会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 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。
    • 3. 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。
    • 4. 发明申请
    • Burner for a Gas Turbine
    • 燃气轮机燃烧器
    • US20070207431A1
    • 2007-09-06
    • US11689655
    • 2007-03-22
    • Gijsbertus OomensBettina PaikertPeter FlohrChristian Steinbach
    • Gijsbertus OomensBettina PaikertPeter FlohrChristian Steinbach
    • F23D14/62
    • F23C7/002F23C2900/07002F23D11/24F23D11/38F23R3/343
    • A premix burner, for example for a gas turbine, having a conical swirl generator (1) and a cylindrical mixing section (2) which follows it in the direction of flow, includes a high-pressure atomizer nozzle (10) with one or more fuel feed passages. The high-pressure atomizer nozzle (10) includes at least two outlet passages, through which liquid fuel enters the swirl generator (1), these passages being arranged off-center with respect to the longitudinal axis of the nozzle and being configured in such a way that the spray cone (11) of the fuel is oriented at an angle (β) with respect to the longitudinal axis of the swirl generator (1) which is smaller than the cone half-angle (α) of the swirl generator (1). The outlet passages in particular have an internal geometry with a conically narrowed section.
    • 包括具有圆锥形涡流发生器(1)的燃气轮机的预混合燃烧器和沿着流动方向跟随其的圆柱形混合部分(2)包括具有一个或多个的高压雾化喷嘴(10) 燃料供给通道。 高压雾化器喷嘴(10)包括至少两个出口通道,液体燃料通过该出口通道进入涡流发生器(1),这些通道相对于喷嘴的纵向轴线偏离中心,并被配置在 燃料的喷雾锥体(11)相对于涡流发生器(1)的纵向轴线以与旋流发生器(1)的锥形半角(α)小的角度(β)定向的方式, )。 出口通道特别具有内部几何形状,具有锥形变窄的部分。
    • 5. 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。
    • 6. 发明申请
    • Premix burner with staged liquid fuel supply and also method for operating a premix burner
    • 具有分段液体燃料供应的预混燃烧器以及操作预混燃烧器的方法
    • US20070099142A1
    • 2007-05-03
    • US11635002
    • 2006-12-07
    • Peter FlohrGijsbertus OomensMartin Zajadatz
    • Peter FlohrGijsbertus OomensMartin Zajadatz
    • F23D14/62
    • F23R3/36F23C2900/07002F23D11/402F23D14/02F23D17/002F23R3/286
    • A premix burner with staged liquid fuel supply is described having at least two partial cone shells which on the radial side form the boundary of a swirl chamber which axialwards conically widens, which partial cone shells are arranged in a partially overlapping manner, the center axes of the partial cone shells of which extend with offset effect in relation to each another, and the mutually overlapping partial cone shell sections of which enclose in each case an air inlet slot which extends tangentially to the swirl chamber, with a burner lance which projects axialwards into the swirl chamber, which lance provides means for feed of liquid fuel into the swirl chamber, and also with further means for feed of liquid fuel which are provided in the region of the air inlet slots. As such, additional means for feed of liquid fuel along at least one air inlet slot are formed and arranged in such a way that the liquid fuel delivery, which is conditioned by the further means, takes place in the form of a fuel spray which propagates perpendicularly to the tangential longitudinal extent of the air inlet slot, and also a fuel spray which propagates perpendicularly to an air flow which is directed through the air inlet slot.
    • 描述了具有分级液体燃料供应的预混合燃烧器,其具有至少两个部分锥形壳体,其在径向侧上形成旋转室的边界,该旋转室的轴向向锥面变宽,该部分锥形壳体以部分重叠的方式布置, 其部分锥形壳体相对于彼此具有偏移效应而延伸,并且其相互重叠的部分锥形壳体部分在每种情况下包围空气入口狭槽,该空气入口狭槽与涡流室相切地延伸,燃烧器喷枪将轴向突出 旋转室,该喷枪提供用于将液体燃料供给到涡流室中的装置,以及用于供给液体燃料的进一步装置,该装置设置在进气口的区域中。 因此,沿着至少一个空气入口狭槽进料液体燃料的附加装置被形成和布置成使得由其它装置调节的液体燃料输送以燃料喷雾的形式发生,该燃料喷雾传播 垂直于空气入口狭槽的切向纵向范围,以及与引导通过进气口的空气流垂直地传播的燃料喷雾。
    • 7. 发明授权
    • Method for injecting fuel into a burner
    • 将燃料喷入燃烧器的方法
    • US06705857B2
    • 2004-03-16
    • US09984613
    • 2001-10-30
    • Christian Oliver PaschereitPeter Flohr
    • Christian Oliver PaschereitPeter Flohr
    • F23D1458
    • F23R3/286F23C2900/07002F23D2210/00
    • In a method for injecting fuel into a burner (1), which burner (1) comprises an inner chamber (22) enclosed by at least one shell (8, 9), at which inner chamber fuel is injected through fuel nozzles (6) into a combustion air stream (23) flowing inside the inner chamber (22), the resulting fuel/air mixture flows within a time-lag (&tgr;) to a flame front (3) in a combustion chamber (2), and is ignited there, the formation of thermoacoustic, ignition-driven vibrations is achieved in that the fuel is injected in such a way by means of fuel nozzles (6) distributed over the burner length that the time-lag (&tgr;) between the injection of the fuel and its combustion at the flame front (3) corresponds to a distribution (12) that varies systematically over the burner length for the various fuel nozzles and reduces the vibrations.
    • 在用于将燃料喷射到燃烧器(1)中的方法中,该燃烧器(1)包括由至少一个外壳(8,9)包围的内室(22),在内室燃料通过燃料喷嘴(6)喷射, 进入在内室(22)内流动的燃烧空气流(23)中,所产生的燃料/空气混合物在燃烧室(2)内的时间滞后(τ)内流动到火焰前端(3),并被点燃 在那里,形成热声,点火驱动的振动是通过燃料喷嘴(6)以这样的方式喷射的,燃料喷嘴分布在燃烧器长度上,即燃料喷射之间的时滞(τ) 并且其在火焰前部(3)处的燃烧对应于在各种燃料喷嘴的燃烧器长度上系统地变化的分布(12),并减少振动。
    • 10. 发明申请
    • METHOD FOR OPERATING A GAS TURBINE
    • 操作气体涡轮的方法
    • US20090260368A1
    • 2009-10-22
    • US12471665
    • 2009-05-26
    • Eribert BenzPeter FlohrAdnan ErogluFelix GuetheJaan Hellat
    • Eribert BenzPeter FlohrAdnan ErogluFelix GuetheJaan Hellat
    • F02C7/22
    • F02C6/003C10J3/00C10J2300/093C10J2300/0959C10J2300/1606C10J2300/165C10J2300/1671C10J2300/1675C10J2300/1678C10J2300/1892F02C3/28F25J3/04545F25J3/04575Y02E20/16Y02E20/18
    • A method for operating a gas turbine (11), which is used especially in a combined-cycle power plant (30), includes inducting and compressing air by the gas turbine (11), the compressed air is fed to a combustor (18, 19) for the combustion of a syngas which is produced from coal, and the hot gases which result during the combustion are expanded in a subsequent turbine (16, 17), performing work, wherein some of the compressed air is separated into oxygen and nitrogen, and the oxygen is used in a coal gasification plant (34) for producing the syngas. With such a method, a reduction of the NOx emission is achieved without noticeable loss of output and flexibility of operation by a gas turbine (11) with reheating being used, which includes two combustors (18, 19) and two turbines (16, 17), wherein in the first combustor (18) syngas is combusted, using the compressed air, and the resulting hot gases are expanded in the first turbine (16), and wherein in the second combustor syngas is combusted, using the gases which issue from the first turbine (16), and the resulting hot gases are expanded in the second turbine (17), the two combustors (18, 19) are operated with undiluted syngas, and the flame temperature (TF) in the first combustor (18) of the gas turbine (11) is lowered compared with the operation with natural gas (TNG), while the second combustor (19) is operated largely in the normal operation (TNG) which is designed for natural gas.
    • 用于特别在联合循环发电厂(30)中使用的燃气轮机(11)的方法包括:通过燃气轮机(11)对空气进行吸入和压缩,将压缩空气供给至燃烧器(18), 19),用于燃烧由煤产生的合成气,并且在燃烧期间产生的热气体在随后的涡轮机(16,17)中膨胀,进行工作,其中一些压缩空气被分离成氧和氮 ,并且在用于生产合成气的煤气化设备(34)中使用氧气。 通过这样的方法,可以实现NOx排放的减少,而不会出现明显的输出损失和使用具有再加热的燃气轮机(11)的操作灵活性,其包括两个燃烧器(18,19)和两个涡轮机(16,17) ),其中在所述第一燃烧器(18)中,使用所述压缩空气燃烧合成气,并且所得热气体在所述第一涡轮机(16)中膨胀,并且其中在所述第二燃烧器中合成气被燃烧,使用从 第一涡轮机(16),并且所产生的热气体在第二涡轮机(17)中膨胀,两个燃烧器(18,19)用未稀释的合成气进行操作,并且第一燃烧器(18)中的火焰温度(TF) 与天然气(TNG)的运转相比,燃气轮机(11)的运转下降,而第二燃烧器(19)在为天然气设计的正常运行(TNG)中运行较大。