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13 条记录 (耗时 0.011 秒)

    AN OPEN CIRCUIT WEAR SENSOR FOR USE WITH A CONDUCTIVE WEAR COUNTERFACE
    3.
    发明公开
    AN OPEN CIRCUIT WEAR SENSOR FOR USE WITH A CONDUCTIVE WEAR COUNTERFACE 审中-公开
    一种用于导电磨损计量面的开路电路传感器

    公开(公告)号：EP2526399A2

    公开(公告)日：2012-11-28

    申请号：EP10801020.8

    申请日：2010-12-03

    申请人： Siemens Energy, Inc.

    发明人： MITCHELL, David, J. ,  KULKARNI, Anand, A.

    IPC分类号： G01N3/56

    CPC分类号： G01N3/56 ,  F04C14/00 ,  F04C14/28 ,  F04C2230/91 ,  F04C2240/81 ,  F04C2270/16 ,  F04C2270/86 ,  G01M5/0016 ,  G01M5/0033 ,  G01M5/0083 ,  G01N3/066

    摘要： A component including a surface subject to wear by an electrically conductive wear counterface (50). The component comprises a substrate (10); one or more material layers (32) overlying the substrate (10); a wear surface layer (16) overlying the one or more material layers (32); a first pair of spaced apart and electrically open wear sensor conductors (12/14) disposed in the substrate (10), in the one or more material layers (32), or in the wear surface layer (16); a first wear warning electrical circuit (68/69/70/74) for communicating with the first pair of conductors (12/14) for providing a first wear warning; and wherein when the wear counterface (50) has worn overlying layers, the wear counterface (50) interconnects the first pair of conductors (12/14) to activate the first wear warning circuit (68/69/70/74)

    摘要翻译： 包括受导电磨损配合面（50）磨损的表面的部件。 该部件包括衬底（10）; 覆盖衬底（10）的一个或多个材料层（32）; 覆盖所述一个或多个材料层（32）的磨损表面层（16）; 布置在所述衬底（10）中，所述一个或更多个材料层（32）中或所述耐磨表面层（16）中的第一对间隔开且电开路的磨损传感器导体（12/14）; 第一磨损警告电路（68/69/70/74），用于与第一对导体（12/14）通信以提供第一磨损警告; 并且其中当所述磨损配合面（50）具有磨损覆盖层时，所述磨损配合面（50）互连所述第一对导体（12/14）以激活所述第一磨损警告电路（68/69/70/74）

    THERMOCOUPLE FOR GAS TURBINE ENVIRONMENTS
    7.
    发明公开
    THERMOCOUPLE FOR GAS TURBINE ENVIRONMENTS 有权
    热电元件燃气轮机ENVIRONMENTS

    公开(公告)号：EP2310819A1

    公开(公告)日：2011-04-20

    申请号：EP09790020.3

    申请日：2009-07-01

    申请人： Siemens Energy, Inc.

    发明人： KULKARNI, Anand, A. ,  MITCHELL, David, J. ,  ROESCH, Edward, R.

    IPC分类号： G01K7/02 ,  G01K7/04 ,  F01D17/08

    CPC分类号： G01K7/028 ,  F01D5/288 ,  F01D17/085 ,  G01K7/04 ,  G01K2013/024 ,  G01K2217/00

    摘要： A thin-film thermocouple (12) is disclosed for use with a gas turbine component. The thermocouple may be formed on a non-planar substrate (22) having formed thereon an electrically insulating layer (34) capable of maintaining its insulating properties at gas turbine operating temperatures. A first thermocouple leg (26) made of pure platinum is then deposited on the dielectric layer (34). A second thermocouple leg (28) made of another pure metal or a transparent ceramic oxide is also formed on the dielectric layer (34) wherein the first and second thermocouple legs make ohmic contact at a first end of each leg to form a hot junction (30) for conversion of heat into an electrical signal. The thermocouple may be deposited on a surface of a thermal barrier coating or between a thermal barrier coating and an underlying metal substrate.

    INSTRUMENTED COMPONENT FOR USE IN AN OPERATING ENVIRONMENT
    9.
    发明公开
    INSTRUMENTED COMPONENT FOR USE IN AN OPERATING ENVIRONMENT 审中-公开
    INSTRUMENTIERTE KOMPONENTE ZUR VERWENDUNG IN EINER BETRIEBSUMGEBUNG

    公开(公告)号：EP2069200A2

    公开(公告)日：2009-06-17

    申请号：EP07872572.8

    申请日：2007-07-24

    申请人： Siemens Energy, Inc. ,  Roesch, Edward, R.

    发明人： MITCHELL, David, J. ,  KULKARNI, Anand, A. ,  SUBRAMANIAN, Ramesh

    IPC分类号： B64C27/00 ,  C23C28/04 ,  F01D17/02 ,  G01D3/08 ,  C04B35/00 ,  F01D21/00 ,  F23R3/00 ,  G01H11/08 ,  G08C17/02 ,  H01L41/187

    CPC分类号： C23C28/321 ,  B33Y70/00 ,  C23C28/3215 ,  C23C28/34 ,  C23C28/341 ,  C23C28/345 ,  C23C28/3455 ,  F01D5/288 ,  F01D17/02 ,  F01D21/003 ,  F01D21/10 ,  F05D2230/90 ,  F05D2300/611 ,  F23R3/007 ,  G01D3/08 ,  H04Q9/00 ,  H04Q2209/40 ,  H04Q2209/50 ,  Y02T50/673

    摘要： An instrumented component (18, 19) for use in various operating environments such as the hot gas path section of a combustion turbine engine (10). The component (18, 19) may have a substrate, a sensor (50, 204, 210) connected with the substrate for sensing a condition of the component (18, 19) within the casing during operation of the combustion turbine (10) and a connector (52, 202) attached to the substrate and in communication with the sensor (50, 204, 210) for routing a data signal from the sensor (50, 204, 210) to a termination location (53). The component (18, 19) may include a wireless telemetry device (54, 202) in communication with the connector (52, 202) for wirelessly transmitting the data signal outside the casing. A transceiver (56) may be located outside the casing for receiving the data signal and transmitting it to a processing module (30) for developing information with respect to a condition of the component (18, 19) or a coating (26) deposited on the component (18, 19).

    摘要翻译： 一种用于各种操作环境（例如燃气涡轮发动机（10）的热气路径部分））的仪表部件（18,19）。 组件（18,19）可以具有衬底，与衬底连接的传感器（50,204,210），用于在燃气轮机（10）的操作期间感测壳体内部件（18,19）的状态，以及 连接器（52,202），其连接到所述基板并与所述传感器（50,204,210）通信，用于将数据信号从所述传感器（50,204,210）路由到终止位置（53）。 组件（18,19）可以包括与连接器（52,202）通信的无线遥测设备（54,202），用于在壳体外部无线地传输数据信号。 收发器（56）可以位于外壳外部，用于接收数据信号并将其发送到处理模块（30），用于相对于组件（18,19）或沉积在其上的涂层（26）的状态显影信息 组件（18,19）。