , Mirko Bothien , Nicolas Noiray , Bruno Schuermans
发明人： Andreas Huber , Mirko Bothien , Nicolas Noiray , Bruno Schuermans
CPC分类号： F23M20/005 , F23D2210/00 , F23R2900/00014 , Y10T137/0396 , Y10T137/7781
摘要： A Helmholtz damper, including an enclosure, a neck extending from the enclosure, and a pipe for inserting into the neck. The portions of the pipe inserted into the neck is adjusted to regulate a resonance frequency of the Helmholtz damper.
摘要翻译： 亥姆霍兹阻尼器，包括外壳，从外壳延伸的颈部和用于插入颈部的管道。 插入颈部的管道部分被调节以调节亥姆霍兹阻尼器的共振频率。
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10.发明申请METHOD FOR PROTECTING A GAS TURBINE ENGINE AGAINST HIGH DYNAMICAL PROCESS VALUES AND GAS TURBINE ENGINE FOR CONDUCTING THE METHOD 有权用于保护气体涡轮发动机的高动态过程值和气体涡轮发动机的方法，用于驱动该方法公开(公告)号：US20120279229A1
公开(公告)日：2012-11-08
申请号：US13462920
申请日：2012-05-03
IPC分类号： F02C9/00
CPC分类号： F02C9/28 , F02C7/057 , F02C9/48 , F05D2260/80 , F05D2260/96 , F05D2270/11 , F05D2270/14 , F23N5/16 , F23N5/242 , F23R2900/00013
摘要： A method can protect a gas turbine engine (10), which includes a compressor (11), a combustor (13), and a turbine (12), against high dynamical process values, especially in combustor/flame pulsations. Effective protection against high dynamical process values, especially in combustor/flame pulsations, can be achieved by: a) measuring the pulsations of the combustor (13) with a suitable sensor (18), b) dividing the frequency spectrum of the measured pulsation signal up into pre-defined band pass sections, c) computing the rms (root mean square) of the signal for each band, d) weighting the computed frequency/frequency band rms with predetermined weighting factors, e) cumulating the weighted frequency/frequency band rms values to get a Pulsation Limit Criterion (PLC) value, f) comparing the PLC value with at least one reference value (23), and g) operating the gas turbine engine (10) according to the result of the comparison.
摘要翻译： 一种方法可以防止包括压缩机（11），燃烧器（13）和涡轮（12）的燃气涡轮发动机（10），抵抗高动力学过程值，特别是在燃烧器/火焰脉动中。 可以通过以下方式来实现对高动力过程值的有效保护，特别是在燃烧器/火焰脉动中：a）用合适的传感器（18）测量燃烧器（13）的脉动，b）将所测量的脉动信号的频谱 c）计算每个频带的信号的均方根（均方根），d）用预定的加权因子对所计算的频率/频带rms进行加权，e）累积加权的频率/频带 rms值以获得脉冲限制标准（PLC）值，f）将PLC值与至少一个参考值（23）进行比较，以及g）根据比较结果来操作燃气涡轮发动机（10）。
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