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11 条记录 (耗时 0.029 秒)

    Method for forming ceramic layer
    1.
    发明申请
    Method for forming ceramic layer 有权
    陶瓷层形成方法

    公开(公告)号：US20060243368A1

    公开(公告)日：2006-11-02

    申请号：US11116291

    申请日：2005-04-28

    申请人： William Stowell ,  Terry Kent ,  Thomas Rentz ,  Jane Murphy ,  Daniel Ivkovich ,  Andrew Skoog

    发明人： William Stowell ,  Terry Kent ,  Thomas Rentz ,  Jane Murphy ,  Daniel Ivkovich ,  Andrew Skoog

    IPC分类号： C03B29/00 ,  B32B37/06

    CPC分类号： F01D5/288

    摘要： A method for forming a ceramic layer on the surface of a turbine component. This method comprises the following steps: (a) providing a turbine component having a surface; (b) providing at least one ceramic tape overlaying the component surface; and (c) manually pressing the at least one ceramic tape against the component surface at a temperature of from about 150° to about 700° F. (from about 66° to about 371° C.) so as to cause the at least one ceramic tape to adhere to the component surface.

    摘要翻译： 一种用于在涡轮机部件的表面上形成陶瓷层的方法。 该方法包括以下步骤：（a）提供具有表面的涡轮机部件; （b）提供覆盖所述部件表面的至少一个陶瓷带; 和（c）在约150°至约700°F（约66°至约371℃）的温度下手动地将至少一种陶瓷带压靠在部件表面上，以使至少一个 陶瓷胶带粘附在组件表面。

    Method of applying an optical coating to an article surface
    5.
    发明申请
    Method of applying an optical coating to an article surface 失效
    将光学涂层施加到制品表面的方法

    公开(公告)号：US20050079284A1

    公开(公告)日：2005-04-14

    申请号：US10681676

    申请日：2003-10-08

    申请人： Daniel Ivkovich ,  Andrew Skoog ,  Jane Murphy ,  Thomas Rentz ,  William Stowell ,  Bryan Bojanowski

    发明人： Daniel Ivkovich ,  Andrew Skoog ,  Jane Murphy ,  Thomas Rentz ,  William Stowell ,  Bryan Bojanowski

    IPC分类号： C23C14/00 ,  C23C26/00 ,  C23C28/00 ,  G02B1/10 ,  B29D11/00

    CPC分类号： G02B1/10 ,  C23C14/0005 ,  C23C26/00 ,  Y02T50/67 ,  Y10T156/1116

    摘要： An optical coating is applied to an article surface of an article by applying a first release system to a deposition substrate, and depositing the optical coating onto the deposition substrate. A second release system and transfer substrate is applied to the second face of the optical coating. The first release system is dissolvable in a first-release-coating solvent that does not dissolve the second release system. The first release system is dissolved in the first-release-coating solvent that does not dissolve the second release system, to separate the optical coating from the deposition substrate. The first face of the optical coating is affixed to the article surface, and the transfer substrate is separated from the optical coating. Any of a variety of affixing techniques may be used.

    摘要翻译： 通过将第一释放系统施加到沉积衬底上并将光学涂层沉积到沉积衬底上，将光学涂层施加到制品的制品表面。 将第二释放系统和转印衬底施加到光学涂层的第二面。 第一释放系统可溶解在不溶解第二释放系统的第一释放 - 涂层溶剂中。 将第一释放系统溶解在不溶解第二释放系统的第一释放 - 涂层溶剂中，以将光学涂层与沉积基材分离。 将光学涂层的第一面固定在物品表面上，并将转印基板与光学涂层分离。 可以使用各种固定技术中的任何一种。

    Field repairable high temperature smooth wear coating
    8.
    发明申请
    Field repairable high temperature smooth wear coating 有权
    现场可修高温平滑磨损涂层

    公开(公告)号：US20050228098A1

    公开(公告)日：2005-10-13

    申请号：US10819856

    申请日：2004-04-07

    申请人： Andrew Skoog ,  Jane Murphy ,  William Stowell ,  David Caldwell

    发明人： Andrew Skoog ,  Jane Murphy ,  William Stowell ,  David Caldwell

    IPC分类号： B05D7/14 ,  C23C24/08 ,  C23C26/00 ,  C08K3/18

    CPC分类号： C23C28/3215 ,  C23C24/08 ,  C23C28/321 ,  C23C28/325 ,  C23C28/345 ,  C23C28/3455 ,  C23C28/347 ,  Y02T50/67

    摘要： A chemical composition and method for repairing a thermal barrier coating on a component designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The method repairs a thermal barrier coating on a component that has suffered localized damage to the thermal barrier coating. After cleaning the surface area of the component exposed by the localized spallation, a paste-like mixture of a ceramic composition comprising ceramic powders and nano-sized ceramic materials in a binder is applied to the surface area of the component, and is optionally smoothed using mechanical means. The composition is then allowed to dry and cure to form a dried coating having polymeric characteristics. Upon subsequent heating, the dried coating reacts to produce a glassy ceramic repair coating. Due to the thixotropic properties of the coating composition upon application to a component, the repair method can be performed in-situ while the component remains installed in its operating environment.

    摘要翻译： 用于修复设计用于恶劣热环境的部件上的热障涂层的化学组成和方法，例如燃气涡轮发动机的涡轮机，燃烧器和增压器部件。 该方法修复已经对热障涂层局部损坏的部件上的热障涂层。 在清洁通过局部剥离暴露的部件的表面积之后，将包含陶瓷粉末和纳米尺寸陶瓷材料的陶瓷组合物的粘合剂的糊状混合物施加到部件的表面区域，并且可选地使用 机械手段。 然后将组合物干燥并固化以形成具有聚合特性的干燥涂层。 随后加热，干燥的涂层反应生成玻璃状陶瓷修补涂层。 由于涂料组合物在施用于组分时的触变性能，可以在组分保持安装在其操作环境中时原位进行修复方法。

    APPARATUS AND METHOD FOR REDUCING METAL OXIDES ON SUPERALLOY ARTICLES
    9.
    发明申请
    APPARATUS AND METHOD FOR REDUCING METAL OXIDES ON SUPERALLOY ARTICLES 审中-公开
    减少金属氧化物超级文章的装置和方法

    公开(公告)号：US20050035085A1

    公开(公告)日：2005-02-17

    申请号：US10604740

    申请日：2003-08-13

    申请人： William Stowell ,  Daniel Ivkovich ,  Timothy Manning

    发明人： William Stowell ,  Daniel Ivkovich ,  Timothy Manning

    IPC分类号： B08B7/00 ,  C23G5/00 ,  F01D25/00 ,  B08B6/00 ,  C23F1/00

    CPC分类号： B08B7/0035 ,  C23G5/00 ,  F01D25/002 ,  F05D2230/90

    摘要： A method of removing a metal oxide from an alloy surface of an article, such as a superalloy turbine blade for a gas turbine engine, by contacting the alloy surface within the vacuum environment of a vacuum chamber with a reductive plasma for a time sufficient to reduce the metal oxide. Typically, the reductive plasma stream is provided by a plasma torch that electrically charges a stream of hydrogen gas, most typically mixed with a much greater portion of an inert gas such as 95% argon, to generate an active plasma stream of H3+ ions. Typically, a biasing circuit is made between the plasma torch and the alloy article to direct the plasma stream to the alloy surface.

    摘要翻译： 通过使真空室的真空环境中的合金表面与还原性等离子体接触足够的时间，从制品的合金表面除去金属氧化物的方法，例如用于燃气涡轮发动机的超级合金涡轮机叶片 金属氧化物。 通常，还原等离子体流由等离子体焰炬提供，该等离子体焰炬对最近通常与惰性气体（例如95％氩）的大部分混合的氢气流进行充电，以产生H3 +的活性等离子体流 离子。 通常，在等离子体焰炬和合金制品之间形成偏压电路以将等离子体流引导到合金表面。

    Low cost antenna array fabrication technology
    10.
    发明申请
    Low cost antenna array fabrication technology 有权
    低成本天线阵列制造技术

    公开(公告)号：US20070102398A1

    公开(公告)日：2007-05-10

    申请号：US11272166

    申请日：2005-11-10

    申请人： William Stowell ,  Michael Steele ,  Thomas Rentz

    发明人： William Stowell ,  Michael Steele ,  Thomas Rentz

    IPC分类号： C03C25/68

    CPC分类号： H01Q21/0087 ,  H01Q1/28 ,  H05K3/061 ,  H05K2203/0531 ,  H05K2203/0537 ,  Y10S428/914 ,  Y10T428/24802

    摘要： Methods are provided for producing large volumes of small antenna arrays. In one embodiment, the method comprises the steps of creating an antenna array pattern as a computer file, printing the created pattern onto the surface of a suitable transfer paper, placing the printed image surface in contact with the surface of a material to be etched, and transferring the printed image to the surface of the material to be etched. The transfer can be effected by any combination of chemicals, heat, and/or pressure. After transfer of the printed image, the transfer paper is removed. The step of removing the transfer paper optionally includes wetting the transfer paper in a manner that dissolves the transfer paper leaving the printed antenna pattern on the surface of the material to be etched. The method further includes the step of etching the non-printed portions of the material, preferably by chemical etching, and removing the printed pattern from the surface of the material to yield an antenna array comprising a non-etched portion of the substrate surface. Arrays, and substrates having an etch-resistant mask for making the arrays, are also provided.

    摘要翻译： 提供了用于生产大量小型天线阵列的方法。 在一个实施例中，该方法包括以下步骤：产生作为计算机文件的天线阵列图案，将所创建的图案印刷到合适的转印纸的表面上，将打印的图像表面与被蚀刻材料的表面接触， 并将印刷图像转印到待蚀刻材料的表面上。 转移可以通过化学品，热和/或压力的任何组合来实现。 转印出的图像后，转印纸被取出。 去除转印纸的步骤可选地包括以使溶解离开印刷天线图案的转印纸在待蚀刻材料的表面上的方式润湿转印纸。 该方法还包括优选通过化学蚀刻来蚀刻材料的非印刷部分，以及从材料表面去除印刷图案以产生包括衬底表面的非蚀刻部分的天线阵列的步骤。 还提供了具有用于制造阵列的耐蚀刻掩模的阵列和衬底。