Thermocouple and method of forming a thermocouple on a contoured gas turbine engine component
    3.
    发明授权
    Thermocouple and method of forming a thermocouple on a contoured gas turbine engine component 有权
    热电偶和在轮廓燃气涡轮发动机部件上形成热电偶的方法

    公开(公告)号:US08961007B2

    公开(公告)日:2015-02-24

    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 )。

    Turbine component instrumented to provide thermal measurements
    4.
    发明授权
    Turbine component instrumented to provide thermal measurements 有权
    汽轮机组件用于提供热测量

    公开(公告)号:US08662746B2

    公开(公告)日:2014-03-04

    申请号:US13015822

    申请日:2011-01-28

    IPC分类号: G01K7/02 G01J5/00

    摘要: A gas turbine component (49) may be instrumented to provide a plurality of signals indicative of thermal measurements in a high temperature combustion environment of the gas turbine. A thermocouple arrangement may include a first thermocouple leg (50) disposed within a thickness of the component. At least two or more thermocouple legs (52, 53, 54) is each electrically connected to the first leg to form individual thermocouple junctions (56, 57, 58, 59) along the first leg for conversion of respective thermal gradients to respective electrical signals, such as electromotive force (emf) based voltages. The thermocouple arrangement may be used in combination with a thermographic system (70) to calculate heat flux over a region of the turbine component.

    摘要翻译: 燃气轮机部件(49)可被装配以提供表示在燃气轮机的高温燃烧环境中的热测量的多个信号。 热电偶布置可以包括设置在部件的厚度内的第一热电偶腿部(50)。 至少两个或更多个热电偶腿(52,53,54)每个电连接到第一腿以沿着第一腿形成单独的热电偶接头(56,57,58,59),用于将相应的热梯度转换成相应的电信号 ,例如基于电动势(emf)的电压。 热电偶装置可以与热成像系统(70)组合使用以计算涡轮机部件的区域上的热通量。

    Bracket assembly for a wireless telemetry component
    5.
    发明授权
    Bracket assembly for a wireless telemetry component 有权
    无线遥测组件的支架组件

    公开(公告)号:US08599082B2

    公开(公告)日:2013-12-03

    申请号:US13018455

    申请日:2011-02-01

    IPC分类号: H01Q1/00

    CPC分类号: F01D17/02 F01D21/003

    摘要: 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.

    摘要翻译: 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。

    Wireless telemetry system for a turbine engine
    6.
    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)。

    ULTRA HIGH TEMPERATURE CIRCUIT COUPLING
    9.
    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%。

    Ceramic wash-coat for catalyst support
    10.
    发明授权
    Ceramic wash-coat for catalyst support 有权
    用于催化剂载体的陶瓷洗涂层

    公开(公告)号:US08242045B2

    公开(公告)日:2012-08-14

    申请号:US11330555

    申请日:2006-01-12

    IPC分类号: B01J23/10

    摘要: A wash-coat (16) for use as a support for an active catalyst species (18) and a catalytic combustor component (10) incorporating such wash-coat. The wash-coat is a solid solution of alumina or alumina-based material (Al2O3-0-3 wt % La2O3) and a further oxide exhibiting a coefficient of thermal expansion that is lower than that exhibited by alumina. The further oxide may be silicon dioxide (2-30 wt % SiO2), zirconia silicate (2-30 wt % ZrSiO4), neodymium oxide (0-4 wt %), titania (Al2O3-3-40% TiO2) or alumina-based magnesium aluminate spinel (Al2O3-25 wt % MgO) in various embodiments. The active catalyst species may be palladium and a second metal in a concentration of 10-50% of the concentration of the palladium.

    摘要翻译: 用作活性催化剂种类(18)和催化燃烧器组分(10)的载体的洗涂层(16),其结合有这种洗衣层。 洗涤涂层是氧化铝或氧化铝基材料(Al 2 O 3 -0-3重量%La 2 O 3)的固溶体和表现出比氧化铝表现出的热膨胀系数更高的氧化物。 另外的氧化物可以是二氧化硅(2-30重量%SiO 2),氧化硅硅酸盐(2-30重量%ZrSiO 4),氧化钕(0-4重量%),二氧化钛(Al 2 O 3 -3-40%TiO 2)或氧化铝 - 铝酸镁尖晶石(Al2O3-25wt%MgO)。 活性催化剂种类可以是钯,浓度为钯浓度的10-50%的第二种金属。