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114 条记录 (耗时 0.023 秒)

    Shaft Failure Detection Using Passive Control Methods
    63.
    发明申请
    Shaft Failure Detection Using Passive Control Methods 审中-公开
    使用被动控制方法的轴故障检测

    公开(公告)号：US20170022907A1

    公开(公告)日：2017-01-26

    申请号：US15149256

    申请日：2016-05-09

    申请人： Rolls-Royce North American Technologies, Inc.

    发明人： Christopher Argote ,  John K. Harvell ,  Arthur L. Rowe

    IPC分类号： F02C9/56 ,  F02C7/262 ,  F02C9/28

    CPC分类号： F02C9/56 ,  F01D21/04 ,  F02C7/262 ,  F02C9/28 ,  F05D2270/02 ,  F05D2270/3015 ,  F05D2270/303

    摘要： A method for use in a turbine control system includes controlling fuel supply to a gas turbine engine at least in part using a fuel supply limit determined as a first function of a rotational speed of a shaft of the gas turbine engine. The method also includes obtaining a first value representative of a rotational speed of the shaft, and differentiating the first value within a processing unit. The processing unit determines an adjusted fuel supply limit as an adjusted function of the first value. The adjusted function is based on the first function and the differentiated first value. The method further includes controlling the fuel supply to the gas turbine engine at least in part using the adjusted fuel supply limit.

    摘要翻译： 一种用于涡轮机控制系统的方法包括至少部分地使用被确定为燃气涡轮发动机的轴的转速的第一函数的燃料供给极限来控制对燃气涡轮发动机的燃料供给。 该方法还包括获得代表轴的转速的第一值，并且将第一值区分在处理单元内。 处理单元将调整后的燃料供给极限确定为第一值的调整函数。 调整后的功能基于第一个功能和差分的第一个值。 该方法还包括至少部分地使用调节的燃料供应限制来控制燃气涡轮发动机的燃料供应。

    SYSTEM AND METHOD OF CONTROLLING A TWO-SHAFT GAS TURBINE
    64.
    发明申请
    SYSTEM AND METHOD OF CONTROLLING A TWO-SHAFT GAS TURBINE 审中-公开
    控制双轴瓦斯涡轮机的系统和方法

    公开(公告)号：US20150135722A1

    公开(公告)日：2015-05-21

    申请号：US14543028

    申请日：2014-11-17

    申请人： MITSUBISHI HITCHI POWER SYSTEMS, LTD.

    发明人： Yasuo TAKAHASHI ,  Takuya TAKEDA

    IPC分类号： F02C3/107 ,  F02C7/36 ,  F02C9/56

    CPC分类号： F02C3/107 ,  F02C3/10 ,  F02C7/1435 ,  F02C7/36 ,  F02C9/54 ,  F02C9/56 ,  F05D2270/023 ,  F05D2270/16 ,  F05D2270/304

    摘要： A two-shaft gas turbine control system and method are provided that can enhance the efficiency and reliability thereof by controlling the amount of intake air spray and the rotational speed of a high-pressure turbine in accordance with the aperture of an inlet guide vane in a state where a two-shaft gas turbine is being operated with the efficiency of its compressor reduced.The control system includes a droplet spray device for spraying droplets to intake air for the compressor and a controller. The controller includes a fuel control section for adjusting a flow rate of the fuel to be supplied to the combustor, a spray flow rate control section for adjusting a flow rate of spray water to be supplied to the droplet spray device, an inlet guide vane aperture control section for adjusting the aperture of the inlet guide vane, and an efficiency improvement control section for outputting a command signal for bringing a balance between driving force for the compressor and power output of the high-pressure turbine to the fuel control section, the spray flow rate control section and the inlet guide aperture control section. In response to the commands from the improvement control section, the controller reduces the rotational speed of the high-pressure turbine and controls the inlet guide vane so as to be more open, thereby appropriately controlling the flow rate of the spray water.

    摘要翻译： 提供了一种双轴燃气轮机控制系统和方法，其通过根据入口导叶的孔径控制进气喷射量和高压涡轮机的旋转速度来提高其效率和可靠性 其中双轴燃气轮机正在以其压缩机的效率降低而运行的状态。 控制系统包括用于将液滴喷射到用于压缩机的进气和控制器的液滴喷射装置。 控制器包括用于调节供给到燃烧器的燃料的流量的燃料控制部，用于调节供给到液滴喷射装置的喷射水的流量的喷雾流量控制部， 用于调节入口引导叶片的孔径的控制部分，以及效率改善控制部分，用于输出用于使压缩机的驱动力和高压涡轮机的功率输出之间的平衡的指令信号到燃料控制部分，喷雾 流量控制部和入口引导孔径控制部。 响应于来自改进控制部的命令，控制器降低高压涡轮机的转速并且控制入口导向叶片以更开放，从而适当地控制喷射水的流量。

    Device for issuing authorization to act on the operating conditions of an aircraft engine and engine control system comprising same
    66.
    发明授权
    Device for issuing authorization to act on the operating conditions of an aircraft engine and engine control system comprising same 有权
    用于发出授权以对包括其的飞机发动机和发动机控制系统的操作条件起作用的装置

    公开(公告)号：US07856295B2

    公开(公告)日：2010-12-21

    申请号：US11721035

    申请日：2005-12-12

    申请人： Patrick Zaccaria ,  Marie-Pierre Fuertes

    发明人： Patrick Zaccaria ,  Marie-Pierre Fuertes

    IPC分类号： G01C5/00

    CPC分类号： F02C9/285 ,  F02C9/56 ,  F05D2260/80

    摘要： A device for issuing authorization to act on the operating conditions of an aircraft engine and engine control system includes a first unit for determining particular parameters concerning the aircraft, including the position of a power lever controlling the supply of fuel to the engine, and a second unit for determining, based on the particular parameters, whether the aircraft is in a state authorizing an action on the operating conditions of the engine and for issuing, as the case may be, a corresponding authorization signal.

    摘要翻译： 用于发出对飞机发动机和发动机控制系统的操作条件起作用的授权的装置包括用于确定与飞行器有关的特定参数的第一单元，包括控制向发动机供应燃料的动力杆的位置，以及第二单元 单元，用于基于特定参数来确定飞机是否处于授权对发动机的操作条件采取行动的状态，并且根据情况发出相应的授权信号。

    Power Turbine Speed Control Using Electrical Load Following
    69.
    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。

    Electrically coupled supercharger for a gas turbine engine
    70.
    发明授权
    Electrically coupled supercharger for a gas turbine engine 有权
    用于燃气涡轮发动机的电耦合增压器

    公开(公告)号：US07513120B2

    公开(公告)日：2009-04-07

    申请号：US11101527

    申请日：2005-04-08

    申请人： Daniel B. Kupratis

    发明人： Daniel B. Kupratis

    IPC分类号： F02C3/10 ,  F02C6/00

    CPC分类号： F02C3/10 ,  F01D15/10 ,  F02C3/113 ,  F02C7/36 ,  F02C9/56 ,  F05D2220/329 ,  F05D2270/023 ,  F05D2270/101

    摘要： A gas turbine engine, in particular a turboshaft engine, includes a spool having a turbine and a gas generator compressor mounted thereto, a source of heat positioned between the turbine and the compressor, a first shaft and a free turbine mounted to the first shaft, and a control system for transferring power between the spool and the shaft. The operating speed of the gas generator compressor is re-matched in order to improve the efficiency and surge margin of the gas generator compressor and to improve the transient performance of the gas turbine engine.

    摘要翻译： 燃气涡轮发动机，特别是涡轮轴发动机包括具有涡轮机和安装在其上的气体发生器压缩机的阀芯，位于涡轮机和压缩机之间的热源，安装在第一轴上的第一轴和自由涡轮机， 以及用于在阀芯和轴之间传递动力的控制系统。 气体发生器压缩机的运行速度重新匹配，以提高气体发生器压缩机的效率和喘振裕度，并改善燃气轮机的瞬态性能。