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1. 发明申请

US20060204665A1 Liquid electrostatic coating composition comprising corrosion resistant metal particulates and method for using same 失效
公开(公告)号：US20060204665A1
公开(公告)日：2006-09-14
申请号：US11075799
申请日：2005-03-10
申请人： Matthew Buczek , Andrew Skoog , Jane Murphy , Brian Hazel
发明人： Matthew Buczek , Andrew Skoog , Jane Murphy , Brian Hazel
IPC分类号： B05D1/04 , B05D5/00
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.

2. 发明申请

US20060121295A1 Sintering resistant, low conductivity, high stability thermal barrier coating/environmental barrier coating/environmental barrier coating system for a ceramic-matrix composite (CMC) article to improve high temperature capability 有权
标题翻译：用于陶瓷基复合材料（CMC）制品的耐烧蚀，低导电性，高稳定性的热障涂层/环境屏障涂层/环境屏障涂层系统，以提高高温能力
公开(公告)号：US20060121295A1
公开(公告)日：2006-06-08
申请号：US11006368
申请日：2004-12-06
申请人： Brett Boutwell , Irene Spitsberg , Christine Govern , Bangalore Nagaraj , Brian Hazel
发明人： Brett Boutwell , Irene Spitsberg , Christine Govern , Bangalore Nagaraj , Brian Hazel
IPC分类号： B32B15/04 , B32B9/00
CPC分类号： C04B41/009 , C04B41/52 , C04B41/89 , C23C28/042 , F01D5/288 , F05D2230/90 , F05D2300/2118 , F05D2300/50211 , F05D2300/611 , C04B41/4527 , C04B41/5096 , C04B41/5024 , C04B41/5037 , C04B41/5042 , C04B41/5031 , C04B41/522 , C04B41/4529 , C04B35/565 , C04B35/584 , C04B35/806 , C04B35/597
摘要： In accordance with an embodiment of the invention, a thermal barrier coating (TBC) for inclusion in a thermal barrier coating/environmental barrier coating system (TBC/EBC system) for use on a silicon containing material substrate is provided. The TBC comprises a compound having a primary constituent portion and a stabilizer portion stabilizing said primary constituent. The primary constituent portion of the TBC comprises hafnia present in an amount of at least about 5 mol % of the primary constituent. The stabilizer portion of said thermal barrier coating comprises at least one metal oxide comprised of cations with a +2 or +3 valence present in the amount of about 10 to about 40 mol % of the thermal barrier coating.
摘要翻译：根据本发明的实施例，提供了一种用于包含在用于含硅材料基板上的隔热涂层/环境阻挡涂层系统（TBC / EBC系统）中的热障涂层（TBC）。 TBC包括具有主要构成部分和稳定所述主要成分的稳定剂部分的化合物。 TBC的主要构成部分包括以至少约5mol％的主要成分的量存在的铪。所述热障涂层的稳定剂部分包含至少一种由阳离子组成的金属氧化物，该阳离子以+2或+3价存在，其热阻层为约10至约40mol％。

3. 发明申请

US20060115661A1 Protection of thermal barrier coating by a sacrificial coating 审中-公开
标题翻译：通过牺牲涂层保护热障涂层
公开(公告)号：US20060115661A1
公开(公告)日：2006-06-01
申请号：US11001884
申请日：2004-12-01
申请人： Brian Hazel , Mark Gorman , Bangalore Nagaraj
发明人： Brian Hazel , Mark Gorman , Bangalore Nagaraj
IPC分类号： B32B15/04 , B32B9/00 , B32B19/00
CPC分类号： C23C26/00 , C23C28/3215 , C23C28/3455 , C23C30/00 , F01D5/284 , F01D5/288 , F05D2230/31 , F05D2260/95 , Y02T50/67 , Y02T50/6765
摘要： According to an embodiment of the invention, an article of manufacture for use in a gas turbine engine is disclosed. The article comprises a part having a surface covered with a ceramic thermal barrier coating. The thermal barrier coating has an outer surface covered with a sacrificial phosphate coating, wherein the sacrificial phosphate coating reacts with contaminant compositions to prevent contaminant infiltration into the thermal barrier coating.
摘要翻译：根据本发明的实施例，公开了一种用于燃气涡轮发动机的制品。该制品包括具有覆盖有陶瓷热障涂层的表面的部分。热障涂层具有被牺牲磷酸盐涂层覆盖的外表面，其中牺牲磷酸盐涂层与污染物组合物反应以防止污染物渗透到热障涂层中。

4. 发明申请

US20070224411A1 Protection of thermal barrier coating by impermeable barrier coating 审中-公开
标题翻译：通过防渗涂层保护热障涂层
公开(公告)号：US20070224411A1
公开(公告)日：2007-09-27
申请号：US11607380
申请日：2006-12-01
申请人： Brian Hazel , Irene Spitsberg , Christine Govern , Bangalore Nagaraj
发明人： Brian Hazel , Irene Spitsberg , Christine Govern , Bangalore Nagaraj
IPC分类号： B05D1/36
CPC分类号： C23C28/3215 , C23C28/321 , C23C28/325 , C23C28/345 , C23C28/3455 , C23C28/36 , F05B2230/90 , F05C2253/12 , Y02T50/67 , Y02T50/6765 , Y10T428/12611 , Y10T428/249953 , Y10T428/263 , Y10T428/31678
摘要： According to an embodiment of the invention, disclosed is a composite comprising a porous thermal barrier coating on a metallic part and an impermeable barrier coating adjacent to the outer surface of the thermal barrier coating. The impermeable barrier coating is dense and non-porous and comprises a rare earth silicate, the impermeable barrier coating thereby preventing infiltration of the contaminant composition into the thermal barrier coating.
摘要翻译：根据本发明的一个实施例，公开了一种复合材料，其包括在金属部件上的多孔热障涂层和邻近该热障涂层的外表面的不可渗透的阻隔涂层。不透水的阻隔涂层是致密且无孔的并且包含稀土硅酸盐，不透水的阻隔涂层从而防止污染物组合物渗透到热障涂层中。

5. 发明申请

US20070128447A1 Corrosion inhibiting ceramic coating and method of application 审中-公开
标题翻译：防腐陶瓷涂层及其应用方法
公开(公告)号：US20070128447A1
公开(公告)日：2007-06-07
申请号：US11293448
申请日：2005-12-02
申请人： Brian Hazel , Lawrence Kool
发明人： Brian Hazel , Lawrence Kool
IPC分类号： B05D3/02 , B05D1/02
CPC分类号： C23C26/00 , C23C28/027 , C23C28/028 , Y02T50/67 , Y02T50/6765
摘要： A corrosion resistant coating for engine components such as turbine disks, turbine seal elements and turbine shafts. This coating may also find application to other turbine components that are subjected to high temperatures and corrosive environments, such as turbine components located within or on the boundary of the gas fluid flow path, including for example turbine blades, turbine vanes, liners and exhaust flaps. The corrosion resistant coating of the present invention in service on a gas turbine component includes a glassy ceramic matrix wherein the glassy matrix is silica-based and particles selected from the group consisting of refractory oxide particles, MCrAlX particles and combinations of these particles, substantially uniformly distributed within the matrix. The refractory oxide and/or the MCrAlX provides the coating with corrosion resistance. Importantly the coating of the present invention has a coefficient of thermal expansion (CTE) greater than alumina. The CTE of the coating is sufficiently close to the substrate material, that is, the component to which it is applied, such that the coating does not spall after frequent engine cycling at elevated temperature
摘要翻译：发动机部件如涡轮盘，涡轮密封元件和涡轮轴的耐腐蚀涂层。该涂层还可以应用于经受高温和腐蚀性环境的其它涡轮机部件，例如位于气体流体流路的边界内或其上的涡轮机部件，包括例如涡轮机叶片，涡轮叶片，衬管和排气翼。在燃气轮机部件上使用的本发明的耐腐蚀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，并且选自由耐火氧化物颗粒，MCrAlX颗粒和这些颗粒的组合组成的组的颗粒，基本均匀分布在矩阵内。难熔氧化物和/或MCrAlX为涂层提供耐腐蚀性。重要的是，本发明的涂层具有比氧化铝大的热膨胀系数（CTE）。涂层的CTE足够接近基材，即其所施加的组分，使得涂层在高温下经常发动机循环后不会分散

6. 发明申请

US20070071995A1 GAMMA PRIME PHASE-CONTAINING NICKEL ALUMINIDE COATING 有权
标题翻译： GAMMA PRIME相含镍镍铝涂层
公开(公告)号：US20070071995A1
公开(公告)日：2007-03-29
申请号：US11162838
申请日：2005-09-26
申请人： Brian Hazel , Ramgopal Darolia , Brett Boutwell , David Wortman
发明人： Brian Hazel , Ramgopal Darolia , Brett Boutwell , David Wortman
IPC分类号： F03B3/12 , B32B15/01 , B23K35/00
CPC分类号： C23C30/00 , Y10T428/12458 , Y10T428/12736 , Y10T428/1275 , Y10T428/12875 , Y10T428/12937 , Y10T428/12944
摘要： An intermetallic composition suitable for use as an environmentally-protective coating on surfaces of components used in hostile thermal environments, including the turbine, combustor and augmentor sections of a gas turbine engine. The coating contains the gamma-prime (Ni3Al) nickel aluminide intermetallic phase and either the beta (NiAl) nickel aluminide intermetallic phase or the gamma solid solution phase. The coating has an average aluminum content of 14 to 30 atomic percent and an average platinum-group metal content of at least 1 to less than 10 atomic percent, the balance of the coating being nickel, incidental impurities, and optionally hafnium.
摘要翻译：适用于在敌对热环境中使用的组件的表面上用作环境保护涂层的金属间组合物，包括燃气涡轮发动机的涡轮机，燃烧器和增压器部分。该涂层含有γ-prime（Ni 3 Al 3）铝铝化物金属间相和β（NiAl）镍铝化物金属间相或γ固溶体相。该涂层的平均铝含量为14〜30原子％，平均铂族金属含量为1〜10原子％以下，其余为镍，附带杂质，以及任选的铪。

7. 发明申请

US20060280963A1 THERMAL/ENVIRONMENTAL BARRIER COATING SYSTEM FOR SILICON-CONTAINING MATERIALS 有权
标题翻译：含硅材料的热/环境阻隔涂层系统
公开(公告)号：US20060280963A1
公开(公告)日：2006-12-14
申请号：US11160212
申请日：2005-06-14
申请人： Brian Hazel , Irene Spitsberg
发明人： Brian Hazel , Irene Spitsberg
IPC分类号： B32B13/04 , B32B19/00 , B32B9/00
CPC分类号： C04B41/89 , C04B41/009 , C04B41/52 , C04B2111/00405 , C09D1/00 , C09D5/18 , C23C28/042 , C23C28/048 , C23C28/324 , C23C28/34 , C23C28/341 , C23C28/345 , C23C28/3455 , C23C28/36 , C04B41/4527 , C04B41/5096 , C04B41/5024 , C04B41/5037 , C04B41/5032 , C04B41/5042 , C04B41/4529 , C04B41/522 , C04B35/565 , C04B35/584 , C04B35/806
摘要： A coating system for Si-containing materials, particularly those for articles exposed to high temperatures. The coating system exhibits improved resistance to corrosion from sea salt and CMAS as a result of using aluminate compounds to protect silicate-containing layers of the coating system. The coating system includes an environmental barrier coating, a thermal barrier coating overlying the environmental barrier coating and formed of a thermal-insulating material, and a transition layer between the environmental barrier coating and thermal barrier coating, wherein the transition layer contains at least one aluminate compound and/or alumina.
摘要翻译：用于含Si材料的涂层系统，特别是用于暴露于高温的制品。由于使用铝酸盐化合物来保护涂层体系中的含硅酸盐层，涂层体系表现出对海盐和CMAS的耐腐蚀性的改善。涂层系统包括环境屏障涂层，覆盖环境屏障涂层并由绝热材料形成的热障涂层，以及环境阻隔涂层和热障涂层之间的过渡层，其中过渡层包含至少一种铝酸盐化合物和/或氧化铝。

8. 发明申请

US20060280962A1 THERMAL/ENVIRONMENTAL BARRIER COATING SYSTEM FOR SILICON-CONTAINING MATERIALS 有权
标题翻译：含硅材料的热/环境阻隔涂层系统
公开(公告)号：US20060280962A1
公开(公告)日：2006-12-14
申请号：US11160185
申请日：2005-06-13
申请人： Brian Hazel , Irene Spitsberg , Christine Govern , Bangalore Nagaraj
发明人： Brian Hazel , Irene Spitsberg , Christine Govern , Bangalore Nagaraj
IPC分类号： B32B17/06 , B32B19/00 , B32B9/00
CPC分类号： C23C28/04 , C04B41/009 , C04B41/52 , C04B41/89 , F01D5/284 , F01D5/288 , Y10T428/12576 , C04B41/4527 , C04B41/5096 , C04B41/5037 , C04B41/5024 , C04B41/5031 , C04B41/5044 , C04B41/5042 , C04B41/4529 , C04B41/522 , C04B35/565 , C04B35/584 , C04B35/806
摘要： A coating system for Si-containing materials, particularly Si-based composites used to produce articles exposed to high temperatures. The coating system is a compositionally-graded thermal/environmental barrier coating (T/EBC) system that includes an intermediate layer containing yttria-stabilized hafnia (YSHf) and mullite, alumina and/or an aluminosilicate, which is used in combination with an inner layer between a Si-containing substrate and the intermediate layer and a thermal-insulating top coat overlying the intermediate layer. The intermediate layer provides environmental protection to the silicon-containing substrate, and has a coefficient of thermal expansion between that of the top coat and that of the inner layer so as to serve as a transition layer therebetween. The intermediate layer is particular well suited for use in combination with an inner layer of an alkaline earth metal aluminosilicate (such as BSAS) and a top coat formed of YSZ or YSHf.
摘要翻译：用于含Si材料的涂层系统，特别是用于生产暴露于高温的制品的Si基复合材料。涂层系统是一种组成分级的热/环境屏障涂层（T / EBC）系统，其包括含有氧化钇稳定的铪（YSHf）和莫来石，氧化铝和/或铝硅酸盐的中间层，其与内部在含Si衬底和中间层之间的层和覆盖中间层的绝热顶涂层。中间层为含硅基材提供环境保护，并且具有顶涂层与内层层之间的热膨胀系数，以便在其间作为过渡层。中间层特别适用于与碱土金属硅铝酸盐（如BSAS）的内层和由YSZ或YSHf形成的顶层组合使用。

9. 发明申请

US20050255329A1 Superalloy article having corrosion resistant coating thereon 审中-公开
标题翻译：在其上具有耐腐蚀涂层的超合金制品
公开(公告)号：US20050255329A1
公开(公告)日：2005-11-17
申请号：US10843966
申请日：2004-05-12
申请人： Brian Hazel
发明人： Brian Hazel
IPC分类号： B32B15/04 , C23C4/10 , C23C14/06 , C23C14/32 , C23C16/00 , C23C30/00 , F01D5/28
CPC分类号： F01D5/288 , C23C14/0021 , C23C14/0617 , C23C14/325 , F05D2230/90 , Y02T50/67
摘要： According to an embodiment of the invention, a turbine engine rotor component comprises a base metal substrate; and an oxidation and corrosion resistant metal nitride or metal carbide overlay coating applied directly on the base metal substrate of the turbine engine rotor component.
摘要翻译：根据本发明的实施例，涡轮发动机转子部件包括基底金属基板; 以及直接施加在涡轮发动机转子部件的基底金属基底上的抗氧化和腐蚀的金属氮化物或金属碳化物覆盖涂层。

10. 发明申请

US20050138805A1 Touch-up of layer paint oxides for gas turbine disks and seals 有权
标题翻译：用于燃气轮机盘和密封件的层漆氧化物的接触
公开(公告)号：US20050138805A1
公开(公告)日：2005-06-30
申请号：US10747458
申请日：2003-12-29
申请人： Brian Hazel , Eva Lanman , Joseph Heaney , Michael Weimer
发明人： Brian Hazel , Eva Lanman , Joseph Heaney , Michael Weimer
IPC分类号： C09D1/00 , C09D1/02 , C09D4/00 , C09D5/18 , F01D5/28 , F01D25/00 , B23P6/00 , B23K9/04
CPC分类号： F01D5/286 , C09D1/00 , C09D1/02 , C09D5/18 , F01D5/288 , F01D25/007 , F05D2230/80 , F05D2230/90 , F05D2300/2112 , F05D2300/611 , Y02T50/67 , Y10T29/49318 , Y10T29/49746 , Y10T29/49885
摘要： The present invention is a process for applying oxide paint as a touch-up paint for an oxide-based corrosion inhibiting coating with at least one imperfection region. Such oxide-based corrosion inhibiting coatings are applied on superalloy components used for moderately high temperature applications, such as the superalloy components found in the high-pressure turbine (HPT) section of a gas turbine engine, including turbine disks and seals. However, during the application of oxide-based corrosion inhibiting coatings, imperfection regions sometimes occur, exposing the superalloy substrate beneath the oxide-based corrosion inhibiting coating. Such imperfection regions can include a spalled region, a scratched region, a chipped region, an uncoated region, or combinations thereof. The process of the present invention is useful where aircraft engine components have been treated with a corrosion inhibiting three-layer paint oxide system comprising chromia and alumina, but where a small imperfection region or regions within the layer oxide system are present after initial manufacture, refurbishment, or repair of the component.
摘要翻译：本发明是一种将氧化物涂料用作具有至少一个不完美区域的氧化物基腐蚀抑制涂层的上涂料的方法。这种基于氧化物的腐蚀抑制涂层被应用于用于适度高温应用的超级合金部件上，例如在包括涡轮盘和密封件的燃气涡轮发动机的高压涡轮机（HPT）部分中发现的超级合金部件。然而，在施加氧化物基腐蚀抑制涂层期间，有时会出现缺陷区域，使超合金基底暴露于氧化物基腐蚀抑制涂层之下。这样的缺陷区域可以包括剥落区域，划痕区域，切屑区域，未涂覆区域或其组合。本发明的方法在飞机发动机部件已经被包括氧化铬和氧化铝的腐蚀抑制三层涂料氧化物体系处理但在初始制造，翻新之后存在于氧化层系中的小缺陷区域或区域的情况下是有用的，或修理组件。

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