Бронированный композиционный материал

Изобретение относится к композиционным материалам, которые используются в качестве брони. Сущность изобретения: предложенный бронированный материал содержит основу из металлического связующего , в качестве которого используют по крайней мере одно вещество, выбранное из группы, содержащей алюминиевый сплав, медный сплав, чугун, титан, железо, никель, сталь и керамический наполнитель, в качестве которого используют по крайней мере одно вещество, выбранное из группы, содержащей глинозем магнезию, оксид циркония , карбид кремния, диборид титана, нитрид кремния, диборид титана, нитрид алюминия, додекаборид алюминия, карбид титана, при содержании керамического наполнителя 36-72 об.%. 2 з.п. ф-лы, 2 табл.

Verfahren zur Herstellung eines Verbundmaterialkörpers mit nichtorganischem Matrix

ZUSAMMENGESETZTE GEGENSTAENDE FUER DIE VERWENDUNG BEI HOHEN TEMPERATUREN

FIBER-REINFORCED METALLIC COMPOSITE MATERIAL

Verfahren zur Herstellung eines Verbundwerkstoffs sowie ein nach dem Verfahren hergestellter Verbundwerkstoff

Die Erfindung bezieht sich unter anderem auf ein Verfahren zur Herstellung eines Verbundwerkstoffs, bei dem eine Vorform als Verstärkungsmatrix durch Kombinieren von Verstärkungselementen mit einem Ergänzungsmaterial gebildet wird, wobei das Ergänzungsmaterial den Verstärkungselementen hinzugefügt wird und wobei durch eine Vorbehandlung auf das Ergänzungsmaterial derart eingewirkt wird, dass es verformt wird und die Verstärkungselemente der Verstärkungsmatrix wenigstens teilweise einbettet. Hierdurch werden Zwischenräume zwischen Verstärkungselementen minimiert, und es wird ein guter Zusammenhalt der Verstärkungsmatrix einerseits und des Verbundwerkstoffs andererseits erreicht.

Herstellung eines festes Werkstoffes in quader- oder zylindrischer Form, der laminiert, gesintert, geschnitten und wärmebehandelt wird

Fibre-reinforced metal strip - produced by thermal decomposition of metal org. salts to metal on fibres and subsequent consolidation

A bonded composite solid consisting of a fibre-reinforced metal matrix is produced by (a) dispersing the fibres in a soln. of an org. salt of a metal which can decompose on heating with deposition of the metal (b) pptg. the salt from soln. to give an intimate mixt. with the fibres and heating this mixt. under conditions such that the salt decomposes and produces finely divided metal (c) bringing the mixt. thus produced at a specific temp. and pressure into the form of a fibre-reinforced compacted mass. The salt soln. for the process is prepd. by dispersing an oxide or carbonate of the metal in a working liq., adding an org. acid to produce a soln. of an org. salt of the metal, and after pptg. the intimate mixt. as in (b) filtering and recycling the filtrate as working liq. Metals having org. salts thermally decomposing below their m.pt. may be used e.g. Fe, Co, Cu, Pb, Ag, Au, Ni or alloys of these and partic. Pb. The org. acid may be formic or acetic or in the case of Ag, the lactate or ...

METALLIC COMPOSITE MATERIAL AND METHOD FOR PRODUCING THE SAME

... 1473210 Making composite wire or rod G RAU 10 Oct 1974 [12 Oct 1973] 44019/74 Heading B3A [Also in Division C7] A wire or rod metallic composite comprising a matrix metal with a powder additive distributed as separate cords extending along the length may be made by filling a matrix metal pipe with additive powder, reducing the diameter by mechanical forming, e.g. hammering and annealing and then bundling a number of the assemblies together and mechanically forming the bundle into a wire or rod of reduced diameter. The additive powders may be CdO, SnO 2 , Al 2 O 3 , MgO, CaO, ZrO 2 , PbO, Nb-Ti, W, Mo, carbides, nitrides, borides, graphite, glass and organic material. The matrix metal may be Ag, Cu or their alloys. The powder filled metal pipes, e.g. Ag-CdO 0À3 mm. diameter, formed by hammering, drawing and intermediate annealing were bundled in a Ag tube 20 mm. diameter and drawn to a 2 mm. diameter wire, the powdered CdO cords forming 10% wt. The wider Ag tube may be removed after drawing ...

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.

Metal fibers, textiles and shapes and process for producing them

... 1,134,162. Making metal fabrics and wire. UNION CARBIDE CORP. 19 Jan., 1967, No. 2869/67. Heading B3A. [Also in Divisions C7, E1 and H1] A process for the production of metal fibres, fabrics and other shapes comprises: 1. Impregnating a preformed organic polymeric material shape with a compound of one or more of the metals of Groups I B , VI B or VIII of the Periodic Table, Tc, Re or Zn. 2. Heating the impregnated material to carbonize and then volatilize the organic material without ignition. 3. The product of step 2 is then heated in a reducing gas to reduce it to the metallic form. The organic material may be for example cellulosic (rayon, saponified cellulose acetate, cotton, wood or ramie), proteinaceous (wool or silk), acrylics, polyesters, vinyls or polyurethanes and may be in the form of ribbons, staple fibres, yarn and roving, woven cloth, knits, braids, felts and papers. The organic material may be pretreated with a suitable solvent to swell it prior to treatment with a solution ...

VERBUNDWERKSTOFF MIT VORZUGSWEISE NICHTMETALLISCHEN EINLAGERUNGEN UND VERFAHREN ZU SEINER HERSTELLUNG

COMPOSITE MATERIAL WITH PREFERABLY NON-METALLIC STORAGES AND PROCEDURE FOR ITS PRODUCTION

COMPOSITE MATERIAL

PROCEDURE FOR THE TREATMENT OF REINFORCEMENT ELEMENTS

METAL MATRIX COMPOSITE (MMC) CONSTRUCTION UNIT

CERAMIC GATHERING MOLDS, YOUR PRODUCTION AND YOUR USES

CHORD GATHERING MOLD FOR FIBER-REINFORCED ARTICLES AND PROCEDURE FOR YOUR PRODUCTION

PROCEDURE FOR THE PRODUCTION OF A TOOL PART

ALUMINUM MATRIX COMPOSITE MATERIAL AND PROCEDURE FOR ITS PRODUCTION

FIBER-REINFORCED COMPOSITE MATERIAL WITH ALUMINUM MATRIX

PRODUCTION OF A CELEBRATION OF MATERIAL IN RIGHT PARALLELEPIPED OR CYLINDRICAL FORM, TO WHICH LAMINATES, SINTERED, CUT AND HEAT TREATED BECOMES

Fiber reinforced aluminum matrix composite

Device for producing semifinished goods and moulded parts made of metal material

INORGANIC FIBROUS MATERIAL AS REINFORCEMENT FOR COMPOSITE MATERIALS AND PROCESS FOR PRODUCTION THEREOF

REFRACTORY FIBERS AND METHOD OF PRODUCING SAME

FIBER REINFORCED-METAL COMPOSITE MATERIAL

The invention provides a fiber-reinforced metal composite material comprising a metal or an alloy as the matrix and an inorganic fiber as the reinforcing material. At least one element selected from elements belonging to the fourth or higher periods of Group IA of the Periodic Table, elements belonging to the fifth or higher periods of the Group IIA of the Periodic Table, and Bi and In, in the form of the uncombined element or an organic or inorganic compound thereof, is incorporated into either one or both of the matrix metal or the reinforcing material in an amount of 0.0005 to 10 % by weight (calculated in terms of the element) so as to enhance the mechanical strength of the composite material.

BORON CARBIDE FIBER PRODUCTION

WEAR-RESISTANT SURFACE COMPOSITE MATERIALS AND METHOD FOR PRODUCING SAME

GAMMA TITANIUM ALUMINUM ALLOYS MODIFIED BY CARBON, CHROMIUM AND NIOBIUM

RD-19,588 Typed: 7/24/89 GAMMA TITANIUM ALUMINUM ALLOYS MODIFIED BY CARBON, CHROMIUM AND NIOBIUM A TiAl composition is prepared to have high strength and to have improved ductility by altering the atomic ratio of the titanium and aluminum to have what has been found to be a highly desirable effective aluminum concentration by addition of chromium, carbon and niobium according to the approximate formula Ti51-43Al46-50Cr2Nb1-5C0.1.

GAMMA TITANIUM ALLOYS MODIFIED BY CHROMIUM AND SILICON AND METHOD OF PREPARATION

RD-19,428 6/21/89 GAMMA TITANIUM ALUMINUM ALLOYS MODIFIED BY CHROMIUM AND SILICON AND METHOD OF PREPARATION A TiAl composition is prepared to have high strength, high oxidation resistance and to have acceptable ductility by altering the atomic ratio of the titanium and aluminum to have what has been found to be a highly desirable effective aluminum concentration by addition of chromium and silicon according to the approximate formula Ti48Al48Cr2Si2.

COMPOSITE CONSTRUCTIONS WITH ORIENTED MICROSTRUCTURE

In one embodiment, composite constructions of the invention are in the form of a plurality of coated fibers bundled together to produce a fibrous composite constructio n in the form of a rod. Each fiber has a core formed from a hard phase material, that is surro unded by a shell formed from a binder phase material. In another embodiment of the invention , monolithic sheets of the hard phase material and the binder phase material are stacked and arr anged to produce a swirled composite in the form of a rod. In still another embodiment of the invention, sheets formed from coated fibers are arranged to produce a swirled composite. Inse rts for use in such drilling applications as roller cone rock bits and percussion hammer bits, a nd shear cutters for use in such drilling applications as drag bits, that are manufactured using conventional methods from these composite constructions exhibit increased fracture toughness due to the continuous binder phase around the hard phase of the composites ...

Alliage cuivre-fer-aluminium

Aus Hartstoffen und Bindemetall bestehendes Sinterhartmetall

Procédé pour la fabrication de fibres réfractaires et appareil pour la mise en oeuvre du procédé

Verstärktes metallisches Konstruktionselement und Verfahren zu seiner Herstellung

Verfahren zur Herstellung von Siliziumkarbidkristallen

NUCLEAR RADIATION ABSORBERS.

COMPOSITE MATERIAL WITH HIGH STRENGTH.

Износостойкий композиционный материал

Изобретение относится к отрасли металлургии, а более конкретно к химико-термической обработке, и может быть использован при производстве металлообрабатывающего инструмента повышенной производительности. Износостойкий композиционный материал на базе системы Fe-W-Cr представляет собой трехфазный природный композит, состоящий из аустенитной матрицы, армированной пластинами и волокнами карбидов двух типов, который получают науглероживанием низкоуглеродистого матричного сплава. Исходный матричный сплав перед науглероживанием имеет следующий состав: 0,04-0,06 масс. % С, 9,1-9,5% масс. % W, 14,3-14,6 мас. % Cr, остальное Fe, который соответствует равновесной концентрации α-фазы в четырехфазной области диаграммы состояния Fe-W-Cr-C. Изобретение обеспечивает улучшение механических свойств режущей поверхности, а именно повышение устойчивости и сопротивления износу.

АНТИФРИКЦІЙНИЙ АЛМАЗОВМІСНИЙ МАТЕРІАЛ НА МЕТАЛЕВІЙ ОСНОВІ "РОМАНІТ-УВЛАЛ", СПОСІБ ЙОГО ОДЕРЖАННЯ ТА ЕЛЕМЕНТ ВУЗЛА ТЕРТЯ

Антифрикційний алмазовмісний матеріал на металевій основі містить мідь або її сплави та додатково містить оксид кремнію, спосібйогоодержання, що включає перемішування та спікання компонентів антифрикційного матеріалу та елемент вузла тертя, що включає несучий елемент із напеченим шаром алмазовмісного антифрикційного матеріалу.

Nano-aluminum-oxide-based metal ceramic mold material and preparation method thereof

Based on continuous fiber surface-modified metal-based composite material 3 D printing method

Fibre-reinforced metal

COMPOSITE MATTERS METAL RENFORCEES BY FIBRES IN PARTICULAR CONTAINING ELEMENTS OF GROUP IA OR GROUP IIA OF THE PERIODIC TABLE OF CLASSIFICATION

Metal composite and method for its manufacture.

COMPOSITE EUTECTIC ALLOY AND ARTICLE

MANUFACTORING PROCESS OF COMPONENTS OUT OF CERAMICS OR METAL BY PIM, BASES ON the USE OF INORGANIC FIBRES OR NANOFIBRES

MAGNESIUM CONTAINING ALLOYS

Method for producing composite materials based on a preform produced in a first reinforcement component in association with a second component consisting of a light metal alloy, as well as the products obtained by this method

Composite material - has tungsten cored silicon carbide fibres in an aluminium/copper alloy matrix

Composite material is composed of SiC fibres with a W core and surrounded by a metallic matrix comprising an alloy whose principal constituent is a metal with poor traction resistance, pref. Al, and a second metal, pref. Cu, whose wt. is 0.5% of the total wt. and which is capable of eliminating from the combination the oxide of the first metal, which would adversely effect the adhesion of the first metal to the fibres.

METHOD OF MANUFACTURING ALUMINIUM-COATED CARBON FIBRE

Improvements with the manufactoring processes of trichite felts

Manufactoring process of a composite material part with nonorganic matrix

Pour fabriquer une pièce en matériau composite à matrice non organique, on réalise tout d'abord un film souple (18), formé de mèches étalées (10) de filaments parallèles (11) revêtus d'un matériau apte à former la matrice, ces filaments étant reliés par un liant provisoire rigidifié, tel que du polystyrène. On drape ensuite des nappes découpées dans le film souple (18), pour former un empilement (20) à partir duquel on réalise une préforme (24) dont l'épaisseur et la forme sont intermédiaires entre celles de l'empilement (20) et celles de la pièce (26) à réaliser. Enfin, on soumet la préforme (24) à un cycle thermomécanique final permettant d'obtenir la pièce (26) et de dégrader le liant provisoire. Pour réaliser la préforme (24), on chauffe l'empilement jusqu'à une température de collage du liant provisoire, on le soumet à une action mécanique de compactage et/ou de formage, et on le refroidit jusqu'au durcissement du liant, tout en maintenant l'action mécanique. To manufacture a part in composite material with an inorganic matrix, a flexible film (18) is first produced, formed of spread strands (10) of parallel filaments (11) coated with a material capable of forming the matrix, these filaments being connected by a stiffened temporary binder, such as polystyrene. Plies cut in the flexible film (18) are then draped to form a stack (20) from which a preform (24) is produced, the thickness and shape of which are intermediate between those of the stack (20) and those of the part (26) to be produced. Finally, the preform (24) is subjected to a final thermomechanical cycle making it possible to obtain the part (26) and to degrade the temporary binder. To make the preform (24), the stack is heated to a temperature for bonding the temporary binder, it is subjected to a mechanical compacting and / or forming action, and it is cooled until the binder hardens, while maintaining the mechanical action.

COMPOSITE EUTECTIC ALLOY AND ARTICLE

METALLIC COMPOSITE MATERIAL AND METHOD FOR PRODUCING THE SAME

NICKEL-TANTALUM BASE ALLOY

Hard metal sintered hard material and a metal binder

METHOD FOR PRODUCING FIBER REINFORCED METAL(FRM) WITH DICASTING MACHINE

The method comprises the steps of: preheating dies by pouring Al molten in the diecasting machine; taking out solidified molten metal from the dies and putting it in a molten metal furnace again; supplying Al molten metal thorough a gate; pressing and impregnating Al molten metal into a preformed body in the dies; opening dies right and left and separating molds. Copyright 1997 KIPO ...

Potassium hexatitanate fibers for use as reinforcement

Reinforcement potassium hexatitanate fiber having an average fiber length of 8-30 μm, an average fiber diameter of 0.2-0.7 μm and a specific surface area of 2-4 m2 /g and a composite materials comprising the whiskers and a light alloy or thermoplastic resin. Also disclosed a process for producing the whiskers.

Method for forming refractory fibers by laser energy

Method and apparatus for forming fibers of refractory materials. A melt volume is continuously formed on a feed rod of the material to be fiberized and a fiber drawn therefrom. The melt volume is formed by introducing the feed rod at a predetermined velocity into a heating zone. The fiber diameter is determined by the relative velocities at which the feed rod is moved and the fiber drawn, and by the fractional density of the feed rod material.

Method of manufacturing parts made of a composite material having a metallic matrix

A method of manufacturing a part made of a composite material having a metallic matrix, for example of titanium or a titanium based alloy, comprises depositing the matrix material on a continuous length of reinforcing fiber, for example of the SiC type, to produce a coating of a predetermined thickness, winding the thus coated fiber onto a former of suitable shape until a desired thickness is obtained, and then heating and isostatically compacting the wound coated fiber to produce the required part.

Production of a solid material in parallelepipedal or cylindrical shape, laminated, sintered, cut-up and thermally treated

MATERIAL FOR THE PREPARATION OF SINTERED COMPOSITE MATERIALS

The present invention relates to a composite base material for the preparation of composite sintered materials reinforced with long fibres, characterized in that said matrix is formed from a combination of a polymer organic material and/or a ceramic-type mineral material and a metal material, preferably intimately mixed. It also relates to materials resulting from the sintering of such base materials, the method for fabricating and utilizing said materials in a field of aircraft engineering, aerospace or high speed vehicles, such as TGV (high speed train), or in the car industry, or in inflammable products.

CHORDAL PREFORMS FOR FIBER-REINFORCED ARTICLES AND METHOD FOR THE PRODUCTION THEREOF

METAL MATRIX COMPOSITE MATERIAL ENHANCED IN STRENGTH, DAMPING CAPACITY, RADIATION RESISTANCE AND CORROSION RESISTANCE

PURPOSE: To provide a metal matrix composite material enhanced in strength, damping capacity, radiation resistance and a corrosion resistance. CONSTITUTION: This metal matrix composite material contg. a shape memory element is the one in which the deformation stress (resistance) on the low temp. side before the inverse transformation of the shape memory alloy material element 1 produced by a rapid solidifying method or the like and imparted with high performance is lower than that of a mother phase metal 2 which is the amorphous one or the one constituted of nonocrystalline substance, and inversely, the shape memory recovering power and deformation stress (resistance) on the high temp. side after the completion of inverse transformation are higher than those of the mother phase metal. The metal matrix composite material is one in which the material performance of the mixed shape memory alloy element and metal mother phase produced by a rapid solidifying method or the like are made use for ...

CONNECTING ROD MADE OF COMPOSITE MATERIAL FOR INTERNAL COMBUSTION ENGINE

PURPOSE: To enable normal operation of an engine for a long period by compositely reinforcing a portion around a piston pin hole and through-holes for bolts of a connecting rod made of composite material including aluminum alloy as matrix by the use of silicon carbide whisker with a specified volmetric ratio. CONSTITUTION: In a connecting rod for an internal combustion engine made of composite material including aluminum alloy as matrix, a portion around a piston pin hole 34a, the main body of the connecting rod, and portion around holes 44, 46 for a bolt which fastens and fixes the connecting rods to each other are reinforced by silicon carbide whisker or silicon carbide particle having 30 to 40% of volmetric ratio. A thermal expansion coefficient is thus set to 15 × 10-6/°C or lower. As a result, when an engine is operated for a long period under a high load and the temperature of the connecting rod is increased, deterioration of a press-in condition of the piston pin or settling of a ...

FIBER REINFORCED COMPOSITE USING CONTROLLED FIBER WITH FINE STRUCTURE

PROBLEM TO BE SOLVED: To obtain a lightweight composite material excellent in strength and toughness without changing its composition by reinforcing a metal by the use of respective pitch-based carbon fibers of radial structure, onion structure, or random structure, respectively. SOLUTION: Metals (Al, Ti, etc.), are reinforced by mixing by using respective pitch-based carbon fibers of radial structure (a structure where the carbon hexagonal net plane of a carbon fiber takes a radiate form with respect to the central axis of the fiber), onion structure (a structure where the carbon hexagonal net plane of a carbon fiber takes a concentrically circular form with respect to the central axis of the fiber), or random structure (a structure where the carbon hexagonal net plane of a carbon fiber takes a random form with respect to the central axis), respectively, or, metals are reinforced by mixing by using a carbon fiber where the crystal size of graphite crystallites is regulated to 7 to 18 nm ...

DRY FRICTION MATERIAL

PURPOSE: To obtain the dry friction material with the wear resistance improved in the light and medium load regions by preparing a dry friction material contg. tin specifying the m.p, and Mohs hardness. CONSTITUTION: An alloy (copper-tin alloy, copper-nickel-tin alloy, etc.) contg. about 10-60wt.% tin and having ≥500°C m.p. and ≥4 Mohs hardness is prepared, and a dry friction material contg. 2-20wt.% of the alloy is prepared. A fiber base material (aromatic polyamide fiber, etc.), a binder (phenolic resin, etc.), a friction conditioner (graphite, etc.), a filler (barium sulfate, etc.), etc., are used for the dry friction material in addition to the tin alloy. A dry friction material is obtained in this way with the friction performance improved. COPYRIGHT: (C)1993,JPO&Japio ...

FIBER-REINFORCED METALLIC FORMED BODY

PURPOSE: To obtain a formed body which does not break even if used for joining of members different from each other in coefficient of thermal expansion by changing the aspect ratios of whiskers on one end face and other end face sides of a formed body in the titled formed body, for use in supporting electrodes, etc., for semiconductor device, in which ceramic or C whiskers are dispersed. CONSTITUTION: A fiber-reinforced metallic formed body 1 is the one disklike in the whole shape in which SiC whiskers, for example, are dispersed in a copper matrix and, in this formed body 1, the lower part A, central part B and upper part C are filled with Si whiskers having aspect ratios (ratio of length to diameter) of 80W100, 60W80 and 40W60 in 30%, 40% and 50% volume content, respectively. In order to manufacture the formed body 1, the whiskers in which aspect ratios are made to vary by changing grain growth conditions in a whisker fiber making process are classified into the above mentioned large, ...

ALUMINUM COMPOSITE MATERIAL EXCELLENT IN WEAR RESISTANCE AND VIBRATION ATTENUATING CAPACITY

PURPOSE: To provide an aluminum composite material excellent in light weightness, ware resistance, vibration attenuating property and scuffing resistance obtained, by dispersing activated carbon and granular or fibrous ceramic in an aluminum alloy base material in specific amounts. CONSTITUTION: An aluminum composite material is obtained by dispersing 1W 10wt% activated carbon and 0.5W20wt% ceramic in an aluminum alloy base material and, as the ceramic, one kind or more of the ceramic selected from Al2O3, SiO2, ZrO2, MgO, SiC, Si3N4, TiM, AlN, TiC, WC, B4C and BN is used in a granular form with an average particle size of 0.05W800μm and/or in a fibrous form with a length of below 3,000μm. The activated carbon has excellent the wear resistence and high vibration attenuating capacity based on viscous fluidity generated at the wide range interface with an alloy materix as a solid lubricant and the ceramic enhances the wear resistence or scuffing resistance without lowerting the capacity of ...

СПОСОБ ПОЛУЧЕНИЯ КОМПОЗИЦИОННОГО МАТЕРИАЛА С ВНУТРЕННИМИ ПОЛОСТЯМИ

Изобретение относится к способам получения слоистых композиционных материалов с внутренними полостями, в частности к способам получения внутренних полостей в конструкционных элементах, выполненных из слоистых композиционных материалов, например в лопатках вентиляторов ГТД, применяемых в авиационной промышленности, судостроении, энергетическом машиностроении. Для получения композиционного материала с внутренними полостями сложной формы, сохраняющего свои высокие механические свойства при получении этих полостей и не требующего высоких затрат, элементы опорного каркаса выполнены путем укладки монослоев волокнистого композиционного материала с металлической матрицей, а удаляемые вставки имеют те же характеристики уплотняемости, что и слоистый волокнистый композиционный материал. Для получения композиционного материала с наружной оболочкой заготовку размещают между элементами наружной оболочки и одновременно с прессованием заготовки дополнительно проводят операцию диффузионной сварки армирующих ...

Composite material used in the assembly of electrical components comprises fibers in the upper surfaces horizontally orientated to a reference surface and the fibers in the lower surfaces orientated vertically to the reference surface

Composite material (1) comprises several fiber surfaces in which fibers (6) in the upper surfaces (13) are horizontally orientated to a first reference surface and the fibers (6) in the lower surfaces (14) are orientated vertically to the first reference surface. An independent claim is also included for a floor plate for assembly electrical components.

Anorganisches poröses Material und dieses enthaltendes Metallmatrixverbundmaterial und Herstellungsverfahren

VERFAHREN ZUR HERSTELLUNG EINES DUKTILEN SILBER-METALLOXID-HALBZEUGS

VERSTAERKTER KOLBEN

VERFAHREN ZUR HERSTELLUNG VON GRENZFLAECHENSCHICHTEN IN VERBUNDWERKSTOFFEN

KALIUMHEXATITANATFASERN UND DIESE FASERN ENTHALTENDES MATERIAL.

VORRICHTUNG ZUR HERSTELLUNG VON HALBZEUGEN UND FORMTEILEN AUS METALLISCHEM MATERIAL

HERSTELLUNG VON SINTERVERBUNDWERKSTOFFEN

NEUE KOHLENFASERN, VERFAHREN ZU IHRER HERSTELLUNG UND DIESE ENTHALTENDE ZUSAMMENSETZUNGEN

Woven and packed composite constructions

Improvements in and relating to copper/iron/aluminium alloys

... 1,137,123. Washing at specified temperatures. NATIONAL RESEARCH DEVELOPMENT CORP. 17 Dec., 1965 [22 Dec., 1964], No. 52152/64. Heading B3V. [Also in Division C7] An alloy consists of the balance, apart from impurities and incidental elements, being copper in an amount of 35-75% and comprises a matrix of a copper rich solid solution phase containing 5-10% Al containing therein, in the form of a fibre, an iron rich solid solution phase containing 10- 20% A1. The required microstructure may be produced by cold working as by hydrostatic extrusion but is preferably done by hot working as by extrusion or rolling above 500‹ C. e.g. at 600-950‹ C. which treatment may be followed by cold working, as by rolling or swageing to further develop the structure. The alloy may then be annealed at 520‹ C. and water quenched or at 800‹ C. followed by furnace cooling.

FIBRE-REINFORCED METAL COMPOSITE MATERIAL

Metal composite material with fiber-reinforcement

A fiber-reinforced metal composite material comprising a metal or alloy as the matrix and an inorganic fiber as the reinforcing material, characterized in that at least one element selected from the group consisting of tin, cadmium and antimony in the form of simple substance or organic or inorganic compound is incorporated into the matrix metal in an amount of 0.0005 to 10% by weight (calculated in terms of the element) so as to enhance the mechanical strength of the composite material.

Composite construction with oriented microstructure

METAL MATRIX COMPOSITES

MATRIX-COATED REINFORCEMENT FOR PRODUCTION OF METAL MATRIX COMPOSITES

COMPOSITE MATERIAL COMPRISING REINFORCED ALUMINUM OR ALUMINUM-BASE ALLOY

... 1484980 Alumina based fibres SUMITOMO CHEMICAL CO Ltd 7 Feb 1975 [8 Feb 1974] 5315/75 Heading C1A [Also in Divisions C7 and B3] An alumina fibre or an alumina-silica fibre which fibre comprises from 72 to 100% by weight of alumina and 0 to 28% by weight of silica and gives rise to substantially no alumina reflection when examined by X-ray diffraction is used to reinforce aluminium base alloy (see Division C7). The fibre may be produced by spinning a solution of poly aluminoxane or a mixture thereof with one or more silicon containing compounds (e.g. polyorganosiloxane, polysilicic acid ester, organosilane) in a solvent (e.g. ethyl ether, tetrahydrofuran, dioxane, benzene, toluene, xylene or mixture thereof) and calcining the fibres, by dipping organic fibre into a solution of aluminium salt and a solution of silicon and calcining the resulting impregnated fibre, by mixing alumina sol or aluminium salt with silica sol or ethyl silicate and a solution of polyethylene oxide or polyvinyl alcohol ...

TANTALUM FIBER AND THEREBY MANUFACTURED CONDENSERS

PRODUCTION OF SINTER COMPOSITE MATERIALS

Procedure for the production of silicon carbide crystals

From hard materials and binder existing sintered hardmetal and procedure for its production

Procedure for the production of a metal carbon fiber composite material

Procedure for the production of a fireproof fiber

INORGANIC FIBER-REINFORCED METALLIC COMPOSITE MATERIAL

Syntactic Metal Matrix Materials and Methods

A syntactic metal foam composite that is substantially fully dense except for syntactic porosity is formed from a mixture of ceramic microballoons and matrix forming metal. The ceramic microballoons have a uniaxial crush strength and a much higher omniaxial crush strength. The mixture is continuously constrained while it is consolidated. The constraining force is less than the omniaxial crush strength. The substantially fully dense syntactic metal foam composite is then constrained and deformation worked at a substantially constant volume. The deformation working is typically performed at a yield strength that is adjusted by way of selecting a working temperature at which the yield strength is approximately less than the omniaxial crush strength of the included ceramic microballoons. This deformation causes at least work hardening and grain refinement in the matrix metal. 115-. (canceled)16. A method for forming a syntactic metal foam composite that is substantially free of non-syntactic porosity comprising:providing ceramic microballoons;applying a metal coating to an outer surface of said ceramic microballoons to form metal-coated microballoons;particle cladding said metal-coated microballoons with a matrix-forming metallic material to form cladded metal-coated microballoons;consolidating said cladded metal-coated microballoons to form a green preform;sintering said green preform to form said syntactic metal foam, said syntactic metal foam formed of said ceramic microballoons and a metal matrix positioned between said ceramic microballoons, said syntactic metal foam having both syntactic and non-syntactic porosity, said syntactic porosity provided by said ceramic microballoons, said syntactic porosity having a syntactic porosity volume, said ceramic microballoons having an average unconstrained uniaxial crush strength, and an average omniaxial crush strength that is greater than said average unconstrained uniaxial crush strength, said metal matrix having a yield ...

SYNTACTIC METAL MATRIX MATERIALS AND METHODS

A syntactic metal foam composite that is substantially fully dense except for syntactic porosity is formed from a mixture of ceramic microballoons and matrix forming metal. The ceramic microballoons have a uniaxial crush strength and a much higher omniaxial crush strength. The mixture is continuously constrained while it is consolidated. The constraining force is less than the omniaxial crush strength. The substantially fully dense syntactic metal foam composite is then constrained and deformation worked at a substantially constant volume. The deformation working is typically performed at a yield strength that is adjusted by way of selecting a working temperature at which the yield strength is approximately less than the omniaxial crush strength of the included ceramic microballoons. This deformation causes at least work hardening and grain refinement in the matrix metal. 1. A deformed syntactic metal foam composite formed of metal-coated microballoons and a metal matrix material that have been sintered together , a plurality of said metal-coated microballoons wherein each is formed of a ceramic microballoon coated with a metal material having a different composition from said ceramic microballoon , said ceramic microballoons having an average particle size of 1 to 500 microns , said ceramic microballoon constituting a greater weight percent of said metal-coated microballoon than said coating of metal material , said metal material coating on said ceramic microballoon formed by chemical vapor deposition or by immersion in a metal slurry prior to combining said metal-coated microballoons with said metal matrix material.2. The deformed syntactic metal foam composite as defined in claim 1 , wherein a weight percent of said metal matrix material is greater than a weight percent of said metal-coated microballoons in said article.3. The deformed syntactic metal foam composite as defined in claim 1 , wherein an average particle size of said metal matrix material prior to ...

HYDRIDE-COATED MICROPARTICLES AND METHODS FOR MAKING THE SAME

A metal microparticle coated with metal nanoparticles is disclosed. Some variations provide a material comprising a plurality of microparticles (1 micron to 1 millimeter) containing a metal or metal alloy and coated with a plurality of nanoparticles (less than 1 micron) or nanoparticle inclusions (potentially larger than 1 micron). The invention eliminates non-uniform distribution of sintering aids by attaching them directly to the surface of the microparticles. No method is previously known to exist which can assemble nanoparticle inclusions onto the surface of a metal microparticle. Some variations provide a solid article comprising a material with a metal or metal alloy microparticles coated with metal hydride or metal alloy nanoparticles, wherein the nanoparticles form continuous or periodic inclusions at or near grain boundaries within the microparticles. 1. An additively manufactured solid article comprising at least 0.25 wt % of a material containing a plurality of metal-containing or metal alloy-containing microparticles that are at least partially coated with a plurality of metal-containing nanoparticle inclusions.2. The additively manufactured solid article of claim 1 , wherein said additively manufactured solid article has an equiaxed-grain-growth structure.3. The additively manufactured solid article of claim 1 , wherein said metal-containing nanoparticle inclusions are continuous or periodic inclusions at or near grain boundaries between said metal-containing or metal alloy-containing microparticles.4. The additively manufactured solid article of claim 1 , wherein said metal-containing or metal alloy-containing microparticles are characterized by an average microparticle size between about 1 micron to about 1 millimeter.5. The additively manufactured solid article of claim 1 , wherein said metal-containing nanoparticle inclusions are characterized by an average nanoparticle size less than 1 micron.6. The additively manufactured solid article of claim 1 ...

Low Thermal Stress Metal Structures

A structured three-phase composite which include a metal phase, a ceramic phase, and a gas phase that are arranged to create a composite having low thermal conductivity, having controlled stiffness, and a CTE to reduce thermal stresses in the composite when exposed to cyclic thermal loads. The structured three-phase composite is useful for use in structures such as, but not limited to, heat shields, cryotanks, high speed engine ducts, exhaust-impinged structures, and high speed and reentry aeroshells. 1. A three- or more phase composite which includes a ceramic phase , a gas phase , and a metal phase , where said gas and ceramic phases are segregated into isolated pockets forming a discontinuous phase in said composite , said metal phase is continuous phase in said composite , said composite having a combination of compression modulus and coefficient of thermal expansion that combined to be at least 40% less than a modulus of said metal forming said metal phase , said composite also having a thermal conductivity that is at least 40% less than a thermal conductivity of said metal that forms said metal phase , said composite having a density that is at least 20% lower than a density of said metal that forms said metal phase.2. The three-phase composite as defined in claim 1 , wherein a plurality of said ceramic phase is formed of ceramic particles that include a central cavity or plurality of cavities that are filled with a portion of said gas phase.3. The three-phase composite as defined in claim 1 , wherein said ceramic phase is formed of one or more materials selected from the group consisting of carbon claim 1 , SiAlON claim 1 , SiN claim 1 , SiC claim 1 , SiOC claim 1 , SiO claim 1 , AlO claim 1 , aluminates claim 1 , zirconates claim 1 , aluminosilicates claim 1 , and ZrO4. The three-phase composite as defined in claim 1 , wherein said gas phase is a vacuum that does not include a gas or includes one or more gasses selected from the group consisting of air claim ...

Composite and multilayered silver films for joining electrical and mechanical components

Materials for die attachment such as silver sintering films may include reinforcing, modifying particles for enhanced performance. Methods for die attachment may involve the of such materials.

HYDRIDE-COATED MICROPARTICLES AND METHODS FOR MAKING THE SAME

A metal microparticle coated with metal hydride nanoparticles is disclosed. Some variations provide a material comprising a plurality of microparticles (1 micron to 1 millimeter) containing a metal or metal alloy and coated with a plurality of nanoparticles (less than 1 micron) containing a metal hydride or metal alloy hydride. The invention eliminates non-uniform distribution of sintering aids by attaching them directly to the surface of the microparticles. No method is previously known to exist which can assemble nanoparticle metal hydrides onto the surface of a metal microparticle. Some variations provide a solid article comprising a material with a metal or metal alloy microparticles coated with metal hydride or metal alloy hydride nanoparticles, wherein the nanoparticles form continuous or periodic inclusions at or near grain boundaries within the microparticles. 1. A material comprising a plurality of non-metallic microparticles that are at least partially coated with a plurality of nanoparticles containing a metal hydride or metal alloy hydride , wherein said microparticles are characterized by an average microparticle size from between 1 micron to about 1 millimeter , and wherein said nanoparticles are characterized by an average nanoparticle size less than 1 micron.2. The material of claim 1 , wherein said material is in powder form.3. The material of claim 1 , wherein said average microparticle size is between about 10 microns to about 500 microns.4. The material of claim 1 , wherein said average nanoparticle size is between about 10 nanometers to about 500 nanometers.5. The material of claim 1 , wherein said plurality of nanoparticles forms a single-layer or multiple-layer nanoparticle coating that is between about 5 nanometers to about 100 microns thick.6. The material of claim 1 , wherein said non-metallic microparticles contain one or more materials selected from the group consisting of a glass claim 1 , a ceramic claim 1 , an organic structure claim 1 ...

Low Thermal Stress Engineered Metal Structures

A structured multi-phase composite which include a metal phase, and a low stiffness, high thermal conductivity phase or encapsulated phase change material, that are arranged to create a composite having high thermal conductivity, having reduced/controlled stiffness, and a low CTE to reduce thermal stresses in the composite when exposed to cyclic thermal loads. The structured multi-phase composite is useful for use in structures such as, but not limited to, high speed engine ducts, exhaust-impinged structures, heat exchangers, electrical boxes, heat sinks, and heat spreaders. 1. An engineered multi-phase composite which includes a high thermal conductivity phase and a metal phase , and wherein said high conductivity phase is segregated into isolated pockets forming a discontinuous phase having equivalent spherical dimensions from 10-400 microns in size and from 20-60 vol. % in said engineered multi-phase composite , said metal phase is a continuous phase in said engineered multi-phase composite , said engineered multi-phase composite has a thermal conductivity that is at least 40% greater than the thermal conductivity of said metal that forms said metal phase.2. The engineered multi-phase composite as defined in claim 1 , wherein said high thermal conductivity phase constitutes 20-50 vol. % of said engineered multi-phase composite claim 1 , said high thermal conductivity phase is optionally formed of ceramic particles that have a lower modulus than said metal forming said metal phase claim 1 , said high thermal conductivity phase is optionally equiaxed or elliptical claim 1 , said high thermal conductivity phase optionally has a thermal conductivity at least two times said metal forming said metal phase claim 1 , said high thermal conductivity phase optionally has a coefficient of thermal expansion (CTE) at least 10% less than the CTE of the metal forming said metal phase.3. The engineered multi-phase composite as defined in claim 1 , wherein said high thermal ...

COMPOSITE AND MULTILA YERED SILVER FILMS FOR JOINING ELECTRICAL AND MECHANICAL COMPONENTS

A silver film for die attachment in the field of microelectronics, wherein the silver film is a multilayer structure comprising a reinforcing silver foil layer between two layers of sinterable particles. Each layer of sinterable particles comprises a mixture of sinterable silver particles and reinforcing particles. The reinforcing particles comprise glass and/or carbon and/or graphite particles. A method for die attachment using a silver film. 1. A silver film , wherein the silver film is a multilayer structure comprising a reinforcing silver foil layer between two layers of sinterable particles wherein each layer of sinterable particles comprises a mixture of sinterable silver particles and reinforcing particles , the reinforcing particles comprising glass and/or carbon and/or graphite particles , wherein the silver film is configured for die attachment by application of heat and pressure to sinter the silver film.2. The silver film of claim 1 , wherein the reinforcing particles comprise said glass particles.3. The silver film of claim 1 , wherein the reinforcing particles consist of said glass particles.4. The silver film of claim 1 , wherein the reinforcing particles comprise said carbon particles.5. The silver film of claim 1 , wherein the reinforcing particles consist of said carbon particles.6. The silver film of wherein the reinforcing particles comprise said graphite particles.7. The silver film of claim 1 , wherein the reinforcing particles consist of said graphite particles.8. The silver film of claim 1 , wherein the reinforcing silver foil layer is configured to support the sinterable silver particles layer and the reinforcing particles.9. The silver film of claim 1 , wherein the reinforcing particles are selected from the group consisting of spheres claim 1 , flakes claim 1 , fibers claim 1 , flowers claim 1 , nanowire claim 1 , and combinations thereof.10. The silver film of claim 1 , wherein the reinforcing particles have a particle size between 2 nm ...

HYDRIDE-COATED MICROPARTICLES AND METHODS FOR MAKING THE SAME

A metal microparticle coated with metal hydride nanoparticles is disclosed. Some variations provide a material comprising a plurality of microparticles (1 micron to 1 millimeter) containing a metal or metal alloy and coated with a plurality of nanoparticles (less than 1 micron) containing a metal hydride or metal alloy hydride. The invention eliminates non-uniform distribution of sintering aids by attaching them directly to the surface of the microparticles. No method is previously known to exist which can assemble nanoparticle metal hydrides onto the surface of a metal microparticle. Some variations provide a solid article comprising a material with a metal or metal alloy microparticles coated with metal hydride or metal alloy hydride nanoparticles, wherein the nanoparticles form continuous or periodic inclusions at or near grain boundaries within the microparticles. 1. A material comprising a plurality of non-metallic microparticles that are at least partially coated with a plurality of nanoparticles containing a metal hydride or metal alloy hydride , wherein said microparticles are characterized by an average microparticle size from between 1 micron to about 1 millimeter , wherein said nanoparticles are characterized by an average nanoparticle size less than 1 micron , and wherein said nanoparticles are attached to said microparticles without organic ligands.2. The material of claim 1 , wherein said material is in powder form.3. The material of claim 1 , wherein said average microparticle size is between about 10 microns to about 500 microns.4. The material of claim 1 , wherein said average nanoparticle size is between about 10 nanometers to about 500 nanometers.5. The material of claim 1 , wherein said plurality of nanoparticles forms a single-layer or multiple-layer nanoparticle coating that is between about 5 nanometers to about 100 microns thick.6. The material of claim 1 , wherein said non-metallic microparticles contain one or more materials selected from ...

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

Composite metal material and method of producing the same

電気部品および機械部品を接合するための複合物および複層銀膜

METHOD FOR PRODUCING A TOOL PART

Composite and multilayered silver films for joining electrical and mechanical components

향상된 성능을 위해, 본 발명의 실버 소결 필름 등의 다이 부착용 재료는 보강, 변형 입자를 포함할 수 있다. 다이 부착을 위한 방법은 이러한 재료를 포함할 수 있다. For improved performance, the die attach material, such as the silver sintered film of the present invention, may include reinforcing, deformable particles. Methods for die attach can include such materials.

Vanadium alloy high-performance cable

本发明公开了一种钒合金高性能电缆，它是由电缆线芯以及电缆线芯外部包裹的橡胶保护套组成，所述电缆线芯的原料按重量份的组分为：铜200-240份、铝100-140份、钒4-6份、纳米二氧化钛8-12份、镍1-3份、硼1-3份、锡1-3份、玻璃纤维6-10份、有机硅1-3份。该电缆导电性能好，具有优良的磁屏蔽性能，用途广泛，主要运用于发电、冶金、化工石油等领域，同时，本发明还具有防火、防水，耐磨，耐高温，防寒抗冻，耐酸碱，耐腐蚀，防静电等性能。

Fiber-reinforced metal

내용 없음. No content.

Heat resistant spring

The method of obtaining materials

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).

A kind of ceramic metal flange

本发明公开了一种金属陶瓷法兰，其特征在于：包括30‑50份陶瓷，8‑12份Co，10‑30份AI 2 O 3 ，5‑10份W，1‑3份Nb，2‑6份H 53 Mn 15 Si 26 ，1‑5份FeSi 2 ，1‑5份MoSi 2 ，5‑10份石墨纤维，5‑10份碳化硅纤维，还包括2‑5份的Ni，所述陶瓷中含有20‑30份的TiC，所述陶瓷优选为40份，所述AI 2 O 3 优选为25份，所述还包括0.5‑1份的稳定剂。本发明硬度高、不易生锈，相对不锈钢和碳钢的重量轻，而且原料和运输成本都相对较低，可以一次加工多个，节约生产时间。

Method of making a tool component

在一种用于生产工具零件的方法中，使多根纤维形成一纤维束。每根纤维具有一芯部和一涂层，芯部包括超硬磨粒或超硬磨粒前体的团块，以及一可选择采用的第二相，所述涂层包括碳化物颗粒和细粒粘合金属的混合物。在挤压纤维束后，纤维束在与其长度成横向的方向上被切断以形成一个层(24)。该层(24)被放在一基底(28)的表面上，使层(24)和基底(28)承受高温高压状态，在该状态下使超硬磨粒结晶稳定。在该方法中，芯部和涂层的组成可以互换。

Metal particles and method of making the same

Verfahren zum Herstellen von Metallteilchen mit den Schritten: Elektrolysieren einer elektrolytischen Lösung, in der die mikrofeinen Kohlenstofffasern dispergiert sind, so daß auf einer Kathode Metallteilchen, in denen die mikrofeinen Kohlenstofffasern eingelagert sind, abgelagert werden und Abtrennen der abgelagerten Metallteilchen von der Kathode.

A kind of vehicle sliding moving fork material prescription

本发明涉及一种汽车滑动叉材料配方，按照重量份比例包括：钢纤维28~44份、碳粉18~24份、氧化钠6~12份、氧化铁15~24份、铜12~35份、氢氧化铝7~14份、硫酸钡23~28份、氧化钾6~28份、锰12~24份、镓1~5份、铟2~8份、铍2~4份和二氧化硅24~26份。本发明提供的配方配比，通过将钢纤维、碳粉、氧化钠、氧化铁、铜、氢氧化铝、硫酸钡、氧化钾、锰、镓、铟、铍和二氧化硅按照配比生产出来的汽车滑动叉，其耐磨度大大增加，从而大大延长其使用寿命，不需要经常更换和维修，节约大量资源和成本。

Composite and multilayered silver films for joining electrical and mechanical components

향상된 성능을 위해, 본 발명의 실버 소결 필름 등의 다이 부착용 재료는 보강, 변형 입자를 포함할 수 있다. 다이 부착을 위한 방법은 이러한 재료를 포함할 수 있다.

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。

Fiber molding for fiber reinforced metal

Syntactic metal matrix materials and methods

A syntactic metal foam composite that is substantially fully dense except for syntactic porosity is formed from a mixture of ceramic microballoons and matrix forming metal. The ceramic microballoons have a uniaxial crush strength and a much higher omniaxial crush strength. The mixture is continuously constrained while it is consolidated. The constraining force is less than the omniaxial crush strength. The substantially fully dense syntactic metal foam composite is then constrained and deformation worked at a substantially constant volume. The deformation working is typically performed at a yield strength that is adjusted by way of selecting a working temperature at which the yield strength is approximately less than the omniaxial crush strength of the included ceramic microballoons. This deformation causes at least work hardening and grain refinement in the matrix metal.

FIBER-REINFORCED METAL COMPOSITE MATERIAL INCLUDING IN PARTICULAR GROUP IA OR GROUP IIA ELEMENTS OF THE PERIODIC CLASSIFICATION TABLE

DES MATIERES COMPOSITES METALLIQUES RENFORCEES PAR DES FIBRES, COMPRENANT UN METAL OU UN ALLIAGE EN TANT QUE MATRICE ET DES FIBRES MINERALES EN TANT QUE MATIERE DE RENFORCEMENT, SONT TELLES QU'AU MOINS UN ELEMENT CHOISI DANS LE GROUPE SE COMPOSANT D'ELEMENTS APPARTENANT A LA QUATRIEME PERIODE OU A DES PERIODES SUPERIEURES DU GROUPE IA DU TABLEAU DE CLASSIFICATION PERIODIQUE, D'ELEMENTS APPARTENANT A LA CINQUIEME PERIODE OU A DES PERIODES SUPERIEURES DU GROUPE IIA DU TABLEAU DE CLASSIFICATION PERIODIQUE, DE BI ET D'IN, SOUS LA FORME DE SUBSTANCE SIMPLE OU DE COMPOSE ORGANIQUE OU MINERAL, EST INCORPORE DANS LE METAL DE MATRICE OU DANS LA MATIERE DE RENFORCEMENT OU DANS LES DEUX, EN QUANTITE DE 0,0005 A 10 EN POIDS (CALCULEE SOUS FORME DE L'ELEMENT) AFIN DE RENFORCER LA RESISTANCE MECANIQUE DE LA MATIERE COMPOSITE. FIBER REINFORCED METAL COMPOSITE MATERIALS, COMPRISING A METAL OR ALLOY AS A MATRIX AND MINERAL FIBERS AS A REINFORCING MATERIAL, ARE SUCH AS AT LEAST ONE CHOSEN ELEMENT FROM THE GROUP CONSISTING OF ELEMENTS BELONGING TO THE FOURTH PERIOD OR UPPER PERIODS OF GROUP IA OF THE PERIODIC CLASSIFICATION TABLE, OF ELEMENTS BELONGING TO THE FIFTH PERIOD OR UPPER PERIODS OF GROUP IIA OF THE PERIODIC CLASSIFICATION TABLE, BI AND SUBSTANCE, IN THE FORMAT SIMPLE OR OF ORGANIC OR MINERAL COMPOUND, IS INCORPORATED IN THE MATRIX METAL OR IN THE REINFORCING MATERIAL OR BOTH, IN QUANTITIES OF 0.0005 TO 10 BY WEIGHT (CALCULATED AS THE ELEMENT) IN ORDER TO REINFORCE THE STRENGTH MECHANICS OF COMPOSITE MATERIAL.

Fibre reinforced ductile metal or alloy - prepd from a mixt of metal and fibre-forming substance which is compacted and hot deformed

The fibre-forming substance such as glass, porcelain-type enamel, B oxide, a metal salt, or a ceramic, is mixed with the metal and the mixt. is compressed. The compact is then hot deformed by drawing, extruding, spinning or rolling so that its cross section is reduced at least in one direction. A fibre-forming substance is chosen which has a softening temp. of 300-600 degrees C. Pref. the fibre reinforced metal is produced in a single operation by using the components in powder form or by introducing the fibre-forming substance into the metal bath which is stirred, or by preparing a dispersion and casting the dispersion into a mould followed by controlled cooling.

PROCESS FOR MANUFACTURING A SILICON COMPOSITE PART REINFORCED WITH SILICON CARBIDE FILAMENTS

A method is described for making a shaped silicon carbide-silicon matrix composite. A confined carbon fiber preform is infiltrated with sufficient molten silicon metal at a temperature in the range of from about 1400 DEG C. to about 1800 DEG C. in an inert atmosphere or vacuum.

Improving tensile strength of boron filaments - by maintaining the filaments under tension in nitrogen

The tensile strength of B filaments is increased by maintaining the filaments under tesion at 200-350 degrees F in a pure N2 atmosphere for a time insufficient to form a nitride. Used in the production of B filament composite impregnated with a resin or metal matrix. The process stress-relieves the filaments and the N2 heals any surface defects.

COMPOSITE METAL COMPONENTS, ESPECIALLY FOR NUCLEAR REACTORS

Electric contact of silver-tin oxide fibre composite - for circuit breakers of 40-400 a rating and 50-500 gauss blowout field strength

Electric contact, eps. for circuit brakers rated at 40-4000 amps. at a magnetic blowout field strength of 50-500 gauss, consists, at least in the contact layer, of a composite of Ag and fibrous embedded SnO2, the SnO2 fibres being aligned parallel and perpendicular to the switching plane. These fibres pref. are 1-15 mu m long and are present in an amt. of 12-18 wt.%. Much lower spark loss then with the conventional Ag/CdO or other metal oxide contacts is obtd.

TURBOMACHINE ROTOR COMPRISING AT LEAST ONE REINFORCED DISK BY A COMPOSITE RING

Rotor de turbomachine comprenant au moins un disque pourvu d'un anneau constitué par exemple d'une bobine de fil de carbure de silicium ou d'alumine enrobé de métal.Selon l'invention, l'anneau composite (18) est logé dans une cavité annulaire close définie par exemple en usinant une gorge (16) dans une partie élargie (14) du disque et en la refermant par une plaque annulaire (20) après mise en place de l'anneau. Turbomachine rotor comprising at least one disc provided with a ring consisting, for example, of a coil of silicon carbide wire or of alumina coated with metal.According to the invention, the composite ring (18) is housed in a closed annular cavity defined for example by machining a groove (16) in an enlarged portion (14) of the disc and closing it by an annular plate (20) after establishment of the ring.

Dispersion - strengthened aluminium - contg alloy prodn - having superplasticity at elevated temp

The alloy is produced by compacting filaments, fibres or strip of 0.7-2 micron thickness of Al, Al alloy and/or an alloy of Ni, Co, Fe or Cu contg. Al in an atm. which ensures that an Al oxide film is formed on the filaments or fibres. The compact is then sintered. Pref. the filaments are obtd. by melt spinning and are used in the alloy with a length >their width, while the width is > their thickness. The final product contains 1-3 vol. % Al2O3. A heat treatment temp.

Fabrication of components from a composite material

A process is claimed for the fabrication of a component in a composite material with a non-organic matrix in which a flexible film is at first produced, formed from a staggered mesh of parallel filaments coated with a matrix forming material, these filaments being bound by a temporary rigidified binder. Sheets cut in the flexible film are then wrapped in order to form a pile from which a preform is produced with a thickness and shape between that of the pile and the component to be made.Finally the preform is subjected to a thermomechanical cycle to produce the ultimate component and to degrade the temporary binder. In order to produce the preform, the pile is heated to a temp. at which the temporary binder becomes sticky, it is subjected to a mechanical compacting and/or shaping and is cooled to allow the hardening of the binder whilst maintaining the mechanical action.The temporary binder used in the process is pref. a polystyrene.

Patent FR2307358B1

Composite material and methods for making

A composite material has portions of a first material such as a metal or ceramic having coatings of a metal material thereon disposed in a metal matrix material and having a diffusion-bonds between the coating and matrix materials securing the portions of the first material at selected locations in the composite material.

Method of making a tool component

In a method of producing a tool component a plurality of fibres is formed into a bundle. Each fibre has a core comprising a mass of ultra-hard abrasive particles or precursor to said ultra-hard abrasive particles and optionally a second phase, and a coating comprising a mixture of carbide particles and particulate binder metal. After extruding the bundle of fibres, the bundle is severed transverse to its length to produce a layer 24. The layer 24 is placed on a surface 26 of a substrate 28 and the layer 24 and substrate 28 are subjected to elevated temperature and pressure conditions at which the ultra-hard abrasive particles are crystallographically stable. The composition of the core and coating may be interchanged in the method.

Manufacturing process for plates and other lead elements reinforced with mineral fibers

Anti-ballistic materials and methods of making the same

Armoured composite material

Изобретение относитс  к композиционным материалам, которые используютс  в качестве брони. Сущность изобретени : предложенный бронированный материал содержит основу из металлического св зующего , в качестве которого используют по крайней мере одно вещество, выбранное из группы, содержащей алюминиевый сплав, медный сплав, чугун, титан, железо, никель, сталь и керамический наполнитель, в качестве которого используют по крайней мере одно вещество, выбранное из группы, содержащей глинозем магнезию, оксид циркони , карбид кремни , диборид титана, нитрид кремни , диборид титана, нитрид алюмини , додекаборид алюмини , карбид титана, при содержании керамического наполнител  36-72 об.%. 2 з.п. ф-лы, 2 табл.

Composite material made from matrix metal reinforced with mixed crystalline alumina-silica fibers and mineral fibers

This composite material includes reinforcing hybrid fiber mixture material in a matrix of metal which is aluminum, magnesium, copper, zinc, lead, tin, or an alloy having these as principal components. The hybrid fiber mixture is a mixture of crystalline alumina-silica fiber material and mineral fiber material. The crystalline alumina-silica fiber material has as principal components 35% to 80% by weight of Al 2 O 3 and 65% to 20% by weight of SiO 2 , with a content of other substances of less than or equal to 10% by weight, and with the percentage of mullite being greater than or equal to 15% by weight, and with the percentage of non fibrous particles with diameters greater than 150 microns being less than or equal to 5% by weight. And the mineral fiber material has as principal components SiO 2 , CaO, and Al 2 O 3 , the content of MgO being less than or equal to 10% by weight, the content of Fe 2 O 3 being less than or equal to 5% by weight, and the content of other inorganic substances being less than or equal to 10% by weight, with the percentage of non fibrous particles being less than or equal to 20% by weight, and with the percentage of non fibrous particles with diameters greater than 150 microns being less than or equal to 7% by weight. The volume proportion of the reinforcing hybrid fiber material is at least 1%. The qualities of this composite material with regard to wear, wear on a mating member, and bending strength are good.

Fibre composite with a mixed-wire fabric

The fibre composite consists of a metal matrix with embedded strength reinforcing fibres (1). It is characterised by the fact that, before the fibre composite is produced, the fibres (1) form a mixed-wire fabric (3) with wire elements (2). The wire elements (2) are made of the material of the metal matrix, and they serve as a carrier material or a framework for the fibres (1).The mixed-wire fabric (3) consists of orthogonally woven fibres (1) and wire elements (2), with the fibres having a strictly fixed constant distance (a) between them. The metal matrix and hence the wire elements are made of aluminium. The fibres are steel fibres. Alternatively, they are ceramic or carbon fibres.

Method for producing a composite consisting of continuous silicon carbide fibers and metallic silicon

Abstract of the Disclosure Fiber composites having high hardness, mechanical strength, heat resistance, oxidation resistance and corrosion resistance consisting of continuous silicon carbide fibers and metallic silicon.

Patent BE554648A

Composition material

Discontinuous carbon fiber reinforced metal matrix composite

Disclosed are methods and materials for preparing metal matrix composite (MMC) components that have low weight, good thermal conductivity and a controllable in-plane coefficient of thermal expansion. One embodiment of the invention features a metal matrix composite that includes a metal alloy and random in-plane discontinuous fibers. In some embodiments, the metal alloy includes aluminum, copper or magnesium. In certain embodiments, the metal matrix composite includes additives that enable solution hardening. In other embodiments, the metal matrix composite includes additives that enable precipitation hardening. Another embodiment of the invention features a method of manufacturing a metal matrix composite. The method includes contacting random in-plane discontinuous fibers with a binder, and pressurizing the random in-plane discontinuous fibers and the binder to form a bound preform. The preform is pressurized to a pressure greater than the molten metal capillary breakthrough pressure of the bound preform. Subsequently, the bound preform is placed in a mold, infiltrated with a molten infiltrant, and the molten toform infiltrant is cooled the metal matrix composite.

Filament winding for metal matrix composites

A wet filament winding method and apparatus for producing a consolidated metal matrix composite is described. The methods are directed to winding a softened metal infiltrated fiber bundle and layering the resulting softened metal infiltrated fiber bundle onto a rotating mandrel in a prescribed pattern on the surface of the mandrel to form a consolidated metal matrix composite. Upon cooling, the matrix metal solidifies and the resulting consolidated metal matrix composite may be removed from the mandrel. The consolidated metal matrix composites may be produced in a variety of shapes, such as cylinder, a tapered cylinder, a sphere, an ovoid, a cube, a rectangular solid, a polygonal solid, and panels.

Fiber reinforced material with matrix metal containing copper and reinforcing fibers containing alumina

This composite material is composed essentially of a matrix metal which is copper or an alloy thereof, and a reinforcing fiber material which is a collection of alumina - silica type short fibers in which the included amount of alumina is about 40% by weight or more, with the total amount of non fibrous particles included in the collection of fibers being less than or equal to about 7% by weight, with the total amount of non fibrous particles with diameter greater than or equal to about 150 microns included in the collection of fibers being less than or equal to about 1% by weight, and with the volume proportion of the short fiber material being from about 0.5% to about 30%. Optionally and preferably, this volume proportion of short fiber material is from about 1.0% to about 25%, or from about 0.5% to about 10%, or even better from about 1.0% to about 5%. And the total amount of non fibrous particles can be less than or equal to about 4% by weight; and the total amount of non fibrous particles with diameter greater than or equal to about 150 microns can be less than or equal to about 0.6% by weight. The reinforcing fiber material can be fibers containing a substantial amount of silica, or alternatively can be a fiber material substantially made only of alumina; and may contain a substantial amount of, or consist substantially only of, alpha alumina. The matrix material may be pure copper, brass, or bronze.

Composite structure with NbTiAlHfCrV or NbTiAlHfCrVZrC allow matrix and niobium base metal reinforcement

Composite structures having a higher density, stronger reinforcing niobium based alloy embedded within a lower density, lower strength niobium based alloy are provided. The matrix is preferably an alloy having a niobium and titanium base according to the expressions: Nb.sub.balance -Ti.sub.27-40.5 -Al.sub.4.5-10.5 -Hf.sub.1.5-5.5 -Cr 4 .5-7.9 -V 0-6 , or Nb.sub.balance -Ti.sub.27-40.5 -Al.sub.4.5-10.5 -Hf.sub.1.5-5.5 -Cr 4 .5-7.9 -V 0-6 -Zr 0-1 C 0-0 .5. The reinforcement may be in the form of strands of the higher strength, higher temperature niobium based alloy. The same crystal form is present in both the matrix and the reinforcement and is specifically body centered cubic crystal form.

Discontinuous carbon fiber reinforced metal matrix composite

Disclosed are methods and materials for preparing metal matrix composite (MMC) components that have low weight, good thermal conductivity and a controllable in-plane coefficient of thermal expansion. One embodiment of the invention features a metal matrix composite that includes a metal alloy and random in-plane discontinuous fibers. In some embodiments, the metal alloy includes aluminum, copper or magnesium. In certain embodiments, the metal matrix composite includes additives that enable solution hardening. In other embodiments, the metal matrix composite includes additives that enable precipitation hardening. Another embodiment of the invention features a method of manufacturing a metal matrix composite. The method includes contacting random in-plane discontinuous fibers with a binder, and pressurizing the random in-plane discontinuous fibers and the binder to form a bound preform. The preform is pressurized to a pressure greater than the molten metal capillary breakthrough pressure of the bound preform. Subsequently, the bound preform is placed in a mold, infiltrated with a molten infiltrant, and the molten infiltrant is cooled to form the metal matrix composite.

A kind of electric power bar connection bolt material

本发明涉及一种电力杆用连接螺栓材料，它包括镁镍合金48‑63份、锰21‑30份、无氧锌16‑24份、硼酸钛8‑17份、火山岩3‑7份、硅粉2‑5份、矿物纤维1‑2份。本发明易加工，产品机械性能优异，连接强度高。

A kind of wear-resisting grinding drill

本发明公开了一种耐磨的磨削钻头，其按照重量份的组分为：钛钢50重量份、纳米氮化硅8重量份、硬硅钙石20重量份、陶瓷纤维15重量份、基体树脂20重量份、玻璃纤维15份、焦磷酸铁5重量份、三氧化二锑4份、锂3重量份、钛8重量份、钴4重量份、镍20重量份、钇1重量份、钨4重量份、聚丙烯15重量份、磷酸酯5重量份。本发明提供的钻头硬度高、耐磨、耐腐蚀、磨削力小、自锐性好、磨削效率高，使用寿命长。

Composite steel bar.

Method of fabricating a metal aluminide composite

A softer metal such as aluminum, or a metal forming a metal aluminide, or an alloy containing these metals is added to a metal aluminide composite during fabrication to promote easy consolidation of the metal aluminide matrix with the reinforcing phase. The metal aluminide may be titanium aluminide, nickel aluminide, or iron aluminide. The softer metal, the metal aluminide matrix, and the reinforcing phase are pressed together at a temperature above the softening temperature of the softer metal. The softened metal promotes flow and consolidation of the matrix and the reinforcement at relatively low temperatures. The composite is held at an elevated temperature to diffuse and convert the soft metal phase into the metal aluminide matrix. By consolidating at a lower temperature, cracking tendencies due to thermal expansion differences between the matrix and reinforcement is reduced. By consolidating at a lower pressure, mechanical damage to the fibers is avoided.

Method of making a tool component

In a method of producing a tool component a plurality of fibres is formed into a bundle. Each fibre has a core comprising a mass of ultra-hard abrasive particles or precursor to said ultra-hard abrasive particles and optionally a second phase, and a coating comprising a mixture of carbide particles and particulate binder metal. After extruding the bundle of fibres, the bundle is severed transverse to its length to produce a layer 24. The layer 24 is placed on a surface 26 of a substrate 28 and the layer 24 and substrate 28 are subjected to elevated temperature and pressure conditions at which the ultra-hard abrasive particles are crystallographically stable. The composition of the core and coating may be interchanged in the method.

A kind of oil field drilling, well workover clamp compoboard and preparation method thereof with without impression

本发明公开了一种油田钻、修井用无压痕夹持组合板，其特征在于：包括板体和防腐金属粉末层，所述防腐金属粉末层通过高温烧结的方式固定在板体上。本发明的优点是：结构简单、制作工艺简单、易于操作，代替传统牙板使用，具有耐磨、防腐、不损伤管（杆）体等特点。

Clad structural member with nbtialcr hf alloy cladding and niobium base metal core

CLAD STRCUTURAL MEMBER WITH NbTiAlCr Hf ALLOY CLADDING AND NIOBIUM BAS METAL CORE ABSTRACT OF THE DISCLOSURE Composite structures having a higher density, stronger reinforcing niobium based alloy embedded within a lower density, lower strength niobium based cladding alloy are provided. The cladding is preferably an alloy having a niobium and titanium base according to the expression: Nb-Ti27-40.5-Al4.5-10.5-Hf1.5-5.5V0-6Cr4.5-8.5Zr0-1C0-0.5, where each metal of the metal/metal composite has a body centered cubic crystal structure, and wherein the ratio of concentrations of Ti to Nb (Ti/Nb) is greater than or equal (?) to 0.5, and wherein the maximum concentration of the Hf+V+Al+Cr additives is less than or equal (?) to the expression: 16.5 + 5 x Ti/Nb . The reinforcement may be in the form of plates, sheets or rods of the higher strength, higher temperature niobium based reinforcing alloy. The same crystal form is present in both the matrix and the reinforcement and is specifically body centered cubic crystal form.

COMPOSITION MATERIALS AND THEIR USE.

Patent FR2191996B1

Process for the production of MMC

Continuous silicon carbide fibre-reinforced silver composite - is suitable for electrochemical appts. and structural applications

Fibre-reinforced Ag composite material (I) comprises continuous SiC fibres (II) consisting of beta-Si C, a Ag matrix (III), consisting of Ag, Ag alloy or a Ag-based composite, and very small amts. fo carbide (IVa) or solid C soln. (IVb) in (III). formed by reaction of free C on the (II) surface with (III). The (II) content of (I) pref. is 5-70 wt. %. (I) has excellent mechanical properties, thermal stability resistance to oxidn. and wear and electrical and thermal conductivity and is suitable for a wide range of applicationsin the electrical industry, for chemical equipment and as structural material. Claimed properties are a high oxidn. resistance, Mohs hardness of 3-8, tensile strength of 20-240 kg/mm2 at room temp. resistivity of (2.0-16.1) x 106 ohm.cm and thermal conductivity of 0.85-0.21 cal/cm.s degrees C.

Fiber compound material

The fiber compound material contains at least one fiber component and at least two matrix components of different material classes which have different thermo-mechanical properties. In a manufacture of the compound material two matrix components can be liquefied and fiber filaments of the fiber component can be wetted by the liquefied matrix components. In this in the liquefied state the one matrix component is not soluble in the other. In a consolidation of the compound material one of the previously liquefied matrix components can be hardened out irreversibly to a duroplastic whereas the other of the previously liquefied matrix components remains meltable.

ANTIBALLISTIC MATERIALS.

Solid abrading tool with fiber abrasive

Abrading tools having shaped solid bodies composed of wearable matrix material and embedded fibers of harder abrasive material with ends exposed at the working surfaces of the tools and constituting the abrasive or cutting elements of the tools. In one case, a honing stone has closely spaced cylindrical fibers arranged in rows of fibers substantially perpendicular to the working face, which has a slight transverse curvature, and alternate arrangements inclined relative to the face so that the ends are oval. In another case, an abrading wheel has radial fibers and another has longitudinal fibers for end-working applications. Suitable fiber materials for machining metals may be boron and boron compounds.

Syntactic metal matrix materials and methods

A syntactic metal foam composite that is substantially fully dense except for syntactic porosity is formed from a mixture of ceramic microballoons and matrix forming metal. The ceramic microballoons have a uniaxial crush strength and a much higher omniaxial crush strength. The mixture is continuously constrained while it is consolidated. The constraining force is less than the omniaxial crush strength. The substantially fully dense syntactic metal foam composite is then constrained and deformation worked at a substantially constant volume. The deformation working is typically performed at a yield strength that is adjusted by way of selecting a working temperature at which the yield strength is approximately less than the omniaxial crush strength of the included ceramic microballoons. This deformation causes at least work hardening and grain refinement in the matrix metal.

Heat transfer element, usable in particular in electronics as a printed circuit or component support and its manufacturing process.

Low-wear aluminum-magnesium-nickel alloy bearing and preparation method thereof

本发明公开了一种低磨耗铝镁镍合金轴承，由如下重量份数的成分制备而得：铝锭45‑60份、镍锭26‑34份、镁锭21‑30份、钛粉8‑15份、玻璃纤维3‑10份、高镁白云石5‑11份、硫酸钴9‑14份、钒酸锂2.5‑6份、碳化铌1.7‑4.2份、碘化铽0.4‑3份、铁渣4‑9份、粉煤灰2‑6份、氟锆酸铵3‑5.8份、雏晶黑云母1.2‑5份、硝酸铥0.3‑2份、三氧化二镓1‑3.5份。本发明还公开所述低磨耗铝镁镍合金轴承的制备方法。本发明制备出的合金轴承具有良好的耐磨性、较低的热膨胀系数，较长的使用寿命，以及良好的表观硬度和压溃强度，在轴承领域具有广阔的应用前景。

Composite structure with NbTiAl and high Hf alloy matrix and niobium base metal reinforcement

Composite structures having a higher density, stronger reinforcing niobium based alloy embedded within a lower density, lower strength niobium based alloy are provided. The matrix is preferably an alloy having a niobium and titanium base according to the expression: Nb--Ti.sub.32-45 --Al.sub.3-18 --Hf.sub.8-15 and the reinforcement may be in the form of strands of the higher strength, higher temperature niobium based alloy. The same crystal form is present in both the matrix and the reinforcement and is specifically body centered cubic crystal form.

METALLIC MATERIAL REINFORCED WITH FIBERS OF INORGANIC SUBSTANCES

Zirconium metal matrix-silicon carbide composite nuclear reactor components

A metallic composite material and nuclear components such as fuel cladding, rod guide thimbles, grids and channels made therefrom. The metallic composite material comprises 90-60 volume percent of a metal matrix of zirconium or a zirconium alloy containing homogeneously incorporated, throughout the matrix, 10-40 volume percent of silicon carbide whiskers.

COMPOSITES BASED ON A METAL OR ALLOY AS A BASE AND INORGANIC FIBERS AS A REINFORCING AGENT

The fibre-strengthened metal

本发明涉及一种使纤维复合在金属中从而能获 得金属单独不能达到之物性的纤维强化金属。以前 的纤维强化金属使用碳素纤维，Si-Ti-C-O纤维作 为复合纤维，但对金属的润湿性不好，因而不能得到 高弹性纤维强化金属，而本发明是使用含氮量为8 原子％以上的氧氮化物玻璃纤维作为复合纤维，因 而解决了以前的问题。即本发明之纤维强化金属与 原来的相比较，具有更高的拉伸强度和弹性模量。

metal elements reinforced with glass fibers

Fibre-reinforced metal

A kind of high-strength tenacity base titanium carbonitride material and preparation method thereof

本发明涉及一种高强韧性金属陶瓷材料及其制备方法，属于金属陶瓷材料制备技术领域。所述高强韧性金属陶瓷材料所用原料由以下组份按重量百分比组成：碳氮化钛粉末35～65％；碳氮化钛晶须0.5～8％；M 10～20％，所述M由钴、镍组成；添加剂A10～30％，所述添加剂A由碳化钨、碳化钼组成；余量为碳化钽；各组分重量百分之和为100％；其中，碳氮化钛粉末的粒度为2～4μm，碳氮化钛晶须直径1～2μm，长度15～20μm。其制备方法为：按设计组分配取各原料后，混合均匀并压制成型，然后在1420～1520℃进行烧结；得到成品。本发明组分设计合理，所得产品性能优良，便于大规模的工业化应用和生产。

Thermal transfer element, usable especially in electronics as printed circuit board or component support and its manufacturing method.

L'invention concerne un élément de transfert thermique utilisable notamment comme support ou boîtier de composant(s) électronique(s). Cet élément comprend un film de diamant (9) au contact d'une source de chaleur telle qu'un composant électronique (11), ce film étant disposé sur une âme (1) en matériau composite à matrice métallique (3), par exemple en Mg ou Al, renforcée par des fibres inorganiques (5) par exemple de carbone graphité ou d'alumine, par l'intermédiaire d'une couche d'accrochage 7, par exemple en titane. Un tel élément permet d'assurer un transfert rapide de la chaleur dégagée par le composant (11) vers un puits thermique. The invention relates to a thermal transfer element which can be used in particular as a support or package for electronic component (s). This element comprises a diamond film (9) in contact with a heat source such as an electronic component (11), this film being arranged on a core (1) of composite material with a metal matrix (3), for example. made of Mg or Al, reinforced by inorganic fibers (5), for example of graphitized carbon or of alumina, by means of a tie layer 7, for example of titanium. Such an element ensures rapid transfer of the heat released by the component (11) to a heat sink.

Patent FR2082928A6

HIGH RESISTANCE COMPOSITE MATERIAL SHAPED IN METAL AND FIBERS

A kind of high-strength wearable carbide-base ceramics bearing and preparation method thereof

本发明公开了一种高强耐磨碳化物基金属陶瓷轴承及其制备方法，该高强耐磨碳化物基金属陶瓷轴承由下列重量份的原料制成：碳化钛50‑60份、铁粉40‑50份、雄黄粉3‑8份、地开石粉3‑11份、磁铁矿粉10‑20份、氧化钇2‑8份、碱式碳酸镍1‑6份、纳米硼纤维6‑8份、氧化钇4‑8份、合成蜡12‑16份。本发明方法制得的高强耐磨碳化物基金属陶瓷轴承与传统的金属陶瓷轴承相比，具有更好强度、抗磨性和耐热性，使得轴承在高温条件下不变形，不易磨损，且制备工艺简单、加工成本低，参数易控，生产过程安全环保，适合大规模的工业化生产。

Molded body with a surface that is highly wear-resistant against mechanical abrasion

A kind of composite titan-based rotor material of high speed centrifuge pull resistance and preparation method thereof

本发明公开了一种高速离心机用抗拉性复合钛基转子材料，由下列重量份的原料制成：钛合金20‑35份、铝合金10‑16份、钢5‑10份、硼纤维10‑17份、碳化硅3‑7份、碳化钛5‑10份、碳化铋2‑5份、硅酸钙5‑19份、二氧化锰5‑7份、氧化锆3‑9份、氧化锌5‑8份、硼酸镁3‑7份、五氧化二钒3‑6份、硬脂酸锌3‑6份、二硼化钒3‑4份、氟硼酸钾7‑15份、聚氧乙烯树脂5‑12份、磷钨酸钾2‑7份、抗氧化剂5‑10份、热稳定剂5‑10份。制备而成的高速离心机用抗拉性复合钛基转子材料，其耐腐蚀好、抗拉强度高、硬度高、高温下不变形。同时，还公开了相应的制备方法。

Turbine engine rotor comprising at least one disk reinforced with a composite ring

Rotor de turbomachine comprenant au moins un disque pourvu d'un anneau constitué par exemple d'une bobine de fil de carbure de silicium ou d'alumine enrobé de métal. Selon l'invention, l'anneau composite (18) est logé dans une cavité annulaire close définie par exemple en usinant une gorge (16) dans une partie élargie (14) du disque et en la refermant par une plaque annulaire (20) après mise en place de l'anneau. Turbomachine rotor comprising at least one disc provided with a ring consisting for example of a coil of silicon carbide wire or alumina coated with metal. According to the invention, the composite ring (18) is housed in a closed annular cavity defined for example by machining a groove (16) in an enlarged portion (14) of the disc and closing it by an annular plate (20) after setting up the ring.

Patent JPH0359969B2

METALLIC MATERIAL REINFORCED WITH FIBERS OF INORGANIC SUBSTANCES

Boron carbide fiber production

Boric oxide fibers having a maximum diameter of about 10 microns are heated in an ammonia atmosphere to about 350*-600*C at a rate of temperature rise of up to about 5,000*C/hr. to produce ammonia-treated fibers consisting essentially of B, N. O and H. The ammonia-treated fibers are heated in an amine atmosphere at about 600*-1,000*C to produce amine-treated fibers consisting essentially of B, C, N, O and H and containing at least about 15% C. The amine-treated fibers may be heated at about 2,000*-2,350*C in an inert atmosphere to produce boron carbide fibers.

High-strength metal-fiber composite material

Composite material and method for producing the same

LEAD COMPOSITE MATERIALS OR ITS ALLOYS REINFORCED WITH POWDER AND / OR CERAMIC FIBERS AND USES OF THE SAME

COMPOSITION MATERIALS AND THEIR USE.

Process for producing a composite using potassium hexatitanate whiskers having a tunnel structure

A potassium hexatitanate whisker having a tunnel structure containing aluminum and niobium impurities in such amounts that Al 2 O 3 /Nb 2 O 3 molar ratio is 0.6 or higher and composite materials using the same. Also disclosed are processes for producing composite materials using the potassium hexatitanate whiskers having a tunnel structure with a light alloy or a thermoplastic resin.

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.