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    Stabilizing A Gas Turbine Engine Via Incremental Tuning During Transients
    4.
    发明申请
    Stabilizing A Gas Turbine Engine Via Incremental Tuning During Transients 有权
    在瞬态期间通过增量调节来稳定燃气轮机发动机

    公开(公告)号：US20140200721A1

    公开(公告)日：2014-07-17

    申请号：US14213122

    申请日：2014-03-14

    申请人： Hany Rizkalla ,  Donald Gauthier ,  Sumit Soni ,  Peter John Stuttaford

    发明人： Hany Rizkalla ,  Donald Gauthier ,  Sumit Soni ,  Peter John Stuttaford

    IPC分类号： G05D7/06

    CPC分类号： G05D7/0676 ,  F02C7/228 ,  F02C9/28 ,  F02C9/34 ,  F05D2270/082 ,  F05D2270/301 ,  F05D2270/31 ,  F23N2041/20 ,  F23R3/343 ,  F23R3/346

    摘要： Methods and systems are provided for automatically tuning a combustor of a gas turbine engine during a transient period, such as when a state of the gas turbine engine is changing. Once it has been determined whether the state of the gas turbine engine is changing, it is then determined whether a lean blowout is imminent, which is based conditions being monitored. A stability bias is applied to the system if either the state is changing or if lean blowout is imminent until the lean blowout is no longer determined to be imminent. The stability bias monitors operating conditions of the gas turbine engine and determines when one of the operating conditions has overcome a threshold value. Once a threshold value is overcome, a fuel flow fraction is adjusted by a predefined increment. The application of the stability bias is gradually terminated once it is determined that the lean blowout is no longer imminent.

    摘要翻译： 提供了用于在诸如燃气涡轮发动机的状态正在改变的过渡期间自动调节燃气涡轮发动机的燃烧器的方法和系统。 一旦确定了燃气涡轮发动机的状态是否正在改变，则确定是否迫在眉睫，这是基于监视的基础条件。 如果状态正在改变，或者如果精密喷吹即将到来，直到不再确定即将来临的稀薄喷射，系统就会施加稳定偏差。 稳定偏差监测燃气涡轮发动机的运行状况，并确定其中一个运行条件是否克服了阈值。 一旦克服了阈值，则燃料流量分数被调整预定的增量。 一旦确定稀薄井喷不再迫在眉睫，稳定性偏差的应用逐渐终止。

    Dynamic and automatic tuning of a gas turbine engine using exhaust temperature and inlet guide vane angle
    5.
    发明授权
    Dynamic and automatic tuning of a gas turbine engine using exhaust temperature and inlet guide vane angle 有权
    使用排气温度和入口导叶角度对燃气涡轮发动机进行动态和自动调谐

    公开(公告)号：US09328669B2

    公开(公告)日：2016-05-03

    申请号：US14213263

    申请日：2014-03-14

    申请人： Hany Rizkalla ,  Donald Gauthier ,  Peter John Stuttaford ,  Sumit Soni

    发明人： Hany Rizkalla ,  Donald Gauthier ,  Peter John Stuttaford ,  Sumit Soni

    IPC分类号： F02C9/22 ,  G05B15/02 ,  F02C9/00 ,  F02C9/48

    CPC分类号： F02C9/22 ,  F02C9/00 ,  F02C9/48 ,  F05D2260/964 ,  G05B15/02

    摘要： Methods and systems are provided for dynamically auto-tuning a gas turbine engine. Initially, parameters of the gas turbine engine are monitored to determine that they are within predefined upper and lower limits such that a margin exists. A first incremental adjustment of an inlet guide vane (IGV) angle is performed. If the monitored parameters are still within the predefined upper and lower limits, a second incremental adjustment of the IGV angle is performed. It is determined that the monitored parameters are still within the predefined upper and lower limits. Additionally, it is determined that a predefined value of the IGV angle has been reached such that the IGV angle is not to be further increased or decreased.

    摘要翻译： 提供了用于动态自动调节燃气涡轮发动机的方法和系统。 首先，监测燃气涡轮发动机的参数以确定它们在预定义的上限和下限内，使得存在余量。 执行入口导叶（IGV）角度的第一增量调节。 如果监视的参数仍处于预定义的上限和下限范围内，则执行IGV角度的第二增量调整。 确定监控的参数仍然在预定义的上限和下限之内。 此外，确定已经达到了IGV角度的预定值，使得IGV角度不被进一步增加或减小。

    EMPLOYING FUEL PROPERTIES TO AUTO-TUNE A GAS TURBINE ENGINE
    6.
    发明申请
    EMPLOYING FUEL PROPERTIES TO AUTO-TUNE A GAS TURBINE ENGINE 有权
    使用燃油特性自动调节气体涡轮发动机

    公开(公告)号：US20110270502A1

    公开(公告)日：2011-11-03

    申请号：US13086978

    申请日：2011-04-14

    申请人： Nicolas Demougeot ,  Donald Gauthier ,  Peter Stuttaford ,  Hany Rizkalla

    发明人： Nicolas Demougeot ,  Donald Gauthier ,  Peter Stuttaford ,  Hany Rizkalla

    IPC分类号： F02C9/26

    CPC分类号： F02C7/224 ,  F02C9/28 ,  F02C9/40

    摘要： A tuning process is provided for monitoring fuel properties of a fuel being consumed by a gas turbine (GT) engine, and for dynamically tuning the GT engine as a function of changes to the monitored fuel properties. Initially, readings are taken from the GT engine during a reference calibration, or commissioning, and utilized to calculate an initial-pressure-drop reference value. The tuning process during commercial operation takes post-calibration readings from the GT engine to calculate a fuel property parameter, which represents a heating value of the fuel. Specifically, the fuel property parameter is calculated by deriving a corrected-pressure-drop dynamic value as a function of pressure and temperature readings of the fuel at a point upstream of a combustor and pressure drops across fuel nozzles that introduce the fuel into the combustor, and solving a ratio of the dynamic value and the reference value.

    摘要翻译： 提供了一种调节过程，用于监测由燃气轮机（GT）发动机消耗的燃料的燃料性质，并且用于根据对所监测的燃料性质的变化来动态调节GT发动机。 最初，在参考校准或调试期间从GT发动机获取读数，并用于计算初始压降参考值。 商业运行过程中的调整过程需要GT发动机的后校准读数，以计算燃料特性参数，该参数代表燃料的热值。 具体地说，燃料特性参数通过导出作为燃料在燃烧器上游一点上燃料的压力和温度读数的函数的校正压降动态值来计算，并且将燃料引入燃烧器的燃料喷嘴之间的压力下降， 并求解动态值和参考值的比值。

    Dynamically Auto-Tuning a Gas Turbine Engine
    7.
    发明申请
    Dynamically Auto-Tuning a Gas Turbine Engine 有权
    动力自动调整燃气轮机发动机

    公开(公告)号：US20110265487A1

    公开(公告)日：2011-11-03

    申请号：US13053910

    申请日：2011-03-22

    申请人： Donald Gauthier ,  Nicolas Demougeot ,  Peter Stuttaford ,  Hany Rizkalla

    发明人： Donald Gauthier ,  Nicolas Demougeot ,  Peter Stuttaford ,  Hany Rizkalla

    IPC分类号： F02C9/26

    CPC分类号： F02C7/228 ,  F02C9/28 ,  F05D2270/301 ,  F05D2270/303 ,  F23N1/002 ,  F23N2037/02 ,  F23N2037/18 ,  F23N2037/28 ,  F23N2041/20 ,  F23R3/34 ,  F23R2900/00013

    摘要： Tuning processes implemented by an auto-tune controller are provided for measuring and adjusting the combustion dynamics and the emission composition of a gas turbine (GT) engine via a tuning process. Initially, the tuning process includes monitoring parameters, such as combustion dynamics and emission composition. Upon determining that one or more of the monitored parameters exceed a critical value, these “out-of-tune” parameters are compared to a scanning order table. Upon comparison, the first out-of-tune parameter that is matched within the scanning order table is addressed. The first out-of-tune parameter is then plotted as overlaid slopes on respective graphs, where the graph represents a fuel-flow split. Typically, the slopes are plotted as a particular out-of-tune parameter against a particular fuel-flow split. The slopes for each graph are considered together by taking into account the combined impact on each out-of-tune parameter when a fuel-flow split is selected for adjustment.

    摘要翻译： 提供由自动调谐控制器实现的调谐过程，用于通过调谐过程测量和调整燃气轮机（GT）发动机的燃烧动力学和发射组成。 最初，调谐过程包括监测参数，如燃烧动态和排放组成。 在确定一个或多个所监视的参数超过临界值时，将这些“失调”参数与扫描顺序表进行比较。 相比之下，寻址在扫描顺序表中匹配的第一个失调参数。 然后将第一个失调参数作为叠加的斜率绘制在各个图上，其中图表示燃料流分流。 通常，斜率被绘制为针对特定燃料流分流的特定失调参数。 当选择燃料流分流进行调整时，通过考虑对每个失调参数的组合影响，每个曲线图的斜率被一起考虑。

    Employing fuel properties to auto-tune a gas turbine engine
    8.
    发明授权
    Employing fuel properties to auto-tune a gas turbine engine 有权
    采用燃油特性自动调节燃气轮机

    公开(公告)号：US08731797B2

    公开(公告)日：2014-05-20

    申请号：US13086978

    申请日：2011-04-14

    申请人： Nicolas Demougeot ,  Donald Gauthier ,  Peter Stuttaford ,  Hany Rizkalla

    发明人： Nicolas Demougeot ,  Donald Gauthier ,  Peter Stuttaford ,  Hany Rizkalla

    IPC分类号： B60T7/12

    CPC分类号： F02C7/224 ,  F02C9/28 ,  F02C9/40

    摘要： A tuning process is provided for monitoring fuel properties of a fuel being consumed by a gas turbine (GT) engine, and for dynamically tuning the GT engine as a function of changes to the monitored fuel properties. Initially, readings are taken from the GT engine during a reference calibration, or commissioning, and utilized to calculate an initial-pressure-drop reference value. The tuning process during commercial operation takes post-calibration readings from the GT engine to calculate a fuel property parameter, which represents a heating value of the fuel. Specifically, the fuel property parameter is calculated by deriving a corrected-pressure-drop dynamic value as a function of pressure and temperature readings of the fuel at a point upstream of a combustor and pressure drops across fuel nozzles that introduce the fuel into the combustor, and solving a ratio of the dynamic value and the reference value.

    摘要翻译： 提供了一种调节过程，用于监测由燃气轮机（GT）发动机消耗的燃料的燃料性质，并且用于根据对所监测的燃料性质的变化来动态调节GT发动机。 最初，在参考校准或调试期间从GT发动机获取读数，并用于计算初始压降参考值。 商业运行过程中的调整过程需要GT发动机的后校准读数，以计算燃料特性参数，该参数代表燃料的热值。 具体地说，燃料特性参数通过导出作为燃料在燃烧器上游一点上燃料的压力和温度读数的函数的校正压降动态值来计算，并且将燃料引入燃烧器的燃料喷嘴之间的压力下降， 并求解动态值和参考值的比值。

    Indirect-fired gas turbine power plant
    9.
    发明授权
    Indirect-fired gas turbine power plant 失效
    间接燃气轮机发电厂

    公开(公告)号：US08448438B2

    公开(公告)日：2013-05-28

    申请号：US12299285

    申请日：2007-05-02

    申请人： Jason Janus ,  Brian Fleck ,  Donald Gauthier ,  Ted R. Heidrick

    发明人： Jason Janus ,  Brian Fleck ,  Donald Gauthier ,  Ted R. Heidrick

    IPC分类号： F01K25/02

    CPC分类号： F02C1/04 ,  F02C1/08 ,  Y02E20/14

    摘要： An indirect-fired gas turbine power plant comprises a compressor; a turbine mechanically coupled to the compressor; a furnace; a heat exchanger inside the furnace and fluidly coupled at an inlet end to the compressor and at an outlet end to the turbine; and means for forming a gas barrier around a portion of the heat exchanger to impede combustion products from contacting the heat exchanger. Such means can be a plurality of gas discharge manifolds located around a portion of the heat exchanger. The manifolds can be coupled to heated working gas exhausted by the turbine.

    摘要翻译： 间接燃烧的燃气轮机发电厂包括压缩机; 机械地联接到压缩机的涡轮机; 一炉 炉内的热交换器，并且在入口端处流体耦合到压缩机并且在出口端处流体连接到涡轮机; 以及用于在所述热交换器的一部分周围形成阻气以阻止燃烧产物接触所述热交换器的装置。 这种装置可以是位于热交换器的一部分周围的多个排气歧管。 歧管可以联接到由涡轮机排出的加热的工作气体。

    PROCESS FOR THE SYNTHESIS OF 4-(3-SULFONYLPHENYL)-PIPERIDINES
    10.
    发明申请
    PROCESS FOR THE SYNTHESIS OF 4-(3-SULFONYLPHENYL)-PIPERIDINES 审中-公开
    合成4-（3-三氟苯基） - 哌啶的方法

    公开(公告)号：US20070238878A1

    公开(公告)日：2007-10-11

    申请号：US11734977

    申请日：2007-04-13

    申请人： Richard Desmond ,  Paul Devine ,  Clas Sonesson ,  Donald Gauthier

    发明人： Richard Desmond ,  Paul Devine ,  Clas Sonesson ,  Donald Gauthier

    IPC分类号： C07D211/18

    CPC分类号： C07D211/24

    摘要： The present invention is directed to processes for the preparation of 4-(sulfonylphenyl)-piperidines of the Formula (VI), and pharmaceutically acceptable salts thereof; which comprises oxidizing a sulfide of the Formula (VII) or Formula (VIII), to give a compound of the Formula (IX) or Formula (X) respectively, followed by catalic reduction of the compound of the Formula (IX) or dehydration of compound of formula (X) to give a compound of Formula (IX) followed by catalytic reduction of the compound formula (IX) to give the compound of the Formula (VI).

    摘要翻译： 本发明涉及制备式（VI）的4-（磺酰基苯基） - 哌啶的方法及其药学上可接受的盐; 其包括使式（VII）或式（VIII）的硫化物氧化，分别得到式（IX）或式（X）的化合物，然后将式（IX）化合物催化还原或脱水 得到式（Ⅸ）化合物，然后将式（Ⅸ）化合物催化还原，得到式（Ⅵ）化合物。