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公开(公告)号：US20080070176A1
公开(公告)日：2008-03-20
申请号：US11850849
申请日：2007-09-06
IPC分类号： F23D14/62
CPC分类号： F23D14/02 , F23C7/002 , F23C2900/07002
摘要： A premix burner for producing an ignitable fuel/air mixture has a swirl generator with at least two burner shells (B) which complement one another to form a throughflow body, which in each case have a first burner shell section (1) with a partial cone shape and together enclose an axially conically widening swirl space and which mutually define, in the axial cone longitudinal direction, tangential air inlet slots (LS), through which the combustion feed air (L) passes into the swirl space, in which an axially spreading swirl flow forms, and includes fuel feeds which are arranged at least in sections along the tangentially running air inlet slots (LS). A second burner shell section (8) curved in opposition to the first burner shell section (1), in each case designed in a partial cone shape, is added flush to the first burner shell section (1), a third burner shell section (9) adjoins the second burner shell section (8) flush, the third burner shell section (9) having a curvature tangentially adapted to the second burner shell section (8), and the third burner shell section (9) defines, on the one side in each case, one of the tangential air inlet slots (LS) and provides a leading edge (12) serving for the combustion feed air (L).
摘要翻译： 用于产生可燃燃料/空气混合物的预混合燃烧器具有涡流发生器，其具有至少两个彼此互补的燃烧器壳体（B），以形成通流体，每个燃烧器壳体具有第一燃烧器壳体部分（1） 锥体形状并且一起包围轴向锥形加宽的旋转空间，并且在轴向锥形纵向方向上相互限定切向空气入口狭槽（LS），燃烧进料空气（L）通过该空气入口狭槽进入涡流空间，其中轴向 扩展涡流形式，并且包括至少沿着切向运行的空气入口狭槽（LS）的部分布置的燃料进料。 与第一燃烧器壳体部分（1）相对弯曲的第二燃烧器壳体部分（8）在每种情况下以部分圆锥形状设计，与第一燃烧器壳体部分（1）齐平，第三燃烧器壳体部分 第二燃烧器壳体部分（8）与第二燃烧器壳部分（8）相邻，第三燃烧器壳部分（9）具有切向适合于第二燃烧器壳体部分（8）的曲率，并且第三燃烧器壳体部分（9） 在每个情况下，切向空气入口槽（LS）中的一个并且提供用于燃烧进料空气（L）的前缘（12）。
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公开(公告)号：US20050164138A1
公开(公告)日：2005-07-28
申请号：US11036107
申请日：2005-01-18
申请人： Thomas Ruck , Sasha Savic , Torsten Strand
发明人： Thomas Ruck , Sasha Savic , Torsten Strand
CPC分类号： F23D11/402 , F23C2900/07002 , F23D17/002 , F23R3/343
摘要： A burner (24) which is useful for operating a heat generator includes a first upstream swirl generator (17) capable of swirling a combustion air stream, a device for injecting at least one fuel into the combustion air stream from the upstream swirl generator (17), an exit ring (1) located at the downstream end of the burner (24) at the edge to the combustion chamber (2) where the fuel is burnt, and preferentially a mixing section (20, 21) downstream from the upstream swirl generator (17) having a downstream end, having at least one transfer duct (20) for transferring downstream a flow of combustion air and fuel formed in the upstream swirl generator (17), and having a mixing tube (21) downstream from the at least one transfer duct (20) and receiving flow from the at least one transfer duct (20), wherein the downstream end of the mixing section borders the combustion chamber (2) and is formed by the exit ring (1). Pilot mode operation of such a burner (24) is advantageously and economically made possible by providing a pilot burner system (8, 15, 28, 35) in the exit ring (1) for injecting liquid fuel (27) into the combustion chamber (2).
摘要翻译： 可用于操作发热体的燃烧器（24）包括能够旋转燃烧空气流的第一上游涡流发生器（17），用于将至少一种燃料喷射到来自上游涡流发生器（17）的燃烧空气流中的装置 ），位于燃烧器（24）的下游端的燃烧器（2）的燃烧室（2）的燃烧室的燃烧室（2）的燃烧室（2）的下游端的出口环（1），优选地在上游涡流下游的混合部（20,21） 具有下游端的发电机（17）具有至少一个传送管道（20），用于向上游涡流发生器（17）中形成的燃烧空气和燃料的流动下游传送，并且在其下游具有混合管（21） 至少一个传送管道（20）并且接收来自所述至少一个传送管道（20）的流动，其中所述混合部分的下游端与所述燃烧室（2）相接并由所述出口环（1）形成。 通过在出口环（1）中设置用于将液体燃料（27）喷射到燃烧室（1）中的引燃燃烧器系统（8,15,28,35），有利且经济地实现这种燃烧器（24）的先导模式操作 2）。
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公开(公告)号：US06640545B2
公开(公告)日：2003-11-04
申请号：US10003230
申请日：2001-12-06
申请人： Thomas Ruck , Hans Peter Knoepfel
发明人： Thomas Ruck , Hans Peter Knoepfel
IPC分类号： F02C100
CPC分类号： F23D14/62 , F23C7/002 , F23C9/006 , F23C2900/07002 , F23D11/402 , F23D14/78 , F23D2206/10 , F23D2212/10
摘要： The invention relates to a premix burner with high flame stability for use in a heat producer, preferably in the combustion chamber of a gas turbine. Modern lean operated premix burners make possible very low pollutant emissions, but sometimes operate very close to the extinction limit. To increase the stability of the lean premix combustion by increasing the distance between the flame temperature and the extinction limit temperature, it is proposed according to the invention to arrange a downstream combustion gas mixing section (300) for the burner, which mixing section (300) projects at least partially into the combustion chamber (50) and enables combustion gases from the combustion chamber (50) access to the fuel/air mixture (144) by means of combustion gas inlet openings (311). The added combustion gases (145) are mixed with the fuel/air mixture (144), and in this manner increase its temperature. This increase in temperature results in a significant increase in the flame speed, as a consequence of which the extent of the flame front (123) and the extinction limit temperature of the burner decrease.
摘要翻译： 本发明涉及具有高火焰稳定性的预混合燃烧器，其用于发热体，优选在燃气轮机的燃烧室中。 现代的精简型预混燃烧器使得污染物排放量非常低，但有时运行非常接近灭绝极限。 为了通过增加火焰温度和消光极限温度之间的距离来提高稀薄预混合燃烧的稳定性，根据本发明提出了一种用于燃烧器的下游燃烧气体混合部分（300），该混合部分（300 ）至少部分地突出到燃烧室（50）中并且使来自燃烧室（50）的燃烧气体能够通过燃烧气体入口（311）进入燃料/空气混合物（144）。 添加的燃烧气体（145）与燃料/空气混合物（144）混合，并且以这种方式增加其温度。 这种温度升高导致火焰速度的显着增加，结果是火焰前沿的程度（123）和燃烧器的消光极限温度降低。
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公开(公告)号：US6152726A
公开(公告)日：2000-11-28
申请号：US417846
申请日：1999-10-14
申请人： Thomas Ruck , Hans-Peter Knopfel
发明人： Thomas Ruck , Hans-Peter Knopfel
CPC分类号： F23C7/002 , F23D11/402 , F23C2900/07002
摘要： A burner for operating a heat generator includes a rotation generator (100) for a combustion air stream (115), a device for injecting at least one fuel (112, 116) into the combustion air stream, a number of transition channels (201) for transferring a flow formed in the rotation generator into a mixing pipe (20) located downstream from these transition channels, and a pilot burner system (300) in the lower part of the mixing pipe (20), in which the pilot burner system (300) is in active connection with rotation generators (400) located at the end side of the mixing pipe (20). The interaction between the pilot burner system and rotation generators ensures maximized flame stability in the combustion chamber (30), and a general minimization of pollutant emissions, while increasing the load range for lower pollutants towards smaller loads.
摘要翻译： 一种用于操作发热器的燃烧器包括用于燃烧空气流（115）的旋转发生器（100），用于将至少一种燃料（112,116）喷射到燃烧空气流中的装置，多个过渡通道（201） 用于将形成在所述旋转发生器中的流体转移到位于所述过渡通道下游的混合管道（20）中;以及在所述混合管道（20）的下部中的引燃燃烧器系统（300），其中所述引燃燃烧器系统 300）与位于混合管（20）的端侧的旋转发生器（400）有效连接。 导向燃烧器系统和旋转发生器之间的相互作用确保燃烧室（30）中的最大化的火焰稳定性，以及污染物排放的一般最小化，同时将较低污染物的负载范围增加到较小的负载。
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公开(公告)号：US6059565A
公开(公告)日：2000-05-09
申请号：US178578
申请日：1998-10-26
申请人： Hans Peter Knopfel , Thomas Ruck
发明人： Hans Peter Knopfel , Thomas Ruck
CPC分类号： F23D17/002 , F23C7/002 , F23D14/62 , F23C2900/07002 , F23D2900/14021
摘要： A burner for operating a heat generator, the burner including a swirl generator for a combustion-air flow and a mechanism for injecting at least one fuel into the combustion-air flow, a mixing section arranged downstream of the swirl generator and having a number of transition passages for passing a flow formed in the swirl generator into a mixing tube arranged downstream of the transition passages. The combustion-air flow into the swirl generator flows against turbulence generators, which are located upstream of the injection of the fuel into the combustion-air flow, and the turbulence generators include individual bars set transversely to the combustion-air flow.
摘要翻译： 一种用于操作热发生器的燃烧器，所述燃烧器包括用于燃烧空气流的涡流发生器和用于将至少一种燃料喷射到所述燃烧空气流中的机构;混合部分，布置在所述涡流发生器的下游并具有多个 用于使形成在涡流发生器中的流动通过布置在过渡通道下游的混合管的过渡通道。 进入涡流发生器的燃烧空气流动抵靠湍流发生器，湍流发生器位于将燃料喷射到燃烧空气流中的上游，并且湍流发生器包括横向于燃烧空气流设置的单独的杆。
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公开(公告)号：US6019596A
公开(公告)日：2000-02-01
申请号：US192512
申请日：1998-11-17
申请人： Hans Peter Knopfel , Thomas Ruck
发明人： Hans Peter Knopfel , Thomas Ruck
IPC分类号： F23C7/00 , F23C7/06 , F23D11/40 , F23D14/02 , F23D14/78 , F23D17/00 , F23D14/46 , F02C1/00 , F23D14/62
CPC分类号： F23C7/002 , F23C7/06 , F23D11/402 , F23D14/02 , F23D14/78 , F23D17/002 , F23C2900/07002 , F23D2209/10 , F23D2214/00
摘要： In a burner for operating a combustion chamber, which burner essentially comprises a swirl generator (100), a transition piece (200) arranged downstream of the swirl generator, and a mixing tube (20), transition piece (200) and mixing tube (20) forming the mixing section of the burner and being arranged upstream of a combustion space (30), there are means (302, 303, 304) in the lower region of the mixing tube (20) which bring about cooling of the base plate (305) forming a front wall. The air quantity (307) used here is passed into the flow (40) of the mixing tube (20). A leaner mixing and lower NOx emissions are thereby achieved.
摘要翻译： 在用于操作燃烧室的燃烧器中，该燃烧器基本上包括涡旋发生器（100），设置在涡流发生器下游的过渡件（200）和混合管（20），过渡件（200）和混合管 20）形成燃烧器的混合部分并且布置在燃烧空间（30）的上游，在混合管（20）的下部区域中存在使基板冷却的装置（302,303,304） （305）形成前壁。 这里使用的空气量（307）进入混合管（20）的流（40）。 由此实现了更精细的混合和更低的NOx排放。
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公开(公告)号：US5735687A
公开(公告)日：1998-04-07
申请号：US753330
申请日：1996-11-22
申请人： Hans Peter Knopfel , Thomas Ruck
发明人： Hans Peter Knopfel , Thomas Ruck
CPC分类号： F23D17/002 , F23C7/002 , F23D11/402 , F23C2900/07002
摘要： In a burner which essentially comprises a swirl generator (100) for a combustion-air flow (115) and means for injecting a fuel into the combustion-air flow (115), a mixing section (220) is arranged downstream of the abovementioned swirl generator. This mixing section (220) has inside a first part (200) of the section a number of transition passages (201) which run in the direction of flow and ensure the smooth passing of the flow (40) formed in the swirl generator (100) into a tube (20) arranged downstream. The outlet plane of this tube (20) to the combustion chamber (30) is formed with a breakaway edge which serves to stabilize and enlarge a backflow zone (50) forming downstream.
摘要翻译： 在基本上包括用于燃烧空气流（115）的涡流发生器（100）和用于将燃料喷射到燃烧空气流（115）中的装置的燃烧器中，混合部分（220）布置在上述涡流 发电机。 该混合部分（220）在该部分的第一部分（200）的内部具有多个沿流动方向延伸的过渡通道（201），并且确保形成在涡流发生器（100）中的流动（40）的平滑通过 ）插入到布置在下游的管（20）中。 该管（20）到燃烧室（30）的出口平面形成有用于稳定和扩大形成下游的回流区（50）的分离边。
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公开(公告)号：US07632091B2
公开(公告)日：2009-12-15
申请号：US11850849
申请日：2007-09-06
IPC分类号： F23D14/46
CPC分类号： F23D14/02 , F23C7/002 , F23C2900/07002
摘要： A premix burner for producing an ignitable fuel/air mixture has a swirl generator with at least two burner shells (B) which complement one another to form a throughflow body, which in each case have a first burner shell section (1) with a partial cone shape and together enclose an axially conically widening swirl space and which mutually define, in the axial cone longitudinal direction, tangential air inlet slots (LS), through which the combustion feed air (L) passes into the swirl space, in which an axially spreading swirl flow forms, and includes fuel feeds which are arranged at least in sections along the tangentially running air inlet slots (LS). A second burner shell section (8) curved in opposition to the first burner shell section (1), in each case designed in a partial cone shape, is added flush to the first burner shell section (1), a third burner shell section (9) adjoins the second burner shell section (8) flush, the third burner shell section (9) having a curvature tangentially adapted to the second burner shell section (8), and the third burner shell section (9) defines, on the one side in each case, one of the tangential air inlet slots (LS) and provides a leading edge (12) serving for the combustion feed air (L).
摘要翻译： 用于产生可燃燃料/空气混合物的预混合燃烧器具有涡流发生器，其具有至少两个彼此互补的燃烧器壳体（B），以形成通流体，每个燃烧器壳体具有第一燃烧器壳体部分（1） 锥体形状并且一起包围轴向锥形加宽的旋转空间，并且在轴向锥形纵向方向上相互限定切向空气入口狭槽（LS），燃烧进料空气（L）通过该空气入口狭槽进入涡流空间，其中轴向 扩展涡流形式，并且包括至少沿着切向运行的空气入口狭槽（LS）的部分布置的燃料进料。 与第一燃烧器壳体部分（1）相对弯曲的第二燃烧器壳体部分（8）在每种情况下以部分圆锥形状设计，与第一燃烧器壳体部分（1）齐平，第三燃烧器壳体部分 第二燃烧器壳体部分（8）与第二燃烧器壳部分（8）相邻，第三燃烧器壳部分（9）具有切向适合于第二燃烧器壳体部分（8）的曲率，并且第三燃烧器壳体部分（9） 在每个情况下，切向空气入口槽（LS）中的一个并且提供用于燃烧进料空气（L）的前缘（12）。
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公开(公告)号：US20080216482A1
公开(公告)日：2008-09-11
申请号：US12115129
申请日：2008-05-05
CPC分类号： F23R3/26 , F23C7/008 , F23C2900/07021 , F23D14/02 , F23R3/286
摘要： A lance for introducing fuel into a combustion chamber of a burner, in particular of a turbine plant is provided. The lance includes a lance head, a fuel feed, an oxidator feed and a control device. The lance head projects into the combustion chamber and includes a fuel nozzle and an oxidator outlet orifice. The fuel feed extends in the lance and is connected to the fuel nozzle. The oxidator feed extends in the lance head and is connected to the oxidator outlet orifice. The control device controls a flow cross sectional area of the oxidator feed. The control device has a control piston installed in the lance head with stroke adjustability for stroke-dependent controlling of the flow cross sectional area of the oxidator feed.
摘要翻译： 提供了用于将燃料引入燃烧器的燃烧室的喷枪，特别是用于涡轮机的燃烧室。 喷枪包括喷枪头，燃料进料，氧化剂进料和控制装置。 喷枪头突入燃烧室并包括燃料喷嘴和氧化器出口孔。 燃料进料在喷枪中延伸并且连接到燃料喷嘴。 氧化剂进料在喷枪头中延伸并连接到氧化剂出口孔。 控制装置控制氧化剂进料的流动横截面积。 控制装置具有安装在喷枪头中的控制活塞，其具有行程可调节性，用于依次控制氧化剂进料的流动横截面积。
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10.发明授权Premix burner arrangement with catalytic combustion and method for its operation 有权具有催化燃烧的预混燃烧装置及其运行方法公开(公告)号：US06625988B2
公开(公告)日：2003-09-30
申请号：US09991969
申请日：2001-11-26
IPC分类号： F02C722
CPC分类号： F23R3/286 , F23C2900/07002 , F23C2900/9901 , F23R3/40
摘要： A premix burner arrangement with catalytic combustion provides a fuel/air mixture to a combustion chamber of a gas turbine arrangement. The premix burner arrangement includes a premix burner, at least one fuel addition unit, and air inlet openings arranged in such a way that at least one of gaseous and liquid fuel can be mixed with combustion inlet air inside the premix burner to form a fuel/air mixture. The fuel/air mixture exits from the premix burner downstream in the direction towards a combustion chamber positioned after the premix burner arrangement and can be ignited inside the combustion chamber. A catalyzer unit is provided before the entrance of the fuel/air mixture into the combustion chamber. Part of the fuel/air mixture can be introduced into and passed through the catalyzer unit before the catalyzed part of the fuel/air mixture flows together with the remaining portion of the fuel/air mixture into the combustion chamber.
摘要翻译： 具有催化燃烧的预混合燃烧器装置为燃气轮机装置的燃烧室提供燃料/空气混合物。 预混合燃烧器装置包括预混合燃烧器，至少一个燃料添加单元和空气入口开口，其中气体和液体燃料中的至少一种可以与预混燃烧器内部的燃烧入口空气混合以形成燃料/ 空气混合物 燃料/空气混合物从预混合燃烧器沿朝向位于预混合燃烧器装置之后的燃烧室的方向下游排出，并可在燃烧室内点燃。 在燃料/空气混合物进入燃烧室之前提供催化剂单元。 燃料/空气混合物的一部分可以在燃料/空气混合物的催化部分与燃料/空气混合物的剩余部分一起流入燃烧室之前引入并通过催化剂单元。
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