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    Instrumented component for use in an operating environment
    2.
    发明申请
    Instrumented component for use in an operating environment 有权
    用于操作环境的仪表组件

    公开(公告)号：US20100226756A1

    公开(公告)日：2010-09-09

    申请号：US11521175

    申请日：2006-09-14

    Applicant: David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian ,  Edward R. Roesch

    Inventor： David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian ,  Edward R. Roesch

    IPC: F01D25/00

    CPC classification number: 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

    Abstract: 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).

    Abstract translation: 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的部件（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）。

    Wireless telemetry for instrumented component
    4.
    发明授权
    Wireless telemetry for instrumented component 有权
    无线遥测仪表组件

    公开(公告)号：US08519866B2

    公开(公告)日：2013-08-27

    申请号：US11936936

    申请日：2007-11-08

    Applicant: David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian ,  Edward R. Roesch ,  Rod Waits ,  John R. Fraley ,  Roberto M. Schupbach ,  Alexander B. Lostetter

    Inventor： David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian ,  Edward R. Roesch ,  Rod Waits ,  John R. Fraley ,  Roberto M. Schupbach ,  Alexander B. Lostetter

    IPC: G08C19/16

    CPC classification number: H04Q9/00 ,  H04Q2209/40 ,  H04Q2209/88

    Abstract: A telemetry system for use in a combustion turbine engine (10) having a compressor (12), a combustor and a turbine (16) that includes a sensor (50, 74) in connection with a turbine blade (18) or vane (22). A telemetry transmitter circuit (210) may be affixed to the turbine blade (18) with a first connecting material (52, 152) deposited on the turbine blade (18) for routing electronic data signals from the sensor (50, 74) to the telemetry transmitter circuit (210), the electronic data signals indicative of a condition of the turbine blade (18). An induction power system for powering the telemetry transmitter circuit (210) may include a rotating data antenna (202) affixed to the turbine blade (18) with a second connecting material (140) deposited on the turbine blade (18) for routing electronic data signals from the telemetry transmitter circuit (210) to the rotating data antenna (202). A stationary data antenna (184) may be affixed to a static seal segment 180 adjacent the turbine blade (18) for receiving electronic data signals from the rotating data antenna (202).

    Abstract translation: 一种在具有压缩机（12），燃烧器和涡轮机（16）的燃气涡轮发动机（10）中使用的遥测系统，其包括与涡轮叶片（18）或叶片（22）连接的传感器（50,74） ）。 遥测发射器电路（210）可以用沉积在涡轮叶片（18）上的第一连接材料（52,152）固定到涡轮叶片（18），用于将电子数据信号从传感器（50,74）转移到 遥测发射器电路（210），指示涡轮叶片（18）的状态的电子数据信号。 为遥测发射机电路（210）供电的感应电力系统可以包括用沉积在涡轮机叶片（18）上的第二连接材料（140）固定到涡轮叶片（18）上的旋转数据天线（202），用于路由电子数据 来自遥测发射机电路（210）到旋转数据天线（202）的信号。 固定数据天线（184）可以固定到与涡轮机叶片（18）相邻的静态密封段180，用于从旋转数据天线（202）接收电子数据信号。

    WIRELESS TELEMETRY SYSTEM FOR A TURBINE ENGINE
    5.
    发明申请
    WIRELESS TELEMETRY SYSTEM FOR A TURBINE ENGINE 有权
    涡轮发动机无线电报系统

    公开(公告)号：US20120197597A1

    公开(公告)日：2012-08-02

    申请号：US13018469

    申请日：2011-02-01

    Applicant: David J. Mitchell ,  Ramesh Subramanian ,  Cora Schillig ,  Anand A. Kulkarni ,  Vinay Jonnalagadda ,  Bulent Acar ,  Sankar Nellian ,  James P. Williams ,  Edward R. Roesch

    Inventor： David J. Mitchell ,  Ramesh Subramanian ,  Cora Schillig ,  Anand A. Kulkarni ,  Vinay Jonnalagadda ,  Bulent Acar ,  Sankar Nellian ,  James P. Williams ,  Edward R. Roesch

    IPC: G06F15/00

    CPC classification number: F01D17/02 ,  F01D17/20

    Abstract: A telemetry system for use in a combustion turbine engine (10) having a compressor (12), a combustor and a turbine (16) and includes a sensor (118) in connection with a turbine blade (111) or vane (23). A transmitter assembly (117) includes a telemetry transmitter circuit/transceiver may be affixed on a turbine blade (111) or seal plate (115) proximate the turbine blade with a first connecting material (119) deposited on the turbine blade (111) for routing electronic data signals, indicative of a condition of the turbine blade (111), from the sensor (118) to the telemetry transmitter circuit/transceiver. An induction power system for powering the telemetry transmitter circuit/transceiver may include a rotating data antenna (116) affixed to the seal plate (115) with an electrical connection (122) between the telemetry transmitting circuit/transceiver for routing electronic data signals from the telemetry transmitter circuit/transceiver to the rotating data antenna (119).

    Abstract translation: 一种用于具有压缩机（12），燃烧器和涡轮机（16）的燃气涡轮发动机（10）中的遥测系统，并且包括与涡轮机叶片（111）或叶片（23）连接的传感器（118）。 发射器组件（117）包括遥测发射器电路/收发器可以用沉积在涡轮叶片（111）上的第一连接材料（119）固定在靠近涡轮机叶片的涡轮叶片（111）或密封板（115）上，用于 将表示涡轮叶片（111）的状况的电子数据信号从传感器（118）路由到遥测发射机电路/收发器。 用于为遥测发射器电路/收发器供电的感应电力系统可以包括在遥测发射电路/收发器之间的电连接（122）固定到密封板（115）的旋转数据天线（116），用于从 遥测发射机电路/收发器到旋转数据天线（119）。

    Thermocouple for gas turbine environments
    7.
    发明授权
    Thermocouple for gas turbine environments 有权
    用于燃气轮机环境的热电偶

    公开(公告)号：US08033722B2

    公开(公告)日：2011-10-11

    申请号：US12327058

    申请日：2008-12-03

    Applicant: Anand A. Kulkarni ,  David J. Mitchell ,  Edward R. Roesch

    Inventor： Anand A. Kulkarni ,  David J. Mitchell ,  Edward R. Roesch

    IPC: G01K7/02

    CPC classification number: G01K7/028 ,  F01D5/288 ,  F01D17/085 ,  G01K7/04 ,  G01K2013/024 ,  G01K2217/00

    Abstract: 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.

    Abstract translation: 公开了一种用于燃气轮机部件的薄膜热电偶（12）。 热电偶可以形成在其上形成有能够在燃气轮机工作温度下保持其绝缘性能的电绝缘层（34）的非平面基板（22）上。 然后将由纯铂制成的第一热电偶腿（26）沉积在电介质层（34）上。 在另一纯金属或透明陶瓷氧化物上形成的第二热电偶腿（28）也形成在电介质层（34）上，其中第一和第二热电偶腿在每条腿的第一端处形成欧姆接触以形成热连接 30）用于将热量转换成电信号。 热电偶可以沉积在热障涂层的表面上，或者在热障涂层和下面的金属基底之间。

    Instrumented component for use in an operating environment
    8.
    发明授权
    Instrumented component for use in an operating environment 有权
    用于操作环境的仪表组件

    公开(公告)号：US08004423B2

    公开(公告)日：2011-08-23

    申请号：US11521175

    申请日：2006-09-14

    Applicant: David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian ,  Edward R. Roesch

    Inventor： David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian ,  Edward R. Roesch

    IPC: G08C19/12

    CPC classification number: 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

    Abstract: 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).

    Abstract translation: 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））的仪表组件（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的部件（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）。

    Instrumented component for combustion turbine engine
    9.
    发明授权
    Instrumented component for combustion turbine engine 有权
    燃气轮机发动机的组件

    公开(公告)号：US07969323B2

    公开(公告)日：2011-06-28

    申请号：US11521193

    申请日：2006-09-14

    Applicant: David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian ,  Edward R. Roesch

    Inventor： David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian ,  Edward R. Roesch

    IPC: G08C19/12

    CPC classification number: F01D21/003 ,  B33Y80/00 ,  F01D17/02 ,  F01D21/14 ,  F05D2260/80

    Abstract: An instrumented component (18, 19) for use in various operating environments such as within a combustion turbine engine (10). The component (18, 19) may have a substrate, a sensor (50, 94, 134) connected with the substrate for sensing a condition of the component (18, 19) during operation of the combustion turbine (10) and a connector (52, 92, 140) attached to the substrate and in communication with the sensor (50, 94, 134) for routing a data signal from the sensor (50, 94, 134) to a termination location (53). The component (18, 19) may include a wireless telemetry device (54, 76, 96) in communication with the connector (52, 92, 140) for wirelessly transmitting the data signal. Recesses (114, 116) may be formed with a root portion (112, 132) of components (18, 19) within which wireless telemetry device (54, 76, 96) may be affixed.

    Abstract translation: 一种在诸如燃气涡轮发动机（10）内的各种操作环境中使用的仪表部件（18,19）。 组件（18,19）可以具有衬底，与衬底连接的传感器（50,94,134），用于在燃气轮机（10）的操作期间感测组件（18,19）的状态和连接器 连接到所述基板并与所述传感器（50,94,134）通信，用于将数据信号从所述传感器（50,94,134）路由至终止位置（53）。 组件（18,19）可以包括与连接器（52,92,140）通信的无线遥测装置（54,76,96），用于无线地发送数据信号。 凹部（114,116）可以形成有可以固定无线遥测装置（54,76,96）的部件（18,19）的根部部分（112,132）。

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