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1. 发明授权

EP1184621B1 Gas only nozzle fuel tip and method for cooling the same 有权
标题翻译：喷嘴燃气燃烧器和用于冷却所述方法相同的方法
公开(公告)号：EP1184621B1
公开(公告)日：2005-09-28
申请号：EP01303783.3
申请日：2001-04-26
申请人： GENERAL ELECTRIC COMPANY
发明人： Bechtel, William Theodore, II , Deleonardo, Guy Wayne , Fitts, David Orus
IPC分类号： F23D14/78 , F23D14/22
CPC分类号： F23D14/78 , F23D14/22 , F23D2211/00 , F23R2900/00001

2. 发明授权

EP0936406B1 Burner with uniform fuel/air premixing for low emissions combustion 有权
标题翻译：燃烧器具有均匀燃料/空气预混合低排放燃烧
公开(公告)号：EP0936406B1
公开(公告)日：2004-05-06
申请号：EP99300964.6
申请日：1999-02-10
申请人： GENERAL ELECTRIC COMPANY
发明人： Battaglioli, John Luigi , Benoit, Jeffrey Arthur , Bland, Robert James , Bechtel, William Theodore, II , Black, Stephen Hugh , Deleonardo, Guy Wayne , Meyer, Stefan Martin , Tuthill, Richard Sterling , Taura, Joseph Charles
IPC分类号： F23D14/02 , F23C7/00 , F23M9/02
CPC分类号： F23C7/004 , F23C2900/07001 , F23D14/02 , F23D2206/10 , F23D2900/14021 , F23M9/02

3. 发明公开

EP1550791A3 Method and system for active tip clearance control in turbines 审中-公开
标题翻译：方法和系统，用于在涡轮机中活性顶隙控制
公开(公告)号：EP1550791A3
公开(公告)日：2012-12-05
申请号：EP04257994.6
申请日：2004-12-21
申请人： GENERAL ELECTRIC COMPANY
发明人： Finnigan, Peter Michael , Albers, Robert Joseph , Srinivas, Mullahalli Venkataramaniah , Deleonardo, Guy Wayne
IPC分类号： F01D11/22 , F01D11/02 , F01D11/24
CPC分类号： F01D11/025 , F01D11/22 , F01D11/24 , F05D2270/62 , F05D2270/66
摘要： A system for controlling blade tip clearance in a turbine. The system includes a stator including a shroud having a plurality of shroud segments (38) and a rotor (12) including a blade (14) rotatable within the shroud. An actuator assembly (30) is positioned radially around the shroud and includes a plurality of actuators (18). A sensor (16) senses a turbine parameter and generates a sensor signal representative of the turbine parameter. A modeling module (22) generates a tip clearance prediction in response to turbine cycle parameters. A controller (20) receives the sensor signal and the tip clearance prediction and generates at least one command signal. The actuators (18) include at least one actuator receiving the command signal and adjusts a position of at least one of the shroud segments (38) in response to the command signal.

4. 发明公开

EP1184621A1 Gas only nozzle fuel tip and method for cooling the same 有权
标题翻译： DüsefürGasbrenner und Verfahren zumKühlenderselben
公开(公告)号：EP1184621A1
公开(公告)日：2002-03-06
申请号：EP01303783.3
申请日：2001-04-26
申请人： GENERAL ELECTRIC COMPANY
发明人： Bechtel, William Theodore, II , Deleonardo, Guy Wayne , Fitts, David Orus
IPC分类号： F23D14/78 , F23D14/22
CPC分类号： F23D14/78 , F23D14/22 , F23D2211/00 , F23R2900/00001
摘要： A diffusion flame nozzle gas tip (20) is provided to convert a dual fuel nozzle to a gas only nozzle. The nozzle tip (20) diverts compressor discharge air from the passage (26) feeding the diffusion nozzle air swirl vanes to a region (28) vacated by removal of the dual fuel components, so that the diverted compressor discharge air can flow to and through effusion holes (42) in the end cap plate (22) of the nozzle tip (20). In a preferred embodiment, the nozzle gas tip defines a cavity (28) for receiving the compressor discharge air from a peripheral passage of the nozzle for flow through the effusion openings (42) defined in the end cap plate (22).
摘要翻译：设置扩散火焰喷嘴气体尖端（20）以将双燃料喷嘴转换成仅气体喷嘴。喷嘴尖端（20）将压缩机排出空气从供给扩散喷嘴空气旋流叶片的通道（26）转移到通过去除双燃料部件而腾出的区域（28），使得转向的压缩机排出的空气可以流过并通过喷嘴头（20）的端盖板（22）中的排出孔（42）。在优选实施例中，喷嘴气体尖端限定用于从喷嘴的周边通道接收压缩机排出空气的空腔（28），用于流过限定在端盖板（22）中的渗出开口（42）。

5. 发明公开

EP1550791A2 Method and system for active tip clearance control in turbines 审中-公开
标题翻译： Verfahren und System zur aktiven Spitzspielkontrolle在Turbomaschinen
公开(公告)号：EP1550791A2
公开(公告)日：2005-07-06
申请号：EP04257994.6
申请日：2004-12-21
申请人： General Electric Company
发明人： Finnigan, Peter Michael , Albers, Robert Joseph , Srinivas, Mullahalli Venkataramaniah , Deleonardo, Guy Wayne
IPC分类号： F01D11/22
CPC分类号： F01D11/025 , F01D11/22 , F01D11/24 , F05D2270/62 , F05D2270/66
摘要： A system for controlling blade tip clearance in a turbine. The system includes a stator including a shroud having a plurality of shroud segments (38) and a rotor (12) including a blade (14) rotatable within the shroud. An actuator assembly (30) is positioned radially around the shroud and includes a plurality of actuators (18). A sensor (16) senses a turbine parameter and generates a sensor signal representative of the turbine parameter. A modeling module (22) generates a tip clearance prediction in response to turbine cycle parameters. A controller (20) receives the sensor signal and the tip clearance prediction and generates at least one command signal. The actuators (18) include at least one actuator receiving the command signal and adjusts a position of at least one of the shroud segments (38) in response to the command signal.
摘要翻译：一种用于控制涡轮机叶片间隙的系统。该系统包括定子，其包括具有多个护罩段（38）的护罩和包括在护罩内可旋转的刀片（14）的转子（12）。致动器组件（30）围绕护罩径向定位并且包括多个致动器（18）。传感器（16）感测涡轮参数并产生代表涡轮参数的传感器信号。建模模块（22）响应于涡轮循环参数产生尖端间隙预测。控制器（20）接收传感器信号和提前间隙预测并产生至少一个命令信号。致动器（18）包括至少一个致动器，其接收命令信号并且响应于命令信号调节至少一个护罩段（38）的位置。

6. 发明公开

EP0936406A3 Burner with uniform fuel/air premixing for low emissions combustion 有权
标题翻译：燃烧器具有均匀燃料/空气预混合低排放燃烧
公开(公告)号：EP0936406A3
公开(公告)日：2000-01-19
申请号：EP99300964.6
申请日：1999-02-10
申请人： GENERAL ELECTRIC COMPANY
发明人： Battaglioli, John Luigi , Benoit, Jeffrey Arthur , Bland, Robert James , Bechtel, William Theodore, II , Black, Stephen Hugh , Deleonardo, Guy Wayne , Meyer, Stefan Martin , Tuthill, Richard Sterling , Taura, Joseph Charles
IPC分类号： F23D14/02 , F23C7/00 , F23M9/02
CPC分类号： F23C7/004 , F23C2900/07001 , F23D14/02 , F23D2206/10 , F23D2900/14021 , F23M9/02
摘要： A burner for use in a combustion system of a heavy-duty industrial gas turbine includes a fuel/air premixer having an air inlet (6), a fuel inlet (29), and an annular mixing passage (3). The fuel/air premixer mixes fuel and air into a uniform mixture for injection into a combustor reaction zone (5). The burner also includes an inlet flow conditioner (1) disposed at the air inlet of the fuel/air premixer for controlling a radial and circumferential distribution of incoming air. The pattern of perforations (11,12) in the inlet flow conditioner is designed such that a uniform air flow distribution is produced at the swirler inlet annulus in both the radial and circumference directions. The premixer includes a swozzle assembly (2) having a series of preferably air foil shaped turning vanes that impart swirl to the airflow entering via the inlet flow conditioner. Each air foil contains intemal fuel flow passages (21,22) that introduce natural gas fuel into the air stream via fuel metering holes that pass through the walls of the air foil shaped turning vanes. By injecting fuel in this manner, an aerodynamically clean flow field is maintained throughout the premixer. By injecting fuel via two separate passages, the fuel/air mixture strength distribution can be controlled in the radial direction to obtain optimum radial concentration profiles for control of emissions, lean blow outs, and combustion driven dynamic pressure activity as machine and combustor load are varied.

7. 发明公开

EP0936406A2 Burner with uniform fuel/air premixing for low emissions combustion 有权
标题翻译： Brenner mitgleichmässigerBrennstoff / Luft Vormischung zur emissionarmen Verbrennung
公开(公告)号：EP0936406A2
公开(公告)日：1999-08-18
申请号：EP99300964.6
申请日：1999-02-10
申请人： GENERAL ELECTRIC COMPANY
发明人： Battaglioli, John Luigi , Benoit, Jeffrey Arthur , Bland, Robert James , Bechtel, William Theodore, II , Black, Stephen Hugh , Deleonardo, Guy Wayne , Meyer, Stefan Martin , Tuthill, Richard Sterling , Taura, Joseph Charles
IPC分类号： F23D14/02 , F23C7/00 , F23M9/02
CPC分类号： F23C7/004 , F23C2900/07001 , F23D14/02 , F23D2206/10 , F23D2900/14021 , F23M9/02
摘要： A burner for use in a combustion system of a heavy-duty industrial gas turbine includes a fuel/air premixer having an air inlet (6), a fuel inlet (29), and an annular mixing passage (3). The fuel/air premixer mixes fuel and air into a uniform mixture for injection into a combustor reaction zone (5). The burner also includes an inlet flow conditioner (1) disposed at the air inlet of the fuel/air premixer for controlling a radial and circumferential distribution of incoming air. The pattern of perforations (11,12) in the inlet flow conditioner is designed such that a uniform air flow distribution is produced at the swirler inlet annulus in both the radial and circumference directions. The premixer includes a swozzle assembly (2) having a series of preferably air foil shaped turning vanes that impart swirl to the airflow entering via the inlet flow conditioner. Each air foil contains intemal fuel flow passages (21,22) that introduce natural gas fuel into the air stream via fuel metering holes that pass through the walls of the air foil shaped turning vanes. By injecting fuel in this manner, an aerodynamically clean flow field is maintained throughout the premixer. By injecting fuel via two separate passages, the fuel/air mixture strength distribution can be controlled in the radial direction to obtain optimum radial concentration profiles for control of emissions, lean blow outs, and combustion driven dynamic pressure activity as machine and combustor load are varied.
摘要翻译：用于重型工业燃气轮机的燃烧系统的燃烧器包括具有空气入口（6），燃料入口（29）和环形混合通道（3）的燃料/空气预混合器。燃料/空气预混合器将燃料和空气混合成均匀的混合物以注入燃烧器反应区（5）。燃烧器还包括设置在燃料/空气预混合器的空气入口处的入口流调节器（1），用于控制进入空气的径向和周向分布。入口流动调节器中的穿孔（11,12）的图案被设计成使得在径向和圆周方向上的旋流器入口环上产生均匀的气流分布。预混合器包括具有一系列优选为空气箔形的转动叶片的喷嘴组件（2），该旋转叶片对通过入口流动调节器进入的气流赋予漩涡。每个空气箔包含内部燃料流动通道（21,22），其通过燃烧计量孔将空气燃料引入空气流中，所述燃料计量孔穿过所述空气箔形转动叶片的壁。通过以这种方式喷射燃料，在整个预混合器中保持空气动力学清洁的流场。通过两个独立的通道喷射燃料，燃料/空气混合物的强度分布可以在径向方向上控制，以获得最佳的径向浓度分布，用于控制排放，稀薄吹出和燃烧驱动的动态压力活动，因为机器和燃烧器负载变化。

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