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公开(公告)号：US07972133B2
公开(公告)日：2011-07-05
申请号：US12238792
申请日：2008-09-26
IPC分类号： F23Q9/00
CPC分类号： F23D17/002 , F23C7/008 , F23C2900/07002 , F23R3/343
摘要： A burner (23) for operating a heat generator includes a swirler (2) for a combustion air flow (9), and also devices (7, 12) for injecting at least one fuel into the combustion air flow (9), wherein a mixing path (3) is arranged downstream of the swirler (2), and wherein at least one nozzle (20) for feeding liquid pilot fuel is arranged in the region radially outside the discharge opening of the mixing path (3) of the burner. With such a burner, an operating mode which is as pollutant-free and overheating-free as possible can be enabled even at low load and under transient conditions if the at least one nozzle (20) is arranged in a burner front plate (32), wherein at least one discharge opening (15), through which the pilot fuel discharges into the combustion chamber (16), is provided in a front face (34) of the burner front plate (32), which is arranged essentially parallel to a combustion chamber rear wall (28).
摘要翻译： 用于操作发热器的燃烧器（23）包括用于燃烧空气流（9）的旋流器（2），以及用于将至少一种燃料喷射到燃烧空气流（9）中的装置（7,12），其中 混合路径（3）布置在旋流器（2）的下游，并且其中用于供给液体引燃燃料的至少一个喷嘴（20）布置在燃烧器的混合路径（3）的排出口径向外侧的区域中。 通过这样的燃烧器，即使在低负载和瞬态条件下，如果至少一个喷嘴（20）布置在燃烧器前板（32）中，也可以实现尽可能无污染和过热的操作模式， 其特征在于，在所述燃烧器前板（32）的前表面（34）上设置有至少一个排气口（15），其中所述先导燃料排出到所述燃烧室（16）中，所述排放口基本上平行于 燃烧室后壁（28）。
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2.发明授权Premix burner with staged liquid fuel supply and also method for operating a premix burner 有权具有分段液体燃料供应的预混燃烧器以及操作预混燃烧器的方法公开(公告)号：US07997896B2
公开(公告)日：2011-08-16
申请号：US11635002
申请日：2006-12-07
申请人： Peter Flohr , Gijsbertus Oomens , Martin Zajadatz
发明人： Peter Flohr , Gijsbertus Oomens , Martin Zajadatz
IPC分类号： F23D14/62
CPC分类号： F23R3/36 , F23C2900/07002 , F23D11/402 , F23D14/02 , F23D17/002 , F23R3/286
摘要： A premix burner with staged liquid fuel supply is described having at least two partial cone shells which on the radial side form the boundary of a swirl chamber which axialwards conically widens, which partial cone shells are arranged in a partially overlapping manner, the center axes of the partial cone shells of which extend with offset effect in relation to each another, and the mutually overlapping partial cone shell sections of which enclose in each case an air inlet slot which extends tangentially to the swirl chamber, with a burner lance which projects axialwards into the swirl chamber, which lance provides means for feed of liquid fuel into the swirl chamber, and also with further means for feed of liquid fuel which are provided in the region of the air inlet slots. As such, additional means for feed of liquid fuel along at least one air inlet slot are formed and arranged in such a way that the liquid fuel delivery, which is conditioned by the further means, takes place in the form of a fuel spray which propagates perpendicularly to the tangential longitudinal extent of the air inlet slot, and also a fuel spray which propagates perpendicularly to an air flow which is directed through the air inlet slot.
摘要翻译： 描述了具有分级液体燃料供应的预混合燃烧器，其具有至少两个部分锥形壳体，其在径向侧上形成旋转室的边界，该旋转室的轴向圆锥形加宽，该部分锥形壳体以部分重叠的方式布置， 其部分锥形壳体相对于彼此具有偏移效应而延伸，并且其相互重叠的部分锥形壳体部分在每种情况下包围空气入口狭槽，该空气入口狭槽与涡流室相切地延伸，燃烧器喷枪将轴向突出 旋转室，该喷枪提供用于将液体燃料供给到涡流室中的装置，以及用于供给液体燃料的进一步装置，该装置设置在进气口的区域中。 因此，沿着至少一个空气入口狭槽进料液体燃料的附加装置被形成和布置成使得由其它装置调节的液体燃料输送以燃料喷雾的形式发生，该燃料喷雾传播 垂直于空气入口狭槽的切向纵向范围，以及与引导通过进气口的空气流垂直地传播的燃料喷雾。
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3.发明申请Premix burner with staged liquid fuel supply and also method for operating a premix burner 有权具有分段液体燃料供应的预混燃烧器以及操作预混燃烧器的方法公开(公告)号：US20070099142A1
公开(公告)日：2007-05-03
申请号：US11635002
申请日：2006-12-07
申请人： Peter Flohr , Gijsbertus Oomens , Martin Zajadatz
发明人： Peter Flohr , Gijsbertus Oomens , Martin Zajadatz
IPC分类号： F23D14/62
CPC分类号： F23R3/36 , F23C2900/07002 , F23D11/402 , F23D14/02 , F23D17/002 , F23R3/286
摘要： A premix burner with staged liquid fuel supply is described having at least two partial cone shells which on the radial side form the boundary of a swirl chamber which axialwards conically widens, which partial cone shells are arranged in a partially overlapping manner, the center axes of the partial cone shells of which extend with offset effect in relation to each another, and the mutually overlapping partial cone shell sections of which enclose in each case an air inlet slot which extends tangentially to the swirl chamber, with a burner lance which projects axialwards into the swirl chamber, which lance provides means for feed of liquid fuel into the swirl chamber, and also with further means for feed of liquid fuel which are provided in the region of the air inlet slots. As such, additional means for feed of liquid fuel along at least one air inlet slot are formed and arranged in such a way that the liquid fuel delivery, which is conditioned by the further means, takes place in the form of a fuel spray which propagates perpendicularly to the tangential longitudinal extent of the air inlet slot, and also a fuel spray which propagates perpendicularly to an air flow which is directed through the air inlet slot.
摘要翻译： 描述了具有分级液体燃料供应的预混合燃烧器，其具有至少两个部分锥形壳体，其在径向侧上形成旋转室的边界，该旋转室的轴向向锥面变宽，该部分锥形壳体以部分重叠的方式布置， 其部分锥形壳体相对于彼此具有偏移效应而延伸，并且其相互重叠的部分锥形壳体部分在每种情况下包围空气入口狭槽，该空气入口狭槽与涡流室相切地延伸，燃烧器喷枪将轴向突出 旋转室，该喷枪提供用于将液体燃料供给到涡流室中的装置，以及用于供给液体燃料的进一步装置，该装置设置在进气口的区域中。 因此，沿着至少一个空气入口狭槽进料液体燃料的附加装置被形成和布置成使得由其它装置调节的液体燃料输送以燃料喷雾的形式发生，该燃料喷雾传播 垂直于空气入口狭槽的切向纵向范围，以及与引导通过进气口的空气流垂直地传播的燃料喷雾。
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公开(公告)号：US20090081599A1
公开(公告)日：2009-03-26
申请号：US12238792
申请日：2008-09-26
IPC分类号： F23D11/00
CPC分类号： F23D17/002 , F23C7/008 , F23C2900/07002 , F23R3/343
摘要： A burner (23) for operating a heat generator includes a swirler (2) for a combustion air flow (9), and also devices (7, 12) for injecting at least one fuel into the combustion air flow (9), wherein a mixing path (3) is arranged downstream of the swirler (2), and wherein at least one nozzle (20) for feeding liquid pilot fuel is arranged in the region radially outside the discharge opening of the mixing path (3) of the burner. With such a burner, an operating mode which is as pollutant-free and overheating-free as possible can be enabled even at low load and under transient conditions if the at least one nozzle (20) is arranged in a burner front plate (32), wherein at least one discharge opening (15), through which the pilot fuel discharges into the combustion chamber (16), is provided in a front face (34) of the burner front plate (32), which is arranged essentially parallel to a combustion chamber rear wall (28).
摘要翻译： 用于操作发热器的燃烧器（23）包括用于燃烧空气流（9）的旋流器（2），以及用于将至少一种燃料喷射到燃烧空气流（9）中的装置（7,12），其中 混合路径（3）布置在旋流器（2）的下游，并且其中用于供给液体引燃燃料的至少一个喷嘴（20）布置在燃烧器的混合路径（3）的排出口径向外侧的区域中。 通过这样的燃烧器，即使在低负载和瞬态条件下，如果至少一个喷嘴（20）布置在燃烧器前板（32）中，也可以实现尽可能无污染和过热的操作模式， 其特征在于，在所述燃烧器前板（32）的前表面（34）上设置有至少一个排气口（15），其中所述先导燃料排出到所述燃烧室（16）中，所述排放口基本上平行于 燃烧室后壁（28）。
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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：US20060183069A1
公开(公告)日：2006-08-17
申请号：US11237848
申请日：2005-09-29
IPC分类号： F23D14/62
CPC分类号： F23R3/286 , F23C2900/07002 , F23D17/002 , F23R2900/00014
摘要： A premix burner includes a vortex generator (30) for combustion air stream (15), devices (17, 17a, 17b, 31-38, 41-48) to inject fuel into the combustion air stream (15), and tangential air ducts (19, 20). The combustion air (15) enters the cone cavity (14) of the vortex generator (30) via the air ducts. The injection of the fuel into the combustion air is done asymmetrically by injection devices (17, 17a, 17b, 31-38, 41-48). At least one of the injection devices (5) is arranged on a fuel lance (3) that extends into the vortex chamber.
摘要翻译： 预混燃烧器包括用于燃烧空气流（15）的涡流发生器（30），将燃料喷射到燃烧空气流（15）中的装置（17,17a，17b，31-38,41,48）和切向 风道（19,20）。 燃烧空气（15）经由空气管道进入涡流发生器（30）的锥形空腔（14）。 通过注射装置（17,17a，17b，31-38,41,48）不对称地将燃料喷射到燃烧空气中。 至少一个注射装置（5）布置在延伸到涡流室中的燃料喷枪（3）上。
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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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8.发明申请Injector for Liquid Fuel, and Staged Premix Burner Having This Injector 审中-公开液体燃料喷射器，以及具有该喷射器的分段预混燃烧器公开(公告)号：US20070231762A1
公开(公告)日：2007-10-04
申请号：US11560936
申请日：2006-11-17
申请人： Stefano Bernero , Christian Motz , Tom Strebel , Martin Zajadatz
发明人： Stefano Bernero , Christian Motz , Tom Strebel , Martin Zajadatz
IPC分类号： F23D14/46
CPC分类号： F23R3/343 , F23C2900/07002 , F23C2900/07021 , F23D11/107 , F23D11/16 , F23D11/383 , F23D2900/00015 , F23R3/286
摘要： An injector (4) for liquid fuel (6a) and a premix burner, in particular for combustion chambers of gas turbines which burner includes an injector (4) of this type, includes a swirl nozzle (14) which is surrounded by a shielding-air passage (11) and has an enlarged cross section of flow in the region of a nozzle-internal swirl generator (12) for the liquid fuel (6a), with this enlarged cross section of flow being reduced again toward an exit opening of the swirl nozzle (14). The injector allows the premix burner to operate with a reduced admission pressure and a high atomization quality.
摘要翻译： 一种用于液体燃料的喷射器（4）和一个预混燃烧器，特别是燃气轮机的燃烧室，燃烧器包括这种类型的喷射器（4），其包括旋转喷嘴（14），其被屏蔽 （11），并且在用于液体燃料（6a）的喷嘴内部旋流发生器（12）的区域中具有扩大的流动横截面，该扩大的横截面再次朝向出口 的旋转喷嘴（14）。 喷射器允许预混合燃烧器以降低的入口压力和高雾化质量进行操作。
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公开(公告)号：US07780437B2
公开(公告)日：2010-08-24
申请号：US11237848
申请日：2005-09-29
CPC分类号： F23R3/286 , F23C2900/07002 , F23D17/002 , F23R2900/00014
摘要： A premix burner includes a vortex generator (30) for combustion air stream (15), devices (17, 17a, 17b, 31-38, 41-48) to inject fuel into the combustion air stream (15), and tangential air ducts (19, 20). The combustion air (15) enters the cone cavity (14) of the vortex generator (30) via the air ducts. The injection of the fuel into the combustion air is done asymmetrically by injection devices (17, 17a, 17b, 31-38, 41-48). At least one of the injection devices (5) is arranged on a fuel lance (3) that extends into the vortex chamber.
摘要翻译： 预混燃烧器包括用于燃烧空气流（15）的涡流发生器（30），用于向燃烧空气流（15）喷射燃料的装置（17,17a，17b，31-38,41-48），以及切向风道 （19,20）。 燃烧空气（15）经由空气管道进入涡流发生器（30）的锥形空腔（14）。 通过注射装置（17,17a，17b，31-38,41-48）不对称地将燃料喷射到燃烧空气中。 至少一个喷射装置（5）布置在延伸到涡流室中的燃料喷枪（3）上。
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公开(公告)号：US20050106522A1
公开(公告)日：2005-05-19
申请号：US10931052
申请日：2004-09-01
CPC分类号： F23C7/002 , F23C2900/07002 , F23D11/402 , F23D17/002
摘要： A burner includes a swirl generator (3) for a combustion airflow, has a conical swirl chamber (2) and a device for admitting fuel into the combustion airflow, wherein the swirl generator (3) incorporates combustion air inlet openings for the combustion airflow tangentially entering into the conical swirl chamber (2), and wherein the device for admitting fuel into the combustion airflow includes a first fuel feeding device having a first group (4) of fuel outlet openings substantially disposed in the direction of the burner axis for a first premix fuel quantity. The burner incorporates at least one second fuel feeding device having at least one second group (5) of fuel outlet openings that are substantially disposed in the direction of the burner axis for a second premix fuel quantity, which can be supplied with fuel independently from the first fuel feeding device, a burner lance (6) along a burner axis (A) projects from the side of the swirl chamber (2) with the smallest swirl chamber cross section into the swirl chamber (2), and the device for supplying fuel into the combustion airflow additionally incorporates at least one fuel outlet opening (8) within the burner lance (6), through which fuel is dischargeable along the burner axis.
摘要翻译： 燃烧器包括用于燃烧气流的涡流发生器（3），具有锥形涡流室（2）和用于将燃料引入燃烧气流中的装置，其中涡流发生器（3）将燃烧空气入口与燃烧气流相切地并入 进入锥形涡流室（2），并且其中用于将燃料引入燃烧空气流的装置包括第一燃料供给装置，其具有基本上沿着燃烧器轴线的方向设置的燃料出口的第一组（4），用于第一 预混燃料量。 燃烧器包括至少一个第二燃料供给装置，其具有燃料出口开口的至少一个第二组（5），其基本上设置在燃烧器轴线的方向上用于第二预混合燃料量，其可独立于燃料供给装置 第一燃料供给装置，沿着燃烧器轴线（A）的燃烧器喷枪（6）从具有最小涡旋室横截面的涡流室（2）的侧面突出到涡流室（2）中，并且用于供给燃料的装置 进入燃烧气流中还包括在燃烧器喷枪（6）内的至少一个燃料出口（8），燃料可以通过燃烧器轴线排出。
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