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    • 7. 发明授权
    • Premix burner and method for burning a low-calorie combustion gas
    • 预燃燃烧器和燃烧低热量燃烧气体的方法
    • US07448218B2
    • 2008-11-11
    • US10590379
    • 2005-02-15
    • Andreas HeilosBerthold KöstlinBernd Prade
    • Andreas HeilosBerthold KöstlinBernd Prade
    • F02C3/28F23R3/36F23D14/58
    • F23R3/14F23D14/583F23R3/286F23R2900/00002
    • The invention relates to a pre-mix burner for burning a low-calorie combustion gas, said burner comprising an air duct which extends along an axis of the burner and can be used to supply combustion air. A swirling device is arranged in the air duct and is used to apply a swirling motion to the combustion air. An injection device for the low-calorie combustion gas is provided downstream of the swirling device. The injection device comprises inlets for the combustion gas, such that the formation of wake regions in the air channel is prevented. The invention also relates to a method for burning a low-calorie combustion gas, according to which a swirling motion is applied to the combustion air, low-calorie combustion gas is injected into the swirled combustion air and intensively mixed therewith, and the mixture is then burned.
    • 本发明涉及一种用于燃烧低热量燃烧气体的预混合燃烧器,所述燃烧器包括沿燃烧器的轴线延伸并可用于供应燃烧空气的空气管道。 涡流装置布置在空气管道中,并用于向燃烧空气施加旋转运动。 用于低热量燃烧气体的注射装置设置在旋转装置的下游。 注射装置包括用于燃烧气体的入口,从而防止在空气通道中形成尾流区。 本发明还涉及一种用于燃烧低热量燃烧气体的方法,根据该方法,对燃烧空气施加旋转运动,将低热燃烧气体注入涡流燃烧空气中并与其集中混合,并且混合物 然后烧了
    • 9. 发明申请
    • TURBINE BURNER
    • 涡轮燃烧器
    • US20130074506A1
    • 2013-03-28
    • US13699801
    • 2011-03-29
    • Boris Ferdinand KockBerthold KöstlinBernd Prade
    • Boris Ferdinand KockBerthold KöstlinBernd Prade
    • F23R3/36
    • F23R3/36F23D2900/00008F23D2900/00014F23D2900/14021F23R3/343F23R2900/00002
    • A turbine burner is provided. The turbine burner has a secondary feed unit and a primary feed unit. The primary feed unit has a primary mixing tube and a fuel nozzle that are arranged concentrically around the secondary feed unit. The primary mixing tube and the fuel nozzle have a fluid flow connection. The fuel nozzle has an annular wall that is radially spaced in the axial direction from the secondary feed unit such that a gap height is fainted by the annular wall and the secondary feed unit. The annular wall has an inside wall directed toward the secondary feed unit and having blades with a leading edge on the upstream side. The fuel nozzle has an inlet and the blades have an axial distance from the inlet. The ratio of the distance to the gap height is greater than 1 and less than the gap height.
    • 提供涡轮燃烧器。 涡轮燃烧器具有二次进料单元和主进料单元。 主进料单元具有主要混合管和燃料喷嘴,其同心地布置在二次进料单元周围。 主混合管和燃料喷嘴具有流体流动连接。 燃料喷嘴具有在轴向方向上与二次进料单元径向隔开的环形壁,使得间隙高度被环形壁和次级进料单元所晕倒。 环形壁具有指向二次进料单元的内壁,并具有在上游侧具有前缘的叶片。 燃料喷嘴具有入口,并且叶片具有与入口的轴向距离。 距离间隙高度的比例大于1且小于间隙高度。