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    SYSTEM AND METHOD FOR TURBOMACHINERY VANE PROGNOSTICS AND DIAGNOSTICS
    23.
    发明申请
    SYSTEM AND METHOD FOR TURBOMACHINERY VANE PROGNOSTICS AND DIAGNOSTICS 审中-公开
    用于涡轮增压器预处理和诊断的系统和方法

    公开(公告)号：US20160123238A1

    公开(公告)日：2016-05-05

    申请号：US14530109

    申请日：2014-10-31

    申请人： General Electric Company

    发明人： Cyron Frank Kay ,  John Carver Maters

    IPC分类号： F02C9/20 ,  F01D17/08 ,  F01D17/04 ,  F01D21/14 ,  F01D21/00 ,  F01D21/04 ,  F01D21/12 ,  F01D9/04 ,  F01D17/12

    摘要： One embodiment includes a system including an actuation system of a gas turbine system including an actuator, a positioner including one or more sensors, a motor, and a controller communicably coupled to the positioner and the motor. The actuator is coupled to one or more inlet guide vanes (IGVs) or variable stator vanes (VSVs) and configured to move the IGVs or VSVs, the positioner is configured to position the actuator so that the actuator moves the IGVs or VSVs to a desired angle, the motor is configured to drive the actuator, and the controller is configured to establish one or more baselines for one or more types of data obtained by the sensors at initialization of the gas turbine system, derive a deviation from the baselines, and perform a preventative action if a deviation that meets or exceeds a threshold is derived.

    摘要翻译： 一个实施例包括包括包括致动器的燃气轮机系统的致动系统的系统，包括一个或多个传感器的定位器，电动机以及可通信地联接到定位器和电动机的控制器。 致动器联接到一个或多个入口导向叶片（IGV）或可变定子叶片（VSV）并且被配置为移动IGV或VSV，定位器被配置为定位致动器，使得致动器将IGV或VSV移动到期望的 电动机被配置为驱动致动器，并且控制器被配置为在燃气轮机系统初始化时由传感器获得的一种或多种类型的数据建立一个或多个基准，导出与基线的偏差，并执行 如果导出满足或超过阈值的偏差，则采取预防措施。

    Method and system for determining creep capability of turbine components prior to operation
    24.
    发明授权
    Method and system for determining creep capability of turbine components prior to operation 有权
    确定运行前涡轮机部件蠕变能力的方法和系统

    公开(公告)号：US09032812B2

    公开(公告)日：2015-05-19

    申请号：US13490191

    申请日：2012-06-06

    申请人： John David Ward

    发明人： John David Ward

    IPC分类号： G01L1/22 ,  G01N29/04 ,  G01N3/08 ,  F01D21/00 ,  F01D21/12 ,  G01M15/14

    CPC分类号： G01N3/08 ,  F01D21/003 ,  F01D21/12 ,  F05D2260/81 ,  F05D2260/83 ,  G01M15/14

    摘要： A method and system for determining creep capability of turbine components is provided. A plurality of turbine components are manufactured from a material having known creep characteristics. Each of the plurality of turbine components is subjected to at least one of tensile stress, centrifugal stress and thermal stress, until a measurable amount of creep is acquired. The turbine components so tested are compared against known creep characteristics for the material used in the components. Components exhibiting an amount of creep greater than a predefined amount of creep will be separated from the plurality of turbine components and not placed into service.

    摘要翻译： 提供了一种确定涡轮机部件蠕变能力的方法和系统。 多个涡轮机部件由具有已知蠕变特性的材料制造。 多个涡轮机部件中的每一个都受到拉伸应力，离心应力和热应力中的至少一个，直到获得可测量的蠕变量。 将如此测试的涡轮机部件与组件中使用的材料的已知蠕变特性进行比较。 表现出大于预定量蠕变量的蠕变量的部件将与多个涡轮机部件分离并且不投入使用。

    Method of moving the rotating means of a wind turbine during transportation or stand still, method of controlling the moving of the rotating means, nacelle, auxiliary device, control and monitoring system and use hereof
    25.
    发明授权
    Method of moving the rotating means of a wind turbine during transportation or stand still, method of controlling the moving of the rotating means, nacelle, auxiliary device, control and monitoring system and use hereof 有权
    在运输或静止期间移动风力涡轮机的旋转装置的方法，控制旋转装置，机舱，辅助装置，控制和监测系统的运动的方法及其使用

    公开(公告)号：US08118542B2

    公开(公告)日：2012-02-21

    申请号：US12549974

    申请日：2009-08-28

    申请人： Søren Damgaard ,  Arne Haarh ,  Nils Bjørn Jensen

    发明人： Søren Damgaard ,  Arne Haarh ,  Nils Bjørn Jensen

    IPC分类号： F01D21/04 ,  F01D21/12 ,  F01D21/14 ,  F01D15/12 ,  F01D25/36

    CPC分类号： F03D1/001 ,  F03D13/10 ,  F03D13/40 ,  F03D15/10 ,  F03D17/00 ,  F03D80/00 ,  F03D80/70 ,  Y02E10/726 ,  Y02E10/728

    摘要： Methods of moving a rotating device of a wind turbine during transportation or standstill are provided. The methods include securing at least one auxiliary device to a position and connecting the device to one or more shafts of the rotating device at transportation or standstill. The auxiliary device is able to store, generate and/or convert energy during transportation, transferring energy continuously from at least one auxiliary device to one or more shafts of the rotating device during transportation or standstill, and moving one or more shafts of the rotating device continuously or discontinuously from a position to another. Also provided is a nacelle for a wind turbine, an auxiliary device, a control system for controlling moving of a rotating device of a wind turbine nacelle during transportation of the nacelle and use thereof.

    摘要翻译： 提供在运输或停止期间移动风力涡轮机的旋转装置的方法。 这些方法包括将至少一个辅助装置固定到一个位置，并且在运输或停止时将装置连接到旋转装置的一个或多个轴。 辅助装置能够在运输期间存储，产生和/或转换能量，在运输或停止期间将能量从至少一个辅助装置连续地传递到旋转装置的一个或多个轴，并且移动旋转装置的一个或多个轴 连续地或不连续地从一个位置到另一个位置。 还提供了一种用于风力涡轮机的机舱，辅助装置，用于在机舱运输期间控制风力涡轮机舱的旋转装置的移动及其使用的控制系统。

    Method and apparatus for monitoring particles in a gas turbine working fluid
    26.
    发明授权
    Method and apparatus for monitoring particles in a gas turbine working fluid 有权
    用于监测燃气轮机工作流体中的颗粒的方法和装置

    公开(公告)号：US07871237B2

    公开(公告)日：2011-01-18

    申请号：US11482614

    申请日：2006-07-07

    申请人： Richard H. Bunce ,  Francisco Dovali-Solis

    发明人： Richard H. Bunce ,  Francisco Dovali-Solis

    IPC分类号： F01D21/00 ,  F01D21/10 ,  F01D21/12 ,  F01D21/14

    CPC分类号： F01D21/003 ,  F05D2260/607 ,  F05D2260/80 ,  G01N1/2202 ,  G01N15/02

    摘要： A method and system for monitoring a gas turbine engine (20) to predict maintenance requirements. Particles suspended in a gas flow (24, 32) of the engine (20) are monitored and quantified to predict a particle accumulation rate. Monitoring may be done using particle flow sensors (61-63) in a diverted portion (33) of the working gas flow (24), such as in the cooling gas flow (32). Particle sampling (S1-S3) may be done to determine particle size and composition distributions. Particle mass flow rates may then be continuously monitored per engine operating condition, and compared to predetermined values such as a normal upper limit per engine operating condition. An integrated particle mass flow may be used in conjunction with an instantaneous mass flow rate to predict a maintenance requirement. Multiple locations (L1-L3) may be monitored to recognize a maintenance requirement by flow section or component.

    摘要翻译： 一种用于监测燃气涡轮发动机（20）以预测维护要求的方法和系统。 监测和定量悬浮在发动机（20）的气流（24,32）中的颗粒以预测颗粒堆积速率。 可以使用例如在冷却气体流（32）中的工作气体流（24）的转向部分（33）中的颗粒流量传感器（61-63）进行监测。 可以进行粒子采样（S1-S3）以确定粒度和组成分布。 然后可以在每个发动机运行状态下连续地监测粒子质量流量，并且与每个发动机操作条件的预定值（例如正常上限）进行比较。 综合的粒子质量流量可与瞬时质量流量一起使用以预测维护要求。 可以监视多个位置（L1-L3），以识别流程部分或部件的维护要求。

    Temperature probe assembly for gas turbine engine
    28.
    发明授权
    Temperature probe assembly for gas turbine engine 失效
    燃气轮机发动机温度探头组件

    公开(公告)号：US4132114A

    公开(公告)日：1979-01-02

    申请号：US777259

    申请日：1977-03-14

    申请人： Chandra C. Shah ,  James A. Laurelli

    发明人： Chandra C. Shah ,  James A. Laurelli

    IPC分类号： G01K13/04 ,  F01D21/12 ,  F01D25/00 ,  F02C7/00 ,  F02C9/00 ,  G01K1/14 ,  G01K7/02

    CPC分类号： G01K1/14

    摘要： A self-contained temperature probe assembly for sensing the disc cavity temperature of a gas turbine engine is shown. The assembly includes a thermocouple probe comprising an upper tube and a lower tube housing the probe leads. The lower tube extends from the cylinder housing through the blade ring to guide the probe tip through a hollow vane to adjacent a rotor disc and includes a tapered portion for sealing engagement with a tapered aperture in the blade ring as biased by a coil spring. The upper tube extends outwardly from the turbine cylinder to the probe head. The adjacent ends of the two tubes are retained in a standard flange in predetermined spaced relation against outward withdrawal and the lead wires are coiled within the space to maintain a slack condition to prevent transmission of vibration of the lead wires into the probe head and also prevent the rather fragile wires from supporting any weight of the probe during shipping or installation of the probe to the turbine.

    摘要翻译： 示出了用于感测燃气涡轮发动机的盘腔温度的独立温度探测器组件。 组件包括热电偶探针，其包括上管和容纳探针的下管。 下管从气缸壳体延伸穿过叶片环，以将探针尖端通过中空叶片引导到邻近转子盘，并且包括锥形部分，用于与螺旋弹簧偏压的叶片环中的锥形孔密封接合。 上管从涡轮机气缸向外延伸到探头。 两个管的相邻端以预定间隔的关系保持在标准法兰中，以防止向外抽出，并且引线在该空间内卷绕以保持松弛状态，以防止引线振动传递到探头中并且还防止 相当脆弱的电线在将探针运送或安装到涡轮机期间支撑探头的任何重量。