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    Segmented thermal barrier coating and method of manufacturing the same
    31.
    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

    Applicant: Ramesh Subramanian

    Inventor： Ramesh Subramanian

    IPC: B32B1504

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

    Abstract: 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.

    Abstract translation: 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
    32.
    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

    Applicant: Ramesh Subramanian ,  Mercedes Keyser

    Inventor： Ramesh Subramanian ,  Mercedes Keyser

    IPC: F01D518

    CPC classification number: F01D5/187 ,  C25D1/02

    Abstract: 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.

    Abstract translation: 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。

    Apparatus and method of monitoring operating parameters of a gas turbine
    35.
    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

    Applicant: David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian

    Inventor： David J. Mitchell ,  Anand A. Kulkarni ,  Ramesh Subramanian

    IPC: G08B21/00

    CPC classification number: F01D17/02 ,  B33Y70/00 ,  F01D21/003 ,  F05D2230/30 ,  F05D2230/90 ,  F05D2260/80 ,  G01K1/024 ,  Y02T50/672

    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。

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