US20070141315A1 - Metal-based carbon fiber composite material and method for producing the same - Google Patents

Metal-based carbon fiber composite material and method for producing the same Download PDF

Info

Publication number
US20070141315A1
US20070141315A1 US10/582,990 US58299004A US2007141315A1 US 20070141315 A1 US20070141315 A1 US 20070141315A1 US 58299004 A US58299004 A US 58299004A US 2007141315 A1 US2007141315 A1 US 2007141315A1
Authority
US
United States
Prior art keywords
carbon fiber
metal
composite material
based carbon
fiber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US10/582,990
Inventor
Kiminori Sato
Nobuaki Ozoe
Jinichi Ogawa
Toshiyuki Ueno
Satoshi Komatsubara
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shimane Prefecture
Original Assignee
Shimane Prefecture
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shimane Prefecture filed Critical Shimane Prefecture
Assigned to SHIMANE PREFECTURAL GOVERNMENT reassignment SHIMANE PREFECTURAL GOVERNMENT ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: KOMATSUBARA, SATOSHI, OGAWA, JINICHI, OZOE, NOBUAKI, SATO, KIMINORI, UENO, TOSHIYUKI
Publication of US20070141315A1 publication Critical patent/US20070141315A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/14Making alloys containing metallic or non-metallic fibres or filaments by powder metallurgy, i.e. by processing mixtures of metal powder and fibres or filaments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B82NANOTECHNOLOGY
    • B82YSPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
    • B82Y10/00Nanotechnology for information processing, storage or transmission, e.g. quantum computing or single electron logic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B82NANOTECHNOLOGY
    • B82YSPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
    • B82Y30/00Nanotechnology for materials or surface science, e.g. nanocomposites
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/02Pretreatment of the fibres or filaments
    • C22C47/025Aligning or orienting the fibres
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C49/00Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/14Alloys containing metallic or non-metallic fibres or filaments characterised by the fibres or filaments
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L23/00Details of semiconductor or other solid state devices
    • H01L23/34Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
    • H01L23/36Selection of materials, or shaping, to facilitate cooling or heating, e.g. heatsinks
    • H01L23/373Cooling facilitated by selection of materials for the device or materials for thermal expansion adaptation, e.g. carbon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • B22F3/105Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
    • B22F2003/1051Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding by electric discharge
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2999/00Aspects linked to processes or compositions used in powder metallurgy
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C26/00Alloys containing diamond or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes
    • C22C2026/002Carbon nanotubes
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L2924/00Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
    • H01L2924/0001Technical content checked by a classifier
    • H01L2924/0002Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Nanotechnology (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Condensed Matter Physics & Semiconductors (AREA)
  • General Physics & Mathematics (AREA)
  • Mathematical Physics (AREA)
  • Theoretical Computer Science (AREA)
  • Composite Materials (AREA)
  • Power Engineering (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Computer Hardware Design (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
  • Powder Metallurgy (AREA)

Abstract

A method is provided for producing a metal-based carbon fiber composite material lightweight, high in the thermal conductivity and also capable of controlling the direction of heat flow, while inhibiting metal carbide formation. The method for producing the metal-based carbon fiber composite material comprises the steps of: obtaining a metal fiber mixture by physically mixing carbon fiber with metal powder; filling the metal fiber mixture into a jig, while the metal fiber mixture is aligned; and setting the jig in an air, vacuum or inert gas atmosphere and directly supplying pulse electric current to the metal fiber mixture, with applying a pressure, to effect sintering by the heat generated therefrom. Here, the composite material contains 10 to 80% by weight of carbon fiber based on a total weight of the composite material and is sintered at 70% or more of ideal density.

Description

    TECHNICAL FIELD
  • carbon fiber composite material. More specifically, the present invention relates to a metal-based carbon fiber composite material having a high thermal conductivity suitable in dissipating the heat from equipment working from ordinary temperature to several hundred degrees Celsius of temperature and a method for producing the metal-based carbon fiber composite material by using a pulsed electric current sintering.
  • BACKGROUND ART
  • Conventionally, metals such as aluminum and copper having a high thermal-conductivity or their alloys have been used in heat-dissipating members (base plate, heat sink, heat spreader and the like) for semiconductor-used electronic equipment and a power module. However, there is a marked tendency that an amount of heat generated from the equipment increases in association with sophistication of the equipment. Further, heat-dissipating members have been required to be made smaller in size and lighter in weight, as the equipment is made smaller and lighter.
  • With regard to the above-described problem, attention has been paid to a metal-based carbon fiber composite material in which carbon fiber excellent in thermal conductivity and also light in weight is used. In general, such metal-based carbon fiber composite material is produced by a liquidized metal impregnation method in which a liquidized metal such as aluminum is impregnated into a preform formed from carbon fibers with or without applying pressure (refer to Patent Document 1).
  • In forming a metal-based carbon fiber composite material by a liquidized metal impregnation method, there is a problem that carbon fibers react with metal in the liquidized metal to generate metal carbides. For example, carbon fibers react with aluminum in the liquidized metal to form Al4C3. It is known that when thus formed carbides such as Al4C3 are brought into contact with water or water vapor at ordinary temperature, they are converted to a hydrocarbon gas such as methane and a metal hydroxide, thereby developing voids between the carbon fibers and the metal of a matrix. It is also known that the voids greatly reduce the strength and the thermal conductivity of the composite material.
  • As a method for inhibiting the formation of carbides in a liquidized metal impregnation method, studies have been made for a method in which coating such as ceramic coating (refer to Patent Document 2) or fluorinated coating (refer to Patent Document 3) is given to carbon fiber. Also, studies have been made for a method in which carbon-based binders (pitch-based resin and the like) are used to form a preform of carbon fibers (refer to Patent Document 4) or a method in which an alloy of metals is used as a liquidized metal to reduce the temperature of the liquidized metal, thereby inhibiting reactions on impregnation of the liquidized metal (refer to Patent Document 5).
    • Patent Document 1: JP-A-2002-194515
    • Patent Document 2: JP-A-2001-300717
    • Patent Document 3: JP-A-H05-125562(1993)
    • Patent Document 4: JP-A-2000-303155
    • Patent Document 5: JP-A-H11-256254(1999)
    DISCLOSURE OF THE INVENTION
  • Problems to be Solved by the Invention
  • However, as mentioned above, additional steps and materials are required in both of the method in which the carbon fiber is coated and the method in which carbon-based binders are used to form a preform, and consequently result in an increased cost of composite materials. Further, the method in which the alloy is used as a liquidized metal requires a step of preparing the alloy. Further, all of the methods require a great amount of energy, since the metal or the alloy used as the matrix must be treated at high temperature for liquidizing them.
  • In contrast, the present invention is to provide a method for producing a metal-based carbon fiber composite material by using commonly available and inexpensive raw materials at less energy consumption, with inhibiting formation of carbides, and the metal-based carbon fiber composite material produced by the method.
  • Means for Solving the Problems
  • A metal-based carbon fiber composite material of a first embodiment of the present invention is a metal-based carbon fiber composite material obtained by sintering of metal and carbon fiber, in which the carbon fiber is contained in a range from 10 to 80% by weight based on a total weight of the composite material, and the composite material is sintered at 70% or more of ideal density. The carbon fiber may be selected from the group consisting of a pitch-based carbon fiber, a PAN-based carbon fiber, a vapor-phase grown carbon fiber, a carbon nanotube, and a nanotube/nanofiber twisted (stranded) wire. The metal may be selected from the group consisting of copper, aluminum, magnesium and alloys thereof. Further, the metal-based carbon fiber composite material preferably has a density of 2.6 g/cm3 or lower where aluminum or its alloy is used as metal, 6.8 g/cm3 or lower where copper or its alloy is used as metal, and 2.1 g/cm3 or lower where magnesium or its alloy is used as metal. Further, the carbon fiber may be aligned in the metal-based carbon fiber composite material. In this instance, it is preferable to have a thermal conductivity of 300 W/mK or more in the aligning direction of carbon fiber.- The above-described metal-based carbon fiber composite material may be used in a heat-dissipating member (base plate, heat sink, heat spreader or the like) for semiconductor-used electronic equipment and a power module.
  • A method for producing a metal-based carbon fiber composite material of a second embodiment of the present invention is characterized by step 1 of obtaining a metal fiber mixture by physically mixing carbon fiber with metal powder, step 2 of filling the metal fiber mixture into a jig, while the metal fiber mixture is aligned, and step 3 of setting the jig in an air, in a vacuum or in an inert gas atmosphere and directly supplying pulse electric current to the metal fiber mixture, with applying the pressure, to effect sintering by the heat generated therefrom. The carbon fiber may be selected from the group consisting of a pitch-based carbon fiber, a PAN-based carbon fiber, a vapor-phase grown carbon fiber, a carbon nanotube, and nanotube/nanofiber twisted wire. The metal may be selected from the group consisting of copper, aluminum, magnesium and alloys thereof. Where the carbon fiber has a fiber length of from 100 nm to 5 mm, the step 1 can be conducted by a physical mixing method in which a ball mill or the like is used. Where the carbon fiber has a fiber length of 5 mm or more, the step 1 can be conducted by a physical mixing method in which a rod mill having rods of an appropriate diameter is used to maintain the direction of fiber. The carbon fiber may be preferably a mixture of pitch-based carbon fiber, PAN-based carbon fiber or nanotube/nanofiber twisted wire with vapor-phase grown carbon fiber or carbon nanotube. Further, in the step 2, the direction of carbon fiber may be also controlled in a two-dimensional manner.
  • Advantages of the Invention
  • By employing the above-described constitution, it become possible to obtain a metal-based carbon fiber composite material which is light in weight and high in thermal conductivity. The obtained composite material is useful as a heat-dissipating member (base plate, heat sink, heat spreader or the like) for semiconductor-used electronic equipment and a power module. Further, the method of the present invention requires no particular additional steps or materials. The inventive method can inhibit the formation of metal carbides resulting from the reaction of metal with carbon fiber. Consequently, the present method can provide a metal-based carbon fiber composite material having excellent properties in a simple and inexpensive manner. Further, in the metal-based carbon fiber composite material of the present invention where the carbon fiber is aligned, it is possible to control the direction of heat flow on the basis of the aligning direction: of the carbon fiber. This characteristic is particularly effective in suppressing the heat flow to adjacent devices in a case of electronic equipment in which semiconductors are highly integrated
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a view illustrating one exemplary equipment used in producing a metal-based carbon fiber composite material of the present invention;
  • FIG. 2 is an optical photomicrograph illustrating the cross section of the metal-based carbon fiber composite material obtained in Example 1; and
  • FIG. 3 is a view illustrating one exemplary equipment used in attaching metal powder to carbon fiber that can be used as continuous fiber.
  • DESCRIPTION OF SYMBOLS
    • 1: vessel
    • 2: die
    • 3: lower punch
    • 4: upper punch
    • 5: platen
    • 6: plunger
    • 7: power source
    • 8: metal fiber mixture
    • 21: unwinding bobbin
    • 22: winding bobbin
    • 23: drying means
    • 24: vessel
    • 25: agitating means
    • 30: fiber bundle
    • 31: metal powder suspension
      Best Modes for Carrying Out the Invention
  • A first embodiment of the present invention is a metal-based carbon fiber composite material obtained by sintering of metal and carbon fiber. As will be explained later in detail, the metal-based carbon fiber composite material is obtained by sintering a composite of metal and carbon fiber, which are mixed in advance in a solid phase, in a pulsed electric current sintering method.
  • Carbon fiber used in the present invention may include a pitch-based carbon fiber, a PAN-based carbon fiber, a vapor-phase grown carbon fiber, a carbon nanotube, or a nanotube/nanofiber twisted wire made by twisting vapor-phase grown carbon fiber or carbon nanotube. Pitch-based carbon fiber and PAN-based carbon fiber are commercially available in a form of several-hundred meters in length, and can be used in the present invention after cut into a desired length. Nanotube/nanofiber twisted wire may be used also in the present invention. Where pitch-based carbon fiber or PAN-based carbon fiber are used, the fiber having a diameter from 5 μm to 20 μm is appropriate. These carbon fibers may be used in a length of 5 mm or more and preferably in a length from 10 mm to 1 m, depending on the dimension of a desired composite material. It is preferable to use carbon fiber having a length from one end to the other end of a desired composite material, in order to align the carbon fiber in one direction and to make it continuous from one end to the other end of the composite material. Such a constitution is effective in achieving a high thermal conductivity.
  • In contrast, vapor-phase grown carbon fiber and carbon nanotube are known to be available in a fiber length from 100 nm to 100 μm. Pitch-based carbon fiber, PAN-based carbon fiber and nanotube/nanofiber twisted wire may be cut into fibers having a length of 5 mm or less (for example, from 100 μm to 5 mm) and used in the present invention. When the above-described fiber is used, a metal-based carbon fiber composite material, in which discontinuous short fibers in a length from 100 nm to 5 mm are dispersed in a metal matrix, is obtained. In certain applications, even though such discontinuous short fibers is used, a sufficient thermal conductivity can be achieved by aligning the fibers in a two-dimensional manner. By “a state that fibers are aligned in a two-dimensional manner”, it is meant that individual fibers are oriented at random in a plane defined by two axes of three axes of orthogonal coordinates (for example, x-axis and y-axis), however not oriented toward the remaining one axis (for example, a z-axis). Where the direction of fibers is not oriented toward the z-axis, the x-y plane is a heat easily-conducting plane.
  • The above-mentioned long fibers having a length of 5 mm or more and the above-mentioned discontinuous short fibers having a length from 100 nm to 5 mm may be mixed together and used. In this instance, a composite material is structured so that short fibers are interposed in spaces formed by long fibers which can be easily aligned in one direction, thereby making it possible to align the short fibers easily in said direction and provide a high thermal conductivity.
  • Metals used in the present invention are those having a high thermal conductivity and include aluminum, aluminum alloy, copper, copper alloy, magnesium and magnesium alloy. Where a primary purpose is to attain a higher thermal conductivity, copper or its alloy may be used. Alternatively, where a primary purpose is to attain a lighter weight, aluminum, aluminum alloy, magnesium or magnesium alloy, which are lower in density, may be used. In particular, where a metal-based carbon fiber composite material having a density of 2.6 g/cm3 or less is fabricated, it is effective to use aluminum, aluminum alloy, magnesium or magnesium alloy. As will be mentioned later, in forming a metal-based carbon fiber composite material of the present invention, metal is allowed to attach on the surface of carbon fiber. For this purpose, the metal is used as powders having a mean particle diameter from 10 nm to 100 μm and preferably from 10 nm to 50 μm.
  • The metal-based carbon fiber composite material of the present invention comprises 10 to 80%, preferably 30 to 80%, and more preferably 50 to 80% by weight of carbon fiber based on the total weight of the composite material. Then, a relative density of the metal-based carbon fiber composite material of the present invention is 70% or more, preferably 90% to 100% of an ideal density. The “ideal density” described in the present invention means a density which is calculated by densities of carbon fiber and metal used as well as a compositional ratio of carbon fiber and metal, on the assumption that the carbon fiber is filled into the metal matrix without any voids. When the metal-based carbon fiber composite material has the composition and the density in the above-mentioned range, the composite material can achieve a thermal conductivity of 300 W/mK (Kelvin/watt/meter) in the arrangement direction of the carbon fiber, although voids are allowed to exist in the material. “Arrangement direction of fiber” described in the present invention means an axial direction of long fibers, where long fibers having a fiber length of 5 mm or more are aligned in one direction, and also means in-plane directions of a heat easily-conducting plane, where short fibers from 100 nm to 5 mm in length are aligned in a two-dimensional manner.
  • Further, in optimizing types of metals used and the compositional ratio of the carbon fiber, the metal-based carbon fiber composite material of the present invention has a density of 2.6 g/cm3 or lower, preferably from 2.2 to 2.6 g/cm3 and more preferably from 2.2 to 2.5 g/cm3, where aluminum or its alloy is used as metal. The metal-based carbon fiber composite material of the present invention has a density of 2.1 g/cm3 or lower, preferably from 1.8 to 2.1 g/cm3 and more preferably from 1.9 to 2.1 g/cm3, where magnesium or its alloy is used as metal. A composite material having such a low density is effective in forming a lightweight heat-dissipating member (base plate, heat sink, heat spreader or the like). Further, where copper or its alloy is used as metal in order to attaining a high thermal conductivity, the metal-based carbon fiber composite material of the present invention should have a density of 6.8 g/cm3 or less, preferably in the range from 2.5 to 6.8 g/cm3 and more preferably from 2.5 to 4.6 g/cm3.
  • A metal-based carbon fiber composite material of the present invention is effectively used as a heat-dissipating member (base plate, heat sink, heat spreader or the like) for semiconductor-used electronic equipment and a power module. The semiconductor-used electronic equipment may be, for example, a central processing unit (CPU), a storage cell (memory cell), a controller IC for various equipments, a flat panel display, an image processing device, communications devices (wireless and wired communications devices) and photo-electric hybrid circuits which are known in the art. The power module includes a converter and an inverter in which elements such as a thyristor, GTO, IGBT and IEGT are used. Further, it is possible to control the direction of heat flow based on the aligning direction of carbon fiber, since the carbon fibers of the inventive metal-based carbon fiber composite material is aligned. This characteristic is particularly effective in suppressing the heat flow to adjacent devices in a case of electronic equipment in which semiconductors are highly integrated. For example, carbon fibers are aligned in a direction from devices to be cooled to the upside of the equipment, thereby making it possible to move the heat flow substantially toward the upside of the equipment. Where the metal-based carbon fiber composite material of the present invention is used as a heat-dissipating member for a heat sink or a heat spreader, the composite material is processed into an appropriate shape and attached to the equipment in such a way that the heat generated in the equipment is transferred to an intermediate or a final cooling medium. In this instance, at a joining part of the composite material of the present invention and the equipment, a pliant heat transfer medium may be used for filling irregularity of the surfaces of the composite material and the equipment, to attain a uniform heat transfer from the equipment to the composite material. The flexible heat transfer medium may be silicone grease, which may contain dispersed particles having high thermal conductivity such as silver, or heat-transfer sheet.
  • Hereinafter, a detailed explanation will be made for a method for producing a metal-based carbon fiber composite material of the present invention. The first step of the production method of the present invention is mixing a metal powder and a carbon fiber together in a solid form, to provide a metal fiber mixture having metal attached on the surface of the carbon fiber.
  • When using long fibers having a fiber length of 5 mm or more (pitch-based carbon fiber, PAN-based carbon fiber or nanotube/nanofiber twisted wire), it is preferable to conduct the present step by a physical mixing method which is capable of maintaining the fiber direction of carbon fiber, in order to facilitate a subsequent arrangement step of the metal fiber mixture. In this case, the present step can be conducted by using a rod mill in which rods having an appropriate diameter are used as a grinding medium. A rod mill used in the present step desirably has a sufficiently small diameter to prevent the carbon fibers from being twisted or entangled with each other. Preferably, the rod mill has an inner diameter of from 10 mm to 20 mm.
  • Where short fibers having a fiber length from 100 nm to 5 mm (vapor-phase grown carbon fiber or carbon nanotube) are used, the present step can be conducted by a physical mixing method with a ball mill, a roll mill or a high-speed rotating mill. In the present step, separately pre-ground metal powder having the above-described particle diameter may be used. Alternatively, in the present step, metal powder having a larger particle diameter may be used and grinding of the metal powder and attachment of the groud powder to carbon fiber may be conducted at the same time.
  • Further, when using a pitch-based carbon fiber, PAN-based carbon fiber and nanotube/nanofiber twisted wire, which can be handled as a continuous fiber, for example, the equipment as illustrated in FIG. 3 is used to immerse the continuous fibers into a suspension in which metal powder is dispersed in a solvent, thereby obtaining a fiber bundle having metal powder attached with a high efficiency and an high accuracy. As used herein, by “To be handled as continuous fibers”, it is meant that a length of the fibers is 100 mm or more. In the equipment illustrated in FIG. 3, a fiber bundle 30 is unwound from an unwinding bobbin 21, immersed into a metal powder suspension 31 in a vessel 24 agitated by an agitator 25, and the fiber bundle 30 to which metal powder is attached is wound up by a winding bobbin 22. Herein, before the bundle is wound up by the winding bobbin 22, solvent attached on the fiber bundle 30 may be evaporated and removed by a drying means 23 such as a hot-air dryer. A solvent used for the metal powder suspension 31 may be selected from organic solvents such as methanol, ethanol, propanol, acetone, hexane, benzene, xylene, toluene, dimethyl ether, diethyl ether, ethylmethyl ether and chloroform, where dispersed metal powder is a powder of aluminum, magnesium or their alloys. Where powder of copper and its alloy is dispersed, water may be selected in addition to the above organic solvents. Preferably, the metal powder suspension 31 further comprises a Pluronic-based dispersant (Pluronic (registered trade mark) F-68 and the like) or polyethylene glycol as a dispersant-adhesive, thereby promoting a uniform attachment of metal powder to fiber bundle. Contents of carbon fiber in a composite material obtained by this method are controlled by an amount of metal powder attached to the fiber bundle. In turn, the amount of the attached metal powder can be regulated by controlling an amount of metal powder mixed in the suspension, a length of a path where the fiber bundle is immersed in the metal powder suspension, a speed of the fiber bundle passing through the metal powder suspension and/or a concentration of the dispersant-adhesive. The second step of the production method of the present invention is a step in which a metal fiber mixture (or a metal powder-attached fiber bundle) is aligned and filled into a jig of a sintering equipment. FIG. 1 illustrates the sintering equipment to be used in the present invention. The sintering equipment shown in FIG. 1 is provided with a vessel 1, a jig constituted with a die 2 having a through hole, a lower punch 3 and an upper punch 4 fitted into the through hole, a platen 5 and a plunger 6 giving pressure to the lower punch 3 and the upper punch 4, and a power source 7 connected to the lower punch 3 and the upper punch 4 and supplying electric current to a metal fiber mixture 8.
  • The metal fiber mixture 8 is filled into a recess formed by fitting the lower punch 3 into the die 2, with aligning fibers in the mixture. When using long fibers having a fiber length of 5 mm or more, it is preferable to align the fibers on filling. When using short fibers having a fiber length from 100 nm to 5 mm, the fibers may be aligned on filling or they may be simulataneously aligned and sintered in the sintering step to be explained later.
  • Here, when using a metal powder-attached fiber bundle obtained by the above-mentioned suspension immersion method, the metal-powder attached fiber bundle unwound from the winding bobbin can be cut at an appropriate length, and the cut metal-powder attached fiber bundle can be aligned and filled into the recess formed by the die 2 and the lower punch 3. Further, where the dispersant-adhesive is used in the metal powder suspension, it is preferable that the filled metal powder attached fiber bundle is heated up to a temperature from 200 to 400° C. to remove the dispersant-adhesive, thereby forming a metal fiber mixture 8 constituted with metal powder and carbon fiber, in a vacuum or in an inert gas atmosphere (nitrogen, argon, helium and the like), either before an upper punch is placed or in a state that low pressure of from 1 to 10 MPa is applied to the upper punch after placement onto the mixture. A step of heating and removing the dispersant-adhesive may be conducted in the pulsed electric current sintering equipment which is further equipped with a heating means or may be conducted in a separate heating apparatus. Where copper powder is used as metal powder, the step of heating and removing the dispersant-adhesive may be conducted at an oxidizing atmosphere (air, oxygen-enriched air, pure oxygen and the like).
  • Next, the upper punch 4 is placed on the filled metal fiber mixture 8, an assembled jig is disposed between a platen 5 and a plunger 6 in a pressing machine inside a vessel 1 to conduct a sintering step. The sintering step is preferably conducted in the air, in a vacuum or in an inert gas atmosphere. In order to make the vessel 1 vacuum, the vessel 1 may be provided with an evacuating port(not illustrated) connected to an appropriate evacuation system. Where a sintering step is conducted in a vacuum, the pressure in the vessel should be maintained in a range from 0 to 20 Pa, preferably from 0 to 5 Pa. Alternatively, the vessel 1 may be provided with an inert gas inlet and a gas outlet (neither of them is illustrated), by which the vessel 1 is purged by inert gas (nitrogen, argon, helium and the like) to accomplish an inert atmosphere.
  • Next, the upper punch 4 is pressed by the plunger 6 to apply pressure to the metal fiber mixture 8. The applied pressure should be in a range from 10 to 100 MPa, preferably from 20 to 50 MPa.
  • Then, the metal fiber mixture 8 is sintered by energizing with a pulse electric current by using the power source 7 connected to the lower punch 3 and the upper punch 4. The pulse duration of the electric current used herein should be from 0.005 to 0.02 seconds, preferably from 0.005 to 0.01 seconds, and the current density (based on cross sectional area of the through hole of the die 2) should be 5×105 to 2×107A/m2, preferably from 5×106 to 1×107A/m2. Voltage for attaining the above current density is usually in a range from 2 to 8V, depending on the resistance value of an electricity-conducting path including the metal fiber mixture 8. Energization by the pulse electric current is continued until a desired sintering is completed, and the duration of the energization will vary, depending on the dimensions of the composite material, the current density and the mixing ratio of carbon fiber.
  • As described above, the supply of pulse electric current causes a plastic deformation of metal particles and fusion of powders, thereby promoting sintering. Where the pulse electric current is used as described in the present step, the heat generated is concentrated at a site where metal particles are to bind together, unlike a case of heating a metal fiber mixture as a whole, thereby making it possible to use electric energy more effectively and conduct sintering more quickly. Then, this method is advantageous over a conventional liquidized-metal impregnation method in that the metal fiber mixture is not substantially elevated in temperature as a whole and, therefore, carbides are not formed due to reaction between metal and carbon fiber. It is, therefore, possible to obtain a metal-based carbon fiber composite material having excellent properties by using inexpensive carbon fibers to which no coating is given. This method is also advantageous over an ordinary resistance heating method in that plasma generated at an initial stage of the energization acts to remove an adsorbed gas and an oxide film on the powder.
  • When using short fibers having a fiber length from 100 nm to 5 mm, the arrangement of fibers proceeds also in the sintering stage. More specifically, in deformation associated with sintering of metal particles by supply of pulse electric current, rod-shaped particles (short fibers) fall from a load-applying direction from the punches and aligned in parallel with a plane perpendicular to the load-applying direction. In this instance, the plane perpendicular to the load-applying direction is a heat easily-conducting plane.
  • Where a mixture of long fibers having a length of 5 mm or more and discontinuous short fibers having a length from 100 nm to 5 mm is used, the short fibers, which are not aligned in parallel with the long fibers on filling, can be aligned in parallel with the long fibers in the sintering step due to the similar action as mentioned above.
  • EXAMPLE 1
  • To a rod mill having an inner diameter of 13 mm was added 6 grams of aluminum powder having a mean particle diameter of 30 μm (available from Kishida Chemical Co., Ltd. ), 3 grams of pitch-based carbon fiber having a fiber length of 20 μm and a diameter of 10 μm (available from Nippon Graphite Fiber Corporation, YS-95A) and a glass rod (5 mm in diameter×20 mm in length). The rod mill was rotated along its axis to mix the ingredients, thereby obtaining a metal fiber mixture.
  • Next, the metal fiber mixture was filled into the equipment shown in FIG. 1, and a pressure in the equipment is set to 8 Pa. The die having a through hole of 20×20 cm was used in this example. Into the die is fitted the lower punch to form a recess, and the metal fiber mixture was filled into the recess such that carbon fiber was aligned in one direction. Next, the upper punch was placed on the filled metal fiber mixture, and pressure of 25 MPa was applied by using the plunger.
  • Then, pulse electric current having a pulse duration of 0.01 seconds, a current density of 1×107A/m2 (maximum) and a voltage of 5V (maximum) flowed through the metal fiber mixture for 20 minutes by using the power source connected to the upper punch and the lower punch, thereby sintering the metal fiber mixture and fabricating a metal-based carbon fiber composite material having dimensions of 20×20×8 cm.
  • The obtained metal-based carbon fiber composite material contained 45% of carbon fiber based on -a total weight of the composite material and had a density of 1.91 g/cm3. The ideal density of the composite material was 2.40 g/cm3 and therefore the composite material had a relative density of 78%. FIG. 2 shows a optical micrograph illustrating the cross section of the thus obtained composite material. Further, the composite material had a thermal conductivity of 350 W/mK, as measured in the aligning direction of the carbon fiber.
  • EXAMPLE 2
  • The same procedures as described in Example 1 are repeated, except that the amount of carbon fiber is changed to 4 grams and that of aluminum powder was changed to 4 grams. The obtained metal-based carbon fiber composite material contained 60% of carbon fiber based on a total weight of the composite material and had a density of 1.75 g/cm3. The composite material had an ideal density of 2.38 g/cm3 and a relative density of 73%. The composite material had a thermal conductivity of 300 W/mK, as measured in the aligning direction of the carbon fiber.
  • EXAMPLE 3
  • In this example, a suspension immersion method was used to prepare a metal fiber mixture, in which an aluminum powder suspension was applied to carbon fiber that can be handled as continuous fiber. The metal fiber mixture was sintered in the pulsed electric current sintering method to provide a metal-based carbon fiber composite material.
  • Pitch-based carbon fiberhaving a thermal conductivity of 1000 W/mK and a diameter of 10 μm was used as carbon fiber and a bundle made of 6000 pieces of the fiber was wound up around an unwinding bobbin 2. Flake-like powder, which is 1 μm or less in thickness and 30 μm in mean representative length toward a surface (in-plane) direction, was used as aluminum powder. The aluminum powder was mixed in ethanol containing 2% by weight (based on weight of the ethanol) of a dispersant-adhesive (Pluronic (registered trade mark) F68) to form a metal powder suspension. The content of aluminum powder was 30% by weight based on the weight of the suspension. The bundle of carbon fiber was unwound from the unwinding bobbin, immersed into the metal powder suspension under agitation, taken up in the air, subjected to hot-air drying (50° C.) and wound up around a winding bobbin to obtain a bundle of carbon fiber to which aluminum powder is attached.
  • The obtained aluminum-powder-attached bundle of carbon fiber was unwound and cut into a strip 20 mm in length. While the fiber bundle was aligned in one direction, 8 grams of the bundle was laid into the rectangular recess (20 mm×20 mm) formed by the lower punch and the die. Then, a pressure in the equipment was set 8 Pa and the upper punch was disposed on the laid fiber bundle, to which the pressure of 25 MPa was applied by a plunger. Then, pulse electric current having pulse duration of 0.01 seconds; current density of 5×106A/m2(maximum); and voltage of 8V (maximum) flowed for 10 minutes through the fiber bundle by using the power source connected to the upper and lower punches, thereby sintering the aluminum-powder-attached fiber bundle to obtain a metal-based carbon fiber composite material.
  • The obtained metal-based carbon fiber composite material had a content of 50% of carbon fiber, density of 2.3 g/cm3 (95% of ideal density) and thermal conductivity of 400 W/mK.
  • EXAMPLE 4
  • In this example, the suspension immersion method was used to prepare a metal fiber mixture, in which a copper powder suspension was applied to carbon fiber that can be handled as continuous fiber. The metal fiber mixture was then sintered in the pulsed electric current sintering method to provide a metal-based carbon fiber composite material.
  • Pitch-based carbon fiber having a thermal conductivity of 1000 W/mK and a diameter of 10 μm was used as carbon fiber and a bundle made of 1000 pieces of the fiber was wound up around an unwinding bobbin. Flake-like powder, which is 1 μm or less in thickness and 30 μm in mean representative length toward a surface direction, was used as copper powder. The copper powder is mixed in ethanol containing 2% by weight (based on the weight of ethanol) of a dispersant-adhesive (Pluronic (registered trade mark) F68) to form a metal powder suspension. The content of copper powder was 60% by weight based on the weight of the suspension. The bundle of carbon fiber was unwound from the unwinding bobbin, immersed into the metal powder suspension under agitation, taken up in the air, subjected to hot-air drying (50° C.) and wound up around a winding bobbin to obtain a bundle of carbon fiber to which copper powder is attached.
  • The obtained aluminum-powder-attached bundle of carbon fiber was unwound and cut into a strip 20 mm in length. While the fiber bundle was aligned in one direction, 12 gram of the bundle was laid into the rectangular recess (20 mm×20 mm) formed by the lower punch and the die. Then, a pressure inside the equipment was set 10 Pa and the upper punch was disposed on the laid fiber bundle, to which the pressure of 25 MPa was applied by a plunger. Then, pulse electric current having pulse duration of 0.01 seconds; current density of 5×106A/m2 (maximum); and voltage of 8V (maximum) flowed for 10 minutes through the fiber bundle by using the power source connected to the upper and lower punches, thereby sintering the copper-powder-attached fiber bundle to obtain a metal-based carbon fiber composite material.
  • The obtained metal-based carbon fiber composite material had a content of 30% of carbon fiber, density of 4.5 g/cm3 (97% of ideal density) and thermal conductivity of 550 W/mK.

Claims (21)

1. A metal-based carbon fiber composite material obtained by sintering of metal and carbon fiber, the composite material comprising 10 to 80% by weight of the carbon fiber based on a total weight of the composite material and the composite material being sintered at 70% or more of ideal density and the carbon fiber is continuously aligned from one end to the other end of the composite material.
2. The metal-based carbon fiber composite material as claimed in claim 1, wherein the carbon fiber is selected from the group consisting of pitch-based carbon fiber, PAN-based carbon fiber, vapor-phase grown carbon fiber, carbon nanotube and nanotube/nanofiber twisted wire.
3. The metal-based carbon fiber composite material as claimed in claim 1, wherein the metal is selected from the group consisting of copper, aluminum, magnesium and their alloys.
4. The metal-based carbon fiber composite material as claimed in claim 3, wherein the metal is aluminum or its alloy, and the composite material has a density of 2.6 g/cm3 or less.
5. The metal-based carbon fiber composite material as claimed in claim 3, wherein the metal is copper or its alloy and the composite material has a density of 6.8 g/cm3 or less.
6. The metal-based carbon fiber composite material as claimed in claim 3, wherein the metal is magnesium or its alloy and the composite material has a density of 2.1 g/cm3 or less.
7. The metal-based carbon fiber composite material as claimed in claim 1, wherein the carbon fiber is aligned.
8. The metal-based carbon fiber composite material, as claimed in claim 21, wherein a thermal conductivity is 300 W/mK or more in the arrangement direction of the carbon fiber.
9. Electronic equipment with semiconductors, wherein the metal-based carbon fiber composite material as claimed in claim 1 is used as a heat-dissipating member.
10. A power module, wherein the metal-based carbon fiber composite material as claimed in claim 1 is used as a heat-dissipating member.
11. A method for producing a metal-based carbon fiber composite material, comprising the steps of:
step 1: obtaining a metal fiber mixture by physically mixing carbon fiber with metal powder;
step 2: filling the metal fiber mixture into a jig, while the metal fiber mixture is aligned, and
step 3: setting the jig in the air, in a vacuum or in an inert gas atmosphere and directly supplying pulse electric current to the metal fiber mixture, with applying the pressure, to effect sintering by the heat generated therefrom.
12. The method for producing a metal-based carbon fiber composite material as claimed in claim 11, wherein the carbon fiber is selected from the group consisting of pitch-based carbon fiber, PAN-based carbon fiber, vapor-phase grown carbon fiber, carbon nanotube, and nanotube/nanofiber twisted wire.
13. The method for producing a metal-based carbon fiber composite material as claimed in claim 11, wherein the metal is selected from the group consisting of copper, aluminum, magnesium and their alloys.
14. The method for producing a metal-based carbon fiber composite material as claimed in claim 11, wherein the carbon fiber has a fiber length of from 100 nm to 5 mm and the step 1 is conducted by a physical mixing method in which a ball mill or the like is used.
15. The method for producing a metal-based carbon fiber composite material as claimed in claim 11, wherein the carbon fiber has a fiber length of 5 mm or more and the step 1 is conducted by a physical mixing method in which the direction of fiber is maintained.
16. The method for producing a metal-based carbon fiber composite material as claimed in claim 11, wherein the carbon fiber has a fiber length of 100 mm or more and the step 1 is conducted by immersing a fiber bundle into a metal powder suspension.
17. The method for producing a metal-based carbon fiber composite material as claimed in claim 1 1, wherein the carbon fiber is a mixture of pitch-based carbon fiber, PAN-based carbon fiber or nanotube/nanofiber twisted wire with vapor-phase grown carbon fiber or carbon nanotube.
18. The method for producing a metal-based carbon fiber composite material as claimed in claim 11, wherein in the step 2, the direction of carbon fiber is controlled in a two-dimensional manner.
19. The method for producing a metal-based carbon fiber composite material as set forth in claim 11, wherein, among the carbon fibers, those which are not continuous from one end of the composite material to the other end have the fiber length of 100 nm to 5 mm, and the step 1 is conducted by a physical mixing method in which a ball mill or the like is used.
20. The method for producing a metal-based carbon fiber composite material as set forth in claim 11, wherein, among the carbon fibers, those which are continuous from one end of the composite material to the other end have the fiber length of the same as the dimension of the composite material, and the step 1 is conducted by a physical mixing method in which the direction of fiber is maintained.
21. The metal-based carbon fiber composite material as set forth in claim 1, comprising 45 to 80% by weight of the carbon fiber, based on the total weight of the composite material.
US10/582,990 2003-12-18 2004-12-16 Metal-based carbon fiber composite material and method for producing the same Abandoned US20070141315A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2003421619 2003-12-18
JP2003-421619 2003-12-18
PCT/JP2004/018823 WO2005059194A1 (en) 2003-12-18 2004-12-16 Metal base carbon fiber composite material and process for producing the same

Publications (1)

Publication Number Publication Date
US20070141315A1 true US20070141315A1 (en) 2007-06-21

Family

ID=34697312

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/582,990 Abandoned US20070141315A1 (en) 2003-12-18 2004-12-16 Metal-based carbon fiber composite material and method for producing the same

Country Status (8)

Country Link
US (1) US20070141315A1 (en)
EP (1) EP1696046B1 (en)
JP (1) JP4106395B2 (en)
KR (1) KR100816412B1 (en)
CN (1) CN1894435B (en)
CA (1) CA2550015C (en)
DE (1) DE602004026630D1 (en)
WO (1) WO2005059194A1 (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080315401A1 (en) * 2007-06-25 2008-12-25 Hitachi, Ltd. Power Semiconductor Module And Method of Manufacturing the Power Semiconductor Module
EP2008598A1 (en) 2007-06-29 2008-12-31 Edward A. Loeser Composite fiber electrosurgical instrument
US20090176090A1 (en) * 2008-01-04 2009-07-09 Sungkyunkwan University Foundation For Corporate Collaboration Method for efficient al-c covalent bond formation between aluminum and carbon material
US20100221526A1 (en) * 2007-09-18 2010-09-02 Shimane Prefectural Government Metal-coated carbon material and carbon-metal composite material using the same
US20100330365A1 (en) * 2008-03-07 2010-12-30 Hassel Joerg Strand-like material composite with cnt yarns and method for the manufacture thereof
US20140070147A1 (en) * 2009-01-30 2014-03-13 Samsung Electronics Co., Ltd. Composite anode active material, anode including the composite anode active material, lithium battery including the anode, and method of preparing the composite anode active material
US20140109804A1 (en) * 2011-06-24 2014-04-24 Graftech International Holdings Inc. Thermal Insulation Assembly
US20150369286A1 (en) * 2012-12-24 2015-12-24 Mahle Inernational Gmbh Sliding bearing with lining layer comprising carbon nanostructures
CN109136791A (en) * 2018-08-01 2019-01-04 玉环双翔机械有限公司 A kind of composite material and preparation method thereof for being used to mark high-speed rail brake block of high durability degree
WO2021215575A1 (en) * 2020-04-22 2021-10-28 부경대학교 산학협력단 Method for manufacturing cooling pipe for electric vehicle powertrain, and cooling pipe manufactured thereby

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006147170A (en) * 2004-11-16 2006-06-08 Sumitomo Electric Ind Ltd Conductive material and its manufacturing method
WO2008063148A2 (en) * 2005-05-20 2008-05-29 University Of Central Florida Carbon nanotube reinforced metal composites
WO2007063764A1 (en) 2005-11-30 2007-06-07 Shimane Prefectural Government Metal-based composite material containing both micro-sized carbon fiber and nano-sized carbon fiber
DE102007012426A1 (en) * 2007-03-15 2008-09-18 Bayerische Motoren Werke Aktiengesellschaft Light metal material
JP5229934B2 (en) * 2007-07-05 2013-07-03 住友精密工業株式会社 High thermal conductivity composite material
WO2009034988A1 (en) * 2007-09-14 2009-03-19 Shimane Prefectural Government Pcr-use temperature controller
KR101497412B1 (en) * 2008-07-16 2015-03-02 주식회사 뉴파워 프라즈마 Heat sink with compound material having covalent bond carbon nanotube
WO2011047743A1 (en) * 2009-10-19 2011-04-28 Ks Kolbenschmidt Gmbh COMPOSITE MATERIALS CONSISTING OF METALS IN WHICH CARBON NANOTUBES (CNTs) ARE DISPERSED
CN101705456B (en) * 2009-11-16 2011-03-30 重庆大学 Method for preparing short carbon fiber reinforced magnesium-base composite material with good damping characteristic
KR101264186B1 (en) * 2010-06-30 2013-05-15 연세대학교 산학협력단 Method of manufacturing metal matrix composite containing networked carbon nanotubes/carbon fibers and the method therefor
CN102116592A (en) * 2010-12-24 2011-07-06 费金华 Air energy non-metal heat exchanger
CN102051534B (en) * 2011-01-14 2012-08-22 南京信息工程大学 Damping wear-resistant copper alloy material and preparation method thereof
CN103243280B (en) * 2013-04-28 2015-03-04 河南科技大学 Carbon fiber reinforced aluminum-based composite material and preparation method thereof
CN103276325B (en) * 2013-06-07 2015-01-21 哈尔滨工业大学 Preparation method of anisotropic composite material for spaceborne radar antenna panel
CN103911566B (en) * 2014-03-11 2016-06-01 上海交通大学 The method for preparing powder metallurgy of a kind of carbon nano tube reinforced aluminum alloy composite material
CN104084583B (en) * 2014-07-28 2016-06-15 中国科学院重庆绿色智能技术研究院 The laser preparing apparatus of a kind of Metal Substrate carbon nano-composite material and method
CN106862566A (en) * 2017-03-14 2017-06-20 西安科技大学 The preparation method of carbon fiber metal material and the manufacture method of carbon fiber metal article
CN109413938A (en) * 2018-10-24 2019-03-01 航天材料及工艺研究所 A kind of efficient cooling means of composite material light and device
KR102228431B1 (en) * 2019-04-16 2021-03-16 부경대학교 산학협력단 Method for manufacturing aluminum-based clad heat sink and aluminum-based clad heat sink manufactured thereby
CN109894615A (en) * 2019-04-19 2019-06-18 扬州海昌新材股份有限公司 Pulsed discharge flash sintering metal base components near-net-shape process
CN110385437B (en) * 2019-07-03 2021-09-10 西安理工大学 Preparation method of directional fiber in-situ reinforced titanium and alloy bracket thereof
EP3997159A1 (en) * 2019-07-10 2022-05-18 Boston Materials, Inc. Systems and methods for forming short-fiber films, composites comprising thermosets, and other composites
KR102293022B1 (en) * 2019-11-18 2021-08-26 한국생산기술연구원 Heat dissipation module including metal-nanocarbon composite intense-pulsed-light sintered
CN111940531B (en) * 2020-06-23 2022-04-08 西安理工大学 Cold extrusion die and preparation method thereof
CN111850433A (en) * 2020-08-03 2020-10-30 南京工业大学 Continuous silicon carbide fiber reinforced metal matrix fiber wire, preparation method and composite material
CN112176262B (en) * 2020-09-09 2021-08-10 上海航天精密机械研究所 High-volume-fraction multiphase hybrid reinforced magnesium-based composite material and preparation method thereof
CN115255606B (en) * 2022-06-21 2023-07-25 北京科技大学 Diffusion connection method for copper and graphite of aluminum-containing intermediate layer

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4083719A (en) * 1975-10-29 1978-04-11 Hitachi, Ltd. Copper-carbon fiber composites and process for preparation thereof
US4500360A (en) * 1981-11-25 1985-02-19 Nippon Soken, Inc. Sliding member made of fiber-reinforced metal
US5002836A (en) * 1985-06-21 1991-03-26 Imperial Chemical Industries Plc Fiber-reinforced metal matrix composites
US5277973A (en) * 1988-08-12 1994-01-11 Ube Industries, Ltd. Carbon fibers having high strength and high modulus of elasticity and polymer composition for their production
US5660923A (en) * 1994-10-31 1997-08-26 Board Of Trustees Operating Michigan State University Method for the preparation of metal matrix fiber composites
US5993733A (en) * 1996-01-24 1999-11-30 Dynax Corporation Method of manufacturing sintered synchronizing ring
US6013371A (en) * 1997-11-20 2000-01-11 Motorcarbon Llc Carbon artifacts and compositions and processes for their manufacture
US20020142146A1 (en) * 1997-03-21 2002-10-03 Daimlerchrysler Ag Melted-infiltrated fiber-reinforced composite ceramic
US20060286361A1 (en) * 2003-05-09 2006-12-21 Koichiro Yonetake Fine carbon fiber with linearity and resin composite material using the same

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5540641B2 (en) * 1974-04-30 1980-10-20
JPS515213A (en) * 1974-07-03 1976-01-16 Hitachi Ltd Do tansosenifukugozaino seizoho
JPS5147508A (en) * 1974-10-23 1976-04-23 Honda Motor Co Ltd ROOTARIIEN JINYOAPETSUKUSUSHI IRUZAI
JPS5218411A (en) * 1975-08-05 1977-02-12 Komatsu Ltd Process for production of al-carbon fiber composite material
GB1590728A (en) * 1977-10-21 1981-06-10 Silag Inc Method for preparing a fibre reinforced metal composite
DE2928955A1 (en) * 1979-07-18 1981-02-12 Glyco Metall Werke Composite material using reinforcing fibres in metal matrix - esp. where aluminium powder is compacted into strip contg. oriented fibres
JPH0419430A (en) * 1990-05-10 1992-01-23 Akebono Brake Res & Dev Center Ltd Light alloy disk rotor
JPH11140559A (en) * 1997-11-05 1999-05-25 Furukawa Electric Co Ltd:The Composite material and its production

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4083719A (en) * 1975-10-29 1978-04-11 Hitachi, Ltd. Copper-carbon fiber composites and process for preparation thereof
US4500360A (en) * 1981-11-25 1985-02-19 Nippon Soken, Inc. Sliding member made of fiber-reinforced metal
US5002836A (en) * 1985-06-21 1991-03-26 Imperial Chemical Industries Plc Fiber-reinforced metal matrix composites
US5277973A (en) * 1988-08-12 1994-01-11 Ube Industries, Ltd. Carbon fibers having high strength and high modulus of elasticity and polymer composition for their production
US5660923A (en) * 1994-10-31 1997-08-26 Board Of Trustees Operating Michigan State University Method for the preparation of metal matrix fiber composites
US5891249A (en) * 1994-10-31 1999-04-06 Board Of Trustees Operating Michigan State University Apparatus for the preparation of metal matrix fiber composites
US5993733A (en) * 1996-01-24 1999-11-30 Dynax Corporation Method of manufacturing sintered synchronizing ring
US20020142146A1 (en) * 1997-03-21 2002-10-03 Daimlerchrysler Ag Melted-infiltrated fiber-reinforced composite ceramic
US6013371A (en) * 1997-11-20 2000-01-11 Motorcarbon Llc Carbon artifacts and compositions and processes for their manufacture
US20060286361A1 (en) * 2003-05-09 2006-12-21 Koichiro Yonetake Fine carbon fiber with linearity and resin composite material using the same

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080315401A1 (en) * 2007-06-25 2008-12-25 Hitachi, Ltd. Power Semiconductor Module And Method of Manufacturing the Power Semiconductor Module
EP2008598A1 (en) 2007-06-29 2008-12-31 Edward A. Loeser Composite fiber electrosurgical instrument
US20100221526A1 (en) * 2007-09-18 2010-09-02 Shimane Prefectural Government Metal-coated carbon material and carbon-metal composite material using the same
US20090176090A1 (en) * 2008-01-04 2009-07-09 Sungkyunkwan University Foundation For Corporate Collaboration Method for efficient al-c covalent bond formation between aluminum and carbon material
US20100330365A1 (en) * 2008-03-07 2010-12-30 Hassel Joerg Strand-like material composite with cnt yarns and method for the manufacture thereof
US20140070147A1 (en) * 2009-01-30 2014-03-13 Samsung Electronics Co., Ltd. Composite anode active material, anode including the composite anode active material, lithium battery including the anode, and method of preparing the composite anode active material
US9178212B2 (en) * 2009-01-30 2015-11-03 Samsung Electronics Co., Ltd. Composite anode active material, anode including the composite anode active material, lithium battery including the anode, and method of preparing the composite anode active material
US20140109804A1 (en) * 2011-06-24 2014-04-24 Graftech International Holdings Inc. Thermal Insulation Assembly
US20150369286A1 (en) * 2012-12-24 2015-12-24 Mahle Inernational Gmbh Sliding bearing with lining layer comprising carbon nanostructures
US10473160B2 (en) * 2012-12-24 2019-11-12 Mahle International Gmbh Sliding bearing with lining layer comprising carbon nanostructures
CN109136791A (en) * 2018-08-01 2019-01-04 玉环双翔机械有限公司 A kind of composite material and preparation method thereof for being used to mark high-speed rail brake block of high durability degree
WO2021215575A1 (en) * 2020-04-22 2021-10-28 부경대학교 산학협력단 Method for manufacturing cooling pipe for electric vehicle powertrain, and cooling pipe manufactured thereby

Also Published As

Publication number Publication date
JP4106395B2 (en) 2008-06-25
CN1894435A (en) 2007-01-10
CN1894435B (en) 2010-07-21
WO2005059194A1 (en) 2005-06-30
KR20060108712A (en) 2006-10-18
DE602004026630D1 (en) 2010-05-27
EP1696046A4 (en) 2007-05-23
CA2550015A1 (en) 2005-06-30
EP1696046B1 (en) 2010-04-14
KR100816412B1 (en) 2008-03-25
JPWO2005059194A1 (en) 2008-04-17
CA2550015C (en) 2013-02-26
EP1696046A1 (en) 2006-08-30

Similar Documents

Publication Publication Date Title
CA2550015C (en) Metal-based carbon fiber composite material and method for producing the same
JP5364905B2 (en) Metal matrix composite containing co-containing micron-sized and nano-sized carbon fibers
JP4441768B2 (en) Metal-graphite composite material having high thermal conductivity and method for producing the same
CN102007090A (en) Carbon fiber carbon composite molded body, carbon fiber-reinforced carbon composite material and manufacturing method thereof
KR910001507B1 (en) Method of making ceramic super conducting wires
CN106498313A (en) High-strength high ductility CNTs SiCp reinforced aluminum matrix composites and preparation method thereof
TW200910384A (en) Conductive ink and conductor
WO2020105328A1 (en) Aluminum-(carbon particle) composite material and method for producing same
US11597012B2 (en) Article and method
KR20190096731A (en) Sintering bonding method for semiconductor devices
JP4260426B2 (en) heatsink
JP2018087372A (en) Manufacturing method of metal-carbon particle composite material
JP7273378B2 (en) Method for producing particle-coated foil and method for producing metal-particle composite
JP7109348B2 (en) Method for producing particle-coated foil and method for producing metal-particle composite
KR20170000220A (en) The heat sink using nano carbon nano-graphene composites
KR102274190B1 (en) Semiconductor device package comprising thermal interface layer and method of fabricating of the same
JP6875211B2 (en) Method for manufacturing metal-carbon particle composite material
JPH0197321A (en) Manufacture of superconductive member
KR20160057878A (en) CNT-graphene Composites and manufacturing method thereof

Legal Events

Date Code Title Description
AS Assignment

Owner name: SHIMANE PREFECTURAL GOVERNMENT, JAPAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SATO, KIMINORI;OZOE, NOBUAKI;OGAWA, JINICHI;AND OTHERS;REEL/FRAME:018276/0207

Effective date: 20060904

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION