Component user interface management

    公开(公告)号:US07086006B2

    公开(公告)日:2006-08-01

    申请号:US10039486

    申请日:2001-11-09

    IPC分类号: G06F3/00

    CPC分类号: G06F9/451

    摘要: A user interface framework management system for managing the user interface of a software application is provided. The user interface framework management comprises a merged application user interface for receiving a software application user interface element of the software application and a component user interface element of a component to be included with the software application, a unification unit for merging the component user interface element with the software user interface element into the merged application user interface, and an identification unit for associating the component with the component user interface element in the merged application user interface.

    Instrumented component for wireless telemetry
    5.
    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
    8.
    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。

    THERMOCOUPLE AND METHOD OF FORMING A THERMOCOUPLE ON A CONTOURED GAS TURBINE ENGINE COMPONENT
    10.
    发明申请
    THERMOCOUPLE AND METHOD OF FORMING A THERMOCOUPLE ON A CONTOURED GAS TURBINE ENGINE COMPONENT 有权
    热电偶及其在轮式涡轮发动机部件上形成热电偶的方法

    公开(公告)号:US20120236899A1

    公开(公告)日:2012-09-20

    申请号:US13417448

    申请日:2012-03-12

    摘要: A method of forming a thermocouple (12), including: depositing a first material on a component (10) to form a first leg (14); depositing a second material through a mask (30) to form a pattern (50) on the component (10), the pattern (50) forming a plurality of discrete second leg junction ends (20) and a continuous patch (52) of the second material comprising indiscrete lead ends of the second legs (16), each second leg junction end (20) spanning from a respective junction (18) with the first leg (14) to the continuous patch (52); and laser-ablating the continuous patch (52) to form discrete lead ends (22) of the second legs (16), each lead end (22) electrically connected to a respective junction end (20), thereby forming discrete second legs (16).

    摘要翻译: 一种形成热电偶(12)的方法,包括:将第一材料沉积在部件(10)上以形成第一腿部(14); 通过掩模(30)沉积第二材料以在部件(10)上形成图案(50),所述图案(50)形成多个离散的第二腿连接端(20)和连续贴片(52) 第二材料包括第二腿部(16)的不连续的引线端,每个第二腿连接端(20)从与第一腿部(14)的相应接合部(18)跨越到连续贴片(52); 并且激光烧蚀所述连续贴片(52)以形成所述第二腿部(16)的离散引线端部(22),每个引线端部(22)电连接到相应的连接端(20),由此形成离散的第二腿部 )。