Thermal barrier coating resistant to sintering
    71.
    发明授权
    Thermal barrier coating resistant to sintering 有权
    隔热涂层耐烧结

    公开(公告)号:US06203927B1

    公开(公告)日:2001-03-20

    申请号:US09245262

    申请日:1999-02-05

    Abstract: A device (10) having a ceramic thermal barrier coating layer (16) characterized by a microstructure having gaps (18) with a sintering inhibiting material (22) disposed on the columns (20) within the gaps (18). The sintering resistant material (22) is stable over the range of operating temperatures of the device (10) and is not soluble with the underlying ceramic layer (16). For a YSZ ceramic layer (16) the sintering resistant layer (22) may preferably be aluminum oxide or yttrium aluminum oxide, deposited as a continuous layer or as nodules.

    Abstract translation: 一种具有陶瓷热障涂层(16)的装置(10),其特征在于具有间隙(18)的微结构,所述微结构具有布置在所述间隙(18)内的所述柱(20)上的烧结抑制材料(22)。 耐烧结材料(22)在器件(10)的工作温度范围内是稳定的,并且不溶于下面的陶瓷层(16)。 对于YSZ陶瓷层(16),耐烧结层(22)可以优选为氧化铝或氧化钇,作为连续层沉积或作为结核沉积。

    Apparatus and method of monitoring operating parameters of a gas turbine
    73.
    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:US08742944B2

    公开(公告)日:2014-06-03

    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。

    TURBINE COMPONENT INSTRUMENTED TO PROVIDE THERMAL MEASUREMENTS
    80.
    发明申请
    TURBINE COMPONENT INSTRUMENTED TO PROVIDE THERMAL MEASUREMENTS 有权
    仪表组件提供热量测量

    公开(公告)号:US20110222582A1

    公开(公告)日:2011-09-15

    申请号:US13015822

    申请日:2011-01-28

    Abstract: 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.

    Abstract translation: 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。

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