METHOD AND DEVICE FOR COATING PATH GENERATION
    111.
    发明申请
    METHOD AND DEVICE FOR COATING PATH GENERATION 审中-公开
    用于涂抹路径生成的方法和装置

    公开(公告)号:US20120156362A1

    公开(公告)日:2012-06-21

    申请号:US12974233

    申请日:2010-12-21

    Abstract: A method for generating a motion path for a spray gun for coating a component is disclosed. Path templates for surface segments of the component are defined, the surface is analyzed, a first motion path is generated, a model of the spray profile is simulated, the coating thickness is simulated for the motion path based on the simulated model of the spray profile and the generated first motion path. The simulated coating thickness is compared with tolerances and when the simulated coating thickness does not achieve the tolerances, an adapted motion path is generated. The coating thickness is simulated for the motion path based on the simulated model of the spray profile and the generated adapted motion path. Repeating the comparing, the motion path generation, and the simulation of the coating thickness based on the generated adapted motion path until the simulated coating thickness achieves the tolerances.

    Abstract translation: 公开了一种用于产生用于涂覆部件的喷枪的运动路径的方法。 定义了部件表面段的路径模板,分析了表面,生成了第一个运动路径,模拟了喷射轮廓的模型,基于喷射轮廓的模拟模型,为运动路径模拟了涂层厚度 和产生的第一运动路径。 将模拟涂层厚度与公差进行比较,并且当模拟涂层厚度不达到公差时,产生适应的运动路径。 基于喷雾轮廓和生成的适应运动路径的模拟模型,为运动路径模拟涂层厚度。 基于生成的适应运动路径重复比较,运动路径生成和涂层厚度的模拟,直到模拟涂层厚度达到公差。

    INSTRUMENTED COMPONENT FOR WIRELESS TELEMETRY
    114.
    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:US20110133949A1

    公开(公告)日:2011-06-09

    申请号:US13015765

    申请日:2011-01-28

    Abstract: 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).

    Abstract translation: 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)。

    Instrumented component for combustion turbine engine
    115.
    发明申请
    Instrumented component for combustion turbine engine 有权
    燃气轮机发动机的组件

    公开(公告)号:US20100226757A1

    公开(公告)日:2010-09-09

    申请号:US11521193

    申请日:2006-09-14

    CPC classification number: F01D21/003 B33Y80/00 F01D17/02 F01D21/14 F05D2260/80

    Abstract: An instrumented component (18, 19) for use in various operating environments such as within a combustion turbine engine (10). The component (18, 19) may have a substrate, a sensor (50, 94, 134) connected with the substrate for sensing a condition of the component (18, 19) during operation of the combustion turbine (10) and a connector (52, 92, 140) attached to the substrate and in communication with the sensor (50, 94, 134) for routing a data signal from the sensor (50, 94, 134) to a termination location (53). The component (18, 19) may include a wireless telemetry device (54, 76, 96) in communication with the connector (52, 92, 140) for wirelessly transmitting the data signal. Recesses (114, 116) may be formed with a root portion (112, 132) of components (18, 19) within which wireless telemetry device (54, 76, 96) may be affixed.

    Abstract translation: 一种在诸如燃气涡轮发动机(10)内的各种操作环境中使用的仪表部件(18,19)。 组件(18,19)可以具有衬底,与衬底连接的传感器(50,94,134),用于在燃气轮机(10)的操作期间感测组件(18,19)的状态和连接器 连接到所述基板并与所述传感器(50,94,134)通信,用于将数据信号从所述传感器(50,94,134)路由至终止位置(53)。 组件(18,19)可以包括与连接器(52,92,140)通信的无线遥测装置(54,76,96),用于无线地发送数据信号。 凹部(114,116)可以形成有可以固定无线遥测装置(54,76,96)的部件(18,19)的根部部分(112,132)。

    Method of forming a catalyst element having a thermal barrier coating as the catalyst substrate
    116.
    发明授权
    Method of forming a catalyst element having a thermal barrier coating as the catalyst substrate 失效
    形成具有热障涂层作为催化剂基材的催化剂元件的方法

    公开(公告)号:US07691341B2

    公开(公告)日:2010-04-06

    申请号:US12099280

    申请日:2008-04-08

    Abstract: A combustion catalyst coating (36) applied to the surface of a ceramic thermal barrier coating (34) which is supported by a metal substrate (32). The microstructure of the thermal barrier coating surface provides the necessary turbulent flow and surface area for interaction of the catalyst and a fuel-air mixture in a catalytic combustor of a gas turbine engine. The temperature gradient developed across the thermal barrier coating protects the underlying metal substrate from a high temperature combustion process occurring at the catalyst surface. The thermal barrier coating deposition process may be controlled to form a microstructure having at least one feature suitable to interdict a flow of fuel-air mixture and cause the flow to become more turbulent than if such feature did not exist.

    Abstract translation: 一种燃烧催化剂涂层(36),其被施加到由金属基底(32)支撑的陶瓷热障涂层(34)的表面上。 热障涂层表面的微观结构为燃气轮机的催化燃烧器中的催化剂和燃料 - 空气混合物的相互作用提供了必要的湍流和表面积。 在隔热涂层上形成的温度梯度保护底层金属基材免受在催化剂表面发生的高温燃烧过程的影响。 可以控制热障涂层沉积过程以形成具有至少一个特征的微结构,该特征适合于阻止燃料 - 空气混合物的流动,并且使得流动比不存在这样的特征时变得更湍流。

    Apparatus and method of monitoring operating parameters of a gas turbine
    118.
    发明授权
    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和方法

    公开(公告)号:US07582359B2

    公开(公告)日:2009-09-01

    申请号:US11269043

    申请日:2005-11-08

    Abstract: A component for use in a combustion turbine (10) is provided that includes a substrate (212) and a microelectromechanical system (MEMS) device (50, 250) affixed to the substrate (212). At least one connector (52) may be deposited in electrical communication with the MEMS device (50, 250) for routing a data signal from the MEMS device (50, 250) to a termination location (59). A barrier coating (216) may be deposited on the substrate (212) wherein the MEMS device (50, 250) is affixed beneath a surface of the barrier coating (216). A plurality of trenches (142) may be formed in the barrier coating (216) at respective different depths below the surface of the barrier coating (216) and a MEMS device (50, 250) deposited within each of the plurality of trenches (142). A monitoring system (30) is provided that may include a processing module (34) programmed for receiving data from the MEMS device (50, 250).

    Abstract translation: 提供了一种用于燃气轮机(10)的部件,其包括固定到基板(212)上的基板(212)和微机电系统(MEMS)装置(50,250)。 至少一个连接器(52)可以沉积成与MEMS器件(50,250)电连通,用于将来自MEMS器件(50,250)的数据信号路由到终止位置(59)。 阻挡涂层(216)可以沉积在衬底(212)上,其中MEMS器件(50,250)被固定在阻挡涂层(216)的表面下方。 多个沟槽(142)可以在阻挡涂层(216)的表面下方的相应不同深度处形成在阻挡涂层(216)中,以及沉积在多个沟槽(142)的每一个内的MEMS装置(50,250) )。 提供了一种监视系统(30),其可包括被编程用于从MEMS装置(50,250)接收数据的处理模块(34)。

    Method of instrumenting a component
    119.
    发明授权
    Method of instrumenting a component 有权
    测量组件的方法

    公开(公告)号:US07572524B2

    公开(公告)日:2009-08-11

    申请号:US11215603

    申请日:2005-08-30

    Abstract: A method of instrumenting a first component (210) for use in a combustion turbine engine (10) wherein the first component (210) has a surface contacted by a second component during operation of the combustion turbine engine (10). The method may include depositing an insulating layer (260) on the surface of the first component (210) and depositing a first conductive lead (232, 254) on the insulating layer (260). A piezoelectric material (230) may be deposited in electrical communication with the first conductive lead (232, 254) and a second conductive lead (236, 256) may be deposited in electrical communication with the piezoelectric material (230) and be insulated from the first conductive lead (232, 254) to form a sensor (50) for detecting pressure exerted on the surface of the first component (210) during operation of the combustion turbine engine (10).

    Abstract translation: 一种仪表用于燃气涡轮发动机(10)的第一部件(210)的方法,其中在所述燃气涡轮发动机(10)的操作期间所述第一部件(210)具有由第二部件接触的表面。 该方法可以包括在第一部件(210)的表面上沉积绝缘层(260)并且在绝缘层(260)上沉积第一导电引线(232,254)。 压电材料(230)可以沉积成与第一导电引线(232,254)电连通,并且第二导电引线(236,256)可以沉积成与压电材料(230)电连通并且与 第一导电引线(232,254),以形成用于在所述燃气涡轮发动机(10)的操作期间检测施加在所述第一部件(210)的表面上的压力的传感器(50)。

    Secured and access controlled peer-to-peer resource sharing
    120.
    发明授权
    Secured and access controlled peer-to-peer resource sharing 失效
    安全和访问控制的对等资源共享

    公开(公告)号:US07475139B2

    公开(公告)日:2009-01-06

    申请号:US11534441

    申请日:2006-09-22

    CPC classification number: H04L67/104 H04L63/08 H04L67/1068 H04L69/329

    Abstract: A peer-to-peer network propagates searches from client to client. Resources within each client are selectively searched in response to authentication and authorization processes. Authentication information may be included in a search request or may be performed by an authentication process external to the client. Authorization is performed by a process external to the client. Only after authentication or authorization may resources of any particular client be accessed. The system allows for secure propagated searches and resource access in a peer-to-peer network environment. The network may further include a server for maintaining a list of clients connected to the peer-to-peer network in order to more efficiently facilitate peer-to-peer communications.

    Abstract translation: 对等网络将搜索从客户端传播到客户端。 响应于认证和授权过程选择性地搜索每个客户端内的资源。 认证信息可以被包括在搜索请求中,或者可以通过客户机外部的认证过程来执行。 授权由客户端外部的进程执行。 只有在认证或授权之后,才能访问任何特定客户端的资源。 该系统允许在对等网络环境中进行安全的传播搜索和资源访问。 网络还可以包括用于维护连接到对等网络的客户端列表的服务器,以便更有效地促进对等通信。

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