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1. 发明申请

US20050100665A1 Method for applying an optical coating to a surface of an article 审中-公开
标题翻译：将光学涂层施加到制品表面的方法
公开(公告)号：US20050100665A1
公开(公告)日：2005-05-12
申请号：US10702801
申请日：2003-11-06
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： C23C4/18 , C23C14/00 , C23C26/00 , G02B1/10 , B05D5/06
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。

2. 发明申请

US20060243368A1 Method for forming ceramic layer 有权
标题翻译：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。

3. 发明申请

US20050136767A1 Advanced anisotropic ceramic matrix composite system 审中-公开
标题翻译：先进的各向异性陶瓷矩阵复合系统
公开(公告)号：US20050136767A1
公开(公告)日：2005-06-23
申请号：US10738189
申请日：2003-12-17
申请人： Daniel Ivkovich , Andrew Skoog , Jane Murphy , Thomas Rentz
发明人： Daniel Ivkovich , Andrew Skoog , Jane Murphy , Thomas Rentz
IPC分类号： B32B18/00 , B32B27/04 , B32B27/12
CPC分类号： B32B18/00 , B32B2315/02 , C04B2235/3217 , C04B2235/3418 , C04B2235/36 , C04B2235/5436 , C04B2235/5445 , C04B2235/77 , C04B2237/341 , C04B2237/343 , C04B2237/348 , C04B2237/38 , C04B2237/704 , Y10T442/2041 , Y10T442/2123 , Y10T442/2148 , Y10T442/2975 , Y10T442/3472 , Y10T442/3496 , Y10T442/3683
摘要： A ceramic matrix composite system includes multiple stacked layers of ceramic fiber cloth impregnated with resin matrix material. The resin matrix material in each of the fiber cloth layers substantially remains with the same layer during subsequent processing. Ceramic-containing material inner layers are applied between each of the fiber cloth layers enhancing the cross ply strength of the composite system.
摘要翻译：陶瓷基体复合体系包括浸渍有树脂基体材料的陶瓷纤维布的多层堆叠层。在随后的处理过程中，每个纤维布层中的树脂基质材料基本保持相同的层。在每个纤维布层之间施加含陶瓷的材料内层，从而提高复合体系的交叉层强度。

4. 发明申请

US20050079284A1 Method of applying an optical coating to an article surface 失效
标题翻译：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。

5. 发明申请

US20070172585A1 METHOD FOR APPLYING AN OPTICAL COATING TO A SURFACE OF AN ARTICLE 有权
标题翻译：将光学涂层应用于文章表面的方法
公开(公告)号：US20070172585A1
公开(公告)日：2007-07-26
申请号：US11623547
申请日：2007-01-16
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： B41M3/12
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。

6. 发明申请

US20050282020A1 SMOOTH OUTER COATING FOR COMBUSTOR COMPONENTS AND COATING METHOD THEREFOR 有权
标题翻译：用于燃烧器部件的平滑外涂层及其涂覆方法
公开(公告)号：US20050282020A1
公开(公告)日：2005-12-22
申请号：US10710110
申请日：2004-06-18
申请人： William Stowell , Daniel Ivkovich , Timothy Manning , Tara McGovern , Jane Murphy , Thomas Rentz , Mathew Roling , Raymond Rowe , Andrew Skoog
发明人： William Stowell , Daniel Ivkovich , Timothy Manning , Tara McGovern , Jane Murphy , Thomas Rentz , Mathew Roling , Raymond Rowe , Andrew Skoog
IPC分类号： C23C4/10 , C23C4/12 , C23C10/30 , C23C28/00 , C23C30/00 , B32B9/00 , B05D1/12 , B32B15/04 , C23C4/00
CPC分类号： C23C24/08 , C23C28/3215 , C23C28/324 , C23C28/345 , C23C28/3455 , Y02T50/67 , Y10T428/252 , Y10T428/256
摘要： A coating and method for overcoating a TBC on a component used in a high-temperature environment, such as the combustor section of an industrial gas turbine. The coating defines the outermost surface of the component and is formed of at least two layers having different compositions. An inner layer of the coating contains alumina in a first silica-containing matrix material that is free of zinc titanate. An outer layer of the coating contains alumina, a glass material, and zinc titanate in a second silica-containing matrix material. The outer layer of the coating has a surface roughness of not greater than three micrometers Ra and forms the outermost surface of the component. The coating reduces the component temperature by reducing the convective and radiant heat transfer thereto.
摘要翻译：用于在高温环境中使用的部件（例如工业燃气轮机的燃烧器部分）上的TBC外涂层的涂层和方法。该涂层限定了该组件的最外表面，并由至少两层具有不同组成。涂层的内层在不含钛酸锌的第一含硅基体材料中含有氧化铝。涂层的外层在第二含硅基体材料中含有氧化铝，玻璃材料和钛酸锌。涂层的外层具有不大于3微米的Ra的表面粗糙度并形成该组件的最外表面。涂层通过减少其对流和辐射热传递而降低了组件温度。

7. 发明申请

US20070141269A1 SMOOTH OUTER COATING FOR COMBUSTOR COMPONENTS AND COATING METHOD THEREFOR 审中-公开
标题翻译：用于燃烧器部件的平滑外涂层及其涂覆方法
公开(公告)号：US20070141269A1
公开(公告)日：2007-06-21
申请号：US11627582
申请日：2007-01-26
申请人： Wiliam Stowell , Daniel Ivkovich , Timothy Manning , Tara McGovern , Jane Murphy , Thomas Rentz , Mathew Roling , Raymond Rowe , Andrew Skoog
发明人： Wiliam Stowell , Daniel Ivkovich , Timothy Manning , Tara McGovern , Jane Murphy , Thomas Rentz , Mathew Roling , Raymond Rowe , Andrew Skoog
IPC分类号： B05D1/36 , C23C4/08
CPC分类号： C23C24/08 , C23C28/3215 , C23C28/324 , C23C28/345 , C23C28/3455 , Y02T50/67 , Y02T50/6765 , Y10T428/252 , Y10T428/256
摘要： A coating and method for overcoating a TBC on a component used in a high-temperature environment, such as the combustor section of an industrial gas turbine. The coating defines the outermost surface of the component and is formed of at least two layers having different compositions. An inner layer of the coating contains alumina in a first silica-containing matrix material that is free of zinc titanate. An outer layer of the coating contains alumina, a glass material, and zinc titanate in a second silica-containing matrix material. The outer layer of the coating has a surface roughness of not greater than three micrometers Ra and forms the outermost surface of the component. The coating reduces the component temperature by reducing the convective and radiant heat transfer thereto.
摘要翻译：用于在高温环境中使用的部件（例如工业燃气轮机的燃烧器部分）上的TBC外涂层的涂层和方法。该涂层限定了该组件的最外表面，并由至少两层具有不同组成。涂层的内层在不含钛酸锌的第一含硅基体材料中含有氧化铝。涂层的外层在第二含硅基体材料中含有氧化铝，玻璃材料和钛酸锌。涂层的外层具有不大于3微米的Ra的表面粗糙度并形成该组件的最外表面。涂层通过减少其对流和辐射热传递而降低了组件温度。

8. 发明申请

US20050100757A1 Thermal barrier coating having a heat radiation absorbing topcoat 审中-公开
标题翻译：具有散热吸收面漆的隔热涂层
公开(公告)号：US20050100757A1
公开(公告)日：2005-05-12
申请号：US10712821
申请日：2003-11-12
申请人： William Stowell , Bangalore Nagaraj , Andrew Skoog , Jane Murphy , John Ackerman , Daniel Ivkovich
发明人： William Stowell , Bangalore Nagaraj , Andrew Skoog , Jane Murphy , John Ackerman , Daniel Ivkovich
IPC分类号： C23C28/00 , F01D5/28 , B21D39/00
CPC分类号： C23C28/345 , C23C8/42 , C23C8/80 , C23C24/08 , C23C28/321 , C23C28/3215 , C23C28/324 , C23C28/3455 , F01D5/288 , F05D2300/2118 , Y02T50/67 , Y02T50/671 , Y02T50/6765 , Y10T428/12535 , Y10T428/12556 , Y10T428/12611
摘要： Coating systems suitable for protecting components exposed to high-temperature environments, such as the hot gas flow path through a gas turbine engine. A multilayer thermal barrier coating (TBC) system characterized by a low coefficient of thermal conductivity and having a heat-absorbing topcoat comprised of the thermal decomposition product of at least one metallic element and at least one ceramic precursor binder component.
摘要翻译：涂覆系统适用于保护暴露于高温环境的组件，例如通过燃气涡轮发动机的热气流路径。一种多层热障涂层（TBC）系统，其特征在于低导热系数，并具有由至少一种金属元素和至少一种陶瓷前体粘合剂组分的热分解产物组成的吸热顶涂层。

9. 发明申请

US20060088727A1 High reflectivity infrared coating applications for use in HIRSS applications 审中-公开
标题翻译：高反射率红外涂层应用于HIRSS应用
公开(公告)号：US20060088727A1
公开(公告)日：2006-04-27
申请号：US10972553
申请日：2004-10-25
申请人： Andrew Skoog , Jane Murphy , John Jasany , Mariah Senter
发明人： Andrew Skoog , Jane Murphy , John Jasany , Mariah Senter
IPC分类号： B32B15/00 , B32B15/01 , B05D1/02 , B05D1/28 , B05D3/02 , B05D3/00
CPC分类号： F02K1/825 , B32B15/018 , C22C19/055 , C23C24/08 , C23C26/00 , C23C30/00 , F05D2230/90 , F05D2300/611 , Y10T428/12771 , Y10T428/12806 , Y10T428/12861 , Y10T428/12875
摘要： The present invention is a hover infrared suppression system for a gas turbine engine comprising a hover infrared suppression system having an upstream first stage, a second stage downstream of the first stage and a third stage downstream of the second stage, the engine operating at a temperature sufficient to cause the hover infrared suppression system to emit infrared radiation. The present invention further comprises a high reflectivity coating applied over a preselected area of at least one of the stages of the hover infrared suppression system to reduce the infrared radiation emitted from the engine, the high reflectivity coating being fired after application.
摘要翻译：本发明是一种用于燃气涡轮发动机的悬浮式红外线抑制系统，其包括具有上游第一级，第一级下游的第二级和第二级下游的第三级的悬停红外线抑制系统，发动机在温度足以使悬停的红外线抑制系统发射红外辐射。本发明还包括施加在悬浮红外线抑制系统的至少一个级的预选区域上的高反射率涂层，以减少从发动机发射的红外辐射，施加后高反射率涂层被烧制。

10. 发明申请

US20050228098A1 Field repairable high temperature smooth wear coating 有权
标题翻译：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。

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