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。

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

IPC分类号： B44C1/175 ,  B29C65/02 ,  B29C65/56 ,  B29C33/58 ,  B32B37/06 ,  B32B37/10

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。

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

IPC分类号： B32B15/04 ,  C09D1/00 ,  B05D3/12

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。

公开(公告)号：US07250192B2

公开(公告)日：2007-07-31

申请号：US10726361

申请日：2003-12-03

申请人： Andrew Jay Skoog ,  Jane Ann Murphy ,  Bryan Thomas Bojanowski

发明人： Andrew Jay Skoog ,  Jane Ann Murphy ,  Bryan Thomas Bojanowski

IPC分类号： B05D3/02 ,  B05D5/00 ,  B05D3/00 ,  B41M5/00

CPC分类号： F01D5/288 ,  B05D1/00 ,  C23C4/02 ,  C23C4/10 ,  C23C4/18 ,  C23C24/04 ,  C23C28/042 ,  C23C30/00 ,  F05D2230/90 ,  F05D2300/14 ,  F05D2300/611 ,  Y02T50/67 ,  Y02T50/671

摘要： A method of applying a heat-rejection coating directly on a substrate of a metallic component is disclosed. The steps include supplying a metallic component, such as of a gas turbine engine, before applying a reflective-coating mixture onto the component, wherein the reflective-coating mixture comprises a metallic pigment and a reflective-coating-mixture carrier, and wherein the step of applying is accomplished by a method selected from the group consisting of air-assisted spraying, airless spraying, brushing, and decal transfer. The component having the reflective-coating mixture thereon is fired to form a reflective coating on the component.

摘要翻译： 公开了一种将排斥涂层直接施加在金属部件的基底上的方法。 所述步骤包括在将反射涂层混合物施加到所述部件之前提供诸如燃气涡轮发动机的金属部件，其中所述反射涂层混合物包括金属颜料和反射涂层混合物载体，并且其中所述步骤 通过选自空气辅助喷雾，无空气喷涂，刷涂和贴花转移的方法来实现。 对其上具有反射涂层混合物的部件进行烧制以在部件上形成反射涂层。

公开(公告)号：US06720034B2

公开(公告)日：2004-04-13

申请号：US10131518

申请日：2002-04-23

申请人： Andrew Jay Skoog ,  Jane Ann Murphy ,  John Frederick Ackerman ,  Paul Vincent Arszman ,  Bryan Thomas Bojanowski ,  Timothy Ray Lattire

发明人： Andrew Jay Skoog ,  Jane Ann Murphy ,  John Frederick Ackerman ,  Paul Vincent Arszman ,  Bryan Thomas Bojanowski ,  Timothy Ray Lattire

IPC分类号： B05D136

CPC分类号： C23C4/18 ,  C23C4/02 ,  C23C24/04 ,  C23C24/08 ,  C23C28/042 ,  C23C30/00 ,  F05C2201/0418 ,  Y02T50/67

摘要： A heat-rejection coating is applied to a metallic component of a gas turbine engine, preferably made of a nickel-base superalloy. A component surface is preferably pre-treated, as by polishing the component surface, thereafter pre-oxidizing the component surface, and thereafter applying a ceramic barrier coating onto the component surface. A reflective-coating mixture is air sprayed onto the pre-treated component surface. The reflective-coating mixture includes a metallic pigment, such as platinum, gold, palladium, and alloys thereof, and a reflective-coating-mixture carrier. The component with the reflective-coating mixture sprayed thereon is fired.

摘要翻译： 排气涂层被施加到优选由镍基超级合金制成的燃气涡轮发动机的金属部件上。 组分表面优选通过抛光组分表面进行预处理，然后预先氧化组分表面，然后在组件表面上施加陶瓷阻挡涂层。 反射涂层混合物被空气喷涂到预处理的组件表面上。 反射涂层混合物包括金属颜料，例如铂，金，钯及其合金，以及反射涂层混合物载体。 将其上喷射有反射涂层混合物的组分烧制。