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    • 3. 发明授权
    • Combustor for a gas turbine
    • 燃气轮机用燃烧器
    • US07484352B2
    • 2009-02-03
    • US11533796
    • 2006-09-21
    • Peter FlohrBruno SchuermansMajed Toqan
    • Peter FlohrBruno SchuermansMajed Toqan
    • F02C9/28
    • F23R3/34F23N2037/02F23R2900/00013
    • In a combustor (1) for a gas turbine, the combustor (1) includes a burner system (2) and a fuel supply system (3). The burner system (2) includes at least two burner groups (A, B) each with at least one burner (5). The fuel supply system (3) includes a main line (7), which is connected to a fuel source (8), and also an auxiliary line (9) for each burner group (A, B). Each auxiliary line (9) is connected to each burner (5) of the associated burner group (A, B) and is connected to the main line (7) by a controllable distribution valve (10). A sensing system (11) measures pressure pulsation values and/or emission values for each burner group (A, B). A control system (12), in dependence upon the pulsation values and/or the emission values, controls the distribution valves (10) so that in each burner group (A, B) the pulsation values and/or the emission values assume and/or fall below predetermined threshold values.
    • 在燃气轮机的燃烧器(1)中,燃烧器(1)包括燃烧器系统(2)和燃料供应系统(3)。 燃烧器系统(2)包括至少两个燃烧器组(A,B),每个燃烧器组具有至少一个燃烧器(5)。 燃料供给系统(3)包括连接到燃料源(8)的主管线(7)和每个燃烧器组(A,B)的辅助管线(9)。 每个辅助管线(9)连接到相关联的燃烧器组(A,B)的每个燃烧器(5),并通过可控分配阀(10)连接到主管线(7)。 感测系统(11)测量每个燃烧器组(A,B)的压力脉动值和/或发射值。 控制系统(12)根据脉动值和/或排放值控制分配阀(10),使得在每个燃烧器组(A,B)中,脉动值和/或发射值假定和/ 或低于预定阈值。
    • 4. 发明授权
    • Combustion chamber
    • 燃烧室
    • US07901203B2
    • 2011-03-08
    • US11676584
    • 2007-02-20
    • Alexander NiValter BellucciPeter FlohrBruno SchuermansMajed ToqanKen-Yves Haffner
    • Alexander NiValter BellucciPeter FlohrBruno SchuermansMajed ToqanKen-Yves Haffner
    • F23N1/02
    • F23N1/002F23N5/08F23N5/082F23N5/16F23N2023/10F23N2025/04F23N2031/06F23N2037/02F23R3/28
    • A combustion chamber (1), in particular in a gas turbine, has at least two burners (A-H) that are connected to a fuel supply (3) via controllable fuel valves (2′ and 2). Each burner (A to H) is assigned at least one optical measuring device (4) for detecting chemiluminescent radiation, and the combustion chamber (1) is assigned a pressure sensor (7) for detecting a combustion chamber pressure. The optical measuring device (4) and the pressure sensor (7) are connected to a computing and control device, which calculates a correlation value from the incoming measured values. A high correlation value signifies that the associated burner is prone to pulsation. The computing and control device (6) is designed in such a way that it determines the burner or a burner group with the highest correlation and controls the associated fuel valve(s) in such a way that more fuel is fed to the respective burner or the respective burner group, and the pulsation tendency thereof is thereby reduced.
    • 特别是在燃气轮机中的燃烧室(1)具有通过可控燃油门(2'和2)连接到燃料供应源(3)的至少两个燃烧器(A-H)。 每个燃烧器(A至H)分配有用于检测化学发光辐射的至少一个光学测量装置(4),并且燃烧室(1)被分配用于检测燃烧室压力的压力传感器(7)。 光学测量装置(4)和压力传感器(7)连接到计算和控制装置,其计算来自测量值的相关值。 高相关值表示相关联的燃烧器容易产生脉动。 计算和控制装置(6)被设计成使得其确定具有最高相关性的燃烧器或燃烧器组,并且以更多的燃料被供给到相应的燃烧器或者相应的燃料 相应的燃烧器组及其脉动趋势由此减小。
    • 5. 发明申请
    • Combustion Chamber
    • 燃烧室
    • US20070224559A1
    • 2007-09-27
    • US11676584
    • 2007-02-20
    • Alexander NiValter BellucciPeter FlohrBruno SchuermansMajed ToqanKen-Yves Haffner
    • Alexander NiValter BellucciPeter FlohrBruno SchuermansMajed ToqanKen-Yves Haffner
    • F23N5/08
    • F23N1/002F23N5/08F23N5/082F23N5/16F23N2023/10F23N2025/04F23N2031/06F23N2037/02F23R3/28
    • A combustion chamber (1), in particular in a gas turbine, has at least two burners (A-H) that are connected to a fuel supply (3) via controllable fuel valves (2′ and 2). Each burner (A to H) is assigned at least one optical measuring device (4) for detecting chemiluminescent radiation, and the combustion chamber (1) is assigned a pressure sensor (7) for detecting a combustion chamber pressure. The optical measuring device (4) and the pressure sensor (7) are connected to a computing and control device, which calculates a correlation value from the incoming measured values. A high correlation value signifies that the associated burner is prone to pulsation. The computing and control device (6) is designed in such a way that it determines the burner or a burner group with the highest correlation and controls the associated fuel valve(s) in such a way that more fuel is fed to the respective burner or the respective burner group, and the pulsation tendency thereof is thereby reduced.
    • 特别是在燃气轮机中的燃烧室(1)具有通过可控燃油门(2'和2)连接到燃料供应源(3)的至少两个燃烧器(A-H)。 每个燃烧器(A至H)分配有用于检测化学发光辐射的至少一个光学测量装置(4),并且燃烧室(1)被分配用于检测燃烧室压力的压力传感器(7)。 光学测量装置(4)和压力传感器(7)连接到计算和控制装置,其计算来自测量值的相关值。 高相关值表示相关联的燃烧器容易产生脉动。 计算和控制装置(6)被设计成使得其确定具有最高相关性的燃烧器或燃烧器组,并且以更多的燃料被供给到相应的燃烧器或者相应的燃料 相应的燃烧器组及其脉动趋势由此减小。
    • 6. 发明申请
    • Combustor for a gas turbine and associated operating method
    • 燃气轮机燃烧器及相关操作方法
    • US20070163267A1
    • 2007-07-19
    • US11533796
    • 2006-09-21
    • Peter FlohrBruno SchuermansMajed Toqan
    • Peter FlohrBruno SchuermansMajed Toqan
    • F02C7/26
    • F23R3/34F23N2037/02F23R2900/00013
    • In a combustor (1) for a gas turbine, the combustor (1) includes a burner system (2) and a fuel supply system (3). The burner system (2) includes at least two burner groups (A, B) each with at least one burner (5). The fuel supply system (3) includes a main line (7), which is connected to a fuel source (8), and also an auxiliary line (9) for each burner group (A, B). Each auxiliary line (9) is connected to each burner (5) of the associated burner group (A, B) and is connected to the main line (7) by a controllable distribution valve (10). A sensing system (11) measures pressure pulsation values and/or emission values for each burner group (A, B). A control system (12), in dependence upon the pulsation values and/or the emission values, controls the distribution valves (10) so that in each burner group (A, B) the pulsation values and/or the emission values assume and/or fall below predetermined threshold values.
    • 在燃气轮机的燃烧器(1)中,燃烧器(1)包括燃烧器系统(2)和燃料供应系统(3)。 燃烧器系统(2)包括至少两个燃烧器组(A,B),每个燃烧器组具有至少一个燃烧器(5)。 燃料供给系统(3)包括连接到燃料源(8)的主管线(7)和每个燃烧器组(A,B)的辅助管线(9)。 每个辅助管线(9)连接到相关联的燃烧器组(A,B)的每个燃烧器(5),并通过可控分配阀(10)连接到主管线(7)。 感测系统(11)测量每个燃烧器组(A,B)的压力脉动值和/或发射值。 控制系统(12)根据脉动值和/或排放值控制分配阀(10),使得在每个燃烧器组(A,B)中,脉动值和/或发射值假定和/ 或低于预定阈值。
    • 9. 发明授权
    • Combustion stabilization systems
    • 燃烧稳定系统
    • US08215949B2
    • 2012-07-10
    • US11749710
    • 2007-05-16
    • Majed Toqan
    • Majed Toqan
    • F23J7/00
    • F23J7/00
    • Systems for stabilizing combustion while minimizing NOx generation by using high-flame-speed additives to stabilize the flame front in combustors operating at relatively low temperatures and/or under oxygen constraints. The system is adapted for use in coal-fired boilers, oil-fired boilers, and gas turbine engines. The methods stabilize the flame front to permit stable combustion under an expanded range of part-load conditions. The system provides substantially complete combustion of coal in coal boilers resulting in ash saleable for use in concrete manufacturing.
    • 用于通过使用高阻燃添加剂来使燃烧器在较低温度和/或氧气约束下操作的燃烧器中的火焰前沿稳定燃烧同时最小化NOx产生的系统。 该系统适用于燃煤锅炉,燃油锅炉和燃气轮机。 这些方法使火焰前端稳定,以允许在部分负载条件的扩展范围内稳定燃烧。 该系统在煤锅炉中提供基本上完全燃烧的煤,导致用于混凝土制造的灰分。