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1.发明申请Thermal barrier coating/environmental barrier coating system for a ceramic-matrix composite (CMC) article to improve high temperature capability 有权陶瓷基复合材料（CMC）制品的隔热涂层/环境屏障涂层系统，以提高高温能力公开(公告)号：US20060121293A1
公开(公告)日：2006-06-08
申请号：US11006292
申请日：2004-12-06
申请人： Brett Boutwell , Irene Spitsberg , Christine Govern , Bangalore Nagaraj , Brian Hazel , Ramgopal Darolia , Curtis Johnson , Yan Gao , Mark Gorman
发明人： Brett Boutwell , Irene Spitsberg , Christine Govern , Bangalore Nagaraj , Brian Hazel , Ramgopal Darolia , Curtis Johnson , Yan Gao , Mark Gorman
CPC分类号： C04B41/009 , C04B41/52 , C04B41/89 , C04B2111/0025 , C23C28/042 , C23C28/322 , C23C28/345 , C23C28/3455 , F01D5/288 , F05D2230/90 , F05D2300/2118 , F05D2300/50211 , F05D2300/611 , C04B41/4527 , C04B41/5096 , C04B41/5035 , C04B41/522 , C04B41/5024 , C04B41/5037 , C04B41/5031 , C04B41/5042 , C04B41/5044 , C04B41/4529 , C04B35/565 , C04B35/584 , C04B35/806
摘要： In accordance with an embodiment of the invention, an article is provided. The article comprises a substrate comprised of silicon containing material, an environmental barrier coating (EBC) overlying the substrate and a thermal barrier coating (TBC) on the environmental barrier coating. The thermal barrier coating comprising a compound having a rhombohedral phase.
摘要翻译： 根据本发明的实施例，提供了一种制品。 该制品包括由含硅材料构成的衬底，覆盖衬底的环境阻挡涂层（EBC）和环境屏障涂层上的热障涂层（TBC）。 该热障涂层包含具有菱面体相的化合物。
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2.发明申请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
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％。
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公开(公告)号：US20070224411A1
公开(公告)日：2007-09-27
申请号：US11607380
申请日：2006-12-01
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。
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4.发明申请公开(公告)号：US20060280962A1
公开(公告)日：2006-12-14
申请号：US11160185
申请日：2005-06-13
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。
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5.发明申请公开(公告)号：US20060057406A1
公开(公告)日：2006-03-16
申请号：US10711364
申请日：2004-09-14
申请人： Ramgopal Darolia , Brett Boutwell , Brian Hazel , Bangalore Nagaraj , Joseph Rigney , Roger Wustman
发明人： Ramgopal Darolia , Brett Boutwell , Brian Hazel , Bangalore Nagaraj , Joseph Rigney , Roger Wustman
CPC分类号： C23C14/226 , C23C14/22 , C23C14/505 , C23C28/321 , C23C28/3215 , C23C28/345 , C23C28/3455 , C23C28/42 , F01D5/288 , F05D2230/90 , F05D2300/611 , Y10T428/24355 , Y10T428/24413
摘要： Thermal barrier coating (TBC) and a method of depositing a TBC having a modulated columnar microstructure that exhibits increased impact resistance. The TBC is deposited to have a columnar microstructure in which columns extend from a substrate surface. The columns having inner regions contacting the surface, outer regions near an outermost surface of the TBC, and interior regions therebetween. The inner regions of the columns are substantially normal to the substrate surface and at least one of the interior and outer regions of the columns are nonaligned with its respective inner regions, so that the columns of the columnar microstructure are continuous but modulated between the inner and outer regions to reduce tensile stresses within the columns resulting from particle impact.
摘要翻译： 热屏蔽涂层（TBC）和沉积具有显示出增加的耐冲击性的调制柱状微结构的TBC的方法。 沉积TBC以具有柱状微结构，其中柱从衬底表面延伸。 具有接触表面的内部区域，靠近TBC的最外表面的外部区域以及它们之间的内部区域的列。 柱的内部区域基本上垂直于基底表面，并且柱的内部和外部区域中的至少一个与其相应的内部区域不对齐，使得柱状微结构的列是连续的但是在内部和/ 外部区域以减少由于颗粒撞击引起的柱内的拉伸应力。
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6.发明申请THERMAL/ENVIRONMENTAL BARRIER COATING WITH TRANSITION LAYER FOR SILICON-COMPRISING MATERIALS 有权具有过渡层的热/环境阻挡层涂层用于含硅材料公开(公告)号：US20060166017A1
公开(公告)日：2006-07-27
申请号：US11040158
申请日：2005-01-21
CPC分类号： C04B35/195 , C04B35/16 , C04B35/185 , C04B41/009 , C04B41/52 , C04B41/89 , C04B2111/00405 , C04B2235/3208 , C04B2235/3213 , C04B2235/3215 , C04B2235/3224 , C04B2235/3427 , C04B2235/3436 , C04B2235/3454 , C04B2235/3463 , C23C28/042 , C23C28/048 , F05B2230/90 , F05C2253/12 , Y10T428/12576 , Y10T428/12667 , Y10T428/12729 , C04B41/4527 , C04B41/5024 , C04B41/5042 , C04B41/5051 , C04B41/5044 , C04B41/5027 , C04B41/522 , C04B35/565 , C04B35/584 , C04B35/806
摘要： An article comprising a substrate formed of a silicon-comprising material, such as an article exposed to the hostile thermal environment of a gas turbine engine. The article further comprises an environmental barrier layer, e.g., an alkaline earth metal aluminosilicate, and a top coat comprising zirconia or hafnia stabilized with an oxide of a metal selected from the group consisting of magnesium, calcium, scandium, yttrium, and lanthanide metals, and mixtures thereof. The article further comprises a transition layer between the environmental barrier layer and the top coat, the transition layer comprising zirconia or hafnia stabilized with an oxide of a metal selected from the group consisting of magnesium, calcium, scandium, yttrium, and lanthanide metals; and a low CTE oxide selected from the group consisting of niobia and tantala; and mixtures thereof. A method for preparing a thermal/environmental barrier coating system on a substrate formed of a silicon-comprising material is also disclosed.
摘要翻译： 一种制品，其包括由含硅材料形成的基底，例如暴露于燃气涡轮发动机的恶劣热环境的制品。 该制品还包括环境屏障层，例如碱土金属铝硅酸盐，以及包含氧化锆或氢氧化铪的顶涂层，所述氧化锆或铪被选自镁，钙，钪，钇和镧系金属的金属氧化物稳定， 及其混合物。 该制品还包括在环境阻挡层和顶部涂层之间的过渡层，过渡层包含用选自镁，钙，钪，钇和镧系金属的金属的氧化物稳定的氧化锆或氢化铪; 和选自iobia和tantala的低CTE氧化物; 及其混合物。 还公开了一种在由含硅材料形成的基底上制备热/环境屏障涂层系统的方法。
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公开(公告)号：US20060166016A1
公开(公告)日：2006-07-27
申请号：US11040157
申请日：2005-01-21
CPC分类号： F01D5/288 , C04B41/009 , C04B41/52 , C04B41/89 , C23C28/042 , C23C28/048 , Y10T428/12576 , Y10T428/12667 , Y10T428/12729 , C04B41/4527 , C04B41/5024 , C04B41/5037 , C04B41/5042 , C04B2111/00405 , C04B41/5044 , C04B41/4529 , C04B41/522 , C04B35/565 , C04B35/584 , C04B35/806
摘要： An article comprising a substrate formed of a silicon-comprising material, such as an article exposed to the hostile thermal environment of a gas turbine engine. The article further comprises an environmental barrier layer, e.g., an alkaline earth metal aluminosilicate, and a top coat comprising hafnia stabilized with from about 0.5 mole % to about 10 mole % of an oxide of a metal selected from the group consisting of magnesium, calcium, scandium, yttrium, and lanthanide metals, and mixtures thereof. The article optionally comprises a transition layer between the environmental barrier layer and the top coat. A method for preparing a thermal/environmental barrier coating on a substrate formed of a silicon-comprising material is also disclosed.
摘要翻译： 一种制品，其包括由含硅材料形成的基底，例如暴露于燃气涡轮发动机的恶劣热环境的制品。 该制品还包括环境屏障层，例如碱土金属铝硅酸盐，和包含用约0.5％摩尔至约10％摩尔的金属氧化物稳定的铪的顶涂层，所述金属氧化物选自镁，钙 钪，钇和镧系金属，及其混合物。 该制品任选地包括环境阻挡层和顶部涂层之间的过渡层。 还公开了在由含硅材料形成的基底上制备热/环境屏障涂层的方法。
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公开(公告)号：US20060115659A1
公开(公告)日：2006-06-01
申请号：US11001983
申请日：2004-12-01
CPC分类号： C23C28/3215 , C23C28/321 , C23C28/325 , C23C28/345 , C23C28/3455 , C23C28/36 , F05B2230/90 , F05C2253/12 , Y02T50/67 , 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。
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9.发明申请THERMAL/ENVIRONMENTAL BARRIER COATING WITH TRANSITION LAYER FOR SILICON-COMPRISING MATERIALS 有权具有过渡层的热/环境阻挡层涂层用于含硅材料公开(公告)号：US20060166015A1
公开(公告)日：2006-07-27
申请号：US11040156
申请日：2005-01-21
CPC分类号： C04B41/009 , C04B41/52 , C04B41/89 , C23C28/042 , C23C28/048 , F01D5/288 , Y10T428/12576 , Y10T428/12667 , Y10T428/12729 , C04B41/4527 , C04B41/5024 , C04B41/5037 , C04B41/5027 , C04B41/5042 , C04B41/5051 , C04B2111/00405 , C04B41/5044 , C04B41/522 , C04B41/4529 , C04B35/565 , C04B35/584 , C04B35/806
摘要： An article comprising a substrate formed of a silicon-comprising material, such as an article exposed to the hostile thermal environment of a gas turbine engine. The article further comprises an environmental barrier layer, e.g., an alkaline earth metal aluminosilicate, and a top coat comprising zirconia or hafnia stabilized with up to about 10 mole % of an oxide of a metal selected from the group consisting of magnesium, calcium, scandium, yttrium, and lanthanide metals, and mixtures thereof. The article further comprises a transition layer between the environmental barrier layer and the top coat, the transition layer comprising zirconia or hafnia stabilized with up to about 10 mole % of an oxide of a metal selected from the group consisting of magnesium, calcium, scandium, yttrium, and lanthanide metals; and a low CTE oxide selected from the group consisting of niobia and tantala; and mixtures thereof. A method for preparing a thermal/environmental barrier coating system on a substrate formed of a silicon-comprising material is also disclosed.
摘要翻译： 一种制品，其包括由含硅材料形成的基底，例如暴露于燃气涡轮发动机的恶劣热环境的制品。 该制品还包括环境屏障层，例如碱土金属硅铝酸盐，以及包含氧化锆或铪的面漆，所述氧化锆或铪被稳定，最多约10摩尔％的选自镁，钙，钪的金属氧化物 ，钇和镧系金属及其混合物。 该制品还包括在环境阻挡层和顶部涂层之间的过渡层，过渡层包含用高达约10摩尔％的金属氧化物稳定的氧化锆或铪，所述氧化物选自镁，钙，钪， 钇和镧系金属; 和选自iobia和tantala的低CTE氧化物; 及其混合物。 还公开了一种在由含硅材料形成的基底上制备热/环境屏障涂层系统的方法。
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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
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。
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