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公开(公告)号：US20090219040A1
公开(公告)日：2009-09-03
申请号：US12469988
申请日：2009-05-21
IPC分类号： G01N27/04
CPC分类号： G01N3/56 , F01D17/02 , F01D21/003 , F05D2230/30 , F05D2230/90 , F05D2250/183 , F05D2260/30 , F05D2260/80
摘要： A wear sensor (30, 50, 60) installed on a surface area (24) of a component (20, 21) subject to wear from an opposing surface (74, 75). The sensor has a proximal portion (32A, 52A, 62A) and a distal portion (32C, 52C, 62C) relative to a wear starting position (26). An electrical circuit (40) measures an electrical characteristic such as resistance of the sensor, which changes with progressive reduction of the sensor from the proximal portion to the distal portion during a widening reduction wear of the surface from the starting position. The measuring circuit quantifies the electrical changes to derive a wear depth based on a known geometry of the wear depth per wear width. In this manner, wear depth may be measured with a surface mounted sensor.
摘要翻译： 一种磨损传感器（30,50,60），安装在从相对表面（74,75）磨损的部件（20,21）的表面区域（24）上。 传感器具有相对于磨损开始位置（26）的近端部分（32A，52A，62A）和远端部分（32C，52C，62C）。 电路（40）测量传感器的电阻特性，传感器的电阻在表面从起始位置的加宽减磨磨损期间随传感器从近端部分到远端部分的逐渐减小而变化。 测量电路基于每个磨损宽度的磨损深度的已知几何形状量化电变化以导出磨损深度。 以这种方式，可以用表面安装的传感器来测量磨损深度。
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32.发明授权公开(公告)号：US07618712B2
公开(公告)日：2009-11-17
申请号：US11269044
申请日：2005-11-08
IPC分类号： B32B9/00
CPC分类号： C23C4/18 , B33Y80/00 , C23C24/04 , C23C28/3215 , C23C28/3455 , F01D17/02 , F01D17/08 , F01D21/003 , F01D21/04 , F01D25/24 , F04D27/001 , F04D29/324 , F04D29/526 , F04D29/542 , F05D2230/30 , F05D2230/90 , F05D2260/80 , F23M5/00 , F23M11/00 , F23R3/007 , G01K7/028 , G01K13/02 , G01K17/20 , G01K2205/04 , G01N3/56 , Y10T428/24926
摘要： 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).
摘要翻译： 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。
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33.发明授权公开(公告)号：US07298818B2
公开(公告)日：2007-11-20
申请号：US11243370
申请日：2005-10-04
IPC分类号： G01B15/06
CPC分类号： G01N23/046 , G01N2223/419
摘要： 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.
摘要翻译： 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。
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34.发明申请THERMOCOUPLE AND METHOD OF FORMING A THERMOCOUPLE ON A CONTOURED GAS TURBINE ENGINE COMPONENT 有权热电偶及其在轮式涡轮发动机部件上形成热电偶的方法公开(公告)号：US20120236899A1
公开(公告)日：2012-09-20
申请号：US13417448
申请日：2012-03-12
CPC分类号： G01K1/026 , C23C28/30 , C23C28/3215 , C23C28/3455 , F01D17/085 , F05D2230/13 , F05D2230/31 , G01K7/028 , G01K11/12 , G01K2013/024 , G01K2205/00 , G01K2217/00
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 ）。
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35.发明申请公开(公告)号：US20100047063A1
公开(公告)日：2010-02-25
申请号：US12227567
申请日：2007-01-10
CPC分类号： C23C30/00 , C04B35/462 , C04B2235/3215 , C04B2235/3224 , C04B2235/76 , C23C28/3215 , C23C28/345 , C23C28/3455 , Y02T50/67
摘要： A tungsten bronze structured ceramic material as a thermal barrier coating is described wherein the tungsten bronze structured ceramic coating material has the formula AO—BvOw—CyOz where O stands for Oxygen, A stands for a 2+ or a 1+ cation, B stands for a 2+ or 3+ cation and C stands for a 4+ or a 5+ cation. The thermal barrier coating may be applied for gas turbine components.
摘要翻译： 描述了作为热障涂层的钨青铜结构陶瓷材料，其中钨青铜结构陶瓷涂层材料具有式AO-BvOw-CyOz，其中O代表氧，A代表2+或1+阳离子，B代表 一个2+或3+阳离子，C代表4+或5+阳离子。 热障涂层可用于燃气轮机部件。
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36.发明授权公开(公告)号：US07507484B2
公开(公告)日：2009-03-24
申请号：US11607343
申请日：2006-12-01
IPC分类号： B32B15/04
CPC分类号： C22C19/00 , C22C19/03 , C22C19/07 , C23C4/073 , C23C24/04 , C23C28/321 , C23C28/3215 , C23C28/345 , C23C28/3455 , C23C28/36 , Y02T50/67 , Y10T428/12611 , Y10T428/12618 , Y10T428/12931 , Y10T428/31678
摘要： A thermal barrier coating (TBC) system (450) capable of self-healing has a substrate (420), a metal-based advanced bond coat (435) overlying the substrate and a ceramic top coat (440) overlying the bond coat. The bond coat (435) comprises ceramic oxide precursor materials capable of forming a non-alumina ceramic oxide composition when exposed to a thermally conditioning oxidizing environment. Embodiments of such bond coat (435) comprise rare earth elements in a range of 1-20 weight percent, and Hf in a range of about 5 to 30 weight percent or Zr in a range of about 2 to 20 weight percent. Examples of self-healing TBC systems (400, 402, 404) are provided using such bond coat (435) or its advanced bond coat chemistries in combination with conventional bond coats (433, 437) or conventional bond coat chemistries.
摘要翻译： 能够自愈的隔热涂层（TBC）系统（450）具有衬底（420），覆盖在衬底上的基于金属的高级粘合涂层（435）和覆盖在粘结涂层上的陶瓷顶涂层（440）。 粘合涂层（435）包括当暴露于热调节氧化环境时能够形成非氧化铝陶瓷氧化物组合物的陶瓷氧化物前体材料。 这种粘合涂层（435）的实施方案包括1-20重量％范围内的稀土元素和约5至30重量％的Hf，约2至20重量％的Zr。 使用这种粘合涂层（435）或其先进的粘结涂层化学与常规粘合涂层（433,437）或常规粘合涂层化学组合来提供自愈TBC系统（400,402,404）的实例。
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37.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
CPC分类号： G01K1/026 , C23C28/30 , C23C28/3215 , C23C28/3455 , F01D17/085 , F05D2230/13 , F05D2230/31 , G01K7/028 , G01K11/12 , G01K2013/024 , G01K2205/00 , G01K2217/00
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 ）。
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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
CPC分类号： B01J23/002 , B01J23/10 , B01J23/63 , B01J37/0242 , B01J37/0248 , B01J2523/00 , F23C13/08 , B01J2523/31 , B01J2523/47 , B01J2523/824 , B01J2523/41 , B01J2523/3706 , B01J2523/3725 , B01J2523/22 , B01J2523/48
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。
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39.发明授权Use of a tungsten bronze structured material and turbine component with a thermal barrier coating 失效使用具有热障涂层的钨青铜结构材料和涡轮机部件公开(公告)号：US08420238B2
公开(公告)日：2013-04-16
申请号：US12227567
申请日：2007-01-10
CPC分类号： C23C30/00 , C04B35/462 , C04B2235/3215 , C04B2235/3224 , C04B2235/76 , C23C28/3215 , C23C28/345 , C23C28/3455 , Y02T50/67
摘要： A tungsten bronze structured ceramic material as a thermal barrier coating is described wherein the tungsten bronze structured ceramic coating material has the formula AO—BvOw—CyOz where O stands for Oxygen, A stands for a 2+ or a 1+ cation, B stands for a 2+ or 3+ cation and C stands for a 4+ or a 5+ cation. The thermal barrier coating may be applied for gas turbine components.
摘要翻译： 描述了作为热障涂层的钨青铜结构陶瓷材料，其中钨青铜结构陶瓷涂层材料具有式AO-BvOw-CyOz，其中O代表氧，A代表2+或1+阳离子，B代表 一个2+或3+阳离子，C代表4+或5+阳离子。 热障涂层可用于燃气轮机部件。
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40.发明授权公开(公告)号：US07582359B2
公开(公告)日：2009-09-01
申请号：US11269043
申请日：2005-11-08
IPC分类号： B32B9/00
CPC分类号： F01D17/02 , B33Y80/00 , F01D17/08 , F01D21/003 , F05D2230/30 , F05D2230/90 , F05D2260/80
摘要： 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).
摘要翻译： 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）。
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