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公开(公告)号:US20060099358A1
公开(公告)日:2006-05-11
申请号:US10982445
申请日:2004-11-05
申请人: Derek Raybould , Chien-Wei Li , Bjoern Schenk , Thomas Strangman
发明人: Derek Raybould , Chien-Wei Li , Bjoern Schenk , Thomas Strangman
IPC分类号: B31B45/00
CPC分类号: C23C30/00 , C04B41/009 , C04B41/5027 , C04B41/52 , C04B41/87 , C04B41/89 , C04B2111/00982 , C23C26/00 , C23C28/042 , Y02T50/67 , Y10T428/13 , Y10T428/131 , Y10T428/1317 , C04B41/4527 , C04B41/5059 , C04B41/5066 , C04B41/522 , C04B41/4539 , C04B41/5024 , C04B41/5042 , C04B35/565 , C04B35/584 , C04B35/806
摘要: A protective coating for a component comprising a ceramic based substrate, and methods for protecting the component, the protective coating adapted for withstanding repeated thermal cycling. The substrate may comprise silicon nitride or silicon carbide, and the protective coating may comprise at least one tantalate of scandium, yttrium, or a rare earth element. The protective coating may further comprise one or more metal oxides. The coating protects the substrate from combustion gases in the high temperature turbine engine environment. The coating may be multi-layered and exhibits strong bonding to Si-based substrate materials and composites.
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公开(公告)号:US20060024528A1
公开(公告)日:2006-02-02
申请号:US10909026
申请日:2004-07-30
申请人: Thomas Strangman , Bjoern Schenk , Paul Yankowich
发明人: Thomas Strangman , Bjoern Schenk , Paul Yankowich
IPC分类号: B32B19/00
CPC分类号: C04B41/52 , C04B41/009 , C04B41/89 , Y10T428/12535 , Y10T428/12611 , Y10T428/249956 , C04B41/4582 , C04B41/5031 , C04B41/5035 , C04B41/522 , C04B41/5037 , C04B41/4527 , C04B41/5045 , C04B41/5024 , C04B41/5042 , C04B35/01 , C04B35/10 , C04B35/803
摘要: A layered structure includes a substrate comprising a layer of an oxide/oxide ceramic based composite material, a first oxide layer disposed directly on the substrate and formed from a material that has no greater than about 10% porosity and is substantially impermeable by water vapor, and a second oxide layer disposed directly on the first oxide layer and having a greater porosity than the first oxide layer. Either or both the first and second oxide layers of the coating system may be deposited using a plasma spraying process, a slurry deposition process which is followed by a sintering step, or an EB-PVD process.
摘要翻译: 分层结构包括:基底,其包括氧化物/氧化物陶瓷基复合材料层,直接设置在基底上并由不大于约10%孔隙率并且基本上不透水蒸气的材料形成的第一氧化物层, 以及直接设置在第一氧化物层上并且具有比第一氧化物层更大的孔隙率的第二氧化物层。 可以使用等离子喷涂工艺,浆料沉积工艺,其后是烧结步骤或EB-PVD工艺来沉积涂料体系的第一和第二氧化物层。
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公开(公告)号:US06977233B2
公开(公告)日:2005-12-20
申请号:US10621168
申请日:2003-07-15
申请人: Chien-Wei Li , Bjoern Schenk , James V. Guiheen
发明人: Chien-Wei Li , Bjoern Schenk , James V. Guiheen
IPC分类号: C04B35/593 , F01D5/28 , C04B35/577 , C04B35/596
CPC分类号: F01D5/284 , C04B35/593 , F05D2300/2283
摘要: Sintered silicon nitride products comprising predominantly β-silicon nitride grains in combination with from about 0.1 to 30 mole % silicon carbide, and grain boundary secondary phases of scandium oxide and scandium disilicate. Such products have high fracture toughness, resistance to recession, and resistance to oxidation at temperatures of at least 1500° C. Methods for preparing sintered silicon nitride products are also disclosed.
摘要翻译: 主要包含β-氮化硅颗粒与约0.1至30摩尔%的碳化硅以及钪氧化物和二硅酸钪的晶界二次相组合的烧结氮化硅产品。 这些产品在至少1500℃的温度下具有高的断裂韧性,抗后退性和耐氧化性。还公开了制备氮化硅烧结体的方法。
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公开(公告)号:US20050042461A1
公开(公告)日:2005-02-24
申请号:US10644523
申请日:2003-08-18
申请人: Chien-Wei Li , Derek Raybould , Thomas Strangman , Bjoern Schenk
发明人: Chien-Wei Li , Derek Raybould , Thomas Strangman , Bjoern Schenk
CPC分类号: C04B41/009 , C04B41/52 , C04B41/89 , Y10T428/265 , C04B41/4531 , C04B41/5066 , C04B41/4558 , C04B41/5027 , C04B41/5035 , C04B41/5022 , C04B41/522 , C04B41/5042 , C04B35/565 , C04B35/58 , C04B35/584
摘要: A component comprising a silicon-based substrate and a diffusion barrier coating disposed on the silicon-based substrate. The diffusion barrier coating comprises an isolation layer disposed directly on the silicon-based substrate and at least one oxygen barrier layer disposed on the isolation layer. The oxygen barrier layer prevents the diffusion of oxygen therethrough, and prevents excessive oxidation of the silicon-based substrate. The isolation layer(s) prevent contaminants and impurities from reacting with the oxygen barrier layer. An environmental barrier coating may be disposed on the diffusion barrier coating, and a thermal barrier coating may be disposed on the environmental barrier coating. Methods for making a component having a diffusion barrier coating are also disclosed.
摘要翻译: 一种组件,包括硅基衬底和设置在硅基衬底上的扩散阻挡涂层。 扩散阻挡涂层包括直接设置在硅基衬底上的隔离层和设置在隔离层上的至少一个氧阻挡层。 氧阻隔层防止氧气扩散通过其中,并防止硅基衬底的过度氧化。 隔离层防止污染物和杂质与氧阻隔层反应。 可以在扩散阻挡涂层上设置环境屏障涂层,并且可以在环境屏障涂层上设置热障涂层。 还公开了制备具有扩散阻挡涂层的组分的方法。
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公开(公告)号:US20050013993A1
公开(公告)日:2005-01-20
申请号:US10621719
申请日:2003-07-16
申请人: Chien-Wei Li , Derek Raybould , Bjoern Schenk , Thomas Strangman
发明人: Chien-Wei Li , Derek Raybould , Bjoern Schenk , Thomas Strangman
CPC分类号: C04B41/009 , C04B41/5027 , C04B41/87 , C23C4/11 , C23C24/08 , C23C26/00 , C23C30/00 , F05B2230/90 , F05C2203/0843 , F05C2253/12 , Y10T428/265 , C04B41/4527 , C04B41/455 , C04B41/5031 , C04B41/5045 , C04B35/565 , C04B35/584 , C04B35/806
摘要: An environmentally and thermally protected component comprising a silicon-based ceramic or composite substrate and an environmental and thermal barrier coating disposed on the substrate. The environmental and thermal barrier coating comprises at least about 50 mole % AlTaO4. The composition of the environmental and thermal barrier coating may be adapted to provide excellent CTE (coefficient of thermal expansion) match with a substrate, such as a SiC-based ceramic or composite. Coating compositions of the invention have a stable crystalline structure at a temperature up to at least about 1550° C. Methods for preparing an environmentally and thermally protected component are also disclosed.
摘要翻译: 环境和热保护的组分,其包含硅基陶瓷或复合衬底以及设置在衬底上的环境和热障涂层。 环境和隔热涂层包含至少约50摩尔%的Al Ta O 4。 环境和隔热涂层的组成可以适于提供优异的CTE(热膨胀系数)与诸如SiC基陶瓷或复合材料的基底匹配。 本发明的涂料组合物在高达至少约1550℃的温度下具有稳定的晶体结构。还公开了制备环境和热保护组分的方法。
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公开(公告)号:US06672786B2
公开(公告)日:2004-01-06
申请号:US10164024
申请日:2002-06-04
申请人: Bjoern Schenk
发明人: Bjoern Schenk
IPC分类号: F16B900
CPC分类号: F02F7/0087 , F01D5/025 , F01D5/284 , F05D2300/21 , F16B2001/0085 , Y10T403/213 , Y10T403/217 , Y10T403/48
摘要: A joint assembly for coupling a ceramic member to a metal member is comprised of a ceramic shaft portion attached to the ceramic member; a slotted shrink fitter formed of a first metal and disposed around and in torque transmitting contact with the ceramic shaft portion to define a first interface surface therebetween; and a sleeve formed of a second metal disposed around and in torque transmitting contact with the shrink fitter to define a second interface surface therebetween. Either the shrink fitter or the sleeve attached to the metal member. The coefficient of thermal expansion of the second metal is relatively low compared to that of the first metal and the diameters of the first interface, (d1), and the second interface, (d2), are determined from the equation, d1/d2=(&agr;c−&agr;1)/(&agr;2−&agr;1) where &agr;c, &agr;1 and &agr;2 are the coefficients of thermal expansion of the ceramic, the first metal and the second metal respectively. A compliant sleeve is disposed the ceramic shaft portion and the slotted shrink fitter.
摘要翻译: 用于将陶瓷构件耦合到金属构件的接合组件包括附接到陶瓷构件的陶瓷轴部分; 一个由第一金属构成的开槽的收缩装配器,并围绕陶瓷轴部分转动传递接触,以限定其间的第一界面; 以及由第二金属形成的套筒,其设置在所述收缩钳位器的周围并且与所述收缩钳位器扭矩传递接触,以在其间限定第二界面。 收缩钳或者连接到金属构件的套筒。 与第一金属相比,第二金属的热膨胀系数相对较低,并且第一界面(d1)和第二界面(d2)的直径由等式d1 / d2 = (alphac-α1)/(α2-α1),其中alphac,α1和α2分别是陶瓷,第一金属和第二金属的热膨胀系数。 柔性套筒设置在陶瓷轴部分和开槽的收缩钳位机上。
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公开(公告)号:US08703661B2
公开(公告)日:2014-04-22
申请号:US13369853
申请日:2012-02-09
申请人: Reza Oboodi , James Piascik , Bjoern Schenk
发明人: Reza Oboodi , James Piascik , Bjoern Schenk
IPC分类号: F16C33/04
CPC分类号: F16C33/12 , C23C18/1662 , C25D15/00 , F16C17/024 , F16C33/6696 , F16C2204/20 , F16C2220/24 , F16C2223/80 , F16C2360/24
摘要: Components, turbochargers, and methods of forming components are provided. In an embodiment, by way of example only, a method of forming a component is provided. The method includes applying a plurality of coated particles to a substrate, wherein each coated particle comprises a solid film lubricant particle and a layer surrounding an entire surface of the solid film lubricant particle, each solid film lubricant particle comprises at least one compound, and the layer comprises a coating material having a greater resistance to oxidation than the compound when subjected to a predetermined processing temperature and heating the substrate to the predetermined processing temperature to form a portion of a coating over the substrate.
摘要翻译: 提供了组件,涡轮增压器和组件的形成方法。 在一个实施例中,仅作为示例,提供了形成部件的方法。 该方法包括将多个涂覆的颗粒施加到基材上,其中每个涂覆的颗粒包含固体膜润滑剂颗粒和围绕固体膜润滑剂颗粒的整个表面的层,每个固体膜润滑剂颗粒包含至少一种化合物,并且 层包括当经受预定处理温度时具有比化合物更大的抗氧化性的涂料,并将基材加热至预定的加工温度以在基材上形成涂层的一部分。
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公开(公告)号:US20100310763A1
公开(公告)日:2010-12-09
申请号:US12479034
申请日:2009-06-05
申请人: Reza Oboodi , James Piascik , Bjoern Schenk , Eric Passman , Richard Bye
发明人: Reza Oboodi , James Piascik , Bjoern Schenk , Eric Passman , Richard Bye
IPC分类号: B05D3/00
CPC分类号: C23C18/1216 , B22F7/04 , C23C18/1225 , C23C18/127 , C23C18/1279 , C23C18/1283 , C23C18/1295 , F16C33/043 , F16C33/1095
摘要: A method includes applying a coating precursor material over a substrate, the coating precursor material comprising a powder having an average particle diameter in a range of about 10 nanometers to about 10 microns comprising a fluoride eutectic, a metal capable of oxidizing at about 535° C. to about 800° C., one or more materials selected from the group consisting of a metal oxide, a glass, a carbide, and a nitride, and optionally, a precious metal selected from silver, palladium, platinum, gold, rhodium, and alloys thereof, subjecting the coating to a sintering heat treatment, occurring at a first temperature in an inert or reducing atmosphere to sinter the metal of the precursor material, and exposing the coating to an oxidizing heat treatment performed in an oxidizing atmosphere at a second temperature that is less than the first temperature to oxidize a portion of the metal in the coating precursor material.
摘要翻译: 一种方法包括将涂层前体材料涂覆在基底上,所述涂层前体材料包含平均粒径在约10纳米至约10微米范围内的粉末,其包含氟化物共晶体,能够在约535℃下氧化的金属 至约800℃,选自金属氧化物,玻璃,碳化物和氮化物的一种或多种材料,以及任选的选自银,钯,铂,金,铑, 及其合金,对涂层进行烧结热处理,在惰性或还原性气氛中的第一温度下进行烧结,烧结前体材料的金属,并在第二次氧化气氛中进行氧化热处理 温度小于第一温度以氧化涂层前体材料中的一部分金属。
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公开(公告)号:US07638178B2
公开(公告)日:2009-12-29
申请号:US10982445
申请日:2004-11-05
CPC分类号: C23C30/00 , C04B41/009 , C04B41/5027 , C04B41/52 , C04B41/87 , C04B41/89 , C04B2111/00982 , C23C26/00 , C23C28/042 , Y02T50/67 , Y10T428/13 , Y10T428/131 , Y10T428/1317 , C04B41/4527 , C04B41/5059 , C04B41/5066 , C04B41/522 , C04B41/4539 , C04B41/5024 , C04B41/5042 , C04B35/565 , C04B35/584 , C04B35/806
摘要: A protective coating for a component comprising a ceramic based substrate, and methods for protecting the component, the protective coating adapted for withstanding repeated thermal cycling. The substrate may comprise silicon nitride or silicon carbide, and the protective coating may comprise at least one tantalate of scandium, yttrium, or a rare earth element. The protective coating may further comprise one or more metal oxides. The coating protects the substrate from combustion gases in the high temperature turbine engine environment. The coating may be multi-layered and exhibits strong bonding to Si-based substrate materials and composites.
摘要翻译: 用于包含基于陶瓷的基材的组分的保护涂层以及用于保护组分的方法,所述保护涂层适于耐受重复的热循环。 衬底可以包括氮化硅或碳化硅,并且保护涂层可以包括至少一种钪,钇或稀土元素的钽酸盐。 保护涂层还可以包含一种或多种金属氧化物。 涂层保护基材免受高温涡轮发动机环境中的燃烧气体的影响。 该涂层可以是多层的并且表现出与Si基底材料和复合材料的牢固结合。
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公开(公告)号:US07251942B2
公开(公告)日:2007-08-07
申请号:US10880820
申请日:2004-06-29
CPC分类号: B64D41/00 , F01D15/10 , F02C3/09 , F02C7/32 , F05D2220/50 , F05D2240/50 , F23R3/06 , H02K7/1823 , Y02T50/675
摘要: An auxiliary power unit (APU) includes a compressor, a turbine, a combustor, and a starter-generator unit all integrated within a single containment housing. The turbine has an output shaft on which the compressor is mounted, and the starter-generator unit is coupled to the turbine output shaft without any intervening gears. The rotating components are all rotationally supported within the containment housing using bearings that do not receive a flow of lubricating fluid.
摘要翻译: 辅助动力单元(APU)包括压缩机,涡轮机,燃烧器和起动器 - 发电机单元,其全部集成在单个容纳壳体内。 涡轮机具有输出轴,压缩机安装在该输出轴上,并且起动器 - 发电机单元联接到涡轮机输出轴,而没有任何中间齿轮。 使用不会受到润滑流体流动的轴承,旋转部件都旋转地支撑在容纳壳体内。
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