Способ повышения проницаемости пор углеграфитовой заготовки

FIELD: metallurgy.SUBSTANCE: invention relates to composite materials with porous carcass impregnation having high wear resistance, antifriction properties and resistance to aggressive media. Method of producing coal-graphite composite material includes vacuum degassing of porous coal-graphite billet, its impregnation with molten matrix lead alloy under the effect of excessive pressure due to thermal expansion of the melt when heated above the liquidus temperature of the lead alloy, wherein degassing is carried out prior to submersion of porous workpiece into melt of matrix alloy, and before impregnation porous workpiece is covered with two-layer galvanic coating consisting of internal copper and outer zinc layers.EFFECT: technical result is improved quality of composite materials by increasing permeability of pores of graphite billet.1 cl, 2 dwg, 1 tbl, 1 ex РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 688 773 C1 (51) МПК C22C 47/08 (2006.01) B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2019.02); B22F 3/26 (2019.02) (21)(22) Заявка: 2018101562, 16.01.2018 (24) Дата начала отсчета срока действия патента: 22.05.2019 Приоритет(ы): (22) Дата подачи заявки: 16.01.2018 (45) Опубликовано: 22.05.2019 Бюл. № 15 2539528 C1, 20.01.2015. EP 1477467 A1, 17.11.2004. JP 2009127116 A, 11.06.2009. SU 1759932 A1, 07.09.1992. (54) Способ повышения проницаемости пор углеграфитовой заготовки (57) Реферат: Изобретение относится к области выше температуры ликвидус сплава свинца, при металлургии, а именно к созданию этом дегазацию проводят до погружения композиционных материалов пропиткой пористой заготовки в расплав матричного сплава, пористого каркаса, имеющих высокую а перед пропиткой пористую заготовку износостойкость, антифрикционные свойства, покрывают двухслойным гальваническим стойкость в агрессивных средах. Способ покрытием, состоящим из внутреннего медного получения углеграфитового композиционного и ...

Способ повышения проницаемости пор углеграфитовой заготовки

Изобретение относится к области металлургии, а именно к созданию композиционных материалов пропиткой пористого каркаса, имеющих высокую электропроводность, антифрикционные свойства, стойкость в агрессивных средах. Способ получения углеграфитового композиционного материала включает вакуумную дегазацию пористой углеграфитовой заготовки, ее пропитку расплавом матричного сплава алюминия под воздействием избыточного давления за счет термического расширения расплава при нагреве выше температуры ликвидус сплава алюминия, при этом дегазацию проводят до погружения пористой заготовки в расплав матричного сплава, а перед пропиткой пористую заготовку покрывают слоем медного гальванического покрытия. Техническим результатом изобретения является повышение качества композиционных материалов за счет увеличения проницаемости пор углеграфитовой заготовки. 1 пр., 1 табл., 2 ил. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 688 525 C1 (51) МПК C22C 47/08 (2006.01) B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2019.02); B22F 3/26 (2019.02) (21)(22) Заявка: 2018101544, 16.01.2018 (24) Дата начала отсчета срока действия патента: 21.05.2019 Приоритет(ы): (22) Дата подачи заявки: 16.01.2018 (45) Опубликовано: 21.05.2019 Бюл. № 15 1759937 A1, 07.09.1992. EP 1477467, 17.11.2004. JP 2009127116 A, 11.06.2009. RU 2276631 C2, 20.05.2006. (54) Способ повышения проницаемости пор углеграфитовой заготовки (57) Реферат: Изобретение относится к области термического расширения расплава при нагреве металлургии, а именно к созданию выше температуры ликвидус сплава алюминия, композиционных материалов пропиткой при этом дегазацию проводят до погружения пористого каркаса, имеющих высокую пористой заготовки в расплав матричного сплава, электропроводность, антифрикционные свойства, а перед пропиткой пористую заготовку стойкость в агрессивных средах. Способ покрывают слоем медного гальванического получения углеграфитового ...

Способ получения углеграфитового композиционного материала

Изобретение относится к области металлургии, а именно к созданию композиционных материалов пропиткой пористого каркаса. Способ получения углеграфитового композиционного материала включает вакуумную дегазацию пористой углеграфитовой заготовки в растворе электролита, нанесение на нее четырехслойного гальванического покрытия, пропитку ее расплавом матричного сплава свинца под воздействием избыточного давления за счет термического расширения расплава при нагреве выше температуры ликвидус сплава свинца, при этом вакуумную дегазацию проводят в растворе никелевого электролита, содержащего 140 г/л сульфата никеля, 50 г/л сульфата натрия, 30 г/л сульфата магния, 20 г/л сухой борной кислоты, а гальваническое покрытие выполняют последовательным нанесением внутреннего никелевого, промежуточных цинкового и серебряного и наружного медного слоев. Техническим результатом изобретения является повышение качества композиционных материалов, в частности повышения прочности на сжатие. 1 табл.

СПОСОБ ПОЛУЧЕНИЯ ДЕТАЛЕЙ ИЗ КОМПОЗИТНОГО МАТЕРИАЛА ПУТЕМ ПРОПИТКИ КОМПОЗИЦИЕЙ С НИЗКОЙ ТЕМПЕРАТУРОЙ ПЛАВЛЕНИЯ

Verfahren zur Herstellung eines Aluminium-Gussbauteils sowie Zylinderkopf für ein Kraftfahrzeug und Fertigungsstrecke zur Durchführung eines Verfahrens

Die Erfindung betrifft ein Verfahren zur Herstellung eines Aluminium-Gussbauteils (22) mit mindestens einem darin angeordneten Verstärkungselement (10), umfassend mindestens die folgenden Verfahrensschritte:a) Herstellung eines Kerns (18), wobei mindestens ein Verstärkungselement (10) in eine erste Form (14) eingelegt wird und zumindest teilweise mit einem Schaumwerkstoff umspritzt wird;b) Einlegen des hergestellten Kerns (18) in eine zweite Form (20);c) Eingießen von Aluminium in die zweite Form (20), so dass das eingegossene Aluminium den Kern (18) zumindest teilweise umgibt und der Schaumwerkstoff beim Umgießen zumindest teilweise entfernt wird.Mittels des Verfahrens soll eine besonders einfache Herstellung eines Aluminium-Gussbauteils mit einem Verstärkungselement ermöglicht werden.Die Erfindung betrifft ferner einen Zylinderkopf für ein Kraftfahrzeug und eine Fertigungsstrecke zur Durchführung eines solchen Verfahrens.

THE MANUFACTURE OF ALUMINIUM/ZIRCONIA COMPOSITES

Method for preparing a SiC whisker-reinforced composite material

The invention provides a method for preparing a SiC whisker-reinforced composite material. A matrix material such as a metal, an alloy or a plastic is introduced into a fibrous base consisting of a SiC whisker sponge-like cake. The resultant structure is compressed into a desired shape as needed. The fibrous base is prepared by heating a mixture of silica gel or ashed rice hulls with a furnace carbon black and an additional amount of NaCl as a space forming agent for forming spaces conducive to whisker growth.

REINFORCEMENT OF ARTICLES OF CAST METAL

UNIDIRECTIONAL SOLIDIFICATION OF METAL

Method and extruder for producing a metal alloy profile

Die Erfindung betrifft ein Verfahren zur Herstellung eines Profils (1) aus einer Metalllegierung, wobei die Metalllegierung im teilflüssigen Zustand verarbeitet wird, wobei die insbesondere in Form von Spänen vorliegende Metalllegierung mit einem Extruder (E) kontinuierlich extrudiert wird, wobei Korn feinende Partikel eingearbeitet werden. Weiter betrifft die Erfindung einen Extruder (E) zur Herstellung eines Profils (1) aus einer Metalllegierung, umfassend einen Zylinder (2) und zumindest eine Schneckenwelle (3), wobei die zumindest eine Schneckenwelle (3) innerhalb des Zylinders (2) angeordnet ist, wobei der Extruder (E) zur Verarbeitung der Metalllegierung im teilflüssigen Zustand ausgebildet ist, wobei eine Heizeinrichtung (5) vorgesehen ist.

COMPOSITE MATERIAL

PROCEDURE FOR THE PRODUCTION OF VERBUNDWERKSTOFFK¯RPERN WITH METAL MATRIX BY VOLUNTEER FROM OUTSIDE INWARD ARRANGED INFILTRATION.

PROCEDURE FOR THE PRODUCTION OF BONDING MATERIAL WITH A METAL MATRIX WITH CONTROLLED REINFORCEMENT PHASE.

CERAMIC GATHERING MOLDS, YOUR PRODUCTION AND YOUR USES

ALUMINUM MATRIX COMPOSITE MATERIAL AND PROCEDURE FOR ITS PRODUCTION

FIBER-REINFORCED COMPOSITE MATERIAL WITH ALUMINUM MATRIX

Fiber reinforced aluminum matrix composite

METAL MATRIX COMPOSITE WIRES, CABLES, AND METHOD

Metal matrix composite wires (59) that include at least one tow comprising a plurality of substantially continuous, longitudinally positioned fibers (51) in a metal matrix. The fibers are selected from the group of ceramic fibers carbon fibers, and mixtures thereof. The wires have certain specified characteristics such as roundness values, roundness uniformity values, and/or diameter uniformity values.

A DIAMOND METAL COMPOSITE

The present invention relates to a method for producing diamond-metal composites comprising mixing diamond particles with metal-filler particles forming a diamond/metal-filler mixture, forming a green body of the diamond/metal-filler mixture, optionally green machining the green body to a work piece before or after pre-sintering by heating the green body to a temperature <= 500 °C, infiltrating the green body or the work piece with one or more wetting elements or infiltrating the green body or the work piecewith one or more wetting alloys, which infiltration step being carried out under vacuum or in an inert gas atmosphere at a pressure < 200 Bar. The invention relates further to a green body, a diamond metal composite, and use of the diamond metal composite.

METHOD OF PRODUCING REINFORCED COMPOSITE MATERIALS

PROCESS FOR PRODUCING COMPOSITE MATERIALS WITH A METAL MATRIX, WITH A CONTROLLED CONTENT OF REINFORCER AGENT

CASE 2934 "PROCESS FOR PRODUCING COMPOSITE MATERIALS WITH A METAL MATRIX, WITH A CONTROLLED CONTENT OF REINFORCER AGENT" A process for producing composite materials with a metal matrix and with a content of powder reinforcer agent lower than is minimum theoretical compaction value, with said process being based on an infiltration technique, is disclosed, which essentially consists in charging the reinforcer material to a casting mould, and then infiltrating into the same mould the metal matrix in the molten state, with said metal matrix being let cool until it solidifies, and characterized in that the reinforcer agent, consisting of non-metal powders, is blended, before being charged to said casting mould, with a diluting agent having a different compaction degree, constituted by metal fibres and/or ceramic fibres and/or ceramic whiskers and/or metal powders of the same composition as of the matrix.

SINGLE CYLINDER OR MULTICYLINDER BLOCK

In a cast linerless single cylinder or multicylinder block made of an aluminum alloy and intended for use in internal combustion engine, the aluminum matrix contains embedded silicon particles, which protrude from the sliding surface of the cylinder. In order to distinctly reduce the cost of the mechanical machining of the entire surface of the single cylinder or multicylinder block, only the sliding surface of the cylinder is constituted by a fibrous body which contains interspersed silicon particles and infiltrated aluminum alloy.

PROCESS FOR PRODUCING FIBER COMPOSITE PRECISION CASTINGS

In a process for producing fiber composite investment castings, at least one preliminary pattern body, which is then used as part of a pattern or the pattern itself, is produced with fibers and a pattern material. A ceramic mold is then formed around the pattern. The pattern material is then removed and finally, metal in liquid, liquid-solid or powdery form is introduced into the mold, wherein the metal is at least partially liquefied in the mold when it is introduced in powdery form. This process allows investment castings having an increased resistance to be produced with a relatively simple casting equipment.

Alliage comprenant une matrice et une phase de renforcement

VERFAHREN ZUR HERSTELLUNG EINES SCHICHTSTOFFS UND ERZEUGNIS DES VERFAHRENS.

Verfahren zur Herstellung von mit Kohlenstoff-Fasern verstärktem Metalldraht und Vorrichtung zur Durchführung des Verfahrens

Alliage composite renforcé, procédé et dispositif pour son obtention

METHOD AND APPARATUS FOR MAKING BARS ALLOY BY UNIDIRECTIONAL SOLIDIFICATION.

Procedure and device for the production of metal matrix composite materials.

Matériau composite.

L'invention concerne un matériau composite (1) composé d'une matrice (2) à base de verre métallique et de renforts (3) à base de fibres. L'invention porte également sur un procédé de fabrication d'un tel matériau.

Composant horloger flexible et mouvement d'horlogerie comportant un tel composant.

L'invention concerne un composant horloger flexible, notamment pour mécanisme oscillateur ou pour barillet d'un mouvement horloger, le composant comportant au moins une partie réalisée en une matière composite (1), la matière composite (1) comprenant une matrice (2) et une multitude de nano-fils (3) répartis dans la matrice (2), les nano-fils (3) étant juxtaposés, la matrice (2) comportant un matériau (4) de remplissage des interstices entre les nano-fils (3) pour les joindre les uns aux autres, chaque nano-fil (3) formant un tube plein monobloc.

Composant horloger flexible pour mécanisme oscillateur, comprenant un matériau de compensation thermique.

L'invention concerne un composant horloger flexible pour mécanisme oscillateur d'un mouvement horloger, le composant comportant au moins une partie réalisée en une matière composite (1), la matière composite (1) comprenant une matrice (2) et une multitude de nanotubes ou de nano-fils (3) répartis dans la matrice (2), les nanotubes ou nano-fils (3) étant juxtaposés et disposés de manière sensiblement parallèles à un axe (A) sensiblement perpendiculaire au plan (P) du composant, la matrice comportant un matériau de remplissage (4) flexible pour remplir les interstices entre les nanotubes ou nano-fils (3), le matériau de remplissage (4) comprenant au moins en partie un matériau de compensation thermique dont le coefficient de thermoélasticité est de signe opposé à celui des autres matériaux de la matière composite (1).

Composant horloger rigide pour mécanisme oscillateur ou pour mécanisme d'échappement et mouvement d'horlogerie comportant un tel composant.

L'invention concerne un composant horloger rigide pour mécanisme oscillateur ou pour mécanisme d'échappement d'un mouvement horloger, le composant comportant au moins une partie réalisée en une matière composite (1), la matière composite (1) comprenant une matrice (2) et une multitude de nanotubes ou de nano-fils (3) répartis dans la matrice (2), les nanotubes ou nano-fils (3) étant juxtaposés et disposés de manière sensiblement parallèles à un axe (A) sensiblement perpendiculaire au plan (P) du composant, la matrice (2) comporte un matériau rigide (4) pour remplir les interstices et joindre les nanotubes ou nano-fils (3) les uns aux autres, le matériau (4) ayant des propriétés mécaniques rigides pour s'opposer à la déformation élastique du composant.

METHOD OF MANUFACTURING COMPOSITE MATERIAL WITH MAKROGETEROGENNOI STRUCTURE

SiC nanowire reinforced aluminum silicon carbide composite material and preparation method thereof

Manufacturing method for metal structural part, metal structural part and mobile terminal

Sputtering target structure

METHOD FOR FORMING METAL MATRIX COMPOSITE BODY BY OUTSIDE-IN SPONTANEOUS INFILTRATION PROCESS

PROCEDE DE FABRICATION D'ALUMINIUM OU D'ALLIAGES D'ALUMINIUM RENFORCES AVEC DE L'ALUMINE EN FIBRES OU FILAMENTS

Procédé de fabrication d'aluminium ou d'alliages d'aluminium renforcés par de l'alumine en fibres ou filaments cristallins. Ce procédé consiste à introduire, dans un moule contenant une couche de fibres ou de filaments d'alumine cristallins enchevêtrés, non modifiés, moule et son contenu qui ont été préchauffés à une température entre 700 et 1 050 degrés C, de l'aluminium fondu et/ou un alliage fondu d'aluminium avec un ou plusieurs autres éléments non-réactifs à l'égard de l'alumine à la température d'introduction ne dépassant pas 1050 degrés C, jusqu'à ce que la couche soit recouverte du métal fondu, à modifier la pression sur le contenu du moule pour vaincre la tension superficielle entre l'alumine et le métal fondu et pour assurer ainsi que le métal en fusion pénètre dans les interstices de la couche d'alumine, et à laisser le métal se solidifier au contact de ladite couche.

Metal objects reinforced by glass

Metal container comprising a carbonaceous.

COMPOSITE LIGHT METAL MATERIAL REINFORCES BY SILICON CONTINUOUS CARBIDE FIBRES

Support tooling for porous preforms to be infiltrated and furnace using such tooling

Preparing a masterbatch based on multi-walled carbon nanotubes, comprises contacting the nanotubes with a metal compound having a fusion point of specified value, and mechanically treating the obtained mixture

La présente invention concerne un procédé de préparation de mélanges-maîtres métalliques renfermant des nanotubes, notamment de carbone, les mélanges-maîtres ainsi obtenus et l'utilisation de ces mélanges-maîtres pour former des composites métalliques.

Manufactoring process of composite materials with metal matrix like device for its setting enoeuvre

Il est proposé un procédé de fabrication de matériaux composites à matrice métallique dans lequel un matériau de renforcement, se présentant comme une préforme, est infiltré, seul, avec un métal porté à l'état liquide par la fusion, sans traitement sous vide préalable de la préforme, par exposition à une pression de gaz et est laissé refroidir, sous pression.

METHOD FOR MANUFACTURING COMPOSITE MATERIAL PARTS BY IMPREGNATING WITH LOW MELTING TEMPERATURE

L'invention concerne un procédé de fabrication de pièce en matériau composite, comprenant les étapes de : - réalisation d'une préforme fibreuse consolidée, les fibres de la préforme étant des fibres de carbone ou de céramique et étant revêtues d'une interphase, - obtention d'une préforme fibreuse consolidée et partiellement densifiée, la densification partielle comprenant la formation sur l'interphase d'une première phase de matrice obtenue par infiltration chimique en phase gazeuse, et - poursuite de la densification par infiltration de la préforme fibreuse avec une composition d'infiltration contenant au moins du silicium et au moins un autre élément apte à abaisser la température de fusion de la composition d'infiltration à une température inférieure ou égale à 1150°C.

METAL MATRIX COMPOSITES, AND METHODS FOR MAKING THE SAME

A metal matrix composite article comprising a first metal and an insert reinforcing the first metal, wherein the first metal selected from the group consisting of aluminium, alloys thereof, and combinations thereof, wherein the insert comprises substantially continuous ceramic oxide fibers and a second metal selected from the group consisting of aluminium, alloys thereof, and combinations thereof, wherein the second metal secures the substantially continuous ceramic oxide fibers in place, wherein the second metal extends along at least a portion of the length of the substantially continuous ceramic oxide fibers, wherein there is an interface layer between the first metal and the insert, and wherein there is an interface layer peak bond strength value between the first metal and the insert of at least 100 MPa. Metal comprising inserts for reinforcing a metal matrix composite article and methods of making t he same. In another aspect, the present invention provides metal matrix composit e ...

THUS PRODUCED METHOD FOR THE FORMATION OF A COMPOSED BODY OF METAL MATRIX FOR A PROCESS OF SPONTANEOUS INFILTRATION EXTERNA-INTERNA AND PRODUCTS

METHOD FOR PREPARING A COMPOSITE MATERIAL AND USE OF A COMPOSITE MATERIAL PREPARED BY THE METHOD

Method for preparing a composite material and use of a composite material prepared by the method, which composite material is prepared from a molten material cast in a mold and a reinforcing material, in which method at least part of the reinforcing material is placed inside at least one support material inclosure and/or onto at least one support material layer, which support material is melted and most preferably evaporated in connection with casting the molten material in the mold, and the distribution of the reinforcing material within the molten material cast in the mold is controlled in a controlled way.

METAL MATRIX COMPOSITES, AND METHODS FOR MAKING THE SAME

Metal comprising inserts for reinforcing a metal matrix composite article and methods of making the same. In another aspect, the present invention provides metal matrix composite articles reinforced with an insert(s) and methods of making the same. Useful metal matrix composite articles comprising the inserts include brake calipers.

Composite material and method of producing the same, and composite metal material and method of producing the same

A method of producing a composite material which includes a carbon-based material and a particulate or fibrous metal material Z. The method includes steps (a) to (c). In the step (a), at least a first carbon material and the metal material Z mixed into an elastomer, and dispersing the first carbon material and the metal material Z by applying a shear force to obtain a composite elastomer, the metal material Z having a melting point lower than a melting point of the first carbon material. In the step (b), the composite elastomer is heat-treated to vaporize the elastomer to obtain an intermediate composite material including a second carbon material and the metal material Z. In the step (c), the intermediate composite material is heat-treated together with a substance including an element Y having a melting point lower than the melting point of the metal material Z to vaporize the substance including the element Y.

Process for producing an MG-based composite material or an MG alloy-based composite material

This invention provides a process which permits impurity-free sound Mg-based composite materials and Mg alloy-based composite materials to be efficiently and inexpensively produced without pressurizing a melt of matrix metal and without using a metal oxide, finely divided metal or metal fluoride. Specifically, it provides a process for producing an Mg-based composite material or an Mg alloy-based composite material which comprises replacing the gas within a mass of reinforcing material (9) by a non-protective gas, and bringing at least a part of the mass of reinforcing material (9) into contact with a melt (7) of Mg or Mg alloy so as to infiltrate the melt (7) into the mass of reinforcing material (9).

Method of manufacturing metal-carbon nanocomposite material

A method of manufacturing a metal-carbon nanocomposite material in which aluminum is used as the matrix is disclosed. The manufacturing method comprises mixing a Si-coated carbon nanomaterial (30) and a powdered Mg material (33), heating the mixture to a melting point of the Mg material or higher, and thereafter cooling the mixture to obtain an Mg-carbon nanomaterial (34). A metal-carbon nanomaterial in which Al is used as the matrix is provided by cooling the Mg-carbon nanomaterial and molten Al (40) in a mixed state.

CARBON COMPOSITES, METHODS OF MANUFACTURE, AND USES THEREOF

КОМПОЗИЦИЯ АЛЮМИНИЕВОГО СПЛАВА С УЛУЧШЕННЫМИ МЕХАНИЧЕСКИМИ СВОЙСТВАМИ ПРИ ПОВЫШЕННОЙ ТЕМПЕРАТУРЕ

Изобретение относится к композиционным материалам с матрицей из алюминиевого сплава. Композитный материал на основе алюминиевого сплава содержит матрицу из алюминиевого сплава, содержащего, мас.%Si 0,50-1,30, Fe 0,2-0,60, Cu 0,15 максимум, Mn 0,5-0,90, Mg 0,6-1,0, Cr 0,20 максимум, остальное - алюминий и неизбежные примеси, и частицы присадочного материала, диспергированные в матрице, причем присадочный материал содержит керамический материал. При этом сплав имеет избыток магния по отношению к тому количеству, которое входит в выделения фазы Mg-Si. Способ получения композитного материала включает получение расплава упомянутого алюминиевого сплава, добавление частиц присадочного материала в расплавленный алюминиевый сплав с получением расплавленной смеси и отливку расплавленной смеси с получением композитного материала, содержащего алюминиевый сплав в качестве материала матрицы и присадочный материал, диспергированный в матрице. Изобретение направлено на получение композиционного материала с высокими механическими свойствами при повышенных температурах. 3 н. и 23 з.п. ф-лы, 5 ил., 5 табл., 1 пр. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 673 270 C2 (51) МПК C22C 21/08 (2006.01) C22C 1/10 (2006.01) C22C 32/00 (2006.01) C22C 1/02 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 21/08 (2006.01); C22C 1/10 (2006.01) (21)(22) Заявка: 2016101213, 19.06.2014 (24) Дата начала отсчета срока действия патента: Дата регистрации: (73) Патентообладатель(и): РИО ТИНТО АЛКАН ИНТЕРНЭШНЛ ЛИМИТЕД (CA) 23.11.2018 (56) Список документов, цитированных в отчете о поиске: WO 2013/133978 A1, 12.09.2013. WO 19.06.2013 US 61/836,953; 31.03.2014 US 61/972,767 (43) Дата публикации заявки: 24.07.2017 Бюл. № 21 2004/038050 A2, 06.05.2004. SU 1838441 A3, 30.08.1993. JP 4541969 B2, 08.09.2010. RU 2296804 C1, 10.04.2007. (45) Опубликовано: 23.11.2018 Бюл. № 33 C 2 C 2 (85) Дата начала рассмотрения заявки PCT на национальной фазе: 19.01. ...

ДЕТАЛЬ ИЗ КОМПОЗИТНОГО МАТЕРИАЛА С МЕТАЛЛИЧЕСКОЙ МАТРИЦЕЙ, ПРОЯВЛЯЮЩАЯ ПОВЫШЕННЫЕ ЖЕСТКОСТЬ И СТОЙКОСТЬ В ПРОДОЛЬНОМ НАПРАВЛЕНИИ

Изобретение относится к изготовлению деталей из композитного материала, которые могут быть использованы в космической промышленности и в других областях. Предложена деталь из композитного материала с металлической матрицей, имеющая удлиненную форму в заданном направлении, содержащая матрицу из сплава на основе алюминия и углеродные волокна, уложенные последовательными слоями параллельно заданному направлению. При этом матрица из сплава на основе алюминия составляет 35-45 об.% изделия, а непрерывные углеродные волокна 55-65 об.%. По меньшей мере 90% волокон являются высокомодульными волокнами с модулем Юнга не меньше 650 ГПа. 25-60% слоев материала содержат высокомодульные углеродные волокна, ориентированные под углом 0±5o к заданному направлению, а в остальных слоях высокомодульные углеродные волокна ориентированы под углом ±20 - ±40o к заданному направлению. Техническим результатом является получение детали, имеющей высокие жесткость, стойкость и высокую размерную стабильность. 2 с. и ...

Способ получения углеграфитового композиционного материала

Изобретение относится к области металлургии, а именно к созданию композиционных материалов пропиткой пористого каркаса. Способ получения углеграфитового композиционного материала включает вакуумную дегазацию пористой углеграфитовой заготовки в растворе медного электролита. Наносят на заготовку двухслойное гальваническое покрытие, содержащее внутренний медный слой. Пропитывают пористую заготовку расплавом матричного сплава алюминия под воздействием избыточного давления за счет термического расширения расплава при нагреве выше температуры ликвидус сплава алюминия. При этом наружный слой гальванического покрытия выполняют из свинца, нанесенного электролизом из электролита, содержащего 200 г/л свинца борфтористого, 50 г/л борфтористоводородной кислоты и 1,0 г/л столярного клея. Техническим результатом изобретения является повышение качества композиционных материалов. 1 табл.

СПОСОБ ИЗГОТОВЛЕНИЯ КОМПОЗИЦИОННОГО МАТЕРИАЛА

FIELD: production of composite and laminated materials strengthened with continuous or elongate filaments and/or threads. SUBSTANCE: method involves making blank from reinforcing material by placing nonsintered tape, strip, sheet or web containing continuous longitudinally oriented filaments or threads spaced one from another by uniformly distributed particles connected by resilient binder; removing or reprocessing the major part of binder; filling cavities and voids with matrix material, when required. Manufacture of composite materials and plastics reinforced with cut and oriented filaments and/or threads involves grinding of nonsintered tape or narrow strip; mixing ground tape or strip with binder, lubricant and/or matrix material and forming product from this mixture by any method. EFFECT: increased efficiency, wider operational capabilities and improved quality of products. 13 cl 6ссСс760с ПЧ Го РОССИЙСКОЕ АГЕНТСТВО ПО ПАТЕНТАМ И ТОВАРНЫМ ЗНАКАМ (19) (51) МПК ВИ” 2 094 229 ' 13) СЛ В 29 С 67/20, 70/00, В 29 В 11/16, С 22 С 1/09 12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ РОССИЙСКОЙ ФЕДЕРАЦИИ (21), (22) Заявка: 92016476/04, 25.06.1991 (30) Приоритет: 29.06.1990 ЕР 90201719.3 (46) Дата публикации: 27.10.1997 (56) Ссылки: Волоконные композиционные материалы / Под ред. Дж.Уитона и З.Скала. - М.: Металлургия, 1918, с. 14 - 17, 20, 52 - 69, ЗЗ и 84, 98 и 134. Композиционные материалы в конструкции летательных аппаратов / Под ред. А.Л.Абибова. - М.: Машиностроение, 19715, с. 254 - 263. (86) Заявка РСТ: МЕ 91/00109 (25.06.91) (71) Заявитель: Флекслайн Сервисиз Лтд. (СУ), Гей Герард Де Ягер (М) (72) Изобретатель: Гей Герард Де Ягер[МЕ] (73) Патентообладатель: Флекслайн Сервисиз Лтд. (СУ), Гей Герард Де Ягер (М) (54) СПОСОБ ИЗГОТОВЛЕНИЯ КОМПОЗИЦИОННОГО МАТЕРИАЛА (57) Реферат: Изобретение касается изготовления композиционных и слоистых материалов, усиленных непрерывными или длинными волокнами и/или нитями. Сущность изобретения заключается В последовательных стадиях: (а) формование ...

КОМПОЗИТНЫЙ МАТЕРИАЛ С АЛЮМИНИЕВОЙ МАТРИЦЕЙ И УГЛЕРОДНЫМ ВОЛОКНОМ И СПОСОБ ЕГО ПОЛУЧЕНИЯ.

Группа изобретений относится к области химической промышленности и может быть использована при изготовлении композитных материалов с металлической матрицей и углеродным волокном. Способ получения композитного материала включает пропитку углеродного волокна с барьерным покрытием жидким алюминием или его сплавом. Нанесение барьерного покрытия на углеродное волокно 2 проводят в емкости с золем на основе осаждаемого оксида 4. Во время обработки на углеродное волокно 2 с помощью токопроводящего ролика 3 подают отрицательный потенциал, при этом в емкость с золем погружают электрод 5 с положительным потенциалом. Во время нанесения покрытия на углеродное волокно 2 золь обрабатывается ультразвуком с помощью ультразвукового волновода 6. После прохождения через емкость с золем волокно сматывается на принимающую катушку 7. Предложен также композитный материал. Технический результат заключается в обеспечении равномерного нанесения барьерного покрытия и повышении механической прочности композитного материала ...

Способ повышения проницаемости пор углеграфитовой заготовки

FIELD: metallurgy. SUBSTANCE: invention relates to metallurgy, namely to creation of composite materials with impregnation of porous frame, having high electric conductivity, antifriction properties, resistance in aggressive media. Method of producing coal-graphite composite material includes vacuum degassing of porous coal-graphite billet, its impregnation in impregnation chamber by molten matrix alloy under effect of excessive pressure due to thermal expansion of lead melt in pressure chamber at heating by 100 °C above the liquidus temperature of the matrix alloy simultaneously with the lead melt, wherein matrix alloy is copper-phosphorous alloy, degassing is carried out before immersing porous workpiece into melt of matrix alloy, and before impregnation porous workpiece is coated with two-layer galvanic coating consisting of internal copper and outer cadmium layers. EFFECT: technical result is improved quality of composite materials by increasing permeability of pores of graphite billet. 1 cl, 2 dwg, 1 tbl, 1 ex РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 688 471 C1 (51) МПК C22C 47/08 (2006.01) B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2019.02); B22F 3/26 (2019.02) (21)(22) Заявка: 2018101533, 16.01.2018 (24) Дата начала отсчета срока действия патента: Дата регистрации: 21.05.2019 (45) Опубликовано: 21.05.2019 Бюл. № 15 Адрес для переписки: 400005, г. Волгоград, пр. Ленина, 28, ВолгГТУ, отдел интеллектуальной собственности (73) Патентообладатель(и): Федеральное государственное бюджетное образовательное учреждение высшего образования "Волгоградский государственный технический университет" (ВолгГТУ) (RU) (56) Список документов, цитированных в отчете о поиске: RU 2539528 C1, 20.01.2015. US 2 6 8 8 4 7 1 R U (54) Способ повышения проницаемости пор углеграфитовой заготовки (57) Реферат: Изобретение относится к области одновременно с расплавом свинца, при этом в металлургии, а именно ...

Component, especially an automobile part or a cooling body for power electronics or fuel cells, is produced by positioning a binder-freed porous ceramic green body in a die casting die prior to light metal pressure infiltration

Die cast component production, by positioning a binder-freed porous ceramic green body in a die casting die prior to light metal pressure infiltration, is new. A component is produced by (a) pressing a mixture of ceramic powder with an organic binder and optionally inorganic and/or organic fillers and heating at \}1150 deg C to burn out the organic components without causing sintering and full consolidation of the ceramic material; (b) placing the resulting porous ceramic green body in a fixed position within a die casting die; and (c) infiltrating with a light metal melt at \}750 deg C and \}900 bars. An Independent claim is also included for a die cast component comprising metallic and non-metallic phases, especially produced by the above process, the metallic phase being a light metal or light metal alloy and the non-metallic phase being a ceramic phase, both phases being solidly bonded preferably as a three-dimension network.

Metallverbundmaterial und dessen Verfahren zur Herstellung

VERFAHREN ZUR HERSTELLUNG VON FORMLINGEN AUS KERAMISCHEN ODER METALLISCHEN FASERN

Mfr. of locally reinforced aluminium alloy composite material - by mixing silicon carbide whiskers with alloy powder, sintering then partially coating with thin aluminium film etc.

Al alloy composite material is produced by mixing SiC whiskers (10-50 microns dia. 0.1-5 microns and length 30-100 microns) and Al alloy powder and sintering to give a starting material. This is then partially coated with a thin Al film (min. purity 99%) some 0.5-20 microns thick by preheating the material to 20-100 deg.C below the solidus temp., then heating the matrix Al alloy 50 deg.C above its liquidus temp. Prod. is then placed in a mould and cast at a pressure of 250-3000 kg/cm2. USE/ADVANTAGE - For the internal combustion engine items, e.g. pistons, avoids problems associated with othr reinforcing systems, e.g. Al2O3 surface films gives good bond strength between matrix material and reinforcer. In an example, Al alloy powder (250 mesh size or less) was dispersed in water along with SiC whiskers (0.5 microns dia. and average length 20 microns), then filtered and dried to give a whisker content of 15%. This was heated to 600 deg.C and 5 x 10 power (-5) torr vacuum and sintered at a ...

Einzelzylinder bzw. Mehrzylinderblock.

Sputtertargetaufbau

Sputtertargetaufbau aus einer Halteplatte und einem durch eine Haftverbindung mit dieser verbundenen Sputtertarget, wobei die Halteplatte aus einem Material besteht, dessen Längenausdehnungskoeffizient von demjenigen des Materials des Sputtertargets um höchstens 2 × 10–6/K abweicht, und wobei eine Kupferplatte mit einer Dicke zwischen 0,3 und 1,5 mm an zumindest einer Flachseite der Halteplatte angeordnet ist.

PROCESS FOR PRODUCING CYLINDRICAL REINFORCING FIBROUS MOLDING

Non-uniform reinforced cast pistons

A piston is manufactured by incorporating a reinforcement which is formed at least in part by a fibre material and which is so non-uniform as to provide differing characteristics in the cast piston in predetermined differing regions of the piston. For example, the volumetric density of the fibres may be different in one region of the reinforcement as compared with another region in order to produce a more resistant region in the cast piston. Additionally or alternatively, the reinforcement may hold finely divided materials which combine with the piston material during casting to give improved properties. Examples of this are the incorporation of particles of silicon, silicon carbide or silicon nitride to improve wear and/or the incorporation of molybdenum disulphide and tungsten disulphide or graphite to improve lubrication.

A method for producing glass-reinforced metal articles

... 846,778. Casting composite articles. OWENSCORNING FIBERGLAS CORPORATION. Nov. 5, 1957 [Nov. 21, 1956], No. 34470/57. Class 83 (1). Glass-reinforced metal articles are made by forcing metal under pressure into contact with the fibrous glass reinforcement. Glass fibres 21, Fig. 1, are drawn from a glass-melting tank 20, are coated with molten metal such as aluminium from an applicator 23, and are wound on a collet 24 into a preform of metal-coated glass 27, Fig. 4, which is placed in a centrifugal casting mould. The mould may be heated to melt the metal, or additional molten metal may be added. The metal collet itself may form part of the preform- and be melted during the casting operation. In a modification, Fig. 5, a tube 34 containing fibrous &c. glass reinforcement 35 is supported in a rotatable mould 31, in packing material 36. A counterweight 37 is provided. The mould is rotated, and metal is poured into the tube 34. In a further modification, Fig. 6, bare or metal-coated glass fibres ...

Manufacture of controlled rate dissolving materials

METAL MATRIX COMPOSITES

Improved fibre metal compacts and method of making same

A metal compact is formed of a matted and sintered mass of metal fibres, the fibres being united by autogenous bonds at their junctions, the sintered skeleton having been subsequently treated with a substance of different composition from that of the fibres so as to at least partially coat and fill the pores of the skeleton. The subsequent treatment may consist of impregnating with liquid metals or alloys, e.g. a stainless steel fibre skeleton may be impregnated with molten magnesium, steel or molybdenum fibre skeletons impregnated with babbitt metal, ferrous fibre skeletons with copper, or tungsten carbide with cobalt, nickel or their alloys. The skeleton may be impregnated with comminuted metals or alloys, e.g. molybdenum skeletons impregnated with silver copper or aluminium powder, stainless steel with magnesium powder or ferrous skeletons with copper powder. The metal skeletons may be impregnated with carbonaceous or resinous compounds. Thus polytetrafluorethylene may be used in stainless ...

LIGHT METAL MATRIX COMPOSITE MATERIALS REINFORCED SILICON CARBIDE FIBRES AND A METHOD FOR PRDUCING SAID COMPOSITE MATERIALS

Improvements in the production of rolled products

A composite metal sheet or plate is manufactured by completely immersing an assembly of parallel metal core sheets in molten metal at a lower melting point than the metal of the core sheets, and after the molten metal has solidified to form a composite ingot reducing the thickness of the ingot by hot rolling in a direction generally normal to the planes of the core sheets. The method has a particularly useful but by no means exclusive application in the production of reinforced aluminium alloy sheets and plates. The sheets may be initially secured in parallel relationship by metal straps. A continuous casting method may be employed to produce the ingot. ...

PROCEDURE FOR THE PRODUCTION OF METAL MATRIX COMPOSITE MATERIALS

FIBER-REINFORCED COMPOUND WIRE WITH ALUMINUM MATRIX, CABLE AND MANUFACTURING PROCESS

VERFAHREN UND VORRICHTUNG ZUR HERSTELLUNG VON METALL-MATRIX-VERBUNDWERKSTOFFEN

VERFAHREN ZUM HERSTELLEN EINER VORLEGIERUNG UND VERWENDUNG DERSELBEN

COMPOSITE MATERIALS WITH METAL MATRIX.

VERFAHREN ZUM HERSTELLEN VON METALL-MATRIX-VERBUNDWERKSTOFFEN

PROCEDURE FOR THE PRODUCTION OF VERBUNDWERKSTOFFK¯RPERN WITH METAL MATRIX, CONTAINING THREE-DIMENSIONAL INTERLACED CO STENCILS AND PRODUCTS OF IT.

METALLMATRIXVERBUNDDRAHTE, CABLE AND PROCEDURE

METAL MATRIX COMPOSITES

A METHOD OF OBTAINING BIMATERIAL PARTS BY MOULDING

MATRICES AND PRODUCTS PRODUCED THEREBY

METAL MATRIX COMPOSITES, AND METHODS FOR MAKING THE SAME

PROCESS FOR PRODUCING FIBER-REINFORCED METAL COMPOSITE MATERIAL

ROD OR PLATE-LIKE REFRACTORY COMPOSITE ALLOYS

PROCESS FOR FORMING METAL-CERAMIC COMPOSITES

... of the Invention A method is taught for the in-situ precipitation of ceramic materials in a metal matrix. By means of the solvent assisted reaction, metal-ceramic composites having highly superior properties may be obtained. The invention involves the reaction of the ceramic forming constituents in a metal solvent medium to provide very finely-dispersed ceramic particles in the metal matrix. Exemplary materials include titanium diboride in an aluminum matrix.

PROCESS FOR PRODUCING CYLINDRICAL REINFORCING FIBROUS MOLDING

A process for producing a cylindrical reinforcing fibrous molding which comprises the steps of: sealing openings at opposite ends of a cylindrical disintegratable mold having a porosity, immersing the mold into an aqueous solution of a molding material containing a reinforcing fiber and an inorganic binder, and depositing the molding material onto an outer peripheral surface of the mold by applying an suction within the mold to form a molding blank; pressing the molding blank against the mold to adjust the shape of the molding blank; heating and drying the molding blank; disintegrating the mold for removal; and firing the molding blank to partially bond the reinforcing fiber with the inorganic binder.

A METHOD FOR FORMING METAL MATRIX COMPOSITE BODIES CONTAINING THREE-DIMENSIONALLY INTERCONNECTED CO-MATRICES AND PRODUCTS PRODUCED THEREBY

The present invention relates to the formation of a metal matrix composite body by the spontaneous infiltration of a molten matrix metal into a three-dimensionally interconnected material. Moreover, the three-dimensionally interconnected material may contain filler material within at least a portion of its porosity. Particularly, an infiltration enhancer and/or an infiltration enhancer precursor and/or an infiltrating atmosphere are in communication with a filler material and/or a three-dimensionally interconnected material and/or a matrix metal at least at some point during the process, which permits molten matrix metal to spontaneously infiltrate the three-dimensionally interconnected material and any filler material contained within at least a portion of the porosity of the three-dimensionally interconnected material.

CARBON COMPOSITES, METHODS OF MANUFACTURE, AND USES THEREOF

A carbon composite contains expanded graphite; and at least one of a filler or a reinforcement; wherein the expanded graphite comprises a plurality of randomly oriented basal planes. Methods of making the carbon composite and articles comprising the carbon composite are also disclosed.

COOLED REFRACTORY STRUCTURE AND MANUFACTURING PROCESS THEREFOR

The structure consists of a composite material having a reinforcement texture and a matrix. The composition of the matrix varies practically without discontinuity, in the structure's thickness direction, from an essentially refractory material (13) in the region of the front face intended to be exposed to very high temperatures, up to a material that is essentially heat conductive (16). Cooling fluid circulation conduits (15) can be arranged within the structure at a portion where the matrix is essentially heat conductive.

MOLDING PROCESS FOR BIMETAL SHAPES

L'invention est relative à un procédé d'obtention par moulage de pièces bimatériaux formées par deux alliages d'aluminium dont l'un constitue l'âme et l'autre la matrice. Ce procédé consiste à mettre en oeuvre une âme, contenant éventuellement un squelette réfractaire, à enlever la couche naturelle d'alumine présente à la surface de l'âme, à revêtir immédiatement après l'ensemble ainsi obtenu d'un film imperméable aux gaz d'un métal tel que le nickel, à placer l'ensemble revêtu dans un moule que l'on remplit avec l'alliage de la matrice à l'état fondu à une température telle qu'au moins 30% de l'âme soit refondue superficiellement. Elle trouve son application dans la confection de pièces automobiles telles que les culasses de moteurs et l'insertion de conduits dans les pièces aéronautiques.

PROCESS FOR MANUFACTURING REINFORCED COMPOSITES AND FILAMENT MATERIAL FOR USE IN SAID PROCESS

... 2086328 9200182 PCTABS00010 This invention relates to a process for manufacturing composites and laminates reinforced with continuous or long fibers and/or filaments, which comprises the subsequent steps of (a) forming a preform of reinforcing material by arranging a green tape, ribbon, sheet or cloth comprising a number of continuous longitudinally oriented fibers or filaments which are spaced from each other by means of uniformly distributed particles, bonded by means of a flexible binder, (b) removing or converting the major part of the binder and, if applicable, (c) filling the voids and cavities with matrix material. Further, this invention relates to a process for manufacturing composites and laminates reinforced with chopped-aligned fibers and/or filaments, which comprises chopping a green tape or ribbon as defined above, mixing the chopped tape or ribbon with a binder, lubricant and/or matrix material and forming mouldings from this mixture by any moulding method.

CERAMIC PREFORMS, MAKING PROCESS AND APPLICATIONS THEREOF

L'invention a pour objet des préformes en céramiques. Ces préformes comprennent des plaquettes hexagonales d'alumine .alpha.. Leur procédé de fabrication comprend la mise en oeuvre d'alumine amorphe, de transition ou hydratée et d'un fondant fluoré. Ces préformes sont utilisables telles quelles ou pour la fabrication de composites.

METAL MATRIX COMPOSITE COMPOSITION AND METHOD

C-4285 METAL MATRIX COMPOSITE COMPOSITION AND METHOD of the Invention A new metal matrix composite of an aluminum based alloy and a ceramic, and a method of making it are provided. In the preferred method, the ceramic is silicon carbide whiskers which are heated to an elevated temperature, generally in the range of between about 750.degree.F and 2000.degree.F. An alloy, comprising by weight about 3 to 6 percent copper, about 0.5 to 5 percent magnesium and the balance essentially aluminum, is heated to melt the alloy. The heated silicon carbide and molten alloy are mixed or intermingled. The intermingled silicon carbide and molten alloy are then cooled at a rate sufficient to sustain supersaturation of the copper and magnesium in the aluminum down to a predetermined temperature. The predetermined temperature is selected so as to permit precipitation of a strengthening copper-rich secondary metallic phase containing copper, magnesium and aluminum and consisting essentially of about 40 to ...

ALUMINIUM MATRIX COMPOSITE MATERIAL AND PROCESS OF PRODUCING SAME

The invention relates to an aluminium matrix composite material consisting of a porous fibre preform which is embedded in an aluminium alloy and which has a higher strength and an improved wear behaviour as compared to the aluminium matrix, wherein the fibre preform consists of a shaped fibre member which comprises a metallic and/or intermetallic structure and into which there is infiltrated a silicon-containing aluminium alloy melt, with the Si-content of the melt amounting to 5 - 14 % by weight. Furthermore, the invention relates to a process of producing an aluminium matrix composite material which consists of a porous fibre preform infiltrated with an aluminium alloy.

Fiber-containing composites

Provided in one embodiment is a method for producing a composition, comprising: heating a first material comprising an amorphous alloy to a first temperature; and contacting the first material with a second material comprising at least one fiber to form a composition comprising the first material and the second material; wherein the first temperature is higher than or equal to a glass transition temperature (T g ) of the amorphous alloy.

COPPER-BASED SUBSTANCES WITH NANOMATERIALS

A composition-of-matter is described herein comprising copper or an alloy thereof, and at least one nanocompound dispersed in the copper or an alloy thereof, wherein the copper or an alloy thereof is a cast metal. Further described herein are articles of manufacture comprising the composition-of-matter, and a process for preparing such a composition-of-matter, by dispersing at least one nanocompound in a melt of copper or and alloy thereof, and cooling the melt. 1. A composition-of-matter comprising copper or an alloy thereof , and at least one nanocompound dispersed in said copper or an alloy thereof , wherein said copper or an alloy thereof is a cast metal.2. The composition-of-matter of claim 1 , comprising a chill zone claim 1 , a columnar zone and an equiaxed zone.3. The composition-of-matter of claim 1 , wherein said cast metal is a sand-cast metal or a permanent mold-cast metal.4. The composition-of-matter of claim 1 , wherein said nanocompound comprises a substance selected from the group consisting of an oxide claim 1 , a nitride claim 1 , a carbon nitride claim 1 , a carbide and/or a carbon-based nanocompound.5. The composition-of-matter of claim 4 , wherein said nanocompound comprises a substance selected from the group consisting of boron nitride claim 4 , titanium nitride claim 4 , titanium carbon nitride claim 4 , titanium carbide claim 4 , silicon carbide claim 4 , tungsten carbide claim 4 , aluminum oxide claim 4 , titanium oxide claim 4 , zinc oxide claim 4 , aluminum diboride claim 4 , and titanium diboride.6. The composition-of-matter of claim 4 , wherein said carbon-based nanocompound comprises carbon in a form selected from the group consisting of diamond claim 4 , graphite claim 4 , graphene claim 4 , and a carbon nanotube.7. The composition-of-matter of claim 1 , wherein said nanocompound comprises a carbon nanotube and/or an inorganic nanotube claim 1 , said nanotube being a single-walled or multi-walled nanotube.8. The composition of claim 7 ...

Manufacture of Controlled Rate Dissolving Materials

A castable, moldable, or extrudable structure using a metallic base metal or base metal alloy. One or more insoluble additives are added to the metallic base metal or base metal alloy so that the grain boundaries of the castable, moldable, or extrudable structure includes a composition and morphology to achieve a specific galvanic corrosion rates partially or throughout the structure or along the grain boundaries of the structure. The insoluble additives can be used to enhance the mechanical properties of the structure, such as ductility and/or tensile strength. The insoluble particles generally have a submicron particle size. The final structure can be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final structure as compared to the non-enhanced structure. 125-. (canceled)26. A metal cast structure that includes a base metal material and a plurality of particles disbursed in said metal cast structure to obtain a desired dissolution rate of said metal cast structure , said particles having a melting point that is greater than a melting point of said base metal material , said particles constitute about 0.1-40 wt. % of said metal cast structure , said particles have a different galvanic potential from said base metal material , said base metal material is a magnesium alloy or an aluminum alloy , said particles including one or more materials selected from the group consisting of iron , copper , titanium , zinc , tin , cadmium , lead , beryllium , nickel , carbon , iron alloy , copper alloy , titanium alloy , zinc alloy , tin alloy , cadmium alloy , lead alloy , beryllium alloy , and nickel alloy.27. The metal cast structure as defined in claim 26 , wherein said base metal material includes a majority weight percent magnesium.28. The metal cast structure as defined in claim 26 , wherein said particles resist forming compounds with said base metal material due to a solubility ...

FIBER-CONTAINING COMPOSITES

Provided in one embodiment is a method for producing a composition, comprising: heating a first material comprising an amorphous alloy to a first temperature; and contacting the first material with a second material comprising at least one fiber to form a composition comprising the first material and the second material; wherein the first temperature is higher than or equal to a glass transition temperature (T) of the amorphous alloy. 1. A method for producing a composite , comprising:heating a structure to a first temperature, wherein the structure comprises a first material comprising an amorphous alloy and a second material comprising at least one fiber,pressurizing the structure to cause the first material to flow into the second material, andcooling the structure to form the composite,{'sub': g', 'x, 'wherein the first temperature is higher than or equal to the glass transition temperature (T) of the amorphous alloy and less than the crystallization temperature (T) of the amorphous alloy.'}2. The method of claim 1 , further comprising contacting the first material and the second material.3. A method for producing a composite claim 1 , comprising:heating a structure to a first temperature, wherein the structure comprises a first material and a second material comprising at least one fiber,pressurizing the structure to cause the first material to flow into the second material, andcooling the structure to form the composite,wherein the cooling the first material is at a first cooling rate sufficient to form an amorphous alloy in the first material and the first temperature is greater than the crystallization temperature (Tx) of the amorphous alloy.4. The method of claim 2 , wherein the contacting further comprises applying a pressure to the first material.5. The method of claim 1 , wherein the first temperature is lower than a melting temperature of the second material.6. The method of claim 2 , wherein the contacting results in substantially no chemical ...

Self-Actuating Device For Centralizing an Object

The invention is directed to the interventionless activation of wellbore devices using dissolving and/or degrading and/or expanding structural materials. Engineered response materials, such as those that dissolve and/or degrade or expand upon exposure to specific environment, can be used to centralize a device in a wellbore. 132-. (canceled)33. A centralizing device configured to be placed on , attached to , or combinations thereof an outside surface of a bore member , said centralizing device includes a body , an active material that includes one or more materials selected from the group consisting of an expandable material and a degradable material , and one or more well bore wall engagement members positioned in a non-deployed position , said one or more well bore wall engagement members including one or more structures selected from the group consisting of slat , wing , bow , leave , ribbon , extension and rib , said one or more well bore wall engagement members configured to move from said non-deployed position to a deployed position , said active configured to cause or to enable said one or more well bore wall engagement members to move from said non-deployed position to said deployed position , a maximum outer perimeter of said centralizing device is greater in size when said one or more well bore wall engagement members are in said deployed position as compared to when said one or more well bore wall engagement members are in said non-deployed position.34. The centralizing device as defined in claim 33 , wherein said active material includes said expandable material claim 33 , said expandable material configured to increase in volume when activated claim 33 , said increase in volume of said expandable material configured to provide a force that causes said one or more well bore wall engagement members to move or deform and thereby move from said non-deployed position to said deployed position.35. The centralizing device as defined in claim 33 , wherein said ...

Additive manufacturing of a component made from a metal matrix composite

The embodiments relate to a method for additive manufacturing of a component made from a metal matrix composite for a vehicle. In a step of the method, a plurality of elongated filaments is provided. In another step, metallic powder is provided. In a further step, the metal matrix composite component is additively manufactured by melting the metallic powder.

Galvanically-Active In Situ Formed Particles for Controlled Rate Dissolving Tools

A tastable, moldable, and/or extrudable structure using a metallic primary alloy. One or more additives are added to the metallic primary alloy so that in situ galvanically-active reinforcement particles are formed in the melt or on cooling from the melt. The composite contains an optimal composition and morphology to achieve a specific galvanic corrosion rate in the entire composite. The in situ formed galvanically-active particles can be used to enhance mechanical properties of the composite, such as ductility and/or tensile strength. The final casting can also be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final composite over the as-cast material. 1. A method of controlling the dissolution properties of a magnesium or a magnesium alloy comprising of the steps of:heating the magnesium or a magnesium alloy to a point above its solidus temperature;adding an additive to said magnesium or magnesium alloy while said magnesium or magnesium alloy is above said solidus temperature of magnesium or magnesium alloy to form a mixture, said additive including one or more first additives having an electronegativity of greater than 1.5, said additive constituting about 0.05-45 wt. % of said mixture;dispersing said additive in said mixture while said magnesium or magnesium alloy is above said solidus temperature of magnesium or magnesium alloy; and,cooling said mixture to form a magnesium composite, said magnesium composite including in situ precipitation of galvanically-active intermetallic phases.2. The method as defined in claim 1 , wherein said first additive has an electronegativity of greater than 1.8.3. The method as defined in claim 1 , wherein said magnesium or magnesium alloy is heated to a temperature that is less than said melting point temperature of at least one of said additives.4. The method as defined in claim 1 , wherein said additive includes one or more metals ...

Method and apparatus for the production of carbon fibre reinforced aluminium matrix composite wires

The invention relates to a method for the production of carbon fibre reinforced aluminium matrix composite wires by drawing carbon fibres through molten salt and molten aluminium in such a way that the molten aluminium and the molten salt are spatially separated, and the carbon fibres are drawn through first the molten salt, then the molten aluminium separated from it. The invention further relates to an apparatus for the implementation of the method. 1. A method for the production of carbon fibre reinforced aluminium matrix composite wires by drawing carbon fibres through molten salt and molten aluminium , characterized in that the molten aluminium and the molten salt are spatially separated , and the carbon fibres are drawn through first the molten salt , then the molten aluminium separated form it.2. The method according to claim 1 , characterized in that a temperature between 700-900° C. is used.3. The method according to claim 1 , characterized in that the molten salt is KTiF claim 1 , dissolved in a molten alkali halide.4. The method according to claim 3 , characterized in that the molten salt is an equimolar mixture of NaCl and KCl claim 3 , containing 10-20 wt % of KTiF5. The method according to claim 1 , characterized in that an air atmosphere at 1 bar pressure or an inert gas atmosphere at 1 bar pressure is used.6. The method according to claim 1 , characterized in that the length of stay of the carbon fibres in the molten salt and the molten aluminium is equal to or exceeds a critical value increasing quadratically with the increase in the diameter of the carbon fibre bundle.7. The method according to claim 6 , characterized in that for a carbon fibre bundle diameter of 2 mm the critical length of stay is about 6 s.834561172ab. An apparatus for the production of carbon fibre reinforced aluminium matrix composite wires claim 6 , the main parts of which are heatable containers for holding the molten salt and the molten aluminium claim 6 , and a supply reel ...

PREPARATION METHOD OF A LITHIUM-CONTAINING MAGNESIUM/ALUMINUM MATRIX COMPOSITE

The present invention relates to a preparation method of a lithium-containing magnesium/aluminum matrix composite. The preparation method is performed according to the following steps: (1) preparing magnesium ingots or aluminum ingots, preparing lithium metal, and preparing flux and reinforcements; (2) heating the flux to prepare flux melt, and adding the reinforcements to the flux melt to prepare a liquid-solid mixture; (3) pouring the liquid-solid mixture in a normal-temperature crucible, and performing cooling to obtain a precursor; (4) preheating a crucible, adding raw materials, and performing melting to form a raw material melt; (5) controlling a temperature of the raw material melt to 973-993K, adding the lithium metal, performing stirring, adding the precursor, performing stirring and mixing, raising temperature to 993-1013K, and performing standing; and (6) scumming operation should be carried out, and performing temperature casting on composite melt. 1. A preparation method of a lithium-containing magnesium/aluminum matrix composite , comprising the following steps:{'sub': 2', '3', '2', '2', '3', '2', '2, '(1) preparing magnesium ingots or aluminum ingots as raw materials, preparing lithium metal, and preparing flux and reinforcements, wherein the flux contains components in percentage by mass of 65%-85% of lithium chloride, 15%-35% of lithium fluoride and less than or equal to 20% of lithium bromide, the reinforcements are elemental metal powder, rare earth oxide, carbide, boride or metal oxide, the elemental metal powder is W, Mo or Ni, the rare earth oxide is LaO, CeOor YO, the carbide is TiC or SiC, the boride is ZrB, and the metal oxide is MgO or SiO, the reinforcements are 0.1%-30% of total volume of the raw materials, the reinforcements are 1%-50% of total volume of the flux, and the lithium metal is 0.1%-10% of total mass of the raw materials;'}(2) putting the flux into a clay crucible or a graphite crucible, performing heating to 673-773K to make ...

PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL

A composite material is provided having functionalized carbon nanotubes and a metal matrix. It is obtained by a process including dispersing functionalized carbon nanotubes or a mixture of functionalized carbon nanotubes and of at least one metal, in an open-pore or semi-open-pore metal foam, in order to form a composite structure, and compacting the composite structure obtained in the preceding stage in order to form the composite material in the form of a solid mass. 1. A composite material , wherein it has functionalized carbon nanotubes and a metal matrix , and it is obtained by a process comprising the steps of:i) dispersing functionalized carbon nanotubes or a mixture of functionalized carbon nanotubes and of at least one metal, in an open-pore or semi-open-pore metal foam, in order to form a composite structure;ii) compacting the composite structure obtained in the preceding stage i) in order to form said composite material in the form of a solid mass.2. The composite material according to claim 1 , wherein the metal foam is a syntactic foam or a metal sponge.3. The composite material according to claim 1 , wherein mixing functionalized carbon nanotubes and at least one metal is carried out according to a step a) prior to step i) by a liquid route claim 1 , by a solid route or by a molten route.4. The composite material according to claim 1 , wherein the at least one metal is chosen from copper claim 1 , aluminum claim 1 , a copper alloy claim 1 , an aluminum alloy and one of their mixtures.5. The composite material according to claim 1 , wherein the open-pore or semi-open-pore metal foam has a metal chosen from copper claim 1 , aluminum claim 1 , a copper alloy claim 1 , an aluminum alloy and one of their mixtures.6. The composite material according to claim 1 , wherein the metal foam is regular.7. The composite material according to claim 1 , wherein the metal foam comprises pores with a mean size ranging from 10 to 20 mm.8. The composite material according ...

Galvanically-Active In Situ Formed Particles for Controlled Rate Dissolving Tools

A castable, moldable, and/or extrudable structure using a metallic primary alloy. One or more additives are added to the metallic primary alloy so that in situ galvanically-active reinforcement particles are formed in the melt or on cooling from the melt. The composite contains an optimal composition and morphology to achieve a specific galvanic corrosion rate in the entire composite. The in situ formed galvanically-active particles can be used to enhance mechanical properties of the composite, such as ductility and/or tensile strength. The final casting can also he enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final composite over the as-cast material. 117-. (canceled)18. A magnesium composite that includes in situ precipitation of galvanically-active intermetallic phases comprising a magnesium or a magnesium alloy and an additive constituting about 0.05-45 wt. % of said magnesium composite , said magnesium having a content in said magnesium composite that is greater than 50 wt. % , said additive forming metal composite particles or precipitant in said magnesium composite , said metal composite particles or precipitant forming said in situ precipitation of said galvanically-active intermetallic phases , said additive including one or more first additives having an electronegativity of greater than 1.5.19. The magnesium composite as defined in claim 18 , further including one or more second additives having an electronegativity of less than 1.25.20. The magnesium composite as defined in claim 18 , wherein said first additive has an electronegativity of greater than 1.8 claim 18 ,2118. The magnesium composite as defined in claim 18 , wherein said first additive includes one or more metals selected from the group consisting of copper claim 18 , nickel claim 18 , cobalt claim 18 , bismuth claim 18 , silver claim 18 , gold claim 18 , lead claim 18 , tin claim 18 , antimony ...

Degradable and/or Deformable Diverters and Seals

A variable stiffness engineered degradable ball or seal having a degradable phase and a stiffener material. The variable stiffness engineered degradable ball or seal can optionally be in the form of a degradable diverter ball or sealing element which can be made neutrally buoyant. 1. A method of forming a temporary seal in a well formation that includes:a. providing a variable stiffness or deformable first degradable component capable of forming a fluid seal;b. combining said first degradable component with a fluid to be inserted into said well formation;c. inserting said fluid including said first degadable component into said well formation to cause said first degradable component to be positioned at or at least partially in an opening located in the well formation that is to be partially or fully sealed;d. causing said first degradable component located at or at least partially in said opening to deform to at least partially form a seal in said opening to partially or fully block or divert a flow of said fluid into and/or through said opening, said first degradable component at least partially deformed by fluid pressure of said fluid;e. optionally causing a plurality of said first degradable component to agglomerate with one another to at least partially form a seal in said opening so as to partially or fully block or divert a flow of said fluid into and/or through said opening, said plurality of said first degradable component at least partially agglomerated together by fluid pressure of said fluid;f. performing operations such as drilling, circulating, pumping, and/or hydraulic fracturing in said well formation for a period of time after said first degradable component has deformed and optionally agglomerated and has at least partially sealed said opening; and,g. causing said first degradable component to partially or fully degrade to cause said first degradable component to be partially or fully removed from said opening to thereby allow 80-100% of fluid flow ...

MANUFACTURING OF A METAL COMPONENT OR A METAL MATRIX COMPOSITE COMPONENT INVOLVING CONTACTLESS INDUCTION OF HIGH-FREQUENCY VIBRATIONS

The present invention relates to a system for contactless induction of high-frequency vibrations in a volume of molten metal () during the manufacturing of a metal component or a metal matrix composite component. The system comprises a moveably arranged electromagnetic primary coil (), adjustment means () for adjusting the position of the primary coil (), and a control unit () for controlling the position of the primary coil () to a predefined distance above and not in physical contact with an upper free surface () of the molten metal () during use of the system. In some embodiments of the invention the molten metal () is contained in a foundry crucible () during manufacturing. In other embodiments, the system is used for an additive manufacturing system, so that the primary coil () is arranged above the melt pool (). In both embodiments, a secondary low-frequency electromagnetic coil () may be arranged around and at a distance from the molten metal (). This secondary coil () is used to induce flow and/or vibrations in the molten metal () which is particularly useful during manufacturing of large components. 1. System for contactless induction of high-frequency vibrations in a volume of molten metal during the manufacturing of a metal component or a metal matrix composite component , the system comprising:a moveably arranged electromagnetic primary coil,adjustment means for adjusting the position of the primary coil, anda control unit for controlling the position of the primary coil to a predefined distance above and not in physical contact with an upper free surface of the molten metal during use of the system.2. System according to claim 1 , wherein the adjustment means comprises a sensor for measuring the distance between the primary coil and the upper free surface of the molten metal during use.3. System according to claim 1 , wherein the primary coil operates at an adjustable frequency in the order of 10 kHz.4. System according to claim 1 , wherein the primary ...

Method of making ceramic nanofibers

Continuous ceramic (e.g., silicon carbide) nanofibers ( 502, 602, 604, 606, 608, 702, 704, 1102, 1104 ) which are optionally p or n type doped are manufactured by electrospinning a polymeric ceramic precursor to produce fine strands of polymeric ceramic precursor which are then pyrolized. The ceramic nanofibers may be used in a variety of applications not limited to reinforced composite materials ( 400 ), thermoelectric generators ( 600, 700 ) and high temperature particulate filters ( 1200 ).

Metal matrix composites

A method of forming a metal matrix composite component comprises: providing a body defining a mould cavity; covering a first surface of the mould cavity with a first reinforcement material; restraining the first reinforcement material relative to the body to restrict movement of the first reinforcement material in the mould cavity; adding a second reinforcement material to the mould cavity, the second reinforcement material being in contact with the first reinforcement material; adding molten metal to the mould cavity such that the first reinforcement material and the second reinforcement material become embedded in a continuous metal matrix when the molten metal solidifies.

Turbomachine components manufactured with carbon nanotube comopsites

A turbomachine component and method for fabricating the turbomachine component are provided. The turbomachine component may include a matrix material and carbon nanotubes combined with the matrix material. The matrix material may include a metal or a polymer. The carbon nanotubes may be contacted with the metal to form a metal-based carbon nanotube composite, and the metal-based carbon nanotube composite may be processed to fabricate the turbomachine component.

PREPARATION METHOD FOR MAGNESIUM MATRIX COMPOSITE

The invention relates to a preparation method for a magnesium matrix composite. The preparation method comprises the following steps: (1) preparing magnesium ingots as raw materials and salt flux and reinforcements; (2) placing the salt flux in a crucible, performing heating to prepare salt flux melts, adding the reinforcements; (3) performing pouring into a normal-temperature crucible, and performing cooling to obtain precursors; (4) adding the raw materials in an iron crucible, and performing melting at 953K-1043K; (5) placing the precursors in raw material melt, after stirring, under a condition of 953K-993K, performing standing so that scum and melt are obtained; and (6) removing the scum, lowering temperature to 973K-982K, and performing casting. The method provided by the present invention is simple in process and low in cost. The method can be used for preparing bulk structural members of the magnesium matrix composite, and can be used for automatic production. 1. A preparation method for a magnesium matrix composite , comprising:{'sub': 2', '3', '2', '2', '3', '2', '2, '(1) preparing magnesium ingots as raw materials; preparing salt flux and reinforcements, wherein the salt flux is a mixture of barium chloride, magnesium chloride, sodium chloride and calcium chloride, the barium chloride accounts for 35-50% of a total mass of the salt flux, the magnesium chloride accounts for 10-20% of a total mass of the salt flux, the sodium chloride accounts for 10-20% of a total mass of the salt flux, a balance is the calcium chloride and impurities, the impurities account for no more than 1% of the total mass of the salt flux, the reinforcements are elementary metal, rare earth oxides, carbides, borides or metal oxides, the elementary metal is W, Mo or Ni, the rare earth oxides are LaO, CeOor YO, the carbides are TiC or SiC, the borides are ZrB, the metal oxides are MgO or SiO, the reinforcements are 0.1%-30% of a total volume of the raw materials, and the ...

Manufacture of Controlled Rate Dissolving Materials

A castable, moldable, or extrudable structure using a metallic base metal or base metal alloy. One or more insoluble additives are added to the metallic base metal or base metal alloy so that the grain boundaries of the castable, moldable, or extrudable structure includes a composition and morphology to achieve a specific galvanic corrosion rates partially or throughout the structure or along the grain boundaries of the structure. The insoluble additives can be used to enhance the mechanical properties of the structure, such as ductility and/or tensile strength. The insoluble particles generally have a submicron particle size. The final structure can be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final structure as compared to the non-enhanced structure. 1. A metal cast structure that includes a base metal or base metal alloy and a plurality of insoluble particles disbursed in said metal cast structure , said insoluble particles having a melting point that is greater than a melting point of said base metal or base metal alloy , at least 50% of said insoluble particles located in grain boundary layers of said metal cast structure.2. The metal cast structure as defined in claim 1 , wherein said insoluble particles have a selected size and shape to control a dissolution rate of said metal cast structure.3. The metal cast structure as defined in claim 1 , wherein said insoluble particles have different galvanic potential than a galvanic potential of said base metal or base metal alloy.4. The metal cast structure as defined in claim 3 , wherein said insoluble particles have said galvanic potential that is more anodic than said galvanic potential of said base metal or base metal alloy.5. The metal cast structure as defined in claim 3 , wherein said insoluble particles have said galvanic potential that is more cathodic than said galvanic potential of said base metal or base ...

HETEROGENEOUS COMPOSITION, ARTICLE COMPRISING HETEROGENEOUS COMPOSITION, AND METHOD FOR FORMING ARTICLE

A heterogeneous composition is disclosed, including an alloy mixture and a ceramic additive. The alloy mixture includes a first alloy having a first melting point of at least a first threshold temperature, and a second alloy having a second melting point of less than a second threshold temperature. The second threshold temperature is lower than the first threshold temperature. The first alloy, the second alloy, and the ceramic additive are intermixed with one another as distinct phases. An article is disclosed including a first portion including a material composition, and a second portion including the heterogeneous composition. A method for forming the article is disclosing, including applying the second portion to the first portion. 1. A heterogeneous composition , comprising: a first alloy having a first melting point of at least a first threshold temperature; and', 'a second alloy having a second melting point of less than a second threshold temperature, the second threshold temperature being lower than the first threshold temperature; and, 'an alloy mixture, includinga ceramic additive,wherein the first alloy, the second alloy, and the ceramic additive are intermixed with one another as distinct phases.2. The heterogeneous composition of claim 1 , wherein the first threshold temperature is about 2 claim 1 ,400° F. claim 1 , and the second threshold temperature is about 2 claim 1 ,350° F.3. The heterogeneous composition of claim 1 , wherein the first alloy is selected from the group consisting of a superalloy claim 1 , a hard-to-weld (HTW) alloy claim 1 , a refractory alloy claim 1 , a nickel-based superalloy claim 1 , a cobalt-based superalloy claim 1 , an iron-based superalloy claim 1 , an iron-based alloy claim 1 , a steel alloy claim 1 , a stainless steel alloy claim 1 , a cobalt-based alloy claim 1 , a nickel-based alloy claim 1 , a titanium-based alloy claim 1 , a titanium aluminide claim 1 , GTD 111 claim 1 , GTD 444 claim 1 , HAYNES 188 claim 1 , ...

Ceramic matrix composite components reinforced for managing multi-axial stresses and methods for fabricating the same

Ceramic matrix composite components and methods for fabricating ceramic matrix composite components are provided. In one example, a ceramic matrix composite component includes a ceramic matrix composite body. The ceramic matrix composite body includes a layer-to-layer weave of ceramic fibers and a layer of 1-directional and/or 2-directional (1D/2D) fabric of ceramic fibers disposed adjacent to the layer-to-layer weave. When stressed, the ceramic matrix composite body forms a relatively high through-thickness stress region and a relatively high in-plane bending stress region. The layer-to-layer weave is disposed through the relatively high through-thickness stress region and the layer of 1D/2D fabric is disposed through the relatively high in-plane bending stress region.

Self-Actuating Device For Centralizing an Object

The invention is directed to the interventionless activation of wellbore devices using dissolving and/or degrading and/or expanding structural materials. Engineered response materials, such as those that dissolve and/or degrade or expand upon exposure to specific environment, can be used to centralize a device in a wellbore.

SELF-ACTUATING DEVICE FOR CENTRALIZING AN OBJECT

The invention is directed to the interventionless activation of wellbore devices using dissolving and/or degrading and/or expanding structural materials. Engineered response materials, such as those that dissolve and/or degrade or expand upon exposure to specific environment, can be used to centralize a device in a wellbore. 1. A centralizing device that is configured to be positioned about an outer surface of a bore member , said centralizing device includes a body , an active material selected from the group consisting of an expandable material and a degradable material , and first and second of well bore wall engagement members , said first and second well bore wall engagement members include one or more structures selected from the group consisting of a slat , a wing , a bow , a leaf , a ribbon , an extension and a rib , said first and second well bore wall engagement members configured to move from a non-deployed position to a deployed position , said active material configured to cause said first and second well bore wall engagement members to move from said non-deployed position to said deployed position , a maximum outer perimeter of said centralizing device is greater in size when said first and second well bore wall engagement members are in said deployed position as compared to when said first and second well bore wall engagement members are in said non-deployed position , at least a portion of said first and second well bore wall engagement members positioned farther from a central axis of said body when in said deployed position than when said first and second well bore wall engagement members are in said non-deployed position.2. The centralizing device as defined in claim 1 , wherein said first and second well bore wall engagement members are formed of a bendable material and said expandable material claim 1 , said expandable material is connected to at least a portion of said bendable material claim 1 , said expandable material is configured to cause ...

NANOCARBON-REINFORCED ALUMINIUM COMPOSITE MATERIALS AND METHOD FOR MANUFACTURING THE SAME

A nanocarbon-reinforced aluminum composite material and a method of manufacturing the same are provided. The method of manufacturing a nanocarbon-reinforced aluminum composite material is characterized in that composite powder, in which ceramic-coated nanocarbon is surrounded by metal powder, is added to molten aluminum and then casting the molten aluminum with the added composite powder. 1. A method of manufacturing a nanocarbon-reinforced aluminum composite material , comprising:adding composite powder, in which ceramic-coated nanocarbon is surrounded by metal powder, to molten aluminum; andcasting the molten aluminum with the added composite powder.2. The method of claim 1 , further comprising steps of:prior to adding the composite powder to molten aluminum and casting the molten aluminum with the added composite powder,coating nanocarbon with ceramic; andmixing the ceramic-coated nanocarbon with metal powder to prepare the composite powder such that the ceramic-coated nanocarbon is surrounded by the metal powder.3. The method of claim 2 , wherein the nanocarbon includes at least one selected from the group consisting of carbon nanotube claim 2 , carbon nanofiber claim 2 , and graphene; andthe ceramic includes at least one selected from the group consisting of oxide, carbide, nitride, and boride.4. The method of claim 3 , wherein the metal powder is aluminum or a metal alloyed with the aluminum or reacted with the aluminum to form an intermetallic compound.5. The method of claim 1 , wherein the ceramic-coated nanocarbon is mixed with the metal powder by ball milling such that the ceramic-coated nanocarbon is surrounded by the metal powder.6. A nanocarbon-reinforced aluminum composite material claim 1 , manufactured by adding composite powder claim 1 , in which ceramic-coated nanocarbon is surrounded by metal powder claim 1 , to molten aluminum claim 1 , and then casting the molten aluminum with the added composite powder. The present application claims the ...

ALUMINUM ALLOY COMPOSITION WITH IMPROVED ELEVATED TEMPERATURE MECHANICAL PROPERTIES

An aluminum alloy includes, in weight percent, 0.50-1.30% Si, 0.2-0.60% Fe, 0.15% max Cu, 0.5-0.90% Mn, 0.6-1.0% Mg, and 0.20% max Cr, the balance being aluminum and unavoidable impurities. The alloy may include excess Mg over the amount that can be occupied by Mg—Si precipitates. The alloy may be utilized as a matrix material for a composite that includes a filler material dispersed in the matrix material. One such composite may include boron carbide as a filler material, and the resultant composite may be used for neutron shielding applications. 2. The alloy of claim 1 , wherein the unavoidable impurities may be present in an amount of up to 0.05 wt. % each and up to 0.15 wt. % total.3. The alloy of claim 1 , wherein the Cu content of the alloy is up to 0.1 max wt. %.4. The alloy of claim 1 , wherein the Si content of the alloy is 0.70-1.30 weight percent.5. The alloy of claim 1 , wherein the Mg content of the alloy is 0.60-0.80 weight percent.6. The alloy of claim 1 , wherein the alloy has excess magnesium over an amount that can be occupied by Mg—Si precipitates.7. The alloy of claim 6 , wherein the alloy has at least 0.25 wt. % excess magnesium.8. The alloy of claim 1 , wherein the alloy further includes up to 0.05 wt. % titanium.10. The composite material of claim 9 , wherein the filler material comprises a ceramic material.11. The composite material of claim 9 , wherein the filler material comprises boron carbide.12. The composite material of claim 11 , wherein the boron carbide filler material includes a titanium-containing intermetallic compound coating at least a portion of a surface thereof13. The composite material of claim 9 , wherein the filler material has greater neutron absorption and radiation shielding capabilities than the matrix.14. The composite material of claim 9 , wherein the filler material has a volume fraction of up to 20% in the composite material.15. The composite material of claim 9 , wherein the filler material has a higher hardness ...

METHOD AND APPARATUS FOR PRODUCING A MIXTURE OF A METALLIC MATRIX MATERIAL AND AN ADDITIVE

In a method for producing a mixture of a metallic matrix material and an additive, a metallic bulk material is molten in a multi-shaft screw machine in a heating zone thereof by means of an inductive heating device to form a metal matrix material. As the at least one housing portion of the housing of the multi-shaft screw machine is made of a non-magnetic and electrically non-conductive material at least partly in the heating zone, a high and efficient energy input for melting the metallic bulk material is achievable in a simple manner. The additive for producing the mixture is admixed to the metallic matrix material by means of treatment element shafts of the multi-shaft screw machine. 1. A method for producing a mixture of a metallic matrix material and an additive , the method comprising the following steps:providing a multi-shaft screw machine comprising a housing, a plurality of housing bores formed in the housing, at least one feed opening leading into the housing bores, a plurality of treatment element shafts arranged in the housing bores in such a way as to be drivable for rotation and an inductive heating device configured to form a heating zone, the housing comprising a plurality of interconnected housing portions arranged in succession in a conveying direction, at least one housing portion in the heating zone being made at least partially of a non-magnetic and electrically non-conductive material, the inductive heating device comprising at least one coil that surrounds the treatment element shafts and defines an inner space, the at least one housing portion being made exclusively of the non-magnetic and electrically non-conductive material in the inner space, the treatment element shafts comprising an electrically conductive material at least in the heating zone, the multi-shaft screw machine further comprising a cooling device configured to dissipate thermal losses generated in the at least one coil;feeding a metallic bulk material and an additive into ...

LOW CARBON STEEL AND CEMENTED CARBIDE WEAR PART

The present disclosure relates to a wear part having high wear resistance and strength and a method of making the same. The wear part is composed of a compound body of cemented carbide particles cast with a low-carbon steel alloy. The low-carbon steel alloy has a carbon content corresponding to a carbon equivalent Ceq=wt % C+0.3(wt % Si+wt % P) of about 0.1 to about 1.5 weight %. The wear part could include a body with a plurality of inserts of cemented carbide particles cast into a low-carbon steel alloy disposed in the body. Each of the plurality of cemented carbide inserts are coated with at least one layer of oxidation protection/chemical resistant material. The plurality of inserts are directly fixed onto a mold corresponding to the shape of the wear part. The cemented carbide inserts are then encapsulated with the molten low-carbon steel alloy to cast the cemented carbide inserts with the low-carbon steel alloy. 1. A wear part having high wear resistance and strength , comprising:a body composed of cemented carbide particles cast with a low-carbon steel alloy, wherein said low-carbon steel alloy has a carbon content corresponding to a carbon equivalent Ceq=wt % C+0.3(wt % Si+wt % P) of about 0.1 to about 1.5 weight percent.2. The wear part according to claim 1 , wherein the cemented carbide particles of the body are encapsulated by the low-carbon steel during casting to form a matrix.3. The wear part according to claim 1 , wherein the cemented carbide particles have a granular size that promotes a balance of heat capacity and heat conductivity between the low-carbon steel alloy and the cemented carbide particles for maximum wetting of the steel alloy onto the cemented carbide particles.4. The wear part according to claim 1 , wherein the volume of the cemented carbide particles is about 0.3 to about 20 cm3.5. The wear part according to claim 1 , further comprising at least one oxidation protection coating disposed on the cemented carbide particles.6. The wear ...

Device for producing a composite component formed from carbon fibers coated with pyrolytic carbon

The invention relates to a method for producing a composite component and to a composite component, the composite component being formed from a metal-matrix composite material made of carbon fibers and a metal or a metal alloy, a fiber composite being formed from the carbon fibers, a preform being formed from the fiber composite, the carbon fibers of the fiber composite being coated with pyrolytic carbon to form the preform, the preform being at least partially infiltrated with molten metal.

SACRIFICIAL 3-DIMENSIONAL WEAVING METHOD AND CERAMIC MATRIX COMPOSITES FORMED THEREFROM

A ceramic matrix composite (CMC) is formed using a three-dimensional (3-D) woven preform by removing the set of sacrificial fibers from the 3-D woven preform and allowing a metal or metal alloy infiltrate the 3-D woven preform. The 3-D woven preform is formed by a method that includes providing a woven layer comprising a first set of ceramic fibers oriented in a first (x) direction woven with a second set of ceramic fibers oriented in a second (y) direction; stacking a plurality of woven layers on top of each other, said woven layers providing a two-dimensional (2-D) preform; weaving a set of sacrificial fibers in a third (z) direction with the 2-D preform, said weaving providing the 3-D woven preform; and shaping the 3-D woven preform into a predetermined shape. 1. A method of forming a three-dimensional (3-D) woven preform for use in a ceramic matrix composite (CMC) , the method comprising:providing a woven layer comprising a first set of ceramic fibers oriented in a first (x) direction woven with a second set of ceramic fibers oriented in a second (y) direction;stacking a plurality of woven layers on top of each other, said woven layers providing a two-dimensional (2-D) preform;weaving a set of sacrificial fibers in a third (z) direction with the 2-D preform, said weaving providing the 3-D woven preform; andshaping the 3-D woven preform into a predetermined shape.2. The method according to claim 1 , wherein the first set of ceramic fibers and the second set of ceramic fibers comprise individual filaments or filament bundles that are the same or different in composition and/or diameter.3. The method according to claim 2 , wherein the first set of ceramic fibers and the second set of ceramic fibers are the same in composition and/or diameter.4. The method according to claim 1 , wherein the first set of ceramic fibers claim 1 , the second set of ceramic fibers claim 1 , and the sacrificial fibers are woven such that each are present in an amount that ranges between ...

High Conductivity Magnesium Alloy

A castable, moldable, or extrudable magnesium-based alloy that includes one or more insoluble additives. The insoluble additives can be used to enhance the mechanical properties of the structure, such as ductility and/or tensile strength. The final structure can be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final structure as compared to the non-enhanced structure. The magnesium-based composite has improved thermal and mechanical properties by the modification of grain boundary properties through the addition of insoluble nanoparticles to the magnesium alloys. The magnesium-based composite can have a thermal conductivity that is greater than 180 W/m-K, and/or ductility exceeding 15-20% elongation to failure.

METHOD FOR PROCESSING AT LEAST ONE CARBON FIBER, METHOD FOR FABRICATING A CARBON COPPER COMPOSITE, AND CARBON COPPER COMPOSITE

A method for processing at least one carbon fiber according to an embodiment may include: electroplating a first metal layer over at least one carbon fiber, wherein the first metal layer includes a metal which can form a common phase with carbon, electroplating a second metal layer over the first metal layer, wherein the second metal layer includes a metal which can form a common phase with the metal of the first metal layer, and annealing the at least one carbon fiber, the first metal layer, and the second metal layer so that the metal of the first metal layer forms a common phase with the carbon of the at least one carbon fiber at an interface between the first metal layer and the at least one carbon fiber and the metal of the first metal layer forms a common phase with the metal of the second metal layer at an interface between the first metal layer and the second metal layer. 1. A method for processing at least one carbon fiber , comprising:electroplating a first metal layer over at least one carbon fiber, wherein the first metal layer comprises a metal which can form a common phase with carbon;electroplating a second metal layer over the first metal layer, wherein the second metal layer comprises a metal which can form a common phase with the metal of the first metal layer; andannealing the at least one carbon fiber, the first metal layer, and the second metal layer so that the metal of the first metal layer forms a common phase with the carbon of the at least one carbon fiber at an interface between the first metal layer and the at least one carbon fiber and the metal of the first metal layer forms a common phase with the metal of the second metal layer at an interface between the first metal layer and the second metal layer.2. The method of claim 1 , whereinthe metal of the first metal layer is chromium or manganese and the metal of the second metal layer is nickel.3. The method of claim 2 , whereinthe annealing is performed at a temperature in the range from ...

High Conductivity Magnesium Alloy

A castable, moldable, or extrudable magnesium-based alloy that includes one or more insoluble additives. The insoluble additives can be used to enhance the mechanical properties of the structure, such as ductility and/or tensile strength. The final structure can be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final structure as compared to the non-enhanced structure. The magnesium-based composite has improved thermal and mechanical properties by the modification of grain boundary properties through the addition of insoluble nanoparticles to the magnesium alloys. The magnesium-based composite can have a thermal conductivity that is greater than 180 W/m-K, and/or ductility exceeding 15-20% elongation to failure. 123-. (canceled)24. A method for at least partially dissolving or degrading a down hole well structure in a well comprising the steps of:providing a down hole well structure, said down hole well structure at least partially dissolvable or degradable, said down hole well structure at least partially formed of a degradable or dissolvable magnesium-based composite, said degradable or dissolvable magnesium-based composite including a base metal and a plurality of insoluble nanoparticles, said base metal formed of a magnesium or magnesium alloy, said base metal including at least 70 wt. % magnesium, said insoluble nanoparticles having a melting point that is greater than a melting point of said base metal, said insoluble nanoparticles having a solubility of less than about 5% in said base metal, said insoluble nanoparticles constituting at least 0.1 vol. % of said magnesium-based composite, at least 50% of said insoluble nanoparticles located within 200 nm of grain boundaries or dislocations in said magnesium-based composite, said insoluble nanoparticles having an average thermal conductivity of above about 140 W/m-K, said magnesium-based composite having at least one ...

Method for producing boron nitride nanotube-reinforced aluminum composite casting, boron nitride nanotube-reinforced aluminum composite casting, and master batch for producing boron nitride nanotube-reinforced aluminum composite casting

Provided is a method for producing a boron nitride nanotube-reinforced aluminum composite casting, the method being capable of reducing cost. The method for producing a boron nitride nanotube-reinforced aluminum composite casting comprises the steps of: (a) mixing boron nitride nanotubes and a first aluminum matrix and then pelletizing the resulting mixture; (b) heating and subjecting pellets obtained in step (a) to melt mixing to obtain a melt; (c) cooling and solidifying the melt obtained in step (b) to obtain a master batch; and (d) subjecting the master batch obtained in step (c) and the second aluminum matrix to melt mixing, and then cooling and solidifying the resulting mixture.

Metal Matrix Composite Comprising Nanotubes And Method Of Producing Same

A metal matrix composite comprising nanotubes; a method of producing the same; and a composition, for example a metal alloy, used in such composites and methods, are disclosed. A method for continuously infiltrating nanotube yarns, tapes or other nanotube preforms with metal alloys using a continuous process or a multistep process, which results in a metal matrix composite wire, cable, tape, sheet, tube, or other continuous shape, and the microstructure of these infiltrated yarns or fibers, are disclosed. The nanotube yarns comprise a multiplicity of spun nanotubes of carbon (CNT), boron nitride (BNNT), boron (BNT), or other types of nanotubes. The element that infiltrates the nanotube yarns or fibers can, for example, be alloyed with a concentration of one or more elements chosen such that the resulting alloy, in its molten state, will exhibit improved wetting of the nanotube material. 1. A metal matrix composite , the composite comprising:a metal; anda plurality of nanotube reinforcements present in a volume fraction of between about 10% by volume and about 90% by volume of the metal matrix composite;the metal matrix composite comprising a continuous structure comprising the metal and the plurality of nanotube reinforcements.2. The metal matrix composite of claim 1 , wherein the plurality of nanotube reinforcements comprise at least one of carbon nanotubes claim 1 , boron nitride nanotubes claim 1 , boron nanotubes claim 1 , boron carbo-nitride nanotubes claim 1 , silicon nanotubes claim 1 , titanium oxide nanotubes and gallium nitride nanotubes.3. The metal matrix composite of or claim 1 , wherein the metal comprises at least one of copper claim 1 , aluminum claim 1 , silver claim 1 , gold claim 1 , tin claim 1 , cobalt claim 1 , nickel and iron.4. The metal matrix composite of any preceding claim claim 1 , wherein the plurality of nanotube reinforcements is present in a volume fraction of between about 40% by volume and about 60% by volume of the metal matrix ...

Galvanically-active in situ formed particles for controlled rate dissolving tools

A tastable, moldable, and/or extrudable structure using a metallic primary alloy. One or more additives are added to the metallic primary alloy so that in situ galvanically-active reinforcement particles are formed in the melt or on cooling from the melt. The composite contains an optimal composition and morphology to achieve a specific galvanic corrosion rate in the entire composite. The in situ formed galvanically-active particles can be used to enhance mechanical properties of the composite, such as ductility and/or tensile strength. The final casting can also be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final composite over the as-cast material.

Composite metal material and method of producing the same, caliper body, bracket, disk rotor, drum, and knuckle

A composite metal material includes a carbon-based material in a matrix of a metal-based material. The carbon-based material has a first bonding structure in which an element X bonds to a carbon atom on a surface of a carbon material. The matrix includes an amorphous peripheral phase containing aluminum, nitrogen, and oxygearound the carbon-based material. The element X includes at least one element selected from boron, nitrogen, oxygen, and phosphorus.

Composite metal material, a method of producing it and its use in brakes.

A composite metal material includes a carbon-based material in a matrix of a metal-based material. The carbon-based material has a first bonding structure in which an element X bonds to a carbon atom on a surface of a carbon material. The matrix includes an amorphous peripheral phase containing aluminum, nitrogen, and oxygearound the carbon-based material. The element X includes at least one element selected from boron, nitrogen, oxygen, and phosphorus.

Composite metal material and method of producing the same, caliper body, bracket, disk rotor, drum, and knuckle

A composite metal material includes a carbon-based material in a matrix of a metal-based material. The carbon-based material has a first bonding structure in which an element X bonds to a carbon atom on a surface of a carbon material. The matrix includes an amorphous peripheral phase containing aluminum, nitrogen, and oxygearound the carbon-based material. The element X includes at least one element selected from boron, nitrogen, oxygen, and phosphorus.

Carbon fiber composite material and method for producing the same, carbon fiber composite molded article and method for producing the same

Composite material and manufacturing method thereof, composite metal material and manufacturing method thereof

Composite metal material and method of producing the same

Carbon fiber-metal composite material and method of producing the same

Metal material and method of producing the same, and carbon fiber-metal composite material and method of producing the same

Composite metal material, a method of producing it and its use in brakes.

Composition material

Method of fabricating composite parts by low melting point impregnation

FIELD: technological processes.SUBSTANCE: invention relates to a method of fabricating a composite part, comprising the steps of: producing a consolidated fibrous preform, wherein the fibres of the preform being carbon fibres or ceramic fibres and being coated with an interphase, obtaining a consolidated and partially densified fibrous preform, wherein the partial densification comprises the formation of the first matrix phase on the interphase obtained by chemical vapour infiltration, and continuation of the densification by infiltration with an infiltration composition containing at least silicon and at least one other element capable of lowering the melting point of the infiltration composition to a temperature less than or equal to 1,150 °C. Infiltration composition, in addition to silicon, comprises 50–75 mass.% nickel or 89–98 mass.% germanium.EFFECT: expulsion of the destruction of the billet fibers in the process of manufacturing a part.11 cl, 1 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 668 431 C2 (51) МПК C04B 35/573 (2006.01) C04B 35/577 (2006.01) C04B 35/80 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C04B 35/573 (2006.01); C04B 35/62272 (2006.01); C04B 35/6286 (2006.01); C04B 35/62878 (2006.01); C04B 35/62884 (2006.01); C04B 35/62894 (2006.01); C04B 35/806 (2006.01); C04B 2235/614 (2006.01) (21)(22) Заявка: 2016105679, 15.07.2014 15.07.2014 Дата регистрации: 01.10.2018 (56) Список документов, цитированных в отчете о поиске: FR 2983193 A1, 31.05.2013. WO 23.07.2013 FR 1357238 (43) Дата публикации заявки: 29.08.2017 Бюл. № 25 2001/07377 A1, 01.02.2001. US 2006/0169404 A1, 03.08.2006. RU 2194683 C2, 20.12.2002. RU 2184715 C2, 10.07.2002. (45) Опубликовано: 01.10.2018 Бюл. № 28 C 2 C 2 (85) Дата начала рассмотрения заявки PCT на национальной фазе: 24.02.2016 (86) Заявка PCT: FR 2014/051821 (15.07.2014) 2 6 6 8 4 3 1 (87) Публикация заявки PCT: R U 2 6 6 8 4 3 1 (73) Патентообладатель(и): ...

Metal material and method of producing the same, and carbon fiber composite metal material and method of producing the same

본 발명은 카본 나노파이버가 균일하게 분산된, 금속 재료 및 그 제조 방법, 탄소 섬유 복합 금속 재료 및 그 제조 방법을 제공하는 데에 있다. The present invention provides a metal material, a method for producing the same, a carbon fiber composite metal material, and a method for producing the same, in which carbon nanofibers are uniformly dispersed. 금속 입자(50)의 주위에 상기 카본 나노파이버(40)가 분산된 금속 재료의 제조 방법은, 카본 나노파이버(40)에 대해서 친화성을 갖는 불포화 결합 또는 기를 갖는 엘라스토머(30)와, 금속 입자(50)와, 카본 나노파이버(40)를 혼합하고, 또한 전단력에 의해서 분산시켜서 탄소 섬유 복합 재료를 얻는 공정 (a)와, 탄소 섬유 복합 재료를 열 처리하여, 상기 탄소 섬유 복합 재료 중에 포함되는 엘라스토머(40)를 기화시키는 공정 (b)를 포함하는 것을 특징으로 한다. The method for producing a metal material in which the carbon nanofibers 40 are dispersed around the metal particles 50 includes the elastomer 30 having an unsaturated bond or group having affinity for the carbon nanofibers 40, and the metal particles. Step (a) of mixing the carbon nanofiber 40 with the carbon nanofiber 40 and dispersing it by shear force to obtain a carbon fiber composite material, and heat treating the carbon fiber composite material to be included in the carbon fiber composite material. It characterized in that it comprises a step (b) of vaporizing the elastomer (40).

包括陶瓷喇叭的超声能量系统和方法

一种用于施加振动能量的声学系统，包括连接到超声能量源的喇叭。喇叭限定了整体长度和波长，至少喇叭的前部包括陶瓷材料。该前部长度至少是1/8喇叭波长。在一个优选实施例中，喇叭整体是一种陶瓷材料，并通过过盈配合被安装到一单独部件，如波导管。无论如何，通过对喇叭的至少一特定部位使用陶瓷材料，本发明的超声系统有利于长时间工作在极端环境，如高温和/或腐蚀性流体介质。本发明对制造金属基质复合导线非常有用。

金属複合材の製造法

(57)【要約】本公報は電子出願前の出願データであるた め要約のデータは記録されません。

Fiber selected from glass, ceramic and metal and treatment of optional fiber coated therewith

一种纽扣电池引脚及其焊接的方法

本发明公开了一种纽扣电池引脚及其焊接的方法，具体涉及纽扣电池领域，该引脚包括导线，所述导线具体为单根线芯导线，所述导线由熔点与电池钢壳熔点接近的单金属或合金材料制成，所述导线通过焊针与电池钢壳焊接连接；引线加工后开始焊接：采用沥青基铝浆、矿物醇和水滑石制备封孔涂层，将封孔涂层涂覆在电池钢壳的焊接部位，采用电焊机，将导线与电池钢壳焊接，并且在焊接完成后，待温度降低到一定程度后，再次在焊接部位涂覆封孔涂层。本发明通过将引线设置为单根线芯导线，且采用的原料为熔点与电池钢壳熔点一至的金属或是合金材料，可将其直接焊接到电池钢壳上，焊接工艺简单，焊接强度高，引线不易断裂脱落，且体积小，节省空间。

Ｆｒｍ用プリフオ−ムワイヤ−，プリフオ−ムシ−トまたはテ−プの製造方法および該方法に用いられる超音波振動装置

(57)【要約】本公報は電子出願前の出願データであるた め要約のデータは記録されません。

一种含铬熔渗粉及其在铜铬硅改性炭/陶摩擦材料中的应用

本发明公开了一种含铬熔渗粉及其在铜铬硅改性炭/陶摩擦材料中的应用；属于新材料技术领域。本发明设计的含铬熔渗粉包含Cu、Cr、Si；其中Cu、Cr、Si的质量比为Cu∶Cr：Si＝(35～50)∶(25～55)：(40～60)。其应用为：首先对炭纤维预制体进行高温热处理后采用快速化学气相渗透法和(或)树脂浸渍/炭化进行致密化，制得低密度的炭/炭多孔体材料，然后采用非浸泡式熔融浸渗技术对炭/炭多孔体材料同时进行Si、Cr、Cu共渗，通过Si与C、Si与Cr及Si与Cu的反应复合成一体制得铜铬硅改性炭/陶摩擦材料。本发明制备工艺简单，所得产品性能优良，便于大规模的工业化应用。

Patent JPS6041136B2

Diamond-metallic composite material

FIELD: process engineering. SUBSTANCE: invention relates to powder metallurgy, particularly, to materials intended for production of diamond-metallic composite materials. It may be used as hard or abrasive material and for making centrifuge nozzles. Diamond particles are mixed with those of metallic filler to produce mix for moulding billet therefrom. Said billet is subjected to pre-sintering by heating to ≤500°C and impregnated with one or more wetting elements or one or more wetting alloys. Impregnation is performed in vacuum or in inert gas at <200 bar. EFFECT: higher density, thermal expansion, crack resistance and solderability. 22 cl, 2 tbl, 3 ex РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) 2 448 827 (13) C2 (51) МПК B24D 3/06 (2006.01) C22C 26/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (21)(22) Заявка: 2010123191/02, 30.10.2008 (24) Дата начала отсчета срока действия патента: 30.10.2008 (73) Патентообладатель(и): АЛЬФА ЛАВАЛЬ КОРПОРЕЙТ АБ (SE) R U Приоритет(ы): (30) Конвенционный приоритет: 08.11.2007 SE 0702474-8 (72) Автор(ы): ЧЕНЬ Цзе (SE) (43) Дата публикации заявки: 20.12.2011 Бюл. № 35 2 4 4 8 8 2 7 (45) Опубликовано: 27.04.2012 Бюл. № 12 (56) Список документов, цитированных в отчете о поиске: US 4246006 А, 20.01.1981. RU 2151814 С1, 27.06.2000. RU 2131347 С1, 10.06.1999. RU2113531 С1, 20.06.1998. US 5116568 А, 26.05.1992. GB 2006733 А, 10.05.1979. 2 4 4 8 8 2 7 R U (86) Заявка PCT: SE 2008/051235 (30.10.2008) C 2 C 2 (85) Дата начала рассмотрения заявки PCT на национальной фазе: 08.06.2010 (87) Публикация заявки РСТ: WO 2009/061265 (14.05.2009) Адрес для переписки: 129090, Москва, ул. Б. Спасская, 25, стр.3, ООО "Юридическая фирма Городисский и Партнеры" (54) АЛМАЗОМЕТАЛЛИЧЕСКИЙ КОМПОЗИТ (57) Реферат: Изобретение относится к порошковой металлургии, в частности к получению алмазометаллических композитов. Может использоваться в качестве твердого или абразивного материала, а также для изготовления сопел ...

Process for forming metal-second phase composites and product thereof

내용 없음. No content.

Method for increasing permeability of pores of graphite workpiece

Изобретение относится к области металлургии, а именно к созданию композиционных материалов пропиткой пористого каркаса, имеющих высокую износостойкость, антифрикционные свойства, стойкость в агрессивных средах. Способ получения углеграфитового композиционного материала включает вакуумную дегазацию пористой углеграфитовой заготовки, ее пропитку в камере пропитки расплавом матричного сплава под воздействием избыточного давления за счет термического расширения расплава свинца в камере давления при нагреве на 100°С выше температуры ликвидус матричного сплава одновременно с расплавом свинца, при этом в качестве матричного сплава используют сплав сурьмы, дегазацию проводят до погружения пористой заготовки в расплав матричного сплава, а перед пропиткой пористую заготовку покрывают гальваническим покрытием, состоящим из медного слоя. Техническим результатом изобретения является повышение качества композиционных материалов за счет увеличения проницаемости пор углеграфитовой заготовки. 2 ил., 1 табл., 1 пр. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 688 557 C1 (51) МПК C22C 47/08 (2006.01) B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2019.02) (21)(22) Заявка: 2018101549, 16.01.2018 (24) Дата начала отсчета срока действия патента: Дата регистрации: 21.05.2019 Приоритет(ы): (22) Дата подачи заявки: 16.01.2018 (56) Список документов, цитированных в отчете о поиске: RU 2529528 C1, 20.01.2015. RU (45) Опубликовано: 21.05.2019 Бюл. № 15 (54) Способ повышения проницаемости пор углеграфитовой заготовки (57) Реферат: Изобретение относится к области температуры ликвидус матричного сплава металлургии, а именно к созданию одновременно с расплавом свинца, при этом в композиционных материалов пропиткой качестве матричного сплава используют сплав пористого каркаса, имеющих высокую сурьмы, дегазацию проводят до погружения износостойкость, антифрикционные свойства, пористой заготовки в расплав матричного сплава ...

Patent JPS5312446B2

Containerless infiltration with electromagnetic levitation

The present invention is directed to new processes in which electromagnetic levitation forces are used to infiltrate a porous matrix with a solid infiltrant. In such processes, controlled heating of these components, melting the infiltrant while both components are subjected to levitation forces, and containerless transportation and subsequent contact of both components results in the infiltration of the porous matrix. Such containerless processing provides for infiltrated porous matrices which are free of contaminants generally introduced by the containers used in traditional methods of infiltration.

Method for producing carbon-graphite composite material

Изобретение относится к области металлургии, а именно к созданию углеграфитовых композиционных материалов с металлической матрицей, имеющих высокую электропроводность, антифрикционные свойства и стойкость в агрессивных средах. Способ получения углеграфитового композиционного материала включает вакуумную дегазацию пористой углеграфитовой заготовки в растворе никелевого электролита, содержащего 140 г/л сульфата никеля, 50 г/л сульфата натрия, 30 г/л сульфата магния, 20 г/л сухой борной кислоты, последовательное нанесение на нее гальванического покрытия, содержащего внутренний никелевый, промежуточный цинковый и наружный медный слои, и пропитку в камере пропитки расплавом матричного сплава сурьмы под воздействием избыточного давления за счет термического расширения расплава свинца в камере давления при его одновременном нагреве на 100°С выше температуры ликвидус матричного сплава сурьмы, причем углеграфитовую заготовку помещают в камеру пропитки при температуре расплава свинца в камере давления на 5-10°С ниже температуры ликвидус сплава свинца. Техническим результатом изобретения является повышение качества композиционных материалов. 1 пр., 1 табл. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 750 065 C1 (51) МПК C22C 47/08 (2006.01) C22C 49/02 (2006.01) C22C 49/14 (2006.01) C22C 101/10 (2006.01) B22F 3/26 (2006.01) C25D 5/10 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2021.02); C22C 49/02 (2021.02); C22C 49/14 (2021.02); B22F 3/26 (2021.02); C25D 5/10 (2021.02) (21)(22) Заявка: 2020142415, 22.12.2020 22.12.2020 21.06.2021 Приоритет(ы): (22) Дата подачи заявки: 22.12.2020 (45) Опубликовано: 21.06.2021 Бюл. № 18 2 7 5 0 0 6 5 R U (56) Список документов, цитированных в отчете о поиске: RU 2688538 C1, 21.05.2019. RU 2688555 C1, 21.05.2019. RU 2688779 C1, 21.05.2019. RU 2688557 C1, 21.05.2019. US 4341823 A1, 27.07.1982. (54) Способ получения углеграфитового композиционного материала (57) Реферат: ...

Method for increasing permeability of pores of graphite workpiece

FIELD: metallurgy.SUBSTANCE: invention relates to composite materials with porous carcass impregnation having high electrical conductivity, antifriction properties and resistance to aggressive media. Method of producing coal-graphite material involves vacuum degassing of porous coal-graphite billet, its impregnation in impregnation chamber of melt of matrix alloy under effect of excessive pressure due to thermal expansion of lead melt in pressure chamber at heating by 100 °C above the liquidus temperature of the matrix alloy simultaneously with the lead melt, wherein matrix alloy is copper-phosphorous alloy, degassing is carried out before immersing porous workpiece into melt of matrix alloy, and before impregnation porous workpiece is covered with two-layer galvanic coating consisting of internal copper and outer chromium layers.EFFECT: technical result is improved quality of composite materials by increasing permeability of pores of graphite billet.1 cl, 1 ex, 1 tbl, 2 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 688 527 C1 (51) МПК C22C 47/08 (2006.01) B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2019.02); B22F 3/26 (2019.02) (21)(22) Заявка: 2018101545, 16.01.2018 (24) Дата начала отсчета срока действия патента: 21.05.2019 Приоритет(ы): (22) Дата подачи заявки: 16.01.2018 (45) Опубликовано: 21.05.2019 Бюл. № 15 3956568 A1, 11.05.1976. US 4707299 A1, 17.11.1987. US 20120114874 A1, 10.05.2012. RU 2571295 C1, 20.12.2005. (54) Способ повышения проницаемости пор углеграфитовой заготовки (57) Реферат: Изобретение относится к области матричного сплава одновременно с расплавом металлургии, а именно к созданию свинца, при этом в качестве матричного сплава композиционных материалов пропиткой используют медно-фосфористый сплав, дегазацию пористого каркаса, имеющих высокую проводят до погружения пористой заготовки в электропроводность, антифрикционные свойства, расплав матричного сплава, а ...

Process for producing whisker-reinforced metal matrix composites by liquid-phase consolidation

A fiber-reinforced metal composite of desired shape is produced by consolidating a mixture of the metal matrix and the fibers under pressure with the mixture maintained at a temperature in which the matrix system is partly in the liquid phase and partly in the solid phase, utilizing a liquid-phase extrusion die cavity of predetermined volume. With approximately one quarter of the matrix system in the liquid phase, and containing up to approximately 50 percent by volume of oriented fibers or whiskers, the material of the composite billet is extruded into the die cavity in order to consolidate the composite billet to the volume of the die cavity, in which the desired shape is to be formed. Heating is discontinued when the cavity is filled completely by the semi-molten metal fiber composite.

Carbon Fiber Composite Material and Process for Producing the Same, Carbon Fiber Composite Product and Process for Producing the Same

본 발명은 카본 나노 화이버가 균일하게 분산된 탄소 섬유 복합 재료 및 그 제조 방법, 탄소 섬유 복합 성형품 및 그 제조 방법, 탄소 섬유 복합 금속 재료 및 그 제조 방법, 탄소 섬유 복합 금속 성형품 및 그 제조 방법을 제공한다. The present invention provides a carbon fiber composite material in which carbon nanofibers are uniformly dispersed, a method for producing the same, a carbon fiber composite molded article and a manufacturing method thereof, a carbon fiber composite metal material and a manufacturing method thereof, and a carbon fiber composite metal molded article and a manufacturing method thereof do. 탄소 섬유 복합 재료의 제조 방법은 카본 나노 화이버에 대하여 친화성을 갖는 불포화 결합 또는 기를 갖는 엘라스토머와 금속 입자를 혼합하는 공정과, 금속 입자를 포함하는 엘라스토머에 카본 나노 화이버를 전단력에 의해서 분산시키는 공정을 포함하는 것을 특징으로 한다. The method for producing a carbon fiber composite material includes mixing an elastomer having an unsaturated bond or a group having affinity for carbon nanofiber and a metal particle, and dispersing the carbon nanofiber by shearing force in the elastomer including the metal particle. It is characterized by including. 카본 나노 화이버, 엘라스토머 Carbon Nanofiber, Elastomer

Composite metal material and process for producing the same, caliper body, bracket, disk rotor, drum and knuckle

표면의 젖음성이 개선된 탄소계 재료를 포함하는 복합 금속 재료 및 그 제조 방법을 제공하는 데에 있다. 또한, 복합 금속 재료를 포함하는 재료에 의하여 형성된, 차량용 캘리퍼 바디, 브래킷, 디스크 로터, 드럼 및 너클을 제공하는 것으로서, 본 발명에 관한 복합 금속 재료는, 금속계 재료의 매트릭스 중에 탄소계 재료를 포함하는 복합 금속 재료이다. 탄소계 재료는, 탄소 재료의 표면을 구성하는 탄소 원자에, 원소 X가 결합된 제 1 결합 구조를 갖고 있다. 매트릭스는, 탄소계 재료의 주위에, 알루미늄, 질소 및 산소를 포함하는 비정질의 주변상을 포함한다. 원소 X는, 붕소, 질소, 산소, 인에서 선택된 적어도 하나를 포함한다. The present invention provides a composite metal material including a carbon-based material having improved surface wettability and a method of manufacturing the same. Also provided is a vehicle caliper body, bracket, disc rotor, drum, and knuckle formed by a material comprising a composite metal material, wherein the composite metal material according to the present invention comprises a carbon-based material in a matrix of the metal-based material. It is a composite metal material. The carbonaceous material has a first bonding structure in which an element X is bonded to a carbon atom constituting the surface of the carbon material. The matrix comprises an amorphous peripheral phase comprising aluminum, nitrogen and oxygen around the carbonaceous material. Element X includes at least one selected from boron, nitrogen, oxygen, phosphorus.

Reinforced pistons

Carbon fiber carbon composite molded body, carbon fiber reinforced carbon composite material, and method for producing the same

To obtain a carbon fiber-reinforced carbon composite material exhibiting excellent thermal conductivity in every direction in the plane containing the X and Y axes. A carbon fiber-carbon composite formed body in which a number of sheet-like dispersions containing pitch-based carbon fibers dispersed therein randomly in the plane containing the X and Y axes are laminated into a carbon fiber laminate, and pyrolytic carbon is deposited on the surfaces of the carbon fibers of the carbon fiber laminate to coat around the carbon fibers, whereby the carbon fiber laminate is filled with the pyrolytic carbon, and a carbon fiber-reinforced carbon composite material obtained using the carbon fiber-carbon composite formed body.

Composite material and process for producing the same, and composite metal material and process for producing the same

본 발명의 목적은 표면의 습윤성이 개선된 탄소계 재료를 포함하는 복합 재료 및 그 제조 방법을 제공하는 것에 있다. 또한, 탄소 재료가 균일하게 분산된 복합 금속 재료 및 그 제조 방법을 제공하는 것에 있다. It is an object of the present invention to provide a composite material comprising a carbonaceous material having improved surface wettability and a method for producing the same. Moreover, it is providing the composite metal material in which a carbon material was disperse | distributed uniformly, and its manufacturing method. 탄소계 재료와, 금속 재료 Z로 이루어지는 복합 재료의 제조 방법은, 공정 (a)∼(c)를 갖는다. 공정 (a)는, 엘라스토머와, 적어도 제1 탄소 재료와, 이 제1 탄소 재료보다도 융점이 낮은 입자 형상 또는 섬유 형상의 금속 재료 Z를 혼합하고, 또한 전단력에 의해 분산시켜 복합 엘라스토머를 얻는다. 공정 (b)는, 복합 엘라스토머를 열처리하여, 엘라스토머를 기화시켜 제2 탄소 재료와 금속 재료 Z로 이루어지는 중간 복합 재료를 얻는다. 공정 (c)는, 중간 복합 재료를, 금속 재료 Z보다도 융점이 낮은 원소(Y)를 갖는 물질과 함께 열처리하여, 원소(Y)를 갖는 물질을 기화시킨다. The manufacturing method of the composite material which consists of a carbon system material and the metal material Z has process (a)-(c). Step (a) mixes the elastomer, at least the first carbon material, and the metallic material Z having a melting point lower than that of the first carbon material, and further disperses by shear force to obtain a composite elastomer. The step (b) heat-treats the composite elastomer to vaporize the elastomer to obtain an intermediate composite material composed of the second carbon material and the metal material Z. Step (c) heat-treats the intermediate composite material together with the material having the element (Y) having a lower melting point than the metal material Z to vaporize the material having the element (Y).

High-flux preparation device and method for metal matrix composite

一种金属基复合材料的高通量制备装置和方法，涉及一种金属基复合材料制备装置及制备方法。它主要解决不同液态金属基体与增强体复合的金属基复合材料高通量制备的问题。装置由提升杆、抽气管、炉体、预热区、熔炼区、网格式坩埚、充气管、预制体安装盘、多个预制体、隔热板、坩埚加热区构成。方法：安装预制体和网格式坩埚、预制体去胶质、气氛保护、真空除气、气压浸渗、成型。本发明可以一次性高通量制备不同材质基体的金属基复合材料，从而可以高效地研究复合材料的界面润湿和界面反应行为，成本低、周期短。本发明适用于高通量制备金属基复合材料。

Method for increasing permeability of pores of a graphite workpiece

FIELD: metallurgy.SUBSTANCE: invention relates to composite materials with porous carcass impregnation having high wear resistance, antifriction properties and resistance to aggressive media. Method of producing coal-graphite composite material includes vacuum degassing of porous coal-graphite billet, its impregnation with molten matrix lead alloy under the effect of excessive pressure due to thermal expansion of the melt when heated above the liquidus temperature of the lead alloy, wherein degassing is carried out prior to submersion of porous workpiece into melt of matrix alloy, and before impregnation porous workpiece is coated with two-layer galvanic coating consisting of internal copper and outer nickel layers.EFFECT: technical result is improved quality of composite materials by increasing permeability of pores of graphite billet.1 cl, 1 ex, 1 tbl, 2 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 688 772 C1 (51) МПК C22C 47/08 (2006.01) B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2019.02) (21)(22) Заявка: 2018101560, 16.01.2018 (24) Дата начала отсчета срока действия патента: 22.05.2019 Приоритет(ы): (22) Дата подачи заявки: 16.01.2018 (45) Опубликовано: 22.05.2019 Бюл. № 15 2539528 C1, 20.01.2015. JP 2009127116 A, 11.06.2009. EP 1477467 A1, 17.11.2004. SU 1759932 A1, 07.09.1992. (54) Способ повышения проницаемости пор углеграфитовой заготовки (57) Реферат: Изобретение относится к области выше температуры ликвидус сплава свинца, при металлургии, а именно к созданию этом дегазацию проводят до погружения композиционных материалов пропиткой пористой заготовки в расплав матричного сплава, пористого каркаса, имеющих высокую а перед пропиткой пористую заготовку износостойкость, антифрикционные свойства, покрывают двухслойным гальваническим стойкость в агрессивных средах. Способ покрытием, состоящим из внутреннего медного получения углеграфитового композиционного и наружного ...

Method for increasing permeability of pores of graphite workpiece

FIELD: metallurgy.SUBSTANCE: invention relates to creation of composite materials with impregnation of porous frame, having high wear resistance, antifriction properties, resistance in aggressive media. Method of producing coal-graphite composite material involves vacuum degassing of porous coal-graphite billet, its impregnation with molten matrix lead alloy under effect of excess pressure due to thermal expansion of the melt when heated above the liquidus temperature of the lead alloy, wherein the degassing is carried out before immersing the porous workpiece into the melt of the matrix alloy, and before impregnation porous workpiece is covered with two-layer galvanic coating consisting of internal copper and outer chromium layers.EFFECT: technical result is improved quality of composite materials by increasing permeability of pores of graphite billet.1 cl, 1 ex, 1 tbl, 2 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 688 558 C1 (51) МПК C22C 47/08 (2006.01) B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2019.02); B22F 3/26 (2019.02) (21)(22) Заявка: 2018101555, 16.01.2018 (24) Дата начала отсчета срока действия патента: 21.05.2019 Приоритет(ы): (22) Дата подачи заявки: 16.01.2018 (45) Опубликовано: 21.05.2019 Бюл. № 15 2539528 C1, 20.01.2015. JP 2009127116 A, 11.06.2009. EP 1477467 A1, 17.11.2004. SU 1759932 A1, 07.09.1992. (54) Способ повышения проницаемости пор углеграфитовой заготовки (57) Реферат: Изобретение относится к области выше температуры ликвидус сплава свинца, при металлургии, а именно к созданию этом дегазацию проводят до погружения композиционных материалов пропиткой пористой заготовки в расплав матричного сплава, пористого каркаса, имеющих высокую а перед пропиткой пористую заготовку износостойкость, антифрикционные свойства, покрывают двухслойным гальваническим стойкость в агрессивных средах. Способ покрытием, состоящим из внутреннего медного получения углеграфитового ...

High-silicon aluminum calcium reinforced fiber, preparation method thereof and aluminum calcium superplastic alloy based composite aluminum

本发明公开高硅铝钙增强纤维及其制备方法与铝钙超塑合金基复合铝。按重量百分比计，由89%‑98%的火成岩、1‑10%的氧化钙和1%的碳粉组成。本发明在天然高硅铝火成岩矿石基础上，通过引入氧化钙组分，生成一种非晶高硅铝钙增强纤维。所述非晶高硅铝钙增强纤维与铝钙超塑铝合金复合，增强材料中的硅、铝、钙组分，会和金属溶体发生分子融合，从而改善复合界面的结合牢度，即提高铝钙超塑合金基复合铝的强度。

Method for increasing permeability of pores of a graphite workpiece

FIELD: metallurgy.SUBSTANCE: invention relates to composite materials with porous carcass impregnation having high electrical conductivity, antifriction properties and resistance to aggressive media. Method of producing graphite composite material comprises vacuum degassing of porous billet, its impregnation with molten metal matrix aluminium alloy under the effect of excessive pressure due to thermal expansion of the melt when heated above the liquidus temperature of the aluminium alloy, wherein degassing is carried out prior to submersion of porous workpiece into melt of matrix alloy, and before impregnation porous workpiece is coated with two-layer galvanic coating consisting of internal copper and outer nickel layers.EFFECT: technical result is improved quality of composite by increasing permeability of pores of graphite billet.1 cl, 2 dwg, 1 tbl, 1 ex РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 688 560 C1 (51) МПК C22C 47/08 (2006.01) B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2019.02); B22F 3/26 (2019.02) (21)(22) Заявка: 2018101557, 16.01.2018 (24) Дата начала отсчета срока действия патента: Дата регистрации: 21.05.2019 (45) Опубликовано: 21.05.2019 Бюл. № 15 Адрес для переписки: 400005, г. Волгоград, пр. Ленина, 28, отдел интеллектуальной собственности ВолгГТУ (73) Патентообладатель(и): Федеральное государственное бюджетное образовательное учреждение высшего образования "Волгоградский государственный технический университет" (ВолгГТУ) (RU) (56) Список документов, цитированных в отчете о поиске: RU 2571295 C1, 20.12.2015. SU 2 6 8 8 5 6 0 R U (54) Способ повышения проницаемости пор углеграфитовой заготовки (57) Реферат: Изобретение относится к области температуры ликвидус сплава алюминия, при металлургии, а именно к созданию этом дегазацию проводят до погружения композиционных материалов пропиткой пористой заготовки в расплав матричного сплава, пористого каркаса, имеющих ...

Method for forming a metal matrix composite body by an outside-in spontaneous infiltration process

본 발명은 실질적으로 비반응성인 충전재를 제공하는 단계, 침투 촉진제 전구물질 및 침투 촉진제 중 하나 이상을 제공하는 단계, 침투 대기를 상기 충전재의 적어도 일부에 편중적으로 접촉시키는 단계, 및 상기 충전재의 적어도 일부에 용융된 금속 기재가 자발적으로 침투하는 단계를 포함하는 금속 기계 복합체의 제조 방법; 및 이 제조방법에 의해 제조방법에 의해 제조된 금속 기재 복합체 제품에 관한 것이다. The present invention provides a method of providing a substantially non-reactive filler, providing at least one of a penetration promoter precursor and a penetration promoter, contacting the atmosphere of penetration to at least a portion of the filler, and at least a portion of the filler. A method of producing a metal mechanical composite comprising spontaneously penetrating a molten metal substrate in a portion; And to a metal based composite product produced by the production method by this production method.

Preparation method of magnesium-based composite material

一种镁基复合材料的制备方法，按以下步骤进行：(1)准备镁锭作为原料；准备盐熔剂和增强体；(2)将盐熔剂置于坩埚中，加热制成盐熔剂熔体；加入增强体；(3)倒入常温的坩埚中，冷却至常温得到前驱体；(4)将铁坩埚预热至赤热状态，加入原料在953～1043K熔化；(5)将前驱体放入原料熔体中，搅拌后在温度953～993K条件下，加入精炼剂搅拌精炼，控制温度后静置形成浮渣和熔体；(6)除渣后将温度降至973～982K，浇铸。本发明的特方法使增强体均匀分散于熔盐之中，使增强体易于均匀分散在基体中；工艺简单，成本低，可以用来制备大体积的镁基复合材料结构件，并且可以进行自动化生产。

Methods for manufacturing carbon fiber reinforced aluminum composites using stir casting process

The present invention relates to a method to manufacture carbon fiber reinforced aluminum composite using a stir casting process. According to the present invention, while using the stir casting process during a melt casting process, carbon fiber is inserted while supplying current to liquid aluminum, thus decreasing a contact angle of carbon with respect to aluminum. As such, the carbon fiber is guided to spontaneously be dispersed in the liquid aluminum, and an aluminum carbonate (Al_4C_3) phase is also prevented from being formed in an interface between the aluminum and the carbon fiber; and a carbon fiber reinforced aluminum composite with excellent electric, thermal, and mechanical characteristics is efficiently manufactured.

Metal matrix composite comprising nanotubes and method of producing same

A metal matrix composite comprising nanotubes; a method of producing the same; and a composition, for example a metal alloy, used in such composites and methods, are disclosed. A method for continuously infiltrating nanotube yarns, tapes or other nanotube preforms with metal alloys using a continuous process or a multistep process, which results in a metal matrix composite wire, cable, tape, sheet, tube, or other continuous shape, and the microstructure of these infiltrated yarns or fibers, are disclosed. The nanotube yarns comprise a multiplicity of spun nanotubes of carbon (CNT), boron nitride (BNNT), boron (BNT), or other types of nanotubes. The element that infiltrates the nanotube yarns or fibers can, for example, be alloyed with a concentration of one or more elements chosen such that the resulting alloy, in its molten state, will exhibit improved wetting of the nanotube material.

Patent JPH0423116B2

Pressure impregnation device for impregnating metal into fiber bundle

Gas rudder, process forming method thereof and rocket

本发明实施例公开一种燃气舵及其工艺成型方法、火箭，在一个具体的实施例中，所述方法包括：根据任务进行三维模型胎模设计得到胎模编织工艺文件；基于所述胎模编织工艺文件进行机械加工得到制作燃气舵所需模具；采用碳纤维增强铝基复合材料进行铺层设计得到预制体；将所述预制体装入所述模具；将铝基复合材料加入炼炉中，并加入预定量的锆元素和镁元素进行熔炼得到新型材料；将所述预制体和新型材料放入炼炉中进行精炼，降温降压进行脱模得到半成品；对所述半成品进行机械加工得到所述任务规定的燃气舵。

Method for producing carbon-graphite composite material

FIELD: metallurgy, composite materials.SUBSTANCE: invention relates to the field of metallurgy, namely the creation of carbon-graphite composite materials with a metal matrix having high electrical conductivity, anti-friction properties and resistance in aggressive environments. The method for producing a carbon-graphite composite material includes vacuum degassing of a porous carbon-graphite billet in an electrolyte solution, applying a galvanic coating on it, containing sequentially applied inner nickel, intermediate zinc and outer copper layers, impregnating it in the impregnation chamber with a melt of a matrix copper-phosphorous alloy under the influence of excessive pressure due to the thermal expansion of the lead melt in the pressure chamber when heated 100°C above the liquidus temperature of the matrix copper-phosphorous alloy simultaneously with molten lead, and along with this, vacuum degassing is carried out in a solution of nickel electrolyte containing 140 g/l of nickel sulfate, 50 g/l of sodium sulfate, 30 g/l of magnesium sulfate, 20 g/l of dry boric acid, and the carbon-graphite billet is placed in the impregnation chamber at the temperature of the lead melt in the pressure chamber for 5-10° below the liquidus temperature of the lead alloy.EFFECT: invention improves quality of carbon-graphite composite materials.1 cl, 1 tbl, 1 ex РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 750 066 C1 (51) МПК C22C 47/08 (2006.01) C22C 49/02 (2006.01) C22C 49/14 (2006.01) C22C 101/10 (2006.01) B22F 3/26 (2006.01) C25D 5/10 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2021.02); C22C 49/02 (2021.02); C22C 49/14 (2021.02); B22F 3/26 (2021.02); C25D 5/10 (2021.02) (21)(22) Заявка: 2020142402, 22.12.2020 22.12.2020 21.06.2021 Приоритет(ы): (22) Дата подачи заявки: 22.12.2020 (45) Опубликовано: 21.06.2021 Бюл. № 18 2 7 5 0 0 6 6 R U (56) Список документов, цитированных в отчете о поиске: RU 2688529 C1, ...

Method of producing base plates for firing ceramic articles

FIELD: construction. SUBSTANCE: for producing such plates, the method has been developed for obtaining a two-layer silicon-carbon composite material with different silicon carbide phase content in the layers. The method for producing base plates for firing ceramic articles includes producing the layered preform from carbon felt on the ribbon of carbon and graphite fabric and its siliconization. The siliconization process is carried out by pulling the resulting preform under a capillary feeder supplying silicon melt, followed by crystallization of the melt. The tensile bending strength of the articles at 1250°C reaches 420 MPa. EFFECT: method provides obtaining articles of large area and relatively small thickness, which can be used in reducing as well as in oxidizing media. 1 ex, 3 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 617 133 C1 (51) МПК C04B 35/577 (2006.01) C04B 35/80 (2006.01) C22C 47/08 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ФОРМУЛА (21)(22) Заявка: ИЗОБРЕТЕНИЯ К ПАТЕНТУ РОССИЙСКОЙ ФЕДЕРАЦИИ 2016111552, 28.03.2016 (24) Дата начала отсчета срока действия патента: 28.03.2016 (72) Автор(ы): Брантов Сергей Константинович (RU) Дата регистрации: 21.04.2017 Приоритет(ы): (22) Дата подачи заявки: 28.03.2016 (56) Список документов, цитированных в отчете о поиске: RU 2194683 C2, 20.12.2002. RU (45) Опубликовано: 21.04.2017 Бюл. № 12 2286317 C1, 27.10.2006. RU 2201542 C1, 27.03.2003. US 5205970 A, 27.04.1993. US 4294788 A, 13.10.1981. (54) Способ получения опорных плит для обжига керамических изделий 2 6 1 7 1 3 3 R U Стр.: 1 C 1 (57) Формула изобретения Способ получения опорных плит для обжига керамических изделий, включающий изготовление слоистой заготовки из углеродного композиционного материала на основе каркаса из углеродно-волокнистого наполнителя и ее силицирование, отличающийся тем, что слоистую заготовку выполняют в виде слоя углеродного войлока на ленте из углеграфитовой ткани, затем проводят протягивание полученной заготовки ...

Method of forming a metal matrix composite containing a three-dimensionally interconnected co-matrix

A kind of wear resistant corrosion resistant composite alloy material and preparation method thereof

本发明公开了一种耐磨耐腐蚀复合合金材料及其制备方法。所述耐磨耐腐蚀复合合金材料包括以下重量份数的原料：铁35‑42份、铝40‑48份、镁8‑13份、废弃陶瓷粉6‑10份、炭黑7‑11份、硼酸锌5‑10份、硅藻土6‑10份、玻璃纤维2‑6份、硒粉4‑8份。本发明的复合合金材料具有较高的耐磨性以及耐腐蚀性，原料易得，制备工艺简单，降低了生产加工成本，适合大规模的工业化生产。性能测试结果显示，耐盐雾70h以上，采用GBT34501‑2017硬质合金耐磨试验方法测试磨损量小于8.6mg。

Method of metal matrix composites and the same product

내용없음. None.

Method for increasing permeability of pores of graphite workpiece

Изобретение относится к области металлургии, а именно к созданию композиционных материалов пропиткой пористого каркаса, имеющих высокую электропроводность, антифрикционные свойства, стойкость в агрессивных средах. Способ получения углеграфитового композиционного материала включает вакуумную дегазацию пористой углеграфитовой заготовки, ее пропитку расплавом матричного сплава алюминия под воздействием избыточного давления за счет термического расширения расплава при нагреве выше температуры ликвидус сплава алюминия, при этом дегазацию проводят до погружения пористой заготовки в расплав матричного сплава, а перед пропиткой пористую заготовку покрывают трехслойным гальваническим покрытием, состоящим из внутреннего медного, среднего никелевого и наружного хромового слоев. Техническим результатом изобретения является повышение качества композиционных материалов за счет увеличения проницаемости пор углеграфитовой заготовки. 2 ил., 1 табл., 1 пр. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 688 524 C1 (51) МПК C22C 47/08 (2006.01) B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 47/08 (2019.02); B22F 3/26 (2019.02) (21)(22) Заявка: 2018101543, 16.01.2018 (24) Дата начала отсчета срока действия патента: Дата регистрации: 21.05.2019 (45) Опубликовано: 21.05.2019 Бюл. № 15 Адрес для переписки: 400005, г. Волгоград, пр. Ленина, 28, ВолгГТУ, отдел интеллектуальной собственности (73) Патентообладатель(и): Федеральное государственное бюджетное образовательное учреждение высшего образования "Волгоградский государственный технический университет" (ВолгГТУ) (RU) (56) Список документов, цитированных в отчете о поиске: RU 2571295 C1, 20.12.2015. SU 2 6 8 8 5 2 4 R U (54) Способ повышения проницаемости пор углеграфитовой заготовки (57) Реферат: Изобретение относится к области выше температуры ликвидус сплава алюминия, металлургии, а именно к созданию при этом дегазацию проводят до погружения композиционных материалов ...

Method for manufacturing filament reinforced metallic composite

PURPOSE: A method for manufacturing the fiber reinforced metallic composite is provided to manufacture a fiber reinforced metallic composite in which the metallic fiber is not aggregated, and a volume fraction of the filament is low. CONSTITUTION: The method for manufacturing a filament reinforced metallic composite comprises a preform preparation step of preparing a preform by continuously passing a desired volume fraction of reinforced fibers(3) through the through holes(8) between two plates(6,7) which are oppositely fixed by supports(8), and on which a plurality of through holes(9) are formed, thereby arranging the filament; and a pressing and cooling step of pressing and cooling the molten metal after putting the preform into a preheated mould and filling molten metal of aluminum or magnesium alloy in the mould, wherein the pressing and cooling step is performed by pressing and cooling the heated powder type alloy after injecting the aluminum or magnesium alloy into the preform in the powder state and heating the powder type alloy to a temperature below the solidus line.

Production of fiber reinforced composite member

(57)【要約】本公報は電子出願前の出願データであるた め要約のデータは記録されません。

METHOD OF OBTAINING OF Nb3Sn SUPERCONDUCTOR USING INTERNAL TIN SOURCE METHOD

FIELD: electricity. SUBSTANCE: work piece of the sub-element Cu/Nb is formed which contains the bars from niobium or alloy on its base distributed in an array from copper or alloy on its base and the central core from tin or from tin-based alloy, the work piece is deformed up to the intermediate size, is cut in parts from which the lengthy composite work piece is formed which comprises an external cylindrical layer from high-pure copper and the internal cylindrical diffusive barrier, the composite work piece is deformed by cold drawing up to a final diameter and the reactionary heat treatment is performed for formation of the superconducting compound Nb 3 Sn, and the work piece of the sub-element Cu/Nb is formed in the induction vacuum furnace by filling with fusion of copper or copper-based alloy, bars of niobium or niobium-based alloy which are placed in a mould designed as a spatial frame. EFFECT: avoidance of labour-intensive processes of chemical etching, pumping out and sealing of compound preparations, obtaining of superconductor with pre-set distribution of fibres in the cross section of superconductor. 8 cl, 3 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (51) МПК H01B 12/00 (13) 2 547 814 C1 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ (21)(22) Заявка: ИЗОБРЕТЕНИЯ К ПАТЕНТУ 2013153579/07, 04.12.2013 (24) Дата начала отсчета срока действия патента: 04.12.2013 (45) Опубликовано: 10.04.2015 Бюл. № 10 (56) Список документов, цитированных в отчете о поиске: US7210216 B2 , 01.05.2007. RU2182736 (73) Патентообладатель(и): Общество с ограниченной ответственностью "Научно-производственное предприятие "НАНОЭЛЕКТРО" (RU) 2 5 4 7 8 1 4 R U (54) СПОСОБ ПОЛУЧЕНИЯ Nb3Sn СВЕРХПРОВОДНИКА МЕТОДОМ ВНУТРЕННЕГО ИСТОЧНИКА ОЛОВА (57) Реферат: Способ относится к электротехнике и может промежуточного размера, нарезают ее на части, быть использован при конструировании и из которых формируют длинномерную изготовлении сверхпроводящих проводов на композиционную ...

Notebook computer magnesium alloy

本发明属于镁合金技术领域，特别涉及一种笔记本电脑用镁合金，按原子百分比计，所述笔记本电脑用镁合金包括：Al 2％～8％；Zn 0.1％～2％；Mn 0.1％～0.6％；Ce 0.2％～1.5％；Nd 0.2％～1.5％；Ca 5％～10％；Bi 0.1％～2％；余量为Mg；所述镁合金内还填充有占镁合金总质量的1wt％‑5wt％的石墨纤维；所述镁合金的表面经过酸洗活化处理，按质量比计，酸洗液的配方为：Na 3 PO 4 ·12H 2 O 50％‑75％；H 3 PO 4 15％‑25％；KMnO 4 8％‑25％；酸洗活化处理的持续时间为1min‑10min。相对于现有技术，本发明具有较高的力学性能、耐蚀性，而且易燃性较低。

Continuous carbon fiber reinforced magnesium-aluminum bimetal-based composite material and preparation method thereof

本发明提供了一种连续碳纤维增强镁‑铝双金属基复合材料及其制备方法，属于高性能金属基复合材料技术领域。本发明先制备出连续碳纤维增强镁基复合材料丝材作为增强体，然后将该增强体与铝合金复合，制备连续碳纤维增强镁‑铝双金属基复合材料；镁合金与连续碳纤维的浸润性好，浸渗形成的缺陷少，而且镁合金与连续碳纤维之间的界面反应少，不会产生界面有害脆性产物，不会损伤连续碳纤维；铝合金不会与碳纤维直接接触反应，避免了传统连续碳纤维增强铝基复合材料制备中因碳纤维与铝合金之间界面润湿性差导致的浸渗困难和制备缺陷多的问题，以及碳纤维与铝合金之间严重的界面反应引起的有害界面脆性相生成和纤维性能受损的问题。

Mineral fiber reinforced metallic composite material

(57)【要約】本公報は電子出願前の出願データであるた め要約のデータは記録されません。

Carbon fiber composite material and its forming products,carbon fiber-metal composite material and its forming products, and method of producing the same

本发明提供均匀地分散碳纳米纤维的碳纤维复合材料及其制造方法、碳纤维复合成形品及其制造方法、碳纤维复合金属材料及其制造方法、碳纤维复合金属成形品及其制造方法。碳纤维复合材料的制造方法，其特征在于：包括将具有对碳纳米纤维具有亲和性的不饱和键或基团的弹性体和金属颗粒进行混合的步骤以及通过剪切力把碳纳米纤维分散在含有金属颗粒的弹性体中的步骤。

PRODUCTION METHOD OF A CERAMIC COMPOUND WITH A METALLIC MATRIX AND A COMPOUND SO OBTAINED

La presente invención se refiere a método de producción de un compuesto con matriz metálica, CARACTERIZADO porque comprende: (a) suministrar una aleación de aluminio que contiene aluminio y por lo menos aproximadamente 1 por ciento en peso de magnesio y una masa permeable de material de carga cerámico; (b) en presencia de un gas que comprende aproximadamente 10 a 100 por ciento en volumen de nitrógeno, siendo el resto gas no oxidante, poner la aleación de aluminio en estado líquido en contacto con la masa permeable e infiltrar la masa permeable con la aleación de aluminio líquida, produciéndose dicha infiltración de la masa permeable en forma espontánea; y (c) luego de una cantidad deseada de infiltración de la masa, dejar que la aleación de aluminio líquida solidifique para formar una estructura de matriz metálica sólida que embebe el material de carga cerámico.

METHOD OF MANUFACTURING METAL MATRIX COMPOSITION PRODUCTS

Fibre-reinforced metal matrix composites

A metal matrix composite comprises randomly-­oriented inorganic oxide fibres of density below 3 g/ml embedded in a metal matrix material such as a light metal, for example aluminium or magnesium or an alloy thereof. In a particular embodiment the fibres are of density l.8 to 2.5 g/ml and preferably are of mean diameter from 2 to l0 microns. The composite can be made by liquid infiltration of a fibre preform comprising the fibres bound together with an inorganic or an organic binder or by extrusion of a mixture of the fibres and a powdered metal matrix material.

Ceramic shell mold for casting metal matrix composites

Title of the Invention CERAMIC SHELL MOLD FOR CASTING METAL MATRIX COMPOSITES Abstract Method for investment casting of metal matrix composites by vacuum infiltration using a ceramic mold formed directly on the pattern.