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1.发明申请Premix burner arrangement for operating a combustion chamber and method for operating a combustion chamber 审中-公开用于操作燃烧室的预混燃烧器装置和用于操作燃烧室的方法公开(公告)号：US20070042307A1
公开(公告)日：2007-02-22
申请号：US11503163
申请日：2006-08-14
CPC分类号： F23R3/286 , F23C2900/07002 , F23D17/002
摘要： A premix burner is disclosed for operating a combustion chamber with a gaseous and/or liquid fuel, having a swirl generator for inducing a swirl flow in an incoming combustion air flow and a device for injecting fuel into the swirl flow, the swirl generator having at least two cone shell segments which fit together to form a flow body and together enclose a conically formed swirl space with a cone angle γ and air inlet slits directed tangentially to the length of the cone. At least at the downstream end region of the swirl generator, a shaped element enclosing the cone shell segments with an inside wall facing the cone shell segments is provided, and that the cone shell segments end in the inside wall in a flush manner while maintaining their shape.
摘要翻译： 公开了一种用于操作具有气体和/或液体燃料的燃烧室的预混燃烧器，其具有用于在进入的燃烧空气流中引起涡流的涡流发生器和用于将燃料喷射到涡流中的装置，所述涡流发生器具有 至少两个锥形壳段，其装配在一起以形成流动体并且一起围绕锥形形成的漩涡空间与锥角γ和空气入口狭缝相切地切向锥体的长度。 至少在涡流发生器的下游端部区域，设置一个封闭锥形壳段的成形元件，其中内壁面向锥形壳段，并且锥形壳段以齐平的方式在内壁中终止，同时保持它们 形状。
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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：US20080229752A1
公开(公告)日：2008-09-25
申请号：US12109585
申请日：2008-04-25
CPC分类号： F23D14/02 , F23C2900/07021 , F23R3/286
摘要： A lance (3) for introducing a fuel into a mixing path (2) of a burner (1) which is provided with a swirler for producing a swirled combustion air flow, especially a burner of a turbine plant, includes a lance head (5), a fuel feed (8) and an oxidator feed (10). The lance head (5) projects into the mixing path (2), has at least one fuel nozzle (6) for injection of the fuel into the mixing path (2), and also has at least one oxidator outlet orifice (7) for introducing an oxidator into the mixing path (2). The fuel feed (8) extends in the lance (3) and is connected to the at least one fuel nozzle (6). The oxidator feed (10) extends in the lance head (5) and is connected to the at least one oxidator outlet orifice (7). In order to improve the operation of the burner (1), the at least one oxidator outlet orifice (7) is located centrally on the lance head (5), and the at least one fuel nozzle (6) is installed on the lance head (5), being offset radially outwards with regard to the at least one oxidator outlet orifice (7).
摘要翻译： 一种用于将燃料引入燃烧器（1）的混合路径（2）中的喷枪（3），其设置有用于产生涡流燃烧空气流的旋流器，特别是涡轮机设备的燃烧器，喷枪头（5） ），燃料进料（8）和氧化剂进料（10）。 喷枪头（5）突出到混合路径（2）中，具有至少一个用于将燃料喷射到混合路径（2）中的燃料喷嘴（6），并且还具有至少一个氧化剂出口孔（7），用于 将氧化剂引入混合路径（2）。 燃料进料（8）在喷枪（3）中延伸并连接到至少一个燃料喷嘴（6）。 氧化剂进料（10）在喷枪头（5）中延伸并连接到至少一个氧化剂出口孔（7）。 为了改善燃烧器（1）的操作，至少一个氧化剂出口孔（7）位于喷枪头（5）的中央，并且至少一个燃料喷嘴（6）安装在喷枪头 （5）相对于所述至少一个氧化剂出口孔（7）径向向外偏移。
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公开(公告)号：US20080032246A1
公开(公告)日：2008-02-07
申请号：US11838999
申请日：2007-08-15
CPC分类号： F23C7/002 , F23C2900/07002 , F23D17/002 , F23D2211/00 , F23R3/286
摘要： A premixing burner for generating an ignitable fuel/air mixture has a swirl generator with at least two burner shells (1) which complement one another to form a throughflow body and which jointly enclose an axial conically widening swirl space and delimit, with respect to one another in the axial longitudinal extent of the cone, tangential air inlet slits (3) through which combustion supply air passes into the swirl space in which an axially propagating swirl flow is formed, and with fuel injection devices, which are provided at least partially along the tangentially running air inlet slits (3). The fuel injection devices are designed as a fuel line (6) which is separate from the burner shell (1) and which is firmly attached to the burner shell (1) so as to be longitudinally movable with respect to the burner shell (1) and so as to be releasable perpendicularly to the surface of the burner shell (1), and in that, in the burner shell (1), orifices (4) are provided, into which issue fuel injectors (7) which are provided along the fuel line (6) and which project beyond the circumferential edge of the fuel line (6).
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，其具有至少两个燃烧器壳体（1），所述燃烧器壳体彼此互补以形成通流体，并且联合地包围轴向锥形加宽的涡流空间并相对于一个 另一个在锥体的轴向纵向范围内，切向空气入口狭缝（3），燃烧供给空气通过其进入涡旋空间中，其中形成轴向传播的涡流，以及燃料喷射装置，其至少部分地沿着 切向运行的空气入口狭缝（3）。 燃料喷射装置被设计为与燃烧器壳体（1）分离并且牢固地附接到燃烧器壳体（1）以相对于燃烧器壳体（1）可纵向移动的燃料管线（6） 并且能够垂直于燃烧器壳体（1）的表面释放，并且在燃烧器壳体（1）中设置有孔口（4），其中设置有沿着燃烧器壳体（1）设置的燃料喷射器 燃料管线（6），并且突出超出燃料管线（6）的周向边缘。
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