System for controlling variable geometry equipment for a turbine engine, especially by bellcranks
    22.
    发明授权
    System for controlling variable geometry equipment for a turbine engine, especially by bellcranks 有权
    用于控制涡轮发动机,特别是曲拐的可变几何设备的系统

    公开(公告)号:US08690521B2

    公开(公告)日:2014-04-08

    申请号:US13121726

    申请日:2009-09-29

    IPC分类号: F04D29/56

    摘要: A system for controlling at least two sets of variable geometry equipment of a turbine engine. The turbine engine includes at least one first body and a second body, the first set of equipment being a stage of variable stator vanes of a compressor of the first body moving between a closed position during idling and an open position at high speed, and the second set of equipment being at least one bleed valve of a compressor of the second body moving between an open position during idling and a closed position at high speed. The actuator drives the second set of equipment by an actuating part that is actuated over part of the course of the actuator and idle on an abutment over the rest of the course, and by a sliding joining element providing a backlash in the actuation of the second set of equipment.

    摘要翻译: 一种用于控制涡轮发动机的至少两组可变几何设备的系统。 涡轮发动机包括至少一个第一主体和第二主体,第一组设备是在空转期间的关闭位置和高速打开位置之间移动的第一主体的压缩机的可变定子叶片的阶段, 第二组设备是第二体的压缩机的至少一个放气阀,其在空转期间的打开位置和高速关闭位置之间移动。 执行器通过致动部件驱动第二组设备,该致动部件在致动部件的一部分上被致动并且在其余部分上的邻接件上空转,并且通过滑动接合元件在第二组件的致动中提供间隙 一套设备

    VARIABLE VANE ASSEMBLY FOR A GAS TURBINE ENGINE HAVING AN INCREMENTALLY ROTATABLE BUSHING
    23.
    发明申请
    VARIABLE VANE ASSEMBLY FOR A GAS TURBINE ENGINE HAVING AN INCREMENTALLY ROTATABLE BUSHING 有权
    用于具有可膨胀的气缸的气体涡轮发动机的可变风扇组件

    公开(公告)号:US20130101385A1

    公开(公告)日:2013-04-25

    申请号:US11656321

    申请日:2007-01-22

    IPC分类号: F02C9/22

    CPC分类号: F02C9/22 F01D17/162 F02K3/06

    摘要: A variable vane assembly for a gas turbine engine having a casing, including: a variable vane including a platform and a vane stem extending outwardly from the platform; a bushing surrounding the vane stem; a lever for moving the vane between a closed position and an open position; and, a mechanism for incrementally rotating the bushing to a new circumferential position with respect to the vane stem as the vane is cycled each time between the closed and open positions.

    摘要翻译: 一种用于具有壳体的燃气涡轮发动机的可变叶片组件,包括:可变叶片,包括平台和从所述平台向外延伸的叶片杆; 围绕叶片杆的衬套; 用于在关闭位置和打开位置之间移动所述叶片的杆; 以及当间歇性地在闭合位置和打开位置之间循环时,使衬套相对于叶片杆逐渐旋转到新的周向位置的机构。

    Blade variation in dependence of the degree of throttling on fluid-flow machine
    24.
    发明授权
    Blade variation in dependence of the degree of throttling on fluid-flow machine 有权
    叶片变化依赖于流体流动机器上的节流程度

    公开(公告)号:US08403621B2

    公开(公告)日:2013-03-26

    申请号:US12076088

    申请日:2008-03-13

    申请人: Volker Guemmer

    发明人: Volker Guemmer

    IPC分类号: F01B25/06

    摘要: A method for the variation of at least one blade row of a fluid-flow machine, in which, in dependence of the actual operating point, in addition to an aerodynamic speed, at least one further quantity pertinent to the position of the operating point in the family of characteristics of the fluid-flow machine is employed for control.

    摘要翻译: 一种用于改变流体流动机器的至少一个叶片排的方法,其中根据实际工作点,除了空气动力学速度之外,至少一个与操作点的位置相关的另外的量 流体流动机的特征系列被用于控制。

    BLOCKED NOZZLE DETECTION AND REMEDIAL METHOD AND SYSTEM
    26.
    发明申请
    BLOCKED NOZZLE DETECTION AND REMEDIAL METHOD AND SYSTEM 有权
    阻塞式喷嘴检测和补救方法与系统

    公开(公告)号:US20110270447A1

    公开(公告)日:2011-11-03

    申请号:US13091525

    申请日:2011-04-21

    IPC分类号: G05D7/00

    摘要: System and method for controlling a stuck nozzle system installed between first and second turbines connected in series to a compressor. The method includes determining whether the nozzle system is stuck; instructing the first turbine to increase a minimum speed reference when the nozzle system is stuck; verifying whether the nozzle system continues to be stuck; instructing the compressor to increase an inlet bleed heat (IBH) flow from a current value to a maximum value when the nozzle system is stuck; verifying whether the nozzle system continues to be stuck; and instructing the compressor to increase an inlet guide vanes (IGV) angle from a current value to a maximum value when the nozzle system is stuck.

    摘要翻译: 用于控制安装在与压缩机串联连接的第一和第二涡轮机之间的卡住喷嘴系统的系统和方法。 该方法包括确定喷嘴系统是否卡住; 指示第一涡轮机在喷嘴系统卡住时增加最小速度参考值; 验证喷嘴系统是否继续卡住; 指示当喷嘴系统被卡住时,压缩机将入口放热(IBH)流从当前值增加到最大值; 验证喷嘴系统是否继续卡住; 并且当喷嘴系统被卡住时,指示压缩机将入口导叶(IGV)角从当前值增加到最大值。

    GAS TURBINE AND METHOD FOR ITS OPERATION
    27.
    发明申请
    GAS TURBINE AND METHOD FOR ITS OPERATION 审中-公开
    气体涡轮及其运行方法

    公开(公告)号:US20110197593A1

    公开(公告)日:2011-08-18

    申请号:US13031918

    申请日:2011-02-22

    IPC分类号: F02C9/00

    摘要: A gas turbine and method are disclosed by which the gas turbine can be safely operated at nominal speed with reduced margin to a surge limit of a compressor. The gas turbine, via a directly driven generator which generates alternating current with an operating frequency and which is connected in a frequency-coupled manner to an electricity grid, can deliver electric power to this grid. In the case of an underfrequency event the compressor of the gas turbine is unloaded by controlled, fast closing of the variable compressor guide vanes (VGV) and as a result maintains a sufficient margin to the surge limit of the compressor.

    摘要翻译: 公开了一种燃气轮机和方法,通过该燃气轮机和方法,燃气轮机可以以标称速度安全地运行,同时减小了压缩机喘振极限的余量。 燃气轮机通过直接驱动的发电机,其产生具有工作频率的交流电并以频率耦合的方式连接到电网,可以向该电网输送电力。 在低频情况下,燃气轮机的压缩机通过控制,快速关闭可变压缩机导叶(VGV)而卸载,因此对压缩机的喘振极限保持足够的余量。

    SYSTEM FOR CONTROLLING VARIABLE GEOMETRY APPARATUSES IN A TURBINE ENGINE
    28.
    发明申请
    SYSTEM FOR CONTROLLING VARIABLE GEOMETRY APPARATUSES IN A TURBINE ENGINE 有权
    用于控制涡轮发动机中可变几何装置的系统

    公开(公告)号:US20110182716A1

    公开(公告)日:2011-07-28

    申请号:US13121700

    申请日:2009-09-23

    IPC分类号: F01D17/00

    摘要: A control system for controlling at least two variable-geometry devices of a turbomachine, and a turbomachine including such a control system, the system including an actuator that actuates both devices; one of the devices including at least one stage of variable-pitch stator vanes, and the other device being an air-bleed valve for a turbomachine body. The system is configured to control progression opening of the vane stage and progressive closing of the air-bleed valve as an actuation parameter of the actuator increases. As a result, the control system serves advantageously to control two devices using a single control system.

    摘要翻译: 一种用于控制涡轮机的至少两个可变几何装置的控制系统和包括这种控制系统的涡轮机,所述系统包括致动器两者的致动器; 所述装置中的一个包括至少一级可变节距定子叶片,另一装置是用于涡轮机体的排气阀。 该系统被配置为当致动器的致动参数增加时控制叶片级的进行开度和排气阀的逐渐关闭。 因此,控制系统有利地使用单个控制系统来控制两个装置。

    GAS TURBINE CONTROL DEVICE
    30.
    发明申请
    GAS TURBINE CONTROL DEVICE 有权
    气体涡轮控制装置

    公开(公告)号:US20110056180A1

    公开(公告)日:2011-03-10

    申请号:US12933963

    申请日:2009-04-10

    IPC分类号: F02C9/00

    摘要: Occurrence of combustion vibration is prevented in a gas turbine plant by enhancing the degree of freedom in setting an airflow rate or a fuel flow rate in correspondence with a target load thereby enhancing combustion stability. A gas turbine controller comprises a first function generator (62) for setting the flow rate of fuel or air being supplied to a combustor (32) in correspondence with a target load, an suction air temperature sensor (22) for detecting intake temperature at the inlet of a compressor, a second function generator (69) for setting a correction amount of a set value of fuel flow rate or air flow rate based on the value detected by the suction air temperature sensor (22), a third function generator (66) for setting a modification amount of the correction amount while taking account of the target load, a first multiplier (68); for operating a modified correction amount from a correction amount set by the second function generator and a modification amount set by the third function generator, and a second multiplier (64) for calculating the flow rate of fuel or air being supplied to a combustor by adding the modified correction amount to the set value of fuel flow rate or air flow rate set by the first function generator.

    摘要翻译: 通过提高与目标负荷相对应地设定气流速度或燃料流量的自由度,从而提高燃烧稳定性,可以防止燃气轮机厂的燃烧振动的发生。 一种燃气轮机控制器包括:第一功能发生器(62),用于根据目标负载设定供给到燃烧器(32)的燃料或空气的流量;吸入空气温度传感器(22),用于检测 第二功能发生器(69),用于基于由吸入空气温度传感器(22)检测的值来设定燃料流量或空气流量的设定值的校正量,第三功能发生器(66) ),用于在考虑目标负载的同时设定修正量的修正量,第一乘法器(68); 用于从由第二函数发生器设定的校正量和由第三函数发生器设置的修正量操作修正校正量;以及第二乘法器(64),用于计算通过添加向燃烧器供应的燃料或空气的流量 将修正校正量设定为由第一函数发生器设定的燃料流量或空气流量的设定值。