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    • 1. 发明申请
    • BURNER FOR THE OPERATION OF A HEAT GENERATOR
    • 燃烧器用于发电机的运行
    • US20090081599A1
    • 2009-03-26
    • US12238792
    • 2008-09-26
    • Stefano BerneroPeter FlohrGijsbertis OomensMartin Zajadatz
    • Stefano BerneroPeter FlohrGijsbertis OomensMartin Zajadatz
    • F23D11/00
    • F23D17/002F23C7/008F23C2900/07002F23R3/343
    • 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).
    • 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)。
    • 2. 发明授权
    • Burner for the operation of a heat generator and method of use
    • 燃烧器用于运行发热体和使用方法
    • US07972133B2
    • 2011-07-05
    • US12238792
    • 2008-09-26
    • Stefano BerneroPeter FlohrGijsbertus OomensMartin Zajadatz
    • Stefano BerneroPeter FlohrGijsbertus OomensMartin Zajadatz
    • F23Q9/00
    • F23D17/002F23C7/008F23C2900/07002F23R3/343
    • 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).
    • 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)。
    • 9. 发明申请
    • SYSTEM FOR CONTROLLING A COMBUSTION PROCESS FOR A GAS TURBINE
    • 用于控制燃气涡轮机燃烧过程的系统
    • US20090229238A1
    • 2009-09-17
    • US12430314
    • 2009-04-27
    • Xiao-Yi ZhangTobias SpitzmuellerStefano Bernero
    • Xiao-Yi ZhangTobias SpitzmuellerStefano Bernero
    • F02C9/00
    • F23N5/003F02C9/24F02K7/02F05D2270/082F05D2270/083F05D2270/301F23N5/16F23N2041/20F23R2900/00013
    • A system (S) for controlling nitrogen oxide (NOx) emissions and combustion pulsation levels of a gas turbine having a gas turbine combustion system, having a single combustion chamber and multiple burners, includes a cascade structure having a first and second control level (1, 2), the first level (1) having a device to control NOx emissions and generate combustion pulsation target levels based on the difference between measured and target NOx emission levels, and the second level (2) having a device to control pulsation levels and generate a ratio (γ) of fuel flow to different types of burners or to different stages of each burner. The fuel flow ratio (γ) is based on the difference between the measured and generated target pulsation levels. The control system (S) enables the operation of a gas turbine to meet NOx emission requirements, while maintaining combustion pulsation levels within limits that ensure improved lifetime of the combustion system.
    • 一种用于控制具有单个燃烧室和多个燃烧器的具有燃气轮机燃烧系统的燃气轮机的氮氧化物(NOx)排放和燃烧脉动水平的系统(S)包括具有第一和第二控制水平(1 ,2),所述第一级(1)具有基于所测量的和目标NOx排放水平之间的差异来控制NOx排放并产生燃烧脉动目标水平的装置,以及具有控制脉动水平的装置的第二水平(2) 产生不同类型燃烧器的燃料流量或每个燃烧器的不同级别的比率(γ)。 燃料流量比(γ)基于测量和产生的目标脉动水平之间的差异。 控制系统(S)使得燃气轮机的操作能够满足NOx排放要求,同时将燃烧脉动水平保持在限制范围内,以确保燃烧系统的寿命提高。