公开(公告)号：US20160256907A1

公开(公告)日：2016-09-08

申请号：US15035096

申请日：2014-05-28

申请人： NIPPON STEEL & SUMIKIN HARDFACING CO., LTD.

发明人： Koichi SHIJO

IPC分类号： B21B27/02 ,  C23C4/12 ,  C23C4/06 ,  B65H18/28 ,  B21C47/06

CPC分类号： B21B27/021 ,  B21B2015/0057 ,  B21C47/00 ,  B21C47/06 ,  B21C47/063 ,  B23K35/30 ,  B65H18/025 ,  B65H18/28 ,  B65H2404/147 ,  B65H2701/173 ,  C23C4/06 ,  C23C4/12 ,  C23C4/18 ,  C23C28/021 ,  C23C28/027

摘要： In rolls of winding equipment in a hot-rolling factory, each roll includes a lower cladding layer formed on the surface of the roll barrel and a self-fluxing alloy layer formed on the lower cladding layer by thermal spraying and containing carbide particles dispersed therein. The lower cladding layer includes an Fe-based cladding layer which has a Shore hardness of 60 or greater and which contains, in terms of mass %, 0.1-0.4 C, up to 2.0 Si, up to 3.0 Mn, 1.0-15.0 Cr, and 2.5-5.0 Ni. The lower cladding layer further contains one or more of Mo, V, and Co, the contents of Mo, V, and Co being 0.1-5.0 mass %, 0.1-3.0 mass %, and 0.5-5.0 mass %, respectively.

摘要翻译： 在热轧厂的卷绕设备中，每个辊包括形成在辊筒表面上的下包层和通过热喷涂形成在下包层上并含有分散在其中的碳化物颗粒的自熔合金层。 下包层包括肖氏硬度为60以上的Fe系包层，以质量％计含有0.1〜0.4C，高达2.0Si，高达3.0Mn，1.0〜15.0.0Cr， 和2.5-5.0镍。 下包层还含有Mo，V和Co中的一种或多种，​​Mo，V和Co的含量分别为0.1-5.0质量％，0.1-3.0质量％和0.5-5.0质量％。

公开(公告)号：US20160251976A1

公开(公告)日：2016-09-01

申请号：US15026755

申请日：2014-09-17

申请人： UNITED TECHNOLOGIES CORPORATION

发明人： Christopher W. Strock ,  Paul M. Lutjen ,  Michael J. Bruskotter

IPC分类号： F01D11/12 ,  F01D11/02 ,  C23C28/00 ,  C23C4/129 ,  C23C4/18 ,  F16J15/40 ,  C23C4/134

CPC分类号： F01D11/122 ,  C23C4/129 ,  C23C4/134 ,  C23C4/18 ,  C23C28/32 ,  C23C28/3455 ,  F01D11/02 ,  F05D2220/32 ,  F05D2230/312 ,  F05D2240/11 ,  F05D2240/55 ,  F16J15/40

摘要： An air seal system for a rotor blade assembly of a gas turbine engine includes a substrate. An optional ceramic interlayer may be disposed on an optional bond coat deposited on the substrate. An erosion resistant thermal barrier coating (E-TBC) layer is disposed on the ceramic interlayer (if present) or on the bond coat, or on the substrate. An abradable layer is disposed on the erosion resistant thermal barrier coating (E-TBC) layer.

摘要翻译： 用于燃气涡轮发动机的转子叶片组件的空气密封系统包括基板。 任选的陶瓷中间层可以设置在沉积在基底上的任选粘结涂层上。 在陶瓷中间层（如果存在）或粘合涂层上或衬底上设置耐侵蚀热障涂层（E-TBC）层。 耐磨层设置在抗侵蚀热障涂层（E-TBC）层上。

公开(公告)号：US09429035B2

公开(公告)日：2016-08-30

申请号：US14237255

申请日：2012-08-03

申请人： Maurizio Della Femina ,  Marco Rossi ,  Raffaele Casillo ,  Carlo Silvestro

发明人： Maurizio Della Femina ,  Marco Rossi ,  Raffaele Casillo ,  Carlo Silvestro

IPC分类号： C23C10/18 ,  F01D25/00 ,  C23C10/48 ,  C23C10/50 ,  C23C24/08 ,  C23C4/06 ,  C23C4/10 ,  C23C4/18

CPC分类号： F01D25/007 ,  C23C4/06 ,  C23C4/073 ,  C23C4/10 ,  C23C4/18 ,  C23C10/18 ,  C23C10/48 ,  C23C10/50 ,  C23C24/087 ,  Y10T428/12618

摘要： The invention refers to a process for the formation of a thermal barrier coating on a substrate, comprising the steps of: a) applying a bond coat on the substrate; b) subjecting the bond coat to a low activity aluminizing process, thus obtaining, above the bond coat, a temporary intermediate diffusion layer; c) applying, on the temporary intermediate diffusion layer, aluminum powder in suspension with a solvent or aqueous base, said aluminum powder having size distribution from 15 to 150 μm; d) performing a thermal treatment in a vacuum at a pressure from 10−3 to 10−5 bars, at a temperature from 800° C. to 1050° C. and with an active phase having duration in the range of 60 minutes to 4 hours, thus obtaining above the bond coat an enriched intermediate diffusion layer; and e) applying a definitive barrier layer on said enriched intermediate diffusion layer.

摘要翻译： 本发明涉及在衬底上形成热障涂层的方法，包括以下步骤：a）在衬底上施加粘合涂层; b）使接合涂层进行低活性镀铝处理，从而在粘结涂层上获得临时中间扩散层; c）在临时中间扩散层上涂覆悬浮液中的铝粉末与溶剂或碱水溶液，所述铝粉末的尺寸分布为15至150μm; d）在10-3至10-5巴的压力下，在800℃至1050℃的温度下进行真空中的热处理，并且活性相的持续时间为60分钟至4分钟 小时，从而在粘结层上方获得富集的中间扩散层; 以及e）在所述富集的中间扩散层上施加确定的阻挡层。

公开(公告)号：US09421740B2

公开(公告)日：2016-08-23

申请号：US13670515

申请日：2012-11-07

申请人： Korea Atomic Energy Research Institute ,  Korea Hydro and Nuclear Power Co., Ltd.

发明人： Kun-Woo Song ,  Yang-Hyun Koo ,  Byoung-Kwon Choi ,  Il-Hyun Kim ,  Hyun-Gil Kim ,  Yang-Il Jung ,  Dong Jun Park ,  Jeong-Yong Park

IPC分类号： C23C4/04 ,  C23C4/08 ,  C23C4/12 ,  B32B15/01 ,  C23C4/18 ,  C23C4/02 ,  C22C16/00 ,  C22F1/18 ,  G21C3/07 ,  G21C3/30

CPC分类号： B32B15/01 ,  C22C16/00 ,  C22F1/186 ,  C23C4/02 ,  C23C4/08 ,  C23C4/134 ,  C23C4/18 ,  G21C3/07 ,  G21C3/30 ,  Y02E30/40 ,  Y10T428/12674 ,  Y10T428/12812

摘要： A zirconium alloy for use in nuclear fuel assemblies is provided, which provides increased resistance against oxidation and corrosion and also improved bonding with parent material, because pure metallic material such as silicon (Si) or chromium (Cr) is evenly coated on the surface of the parent material by plasma spraying. Because the plasma spray coating used to coat the pure metallic material on the zirconium alloy does not require vacuum equipment and also is not limited due to the shape of the coated product, this is particularly useful when evenly treating the surface of the component such as 4 m-long tube or spacer grip arrangement which is very complicated in shape. Furthermore, because the coated zirconium alloy confers excellent resistance to oxidation and corrosion under emergency such as accident as well as normal service condition, both the economic and safety aspects of nuclear fuel are improved.

摘要翻译： 提供了用于核燃料组件的锆合金，其提供增加的抗氧化和腐蚀性，并且还改善了与母体材料的接合，因为诸如硅（Si）或铬（Cr）的纯金属材料被均匀地涂覆在 母材通过等离子喷涂。 由于用于在锆合金上涂覆纯金属材料的等离子体喷涂不需要真空设备，并且由于涂覆产品的形状也不受限制，因此当将组分的表面均匀地处理如4 m形管子或间隔手柄装置，其形状非常复杂。 此外，由于涂覆的锆合金在事故和正常使用条件下在紧急情况下具有优异的抗氧化和耐腐蚀性，因此提高了核燃料的经济性和安全性。

公开(公告)号：US09371253B2

公开(公告)日：2016-06-21

申请号：US14069547

申请日：2013-11-01

申请人： PRAXAIR S.T. TECHNOLOGY, INC.

发明人： Thomas Alan Taylor ,  Danny Lee Appleby ,  Albert Feuerstein ,  Ann Bolcavage ,  Neil Hitchman ,  James Munroe

IPC分类号： C23C4/10 ,  C04B35/48 ,  C23C4/02 ,  C23C4/18 ,  F01D5/28 ,  B32B3/00

CPC分类号： C04B35/48 ,  B32B3/00 ,  C23C4/02 ,  C23C4/10 ,  C23C4/11 ,  C23C4/18 ,  F01D5/288 ,  Y02T50/67 ,  Y10T428/12361 ,  Y10T428/1241 ,  Y10T428/12618 ,  Y10T428/12931 ,  Y10T428/12944 ,  Y10T428/12979 ,  Y10T428/24273 ,  Y10T428/24298 ,  Y10T428/24314 ,  Y10T428/24372 ,  Y10T428/24413 ,  Y10T428/24471 ,  Y10T428/24496 ,  Y10T428/24802 ,  Y10T428/24926 ,  Y10T428/25 ,  Y10T428/252 ,  Y10T428/26 ,  Y10T428/268 ,  Y10T428/2982 ,  Y10T428/2991

摘要： This invention relates to high purity yttria or ytterbia stabilized zirconia powders comprising from about 0 to about 0.15 weight percent impurity oxides, from about 0 to about 2 weight percent hafnium oxide (hafnia), from about 6 to about 25 weight percent yttrium oxide (yttria) or from about 10 to about 36 weight percent ytterbium oxide (ytterbia), and the balance zirconium oxide (zirconia). Thermal barrier coatings for protecting a component such as blades, vanes and seal surfaces of gas turbine engines, made from the high purity yttria or ytterbia stabilized zirconia powders, have a density greater than 88% of the theoretical density with a plurality of verticalzA macrocracks homogeneously dispersed throughout the coating to improve its thermal fatigue resistance.

摘要翻译： 本发明涉及包含约0至约0.15重量百分比的杂质氧化物，约0至约2重量百分比的氧化铪（hafnia），约6至约25重量％的氧化钇（氧化钇）的高纯度氧化钇或氧化钇稳定的氧化锆粉末 ）或约10至约36重量％的氧化镱（yttebia），余量为氧化锆（氧化锆）。 用于保护由高纯度氧化钇或稳定的氧化锆粉末制成的燃气涡轮发动机的叶片，叶片和密封表面的部件的热障涂层具有大于理论密度的88％的密度，同时具有多个verticalzA宏观裂纹 分散在整个涂层中以改善其耐热疲劳性。

公开(公告)号：US09364895B2

公开(公告)日：2016-06-14

申请号：US13507447

申请日：2012-06-29

申请人： Martin Hosek ,  Sripati Sah

发明人： Martin Hosek ,  Sripati Sah

IPC分类号： B22F3/115 ,  B22D23/00 ,  C23C4/18 ,  C23C6/00 ,  H01F1/24 ,  H01F3/08 ,  H01F41/02

CPC分类号： B22D23/003 ,  B22F3/115 ,  C23C4/18 ,  C23C6/00 ,  H01F1/24 ,  H01F3/08 ,  H01F41/0246 ,  Y10T428/24413

摘要： A system for making a material having domains with insulated boundaries is provided. The system includes a droplet spray subsystem configured to create molten alloy droplets and direct the molten alloy droplets to a surface, a spray subsystem configured to direct a spray of an agent at deposited droplets on the surface. The agent creates insulation layers on the deposited droplets such that the droplets form a material having domains with insulated boundaries on the surface.

公开(公告)号：US20160138156A1

公开(公告)日：2016-05-19

申请号：US14543948

申请日：2014-11-18

申请人： The Boeing Company

发明人： Thomas Karl Tsotsis

IPC分类号： C23C16/26 ,  B05D1/02 ,  B05D1/00 ,  B05D1/26 ,  B32B9/04 ,  B32B37/18 ,  C23C14/06 ,  C23C14/34 ,  B32B9/00 ,  C23C4/04 ,  B32B38/00

CPC分类号： C23C16/26 ,  C23C4/04 ,  C23C4/18 ,  C23C14/0605

摘要： A high-temperature polymeric-matrix composite (HTPMC) structure and a method for protecting an HTPMC from exposure to high temperatures in the presence of air, and prevent thermo-oxidative degradation. A thin, lightweight layer of a carbon-based barrier is applied onto a surface of the HTPMC structure. The carbon-based barrier coating is composed of graphene, amorphous carbon, or a mixture comprising a combination of graphene and amorphous carbon, and has coefficient of thermal expansion that is less than 10 times the coefficient of thermal expansion of the HTPMC structure. The carbon-based barrier may be coated with an erosion-barrier.

摘要翻译： 高温聚合物基复合材料（HTPMC）结构以及在空气存在下保护HTPMC免受高温暴露并防止热氧化降解的方法。 在HTPMC结构的表面上施加薄的，轻质的碳基阻挡层。 碳基阻挡涂层由石墨烯，无定形碳或包含石墨烯和无定形碳的组合的混合物组成，并且具有小于HTPMC结构的热膨胀系数的10倍的热膨胀系数。 碳基阻挡层可以被涂覆有侵蚀屏障。

公开(公告)号：US20160138151A1

公开(公告)日：2016-05-19

申请号：US14897113

申请日：2013-06-10

申请人： HITACHI, LTD.

发明人： Kousuke KUWABARA ,  Minseok PARK

IPC分类号： C23C8/66 ,  C23C28/04 ,  C23C4/06

CPC分类号： C23C8/66 ,  C23C4/06 ,  C23C4/18 ,  C23C24/04 ,  C23C28/048

摘要： A plurality of layers are laminated on at least part of the member under treatment made of steel, the plurality of layers having carbon concentrations higher than that of the member under treatment and 1.0 wt. % or less, the carbon concentration of an outermost layer of the plurality of layers being the highest. A method for manufacturing a steel part, including spraying powder containing carbon on at least part of an member under treatment made of steel so as to form a first layer having a carbon concentration higher than that of the member under treatment and spraying powder containing carbon on at least part of the first layer so as to form a second layer having a carbon concentration higher than that of the first layer. Carbon concentrations of a plurality of layers including the first layer and the second layer are 1.0 wt. % or less.

摘要翻译： 在由钢制成的处理部件的至少一部分上层叠多个层，多个层的碳浓度高于处理部件的碳浓度，1.0重量％ ％以下，多层的最外层的碳浓度最高。 一种钢部件的制造方法，其特征在于，在由钢制成的处理部件的至少一部分上喷涂含有碳的粉末，形成碳浓度高于所述处理部件的碳浓度的第一层，并且喷涂含有碳的粉末 至少部分第一层，以便形成碳浓度高于第一层的第二层。 包括第一层和第二层的多个层的碳浓度为1.0重量％。 ％ 或更少。

公开(公告)号：US20160122877A1

公开(公告)日：2016-05-05

申请号：US14896767

申请日：2013-10-16

申请人： INSTITUTE OF METAL RESEARCH, CHINESE ACADEMY OF SCIENCES

发明人： Fuhui WANG ,  Shenglong ZHU ,  Minghui CHEN ,  Mingli SHEN ,  Cheng WANG

IPC分类号： C23C24/08 ,  B22F9/04 ,  B22F1/00 ,  C22C19/05

CPC分类号： C23C24/085 ,  B22F1/0003 ,  B22F9/04 ,  B22F2009/041 ,  B22F2301/15 ,  B22F2302/20 ,  B22F2302/25 ,  B22F2302/253 ,  B22F2302/256 ,  B22F2302/45 ,  B22F2303/05 ,  B22F2303/30 ,  C22C1/05 ,  C22C1/1084 ,  C22C19/056 ,  C22C19/058 ,  C22C30/00 ,  C22C32/0026 ,  C22C32/0063 ,  C22C32/0068 ,  C22F1/10 ,  C23C4/02 ,  C23C4/18 ,  C23C28/324 ,  C23C28/345

摘要： The present invention provides a surface alloy coating composite material for a high temperature resistant material, a coating and a manufacturing method thereof, wherein the surface alloy coating composite material is made of metal alloy powder having a face-centered cubic structure and enamel powder, and a component percentage thereof is as follows: 10-70wt % is the metal alloy powder, and remaining is the enamel powder; the metal alloy powder is selected from at least one type of NiCrAIX, NiCrX and NiCoCrAIX, wherein X is at least one type of hafnium, zirconium, a rare earth element and mixed rare earth, and the mixed rare earth can be two types or more than two types of rare earth elements that are used together or a rare earth element and one type or multiple types of Na, K, Ca, Sr and Ba that are used in a combined way.

摘要翻译： 本发明提供一种耐高温材料用表面合金涂层复合材料及其制备方法，其中表面合金涂层复合材料由具有面心立方结构和搪瓷粉末的金属合金粉末制成， 其成分百分比如下：金属合金粉末为10-70wt％，剩余为搪瓷粉末; 金属合金粉末选自NiCrAIX，NiCrX和NiCoCrAIX中的至少一种，其中，X为铪，锆，稀土元素和混合稀土中的至少一种，混合稀土可以为两种以上 一起使用的两种类型的稀土元素或稀土元素以及以组合方式使用的一种或多种类型的Na，K，Ca，Sr和Ba。

公开(公告)号：US20160097459A1

公开(公告)日：2016-04-07

申请号：US14507765

申请日：2014-10-06

申请人： Caterpillar Inc.

发明人： Mark Veliz ,  Daniel Sordelet

IPC分类号： F16K1/34 ,  F02M35/10 ,  B05D1/02 ,  F16K25/00

CPC分类号： F16K1/34 ,  B05D1/02 ,  C23C4/02 ,  C23C4/18 ,  C23C8/02 ,  C23C8/24 ,  C23C8/30 ,  C23C8/36 ,  C23C8/48 ,  C23C8/54 ,  F01L3/04 ,  F01L2103/00 ,  F02M35/10255 ,  F16K25/005

摘要： A valve for use in an internal combustion engine is disclosed. The valve includes a stem connected to a fillet disposed between the stem and a seat face. A thermal spray technique, such as a high velocity oxy fuel coating spray (HVOF) is applied to the seat face. A nitriding treatment that includes a nitrogen source, which may or may not contain carbon, and heat may be applied after the HVOF spray. The heat allows the nitrogen and/or carbon to penetrate the HVOF layer and the seat face to form a compound zone. The compound zone enhances the wear resistance of the surface during engine operation.

摘要翻译： 公开了一种用于内燃机的阀。 阀包括连接到设置在杆和座面之间的圆角的杆。 将热喷涂技术，例如高速氧燃料喷涂（HVOF）施加到座面上。 在HVOF喷涂之后，可以施加包括可能含有或可以不含碳的氮源和热的氮化处理。 热量允许氮和/或碳穿透HVOF层和座面以形成复合区。 复合区域在发动机运行期间增强了表面的耐磨性。