PWB warp gauge
    1.
    发明申请
    PWB warp gauge 审中-公开
    PWB经线

    公开(公告)号:US20050241168A1

    公开(公告)日:2005-11-03

    申请号:US10834657

    申请日:2004-04-29

    IPC分类号: G01B5/25 G01B5/28

    CPC分类号: G01B5/285

    摘要: According to one embodiment, the present invention comprises an apparatus having a base structure, a measuring structure, and a linking mechanism coupled to the base structure. The exemplary apparatus also includes an output device configured to determine the position of the measuring structure with respect to the base structure in response to a substrate disposed between the measuring structure and the base structure to indicate a quantity of warpage in the substrate.

    摘要翻译: 根据一个实施例,本发明包括具有底座结构,测量结构和联接到基座结构的连接机构的设备。 示例性装置还包括输出装置,其被配置为响应于设置在测量结构和基部结构之间的衬底来确定测量结构相对于基座结构的位置,以指示衬底中的翘曲量。

    Automatic requirement verification engine and analytics

    公开(公告)号:US10853536B1

    公开(公告)日:2020-12-01

    申请号:US15613183

    申请日:2017-06-03

    IPC分类号: G06F30/20

    摘要: This invention presents a transformative design decision support tool (an e-Design Assessment Engine), one that 1. Significantly reduces cost and risk of engineering design projects, over the state of affair, in part through early and automatic detection of design oversights; 2. Offers compelling reduction in the development time of designs, through improved productivity, but without compromising quality or creativity; 3. Offers wide range of flexibility in terms of supporting design processes employed at different design organizations. The design oversights are identified through proper structuring of the engineering design requirements, extraction of relevant design parameters through application program interfaces provided by the pertinent design tools, and mapping against the requirements. Big data analytics are applied to repositories of past designs, for the purpose of improving new designs. The Engine can be used stand-alone, as a part of a design ecosystem, or integrated into existing systems for product lifecycle or data management.

    Apparatus and method of detecting wear in an abradable coating system
    3.
    发明申请
    Apparatus and method of detecting wear in an abradable coating system 有权
    在可磨损涂层系统中检测磨损的装置和方法

    公开(公告)号:US20060056960A1

    公开(公告)日:2006-03-16

    申请号:US11269044

    申请日:2005-11-08

    IPC分类号: F04D29/00

    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。

    Methodologies for non-destructive quantification of thermal barrier coating temperatures on service run parts

    公开(公告)号:US20070076845A1

    公开(公告)日:2007-04-05

    申请号:US11243370

    申请日:2005-10-04

    IPC分类号: G01B15/06 G01N23/02

    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.

    Ceramic wash-coat for catalyst support
    5.
    发明申请
    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:US20070161507A1

    公开(公告)日:2007-07-12

    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 - 3重量%La 2 O 3)的固溶体 3)和另外表现出比氧化铝表现出的热膨胀系数低的氧化物。 另外的氧化物可以是二氧化硅(2-30重量%SiO 2),氧化锆硅酸盐(2-30重量%ZrSiO 4+),氧化钕(0-4重量% %),二氧化钛(Al 2 O 3 3→3%%TiO 2)或氧化铝基铝酸镁尖晶石(Al 2 O 3) 2 O 3 -25%(重量)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。

    Apparatus and method of monitoring operating parameters of a gas turbine
    6.
    发明申请
    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:US20060056959A1

    公开(公告)日:2006-03-16

    申请号:US11269043

    申请日:2005-11-08

    IPC分类号: F04D29/00

    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)。

    NON-INVASIVE DEVICE NADI TARANGINI USEFUL FOR QUANTITAVE DETECTION OF ARTERIAL NADI PULSE WAVEFORM
    7.
    发明申请
    NON-INVASIVE DEVICE NADI TARANGINI USEFUL FOR QUANTITAVE DETECTION OF ARTERIAL NADI PULSE WAVEFORM 审中-公开
    非侵入性装置NADI TARANGINI有用于定量检测阿片样NADA脉冲波形

    公开(公告)号:US20100152594A1

    公开(公告)日:2010-06-17

    申请号:US12733153

    申请日:2008-08-07

    IPC分类号: A61B5/0245

    摘要: The present invention discloses the procedure for obtaining complete spectrum of the Nadi pulses, as a time series and capable of detecting the major types and the subtypes of the Nadi pulses. The device of this invention involves three diaphragm elements equipped with strain gauge, three transmitters cum amplifiers, and a digitizer for quantifying analog signal. The system acquires the data with 12-bit accuracy with practically no electronic and/or external interfering noise. The pertaining proofs are given which clearly shows the capability of delivering the accurate spectrums, with repeatability of the pulses from the invented system. ‘Nadi-Nidan’ is a prominent method in Ayurveda (Ayurveda is a Sanskrit word derived from ‘Ayus’ and ‘vid’, meaning life and knowledge respectively. It is a holistic science encompassing mental, physical and spiritual health), which is known to dictate all the salient features of a human body. Nadi-Nidan is a specialty of ‘Vaidyas’ (Ayurvedic physicians) and hence the present system would enable the diagnosis accurately, quantitatively and independent of any human errors.

    摘要翻译: 本发明公开了用于获得Nadi脉冲的完整光谱作为时间序列并且能够检测Nadi脉冲的主要类型和亚型的过程。 本发明的装置包括配有应变计的三个隔膜元件,三个发射器和放大器以及用于量化模拟信号的数字化仪。 系统以12位精度获取数据,几乎没有电子和/或外部干扰噪声。 给出了相关证明,其清楚地显示了传递精确谱的能力,并且具有来自本发明系统的脉冲的可重复性。 “N adi an an an an known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known known 规定人体的所有显着特征。 Nadi-Nidan是“Vaidyas”(阿育吠陀医师)的专长,因此本系统能使诊断准确,定量和独立于任何人为错误。

    System and computer program product for non-destructive quantification of thermal barrier coating temperatures on service run parts
    8.
    发明申请
    System and computer program product for non-destructive quantification of thermal barrier coating temperatures on service run parts 有权
    系统和计算机程序产品,可在服务运行部件上对热障涂层温度进行非破坏性定量

    公开(公告)号:US20070078609A1

    公开(公告)日:2007-04-05

    申请号:US11242664

    申请日:2005-10-04

    IPC分类号: G06F19/00

    摘要: System and computer program product 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: 系统和计算机程序产品,用于对部件中的热障涂层(TBC)进行非破坏性检查和表征微结构特征,其中微结构特征限定了TBC中的孔隙和裂纹(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。

    Catalytic thermal barrier coatings
    9.
    发明申请
    Catalytic thermal barrier coatings 有权
    催化热障涂层

    公开(公告)号:US20060245984A1

    公开(公告)日:2006-11-02

    申请号:US11244739

    申请日:2005-10-06

    IPC分类号: B01D50/00

    CPC分类号: F23C13/08 F23C13/00 F23R3/40

    摘要: A catalyst element (30) for high temperature applications such as a gas turbine engine. The catalyst element includes a metal substrate such as a tube (32) having a layer of ceramic thermal barrier coating material (34) disposed on the substrate for thermally insulating the metal substrate from a high temperature fuel/air mixture. The ceramic thermal barrier coating material is formed of a crystal structure populated with base elements but with selected sites of the crystal structure being populated by substitute ions selected to allow the ceramic thermal barrier coating material to catalytically react the fuel-air mixture at a higher rate than would the base compound without the ionic substitutions. Precious metal crystallites may be disposed within the crystal structure to allow the ceramic thermal barrier coating material to catalytically react the fuel-air mixture at a lower light-off temperature than would the ceramic thermal barrier coating material without the precious metal crystallites.

    摘要翻译: 一种用于高温应用的催化剂元件(30),例如燃气涡轮发动机。 催化剂元件包括金属基底,例如具有设置在基底上的陶瓷热障涂层材料层(34)的管(32),用于将金属基底与高温燃料/空气混合物进行绝热。 陶瓷热障涂层材料由填充有基底元件的晶体结构形成,但是晶体结构的选定位置由选择的替代离子填充以允许陶瓷热障涂层材料以更高的速率催化反应燃料 - 空气混合物 比没有离子取代基础化合物。 贵金属微晶可以设置在晶体结构内,以允许陶瓷热障涂层材料在比没有贵金属微晶的陶瓷热障涂层材料低的关闭温度下催化反应燃料 - 空气混合物。