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    • 51. 发明授权
    • Apparatus and method of detecting wear in an abradable coating system
    • 在可磨损涂层系统中检测磨损的装置和方法
    • US07618712B2
    • 2009-11-17
    • US11269044
    • 2005-11-08
    • Stephen M. SabolRamesh SubramanianAnand A. Kulkarni
    • Stephen M. SabolRamesh SubramanianAnand A. Kulkarni
    • B32B9/00
    • C23C4/18B33Y80/00C23C24/04C23C28/3215C23C28/3455F01D17/02F01D17/08F01D21/003F01D21/04F01D25/24F04D27/001F04D29/324F04D29/526F04D29/542F05D2230/30F05D2230/90F05D2260/80F23M5/00F23M11/00F23R3/007G01K7/028G01K13/02G01K17/20G01K2205/04G01N3/56Y10T428/24926
    • 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).
    • 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。
    • 58. 发明授权
    • Methodologies for non-destructive quantification of thermal barrier coating temperatures on service run parts
    • 无缝量化服务运行部件上热障涂层温度的方法
    • US07298818B2
    • 2007-11-20
    • US11243370
    • 2005-10-04
    • Ramesh SubramanianAnand A. Kulkarni
    • Ramesh SubramanianAnand A. Kulkarni
    • G01B15/06
    • G01N23/046G01N2223/419
    • Methodologies for non-destructively inspecting and characterizing micro-structural features in a thermal barrier coating (TBC) on a component, wherein the micro-structural features define pores and cracks, if any, in the TBC. The micro-structural features having characteristics at least in part based on a type of process used for developing the TBC and affected by operational thermal loads to which a TBC is exposed. In one embodiment, the method allows detecting micro-structural features in a TBC, wherein the detecting of the micro-structural features is based on energy transmitted through the TBC, such as may be performed with a micro-feature detection system 20. The transmitted energy is processed to generate data representative of the micro-structural features, such as may be generated by a controller 26. The data representative of the micro-structural features is processed (e.g., by a processor 30) to determine at least one of the following: volumetric porosity information for the TBC and variation in the characteristics of the micro-structural features over a thickness of the TBC. Based on the results of the data processing, information is generated regarding at least one of the following: a present condition of the thermal barrier coating and a future likely condition of the thermal barrier coating. In another embodiment, one can estimate a level of thermal load to which the thermal barrier coating has been exposed.
    • 用于非破坏性地检查和表征部件上的热障涂层(TBC)中的微结构特征的方法,其中微结构特征限定了TBC中的孔和裂纹(如果有的话)。 所述微结构特征至少部分地基于用于显影TBC并受TBC暴露于的​​操作热负荷影响的过程的类型的特征。 在一个实施例中,该方法允许检测TBC中的微结构特征,其中微结构特征的检测基于通过TBC传输的能量,诸如可以用微特征检测系统20执行。 处理发送的能量以产生表示微结构特征的数据,诸如可由控制器26产生。 代表微结构特征的数据被处理(例如,由处理器30),以确定以下中的至少一个:TBC的体积孔隙度信息和微结构特征在特征厚度方面的变化 TBC。 基于数据处理的结果,产生关于以下中的至少一个的信息:热障涂层的现状和热障涂层的将来可能的状态。 在另一个实施例中,可以估计已经暴露了热障涂层的热负荷水平。