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    Assembly for preventing fluid flow
    1.
    发明授权
    Assembly for preventing fluid flow 有权
    防止流体流动的装置

    公开(公告)号：US08678754B2

    公开(公告)日：2014-03-25

    申请号：US13012380

    申请日：2011-01-24

    Applicant: Victor John Morgan ,  Rebecca Evelyn Hefner ,  Stephen Gerard Pope

    Inventor： Victor John Morgan ,  Rebecca Evelyn Hefner ,  Stephen Gerard Pope

    IPC: F01D11/00

    CPC classification number: F01D11/005 ,  C04B14/20 ,  F01D11/003 ,  F05C2203/00

    Abstract: According to one aspect of the invention, an assembly for preventing fluid flow between turbine components includes a shim and a first woven wire mesh layer that includes a first surface coupled to a first side of the shim and a second surface of the woven wire mesh layer opposite the first surface. The assembly also includes a first outer layer coupled to the second surface of the woven wire mesh layer, where the first outer layer includes a high temperature non-metallic material.

    Abstract translation: 根据本发明的一个方面，一种用于防止涡轮机部件之间的流体流动的组件包括垫片和第一编织丝网层，该第一编织丝网层包括联接到垫片的第一侧的第一表面和编织丝网层的第二表面 与第一个表面相对。 组件还包括耦合到编织金属丝网层的第二表面的第一外层，其中第一外层包括高温非金属材料。

    FUEL NOZZLE
    5.
    发明申请
    FUEL NOZZLE 审中-公开
    燃油喷嘴

    公开(公告)号：US20130284825A1

    公开(公告)日：2013-10-31

    申请号：US13459483

    申请日：2012-04-30

    Applicant: Christopher Michael Prue ,  Thomas Edward Johnson ,  Stephen Gerard Pope

    Inventor： Christopher Michael Prue ,  Thomas Edward Johnson ,  Stephen Gerard Pope

    IPC: F02M63/00

    CPC classification number: F23D11/383 ,  F23D11/406 ,  F23R3/28 ,  F23R3/286

    Abstract: A fuel nozzle includes a center body and a shroud circumferentially surrounding at least a portion of the center body to define an annular passage between the center body and the shroud. A plurality of vanes extend radially between the center body and the shroud in the annular passage. A first ceramic extension extends downstream from the shroud to define at least a portion of the annular passage downstream from the shroud.

    Abstract translation: 燃料喷嘴包括中心体和围绕中心体的至少一部分的护罩，以在中心体和护罩之间限定环形通道。 多个叶片在环形通道中在中心体和护罩之间径向延伸。 第一陶瓷延伸部从护罩的下游延伸以限定环形通道在护罩下游的至少一部分。

    RADIATION MITIGATED ARTICLES AND METHODS OF MAKING THE SAME
    6.
    发明申请
    RADIATION MITIGATED ARTICLES AND METHODS OF MAKING THE SAME 审中-公开
    辐射减缓文章及其制作方法

    公开(公告)号：US20130177772A1

    公开(公告)日：2013-07-11

    申请号：US13344211

    申请日：2012-01-05

    Applicant: Jon Conrad Schaeffer ,  Stephen Gerard Pope

    Inventor： Jon Conrad Schaeffer ,  Stephen Gerard Pope

    IPC: B32B17/06 ,  E04B1/74 ,  B32B9/00 ,  B05D1/36 ,  B32B18/00 ,  B32B15/04

    CPC classification number: C23C28/3455 ,  C23C28/322 ,  C23C28/3225 ,  C23C28/324 ,  C23C28/34 ,  C23C28/341 ,  C23C28/345 ,  Y10T428/31678

    Abstract: Articles comprising a substrate; a thermal barrier coating disposed on the substrate, the thermal barrier coating comprising a radioactive element, the radioactive element having a base radiation emission; and a radiation inhibitor disposed in or on the thermal barrier coating, or a combination thereof, the thermal barrier coating and radiation inhibitor having a mitigated radiation emission, wherein the mitigated radiation emission is lower than the base radiation emission and a methods of making the same.

    Abstract translation: 包含基材的制品; 设置在所述基板上的热障涂层，所述热障涂层包括放射性元素，所述放射性元件具有基底辐射发射; 以及设置在所述热障涂层中或其上的辐射抑制剂或其组合，所述热障涂层和辐射抑制剂具有减轻的辐射发射，其中所述减轻的辐射发射低于所述基本辐射发射，并且所述辐射抑制剂的制备方法 。

    ASSEMBLY FOR PREVENTING FLUID FLOW
    7.
    发明申请
    ASSEMBLY FOR PREVENTING FLUID FLOW 有权
    用于防止流体流动的装置

    公开(公告)号：US20120189435A1

    公开(公告)日：2012-07-26

    申请号：US13012380

    申请日：2011-01-24

    Applicant: Victor John Morgan ,  Rebecca Evelyn Hefner ,  Stephen Gerard Pope

    Inventor： Victor John Morgan ,  Rebecca Evelyn Hefner ,  Stephen Gerard Pope

    IPC: F01D11/00

    CPC classification number: F01D11/005 ,  C04B14/20 ,  F01D11/003 ,  F05C2203/00

    Abstract: According to one aspect of the invention, an assembly for preventing fluid flow between turbine components includes a shim and a first woven wire mesh layer that includes a first surface coupled to a first side of the shim and a second surface of the woven wire mesh layer opposite the first surface. The assembly also includes a first outer layer coupled to the second surface of the woven wire mesh layer, where the first outer layer includes a high temperature non-metallic material.

    Abstract translation: 根据本发明的一个方面，一种用于防止涡轮机部件之间的流体流动的组件包括垫片和第一编织丝网层，该第一编织丝网层包括联接到垫片的第一侧的第一表面和编织丝网层的第二表面 与第一个表面相对。 组件还包括耦合到编织金属丝网层的第二表面的第一外层，其中第一外层包括高温非金属材料。

    Methods for controlling plasma spray coating porosity on an article and articles manufactured therefrom
    8.
    发明授权
    Methods for controlling plasma spray coating porosity on an article and articles manufactured therefrom 有权
    用于控制由其制造的制品和制品上的等离子体喷涂孔隙率的方法

    公开(公告)号：US07722916B2

    公开(公告)日：2010-05-25

    申请号：US11420867

    申请日：2006-05-30

    Applicant: Hsin-Pang Wang ,  Michael Charles Ostrowski ,  Eric Moran ,  Stephen Gerard Pope ,  John Drake Vanselow ,  Edward Richard Haupt

    Inventor： Hsin-Pang Wang ,  Michael Charles Ostrowski ,  Eric Moran ,  Stephen Gerard Pope ,  John Drake Vanselow ,  Edward Richard Haupt

    IPC: C23C16/52

    CPC classification number: B05B12/00 ,  C23C4/12

    Abstract: Disclosed herein is a spray coating process for a robotic spray gun assembly comprising importing a discretized model of an object geometry to be coated; importing a numerically characterized spray pattern file; importing a robot motion file comprising a plurality of motion positions, dwell times and orientations defining a spray direction of the robotic spray gun; reading each motion position within the motion file; determining which portions of the object geometry are visible at each motion position; computing a void volume fraction at each visible portion of the object geometry based on the core compression, the incident angle of the robotic spray gun and the ricocheting of the spray for each motion position; and calculating total coating thickness on portions of the object geometry for the complete motion step.

    Abstract translation: 本文公开了一种用于机器人喷枪组件的喷涂方法，包括导入待涂覆的物体几何体的离散模型; 导入数字表征的喷雾图案文件; 导入包括限定所述机器人喷枪的喷射方向的多个运动位置，停留时间和方向的机器人运动文件; 读取运动文件内的每个运动位置; 确定对象几何的哪些部分在每个运动位置可见; 基于核心压缩，机器人喷枪的入射角度和每个运动位置的喷射喷射计算物体几何体的每个可见部分处的空隙体积分数; 以及在整个运动步骤的对象几何部分上计算总涂层厚度。

    METHOD FOR DETECTING AND REMOVING NITRIDE LAYER FORMED ON THE SURFACE OF A STEEL ALLOY
    9.
    发明申请
    METHOD FOR DETECTING AND REMOVING NITRIDE LAYER FORMED ON THE SURFACE OF A STEEL ALLOY 审中-公开
    检测和去除钢铁合金表面形成的氮化物层的方法

    公开(公告)号：US20100170079A1

    公开(公告)日：2010-07-08

    申请号：US12350476

    申请日：2009-01-08

    Applicant: Warren Tan KING ,  Stephen Gerard Pope ,  Susan Drake

    Inventor： Warren Tan KING ,  Stephen Gerard Pope ,  Susan Drake

    IPC: B23P17/00

    CPC classification number: G01N27/825 ,  G01B7/105 ,  Y10T29/4998

    Abstract: A method of treating a component made of a non magnetic alloy on which a magnetic surface layer has formed includes: (a) engaging a magnet of a calibrated magnet gauge with a surface of the component; (b) disengaging the magnet from the surface of the component and measuring a force required to disengage the magnet; (c) correlating the force with a thickness of the magnetic surface layer; and (d) if the thickness of the surface layer is greater than a predetermined minimum thickness, removing the surface layer.

    Abstract translation: 一种处理其上形成有磁性表面层的非磁性合金构成的部件的方法包括：（a）将校准的磁力计的磁体与部件的表面接合; （b）将磁体从部件的表面分离并测量使磁体脱离所需的力; （c）使力与磁性表面层的厚度相关; 和（d）如果表面层的厚度大于预定的最小厚度，则去除表面层。

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