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    SETTING CONTROL FOR GAS TURBINE ENGINE COMPONENT(S)
    2.
    发明申请
    SETTING CONTROL FOR GAS TURBINE ENGINE COMPONENT(S) 审中-公开

    公开(公告)号：US20170211485A1

    公开(公告)日：2017-07-27

    申请号：US15402885

    申请日：2017-01-10

    申请人： ROLLS-ROYCE plc

    发明人： Timothy TRAMONTIN

    IPC分类号： F02C9/22 ,  F01D9/04

    CPC分类号： F02C9/22 ,  F01D9/041 ,  F02C9/20 ,  F05D2200/30 ,  F05D2260/821 ,  F05D2270/021 ,  F05D2270/112 ,  F05D2270/309 ,  F05D2270/44

    摘要： A method of controlling settings of one or more actuatable gas turbine engine components includes: providing a first matrix which relates reduction in the operational parameter maximum value during the transient manoeuvre to settings of the component(s); providing a second matrix which relates the operational parameter maximum values attained during the transient manoeuvre: time to attain the maximum value after transient manoeuvre initiation, and operational parameter rate of change at the time of the maximum value; monitoring the engine in operation to identify a start of a transient manoeuvre; predicting, on the basis of the second matrix maximum values, an overshoot operational parameter amount during the identified transient manoeuvre and a time the overshoot occurrence; selecting a setting, using the first matrix, to eliminate the predicted overshoot; and applying the setting to the component(s) for a predetermined period around the predicted time of occurrence to reduce or avoid the overshoot.

    Method and Apparatus for Controlling Gas Turbine Combustor
    3.
    发明申请
    Method and Apparatus for Controlling Gas Turbine Combustor 审中-公开
    燃气轮机燃烧器控制方法与装置

    公开(公告)号：US20150159562A1

    公开(公告)日：2015-06-11

    申请号：US14621575

    申请日：2015-02-13

    申请人： Mitsubishi Hitachi Power Systems, Ltd.

    发明人： Tatsuya SEKIGUCHI ,  Shouhei YOSHIDA ,  Yoshitaka HIRATA ,  Akinori HAYASHI ,  Nozomi SAITOU ,  Kazuo TAKAHASHI ,  Takeo SAITOU

    IPC分类号： F02C9/26 ,  F02C9/28

    CPC分类号： F02C9/263 ,  F02C9/28 ,  F02C9/34 ,  F02C9/46 ,  F05D2270/082 ,  F05D2270/091 ,  F05D2270/304 ,  F05D2270/309 ,  F05D2270/31 ,  F05D2270/331 ,  F23N1/002 ,  F23N2041/20

    摘要： An apparatus for controlling a gas turbine combustor having a diffusion combustion burner and a premix combustion burner comprising: a rotating speed detector for detecting a rotating speed of gas turbine, a recorder for recording the detected value of the rotating speed of gas turbine detected by the rotating speed detector, an arithmetic unit for calculating a change with time of the rotating speed of gas turbine in accordance with details of the detected value of the rotating speed of gas turbine recorded in the recorder, and a fuel control unit for judging a starting situation of reduction in the rotating speed of gas turbine on the basis of the change with time of the rotating speed of gas turbine calculated by the arithmetic unit and controlling respectively a fuel flow rate for the diffusion combustion burner to be fed to the diffusion combustion burner installed in the gas turbine combustor and a fuel flow rate for the premix combustion to be fed to the premix combustion burner.

    摘要翻译： 一种用于控制具有扩散燃烧燃烧器和预混合燃烧器的燃气轮机燃烧器的装置，包括：用于检测燃气轮机转速的转速检测器，用于记录由所述燃气轮机检测到的燃气轮机的转速的检测值的记录器 旋转速度检测器，用于根据记录在记录器中的燃气轮机的转速的检测值的细节计算燃气轮机的转速随时间的变化的算术单元，以及用于判断起动情况的燃料控制单元 基于由运算单元计算的燃气轮机的转速随时间的变化而分别降低燃气轮机的转速，并分别控制要供给到扩散燃烧器的扩散燃烧器的燃料流量 在燃气轮机燃烧器中的燃料流量和用于预混合燃烧的燃料流量被供给到预混燃烧器 。

    HEAT EXCHANGE ARRANGEMENT
    5.
    发明申请
    HEAT EXCHANGE ARRANGEMENT 审中-公开
    热交换装置

    公开(公告)号：US20140131027A1

    公开(公告)日：2014-05-15

    申请号：US14072287

    申请日：2013-11-05

    申请人： ROLLS-ROYCE PLC

    发明人： Adam Philip CHIR

    IPC分类号： F02C9/00 ,  F28F27/00

    CPC分类号： F28F27/00 ,  F02C7/185 ,  F02K3/115 ,  F05D2270/303 ,  F05D2270/3062 ,  F05D2270/309 ,  F05D2270/702 ,  F05D2270/704 ,  Y02T50/675

    摘要： A heat exchange arrangement (40) for a gas turbine engine (10). The arrangement (40) comprises a first conduit (46) for an engine component cooling fluid and a second conduit (44) for a second fluid. The arrangement further comprises a heat exchange portion (42) in which fluids flowing through the first and second conduits (46, 44) are in a heat exchange relationship. A valve 48 is provided, which is configured to moderate the mass flow rate of one of the fluids through the heat exchange portion (42). The arrangement comprises a temperature sensor (50) configured to sense a temperature of one of the fluids after said fluid has passed through the heat exchange portion (42) and a controller (52). The controller (52) is configured to control the valve (48) in response to a rate of change of the temperature with respect to time of the fluid sensed by the temperature sensor (50).

    摘要翻译： 一种用于燃气涡轮发动机（10）的热交换装置（40）。 装置（40）包括用于发动机部件冷却流体的第一管道（46）和用于第二流体的第二管道（44）。 该装置还包括热交换部分（42），流过第一和第二导管（46,44）的流体处于热交换关系。 设置阀48，其构造成调节通过热交换部分（42）的一种流体的质量流率。 该装置包括温度传感器（50），其被配置为在所述流体通过热交换部分（42）和控制器（52）之后感测一种流体的温度。 控制器（52）被配置为响应于由温度传感器（50）感测的流体相对于时间的温度变化的速率来控制阀（48）。

    Systems, methods, and apparatus for determining steady state conditions in a gas turbine
    7.
    发明授权
    Systems, methods, and apparatus for determining steady state conditions in a gas turbine 有权
    用于确定燃气轮机中的稳态条件的系统，方法和装置

    公开(公告)号：US08285516B2

    公开(公告)日：2012-10-09

    申请号：US12834929

    申请日：2010-07-13

    申请人： Justin V. John ,  Scott William Szepek

    发明人： Justin V. John ,  Scott William Szepek

    IPC分类号： G06F15/00

    CPC分类号： F02C9/54 ,  F05D2200/20 ,  F05D2270/024 ,  F05D2270/309 ,  F05D2270/44

    摘要： Certain embodiments of the invention may include systems, methods, and apparatus for determining steady state conditions in a gas turbine. According to an example embodiment of the invention, a method for determining stability in a gas turbine is provided. The method can include receiving a guide vane (VGV) command and a fuel stroke reference (FSR) command associated with a gas turbine control system, determining a filtered VGV change based at least in part on the received VGV command, determining a filtered FSR change based at least in part on the received FSR command, and outputting a unit stability signal after a pickup delay time when the filtered VGV change is less than a predetermined VGV stability threshold and the filtered FSR change is less than a predetermined FSR stability threshold.

    摘要翻译： 本发明的某些实施例可以包括用于确定燃气轮机中的稳态条件的系统，方法和装置。 根据本发明的示例性实施例，提供了一种用于确定燃气轮机中的稳定性的方法。 该方法可以包括接收与燃气轮机控制系统相关联的引导叶片（VGV）命令和燃料冲程参考（FSR）命令，至少部分地基于所接收的VGV命令来确定经滤波的VGV改变，确定经滤波的FSR改变 至少部分地基于接收到的FSR命令，并且当经过滤波的VGV变化小于预定的VGV稳定性阈值并且滤波的FSR变化小于预定的FSR稳定性阈值时，在拾取延迟时间之后输出单元稳定性信号。

    Power Turbine Speed Control Using Electrical Load Following
    9.
    发明申请
    Power Turbine Speed Control Using Electrical Load Following 有权
    使用电气负载的功率涡轮速度控制

    公开(公告)号：US20100013243A1

    公开(公告)日：2010-01-21

    申请号：US12568439

    申请日：2009-09-28

    申请人： David G. Halsey ,  Charles J. Romenesko

    发明人： David G. Halsey ,  Charles J. Romenesko

    IPC分类号： F02D29/06

    CPC分类号： F02C9/56 ,  F01D15/10 ,  F01D21/14 ,  F02C3/10 ,  F02C6/00 ,  F02C9/26 ,  F02C9/28 ,  F05D2220/76 ,  F05D2270/052 ,  F05D2270/304 ,  F05D2270/309 ,  F05D2270/44

    摘要： A power turbine speed control system for a turbo-shaft type gas turbine engine that has a gas generator compressor spool and a power turbine spool and drives an electrical generator that powers at least one electrical load by way of at least one electrical bus, comprises a power turbine controller that senses the rotary speed of the power turbine spool and generates at least one signal that changes the torque of the electrical generator in response to the sensed change in the rotary speed of the power turbine spool.

    摘要翻译： 一种用于涡轮轴式燃气涡轮发动机的动力涡轮机速度控制系统，其具有气体发生器压缩机线轴和动力涡轮机线轴，并驱动通过至少一个电气总线对至少一个电力负载供电的发电机，包括： 动力涡轮机控制器，其感测动力涡轮阀芯的旋转速度并产生响应于感测到的动力涡轮阀芯的转速的变化而改变发电机的扭矩的至少一个信号。

    Method for turbine maintenance
    10.
    发明申请
    Method for turbine maintenance 审中-公开
    涡轮机维护方法

    公开(公告)号：US20090132202A1

    公开(公告)日：2009-05-21

    申请号：US11666398

    申请日：2005-10-28

    申请人： Ronald Stephen Walker ,  Philip S. Foster

    发明人： Ronald Stephen Walker ,  Philip S. Foster

    IPC分类号： G21C17/00

    CPC分类号： F01D19/00 ,  F05D2260/80 ,  F05D2270/309 ,  F05D2270/44 ,  G05B23/0283

    摘要： A turbine and method for determining turbine maintenance. The method for determining hot gas path turbine maintenance comprises recording a number of part load starts (79), base load starts (89), fast starts (141), full speed no load trips (231), and load trips (237); forming a weighted equivalent starts as a weighted summation of part load starts, base load starts, fast starts, full speed no load trips, and load trips; comparing the weighted equivalent starts to a predetermined threshold; and initiating the maintenance procedure. The method for determining rotor parts turbine maintenance comprises recording the number of fast starts, normal starts (143), and elapsed time starts (135) from shutdown to restart; forming a weighted equivalent starts as a weighted combination of fast starts, normal starts, and elapsed time starts from shutdown to restart; comparing the weighted equivalent starts to a predetermined threshold; and if a weighted equivalent starts exceeds the predetermined threshold, initiating the maintenance procedure.

    摘要翻译： 一种用于确定涡轮机维护的涡轮机和方法。 用于确定热气路径涡轮机维护的方法包括记录多个部分负载启动（79），基本负载启动（89），快速启动（141），全速无负载跳闸（231）和负载跳闸（237）; 形成加权等价物作为部分负荷启动的加权求和，基本负载启动，快速启动，全速无负载跳闸和负载跳闸启动; 将加权等效开始与预定阈值进行比较; 并启动维护程序。 用于确定转子部件涡轮机维护的方法包括从关机到重新开始记录快速启动次数，正常启动次数（143）和经过时间开始（135） 形成加权等价物从快速启动，正常启动和经过时间的加权组合开始，从关机到重新启动; 将加权等效开始与预定阈值进行比较; 并且如果加权等效启动超过预定阈值，则启动维护过程。