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    • 3. 发明授权
    • Burner arrangement for a gas turbine including an inlet-air impingement plate
    • 包括入口 - 空气冲击板的燃气轮机的燃烧器装置
    • US06209327B1
    • 2001-04-03
    • US09369836
    • 1999-08-09
    • Jakob KellerJochem FischerUlf Christian MüllerFrank ReissPirmin Schiessel
    • Jakob KellerJochem FischerUlf Christian MüllerFrank ReissPirmin Schiessel
    • F02C100
    • F23C7/02F23M9/02
    • A burner arrangement (20) for a gas turbine comprises an interior space (22) enclosed by a casing (23), in which interior space (22) at least one burner (21) is arranged, and into which interior space (22) in each case a jet (26, 27) of a gaseous medium, in particular air, is sprayed through at least two nozzle openings (24, 25) against the direction of flow of the burner (21) and along the inner wall (23a) of the casing (23) which jets (26, 27), guided by the inner wall (23a), meet one another from opposite directions and combine to form a secondary flow (28) flowing off perpendicularly from the inner wall (23a). In such a burner arrangement, the flow is stabilized and evened out by virtue of the fact that, to establish the impingement point of the jets (26, 27), a dividing plate (29) arranged in the flow path of the jets (26, 27) and disposed essentially perpendicularly to the inner wall (23a) is provided.
    • 一种用于燃气轮机的燃烧器装置(20)包括由壳体(23)包围的内部空间(22),其中布置有至少一个燃烧器(21)的内部空间(22),并且内部空间(22) 在每种情况下,气体介质(特别是空气)的射流(26,27)通过至少两个喷嘴开口(24,25)被喷射抵靠燃烧器(21)的流动方向并且沿着内壁(23a) )由外壁(23a)引导的外壳(23,27)从相反的方向彼此相遇并结合形成从内壁(23a)垂直流动的二次流(28) 。 在这种燃烧器装置中,由于为了确定射流(26,27)的冲击点,布置在射流(26,27)的流动路径中的分隔板(29),流体被稳定和平衡, ,27)并且基本上垂直于内壁(23a)设置。
    • 5. 发明授权
    • Premix burner
    • 预混燃烧器
    • US07013648B2
    • 2006-03-21
    • US10989029
    • 2004-11-16
    • Timothy GriffinFrank ReissDieter Winkler
    • Timothy GriffinFrank ReissDieter Winkler
    • F23D14/62
    • F23D14/62F23C2900/07002F23C2900/9901F23D17/002F23R3/286
    • A premix burner includes a swirler (7) for a combustion air stream and a device for injection of fuel into the combustion air stream. The swirler (7) includes one or more inlet openings for combustion air of the combustion air stream entering the burner. The device for injection of fuel into the combustion air stream includes one or more first fuel lines (8) with first fuel injection openings (4). The opening diameter and/or the injection angle of the injection openings varies with respect to the axial and/or radial direction. Alternatively or in addition, some of the first fuel injection openings (4) may be arranged in one or more first groups of closely grouped fuel injection openings (4) so that each of the first groups forms one fuel jet with a large cross section. An improved mixing of the fuel with the combustion air is achieved with the burner in particular in cases in which the fuel is injected at the end of the burner facing the combustion chamber.
    • 预混燃烧器包括用于燃烧空气流的旋流器(7)和用于将燃料喷射到燃烧空气流中的装置。 旋流器(7)包括用于燃烧空气流进入燃烧器的燃烧空气的一个或多个入口。 用于将燃料喷射到燃烧空气流中的装置包括具有第一燃料喷射开口(4)的一个或多个第一燃料管线(8)。 喷射开口的开口直径和/或喷射角度相对于轴向和/或径向方向变化。 或者或另外,一些第一燃料喷射开口(4)可以布置在紧密分组的燃料喷射开口(4)的一个或多个第一组中,使得每个第一组形成具有大横截面的一个燃料喷射。 燃烧器与燃烧空气的改进的混合是通过燃烧器实现的,特别是在燃烧器面向燃烧室的燃烧器端部喷射燃料的情况下。
    • 6. 发明授权
    • Method for cooling a component and appliance for carrying out the method
    • 用于冷却部件和器具进行该方法的方法
    • US5581994A
    • 1996-12-10
    • US290129
    • 1994-08-15
    • Frank ReissStefan Tschirren
    • Frank ReissStefan Tschirren
    • F01D5/18F01D9/02F01D25/12F02C7/18F23R3/00F23R3/02
    • F01D25/12F01D9/023F23R3/002F05D2260/201
    • In a method for cooling a thermally loaded component (1) with a plate-type outer wall (2), in which method cooling air is supplied, in a first cooling section (A) of the component (1), through a cooling air supply (5) in the direction towards the outer wall (2) and is deflected laterally before the outer wall (2) and in a second cooling section (B) is further guided parallel to the outer wall (2) in a laterally adjoining cooling air duct (3) for the purpose of further cooling, homogenization of the cooling is achieved wherein, in order to reduce the impingement cooling in the first cooling section (A), the cooling airflow coming from the cooling airsupply (5) is subdivided into a main flow and a by-pass flow, the main flow is guided directly along the outer wall (2) of the component (1) to the cooling air duct (3), the by-pass flow is guided to the cooling air duct (3) without contacting the outer wall (2) and both partial flows are recombined at the inlet to the cooling air duct (3).
    • 在通过冷却空气(1)的第一冷却部分(A)中冷却空气的板式外壁(2)冷却热负荷部件(1)的方法中, 在朝向外壁(2)的方向上供应(5)并且在外壁(2)之前横向偏转,并且在第二冷却部分(B)中以横向相邻的冷却方式进一步平行于外壁(2)引导 为了进一步冷却,实现冷却均质化,为了减少第一冷却部分(A)中的冲击冷却,将来自冷却空气供应(5)的冷却气流细分为 主流和旁通流,主流直接沿着部件(1)的外壁(2)引导到冷却空气管道(3),旁路流被引导到冷却风道 (3),而不接触外壁(2),并且两个部分流在入口处与冷却风道(3)重新组合。
    • 10. 发明申请
    • Premix burner
    • 预混燃烧器
    • US20050115244A1
    • 2005-06-02
    • US10989029
    • 2004-11-16
    • Timothy GriffinFrank ReissDieter Winkler
    • Timothy GriffinFrank ReissDieter Winkler
    • F23D14/62F23D17/00F23R3/28F23R3/30
    • F23D14/62F23C2900/07002F23C2900/9901F23D17/002F23R3/286
    • A premix burner includes a swirler (7) for a combustion air stream and a device for injection of fuel into the combustion air stream. The swirler (7) includes one or more inlet openings for combustion air of the combustion air stream entering the burner. The device for injection of fuel into the combustion air stream includes one or more first fuel lines (8) with first fuel injection openings (4). The opening diameter and/or the injection angle of the injection openings varies with respect to the axial and/or radial direction. Alternatively or in addition, some of the first fuel injection openings (4) may be arranged in one or more first groups of closely grouped fuel injection openings (4) so that each of the first groups forms one fuel jet with a large cross section. An improved mixing of the fuel with the combustion air is achieved with the burner in particular in cases in which the fuel is injected at the end of the burner facing the combustion chamber.
    • 预混燃烧器包括用于燃烧空气流的旋流器(7)和用于将燃料喷射到燃烧空气流中的装置。 旋流器(7)包括用于燃烧空气流进入燃烧器的燃烧空气的一个或多个入口。 用于将燃料喷射到燃烧空气流中的装置包括具有第一燃料喷射开口(4)的一个或多个第一燃料管线(8)。 喷射开口的开口直径和/或喷射角度相对于轴向和/或径向方向变化。 或者或另外,一些第一燃料喷射开口(4)可以布置在一组或多个紧密分组的燃料喷射开口(4)中,使得每个第一组形成具有大截面的一个燃料喷射。 燃烧器与燃烧空气的改进的混合是通过燃烧器实现的,特别是在燃烧器面向燃烧室的燃烧器端部喷射燃料的情况下。