Instrumented Component for Wireless Telemetry
    12.
    发明申请
    Instrumented Component for Wireless Telemetry 有权
    无线遥测仪表组件

    公开(公告)号:US20090121896A1

    公开(公告)日:2009-05-14

    申请号:US11936936

    申请日:2007-11-08

    IPC分类号: G08C19/06 G08B21/00 G01L19/08

    摘要: 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).

    摘要翻译: 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。 用于为遥测发射机电路(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)固定到涡轮机叶片(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。

    Instrumented component for wireless telemetry
    13.
    发明授权
    Instrumented component for wireless telemetry 有权
    无线遥测仪表组件

    公开(公告)号:US09071888B2

    公开(公告)日:2015-06-30

    申请号:US13015782

    申请日:2011-01-28

    摘要: 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 (306) in connection with a turbine blade (301) or vane (22). A telemetry transmitter circuit (312) may be affixed to the turbine blade with an electrical connecting material (307) for routing electronic data signals from the sensor (306) to the telemetry transmitter circuit, the electronic data signals indicative of a condition of the turbine blade. A resonant energy transfer system for powering the telemetry transmitter circuit may include a rotating data antenna (314) affixed to the turbine blade or on a same substrate as that of the circuit. A stationary data antenna (320) may be affixed to a stationary component such as a stator (323) proximate and in spaced relation to the rotating data antenna for receiving electronic data signals from the rotating data antenna.

    摘要翻译: 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)的遥测系统,其包括与涡轮机叶片(301)或叶片(22)连接的传感器(306)。 遥测发射器电路(312)可以用电连接材料(307)固定到涡轮机叶片,用于将来自传感器(306)的电子数据信号路由到遥测发射器电路,指示涡轮机状态的电子数据信号 刀。 用于为遥测发射器电路供电的谐振能量传递系统可以包括固定到涡轮机叶片上的旋转数据天线(314)或与电路相同的基板上。 固定数据天线(320)可以固定到诸如定子(323)的固定部件,该固定部件靠近和间隔开关于旋转数据天线,用于从旋转数据天线接收电子数据信号。

    Instrumented component for wireless telemetry
    17.
    发明授权
    Instrumented component for wireless telemetry 有权
    无线遥测仪表组件

    公开(公告)号:US08797179B2

    公开(公告)日:2014-08-05

    申请号:US13015765

    申请日:2011-01-28

    IPC分类号: G08C19/16 G08C19/22 H04Q9/00

    摘要: A telemetry system for use in a combustion turbine engine (10) that includes a first sensor (306) in connection with a turbine blade (301) or vane (22). A first telemetry transmitter circuit (312) is affixed to the turbine blade and routes electronic data signals, indicative of a condition of the blade, from the sensor to a rotating data antenna (314) that is affixed to the turbine blade or is on a same substrate as that of the circuit. A stationary data antenna (333) may be affixed to a stationary component (323) proximate and in spaced relation to the rotating data antenna for receiving electronic data signals from the rotating data antenna. A second sensor (335) transmits electronic data signals indicative of the stationary component to a second telemetry circuit (332), which routes the signals to the stationary antenna. The stationary antenna transmits the electronic data signals to a receiver (338).

    摘要翻译: 一种用于燃气涡轮发动机(10)的遥测系统,其包括与涡轮叶片(301)或叶片(22)连接的第一传感器(306)。 第一遥测发射器电路(312)被固定到涡轮机叶片并且将表示叶片的状态的电子数据信号从传感器传送到固定到涡轮叶片上的旋转数据天线(314) 与电路相同的衬底。 固定数据天线(333)可以固定到与旋转数据天线接近且间隔开的固定部件(323),用于从旋转数据天线接收电子数据信号。 第二传感器(335)将指示静止分量的电子数据信号发送到第二遥测电路(332),其将信号路由到固定天线。 固定天线将电子数据信号发送到接收器(338)。

    Wireless telemetry for instrumented component
    19.
    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

    IPC分类号: G08C19/16

    摘要: 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).

    摘要翻译: 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。