公开(公告)号：EP3062323B1

公开(公告)日：2018-11-21

申请号：EP14849668.0

申请日：2014-09-29

申请人： Shanghai Institute of Ceramics, Chinese Academy of Sciences

发明人： HUANG, Fuqiang ,  WANG, Zhou ,  YANG, Chongyin

IPC分类号： H01G11/46 ,  H01G11/86 ,  C04B35/628 ,  C01G23/04 ,  C04B35/622 ,  H01G11/38

CPC分类号： H01G11/46 ,  C01G23/043 ,  C01P2002/52 ,  C01P2004/04 ,  C01P2006/40 ,  C04B35/62259 ,  C04B35/62857 ,  C04B35/62865 ,  C04B35/62897 ,  C04B2235/3232 ,  C04B2235/5284 ,  H01G11/38 ,  H01G11/86 ,  Y02E60/13

摘要： A titanium oxide-based supercapacitor electrode material and a method of manufacturing same. A reactive substance of the titanium oxide-based supercapacitor electrode material is a conductive titanium oxide. The conductive titanium oxide is a sub-stoichiometric titanium oxide, reduced titanium dioxide, or doped reduced titanium dioxide obtained by further doping an element in reduced titanium dioxide. The titanium oxide-based supercapacitor electrode material has a carrier concentration greater than 10 18 cm -3 , and the titanium oxide-based supercapacitor electrode material has a specific capacitance 20 F/g to 1,740 F/g at a charge/discharge current of 1 A/g.

公开(公告)号：EP2340238B1

公开(公告)日：2018-04-18

申请号：EP09747903.4

申请日：2009-09-23

申请人： Safran Ceramics

发明人： EBERLING-FUX, Nicolas ,  BOUILLON, Eric ,  PHILIPPE, Eric ,  TAWIL, Henri

IPC分类号： C04B35/80

CPC分类号： C04B35/83 ,  B82Y30/00 ,  C04B35/571 ,  C04B35/6286 ,  C04B35/62865 ,  C04B35/62873 ,  C04B35/62884 ,  C04B35/62894 ,  C04B35/62897 ,  C04B35/806 ,  C04B2235/3821 ,  C04B2235/3826 ,  C04B2235/3843 ,  C04B2235/386 ,  C04B2235/424 ,  C04B2235/427 ,  C04B2235/5248 ,  C04B2235/5252 ,  C04B2235/5445 ,  C04B2235/5454 ,  C04B2235/614 ,  C04B2235/616

公开(公告)号：EP3158563A4

公开(公告)日：2018-02-14

申请号：EP15811002

申请日：2015-06-23

申请人： FREE FORM FIBERS LLC

发明人： PEGNA JOSEPH ,  VAALER ERIK G ,  HARRISON SHAY L ,  SCHNEITER JOHN L ,  WILLIAMS KIRK L ,  GODUGUCHINTA RAM K

IPC分类号： G21C3/02 ,  B23B19/00 ,  C04B35/565 ,  C04B35/628 ,  C04B35/80 ,  G21C3/04 ,  G21C3/42 ,  G21C21/02

CPC分类号： G21C3/20 ,  C04B35/565 ,  C04B35/62857 ,  C04B35/6286 ,  C04B35/62863 ,  C04B35/62865 ,  C04B35/62868 ,  C04B35/62873 ,  C04B35/62878 ,  C04B35/62884 ,  C04B35/62889 ,  C04B35/62894 ,  C04B35/62897 ,  C04B35/806 ,  C04B35/83 ,  C04B2235/3244 ,  C04B2235/3813 ,  C04B2235/422 ,  C04B2235/524 ,  C04B2235/5244 ,  C04B2235/5264 ,  C04B2235/5454 ,  C04B2235/614 ,  C23C16/08 ,  C23C16/483 ,  G21C3/04 ,  G21C3/07 ,  G21C3/18 ,  G21C3/28 ,  G21C3/42 ,  G21C3/62 ,  G21C21/02 ,  Y02E30/38

摘要： Nuclear fuel structures and methods for fabricating are disclosed herein. The nuclear fuel structure includes a plurality of fibers arranged in the structure and a multilayer fuel region within at least one fiber of the plurality of fibers. The multilayer fuel region includes an inner layer region made of a nuclear fuel material, and an outer layer region encasing the nuclear fuel material. A plurality of discrete multilayer fuel regions may be formed over a core region along the at least one fiber, the plurality of discrete multilayer fuel regions having a respective inner layer region of nuclear fuel material and a respective outer layer region encasing the nuclear fuel material. The plurality of fibers may be wrapped around an inner rod or tube structure or inside an outer tube structure of the nuclear fuel structure, providing both structural support and the nuclear fuel material of the nuclear fuel structure.

公开(公告)号：EP2567948B1

公开(公告)日：2017-03-29

申请号：EP12182707.5

申请日：2012-09-03

申请人： General Electric Company

发明人： ROBERTS lll, Herbert Chidsey ,  GRAY, Paul Edward ,  MATSUMOTO, Roger Lee Ken ,  BOY, Jeffrey H. ,  MONAGHAN, Philip Harold ,  HALADA, Joseph

IPC分类号： C04B35/573 ,  C04B35/628 ,  C04B35/80 ,  C04B37/00 ,  B29C65/06

CPC分类号： B29C65/0672 ,  B29C65/06 ,  C04B35/573 ,  C04B35/62857 ,  C04B35/6286 ,  C04B35/62863 ,  C04B35/62865 ,  C04B35/62868 ,  C04B35/62871 ,  C04B35/62873 ,  C04B35/62876 ,  C04B35/62894 ,  C04B35/806 ,  C04B37/001 ,  C04B2237/365 ,  C04B2237/38 ,  C04B2237/50 ,  C04B2237/84 ,  Y10T156/1089

公开(公告)号：EP2340238A2

公开(公告)日：2011-07-06

申请号：EP09747903.4

申请日：2009-09-23

申请人： Snecma Propulsion Solide

发明人： EBERLING-FUX, Nicolas ,  BOUILLON, Eric ,  PHILIPPE, Eric ,  TAWIL, Henri

IPC分类号： C04B35/80

CPC分类号： C04B35/83 ,  B82Y30/00 ,  C04B35/571 ,  C04B35/6286 ,  C04B35/62865 ,  C04B35/62873 ,  C04B35/62884 ,  C04B35/62894 ,  C04B35/62897 ,  C04B35/806 ,  C04B2235/3821 ,  C04B2235/3826 ,  C04B2235/3843 ,  C04B2235/386 ,  C04B2235/424 ,  C04B2235/427 ,  C04B2235/5248 ,  C04B2235/5252 ,  C04B2235/5445 ,  C04B2235/5454 ,  C04B2235/614 ,  C04B2235/616

摘要： The invention relates to a method for producing a part made of a thermostructural composite material, said method including making a fibrous preform made of wires or cables and impregnated with a consolidating composition containing a carbon or ceramic precursor, converting the precursor into carbon or ceramic by pyrolysis, and densifying the preform by gaseous-phase chemical infiltration. The consolidating composition further contains refractory solid fillers powder form having an average grain size lower than 200 nanometers and leaving, after pyrolysis, a consolidating solid phase in which the carbon or ceramic resulting from the precursor comprises a volume of between 3 and 10 % of the visible volume of the preform, while the solid fillers comprise a volume of between 0.5 and 5 % of the visible volume of the perform.

摘要翻译： 本发明涉及一种用于制造由热结构复合材料制成的部件的方法，所述方法包括制造由电线或电缆制成的纤维预制件，并且用含有碳或陶瓷前体的固结组合物浸渍，通过以下方式将所述前体转化成碳或陶瓷： 热解并通过气相化学渗透致密预制品。 该固结组合物还含有平均粒度小于200纳米的耐火固体填料粉末形式，并且在热解之后留下固结固相，其中由前体得到的碳或陶瓷占固体填料的3％至10％的体积 预制件的可见体积，而固体填料占该预制件的可见体积的0.5至5％之间的体积。

公开(公告)号：EP1618222A2

公开(公告)日：2006-01-25

申请号：EP04749877.9

申请日：2004-04-08

申请人： DOW GLOBAL TECHNOLOGIES INC.

发明人： PYZIK, Aleksander, J. ,  HU, Terry, I. ,  MORGAN, Ted, A. ,  LISTER, Daniel, R. ,  NEWMAN, Robert, A. ,  LUNGARD, Richard, Allen ,  DENG, Qin

IPC分类号： C22C1/10

CPC分类号： C23C14/223 ,  C04B35/62857 ,  C04B35/6286 ,  C04B35/62865 ,  C04B35/62873 ,  C04B35/62876 ,  C04B35/62884 ,  C04B35/62894 ,  C04B2235/3217 ,  C04B2235/3418 ,  C04B2235/3804 ,  C22C1/101 ,  C22C1/1036 ,  C22C47/04 ,  C22C47/06 ,  C22C2001/1021 ,  C23C14/0641 ,  C23C14/067 ,  Y10T428/12007 ,  Y10T428/31678

摘要： In one embodiment, a composition (10) to be mixed with a molten metal to make a metal matrix composite, the composition characterized by: a ceramic reinforcing filler (12), the ceramic reinforcing filler not being wettable by molten aluminum and/or not being chemically stable in molten aluminum, the ceramic reinforcing filler being coated with a ceramic material, the ceramic material being wettable by and chemically stable in molten aluminum. In a related embodiment, a composition (20) to make a porous preform to be infiltrated by molten metal to make a metal matrix composite, the composition characterized by: a ceramic reinforcing filler (23), the ceramic reinforcing filler not being wettable by molten aluminum, the ceramic reinforcing filler being coated with a ceramic material (22) and optionally with a metal (21) such as nickel, the ceramic material being wettable by molten aluminum. The ceramic material can be coated on the ceramic reinforcing filler by a vacuum deposition technique such as vacuum sputtering.

公开(公告)号：EP3112597A1

公开(公告)日：2017-01-04

申请号：EP15175008.0

申请日：2015-07-02

申请人： Airbus Defence and Space GmbH

发明人： STEINWANDEL, Jürgen, Dr. ,  WANG, Ning, Dipl.-Ing. ,  PIRINGER, Helmut, Dipl.-Ing.

IPC分类号： F01D5/28 ,  C04B35/00

CPC分类号： F01D5/282 ,  B28B1/24 ,  B28B11/243 ,  C04B35/053 ,  C04B35/117 ,  C04B35/486 ,  C04B35/505 ,  C04B35/62857 ,  C04B35/6286 ,  C04B35/62863 ,  C04B35/62865 ,  C04B35/62894 ,  C04B35/62897 ,  C04B35/6348 ,  C04B35/76 ,  C04B35/803 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/614 ,  C04B2235/616 ,  C23C16/045 ,  C23C16/30 ,  C23C16/32 ,  C23C16/442 ,  F01D5/284 ,  F01D5/288 ,  F05D2220/32 ,  F05D2230/90 ,  F05D2300/2112 ,  F05D2300/2118 ,  F05D2300/226 ,  F05D2300/228 ,  F05D2300/44 ,  F05D2300/601 ,  F05D2300/6033

摘要： Die vorliegende Erfindung betrifft eine Turbinenschaufel, umfassend ein vorgeformtes Fasergewebe aus Kohlenstoff-, Siliciumcarbid- oder Rheniumfasern, welches mit einem Bindemittelharz fixiert ist, und wobei das vorgeformte und fixierte Fasergewebe mit B 4 C beschichtet bzw. infiltriert ist, wobei das vorgeformte, fixierte und mittels B 4 C beschichtete bzw. infiltrierte Fasergewebe weiterhin eine mehrlagige Beschichtung aufweist aus mindestens einer Siliciumcarbidschicht und mindestens einer Schicht aus einem Metallborid, Metallnitrid oder Metallcarbid, und wobei über der mehrlagigen Beschichtung eine Oxidkeramik aufgebracht ist. Die Turbinenschaufel der vorliegenden Erfindung ist beständig gegen hohe Temperaturen und besonders zur Verwendung in einer Gasturbine geeignet. Ferner werden Verfahren zur Herstellung der erfindungsgemäßen Turbinenschaufel beschrieben.

摘要翻译： 这涉及一种涡轮机叶片，其包括由碳，碳化硅或铼固定的粘合剂树脂组成的纤维的预成型纤维织物，并且其中预先形成的和固定的纤维织物分别用B4C涂覆和渗透，其中预成型纤维织物 已经用B4C分别固定和涂覆和渗透的多层涂层进一步具有由至少一层碳化硅和至少一层金属硼化物，金属氮化物或金属碳化物组成的多层涂层，并且其中氧化物陶瓷 施加在多层涂层上。 涡轮叶片耐高温，特别适用于燃气轮机。 还描述了用于生产涡轮叶片的方法。

公开(公告)号：EP3047048A1

公开(公告)日：2016-07-27

申请号：EP14845964.7

申请日：2014-08-25

申请人： United Technologies Corporation

发明人： SCHMIDT, Wayde R.

IPC分类号： C23C26/00

CPC分类号： C04B35/62868 ,  C04B35/565 ,  C04B35/584 ,  C04B35/62865 ,  C04B35/62884 ,  C04B35/80 ,  C04B35/806 ,  C04B41/009 ,  C04B41/5063 ,  C04B41/87 ,  C04B2235/524 ,  C04B2235/5244 ,  C04B2235/5248 ,  C23C16/34 ,  D06M11/58 ,  D06M11/80 ,  D06M2101/40 ,  F01D5/288 ,  F05D2300/222 ,  F05D2300/2281 ,  F05D2300/2282 ,  C04B41/5064

摘要： An article includes a substrate and a coating on the substrate. The coating includes a compound of aluminum, boron and nitrogen in a continuous chemically bonded network having Al—N bonds and B—N bonds. Also disclosed is an article wherein the substrate is a plurality of fibers and the coating is a conformed coating of a compound of aluminum, boron and nitrogen having Al—N bonds and B—N bonds. The fibers are disposed in a matrix. Also disclosed is a method of protecting an article from environmental conditions. The method includes protecting a substrate that is susceptible to environmental chemical degradation using a coating that includes a compound of aluminum, boron and nitrogen having Al—N bonds and B—N bonds.

公开(公告)号：EP2804969A4

公开(公告)日：2016-03-09

申请号：EP13796908

申请日：2013-01-18

申请人： FREE FORM FIBERS LLC

发明人： PEGNA JOSEPH ,  SCHNEITER JOHN ,  WILLIAMS KIRK ,  GODUGUCHINTA RAMKIRAN

IPC分类号： D01F9/08 ,  C01B31/36 ,  C04B35/565 ,  C04B35/628 ,  C04B35/76 ,  C04B35/80 ,  C04B41/50 ,  C04B111/00 ,  D06M11/74

CPC分类号： C04B35/76 ,  C01B32/956 ,  C04B35/565 ,  C04B35/62865 ,  C04B35/62868 ,  C04B35/62873 ,  C04B35/806 ,  C04B2235/3409 ,  C04B2235/5244 ,  C04B2235/5264 ,  C04B2235/616 ,  D01F9/08 ,  D10B2101/16 ,  Y10T428/249964

摘要： A method and apparatus for forming a plurality of fibers from (e.g., CVD) precursors, including a reactor adapted to grow a plurality of individual fibers; and a plurality of independently controllable lasers, each laser of the plurality of lasers growing a respective fiber. A high performance fiber (HPF) structure, including a plurality of fibers arranged in the structure; a matrix disposed between the fibers; wherein a multilayer coating is provided along the surfaces of at least some of the fibers with an inner layer region having a sheet-like strength; and an outer layer region, having a particle-like strength, such that any cracks propagating toward the outer layer from the matrix propagate along the outer layer and back into the matrix, thereby preventing the cracks from approaching the fibers. A method of forming an interphase in a ceramic matrix composite material having a plurality of SiC fibers, which maximizes toughness by minimizing fiber to fiber bridging, including arranging a plurality of SiC fibers into a preform; selectively removing (e.g., etching) silicon out of the surface of the fibers resulting in a porous carbon layer on the fibers; and replacing the porous carbon layer with an interphase layer (e.g., Boron Nitride), which coats the fibers to thereby minimize fiber to fiber bridging in the preform.

公开(公告)号：EP1618222B1

公开(公告)日：2008-07-02

申请号：EP04749877.9

申请日：2004-04-08

申请人： DOW GLOBAL TECHNOLOGIES INC.

发明人： PYZIK, Aleksander, J. ,  HU, Terry, I. ,  MORGAN, Ted, A. ,  LISTER, Daniel, R. ,  NEWMAN, Robert, A. ,  LUNDGARD, Richard, Allen ,  DENG, Qin

IPC分类号： C22C1/10

CPC分类号： C23C14/223 ,  C04B35/62857 ,  C04B35/6286 ,  C04B35/62865 ,  C04B35/62873 ,  C04B35/62876 ,  C04B35/62884 ,  C04B35/62894 ,  C04B2235/3217 ,  C04B2235/3418 ,  C04B2235/3804 ,  C22C1/101 ,  C22C1/1036 ,  C22C47/04 ,  C22C47/06 ,  C22C2001/1021 ,  C23C14/0641 ,  C23C14/067 ,  Y10T428/12007 ,  Y10T428/31678

摘要： In one embodiment, a composition (10) to be mixed with a molten metal to make a metal matrix composite, the composition characterized by: a ceramic reinforcing filler (12), the ceramic reinforcing filler not being wettable by molten aluminum and/or not being chemically stable in molten aluminum, the ceramic reinforcing filler being coated with a ceramic material, the ceramic material being wettable by and chemically stable in molten aluminum. In a related embodiment, a composition (20) to make a porous preform to be infiltrated by molten metal to make a metal matrix composite, the composition characterized by: a ceramic reinforcing filler (23), the ceramic reinforcing filler not being wettable by molten aluminum, the ceramic reinforcing filler being coated with a ceramic material (22) and optionally with a metal (21) such as nickel, the ceramic material being wettable by molten aluminum. The ceramic material can be coated on the ceramic reinforcing filler by a vacuum deposition technique such as vacuum sputtering.