Gas turbine engine comprising an ultra high temperature circuit coupling open core transformer
    1.
    发明授权
    Gas turbine engine comprising an ultra high temperature circuit coupling open core transformer 有权
    燃气涡轮发动机包括一个超高温电路耦合开芯变压器

    公开(公告)号:US09129742B2

    公开(公告)日:2015-09-08

    申请号:US13176800

    申请日:2011-07-06

    IPC分类号: G08C17/04 G01R15/18 H01F38/14

    摘要: An inductance-stable ultra high temperature circuit coupling transformer (50) used to transmit and receive alternating current power and/or data signals (29″, 33″). Primary (30″) and secondary (34″) windings are formed on nanostructured laminated (31′) primary and secondary steel cores (32″) having a Curie temperature exceeding an ultra high operating temperature. The operating range can extend from ambient to 250° C. or to in excess of 550° C. or up to 700° C. with a change in inductance of less than 10% in various embodiments.

    摘要翻译: 用于发送和接收交流电力和/或数据信号(29“,33”)的电感稳定的超高温电路耦合变压器(50)。 主要(30“)和次级(34”)绕组形成在居里温度超过超高工作温度的纳米结构层压(31')初级和次级钢芯(32“)上。 在各种实施例中,工作范围可以从环境温度延伸至250℃或超过550℃或高达700℃,电感变化小于10%。

    ULTRA HIGH TEMPERATURE CIRCUIT COUPLING
    2.
    发明申请
    ULTRA HIGH TEMPERATURE CIRCUIT COUPLING 有权
    超高温电路耦合

    公开(公告)号:US20130008179A1

    公开(公告)日:2013-01-10

    申请号:US13176800

    申请日:2011-07-06

    摘要: An inductance-stable ultra high temperature circuit coupling transformer (50) used to transmit and receive alternating current power and/or data signals (29″, 33″). Primary (30″) and secondary (34″) windings are formed on nanostructured laminated (31′) primary and secondary steel cores (32″) having a Curie temperature exceeding an ultra high operating temperature. The operating range can extend from ambient to 250° C. or to in excess of 550° C. or up to 700° C. with a change in inductance of less than 10% in various embodiments.

    摘要翻译: 用于发送和接收交流电力和/或数据信号(29“,33”)的电感稳定的超高温电路耦合变压器(50)。 主要(30“)和次级(34”)绕组形成在居里温度超过超高工作温度的纳米结构层压(31')初级和次级钢芯(32“)上。 在各种实施例中,工作范围可以从环境温度延伸至250℃或超过550℃或高达700℃,电感变化小于10%。

    WIRELESS TELEMETRY SYSTEM FOR A TURBINE ENGINE
    3.
    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

    IPC分类号: G06F15/00

    CPC分类号: F01D17/02 F01D17/20

    摘要: 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).

    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)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)。

    Wireless telemetry system for a turbine engine
    4.
    发明授权
    Wireless telemetry system for a turbine engine 有权
    用于涡轮发动机的无线遥测系统

    公开(公告)号:US08527241B2

    公开(公告)日:2013-09-03

    申请号:US13018469

    申请日:2011-02-01

    IPC分类号: G06F11/00 G08C19/16 G01K1/08

    CPC分类号: F01D17/02 F01D17/20

    摘要: 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).

    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)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)。

    INSTRUMENTED COMPONENT FOR WIRELESS TELEMETRY
    6.
    发明申请
    INSTRUMENTED COMPONENT FOR WIRELESS TELEMETRY 有权
    用于无线电报的仪表组件

    公开(公告)号:US20110133950A1

    公开(公告)日:2011-06-09

    申请号:US13015782

    申请日:2011-01-28

    IPC分类号: G08C19/12

    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
    8.
    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。