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1.发明申请METHOD FOR MAKING STRAIN TOLERANT CORROSION PROTECTIVE COATING COMPOSITIONS AND COATED ARTICLES 审中-公开制造耐腐蚀保护涂料组合物和涂层制品的方法公开(公告)号：US20110076410A1
公开(公告)日：2011-03-31
申请号：US12570474
申请日：2009-09-30
CPC分类号： C04B26/30 , C04B28/34 , C04B2111/26 , C09D5/084 , C09D5/10 , C09D5/18 , C23C28/321 , C23C28/3215 , C23C28/324 , C23C28/34 , C23C28/341 , C23C28/345 , C23C28/3455 , C23C28/36 , C23C30/00 , F01D25/007 , Y02T50/67 , Y02T50/671 , Y02T50/6765 , C04B14/30 , C04B14/303 , C04B14/304 , C04B14/305 , C04B14/306 , C04B14/307 , C04B20/0096
摘要： Method comprising providing a coating precursor composition including a corrosion resistant particulate component having an average coefficient of thermal expansion (CTE) greater than alumina at 1200° F. (649° C.) dispersed in a binder matrix, wherein an aspect ratio of at least a portion of the corrosion resistant particulate component is greater than about 2:1, and wherein the binder matrix includes at least one member of the group consisting of a silicon-containing material and a phosphate-containing material; providing the coating precursor composition on at least a portion of a metal substrate, and; curing the coating precursor composition to provide a corrosion-resistant coating on at least the portion of the metal substrate.
摘要翻译： 方法包括提供一种涂覆前体组合物，其包含分散在粘合剂基质中的1200°F（649℃）下平均热膨胀系数（CTE）大于氧化铝的耐腐蚀性颗粒组分，其中纵横比至少为 耐腐蚀性颗粒组分的一部分大于约2:1，并且其中所述粘合剂基质包括由含硅材料和含磷酸盐材料组成的组中的至少一个; 在所述金属基材的至少一部分上提供所述涂料前体组合物，和 固化涂料前体组合物以在金属基材的至少一部分上提供耐腐蚀涂层。
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2.发明申请STRAIN TOLERANT CORROSION PROTECTIVE COATING COMPOSITIONS AND COATED ARTICLES 审中-公开耐腐蚀耐腐蚀涂料组合物和涂层制品公开(公告)号：US20110076480A1
公开(公告)日：2011-03-31
申请号：US12570402
申请日：2009-09-30
CPC分类号： C04B26/30 , C04B28/34 , C04B2111/26 , C23C28/321 , C23C28/3215 , C23C28/324 , C23C28/34 , C23C28/341 , C23C28/345 , C23C28/3455 , C23C28/36 , F01D5/288 , Y02T50/67 , Y02T50/671 , Y02T50/673 , Y02T50/6765 , Y10T428/249967 , Y10T428/249969 , Y10T428/31678 , C04B14/30 , C04B14/303 , C04B14/304 , C04B14/305 , C04B14/306 , C04B14/307 , C04B20/0096
摘要： A coated article suitable for use at elevated temperature includes a metal substrate and a coating on the substrate. The coating includes a corrosion resistant particulate component having an average coefficient of thermal expansion (CTE) greater than alumina at 1200° F. (649° C.) dispersed in a binder matrix. An aspect ratio of at least a portion of the corrosion resistant particulate component is greater than about 2:1. The binder matrix includes a silicon-containing material and/or a phosphate-containing material.
摘要翻译： 适合在高温下使用的涂覆制品包括金属基材和基材上的涂层。 该涂层包括耐分散在粘合剂基质中的1200°F（649℃）下平均热膨胀系数（CTE）大于氧化铝的耐腐蚀颗粒组分。 耐腐蚀性颗粒组分的至少一部分的纵横比大于约2:1。 粘合剂基质包括含硅材料和/或含磷酸盐的材料。
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3.发明授权Liquid electrostatic coating composition comprising corrosion resistant metal particulates and method for using same 失效包含耐腐蚀金属微粒的液体静电涂层组合物及其使用方法公开(公告)号：US07601400B2
公开(公告)日：2009-10-13
申请号：US11075799
申请日：2005-03-10
IPC分类号： B05D1/04
CPC分类号： C04B28/34 , C03C1/008 , C03C8/14 , C03C2207/00 , C03C2207/04 , C04B28/24 , C04B2111/00525 , C04B2111/90 , C09D5/084 , C23C4/123 , C23C22/74 , C23C26/02 , C23C28/022 , C23C28/027 , C23C28/321 , C23C28/3215 , C23C28/345 , F01D5/288 , F05D2230/90 , C04B14/34
摘要： A composition comprising a liquid mixture having: a corrosion resistant metal particulate component comprising aluminum-containing metal particulates, wherein the aluminum-containing metal particulates have a phosphate and/or silica-containing insulating layer; a glass-forming binder component; and a liquid carrier component. Also disclosed is a method comprising the following steps: (a) providing an article comprising a metal substrate; (b) imparting to the metal substrate an electrical charge; and (c) electrostatically applying a liquid coating composition to the electrically charged metal substrate, wherein the liquid coating composition comprises a liquid mixture having: a corrosion resistant metal particulate component comprising aluminum-containing metal particulates having a phosphate and/or silica-containing insulating layer; glass-forming binder component; and a liquid carrier component.
摘要翻译： 一种包含液体混合物的组合物，其具有：包含含铝金属微粒的耐腐蚀金属颗粒组分，其中所述含铝金属微粒具有磷酸盐和/或二氧化硅的绝缘层; 玻璃形成粘合剂组分; 和液体载体组分。 还公开了一种包括以下步骤的方法：（a）提供包含金属基底的制品; （b）向金属基板施加电荷; 和（c）将液体涂料组合物静电涂覆到带电的金属基底上，其中该液体涂料组合物包含一种液体混合物，该液体混合物具有：包含含磷金属和/或二氧化硅的绝缘的含铝金属微粒的耐腐蚀金属颗粒组分 层; 玻璃形成粘合剂成分; 和液体载体组分。
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4.发明申请公开(公告)号：US20090098394A1
公开(公告)日：2009-04-16
申请号：US11616048
申请日：2006-12-26
申请人： Andrew Jay Skoog , Bryan Thomas Bojanowski , Brian Thomas Hazel , Jane Ann Murphy , Michael James Weimer , Timothy A. Doyle
发明人： Andrew Jay Skoog , Bryan Thomas Bojanowski , Brian Thomas Hazel , Jane Ann Murphy , Michael James Weimer , Timothy A. Doyle
CPC分类号： C23C26/00 , C23C28/321 , C23C28/3215 , C23C28/324 , C23C28/34 , C23C28/345 , C23C28/3455 , C23C28/36 , F01D5/28 , F01D5/288 , F05D2300/21 , F05D2300/2102 , F05D2300/211 , Y02T50/67 , Y02T50/6765
摘要： A corrosion resistant tape coating for gas turbine engine includes a glassy ceramic matrix wherein the glassy matrix is silica-based, and includes corrosion resistant particles selected from refractory particles and non-refractory MCrAlX particles, and combinations thereof. The corrosion resistant particles are substantially uniformly distributed within the matrix, and provide the coating with corrosion resistance. Importantly the coating of the present invention has a coefficient of thermal expansion (CTE) greater than that of alumina at engine operating temperatures. The CTE of the coating is sufficiently close to the substrate material such that the coating does not spall after frequent engine cycling at temperatures above 1200° F.
摘要翻译： 用于燃气涡轮发动机的耐腐蚀胶带涂层包括玻璃质陶瓷基体，其中玻璃质基质是基于二氧化硅的，并且包括选自耐火颗粒和非难熔MCrAlX颗粒的耐腐蚀颗粒及其组合。 耐腐蚀颗粒基本上均匀分布在基质内，并为涂层提供耐腐蚀性。 重要的是，本发明的涂层在发动机工作温度下的热膨胀系数（CTE）大于氧化铝的热膨胀系数。 涂层的CTE足够接近基底材料，使得涂层在高于1200°F的温度下经常发动机循环后不会分散。
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公开(公告)号：US07588797B2
公开(公告)日：2009-09-15
申请号：US10819856
申请日：2004-04-07
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。
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公开(公告)号：US07473331B2
公开(公告)日：2009-01-06
申请号：US10681676
申请日：2003-10-08
申请人： Daniel Peter Ivkovich, Jr. , Andrew Jay Skoog , Jane Ann Murphy , Thomas Walter Rentz , William Randolph Stowell , Bryan Thomas Bojanowski
发明人： Daniel Peter Ivkovich, Jr. , Andrew Jay Skoog , Jane Ann Murphy , Thomas Walter Rentz , William Randolph Stowell , Bryan Thomas Bojanowski
IPC分类号： B44C1/175 , B29C65/02 , B29C65/56 , B29C33/58 , B32B37/06 , B32B37/10 , B29C65/48 , B29C33/72 , B29C33/74 , B32B37/22
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。
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公开(公告)号：US20120148834A1
公开(公告)日：2012-06-14
申请号：US13402565
申请日：2012-02-22
申请人： Andrew Jay Skoog , Jane Ann Murphy
发明人： Andrew Jay Skoog , Jane Ann Murphy
CPC分类号： C23C24/00 , B05B5/043 , C23C4/12 , C23C4/18 , Y02T50/67 , Y02T50/6765 , Y10T428/26 , Y10T428/263 , Y10T428/264 , Y10T428/265
摘要： A thermal coating includes a substrate, a first coating layer, and a second coating layer. The substrate is selected from the group consisting of superalloys and ceramic matrix composites. The first coating layer comprises an alumina powder, a silica binder, and at least one additive selected from either a first group or a second group. The second coating layer comprises at least one of zinc titanate or cerium oxide. A method for applying a thermal coating system includes spraying a bond coat mixture onto a substrate using a liquid electrostatic sprayer. The bond coat mixture comprises an alumina powder, a silica binder, and at least one additive selected from either a first group or a second group. The method further includes applying a top coat mixture onto the bond coat mixture, wherein the top coat mixture comprises at least one of zinc titanate or cerium oxide.
摘要翻译： 热涂层包括基底，第一涂层和第二涂层。 基材选自超级合金和陶瓷基复合材料。 第一涂层包含氧化铝粉末，二氧化硅粘合剂和至少一种选自第一组或第二组的添加剂。 第二涂层包含钛酸锌或氧化铈中的至少一种。 施加热涂覆系统的方法包括使用液体静电喷涂器将粘合涂层混合物喷涂到基底上。 粘合涂层混合物包含氧化铝粉末，二氧化硅粘合剂和至少一种选自第一组或第二组的添加剂。 该方法还包括将面漆混合物施加到粘合涂层混合物上，其中顶涂层混合物包含钛酸锌或氧化铈中的至少一种。
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8.发明申请METHOD OF REPAIRING A THERMAL BARRIER COATING AND REPAIRED COATING FORMED THEREBY 审中-公开修复热障涂层和修复涂层的方法公开(公告)号：US20110059321A1
公开(公告)日：2011-03-10
申请号：US12144109
申请日：2008-06-23
申请人： Andrew Jay Skoog , Jane Ann Murphy
发明人： Andrew Jay Skoog , Jane Ann Murphy
CPC分类号： C23C24/08 , C04B35/18 , C04B35/6263 , C04B35/6316 , C04B2235/3206 , C04B2235/3208 , C04B2235/3232 , C04B2235/3418 , F01D5/288 , F05D2230/80 , F05D2300/2112 , Y02T50/67 , Y02T50/671 , Y02T50/673 , Y02T50/6765
摘要： A coating composition and repair method suitable for repairing thermal barrier coatings (TBCs), and particularly TBCs based on alumina-silica compositions. The method includes preparing a coating composition containing solid ceramic particles, hollow ceramic particles, and a silica precursor binder, applying the coating composition on a surface area of a component exposed by an opening, for example, spallation of the TBC, and then reacting the binder to yield a repair coating that covers the surface area of the component. The resulting repair coating contains the solid ceramic particles and the hollow ceramic particles in a silica matrix formed by thermally decomposing the binder.
摘要翻译： 适用于修复热障涂层（TBC）的涂料组合物和修复方法，特别是基于氧化铝 - 二氧化硅组合物的TBC。 该方法包括制备含有固体陶瓷颗粒，中空陶瓷颗粒和二氧化硅前体粘合剂的涂料组合物，将涂料组合物涂布在通过开口暴露的组分的表面区域上，例如TBC的剥离，然后使 粘合剂以产生覆盖部件的表面积的修复涂层。 所得到的修补涂层含有固体陶瓷颗粒和通过热分解粘合剂形成的二氧化硅基质中的中空陶瓷颗粒。
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公开(公告)号：US07754043B2
公开(公告)日：2010-07-13
申请号：US11623547
申请日：2007-01-16
申请人： Daniel Peter Ivkovich, Jr. , Andrew Jay Skoog , Jane Ann Murphy , Thomas Walter Rentz , William Randolph Stowell , Bryan Thomas Bojanowski
发明人： Daniel Peter Ivkovich, Jr. , Andrew Jay Skoog , Jane Ann Murphy , Thomas Walter Rentz , William Randolph Stowell , Bryan Thomas Bojanowski
CPC分类号： G02B1/10 , C23C4/185 , C23C14/0005 , C23C26/00 , Y02T50/67 , Y10T156/1111
摘要： An optical coating is applied to an article surface of an article by providing a deposition substrate other than the article surface, wherein the deposition substrate is made of a removable material. The optical coating is thereafter deposited onto the deposition substrate. The optical coating is thereafter transferred to the article surface using a transfer support, which may be the deposition substrate or may be a different piece. The method includes thereafter affixing the optical coating to the article surface, and thereafter removing the transfer support.
摘要翻译： 通过提供除制品表面之外的沉积基板将光学涂层施加到制品的物品表面，其中沉积基板由可移除材料制成。 然后将光学涂层沉积到沉积基板上。 然后使用可以是沉积衬底的转移支撑体将光学涂层转移到制品表面，或者可以是不同的片。 该方法包括随后将光学涂层固定在制品表面上，然后除去转印支撑体。
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公开(公告)号：US20110044821A1
公开(公告)日：2011-02-24
申请号：US11654182
申请日：2007-01-17
申请人： Raymond Grant Rowe , Tara Easter McGovern , Jane Ann Murphy , Andrew Jay Skoog , William R. Stowell , Paul Thomas Marks , Lisa DeBellis , James H. Clare
发明人： Raymond Grant Rowe , Tara Easter McGovern , Jane Ann Murphy , Andrew Jay Skoog , William R. Stowell , Paul Thomas Marks , Lisa DeBellis , James H. Clare
CPC分类号： C23C4/02 , F01D5/288 , F05D2230/90 , Y02T50/673
摘要： A method of fabricating a component for a gas turbine engine is provided. The method includes applying a bond coat to at least a portion of the component, applying a dense vertically cracked (DVC) thermal barrier coating to at least a portion of the bond coat using a spray mechanism positioned a first distance from the component, and overlying at least a portion of the DVC thermal barrier coating with a soft coat thermal barrier coating using a spray mechanism that is positioned a second distance away from the component, wherein the second distance is greater than the first distance to facilitate adherence of the soft coating thermal barrier coating to the DVC thermal barrier coating.
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