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1. 发明授权

US6164058A Arrangement for damping combustion-chamber oscillations 失效
标题翻译：阻尼燃烧室振荡的布置
公开(公告)号：US6164058A
公开(公告)日：2000-12-26
申请号：US111779
申请日：1998-07-08
申请人： Klaus Dobbeling , Christian Paschereit , Wolfgang Polifke
发明人： Klaus Dobbeling , Christian Paschereit , Wolfgang Polifke
IPC分类号： F02C7/045 , F23R3/00 , F23R3/04 , F23R3/50
CPC分类号： F23R3/005 , F02C7/045 , F05D2260/96 , F23R2900/00014 , F23R2900/03041
摘要： In an annular combustion chamber for a gas turbine, a combustion-chamber dome (14) is arranged upstream of an air-cooled combustion chamber (10). A first portion of an air flow (46) which comes from the compressor is admixed as combustion air to the combustion operation and cooling ducts (22; 24) feed a second portion of the air flow (46) coming from the compressor as cooling air into the combustion chamber (10). In this case, the cooling ducts (22; 24), which run at least in sections along the combustion chamber (10), have an entry (23; 25) into the combustion-chamber dome (14). The cooling ducts (22; 24) are designed for damping combustion-chamber oscillations in such a way that the acoustic impedance at the entry (23; 25) of the cooling ducts (22; 24) into the combustion-chamber dome (14) is minimized.
摘要翻译：在用于燃气轮机的环形燃烧室中，燃烧室拱顶（14）布置在空气冷却燃烧室（10）的上游。将来自压缩机的空气流（46）的第一部分作为燃烧空气混合到燃烧操作中，冷却管道（22; 24）将来自压缩机的空气流（46）的第二部分作为冷却空气进入燃烧室（10）中。在这种情况下，至少沿着燃烧室（10）的部分运行的冷却管道（22; 24）具有进入燃烧室拱顶（14）的入口（23; 25）。冷却管道（22; 24）设计成用于阻止燃烧室振荡，使得冷却管道（22; 24）入口（23; 25）入口（29; 25）内的声阻抗进入燃烧室穹顶（14）被最小化。

2. 发明申请

US20070059655A1 Premix burner with a swirl generator delimiting a conical swirl space and having sensor monitoring 有权
标题翻译：具有涡流发生器的预混合燃烧器限定圆锥形漩涡空间并具有传感器监测功能
公开(公告)号：US20070059655A1
公开(公告)日：2007-03-15
申请号：US11502468
申请日：2006-08-11
申请人： Philipp Brunner , Jaan Hellat , Christian Paschereit
发明人： Philipp Brunner , Jaan Hellat , Christian Paschereit
IPC分类号： F23M3/00
CPC分类号： F23C7/002 , F23D14/46 , F23N5/022 , F23N2041/20
摘要： A premix burner is disclosed, with a swirl generator which delimits a conical swirl space and provides at least two conical part shells which are arranged, offset to one another, along a burner axis, mutually enclose in each case air inlet slits running longitudinally with respect to the burner axis and have in combination a conically widening premix burner outer contour having a maximum outside diameter which narrows axially into a region with a minimum outside diameter. At least one conical part shell provides, in the region between the maximum and the minimum outside diameter, a reception unit which deviates from the conically widening premix burner outer contour and locally elevates the premix burner outer contour radially outward and which has a maximum radial extent which is dimensioned smaller than half the maximum outside diameter of the premix burner outer contour. Within the reception unit, at least one hollow duct is provided, with at least one duct orifice facing away from the swirl space and with a duct longitudinal extent which runs essentially parallel to the burner axis.
摘要翻译：公开了一种预混合燃烧器，其具有涡流发生器，其限定圆锥形漩涡空间并且提供沿着燃烧器轴线彼此偏移地设置的至少两个锥形部分壳体，每个壳体相互包围相对于纵向延伸的空气入口狭缝并且组合有锥形加宽的预混合燃烧器外轮廓，其具有最大外径，其将轴向变窄成具有最小外径的区域。至少一个锥形部分壳体在最大外径和最小外径之间的区域中提供接收单元，该接收单元偏离锥形加宽的预混燃烧器外轮廓并且将预混合器外轮廓径向向外提升并具有最大径向范围其尺寸小于预混合燃烧器外轮廓的最大外径的一半。在接收单元内，提供至少一个中空管道，其中至少一个管道孔口背离涡流空间，并具有基本上平行于燃烧器轴线延伸的管道纵向延伸部分。

3. 发明申请

US20050019713A1 Method and device for affecting thermoacoustic oscillations in combustion systems 有权
标题翻译：影响燃烧系统热声振荡的方法和装置
公开(公告)号：US20050019713A1
公开(公告)日：2005-01-27
申请号：US10725562
申请日：2003-12-03
申请人： Ephraim Gutmark , Christian Paschereit
发明人： Ephraim Gutmark , Christian Paschereit
IPC分类号： F23C9/00 , F23M99/00 , F23C11/04
CPC分类号： F23C9/006 , F23C2900/07002 , F23K2900/05003 , F23M20/005 , F23R2900/00013
摘要： The present invention relates to a method and a device for affecting thermoacoustic oscillations in a combustion system (1) comprising at least one burner (2) and at least one combustor (3), modulated injection of fuel being carried out. In order to improve the action of affecting the thermoacoustic oscillations, the modulated injection of the fuel is carried out into a recirculation zone (7) which forms in the combustor (3).
摘要翻译：本发明涉及一种用于影响燃烧系统（1）中的热声振荡的方法和装置，该燃烧系统（1）包括至少一个燃烧器（2）和至少一个燃烧器（3），所述燃烧系统（1）被执行调节的燃料喷射。为了改善影响热声振动的作用，燃料的调节喷射被进入在燃烧器（3）中形成的再循环区（7）。

4. 发明申请

US20050016181A1 Method and device for affecting thermoacoustic oscillations in combustion systems 审中-公开
标题翻译：影响燃烧系统热声振荡的方法和装置
公开(公告)号：US20050016181A1
公开(公告)日：2005-01-27
申请号：US10725564
申请日：2003-12-03
申请人： Ephraim Gutmark , Christian Paschereit
发明人： Ephraim Gutmark , Christian Paschereit
IPC分类号： F23R3/28 , F02C6/04
CPC分类号： F23R3/28 , F05B2260/96 , F23C2205/10 , F23N5/082 , F23R2900/00014
摘要： The present invention relates to a method and a device (1) for affecting thermoacoustic oscillations in a combustion system (5) comprising at least one burner (6) and at least one combustor (7), a gas flow forming in the region of the burner (6) being excited acoustically and/or modulated injection of fuel being carried out. In order to improve the action of affecting the thermoacoustic oscillations, the acoustic excitations of the gas flow and/or the modulated injections of the fuel are coordinated in order to affect at least two different interference frequencies of the thermoacoustic oscillations.
摘要翻译：本发明涉及一种用于影响燃烧系统（5）中的热声振荡的方法和装置（1），其包括至少一个燃烧器（6）和至少一个燃烧器（7），在所述燃烧系统燃烧器（6）被进行声学和/或调制的燃料喷射。为了改善影响热声振荡的作用，气体流的声学激发和/或调节的燃料喷射被协调以便影响热声振荡的至少两个不同的干扰频率。

5. 发明申请

US20060154192A1 Burner with stepped fuel injection 有权
标题翻译：带燃油喷射器的燃烧器
公开(公告)号：US20060154192A1
公开(公告)日：2006-07-13
申请号：US10874161
申请日：2004-06-24
申请人： Peter Flohr , Christian Paschereit
发明人： Peter Flohr , Christian Paschereit
IPC分类号： F23C7/00 , F23M3/00 , F23C5/00
CPC分类号： F23R3/286 , F23C2900/07002 , F23R2900/00014
摘要： In a burner (1) having an interior space (22) surrounded by at least one shell (8, 9) in which burner (1) fuel is injected through fuel nozzles (6) arranged at the burner shells (8, 9) into a combustion air stream (23) flowing within the interior space (22), the fuel/air mix which is formed flows to a flame front (3) in a combustion chamber (2) within a delay time (τ), where it is ignited, the formation of combustion-driven thermoacoustic oscillations is avoided by virtue of the fact that means (24), which allow fuel to be injected into the combustion air stream (23) via at least two fuel injection holes (25) distributed over the length of the means (24) are arranged so as to project from the burner base (27) into the interior space (22) substantially in the direction of the combustion chamber (2), so that the delay time (τ) between injection of the fuel and its combustion at the flame front (3) corresponds to a distribution (12) which avoids combustion-driven oscillations in premix operation.
摘要翻译：在具有由至少一个壳体（8,9）围绕的内部空间（22）的燃烧器（1）中，燃烧器（1）通过布置在燃烧器壳体（8,9）处的燃料喷嘴（6）喷射燃料（1）在内部空间（22）内流动的燃烧空气流（23），所形成的燃料/空气混合物在延迟时间（τ）内流动到燃烧室（2）中的火焰前部（3）燃烧驱动的热声振荡的形成由于以下事实而避免：通过分配在上述燃烧驱动的热声振荡中的至少两个燃料喷射孔（25）将燃料喷射到燃烧空气流（23）中的装置（24）装置（24）的长度被布置成基本上沿燃烧室（2）的方向从燃烧器基座（27）突出到内部空间（22）中，使得喷射器燃料及其在火焰前端（3）处的燃烧对应于避免c的分布（12）预混合操作中的振荡驱动振荡。

6. 发明申请

US20050229581A1 REHEAT COMBUSTION SYSTEM FOR A GAS TURBINE 有权
标题翻译：用于气体涡轮机的再燃烧燃烧系统
公开(公告)号：US20050229581A1
公开(公告)日：2005-10-20
申请号：US10460363
申请日：2003-06-13
申请人： Valter Bellucci , Peter Flohr , Christian Paschereit , Bruno Schuermans , Daniele Tabacco
发明人： Valter Bellucci , Peter Flohr , Christian Paschereit , Bruno Schuermans , Daniele Tabacco
IPC分类号： F23D11/40 , F23M99/00 , F23R3/28 , F02C1/06
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 bed 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; 通过所述混合管的燃烧室床; 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。

7. 发明申请

US20060228658A1 APPARATUS AND METHOD FOR TESTING COMBUSTION 有权
标题翻译：用于测试燃烧的装置和方法
公开(公告)号：US20060228658A1
公开(公告)日：2006-10-12
申请号：US11279421
申请日：2006-04-12
申请人： Christian Paschereit , Bruno Schuermans , Martin Zajadatz
发明人： Christian Paschereit , Bruno Schuermans , Martin Zajadatz
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，

8. 发明申请

US20050100846A1 Burner 审中-公开
标题翻译：刻录机
公开(公告)号：US20050100846A1
公开(公告)日：2005-05-12
申请号：US10954482
申请日：2004-10-01
申请人： Ephraim Gutmark , Christian Paschereit
发明人： Ephraim Gutmark , Christian Paschereit
IPC分类号： F23R3/16 , F23R3/28 , F23D11/00
CPC分类号： F23R3/16 , F23C2900/07002 , F23D2210/00 , F23R3/286 , F23R2900/00014
摘要： A burner 1 for a heat generator comprises an outlet 10 connectable to a combustion chamber 9, wherein at least part of an inner surface of the outlet 10 is provided with corrugations 11 which are adapted to facilitate the production of axial vorticity in the region of the outlet 10.
摘要翻译：用于热发生器的燃烧器1包括可连接到燃烧室9的出口10，其中出口10的内表面的至少一部分设置有波纹11，其适于促进在该区域中产生轴向涡度出口10。

9. 发明申请

US20070128564A1 Burner 有权
标题翻译：刻录机
公开(公告)号：US20070128564A1
公开(公告)日：2007-06-07
申请号：US11540636
申请日：2006-10-02
申请人： Christian Paschereit , Bruno Schuermans
发明人： Christian Paschereit , Bruno Schuermans
IPC分类号： F23D14/46
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。

10. 发明申请

US20060218933A1 Method for producing a model-based control device 审中-公开
标题翻译：用于生产基于模型的控制装置的方法
公开(公告)号：US20060218933A1
公开(公告)日：2006-10-05
申请号：US11276005
申请日：2006-02-09
申请人： Bruno Schuermans , Christian Paschereit
发明人： Bruno Schuermans , Christian Paschereit
IPC分类号： F02C7/26
CPC分类号： F23N1/002 , F23N5/16 , F23N5/24 , F23N2041/20 , F23R2900/00013 , G05B17/02
摘要： Relating to a model-based active control system for a gas turbine, a method for obtaining the data that are used for deriving an active closed loop controller for the gas turbine includes splitting the combustion system into a number of submodels. The measurement of some submodels is achieved by system identification on a single burner test facility. Other submodels are then determined by using known acoustic models. The different submodels are subsequently combined to form an acoustic network model that is subsequently used to develop a closed loop controller.
摘要翻译：关于用于燃气轮机的基于模型的主动控制系统，用于获得用于导出用于燃气轮机的主动闭环控制器的数据的方法包括将燃烧系统分解成多个子模型。通过在单个燃烧器测试设备上的系统识别来实现某些子模型的测量。然后通过使用已知的声学模型来确定其它子模型。随后将不同的子模型组合以形成随后用于开发闭环控制器的声学网络模型。

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