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    • 2. 发明申请
    • BRACKET ASSEMBLY FOR A WIRELESS TELEMETRY COMPONENT
    • 用于无线远程组件的支架组件
    • US20120194396A1
    • 2012-08-02
    • US13018455
    • 2011-02-01
    • David J. MitchellAnand A. Kulkarni
    • David J. MitchellAnand A. Kulkarni
    • H01Q1/22H01Q1/42F16M13/02
    • F01D17/02F01D21/003
    • A bracket assembly is used to mount a wireless telemetry component proximate a rotating component of a combustion turbine engine (10), wherein the wireless telemetry component includes an RF transparent ceramic cover (128). The bracket assembly comprises a first mounting bracket (125) on a surface proximate the rotating component that includes a first (138) and second (139) bracket member spaced apart from one another. The first (138) and second (139) bracket members are disposed generally perpendicular to a direction of centrifugal forces generated by the rotating component. At least one of the first (138) or second bracket (139) members is inclined toward the other bracket member and disposed at an acute angle relative to the surface (141) proximate the rotating component.
    • 支架组件用于将无线遥测部件安装在燃气涡轮发动机(10)的旋转部件附近,其中无线遥测部件包括RF透明陶瓷盖(128)。 支架组件包括在靠近旋转部件的表面上的第一安装支架(125),其包括彼此间隔开的第一(138)和第二(139)支架部件。 第一(138)和第二(139)支架构件大致垂直于由旋转部件产生的离心力的方向设置。 第一(138)或第二托架(139)构件中的至少一个朝向另一托架构件倾斜,并且相对于靠近旋转构件的表面(141)以锐角设置。
    • 6. 发明申请
    • Instrumented Component for Wireless Telemetry
    • 无线遥测仪表组件
    • US20090121896A1
    • 2009-05-14
    • US11936936
    • 2007-11-08
    • David J. MitchellAnand A. KulkarniRamesh SubramanianEdward R. RoeschRod WaitsJohn R. FraleyRoberto M. SchupbachAlexander B. Lostetter
    • David J. MitchellAnand A. KulkarniRamesh SubramanianEdward R. RoeschRod WaitsJohn R. FraleyRoberto M. SchupbachAlexander B. Lostetter
    • G08C19/06G08B21/00G01L19/08
    • H04Q9/00H04Q2209/40H04Q2209/88
    • 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).
    • 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。