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195 条记录 (耗时 0.018 秒)

    A LEVERED JOINT
    71.
    发明授权
    A LEVERED JOINT 有权
    杠杆联合

    公开(公告)号：EP3144484B1

    公开(公告)日：2018-01-17

    申请号：EP16182194.7

    申请日：2016-08-01

    申请人： Rolls-Royce plc

    发明人： Smith, William ,  Shorney, Andrew ,  Mawhinney, Paul

    IPC分类号： F01D21/04

    CPC分类号： F01D11/02 ,  F01D11/001 ,  F01D21/045 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/24 ,  F05D2270/09

    摘要： Described is a gas turbine engine, comprising: a first chamber (330) and a second chamber (332) separated by a partition wall (322); wherein the partition wall (322) includes a stationary element and a rotating element separated by a seal and either of the stationary element and the rotating element of the partition wall (322) is segmented by a levered joint (346), wherein the levered joint (346) includes a lever (348) having a trigger plate (350), a fixture portion (352) and a fulcrum portion (354); and, the other of the stationary element and rotating element includes a hammer 360 which is axially aligned and separated from the trigger plate (350) in a first position, and forcibly contacts the hammer (360) portion in a second position so as to create a moment on the lever (348) via the trigger plate (350), the moment forcing the levered joint apart.

    STEAM TURBINE
    74.
    发明授权
    STEAM TURBINE 有权
    DAMPFTURBINE

    公开(公告)号：EP2960442B1

    公开(公告)日：2017-05-03

    申请号：EP13879003

    申请日：2013-03-22

    申请人： MITSUBISHI HEAVY IND COMPRESSOR CORP

    发明人： KATAGAKE MAKOTO

    IPC分类号： F01D17/10 ,  F01D17/14 ,  F01D17/18 ,  F01D17/24 ,  F01D21/00 ,  F01D21/14 ,  H02P3/02

    CPC分类号： F01D17/18 ,  F01D17/145 ,  F01D17/24 ,  F01D21/006 ,  F01D21/14 ,  F05D2220/31 ,  F05D2260/90 ,  F05D2270/09

    摘要： A steam turbine includes a turbine body; a steam flow passage; a regulating valve which regulates opening and closing of the steam flow passage with a linear motion; a switching drive mechanism which drives the regulating valve; an electronic governor which controls at least the switching drive mechanism; and a controller unit. The switching drive mechanism has an electric motor which rotates when supplied with power, a conversion mechanism which converts a rotary motion of the electric motor into a linear motion of the regulating valve, and a brake which brakes the rotary motion of the electric motor. At least one of the controller unit and the electronic governor performs control such that the brake is actuated and the position of the regulating valve is maintained when at least one of the electric motor and the controller unit breaks down.

    摘要翻译： 蒸汽涡轮机包括涡轮机体; 蒸汽流动通道; 调节阀，其以直线运动调节蒸汽流动通道的开启和关闭; 驱动调节阀的切换驱动机构; 电子调速器，其至少控制所述切换驱动机构; 和一个控制器单元。 切换驱动机构具有在通电时旋转的电动机，将电动机的旋转运动转换为调节阀的直线运动的转换机构以及制动电动机的旋转运动的制动器。 控制器单元和电子调速器中的至少一个执行控制，使得制动器被致动，并且当电动机和控制器单元中的至少一个故障时维持调节阀的位置。

    TURBINE ENGINE HAVING VARIABLE PITCH OUTLET GUIDE VANES
    76.
    发明公开
    TURBINE ENGINE HAVING VARIABLE PITCH OUTLET GUIDE VANES 审中-公开
    TURBINENMOTOR MIT VERSTELLBARER NACHLEITSCHAUFEL

    公开(公告)号：EP3093443A1

    公开(公告)日：2016-11-16

    申请号：EP16168718.1

    申请日：2016-05-09

    申请人： General Electric Company

    发明人： MILLER, Brandon Wayne ,  BREEZE-STRINGFELLOW, Andrew ,  ZATORSKI, Darek Tomasz

    IPC分类号： F01D9/04 ,  F01D17/16 ,  F02K3/06 ,  F04D29/56

    CPC分类号： F01D17/162 ,  F01D9/041 ,  F02C7/042 ,  F02K3/04 ,  F02K3/06 ,  F04D27/0246 ,  F04D27/0292 ,  F04D29/563 ,  F05D2220/36 ,  F05D2270/09 ,  Y02T50/673

    摘要： A gas turbine engine (10) including a core engine (16) and a fan (38) configured in mechanical communication with the core engine (16) is provided. The gas turbine engine (10) also includes a plurality of outlet guide vanes (50) positioned downstream from the fan (38) along an axial direction (A) defined by the gas turbine engine (10). The plurality of outlet guide vanes (50) extend outwardly from an outer casing (18) the core engine (16) generally along the radial direction (R) defined by the gas turbine engine (10). Each outlet guide vane (50) defines a center of pressure (52) and a pitch axis (P). The pitch axis (P) of each outlet guide vane (50) is positioned forward the center of pressure (52) of each outlet guide vane (50) such that in the event of a mechanical failure, the outlet guide vane (50) defaults to a neutral position.

    摘要翻译： 提供一种燃气涡轮发动机（10），其包括配置成与所述核心发动机（16）机械连通的核心发动机（16）和风扇（38）。 燃气涡轮发动机（10）还包括沿着由燃气涡轮发动机（10）限定的轴向（A）定位在风扇（38）下游的多个出口导流叶片（50）。 多个出口导向叶片（50）通常沿着由燃气涡轮发动机（10）限定的径向方向（R）从外壳（18）向核心发动机（16）向外延伸。 每个出口导向叶片（50）限定了压力中心（52）和俯仰轴线（P）。 每个出口引导叶片（50）的俯仰轴线（P）位于每个出口引导叶片（50）的压力中心（52）的前方，使得在机械故障的情况下，出口引导叶片（50）默认 到中立位置。

    COMPONENT, GAS TURBINE COMPONENT AND CORRESPONDING METHOD OF FORMING
    77.
    发明公开
    COMPONENT, GAS TURBINE COMPONENT AND CORRESPONDING METHOD OF FORMING 审中-公开
    宝洁，GASTURBINENBAUTEIL UNDZUGEHÖRIGESHERSTELLUNGSVERFAHREN

    公开(公告)号：EP3054105A1

    公开(公告)日：2016-08-10

    申请号：EP16153118.1

    申请日：2016-01-28

    申请人： General Electric Company

    发明人： DELVAUX, John McConnell ,  GARCIA-CRESPO, Andres Jose ,  MORGAN, Victor John ,  KITTLESON, Jacob John

    IPC分类号： F01D11/08 ,  F01D5/18 ,  F01D5/28

    CPC分类号： C04B35/565 ,  B29C70/545 ,  B29C71/04 ,  B29L2031/7504 ,  B32B3/266 ,  C04B35/44 ,  C04B35/52 ,  F01D5/186 ,  F01D5/282 ,  F01D5/284 ,  F01D5/288 ,  F01D11/08 ,  F01D11/24 ,  F01D25/12 ,  F01D25/14 ,  F02C6/06 ,  F02C6/08 ,  F05D2230/90 ,  F05D2240/11 ,  F05D2260/202 ,  F05D2260/232 ,  F05D2270/09 ,  F05D2270/11 ,  F05D2270/112 ,  F05D2300/2261 ,  F05D2300/6033

    摘要： Components (101) are disclosed which include a CMC substrate (103) having a first surface (105) and a second surface (107). The first surface (105) is in fluid communication with a compressed, dry fluid (109), and the second surface (107) is in fluid communication with a wet fluid stream (111) and includes a hermetic coating (113). The components (101) further include at least one opening (201) extending from the first surface (105) through a portion (203) of the CMC substrate (103), wherein, upon removal of a fragment of one or both of the hermetic coating (113) and the CMC substrate (103), the at least one opening (201) selectively permits a flow (303) of the compressed, dry fluid (109) to the second surface (107). In one embodiment, the component (101) is a gas turbine component, the wet fluid stream (111) is a hot combustion stream, the hermetic coating (113) is an environmental barrier coating (119), and the flow (303) reduces or eliminates volatilization of the CMC substrate (103). Methods for forming the components (101) are also disclosed.

    摘要翻译： 公开了包括具有第一表面（105）和第二表面（107）的CMC基板（103）的部件（101）。 第一表面（105）与压缩的干燥流体（109）流体连通，并且第二表面（107）与湿流体流（111）流体连通并且包括气密涂层（113）。 所述部件（101）还包括从所述第一表面（105）延伸穿过所述CMC基底（103）的一部分（203）的至少一个开口（201），其中，在去除所述密封件 涂层（113）和CMC衬底（103），所述至少一个开口（201）选择性地允许压缩的干燥流体（109）到第二表面（107）的流动（303）。 在一个实施例中，部件（101）是燃气轮机部件，湿流体流（111）是热燃烧流，气密涂层（113）是环境阻隔涂层（119），流体（303）减少 或消除CMC基材（103）的挥发。 还公开了用于形成部件（101）的方法。

    GAS TURBINE FLAMEOUT DETECTION
    78.
    发明公开
    GAS TURBINE FLAMEOUT DETECTION 审中-公开
    NACHWEIS VON FLAMMENDURCHSCHLAG BEI EINER GASTURBINE

    公开(公告)号：EP3039270A1

    公开(公告)日：2016-07-06

    申请号：EP14839611.2

    申请日：2014-08-26

    申请人： United Technologies Corporation

    发明人： AJAMI, Andre, M. ,  TURNER, Jason, Eric ,  WINSTON, Kenneth, W.

    IPC分类号： F02C9/00 ,  F02C9/28 ,  F02C9/46 ,  G01K13/00 ,  F02D41/22

    CPC分类号： F02C9/263 ,  F02C9/28 ,  F05D2260/80 ,  F05D2270/0831 ,  F05D2270/09 ,  F05D2270/092 ,  F05D2270/303 ,  F05D2270/309 ,  G01K3/10 ,  G01K13/02 ,  G01K2013/024

    摘要： A method includes receiving an indication of exhaust gas temperature (EGT) for a gas turbine engine, and determining, by at least one processor, based on the received indication of the EGT, a representation of a second derivative with respect to time of the EGT. The method further includes comparing the representation of the second derivative of the EGT to a threshold value, and determining, based on the comparing, an engine flameout condition of the gas turbine engine. In some embodiments, the at least one processor can determine a representation of a first derivative with respect to time of the EGT. The representation of the first derivative of the EGT can be compared to a threshold value, determined based on the received indication of the EGT, to determine the engine flameout condition.

    摘要翻译： 一种方法包括接收燃气涡轮发动机的排气温度（EGT）的指示，以及由至少一个处理器根据接收到的EGT的指示确定相对于EGT的时间的二阶导数的表示 。 该方法还包括将EGT的二阶导数的表示与阈值进行比较，并且基于比较来确定燃气涡轮发动机的发动机熄火状态。 在一些实施例中，至少一个处理器可以确定相对于EGT的时间的一阶导数的表示。 可以将EGT的一阶导数的表示与基于EGT的接收指示确定的阈值进行比较，以确定发动机熄火状况。

    STEAM TURBINE
    79.
    发明公开
    STEAM TURBINE 有权
    汽轮机

    公开(公告)号：EP2960442A1

    公开(公告)日：2015-12-30

    申请号：EP13879003.5

    申请日：2013-03-22

    申请人： Mitsubishi Heavy Industries Compressor Corporation

    发明人： KATAGAKE Makoto

    IPC分类号： F01D17/10

    CPC分类号： F01D17/18 ,  F01D17/145 ,  F01D17/24 ,  F01D21/006 ,  F01D21/14 ,  F05D2220/31 ,  F05D2260/90 ,  F05D2270/09

    摘要： A steam turbine includes a turbine body; a steam flow passage; a regulating valve which regulates opening and closing of the steam flow passage with a linear motion; a switching drive mechanism which drives the regulating valve; an electronic governor which controls at least the switching drive mechanism; and a controller unit. The switching drive mechanism has an electric motor which rotates when supplied with power, a conversion mechanism which converts a rotary motion of the electric motor into a linear motion of the regulating valve, and a brake which brakes the rotary motion of the electric motor. At least one of the controller unit and the electronic governor performs control such that the brake is actuated and the position of the regulating valve is maintained when at least one of the electric motor and the controller unit breaks down.

    摘要翻译： 蒸汽涡轮机包括涡轮机体; 蒸汽流动通道; 调节阀，其以直线运动调节蒸汽流动通道的开启和关闭; 驱动调节阀的切换驱动机构; 电子调速器，其至少控制所述切换驱动机构; 和一个控制器单元。 切换驱动机构具有在通电时旋转的电动机，将电动机的旋转运动转换为调节阀的直线运动的转换机构以及制动电动机的旋转运动的制动器。 控制器单元和电子调速器中的至少一个执行控制，使得制动器被致动，并且当电动机和控制器单元中的至少一个故障时维持调节阀的位置。

    Active temperature monitoring in gas turbine combustors
    80.
    发明公开
    Active temperature monitoring in gas turbine combustors 审中-公开
    AktiveTemperaturüberwachung在Gasturbinenbrennkammern

    公开(公告)号：EP2887037A1

    公开(公告)日：2015-06-24

    申请号：EP14194584.0

    申请日：2014-11-24

    申请人： Siemens Energy, Inc.

    发明人： DeSilva, Upul P.

    IPC分类号： G01K11/24 ,  F01D17/08 ,  G01K11/26 ,  G01K13/02

    CPC分类号： G01K11/24 ,  F01D17/085 ,  F02C3/04 ,  F05D2260/80 ,  F05D2270/09 ,  F05D2270/303 ,  G01F1/667 ,  G01K7/42 ,  G01K11/26 ,  G01K13/02 ,  G01K2013/024 ,  G01M15/14

    摘要： Acoustic pyrometry-based active temperature monitoring of gas turbine combustors, including industrial gas turbine (IGT) combustors is incorporated into the combustion monitoring and control system by addition of an acoustic transmitter or acoustic transceiver that transmits a sound wave in a line-of-sight with a plurality of thermoacoustic sensors, such as dynamic pressure sensors. Sound transmission time-of-flight is measured by the controller and correlated with path temperature along the line-of-sight. Path(s) of acoustic transmission serve as absolute temperature measurement that optionally is used for calibrating dominant mode passive bulk temperature measurement. In an integrated thermoacoustic pressure-based sensor and monitoring/control system embodiment, the controller correlates performance of an combustion thermoacoustic properties in order to identify combustion anomalies by wavelet or Fourier analysis techniques, determine bulk temperature characteristics within the combustor with dominant mode frequency analysis techniques and determines absolute active path temperatures within the combustor with acoustic transmission and time-of-flight analysis techniques.

    摘要翻译： 包括工业燃气轮机（IGT）燃烧器在内的燃气轮机燃烧器的基于高温测量的主动温度监测通过添加在视线中传输声波的声发射器或声收发器而被并入到燃烧监测和控制系统中 具有多个热声传感器，例如动态压力传感器。 声音传输的飞行时间由控制器测量，并与视线的路径温度相关。 声学传播的路径用作绝对温度测量，可选地用于校准主模式被动体温度测量。 在基于集成热声压力的传感器和监测/控制系统实施例中，控制器将燃烧热声特性的性能相关联，以通过小波或傅立叶分析技术识别燃烧异常，以主模式频率分析技术确定燃烧室内的体温特性 并用声传播和飞行时间分析技术确定燃烧器内的绝对主动路径温度。