DAMPER FINGER SEGMENT
    371.
    发明申请
    DAMPER FINGER SEGMENT 审中-公开
    阻尼指尖

    公开(公告)号:US20150207373A1

    公开(公告)日:2015-07-23

    申请号:US14601294

    申请日:2015-01-21

    CPC classification number: H02K3/16 H02K1/26 H02K1/265 H02K3/51

    Abstract: A damper finger segment is radially disposed between a retaining ring and a damper ring arrangement at a rotor end of a generator arrangement, in particular of a high power turbogenerator, having a multitude of plate-like finger elements with a longitudinal extension and arranged parallel to each other. Each neighboring pair of finger elements encloses a gap and all finger elements are joined at one end of each finger element by a band-like strip section having a longitudinal extension being oriented orthogonally to the longitudinal extension of the finger elements. At least one slot is provided in each plate-like finger element and/or in the band-like strip section. The at least one slot has a slot axis oriented parallel to the longitudinal extension of the plate-like finger elements.

    Abstract translation: 缓冲器指状部分径向地设置在发电机装置的转子端部处的保持环和阻尼器环装置之间,特别是大功率涡轮发电机,具有多个具有纵向延伸的板状指状元件并且平行于 彼此。 每个相邻的一对指状元件包围间隙,并且所有指状元件通过具有纵向延伸方向与手指元件的纵向延伸定向的带状条状部分在每个指状元件的一端连接。 在每个板状指状元件和/或带状条形部分中设置至少一个槽。 所述至少一个槽具有平行于板状指状元件的纵向延伸方向定位的槽轴。

    SEQUENTIAL COMBUSTION ARRANGEMENT WITH DILUTION GAS
    372.
    发明申请
    SEQUENTIAL COMBUSTION ARRANGEMENT WITH DILUTION GAS 审中-公开
    连续燃烧装置与稀释气体

    公开(公告)号:US20150198334A1

    公开(公告)日:2015-07-16

    申请号:US14593032

    申请日:2015-01-09

    Abstract: The invention refers to a sequential combustor arrangement including a first combustor with a first burner for admitting a first fuel into a combustor inlet gas during operation and a first combustion chamber for burning the first fuel, a dilution gas admixer for admixing a dilution gas to the first combustor combustion products leaving the first combustion chamber, and a second burner for admixing a second fuel and a second combustion chamber. To assure good mixing over a wide operating range, the ratio of the pressure loss of the first combustor to the pressure loss of the dilution gas admixer is in the range of 1 to 6. The invention further refers to a gas turbine including such a sequential combustor arrangement as well as method for operating a gas turbine with such a sequential combustor arrangement.

    Abstract translation: 本发明涉及一种连续燃烧器装置,其包括具有第一燃烧器的第一燃烧器,其具有用于在操作期间将第一燃料引入燃烧器入口气体中的第一燃烧器和用于燃烧第一燃料的第一燃烧室,用于将稀释气体混合到稀释气体的稀释气体混合器 离开第一燃烧室的第一燃烧器燃烧产物和用于混合第二燃料和第二燃烧室的第二燃烧器。 为了确保在宽的工作范围内的良好混合,第一燃烧器的压力损失与稀释气体混合器的压力损失之比在1至6的范围内。本发明还涉及一种燃气轮机,其包括这样的顺序 燃烧器装置以及用这种连续燃烧器装置操作燃气轮机的方法。

    SYSTEM AND METHOD FOR EVAPORATOR OUTLET TEMPERATURE CONTROL
    373.
    发明申请
    SYSTEM AND METHOD FOR EVAPORATOR OUTLET TEMPERATURE CONTROL 审中-公开
    蒸发器出口温度控制的系统和方法

    公开(公告)号:US20150176878A1

    公开(公告)日:2015-06-25

    申请号:US14139483

    申请日:2013-12-23

    CPC classification number: F25B39/02 F22B35/102 F22B35/108 G05D23/1934

    Abstract: Exemplary embodiments are directed to systems and methods for controlling an outlet temperature of an evaporator having a plurality of evaporator tube bundles, in which a processor is configured to compute an outlet temperature setpoint for the evaporator based on outlet temperatures of each of the plurality of evaporator tube bundles. The processor also regulates fluid flow through at least one of the evaporator tube bundles to reduce deviation between the outlet temperature of the evaporator and the outlet temperature setpoint for the evaporator.

    Abstract translation: 示例性实施例涉及用于控制具有多个蒸发器管束的蒸发器的出口温度的系统和方法,其中处理器被配置为基于多个蒸发器中的每一个的出口温度来计算蒸发器的出口温度设定点 管束。 处理器还调节通过至少一个蒸发器管束的流体流动,以减少蒸发器的出口温度与蒸发器的出口温度设定点之间的偏差。

    SOLAR RECEIVER
    374.
    发明申请
    SOLAR RECEIVER 有权
    太阳能接收器

    公开(公告)号:US20150176863A1

    公开(公告)日:2015-06-25

    申请号:US14139904

    申请日:2013-12-24

    CPC classification number: F24S80/30 F24S20/20 F24S2080/03 Y02E10/41

    Abstract: A solar receiver, designed to use a heat transfer medium, includes a plurality of panels. Each panel is arranged and configured to enable the heat transfer medium to flow in at least one flow direction, one flow direction defining a pass, to obtain unique mass flux in each pass to optimize the heat flux capability of the pass while minimizing pressure drop across the selected passes of the heat transfer surface. A method thereof is also provided.

    Abstract translation: 设计为使用传热介质的太阳能接收器包括多个面板。 每个面板被布置和配置成使得传热介质能够在至少一个流动方向(一个流动方向限定通过)中流动,以在每次通过中获得独特的质量通量,以优化通过的热通量能力,同时最小化压差 传热表面的选定通道。 还提供了其方法。

    Method for operating a combined cycle power plant
    375.
    发明授权
    Method for operating a combined cycle power plant 有权
    操作联合循环发电厂的方法

    公开(公告)号:US09046037B2

    公开(公告)日:2015-06-02

    申请号:US13714568

    申请日:2012-12-14

    Abstract: A method for operating a combined cycle power plant is disclosed, which has a gas turbine installation and a water-steam cycle connected to the gas turbine installation by a waste heat steam generator and has at least one steam turbine, the gas turbine installation includes a compressor, a combustion chamber, and a turbine. To cool the turbine, air compressed at the compressor is removed, cooled in at least one cooler flowed through by water, thus generating steam, and introduced into the turbine. At least with the gas turbine installation running, prior to or during the start-up of the water-steam cycle, waste heat, which is contained in the steam generated in the at least one cooler, is used to good effect for pre-heating the installation inside the combined cycle power plant.

    Abstract translation: 公开了一种用于操作联合循环发电厂的方法,其具有燃气轮机装置和通过废热蒸汽发生器连接到燃气轮机装置的水蒸汽循环,并且具有至少一个汽轮机,燃气轮机装置包括: 压缩机,燃烧室和涡轮。 为了冷却涡轮机,去除在压缩机处被压缩的空气,在至少一个由水流过的冷却器中冷却,从而产生蒸汽并引入涡轮。 至少在燃气轮机安装运行时,在水蒸汽循环启动之前或期间,包含在至少一个冷却器中产生的蒸汽中的废热被用于对预热的良好效果 联合循环发电厂内的安装。

    METHOD FOR MANAGING A SHUT DOWN OF A BOILER
    376.
    发明申请
    METHOD FOR MANAGING A SHUT DOWN OF A BOILER 审中-公开
    管理锅炉关闭的方法

    公开(公告)号:US20150122202A1

    公开(公告)日:2015-05-07

    申请号:US14533568

    申请日:2014-11-05

    Abstract: The method for managing a shut down of a boiler having a duct and heat exchanging components is provided. The heat exchanging component having tubed heat exchanging surfaces within the duct and headers outside the duct. The method includes regulating the temperature of the headers during shut down to a temperature close to the one expected for the steam moving from the tubed heat exchanging surfaces into the headers at a starting up following the shut down.

    Abstract translation: 提供了具有管道和热交换部件的锅炉关闭管理方法。 热交换部件具有管道内的热交换表面和管道外部的集管。 该方法包括在关闭期间将集管的温度调节到接近预期的温度,该温度在关闭之后的启动时从管式热交换表面移动到集管中预期的温度。

    Journal bearing pad for turbine
    377.
    发明授权
    Journal bearing pad for turbine 有权
    涡轮轴承垫

    公开(公告)号:US09022658B2

    公开(公告)日:2015-05-05

    申请号:US13904164

    申请日:2013-05-29

    Abstract: A hydrodynamic journal pad bearing is provided having several pads circumferentially distributed around the rotor of a large steam turbine with each pad mounted onto a platform separating the pad from a cylindrical cage in turn connected to the floor of a hall housing the turbine and having an interface between at least one of the several pads and the platform on which the at least one of the several pads is mounted is formed such as to include at least two areas with different curvatures to increase the stiffness of the interface in the event of a relative movement between the pad and the platform.

    Abstract translation: 提供了一种流体动力轴颈垫轴承,其具有围绕大型蒸汽轮机的转子周向分布的多个垫,每个垫安装到将垫与圆柱形笼分开的平台上,该平台又连接到容纳涡轮的大厅的地板并具有界面 在几个垫中的至少一个垫和其中安装有多个垫中的至少一个垫的平台之间形成为包括具有不同曲率的至少两个区域,以在相对运动的情况下增加界面的刚度 垫与平台之间。

    IMPINGEMENT COOLING ARRANGEMENT
    378.
    发明申请
    IMPINGEMENT COOLING ARRANGEMENT 有权
    冲击冷却装置

    公开(公告)号:US20150118019A1

    公开(公告)日:2015-04-30

    申请号:US14514683

    申请日:2014-10-15

    Abstract: The present disclosure refers to an impingement cooling arrangement for cooling a duct wall of a duct guiding a hot gas flow. The impingement cooling arrangement includes an impingement sleeve which is at least partly disposed in a compressed air plenum, and spaced at a distance to the duct wall to form a cooling flow path between the duct wall and the impingement sleeve such that cooling air injected from the compressed air plenum through apertures in the sleeve impinges on the duct wall. At least one flow diverter is arranged in the cooling flow path to divert the cross flow away from at least one aperture. Besides the impingement cooling arrangement a gas turbine with such an arrangement as well as a method for cooling a duct wall are provided.

    Abstract translation: 本公开内容涉及用于冷却引导热气流的管道的管道壁的冲击冷却装置。 冲击冷却装置包括冲击套管,其至少部分地设置在压缩空气通风室中,并且与导管壁间隔一定距离,以在管道壁和冲击套管之间形成冷却流动路径,使得从 通过套筒中的孔的压缩空气通风室冲击管道壁。 至少一个流量分配器布置在冷却流动路径中,以将横流转移离开至少一个孔。 除了冲击冷却装置之外,还提供了一种具有这种布置的燃气轮机以及用于冷却导管壁的方法。

    DAMPING DEVICE FOR A COMBUSTOR OF A GAS TURBINE
    379.
    发明申请
    DAMPING DEVICE FOR A COMBUSTOR OF A GAS TURBINE 审中-公开
    用于燃气轮机燃烧器的阻尼装置

    公开(公告)号:US20150113991A1

    公开(公告)日:2015-04-30

    申请号:US14522994

    申请日:2014-10-24

    Abstract: The present invention relates to a damping device for a combustor of a gas turbine for suppressing combustion instabilities. More specifically, the invention relates to a design of a broadband damping device for a low emission combustor having at least one resonator for damping pressure fluctuations in the combustion chamber. It is an object of the invention to provide a damping device with a quarter wave damper having broadband characteristics. The damping device for a combustor of a gas turbine according to the invention comprises a casing defining a resonator volume, a hole at a front face of the casing for allowing fluid communication between the resonator volume and the combustion chamber, the casing having parameters such that it acts as a quarter wave damper, is characterized in that the resonator volume is limited by a rear face and at least one lateral surface of the casing, whereby at least one lateral surface is equipped with one or more cavities inside and the rear face is equipped with at least one feed hole for feeding a purging fluid into the resonator volume. The preferably groove-shaped side cavities initiate energy dissipating vertical flows.

    Abstract translation: 本发明涉及一种用于抑制燃烧不稳定性的燃气轮机燃烧器的阻尼装置。 更具体地,本发明涉及一种用于低排放燃烧器的宽带阻尼装置的设计,其具有用于阻止燃烧室中的压力波动的至少一个谐振器。 本发明的目的是提供具有宽带特性的四分之一波形阻尼器的阻尼装置。 根据本发明的用于燃气轮机的燃烧器的阻尼装置包括限定谐振器体积的壳体,在壳体的前表面处的孔,用于允许谐振器体积和燃烧室之间的流体连通,壳体具有如下参数: 其作用为四分之一波浪阻尼器,其特征在于,谐振器体积受到壳体的后表面和至少一个侧表面的限制,由此至少一个侧表面在内部配备有一个或多个空腔,而后面是 配备有至少一个进料孔,用于将清洗流体进料到共振器体积中。 优选的槽形侧腔引发能量消散垂直流。

    HELMHOLTZ DAMPER FOR GAS TURBINE WITH COOLING AIR FLOW
    380.
    发明申请
    HELMHOLTZ DAMPER FOR GAS TURBINE WITH COOLING AIR FLOW 有权
    用于具有冷却空气流的气体涡轮机的HELMHOLTZ阻尼器

    公开(公告)号:US20150113990A1

    公开(公告)日:2015-04-30

    申请号:US14510562

    申请日:2014-10-09

    Inventor: Adnan EROGLU

    Abstract: A Helmholtz damper for a combustor of a gas turbine includes an enclosure defining a damping volume from which a neck portion extends and which has a flow path (F) for cooling and purging air with an inlet opening and an outlet opening to the enclosure. The outlet opening is formed in the neck portion. A seal is arranged at the neck portion adjacent to the outlet opening for cooling and purging air such that a cooling effect of the seal is provided.

    Abstract translation: 用于燃气涡轮机的燃烧器的亥姆霍兹阻尼器包括限定阻尼体积的外壳,颈部延伸从所述外壳中延伸并具有用于冷却和吹扫空气的流动通道(F),所述流动通道具有入口开口和到所述外壳的出口开口。 出口开口形成在颈部。 在靠近出口开口处的颈部设置密封件,用于冷却和吹扫空气,从而提供密封件的冷却效果。

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