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    Gas turbine engine combustor hot streak control
    3.
    发明授权
    Gas turbine engine combustor hot streak control 失效
    燃气轮机发动机燃烧器热条纹控制

    公开(公告)号：US07739873B2

    公开(公告)日：2010-06-22

    申请号：US11256786

    申请日：2005-10-24

    申请人： Kattalaicheri Srinivasan Venkataramani ,  William Joseph Myers, Jr. ,  Robert Joseph Orlando ,  Paul Cooker ,  Ching-Pang Lee

    发明人： Kattalaicheri Srinivasan Venkataramani ,  William Joseph Myers, Jr. ,  Robert Joseph Orlando ,  Paul Cooker ,  Ching-Pang Lee

    IPC分类号： F02C9/00

    CPC分类号： F02C9/263 ,  F05D2270/112 ,  F05D2270/3032 ,  F23K5/005 ,  F23K5/06 ,  F23K2203/105 ,  F23N1/00 ,  F23N1/002 ,  F23N5/02 ,  F23N5/022 ,  F23N5/24 ,  F23N5/242

    摘要： A gas turbine engine combustion system includes a plurality of fuel injectors circumferentially disposed around a combustor in a one to one fuel supply relationship with a plurality of fuel nozzle valves, and an electronic controller for controlling the fuel nozzle valves to eliminate and/or reduce hot streaking in response to sensed hot streak conditions. The fuel nozzle valves may be modulating valves. The electronic controller may be used to individually control the fuel nozzle valves. The hot streak conditions may be sensed with temperature sensors such as temperature sensors operably mounted in the combustor. A program in the electronic controller may be used for determining broken or malfunctioning sensors by calculating a combustor temperature and comparing it to measured temperatures from the sensors and comparing the measured fuel pressures in the individual fuel nozzle circuits with the simulated or calculated fuel pressures.

    摘要翻译： 燃气涡轮发动机燃烧系统包括多个燃料喷射器，其周向地设置在与多个燃料喷嘴阀一对一燃料供给关系中的燃烧器周围;以及电子控制器，用于控制燃料喷嘴阀以消除和/或减少热量 响应于感测到的热条件条件。 燃料喷嘴阀可以是调节阀。 电子控制器可以用于单独地控制燃料喷嘴阀。 温度传感器可以感测热条纹条件，诸如可操作地安装在燃烧器中的温度传感器。 电子控制器中的程序可用于通过计算燃烧器温度并将其与来自传感器的测量温度进行比较并将各个燃料喷嘴回路中测量的燃料压力与模拟或计算的燃料压力进行比较来确定破坏或故障的传感器。

    Method of increasing engine temperature limit margins
    4.
    发明授权
    Method of increasing engine temperature limit margins 失效
    提高发动机温度限制裕度的方法

    公开(公告)号：US06681558B2

    公开(公告)日：2004-01-27

    申请号：US09817884

    申请日：2001-03-26

    申请人： Robert Joseph Orlando ,  Paul Cooker

    发明人： Robert Joseph Orlando ,  Paul Cooker

    IPC分类号： F23R300

    CPC分类号： F02K1/06 ,  F01D9/041 ,  F01D17/162 ,  F02C9/00 ,  F05D2270/11

    摘要： A method of extending a useful serviceable life of a gas turbine engine by increasing a limiting exhaust gas temperature margin degraded by engine use without replacing engine hardware. The method includes adjusting at least one engine parameter selected from a first group of engine parameters including a nozzle area and a rotor speed.

    摘要翻译： 一种通过增加由发动机使用而劣化的限制性排气温度余量而不替换发动机硬件来延长燃气涡轮发动机的有用可用寿命的方法。 该方法包括调整从包括喷嘴区域和转子速度的第一组发动机参数中选择的至少一个发动机参数。

    Continuous real time EGT margin control
    5.
    发明申请
    Continuous real time EGT margin control 审中-公开
    连续实时EGT保证金控制

    公开(公告)号：US20070214795A1

    公开(公告)日：2007-09-20

    申请号：US11376507

    申请日：2006-03-15

    申请人： Paul Cooker ,  Robert Orlando ,  Ching-Pang Lee ,  Kattalaicheri Venkataramani

    发明人： Paul Cooker ,  Robert Orlando ,  Ching-Pang Lee ,  Kattalaicheri Venkataramani

    IPC分类号： F02C1/00

    CPC分类号： F02K1/06 ,  F02C9/22 ,  F02C9/28 ,  F02K1/08 ,  F02K1/09 ,  F02K3/06 ,  F05D2270/112 ,  F05D2270/303 ,  F05D2270/3032

    摘要： A method and system for maintaining a limiting gas temperature in a gas turbine engine working fluid flowpath by monitoring the gas temperature and adjusting one or more parameters when the gas temperature exceeds a predetermined or a calculated temperature limit during engine operation. The parameters include one or more of a group of engine parameters including high and low pressure turbine nozzle flow areas, fan and core flow areas, and a rotor speed. The one or more parameters are adjusted to lower the gas temperature to below the temperature limit during engine operation. The limiting gas temperature may be a turbine exhaust gas temperature such as a high pressure turbine exhaust gas temperature. The turbine nozzle flow areas may be adjusted with variable nozzle vanes and the fan and core exhaust nozzle flow areas with a translatable fan nozzle cowling and a translatable core nozzle plug, respectively.

    摘要翻译： 一种用于通过监测气体温度并在发动机运行期间当气体温度超过预定或计算的温度极限时调节一个或多个参数来维持燃气涡轮发动机工作流体流路中的限制气体温度的方法和系统。 这些参数包括一组发动机参数中的一个或多个，包括高压和低压涡轮喷嘴流动区域，风扇和核心流动区域以及转子速度。 调节一个或多个参数以在发动机运行期间将气体温度降低到温度极限以下。 限制气体温度可以是涡轮机废气温度，例如高压汽轮机废气温度。 涡轮喷嘴流动面积可以分别用可变喷嘴叶片和风扇和核心排气喷嘴流动区域调节，其中分别具有可平移的风扇喷嘴罩和可平移的芯喷嘴塞。

    Gas turbine engine combustor hot streak control
    6.
    发明申请
    Gas turbine engine combustor hot streak control 失效
    燃气轮机发动机燃烧器热条纹控制

    公开(公告)号：US20070089424A1

    公开(公告)日：2007-04-26

    申请号：US11256786

    申请日：2005-10-24

    申请人： Kattalaicheri Venkataramani ,  William Myers ,  Robert Orlando ,  Paul Cooker ,  Ching-Pang Lee

    发明人： Kattalaicheri Venkataramani ,  William Myers ,  Robert Orlando ,  Paul Cooker ,  Ching-Pang Lee

    IPC分类号： F02C9/26

    CPC分类号： F02C9/263 ,  F05D2270/112 ,  F05D2270/3032 ,  F23K5/005 ,  F23K5/06 ,  F23K2203/105 ,  F23N1/00 ,  F23N1/002 ,  F23N5/02 ,  F23N5/022 ,  F23N5/24 ,  F23N5/242

    摘要： A gas turbine engine combustion system includes a plurality of fuel injectors circumferentially disposed around a combustor in a one to one fuel supply relationship with a plurality of fuel nozzle valves, and an electronic controller for controlling the fuel nozzle valves to eliminate and/or reduce hot streaking in response to sensed hot streak conditions. The fuel nozzle valves may be modulating valves. The electronic controller may be used to individually control the fuel nozzle valves. The hot streak conditions may be sensed with temperature sensors such as temperature sensors operably mounted in the combustor. A program in the electronic controller may be used for determining broken or malfunctioning sensors by calculating a combustor temperature and comparing it to measured temperatures from the sensors and comparing the measured fuel pressures in the individual fuel nozzle circuits with the simulated or calculated fuel pressures.

    摘要翻译： 燃气涡轮发动机燃烧系统包括多个燃料喷射器，其周向地设置在与多个燃料喷嘴阀一对一燃料供给关系中的燃烧器周围;以及电子控制器，用于控制燃料喷嘴阀以消除和/或减少热量 响应于感测到的热条件条件。 燃料喷嘴阀可以是调节阀。 电子控制器可以用于单独地控制燃料喷嘴阀。 温度传感器可以感测热条纹条件，诸如可操作地安装在燃烧器中的温度传感器。 电子控制器中的程序可用于通过计算燃烧器温度并将其与来自传感器的测量温度进行比较并将各个燃料喷嘴回路中测量的燃料压力与模拟或计算的燃料压力进行比较来确定破坏或故障的传感器。