公开(公告)号：US5418071A

公开(公告)日：1995-05-23

申请号：US12845

申请日：1993-02-04

Applicant: Michio Satou ,  Takashi Yamanobe ,  Takashi Ishigami ,  Mituo Kawai ,  Noriaki Yagi ,  Toshihiro Maki ,  Minoru Obata ,  Shigeru Ando

Inventor： Michio Satou ,  Takashi Yamanobe ,  Takashi Ishigami ,  Mituo Kawai ,  Noriaki Yagi ,  Toshihiro Maki ,  Minoru Obata ,  Shigeru Ando

IPC: B22F3/14 ,  C04B35/58 ,  C22C1/05 ,  C23C14/06 ,  C23C14/34 ,  H01L21/28 ,  H01L21/285 ,  B22F7/06

CPC classification number: C04B35/58085 ,  C04B35/58092 ,  C04B35/645 ,  C04B35/65 ,  C23C14/3414 ,  Y10T428/12014 ,  Y10T428/12028 ,  Y10T428/12049 ,  Y10T428/12056

Abstract: In the present invention, metal silicide grains form an interlinked structure of a metal silicide phase, and Si grains which form a Si phase are discontinuously dispersed between the metal silicide phase to provide a sputtering target having a high density two-phased structure and having an aluminum content of 1 ppm or less. Because of the high density and high strength of the target, the generation of particles from the target during sputtering is reduced, and due to the reduced carbon content of the target, the mixing of carbon into the thin film during sputtering can be prevented.

Abstract translation: 在本发明中，金属硅化物晶粒形成金属硅化物相的互连结构，形成Si相的Si晶粒不连续地分散在金属硅化物相之间，以提供具有高密度二相结构的溅射靶，并具有 铝含量为1ppm以下。 由于目标的高密度和高强度，溅射期间从目标产生颗粒减少，并且由于靶的碳含量降低，可以防止在溅射期间将碳混入薄膜中。

公开(公告)号：US5023214A

公开(公告)日：1991-06-11

申请号：US336397

申请日：1989-04-11

Applicant: Roger L. K. Matsumoto ,  Allan B. Rosenthal

Inventor： Roger L. K. Matsumoto ,  Allan B. Rosenthal

IPC: C04B35/584 ,  C04B35/593

CPC classification number: C04B35/593 ,  C04B35/58085 ,  C04B35/584 ,  C04B35/587 ,  C04B35/5935 ,  C04B35/645 ,  C04B35/65 ,  C04B2235/3206 ,  C04B2235/3208 ,  C04B2235/3213 ,  C04B2235/3217 ,  C04B2235/3218 ,  C04B2235/3224 ,  C04B2235/3225 ,  C04B2235/3244 ,  C04B2235/3246 ,  C04B2235/327 ,  C04B2235/3275 ,  C04B2235/3279 ,  C04B2235/3891 ,  C04B2235/405 ,  C04B2235/77 ,  C04B2235/96

Abstract: Disclosed is a sintered ceramic product comprising (a) 20-98 percent by weight silicon nitride, (b) 1-80 percent by weight of a silicide of iron, cobalt or nickel and (c) 0.02-20 parts by weight of at least one oxide, nitride, or silicate of an element of IUPAC groups 2, 3, 4, 13 or the lanthanide series. A method for making such a product is also disclosed.

公开(公告)号：US4906493A

公开(公告)日：1990-03-06

申请号：US170180

申请日：1988-03-18

Applicant: Richard M. Laine

Inventor： Richard M. Laine

IPC: B22F3/00 ,  C01B21/06 ,  C01B25/08 ,  C01B31/30 ,  C01B31/34 ,  C01B33/06 ,  C01B35/04 ,  C04B35/56 ,  C04B35/58 ,  C04B35/622 ,  C04B35/626 ,  C04B41/51 ,  C04B41/88 ,  C22B5/00 ,  C22B5/20 ,  C22B25/02 ,  C22B59/00 ,  C22B60/02 ,  C22B60/04 ,  C22C1/00 ,  C23C18/02 ,  C23C18/12

CPC classification number: C04B35/5611 ,  B22F3/001 ,  B82Y30/00 ,  C01B21/0615 ,  C01B21/0635 ,  C01B25/08 ,  C01B31/30 ,  C01B31/301 ,  C01B31/305 ,  C01B31/306 ,  C01B31/34 ,  C01B33/06 ,  C01B35/04 ,  C04B35/58042 ,  C04B35/58071 ,  C04B35/58085 ,  C04B35/62227 ,  C04B35/626 ,  C04B41/5133 ,  C04B41/88 ,  C22B25/02 ,  C22B5/00 ,  C22B5/20 ,  C22B59/00 ,  C22B60/0213 ,  C22B60/0291 ,  C22B60/0295 ,  C22B60/04 ,  C22C1/00 ,  C23C18/02 ,  C23C18/1208 ,  C23C18/1225 ,  C23C18/1275 ,  C01P2002/72 ,  C01P2002/82 ,  C01P2002/85 ,  C01P2004/04 ,  C01P2004/10 ,  C01P2004/54 ,  C01P2004/64 ,  C01P2006/12 ,  C01P2006/42 ,  C01P2006/80 ,  C01P2006/90

Abstract: Coatings of metals, metal alloys, metal carbides, nitrides, borides, silicides and phosphides are provided. A precursor having organic ligands bonded to one or more metal atoms, such precursor having the element X also bonded directly or indirectly to the metal or metals, is pyrolyzed on a substrate surface to give a coating of M.sub.a X.sub.b. M represents a transition, lanthanide or actinide metal or tin, X represents C, N, B, Si, or P, and a and b represent the atomic proportions of M and X. The subscript b may be zero if an alloy or pure metal is to be prepared. The product M.sub.a X.sub.b can be prepared by relatively low temperature pyrolysis and the precursor can be used as a solution or a low melting solid.

Abstract translation: 提供金属，金属合金，金属碳化物，氮化物，硼化物，硅化物和磷化物的涂层。 具有与一个或多个金属原子结合的有机配体的前体，具有也直接或间接地结合到金属或金属的元素X的前体在基底表面上被热解，得到MaXb的涂层。 M表示过渡态，镧系元素或锕系金属或锡，X表示C，N，B，Si或P，a和b表示M和X的原子比例。如果合金或纯金属 准备好了 产物MaXb可以通过相对低温的热解制备，并且前体可以用作溶液或低熔点固体。

公开(公告)号：US11834559B2

公开(公告)日：2023-12-05

申请号：US17158665

申请日：2021-01-26

Applicant: NANOCORE APS ,  Mikkel Dybro Lundorf ,  Henrik Pedersen

Inventor： Mikkel Dybro Lundorf ,  Henrik Pedersen ,  Tore Dehli

IPC: C08J5/00 ,  B82Y30/00 ,  B82Y40/00 ,  C08K9/04 ,  C08K9/08 ,  C01B32/05 ,  C01B32/174 ,  C01B32/194 ,  C04B35/565 ,  C04B35/58 ,  C04B35/50 ,  C04B35/10 ,  C04B35/56 ,  C04B35/48 ,  C04B28/02 ,  C04B35/01 ,  C04B35/51 ,  C01B32/156 ,  C01B32/168 ,  C04B14/38 ,  C04B16/06 ,  C04B35/80 ,  C08F292/00 ,  C08J5/06 ,  C09D5/24 ,  C09D11/03 ,  C09D11/04 ,  C09D11/107 ,  C09D11/52 ,  C09D133/14 ,  C08K3/04 ,  C22C26/00 ,  H01B1/04

CPC classification number: C08J5/005 ,  B82Y30/00 ,  B82Y40/00 ,  C01B32/05 ,  C01B32/156 ,  C01B32/168 ,  C01B32/174 ,  C01B32/194 ,  C04B14/386 ,  C04B16/0675 ,  C04B28/02 ,  C04B35/01 ,  C04B35/10 ,  C04B35/48 ,  C04B35/50 ,  C04B35/51 ,  C04B35/56 ,  C04B35/565 ,  C04B35/58 ,  C04B35/58085 ,  C04B35/80 ,  C08F292/00 ,  C08J5/06 ,  C08K9/04 ,  C08K9/08 ,  C09D5/24 ,  C09D11/03 ,  C09D11/04 ,  C09D11/107 ,  C09D11/52 ,  C09D133/14 ,  C04B2235/48 ,  C04B2235/5252 ,  C04B2235/5288 ,  C08F2810/20 ,  C08J2323/06 ,  C08J2363/00 ,  C08J2367/00 ,  C08J2369/00 ,  C08J2375/04 ,  C08J2377/06 ,  C08K3/041 ,  C08K3/042 ,  C08K2201/001 ,  C08K2201/011 ,  C22C26/00 ,  C22C2026/001 ,  H01B1/04 ,  C08K9/04 ,  C08L23/04 ,  C08K9/08 ,  C08L23/04 ,  C04B28/02 ,  C04B14/024 ,  C04B14/026 ,  C04B14/06 ,  C04B18/08 ,  C04B18/141 ,  C04B18/146 ,  C04B2103/10 ,  C04B2103/20 ,  C04B2103/32

Abstract: A type of composite material where the matrix material and additive are held together by covalently or non-covalently bound ligands is described. A particularly useful composite material covered by the present invention is a carbon nanotube-reinforced composite material where the matrix consists of a polymer, covalently attached to a linker, where said linker is non-covalently attached to the carbon nanotube. Methods for the preparation of such composite materials are provided.

公开(公告)号：US20180175270A1

公开(公告)日：2018-06-21

申请号：US15605584

申请日：2017-05-25

Applicant: Hyundai Motor Company ,  Kia Motors Corporation ,  Industry-Academic Cooperation Foundation, Yonsei University

Inventor： Byung Wook KIM ,  Jong Kook LEE ,  Han Saem LEE ,  In Woong LYO ,  Jin Woo KWAK ,  Woo Young LEE ,  Gwan Sik KIM ,  Hwi Jong LEE

IPC: H01L35/16 ,  H01L35/18 ,  H01L35/14 ,  H01L35/34 ,  H01L35/28 ,  C04B35/58 ,  C04B35/626 ,  C04B35/645

CPC classification number: H01L35/16 ,  C04B35/58085 ,  C04B35/6261 ,  C04B35/6264 ,  C04B35/62645 ,  C04B35/645 ,  C04B2235/3891 ,  C04B2235/422 ,  C04B2235/5436 ,  C04B2235/602 ,  C04B2235/6567 ,  C04B2235/6581 ,  C04B2235/666 ,  C04B2235/9607 ,  H01L35/14 ,  H01L35/18 ,  H01L35/22 ,  H01L35/28 ,  H01L35/34

Abstract: Provided herein are a thermoelectric material and a method for preparing the same, wherein the thermoelectric material has excellent thermoelectric performance and high mechanical properties (in particular, fracture toughness), and thus, when the thermoelectric material is applied to a thermoelectric module, the thermoelectric module has excellent performance and efficiency and a long lifespan.

公开(公告)号：US09944021B2

公开(公告)日：2018-04-17

申请号：US15274899

申请日：2016-09-23

Applicant: Dynamic Material Systems, LLC

Inventor： William Easter ,  Arnold Hill

IPC: B29C64/106 ,  B29C64/153 ,  B29C64/165 ,  B28B1/00 ,  B22F3/105 ,  B33Y10/00 ,  B33Y70/00 ,  B29C67/00 ,  B23K26/342 ,  B23K26/00 ,  C04B35/56 ,  C04B35/571 ,  C04B35/589 ,  C04B35/626 ,  C04B38/00 ,  C10M159/00 ,  C04B35/01 ,  C04B35/52 ,  C04B35/532 ,  C04B35/58 ,  C04B35/634 ,  C22C29/00 ,  B23K103/00 ,  B23K103/18 ,  B23K103/16 ,  B23K103/08 ,  B23K103/02 ,  C04B111/00

CPC classification number: B29C64/165 ,  B22F3/1055 ,  B23K26/0006 ,  B23K26/342 ,  B23K2103/02 ,  B23K2103/08 ,  B23K2103/16 ,  B23K2103/18 ,  B23K2103/42 ,  B23K2103/52 ,  B28B1/001 ,  B29C64/106 ,  B29C64/153 ,  B33Y10/00 ,  C04B35/01 ,  C04B35/522 ,  C04B35/532 ,  C04B35/56 ,  C04B35/5603 ,  C04B35/571 ,  C04B35/58 ,  C04B35/58085 ,  C04B35/589 ,  C04B35/6269 ,  C04B35/62695 ,  C04B35/634 ,  C04B38/008 ,  C04B2111/00181 ,  C04B2235/32 ,  C04B2235/3817 ,  C04B2235/3852 ,  C04B2235/3891 ,  C04B2235/425 ,  C04B2235/427 ,  C04B2235/483 ,  C04B2235/5248 ,  C04B2235/5264 ,  C04B2235/5288 ,  C04B2235/602 ,  C04B2235/6026 ,  C04B2235/6028 ,  C04B2235/95 ,  C10M159/00 ,  C22C29/00 ,  Y02P10/295 ,  C04B35/00 ,  C04B38/0074 ,  C04B38/0615

Abstract: Methods, processes, systems, devices and apparatus are provided for additive manufacture resulting in the 3D printing of novel ceramic composites. Additive manufacture or 3D printing of bulk ceramic and ceramic composite components occurs at considerably lower temperatures and shorter manufacturing intervals than the current state of the art. The methods, processes, systems, devices and apparatus and selection of precursor resins produce ceramic and ceramic composite material systems which have not been produced before by 3D printing.

公开(公告)号：US20180079648A1

公开(公告)日：2018-03-22

申请号：US15267517

申请日：2016-09-16

Applicant: General Electric Company

Inventor： Glen Harold Kirby ,  Julin Wan

IPC: C01B35/12 ,  C09D1/00 ,  C04B35/50 ,  C04B35/622 ,  C04B41/87 ,  C04B41/50

CPC classification number: C01B35/128 ,  C04B35/01 ,  C04B35/2675 ,  C04B35/44 ,  C04B35/50 ,  C04B35/505 ,  C04B35/58085 ,  C04B35/58092 ,  C04B41/009 ,  C04B41/52 ,  C04B41/89 ,  C04B2235/3217 ,  C04B2235/3222 ,  C04B2235/3224 ,  C04B2235/3225 ,  C04B2235/3227 ,  C04B2235/3229 ,  C04B2235/3272 ,  C04B2235/3274 ,  C04B2235/3286 ,  C04B2235/3409 ,  C04B2235/3891 ,  C04B2235/428 ,  C04B2235/764 ,  F01D5/288 ,  F01D9/02 ,  F05D2300/222 ,  F05D2300/6033 ,  F05D2300/611 ,  C04B35/565 ,  C04B35/806 ,  C04B35/584 ,  C04B35/10 ,  C04B35/803 ,  C04B35/14 ,  C04B35/18 ,  C04B41/5006 ,  C04B41/5027 ,  C04B41/5096 ,  C04B41/5071 ,  C04B41/522 ,  C04B41/4558 ,  C04B41/5022 ,  C04B41/5024 ,  C04B41/5042

Abstract: A compound is generally provided that has the formula: Ln3-xBxM5-yByO12, where Ln comprises Sc, Y, La, Ce, Pr, Nd, Pm, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb, Lu, or a mixture thereof; x is 0 to about 1.5; M comprises Ga, In, Al, Fe, or a combination thereof; y is 0 to about 2.5; and x+y is greater than 0. A composition is also provided that includes a silicon-containing material (e.g., silicon metal and/or a silicide) and the boron-doped refractory compound having the formula described above, such as about 0.001% to about 85% by volume of the boron-doped refractory compound.

公开(公告)号：US20160153288A1

公开(公告)日：2016-06-02

申请号：US13833822

申请日：2013-03-15

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Krishan Lal LUTHRA

IPC: F01D5/28 ,  C23C4/134 ,  C23C16/44

CPC classification number: F01D5/284 ,  C04B41/009 ,  C04B41/52 ,  C04B41/89 ,  C23C4/134 ,  C23C16/44 ,  C23C28/042 ,  C23C28/044 ,  C23C28/048 ,  F01D5/282 ,  F01D5/288 ,  Y02T50/672 ,  C04B35/565 ,  C04B35/806 ,  C04B35/584 ,  C04B35/58085 ,  C04B41/5024 ,  C04B41/5096

Abstract: The disclosure relates generally to recession resistant gas turbine engine articles that comprise a silicon containing substrate, and related coatings and methods. The present disclosure is directed, inter alia, to an engine article comprising a silicon substrate which is coated with a chemically stable porous oxide layer. The present disclosure also relates to articles comprising a substrate and a bond coat on top comprising a two phase layer of interconnected silicon and interconnected oxide, followed by a layer of silicon. The present disclosure further relates to a recession resistant article comprising an oxide in a silicon containing substrate, such that components of the silicon containing substrate is interconnected with oxides dispersed in the substrate and form the bulk of the recession resistant silicon containing article.

Abstract translation: 本公开总体上涉及包含含硅衬底的耐衰退燃气涡轮发动机制品，以及相关的涂层和方法。 本公开尤其涉及一种包括涂覆有化学稳定的多孔氧化物层的硅衬底的发动机制品。 本公开还涉及包含基底和顶部的粘合涂层的制品，其包含互连的硅和互连的氧化物的两相层，之后是一层硅。 本公开还涉及包含含硅衬底中的氧化物的耐衰退制品，使得含硅衬底的组分与分散在衬底中的氧化物相互连接并形成耐久性含硅物品的大部分。

公开(公告)号：US09341412B2

公开(公告)日：2016-05-17

申请号：US13717773

申请日：2012-12-18

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Krishan Lal Luthra

IPC: F01D5/28 ,  F02C6/08 ,  F02C7/18 ,  F26B23/02 ,  F23R3/00 ,  C04B41/00 ,  C04B41/45 ,  C04B41/80

CPC classification number: F26B23/02 ,  C04B41/009 ,  C04B41/4519 ,  C04B41/80 ,  F01D5/28 ,  F01D5/288 ,  F02C6/08 ,  F02C7/18 ,  F23R3/007 ,  C04B35/565 ,  C04B35/806 ,  C04B35/584 ,  C04B35/58085

Abstract: The present disclosure relates to methods and systems for reducing silica recession of silicon-containing ceramics or silicon-containing ceramic composites, particularly those exposed to a combustion gas or to combustion gas environments, including those exposed to high temperature combustion gas environments. The methods and systems involve silicon-doping of compressed air and/or removal of moisture from compressed air prior to co-mingling the treated compressed air with the combustion gas to which the silicon-containing ceramics or silicon-containing ceramic composites are exposed.

Abstract translation: 本公开内容涉及用于减少含硅陶瓷或含硅陶瓷复合材料的二氧化硅凹陷的方法和系统，特别是暴露于燃烧气体或燃烧气体环境中的那些，包括暴露于高温燃烧气体环境的那些。 在将经处理的压缩空气与含硅陶瓷或含硅陶瓷复合材料暴露于其中的燃烧气体共混之前，该方法和系统涉及压缩空气的硅掺杂和/或从压缩空气中去除水分。

公开(公告)号：US20150345302A1

公开(公告)日：2015-12-03

申请号：US14706045

申请日：2015-05-07

Applicant: United Technologies Corporation

Inventor： Michael J. Birnkrant ,  Dominic J. Mongillo, JR. ,  Joel H. Wagner ,  Weina Li ,  Jose L. Santana ,  Carey Clum ,  James T. Beals

IPC: F01D5/18

CPC classification number: F01D5/183 ,  C04B35/01 ,  C04B35/10 ,  C04B35/453 ,  C04B35/56 ,  C04B35/565 ,  C04B35/58 ,  C04B35/58085 ,  C04B38/00 ,  C04B38/0054 ,  C04B38/0074 ,  C04B2111/00982 ,  C04B2111/763 ,  F05D2260/203 ,  F05D2300/10 ,  F05D2300/20 ,  F05D2300/514 ,  F05D2300/612 ,  Y02T50/676 ,  C04B38/0045

Abstract: A transpiration-cooled article includes a body wall that has first and second opposed surfaces. The first surface is adjacent a passage that is configured to receive a pressurized cooling fluid. At least a portion of the body wall includes a nanocellular foam through which the pressurized cooling fluid from the passage can flow to the second surface. The article can be an airfoil that includes an airfoil body that has an internal passage and an outer gas-path surface. At least a portion of the airfoil body includes a nanocellular foam through which cooling fluid from the internal passage can flow to the gas-path surface.

Abstract translation: 蒸发冷却制品包括具有第一和第二相对表面的主体壁。 第一表面邻近经配置以接收加压冷却流体的通道。 体壁的至少一部分包括纳米细胞泡沫，来自通道的加压冷却流体可以通过该泡沫泡沫流到第二表面。 该制品可以是包括具有内部通道和外部气体路径表面的翼型件的翼型件。 翼型体的至少一部分包括纳米孔泡沫，通过该纳米孔泡沫，来自内部通道的冷却流体可通过其流到气体路径表面。