Instrumented component for use in an operating environment
    82.
    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

    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)。

    Apparatus and Method of Monitoring Operating Parameters of a Gas Turbine
    83.
    发明申请
    Apparatus and Method of Monitoring Operating Parameters of a Gas Turbine 有权
    监测燃气轮机运行参数的装置及方法

    公开(公告)号:US20100117859A1

    公开(公告)日:2010-05-13

    申请号:US12550715

    申请日:2009-08-31

    Abstract: An integrated, self-powered, sensing and transmitting module (300) that can be placed within an operating environment, such as by being affixed to a gas turbine engine component, in order to sense the local operating environment and to deliver real-time operating environment data to a location outside of the environment. Such a module may integrate a power element (302); a sensing element 9304); and a transmitting element (308) on a single substrate (320) within a single housing (310). Both sensors and circuitry components are formed directly on or in the substrate in novel configurations to decrease the size and weight of the module.

    Abstract translation: 集成的,自供电的感测和传输模块(300),其可以放置在操作环境内,例如通过固定到燃气涡轮发动机部件,以便感测本地操作环境并且传送实时操作 环境数据到环境以外的位置。 这样的模块可以集成功率元件(302); 感测元件9304); 以及在单个壳体(310)内的单个基板(320)上的发射元件(308)。 传感器和电路组件都以新颖的结构直接形成在基板上或基板上,以减小模块的尺寸和重量。

    Apparatus and method of detecting wear in an abradable coating system
    85.
    发明授权
    Apparatus and method of detecting wear in an abradable coating system 有权
    在可磨损涂层系统中检测磨损的装置和方法

    公开(公告)号:US07618712B2

    公开(公告)日:2009-11-17

    申请号:US11269044

    申请日:2005-11-08

    Abstract: A component for use in a combustion turbine (10) is provided that includes a substrate (212) and an abradable coating system (216) deposited on the substrate (212). A planar proximity sensor (250) may be deposited beneath a surface of the abradable coating system (216) having circuitry (252) configured to detect intrusion of an object (282) into the abradable coating system (216). A least one connector (52) may be provided in electrical communication with the planar proximity sensor (250) for routing a data signal from the planar proximity sensor (250) to a termination location (59). A plurality of trenches (142) may be formed at respective different depths below the surface of the abradable coating system (216) with a planar proximity sensor (250) deposited within each of the plurality of trenches (142). A processing module (34) may be programmed for receiving data from the planar proximity sensor (250) and calculating a clearance between a row of blades (18,19) within a combustion turbine and the planar proximity sensor (250). The processing module (34) may control a clearance between the row of blades (18) and a ring segment (284) based on data received from the planar proximity sensors (250).

    Abstract translation: 提供了一种用于燃气轮机(10)的部件,其包括沉积在基板(212)上的基板(212)和可磨损涂层系统(216)。 平面接近传感器(250)可以沉积在具有电路(252)的可磨损涂层系统(216)的表面下方,该电路被构造成检测物体(282)侵入到可磨损涂层系统(216)中。 可以提供与平面接近传感器(250)电通信的至少一个连接器(52),用于将数据信号从平面接近传感器(250)路由到终止位置(59)。 可以在沉积在多个沟槽(142)的每一个内的平面接近传感器(250)在可磨损涂层系统(216)的表面下方的相应不同深度处形成多个沟槽(142)。 处理模块(34)可以被编程为从平面接近传感器(250)接收数据并且计算燃烧涡轮机内的一排叶片(18,19)与平面接近传感器(250)之间的间隙。 处理模块(34)可以基于从平面接近传感器(250)接收的数据来控制叶片行(18)和环形段(284)之间的间隙。

Patent Agency Ranking