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159 条记录 (耗时 0.047 秒)

    Method of instrumenting a component
    63.
    发明申请
    Method of instrumenting a component 有权
    测量组件的方法

    公开(公告)号：US20050287386A1

    公开(公告)日：2005-12-29

    申请号：US11215603

    申请日：2005-08-30

    申请人： Stephen Sabol ,  Ramesh Subramanian

    发明人： Stephen Sabol ,  Ramesh Subramanian

    IPC分类号： B32B9/04 ,  F01D17/02 ,  F01D17/08 ,  F01D21/00

    CPC分类号： F01D21/003 ,  B33Y80/00 ,  F01D17/02 ,  F01D17/08 ,  F01D17/085 ,  F05D2230/30 ,  F05D2230/90 ,  F05D2260/80 ,  G01H1/006 ,  G01P15/0915 ,  Y10T428/26 ,  Y10T428/8305

    摘要： A method of instrumenting a first component (210) for use in a combustion turbine engine (10) wherein the first component (210) has a surface contacted by a second component during operation of the combustion turbine engine (10). The method may include depositing an insulating layer (260) on the surface of the first component (210) and depositing a first conductive lead (232, 254) on the insulating layer (260). A piezoelectric material (230) may be deposited in electrical communication with the first conductive lead (232, 254) and a second conductive lead (236, 256) may be deposited in electrical communication with the piezoelectric material (230) and be insulated from the first conductive lead (232, 254) to form a sensor (50) for detecting pressure exerted on the surface of the first component (210) during operation of the combustion turbine engine (10).

    摘要翻译： 一种仪表用于燃气涡轮发动机（10）的第一部件（210）的方法，其中在所述燃气涡轮发动机（10）的操作期间所述第一部件（210）具有由第二部件接触的表面。 该方法可以包括在第一部件（210）的表面上沉积绝缘层（260）并且在绝缘层（260）上沉积第一导电引线（232,254）。 压电材料（230）可以沉积成与第一导电引线（232,254）电连通，并且第二导电引线（236,256）可以沉积成与压电材料（230）电连通并且与 第一导电引线（232,254），以形成用于在所述燃气涡轮发动机（10）的操作期间检测施加在所述第一部件（210）的表面上的压力的传感器（50）。

    Sinter resistant abradable thermal barrier coating
    64.
    发明授权
    Sinter resistant abradable thermal barrier coating 有权
    耐烧蚀耐热耐热涂层

    公开(公告)号：US06946208B2

    公开(公告)日：2005-09-20

    申请号：US10454802

    申请日：2003-06-04

    申请人： Ramesh Subramanian ,  David B. Allen

    发明人： Ramesh Subramanian ,  David B. Allen

    IPC分类号： C23C4/04 ,  C23C4/10 ,  C23C4/18 ,  C23C14/08 ,  C23C28/00 ,  C23C30/00 ,  F01D5/28 ,  F23M5/00 ,  F23R3/00 ,  B32B9/00

    CPC分类号： C23C4/04 ,  C23C4/11 ,  C23C4/18 ,  C23C14/08 ,  C23C28/042 ,  C23C28/3215 ,  C23C28/3455 ,  C23C28/36 ,  C23C30/00 ,  F01D5/288 ,  F23M5/00 ,  F23R3/007 ,  Y10T428/12618 ,  Y10T428/249953

    摘要： An abradable thermal barrier coating material (10) formed of a highly defective fluorite ceramic matrix (16) having a desired degree of porosity (18) created in part by the addition of a fugitive material (19). The ceramic material has a concentration of a stabilizer sufficiently high that the oxygen vacancies created by the stabilizer interact within the matrix to form multi-vacancies, thereby improving the sintering resistance of the material. Such a concentration of stabilizer results in a material that is softer than prior art materials having lower concentrations of stabilizer, and that will be more resistive to sintering than prior art materials. Embodiments include a fluorite matrix of zirconia stabilized by at least 30 wt. % yttria, or stabilized by at least 30 wt. % ytterbia, and with porosity of 10-40%. In one embodiment, a metallic gas turbine seal ring segment is coated with a bond coat layer, then with a layer of porous 8 wt. % YSZ material, and finally with a layer of 33 mole % YbSZ (61.3 wt. % YbSZ) material having porosity of 10-40%.

    摘要翻译： 由耐火材料（19）部分产生的具有所需孔隙率（18）的高度有缺陷的萤石陶瓷基体（16）形成的可磨损热障涂层材料（10）。 陶瓷材料具有足够高的稳定剂浓度，使得由稳定剂产生的氧空位在基质内相互作用以形成多空位，从而提高材料的耐烧结性。 这种稳定剂的浓度导致比现有技术的具有较低浓度稳定剂的材料更柔软的材料，并且比现有技术材料更耐烧结。 实施方案包括通过至少30重量％稳定的氧化锆的萤石基质。 ％氧化钇，或稳定至少30wt。 百日咳，孔隙度为10-40％。 在一个实施例中，金属燃气涡轮机密封环段用粘合涂层涂覆，然后用多孔8wt。 ％YSZ材料，最后使用具有10-40％孔隙率的33摩尔％YbSZ（61.3重量％YbSZ）材料层。

    Segmented thermal barrier coating and method of manufacturing the same
    67.
    发明授权
    Segmented thermal barrier coating and method of manufacturing the same 有权
    分段热障涂层及其制造方法

    公开(公告)号：US06703137B2

    公开(公告)日：2004-03-09

    申请号：US09921206

    申请日：2001-08-02

    申请人： Ramesh Subramanian

    发明人： Ramesh Subramanian

    IPC分类号： B32B1504

    CPC分类号： C23C4/18 ,  C23C28/3215 ,  C23C28/345 ,  C23C28/3455 ,  F01D5/288 ,  F05D2230/13 ,  Y10T428/24314 ,  Y10T428/249953 ,  Y10T428/249967 ,  Y10T428/249981

    摘要： A thermal barrier coating (18) having a less dense bottom layer (20) and a more dense top layer (22) with a plurality of segmentation gaps (28) formed in the top layer to provide thermal strain relief. The top layer may be at least 95% of the theoretical density in order to minimize the densification effect during long term operation, and the bottom layer may be no more than 95% of the theoretical density in order to optimize the thermal insulation and strain tolerance properties of the coating. The gaps are formed by a laser engraving process controlled to limit the size of the surface opening to no more than 50 microns in order to limit the aerodynamic impact of the gaps for combustion turbine applications. The laser engraving process is also controlled to form a generally U-shaped bottom geometry (54) in the gaps in order to minimize the stress concentration effect.

    摘要翻译： 具有较低密度的底层（20）和更致密的顶层（22）的热障涂层（18），其具有形成在顶层中的多个分割间隙（28），以提供热应变消除。 顶层可以是理论密度的至少95％，以便在长期操作期间最小化致密效应，并且底层可以不超过理论密度的95％，以优化绝热和应变耐受性 涂层的性能。 通过激光雕刻过程形成间隙，该激光雕刻工艺被控制以将表面开口的尺寸限制在不超过50微米，以限制燃气轮机应用的间隙的空气动力学冲击。 还控制激光雕刻工艺以在间隙中形成大致U形的底部几何形状（54），以便最小化应力集中效应。

    Cooling structure and method of manufacturing the same
    68.
    发明授权
    Cooling structure and method of manufacturing the same 有权
    冷却结构及其制造方法

    公开(公告)号：US06602053B2

    公开(公告)日：2003-08-05

    申请号：US09921084

    申请日：2001-08-02

    申请人： Ramesh Subramanian ,  Mercedes Keyser

    发明人： Ramesh Subramanian ,  Mercedes Keyser

    IPC分类号： F01D518

    CPC分类号： F01D5/187 ,  C25D1/02

    摘要： A method of forming a cooling feature (28) on a surface (14) of a substrate (12) to protect the substrate from a high temperature environment. The cooling feature is formed by first depositing a layer of a masking material (16) such as epoxy resin on the surface of the substrate. A pattern of voids (18) is then cut into the masking material by a laser engraving process which exposes portions of the substrate surface. A plurality of supports (20) are then formed by electroplating a support material onto the exposed portions of the substrate surface. A layer of material is then electroplated onto the supports and over the masking material to form a skin that interconnects the supports. Finally, the remaining portions of the masking material are removed to form a plurality of cooling channels (26) defined by the supports, skin and substrate surface. An additional layer of material (42) may be deposited onto a top surface (50) of the cooling feature to provide additional thermal and/or mechanical protection.

    摘要翻译： 一种在衬底（12）的表面（14）上形成冷却特征（28）以保护衬底免受高温环境的方法。 冷却特征通过首先在衬底的表面上沉积诸如环氧树脂的掩模材料（16）的层来形成。 然后通过暴露基板表面的一部分的激光雕刻工艺将空隙（18）的图案切割成掩模材料。 然后通过将支撑材料电镀到衬底表面的暴露部分上来形成多个支撑件（20）。 然后将一层材料电镀到载体上并在掩模材料上形成将支撑物互连的皮肤。 最后，去除掩模材料的其余部分以形成由支撑体，皮肤和基底表面限定的多个冷却通道（26）。 可以将另外的材料层（42）沉积到冷却特征的顶表面（50）上以提供额外的热和/或机械保护。