WO2021106561A1 - サンドイッチ構造体およびその製造方法 - Google Patents
サンドイッチ構造体およびその製造方法 Download PDFInfo
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- WO2021106561A1 WO2021106561A1 PCT/JP2020/042007 JP2020042007W WO2021106561A1 WO 2021106561 A1 WO2021106561 A1 WO 2021106561A1 JP 2020042007 W JP2020042007 W JP 2020042007W WO 2021106561 A1 WO2021106561 A1 WO 2021106561A1
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- WO
- WIPO (PCT)
- Prior art keywords
- sandwich structure
- core material
- heat conductive
- iii
- conductive material
- 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.)
- Ceased
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- H—ELECTRICITY
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- H10W40/25—Arrangements for cooling characterised by their materials
- H10W40/255—Arrangements for cooling characterised by their materials having a laminate or multilayered structure, e.g. direct bond copper [DBC] ceramic substrates
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- H10W40/25—Arrangements for cooling characterised by their materials
- H10W40/257—Arrangements for cooling characterised by their materials having a heterogeneous or anisotropic structure, e.g. powder or fibres in a matrix, wire mesh or porous structures
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Definitions
- the present invention relates to a sandwich structure and a method for producing the sandwich structure.
- Patent Document 1 describes the invention of a sandwich structure in which a heat conductive material and a rigidity holding material are laminated. It is said that a sandwich structure having both excellent thermal conductivity and excellent rigidity can be obtained by laminating a heat conductive material and a rigidity holding material.
- Patent Document 2 a graphite sheet having excellent thermal conductivity and support sheets are laminated on both sides of the graphite sheet, and a sealing spacer having a thickness substantially equal to that of the graphite sheet is provided on at least one end surface of the graphite sheet.
- the invention of the attached sandwich structure is described.
- Patent Document 3 describes an invention of a highly thermally conductive housing in which a laminate of graphite sheets is coated with a resin layer. It is said that it is possible to prevent peeling between graphite films by coating the edges of the graphite sheet with resin.
- the high thermal conductivity housing in Patent Document 3 protects the graphite sheet by coating the surface and edges of the graphite sheet with resin, but the rigidity and strength are low due to the protection with resin.
- the present invention has been made in view of the above problems, and an object of the present invention is to provide a sandwich structure having both excellent heat dissipation and excellent mechanical properties.
- the sandwich structure of the present invention has the following configuration.
- a sandwich structure having a core material (I) and a fiber reinforced material (II) arranged on both sides of the core material (I), wherein the core material (I) has an in-plane thermal conductivity of 300 W.
- the sandwich structure in the present specification is a structure in which a skin material having a higher elastic modulus than the core material is arranged on both sides of the core material.
- the core material is the core material (I) containing the sheet-shaped heat conductive material (III), and the skin material is the fiber reinforced material (II).
- the sheet shape refers to a sheet having a thin thickness and a wide width, and means a sheet having a thickness of 0.01 ⁇ m or more and 10 mm or less and an aspect ratio of width to thickness of 10 or more.
- the core material (I) includes a sheet-shaped heat conductive material (III) (hereinafter, may be simply referred to as a heat conductive material (III)).
- III heat conductive material
- the term "included” as used herein means that the heat conductive material (III) is present as a part of the layer of the core material (I) in the laminated structure of the sandwich structure.
- the core material (I) 2 covers one end surface (right end surface in FIG. 1) and one surface (upper surface in FIG. 1) of the heat conductive material (III) 4.
- the core material (I) 2 covers both sides (both surfaces) of the heat conductive material (III) 4 and all the end faces, that is, the core material (I) contains the heat conductive material (III). It can be said that the core material (I) contains the heat conductive material (III).
- all the end faces of the heat conductive material (III) (graphite sheet 9) are exposed, that is, only the heat conductive material (III) can be regarded as forming an independent layer.
- the core material (I) preferably covers at least two end faces of the heat conductive material (III), more preferably covers both sides of the heat conductive material (III), and the heat conductive material (III). It is more preferable that both sides and all the end faces of the above are covered, that is, the heat conductive material (III) is included.
- the core material (I) may cover the heat conductive material (III) with another member such as an adhesive or a cushioning material. Further, there may be a gap between the core material (I) and the heat conductive material (III).
- At least one end face of the heat conductive material (III) is in direct contact with the core material (I) without interposing another member. Further, it is preferable that at least one surface of the heat conductive material (III) is in contact with the core material (I). Since the heat conductive material (III) is in direct contact with the core material (I) in this way, the heat transferred from the surface of the sandwich structure is quickly transferred from the core material (I) to the heat conductive material (III). be able to.
- the heat conductive material (III) is not adhered to the core material (I).
- the heat conductive material (III) occupies the sandwich structure due to the adhesive.
- the ratio of (III) is reduced, and the heat dissipation of the sandwich structure is lowered.
- the heat conductive material (III) is not adhered to the core material (I)
- the ratio of the stress applied to the sandwich structure is borne by the core material (I) is increased, and therefore the heat conductive material (III) is borne by the core material (I). )
- the transfer of stress to) is suppressed, and the destruction of the heat conductive material (III) can be suppressed.
- the sandwich structure of the present invention preferably has a flexural rigidity per unit width of 0.5 N ⁇ m or more, more preferably 1.0 N ⁇ m or more, and preferably 1.5 N ⁇ m or more. More preferred.
- the flexural rigidity per unit width can be calculated by the following formula from the elastic modulus E (Pa) of the sandwich structure, the moment of inertia of area I (m 4 ), and the width b (m) of the sandwich structure.
- -Flexural rigidity per unit width (Nm) E (Pa) x I (m 4 ) / b (m)
- the cross section of the sandwich structure is a rectangular cross section
- the second moment I of the rectangular cross-section are the bh 3/12 (m 4) , it can be calculated by the following equation.
- -Flexural rigidity per unit width (Nm) E (Pa) x h 3 (m 3 ) / 12
- a method of using a fiber reinforcing material (II) as a skin material as in the sandwich structure of the present invention can be mentioned.
- a method of increasing the thickness of the sandwich structure can be mentioned.
- the sandwich structure of the present invention preferably has a maximum thickness of 0.3 mm or more and 3.0 mm or less, and more preferably 0.5 mm or more and 1.5 mm or less. Although the effect of weight reduction is obtained by making the thickness of the sandwich structure thin, the rigidity of the sandwich structure thinner than 0.3 mm may be insufficient.
- the heat conductive material (III) is in the form of a sheet, and its in-plane thermal conductivity is 300 W / m ⁇ K or more.
- the in-plane thermal conductivity of the heat conductive material (III) is preferably 500 w / m ⁇ K or more, and more preferably 1000 w / m ⁇ K or more. Since the higher the in-plane thermal conductivity is, the more preferable it is. Therefore, the upper limit of the in-plane thermal conductivity is not particularly limited, but a thermal conductive material having an in-plane thermal conductivity of about 2000 W / m ⁇ K is known. ..
- the in-plane thermal conductivity of the heat conductive material (III) is 300 W / m ⁇ K or more, the heat diffusion of the sandwich structure in the in-plane direction is excellent, and the heat dissipation of the sandwich structure is excellent.
- the sample in the sample holder for in-plane measurement by the laser flash method, and set the sample size to about 20 to 30 mm in diameter and 1.0 mm or less in thickness. Can be measured with.
- a blackening film is thinly and uniformly formed on the sample surface.
- the same treatment is performed on the back surface of the sample.
- the material of the heat conductive material (III) is not particularly limited as long as the in-plane thermal conductivity is 300 w / m ⁇ K or more.
- heat is generated by adding a highly heat conductive filler to ceramics, metal, graphite, or resin.
- a high thermal conductivity resin having an increased conductivity can be used.
- the heat conductive material (III) preferably contains a heat conductive sheet selected from the group consisting of a graphite sheet, a metal sheet and a ceramic sheet, and the heat selected from the group consisting of a graphite sheet, a metal sheet and a ceramic sheet. More preferably, it consists of a conductive sheet.
- the ceramic sheet include sheets of silica, zirconia, alumina, boron nitride, silicon carbide, silicon nitride and the like.
- the metal sheet include a sheet made of titanium, aluminum, magnesium, iron, silver, gold, platinum, copper, nickel, or an alloy containing these metals as a main component.
- the metal sheet is relatively inexpensive, and the copper sheet is particularly inexpensive and has excellent thermal conductivity, so it is preferable from the viewpoint of raw material cost. Since the graphite sheet has a small specific gravity and excellent thermal conductivity, it is particularly preferable in the present invention from the viewpoint of improving the light weight and heat dissipation of the sandwich structure.
- the graphite sheet a sheet obtained by mixing and molding graphite powder with a binder resin, a sheet obtained by rolling expanded graphite, a sheet obtained by laminating carbon atoms on a substrate by a CVD method using a hydrocarbon gas, and then annealing, a polymer compound.
- a sheet obtained by graphitizing the film of the above can be mentioned.
- a sheet obtained by graphitizing a film of a polymer compound is preferable because it has extremely high thermal conductivity.
- the heat conductive material (III) preferably contains a laminated structure of a plurality of heat conductive sheets, and more preferably a laminated structure of a plurality of heat conductive sheets.
- the orientation of the graphene structure in the sheet affects the thermal conductivity, and in general, the thin graphite sheet has a higher thermal conductivity. Therefore, when a graphite sheet is used as the heat conductive sheet, the heat dissipation of the sandwich structure can be improved by using a plurality of laminated structures as the heat conductive material (III).
- the plurality of heat conductive sheets constituting the heat conductive material (III) are in direct contact with each other without using an adhesive or the like.
- the ratio of the heat conductive material (III) to the sandwich structure can be increased, and the heat dissipation of the sandwich structure is improved. Further, since the heat conductive sheets are in direct contact with each other, the heat diffusion in the out-of-plane direction is also excellent.
- the number of laminated heat conductive sheets is preferably 2 or more and 10 or less, and more preferably 3 or more and 5 or less. Increasing the number of layers improves the heat dissipation of the sandwich structure. On the other hand, if the number of laminated sheets is increased too much, the processability becomes low.
- the average thickness of the heat conductive material (III) is preferably 0.01 ⁇ m or more and 2.0 mm or less, more preferably 5 ⁇ m or more and 1.0 mm or less, and further preferably 15 ⁇ m or more and 0.5 mm or less. .. If the average thickness of the heat conductive material (III) is too small, the heat dissipation of the sandwich structure is lowered, and if the average thickness of the heat conductive material (III) is too large, the weight of the sandwich structure becomes heavy.
- the method for measuring the average thickness of the heat conductive material (III) is to measure the thickness of nine points of the heat conductive material (III) to one decimal place using a micrometer, and use the average value as the average thickness. For the points to be measured, measure at a total of 9 points, 3 points each in the vertical and horizontal directions so that the distance between each measurement point and the adjacent point or the sample end is even in the vertical and horizontal directions. ..
- the core material (I) preferably contains a porous body, and the core material (I) is more preferably a porous body. Since the core material (I) contains a porous body, it is advantageous from the viewpoint of lightness of the sandwich structure. Further, when the core material (I) contains the heat conductive material (III), the core material (I), which is a porous body, collapses or swells in the out-of-plane direction, so that the position of the heat conductive material (III) The core material (I) can include the heat conductive material (III) without deviation.
- the volume content of the voids in the core material (I) is preferably 10% or more and 85% or less with respect to the apparent volume of the core material (I). It is more preferably 20% or more and 85% or less, and further preferably 50% or more and 80% or less from the viewpoint of achieving both light weight and mechanical properties.
- the material of the core material (I) is not particularly limited, but for example, a fiber reinforced resin reinforced with continuous fibers or discontinuous fibers is preferably used.
- the continuous reinforcing fiber means a continuous reinforcing fiber having a length of at least 15 mm or more, preferably 100 mm or more in one direction.
- a unidirectional fiber reinforced resin or a woven fiber reinforced resin can be used.
- the fiber reinforced resin reinforced with discontinuous fibers either a short fiber reinforced resin or a long fiber reinforced resin can be used.
- a resin sheet, a resin foam, or the like can also be used.
- the resin is not particularly limited and may be a thermosetting resin or a thermoplastic resin.
- the thermoplastic resin is, for example, "polyethylene terephthalate (PET), polybutylene terephthalate (PBT), polytrimethylene terephthalate (PTT), polyethylene naphthalate (PEN), polyester such as liquid crystal polyester, polyethylene (PE), polypropylene ( Polyetherketone such as PP) and polybutylene, polyarylene sulfide such as polyoxymethylene (POM), polyamide (PA), and polyphenylene sulfide (PPS), polyetherketone (PK), polyetherketone (PEK), and polyetheretherketone (PEEK).
- Polyetherketone Ketone PEKK
- Polyethernitrile PEN
- Polytetrafluoroethylene and other fluororesins "Sterine resins, polycarbonate (PC), Polymethylmethacrylate (PMMA) ), Polyvinyl chloride (PVC), Polyphenylene ether (PPE), Polyethylene (PI), Polyamideimide (PAI), Polyetherimide (PEI), Polysalphon (PSU), Polyethersalphon, Polyallylate (PAR), etc.
- Non-crystalline resin, other phenol-based resin, phenoxy resin, and thermoplastic elastomers such as polystyrene-based, polyolefin-based, polyurethane-based, polyester-based, polyamide-based, polybutadiene-based, polyisoprene-based, fluorine-based resin, and acrylonitrile-based And the thermoplastic resin selected from these copolymers and modified products.
- polyolefin is preferable from the viewpoint of the light weight of the obtained sandwich structure.
- the core material (I) contains a porous body
- polyolefin is preferable because it synergizes the lightweight effect.
- polyamide is preferable from the viewpoint of strength.
- the core material (I) when the core material (I) is made of a fiber reinforced resin, polyamide is preferable from the viewpoint of the interfacial bonding strength between the reinforced fiber and the resin.
- the thermosetting resin includes, for example, unsaturated porester resin, vinyl ester resin, epoxy resin, phenol (resole) resin, urea resin, melamine resin, polyimide resin, maleimide resin, benzoxazine resin, and the like, and two types thereof. Examples thereof include thermosetting resins such as resins blended with the above.
- an epoxy resin is preferably used from the viewpoint of the interfacial bonding strength between the reinforced fiber and the resin.
- the resins include mica, talc, kaolin, hydrotalcite, sericite, bentonite, zonotrite, sepiolite, smectite, montmorillonite, wallastenite, silica, calcium carbonate, glass beads, glass flakes, glass micros, depending on the application.
- Fillers such as metal-based, metal oxide-based, conductivity-imparting materials such as carbon black and graphite powder, halogen-based flame retardants such as brominated resin, antimony-based flame retardants such as antimony trioxide and antimony pentoxide, polyphosphorus.
- Phosphoric flame retardants such as ammonium acid, aromatic phosphate and red phosphorus, organic acid metal salt flame retardants such as borate metal salts, carboxylic acid metal salts and aromatic sulfonimide metal salts, zinc borate, zinc, zinc oxide And inorganic flame retardants such as zirconium compounds, nitrogen-based flame retardants such as cyanuric acid, isocyanuric acid, melamine, melamine cyanurate, melamine phosphate and guanidine nitrogenized, fluorine-based flame retardants such as PTFE, silicone-based such as polyorganosiloxane.
- organic acid metal salt flame retardants such as borate metal salts, carboxylic acid metal salts and aromatic sulfonimide metal salts, zinc borate, zinc, zinc oxide
- inorganic flame retardants such as zirconium compounds
- nitrogen-based flame retardants such as cyanuric acid, isocyanuric acid, melamine, melamine cyanurate, mel
- Metal hydroxide flame retardants such as aluminum hydroxide and magnesium hydroxide, and other flame retardants, cadmium oxide, zinc oxide, cuprous oxide, cupric oxide, ferrous oxide, secondary flame retardant Flame retardants such as iron, cobalt oxide, manganese oxide, molybdenum oxide, tin oxide and titanium oxide, pigments, dyes, lubricants, mold release agents, compatibilizers, dispersants, crystal nucleating agents such as mica, talc and kaolin.
- metal hydroxide flame retardants such as aluminum hydroxide and magnesium hydroxide, and other flame retardants
- cadmium oxide zinc oxide
- cuprous oxide cupric oxide
- ferrous oxide ferrous oxide
- secondary flame retardant Flame retardants such as iron, cobalt oxide, manganese oxide, molybdenum oxide, tin oxide and titanium oxide, pigments, dyes, lubricants, mold release agents, compatibilizers, dispersants, crystal nucleating agents such as mica, talc and kaolin.
- Plastics such as phosphate esters, heat stabilizers, antioxidants, color inhibitors, UV absorbers, fluidity modifiers, foaming agents, antibacterial agents, anti-vibration agents, deodorants, slidable modifiers , And an antistatic agent such as polyether ester amide may be added.
- flame retardancy may be required, and phosphorus-based flame retardants, nitrogen-based flame retardants, and inorganic flame retardants are preferably added.
- the flame retardant is 1 to 20 parts by mass with respect to 100 parts by mass of the resin in order to exhibit a flame retardant effect and maintain a good balance between the mechanical properties of the resin used and the fluidity of the resin during molding. Is preferable. More preferably, it is 1 to 15 parts by mass.
- the specific gravity of the core material (I) is preferably 0.01 to 1.5 from the viewpoint of the light weight of the sandwich structure. It is more preferably 0.1 to 1.3, and even more preferably 0.3 to 1.1.
- the specific gravity can be measured by cutting out the core material (I) and measuring it in accordance with ISO1183 (1987) or ISO0845 (1988).
- the type of reinforcing fiber contained is not particularly limited, and for example, carbon fiber, glass fiber, aramid fiber, alumina fiber, silicon carbide fiber, boron fiber, metal fiber, etc. Natural fibers, mineral fibers and the like can be used, and these may be used alone or in combination of two or more.
- carbon fibers such as PAN-based, pitch-based, and rayon-based are preferably used from the viewpoint of high specific strength and specific rigidity and weight reduction effect.
- glass fiber can be preferably used, and in particular, carbon fiber and glass fiber are preferably used in combination from the viewpoint of the balance between mechanical properties and economic efficiency.
- aramid fibers can be preferably used from the viewpoint of enhancing the shock absorption and shapeability of the obtained sandwich structure, and it is particularly preferable to use carbon fibers and aramid fibers in combination from the viewpoint of the balance between mechanical properties and shock absorption. .. Further, from the viewpoint of increasing the conductivity of the obtained sandwich structure, reinforcing fibers coated with a metal such as nickel, copper or ytterbium, or pitch-based carbon fibers can also be used.
- the reinforcing fibers are surface-treated with a sizing agent from the viewpoint of improving mechanical properties.
- a sizing agent include polyfunctional epoxy resins, acrylic acid-based polymers, polyhydric alcohols, polyethyleneimines, and the like. Specific examples thereof include glycerol triglycidyl ether, diglycerol polyglycidyl ether, polyglycerol polyglycidyl ether, and sorbitol polyglycidyl ether.
- Arabitol polyglycidyl ether trimethylolpropan triglycidyl ether, polyglycidyl ether of aliphatic polyhydric alcohols such as pentaerythritol polyglycidyl ether, polyacrylic acid, copolymer of acrylic acid and methacrylic acid, acrylic acid and malein Polymers with acids, or mixtures of two or more of these, polyvinyl alcohol, glycerol, diglycerol, polyglycerol, sorbitol, arabitol, trimethylolpropane, pentaerythritol, polyethyleneimine containing more amino groups in one molecule, etc.
- polyvinyl alcohol glycerol, diglycerol, polyglycerol, sorbitol, arabitol, trimethylolpropane, pentaerythritol, polyethyleneimine containing more amino groups in one molecule, etc.
- glycerol triglycidyl ether diglycerol polyglycidyl ether, and polyglycerol polyglycidyl are available because they contain a large amount of highly reactive epoxy groups in one molecule, are highly water-soluble, and are easy to apply. Ether is preferably used.
- the porous body is made of a fiber reinforced resin.
- the reinforcing fiber of the fiber reinforced resin may be a continuous fiber or a discontinuous fiber, but is preferably a discontinuous fiber, and the discontinuous fiber forms a three-dimensional network and is a discontinuous fiber. It is more preferable to have a structure in which the intersections of the two are bonded by a resin. By joining the discontinuous fibers with the resin, the shear elastic modulus of the core material (I) is increased, and the rigidity of the sandwich structure is increased.
- this aspect will be described.
- the discontinuous fibers preferably exist as fineness strands of less than 500 fibers, and more preferably dispersed in the form of single fibers.
- the fiber length of the discontinuous fiber is preferably 1 to 50 mm, more preferably 3 to 30 mm. When it is 1 mm or more, the reinforcing effect of the discontinuous fibers can be efficiently exhibited. Further, when it is 50 mm or less, the dispersion of discontinuous fibers can be kept good.
- the ratio of the number of bonded portions in which the single fibers of the discontinuous fibers are bonded by the resin is 50% or more, more preferably 70% or more, and further, to the total number of crossed portions in which the discontinuous fibers are crossed. It is preferably 90% or more.
- the mass ratio of the discontinuous fibers is preferably 5 to 60% by mass, more preferably 10 to 50% by mass, and further preferably 10 to 50% by mass with respect to the entire core material (I) from the viewpoint of achieving both mechanical properties and moldability. Is 15 to 40% by mass.
- the fiber reinforced resin it is preferable that 30% or more, more preferably 50% or more, still more preferably 80% or more of the surface of the discontinuous fiber is coated with the resin.
- the rigidity of the core material (I) can be increased.
- the coverage is measured by observing the cross section of the core material (I) with a scanning electron microscope (SEM) and distinguishing between the reinforcing fiber and the resin.
- the fiber reinforcing material (II) is a member containing reinforcing fibers, which constitutes the skin material of the sandwich structure and has a higher elastic modulus than the core material (I).
- the material of the fiber reinforcing material (II) is not particularly limited as long as it has a higher elastic modulus than the core material (I), and even a fiber reinforced resin reinforced with continuous fibers or reinforced with discontinuous fibers. It may be a fiber reinforced resin. As the fiber reinforced resin reinforced with continuous fibers, a unidirectional fiber reinforced resin or a woven fiber reinforced resin can be used. As the fiber reinforced resin reinforced with discontinuous fibers, either a short fiber reinforced resin or a long fiber reinforced resin can be used. From the viewpoint of the mechanical properties of the sandwich structure, it is preferable to use a continuous fiber reinforcing material, and it is more preferable to use a unidirectional fiber reinforcing material.
- a discontinuous fiber reinforced material can be preferably used.
- the matrix resin of the fiber reinforced resin is not particularly limited, and either a thermosetting resin or a thermoplastic resin can be used, and the same resin as exemplified in the above description of the core material (I) should be used. Can be done. Further, the matrix resin may contain an additive, and examples of the additive include the additives exemplified in the above description of the core material (I).
- the type of reinforcing fiber contained in the fiber reinforcing material (II) is not particularly limited, and the same reinforcing fiber as that exemplified in the above description of the core material (I) can be used.
- the mass ratio of the reinforcing fibers in the fiber reinforcing material (II) is preferably 30 to 90% by mass, more preferably 40 to 90% by mass, based on 100% by mass of the fiber reinforcing material (II), from the viewpoint of achieving both mechanical properties and moldability. It is 80% by mass, more preferably 50 to 70% by mass. It may be a range in which any of the above upper limit and lower limit is combined.
- the fiber reinforcing material (II) preferably contains a carbon fiber reinforced resin, and more preferably is made of a carbon fiber reinforced resin.
- the carbon fiber reinforced resin is composed of carbon fiber and a matrix resin.
- pitch-based carbon fibers having high elastic modulus and thermal conductivity are more preferable. By using pitch-based carbon fibers, it is expected that the rigidity and heat dissipation of the sandwich structure will be improved.
- the fiber reinforcing material (II) may have a laminated structure in which a plurality of the above-mentioned members are laminated.
- the sandwich structure of the present invention can be preferably produced by any of the methods [1] to [3] shown below.
- Method [1] A method for producing a sandwich structure of the present invention, in which a precursor of a core material (I) is placed on at least one surface and at least one end face of the heat conductive material (III) and heat pressed.
- a method for producing a sandwich structure which comprises a step of joining the fiber reinforcing material (II) to both sides of the core material (I) in this order.
- Method [2] A method for producing a sandwich structure of the present invention, wherein a precursor of the core material (I) is placed on at least one surface and at least one end face of the heat conductive material (III).
- a method for producing a sandwich structure which comprises a step of arranging a precursor of the fiber reinforcing material (II) on both sides of the precursor of the core material (I) and a step of heat pressing in this order.
- Method [3] A method for producing a sandwich structure of the present invention, in which a precursor of a core material (I) is placed on at least one surface and at least one end face of the heat conductive material (III) and heat pressed.
- a method for producing a sandwich structure which comprises a step of arranging a precursor of the fiber reinforcing material (II) on both sides of the core material (I), and a step of heat pressing in this order.
- arranging the precursor of the core material (I) on at least one surface and at least one end face of the heat conductive material (III) means the precursor of the core material (I). It means that the body is arranged so as to cover at least one surface and at least one end face of the heat conductive material (III).
- the precursor of the core material (I) is arranged on both sides of the heat conductive material (III). Further, in the methods [1] to [3], the precursor of the core material (I) is more preferably arranged on at least two end faces of the heat conductive material (III), and further, of the heat conductive material (III). It is more preferably arranged on both sides, and it is particularly preferable that the heat conductive material (III) is arranged on both sides and all end faces, that is, the heat conductive material (III) is included.
- the precursor of the core material (I) is, for example, a prepreg containing the reinforcing fibers and the resin when the core material (I) is a fiber reinforced resin.
- the core material (I) is a non-fiber reinforced resin, examples thereof include a resin sheet containing a foaming agent and a laminate of resin sheets.
- the precursor of the core material (I) is, for example, a discontinuous reinforcing fiber. It can be produced by impregnating a mat with a film or non-woven fabric of a thermoplastic resin while compressing it.
- the discontinuous reinforcing fiber mat is produced, for example, by previously dispersing discontinuous reinforcing fibers in a strand shape, preferably in the form of substantially single fibers, and more preferably in the form of single fibers.
- dry processes such as the airlaid method in which discontinuous reinforcing fibers are dispersed by an air flow to form a sheet, and the carding method in which discontinuous reinforcing fibers are mechanically combed to form a sheet.
- dry processes such as the airlaid method in which discontinuous reinforcing fibers are dispersed by an air flow to form a sheet, and the carding method in which discontinuous reinforcing fibers are mechanically combed to form a sheet.
- examples thereof include a wet process by the Radrite method in which discontinuous reinforcing fibers are stirred in water to make paper.
- a means for making discontinuous reinforcing fibers closer to a single fiber as a means for making discontinuous reinforcing fibers closer to a single fiber, a means for providing a spread bar, a means for vibrating the spread bar, a means for finening the eyes of the card, and a means for adjusting the rotation speed of the card. Examples of means for doing so can be exemplified.
- a means for adjusting the stirring conditions of the discontinuous reinforcing fibers, a means for diluting the reinforcing fiber concentration of the dispersion liquid, a means for adjusting the viscosity of the dispersion liquid, and a vortex flow when transferring the dispersion liquid examples thereof include means for suppressing the suppression.
- the discontinuous reinforcing fiber mat is preferably manufactured by a wet method, and the discontinuous reinforcement is performed by increasing the concentration of the input fiber or adjusting the flow velocity (flow rate) of the dispersion liquid and the speed of the mesh conveyor.
- the proportion of reinforcing fibers in the fiber mat can be easily adjusted. For example, by slowing the speed of the mesh conveyor with respect to the flow velocity of the dispersion liquid, it becomes difficult for the fibers in the obtained discontinuous reinforcing fiber mat to be oriented in the take-back direction, and a bulky discontinuous reinforcing fiber mat can be manufactured. Is.
- the discontinuous reinforcing fiber mat may be composed of a single discontinuous reinforcing fiber, the discontinuous reinforcing fiber is mixed with a matrix resin component in the powder shape or the fiber shape, or the discontinuous reinforcing fiber is organic. It may be mixed with a compound or an inorganic compound, or discontinuous reinforcing fibers may be sealed with a resin component.
- the pressure when the discontinuous reinforcing fiber mat is impregnated with the thermoplastic resin film or non-woven fabric is preferably 0.5 MPa or more and 30 MPa or less, more preferably 1 MPa or more and 5 MPa or less. If the pressure is less than 0.5 MPa, the thermoplastic resin may not impregnate the discontinuous reinforcing fiber mat, and if it is more than 30 MPa, it becomes difficult to adjust the thickness of the precursor of the core material.
- the temperature at which the thermoplastic resin film or non-woven fabric is impregnated is preferably a temperature equal to or higher than the melting point or the glass transition point of the thermoplastic resin, and is equal to or higher than the temperature obtained by adding 10 ° C. to the melting point or the glass transition point.
- the temperature is more preferably 20 ° C. or higher added to the melting point or the glass transition point. If the temperature at which the film or non-woven fabric of the thermoplastic resin is impregnated is too high than the melting point of the thermoplastic resin or the glass transition point, the thermoplastic resin may be decomposed or deteriorated, so that the thermoplastic resin is plastic. It is preferably equal to or lower than the temperature obtained by adding 150 ° C. to the melting point of the resin or the glass transition point.
- a compression molding machine or a double belt press machine can be preferably used as equipment for realizing a method of impregnating a discontinuous reinforcing fiber mat with a film or non-woven fabric of a thermoplastic resin.
- the compression molding machine is a batch type, and productivity can be improved by using an intermittent press system in which two or more machines for heating and cooling are arranged in parallel.
- the double belt press machine is a continuous type and is excellent in continuous productivity because continuous processing can be easily performed.
- the precursor of the fiber reinforcing material (II) is usually a prepreg containing reinforcing fibers and a resin.
- a prepreg containing reinforcing fibers and a resin for example, a unidirectional fiber prepreg or a woven fiber prepreg reinforced with continuous fibers, or a laminate in which a reinforcing fiber sheet and a resin sheet are laminated can be mentioned.
- Each of the methods [1] to [3] has a step of heat pressing.
- a precursor of the core material (I) is placed on at least one surface and at least one end face of the heat conductive material (III), which is necessary for the expansion temperature or joining of the precursor of the core material (I).
- the heat conductive material can be included in the core material by hot pressing at a different temperature.
- a compression molding machine can be preferably used as the heat pressing equipment.
- the compression molding machine is a batch type, and productivity can be improved by using an intermittent press system in which two or more machines for heating and cooling are arranged in parallel.
- the heat conductive material (III) is included in the core material (I), and then the fiber reinforced materials (II) are formed on both sides of the molded core material (I). It is a method of joining.
- the means for joining the core material (I) and the fiber reinforcing material (II) is not particularly limited, but for example, the core material (I) and the fiber reinforcing material (II) are hot-plate welded, vibration-welded, or super-welded. There are methods of joining by ultrasonic welding, laser welding, resistance welding, induction heating welding, or an adhesive. It can be preferably used when the molding conditions such as the molding temperature and the molding pressure of the core material (I) and the fiber reinforced material (II) are significantly different.
- Method [2] is a method of simultaneously molding and joining the core material (I) and the fiber reinforced material (II). It can be preferably used when the molding conditions such as the molding temperature and the molding pressure of the core material (I) and the fiber reinforced material (II) are close to each other. Since the core material (I) and the fiber reinforced material (II) can be molded and joined at the same time, it is preferable from the viewpoint of productivity.
- the heat conductive material (III) is included in the core material (I), and then the fiber reinforced material (II) is formed on both sides of the molded core material (I). It is a method of arranging the precursor of the above and performing heat pressing. Since the core material (I) and the fiber reinforced material (II) can be joined and the fiber reinforced material (II) can be formed at the same time, it is preferable from the viewpoint of productivity.
- the housing of the present invention is made by using the sandwich structure of the present invention.
- the sandwich structure of the present invention it is possible to obtain a housing having both excellent mechanical properties and light weight. Further, from the viewpoint of mass productivity, it is preferable because molding by high cycle molding such as press molding is possible.
- the housing of the present invention can be obtained, for example, by producing a sandwich structure having a desired housing shape by the above-mentioned method for manufacturing a sandwich structure.
- a 0.1% by mass aqueous dispersion of a surfactant (polyoxyethylene lauryl ether (trade name) manufactured by Nakaraitex Co., Ltd.) was prepared, and this dispersion and a chopped carbon fiber bundle were put into a papermaking machine to generate carbon.
- a fiber mat was prepared.
- the paper machine includes a dispersion tank, a paper making tank, and a transport unit that connects the dispersion tank and the paper making tank.
- the dispersion tank is equipped with a stirrer and can disperse the charged dispersion liquid and the chopped carbon fiber bundle.
- the papermaking tank is provided with a mesh conveyor having a papermaking surface at the bottom, and a conveyor capable of transporting the papermaking carbon fiber mat is connected to the mesh conveyor. Papermaking was carried out with the fiber concentration in the dispersion liquid being 0.05% by mass.
- the paper-made carbon fiber mat was dried in a drying oven at 200 ° C.
- a 3% by mass aqueous dispersion of the binder (“Polyment” (registered trademark) SK-1000, manufactured by Nippon Shokubai Co., Ltd.) was applied to the upper surface of the carbon mat transported by the conveyor. It was sprayed. The excess binder was sucked and dried in a drying oven at 200 ° C. to obtain a carbon fiber mat. The basis weight of the obtained carbon fiber mat was 50 g / m 2 .
- Reference Example 5 Preparation of unidirectional prepreg
- the carbon fiber bundles of Reference Example 1 are arranged in one direction in a sheet shape, two epoxy resin films of Reference Example 4 are laminated from both sides of the carbon fiber bundle, and the resin is heated and pressed.
- a unidirectional prepreg having a carbon fiber texture of 110 g / m 2 , a thickness of 0.1 mm, and a matrix resin mass fraction of 30 mass% was obtained.
- Example 1 Carbon fiber mat of Reference Example 2, polypropylene resin film of Reference Example 3, unidirectional prepreg of Reference Example 5, graphite sheet (manufactured by Panasonic Corporation, "PGS” (registered trademark) EYGS182307, in-plane thermal conductivity
- PPS registered trademark
- This laminate was sandwiched between release films and further sandwiched between tool plates. They were put into a press molding machine having a board surface temperature of 180 ° C. and heat-pressed at 3 MPa for 10 minutes to cure the prepreg and impregnate the carbon fiber mat with polypropylene resin. Next, a spacer having a thickness of 1 mm is inserted between the tool plates, put into a press molding machine having a plate surface temperature of 40 ° C., and cooled and pressed until the laminate cools at a surface pressure of 3 MPa. Obtained a sandwich structure in which When the thickness of the sample was measured with a micrometer, the thickness was 1.0 mm.
- the carbon fiber mat impregnated with polypropylene resin springs back, and the core material becomes a porous body. Since the sample in this example is a flat plate, the thickness is constant. Therefore, the thickness measured at any point of the sample is the maximum thickness. The same applies to the other examples and comparative examples.
- the bending test piece was preformed in the same manner except that the carbon fiber mat, the polypropylene resin film, and the unidirectional prepreg were adjusted to a size of 50 mm ⁇ 40 mm, and the graphite sheet was adjusted to a size of 40 mm ⁇ 30 mm.
- Press molding was performed to obtain a bending test piece of a sandwich structure in which a core material was arranged around a heat conductive material.
- a cross-sectional view of the obtained sandwich structure is shown in FIG.
- the obtained sandwich structure has a fiber reinforcing material layer composed of a unidirectional fiber reinforcing material 0 ° 7 and a unidirectional fiber reinforcing material 90 ° 8 on both sides of the core material 2.
- the graphite sheet 9 has a structure in which both sides and all end faces are covered with a core material, and has a structure protected by the core material. Therefore, the mechanical properties of the obtained sandwich structure were excellent, and the graphite sheet was not peeled off and the graphite sheet fragments were not scattered. Moreover, since it contains a graphite sheet, it has excellent heat dissipation.
- Example 2 The number of laminated graphite sheets was changed to 4, [One-way prepreg 0 ° / One-way prepreg 90 ° / Polypropylene resin film / Carbon fiber mat / Graphite sheet / Graphite sheet / Graphite sheet / Graphite sheet / Carbon fiber mat / Polypropylene Preform and press molding were performed in the same manner as in Example 1 except that the resin film / unidirectional prepreg 90 ° / unidirectional prepreg 0 °] was laminated, and the core material was arranged around the heat conductive material. , A sandwich structure and a bending test piece of the sandwich structure were obtained. A cross-sectional view of the obtained sandwich structure is shown in FIG. Since the graphite sheet was protected by the core material, the mechanical properties of the obtained sandwich structure were excellent. In addition, since it contains a plurality of graphite sheets, it has excellent heat dissipation.
- Example 1 Preform and press molding were carried out in the same manner as in Example 1 except that the size of the graphite sheet was adjusted to a size of 50 ⁇ 150 mm to obtain a sandwich structure in which all the ends of the heat conductive material were exposed. Further, at the time of producing the bending test piece, preform and press molding were performed in the same manner as in Example 1 except that the graphite sheet was adjusted to a size of 50 mm ⁇ 40 mm, and all the ends of the heat conductive material were exposed. , A bending test piece of a sandwich structure was obtained. A cross-sectional view of the obtained sandwich structure is shown in FIG. In the obtained sandwich structure, all edges of the graphite sheet were exposed, so that peeling occurred between the layers of the graphite sheet.
- Example 2 Preform and press molding were carried out in the same manner as in Example 2 except that the size of the graphite sheet was adjusted to a size of 50 ⁇ 150 mm to obtain a sandwich structure in which all the ends of the heat conductive material were exposed. Further, at the time of producing the bending test piece, preform and press molding were performed in the same manner as in Example 2 except that the graphite sheet was adjusted to a size of 50 mm ⁇ 40 mm, and all the ends of the heat conductive material were exposed. , A bending test piece of a sandwich structure was obtained. A cross-sectional view of the obtained sandwich structure is shown in FIG. The strength of the obtained sandwich structure was very low, and peeling occurred between the graphite sheets after press molding, so that the bending test and the heat dissipation evaluation could not be performed.
- Example 3 Preform and press molding were carried out in the same manner as in Example 1 except that the graphite sheets were not laminated to obtain a sandwich structure containing no heat conductive material. Similarly, when the bending test piece was produced, the bending test piece of the sandwich structure containing no heat conductive material was preformed and press-molded in the same manner as in Example 1 except that the graphite sheets were not laminated. Got A cross-sectional view of the obtained sandwich structure is shown in FIG. The obtained sandwich structure did not contain a heat conductive material, and therefore had low heat dissipation.
- the sandwich structure of the present invention can achieve both excellent heat dissipation and excellent mechanical properties. Therefore, it can be applied to a wide range of industrial fields as structural members of electric / electronic devices, robots, motorcycles, automobiles, aircraft, and the like. In particular, it can be preferably applied to a housing of an electronic device or the like that requires high heat dissipation.
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Abstract
Description
本明細書におけるサンドイッチ構造体とは、芯材の両面に、当該芯材よりも高い弾性率を有する表皮材を配置した構造体である。本発明のサンドイッチ構造体においては、芯材は、シート状の熱伝導材(III)を含む芯材(I)であり、表皮材は、繊維強化材(II)である。また、シート状とは、厚みが薄くて幅が広いものを指し、厚みが0.01μm以上10mm以下であり、幅と厚みのアスペクト比が10以上のものを意味するものとする。
・単位幅あたりの曲げ剛性(N・m)=E(Pa)×I(m4)/b(m)
また、サンドイッチ構造体の断面が矩形断面である場合は、矩形断面の断面二次モーメントIは、bh3/12(m4)であるため、次式により算出できる。
・単位幅あたりの曲げ剛性(N・m)=E(Pa)×h3(m3)/12
単位幅当たりの曲げ剛性を上述の範囲とするための手段としては、例えば、本発明のサンドイッチ構造体のように、表皮材として繊維強化材(II)を用いる方法が挙げられる。また、例えば、サンドイッチ構造体の厚みを厚肉とする方法が挙げられる。
本発明において、熱伝導材(III)はシート状であり、その面内熱伝導率は、300W/m・K以上である。熱伝導材(III)の面内熱伝導率は、500w/m・K以上が好ましく、1000w/m・K以上がさらに好ましい。面内熱伝導率は高ければ高いほど好ましいため、面内熱伝導率の上限については特に制限はないが、2000W/m・K程度の面内熱伝導率を有する熱伝導材が知られている。熱伝導材(III)の面内熱伝導率が300W/m・K以上であれば、サンドイッチ構造体の面内方向への熱の拡散が優れ、サンドイッチ構造体の放熱性は優れるものとなる。熱伝導材(III)の面内熱伝導率はレーザーフラッシュ法によりインプレーン測定用のサンプルホルダーにサンプルをセットし、サンプルの大きさを直径20~30mm程度、厚みを1.0mm以下とすることで測定することができる。また、レーザー光を吸収しにくい材料に対しては、サンプル表面に黒化膜を薄く均一に製膜する。赤外線検出素子の測温波長における放射率が低い材料に対しては、サンプル裏面に同様の処理を行う。
本発明においては、芯材(I)が多孔質体を含むことが好ましく、芯材(I)が多孔質体であることがより好ましい。芯材(I)が多孔質体を含むことにより、サンドイッチ構造体の軽量性の観点で有利である。また、芯材(I)に熱伝導材(III)を含ませる際、多孔質体である芯材(I)が、面外方向に潰れる、あるいは膨れることで、熱伝導材(III)の位置ずれなく、芯材(I)が熱伝導材(III)を含むことができる。芯材(I)が多孔質体である場合、芯材(I)中における空隙の体積含有率は、芯材(I)の見掛け体積に対して10%以上85%以下であることが好ましく、20%以上85%以下がより好ましく、軽量性と機械特性の両立の観点から50%以上80%以下であることがさらに好ましい。
上記難燃剤は、難燃効果の発現とともに、使用する樹脂の機械特性や成形時の樹脂流動性などと良好な特性バランスを保つために、樹脂100質量部に対して難燃剤1~20質量部とすることが好ましい。より好ましくは1~15質量部である。
本発明において、繊維強化材(II)はサンドイッチ構造体の表皮材を構成する、芯材(I)よりも弾性率が高い、強化繊維を含む部材である。
本発明のサンドイッチ構造体は、以下に示す[1]~[3]のいずれかの方法で、好ましく製造することができる。
本発明の筐体は、本発明のサンドイッチ構造体を用いてなる。本発明のサンドイッチ構造体を利用することで優れた力学特性と軽量性を両立した筐体を得ることが出来る。また、量産性の観点でもプレス成形などのハイサイクル成形での成形が可能であるため好ましい。
作製したサンドイッチ構造体の曲げ試験片を、ISO178法(1993)に従い曲げ特性を測定した。曲げ試験片の最表面の繊維方向を曲げ方向として、測定数n=5とし、平均値を曲げ強度および曲げ弾性率とした。測定装置としてはインストロン・ジャパン(株)製、“インストロン”(登録商標)5565型万能材料試験機を使用した。
図3に示すように、作製したサンドイッチ構造体1の裏面四隅に10mm×10mmの厚み3mmのゴム製スペーサ6を貼り付け、実験台に設置した。設置したサンドイッチ構造体の表面片隅に50mm×25mmのマイクロセラミックヒーター5(坂口電熱(株)製、マイクロセラミックヒーターMS-2(商品名))を設置し、一定電流・一定電圧下、10Wでヒーターを加熱した。ヒーター加熱開始から15分後のヒーター温度が一定になった時のヒーター温度から放熱性を、下記基準により評価した。
A:ヒーター温度100℃未満(放熱性が非常に高い)
B:ヒーター温度100℃以上120℃未満(放熱性が高い)
C:ヒーター温度120℃以上(放熱性が低い)
(参考例1)炭素繊維束の作製
ポリアクリロニトリルを主成分とする重合体から紡糸、焼成処理を行い、総フィラメント数12000本の炭素繊維連続束を得た。該炭素繊維連続束に浸漬法によりサイジング剤を付与し、120℃の温度の加熱空気中で乾燥し、炭素繊維束を得た。この炭素繊維束の特性は次の通りであった。
単位長さ当たりの質量:0.8g/m
密度:1.8g/cm3
引張強度:4.2GPa
引張弾性率:230GPa
サイジング種類:ポリオキシエチレンオレイルエーテル
サイジング付着量:1.5質量%
(参考例2)炭素繊維マットの作製
参考例1の炭素繊維束をカートリッジカッターで繊維長6mmにカットし、チョップド炭素繊維束を得た。界面活性剤(ナカライテクス(株)製、ポリオキシエチレンラウリルエーテル(商品名))0.1質量%の水分散液を作製し、この分散液とチョップド炭素繊維束を抄紙機に投入し、炭素繊維マットを作製した。
無変性ポリプロピレン樹脂(プライムポリマー(株)製、“プライムポリプロ”(登録商標)J105G)を90質量%と、酸変性ポリプロピレン樹脂(三井化学(株)製、“アドマー”(登録商標)QE510)を10質量%と、をブレンドした。このブレンド品を押出機で溶融混錬した後、T字ダイから押出した。その後、60℃のチルロールで引き取り、樹脂を冷却固化することで、ポリプロピレン樹脂フィルムを得た。
エポキシ樹脂(ベースレジン:ジシアンジアミド/ジクロロフェニルメチルウレア硬化系エポキシ樹脂)を、コーターを用いて、離型紙上に塗布してエポキシ樹脂フィルムを得た。
参考例1の炭素繊維束をシート状に一方向に配列させ、参考例4のエポキシ樹脂フィルム2枚を炭素繊維束の両面から重ね、加熱加圧により樹脂を含浸させ、炭素繊維の目付が110g/m2、厚み0.1mm、マトリックス樹脂の質量分率が30質量%の一方向プリプレグを得た。
参考例2の炭素繊維マットと、参考例3のポリプロピレン樹脂フィルムと、参考例5の一方向プリプレグと、グラファイトシート(パナソニック(株)製、“PGS”(登録商標)EYGS182307、面内熱伝導率1000W/m・K)とを用いて、サンドイッチ構造体を作製した。炭素繊維マットと、ポリプロピレン樹脂フィルムと、一方向プリプレグを50mm×150mmのサイズに調整し、グラファイトシートを40mm×140mmのサイズに調整した後、[一方向プリプレグ0°/一方向プリプレグ90°/ポリプロピレン樹脂フィルム/炭素繊維マット/グラファイトシート/炭素繊維マット/ポリプロピレン樹脂フィルム/一方向プリプレグ90°/一方向プリプレグ0°]の順に表面の一方向プリプレグの繊維方向がサンプルの長手方向となるように積層した。この際、グラファイトシートは積層体の中央に配置した。この積層体を離型フィルムで挟み、さらにツール板で挟んだ。それらを盤面温度が180℃のプレス成形機に投入し、3MPaで10分間、加熱プレスすることで、プリプレグの硬化と炭素繊維マットへのポリプロピレン樹脂の含浸を行った。次に、ツール板の間に厚み1mmのスペーサを挿入し、盤面温度が40℃のプレス成形機に投入し、面圧3MPaで積層体が冷えるまで冷却プレスすることで、熱伝導材の周囲に芯材が配置された、サンドイッチ構造体を得た。マイクロメーターでサンプルの厚みを測定したところ、厚みは1.0mmであった。ツール板の間に厚み1.0mmのスペーサを挿入することで、ポリプロピレン樹脂が含浸した炭素繊維マットがスプリングバックし、芯材が多孔質体となる。なお、本実施例におけるサンプルは平板であるため、厚みは一定である。したがって、サンプルのいずれかの点で測定した厚みが最大厚みとなる。他の実施例、比較例についても同様である。
グラファイトシートの積層枚数を4枚に変更し、[一方向プリプレグ0°/一方向プリプレグ90°/ポリプロピレン樹脂フィルム/炭素繊維マット/グラファイトシート/グラファイトシート/グラファイトシート/グラファイトシート/炭素繊維マット/ポリプロピレン樹脂フィルム/一方向プリプレグ90°/一方向プリプレグ0°]の順に積層したこと以外は実施例1と同様にして、プリフォーム、プレス成形を行い、熱伝導材の周囲に芯材が配置された、サンドイッチ構造体と、サンドイッチ構造体の曲げ試験片を得た。得られたサンドイッチ構造体の断面図を図5に示す。グラファイトシートが芯材に保護されているため、得られたサンドイッチ構造体の機械特性は優れていた。また、複数のグラファイトシートを含んでいるため、放熱性も非常に優れていた。
グラファイトシートのサイズを50×150mmのサイズに調整したこと以外は実施例1と同様にして、プリフォーム、プレス成形を行い、熱伝導材のすべての端部が露出したサンドイッチ構造体を得た。また、曲げ試験片作製時は、グラファイトシートを50mm×40mmのサイズに調整したこと以外は実施例1と同様にして、プリフォーム、プレス成形を行い、熱伝導材のすべての端部が露出した、サンドイッチ構造体の曲げ試験片を得た。得られたサンドイッチ構造体の断面図を図6に示す。得られたサンドイッチ構造体は、グラファイトシートのすべての端部が露出しているため、グラファイトシートの層間で剥離が生じた。
グラファイトシートのサイズを50×150mmのサイズに調整したこと以外は実施例2と同様にして、プリフォーム、プレス成形を行い、熱伝導材のすべての端部が露出したサンドイッチ構造体を得た。また、曲げ試験片作製時は、グラファイトシートを50mm×40mmのサイズに調整したこと以外は実施例2と同様にして、プリフォーム、プレス成形を行い、熱伝導材のすべての端部が露出した、サンドイッチ構造体の曲げ試験片を得た。得られたサンドイッチ構造体の断面図を図7に示す。得られたサンドイッチ構造体の強度はとても低く、プレス成形後にグラファイトシートとグラファイトシートの間で剥離が生じたため、曲げ試験、放熱性評価は実施できなかった。
グラファイトシートを積層しなかったこと以外は実施例1と同様にして、プリフォーム、プレス成形を行い、熱伝導材を含まないサンドイッチ構造体を得た。また、曲げ試験片作製時も同様に、グラファイトシートを積層しなかったこと以外は実施例1と同様にして、プリフォーム、プレス成形を行い、熱伝導材を含まないサンドイッチ構造体の曲げ試験片を得た。得られたサンドイッチ構造体の断面図を図8に示す。得られたサンドイッチ構造体は、熱伝導材を含んでいないため、放熱性が低かった。
2.芯材(I)
3.繊維強化材(II)
4.熱伝導材(III)
5.ヒーター
6.ゴム製スペーサ
7.一方向繊維強化材0°
8.一方向繊維強化材90°
9.グラファイトシート
Claims (15)
- 芯材(I)と、前記芯材(I)の両面に配置された繊維強化材(II)とを有するサンドイッチ構造体であって、前記芯材(I)が、面内熱伝導率が300W/m・K以上のシート状の熱伝導材(III)を含むサンドイッチ構造体。
- 前記芯材(I)が前記熱伝導材(III)の少なくとも二つの端面を覆っている、請求項1に記載のサンドイッチ構造体。
- 前記芯材(I)が前記熱伝導材(III)の両面および全ての端面を覆っている、請求項2に記載のサンドイッチ構造体。
- 前記熱伝導材(III)が、グラファイトシート、金属シートおよびセラミックスシートからなる群より選択される熱伝導シートを含む、請求項1~3のいずれかに記載のサンドイッチ構造体。
- 前記熱伝導材(III)が複数の前記熱伝導シートの積層構造体を含む、請求項4に記載のサンドイッチ構造体。
- 前記熱伝導材(III)が前記芯材(I)と接着されていない、請求項1~5のいずれかに記載のサンドイッチ構造体。
- 前記芯材(I)が多孔質体を含む、請求項1~6のいずれかに記載のサンドイッチ構造体。
- 前記多孔質体が繊維強化樹脂からなる、請求項7に記載のサンドイッチ構造体。
- 前記繊維強化材(II)が炭素繊維強化樹脂を含む、請求項1~8のいずれかに記載のサンドイッチ構造体。
- 単位幅あたりの曲げ剛性が0.5N・m以上である、請求項1~9のいずれかに記載のサンドイッチ構造体。
- 最大厚みが0.3mm以上3.0mm以下である、請求項1~10のいずれかに記載のサンドイッチ構造体。
- 請求項1~11のいずれかに記載のサンドイッチ構造体を用いてなる筐体。
- 請求項1~11のいずれかに記載のサンドイッチ構造体を製造する方法であって、前記熱伝導材(III)の少なくとも一つの表面及び少なくとも一つの端面に芯材(I)の前駆体を配置して熱プレスする工程、および前記芯材(I)の両面に前記繊維強化材(II)を接合する工程をこの順に含む、サンドイッチ構造体の製造方法。
- 請求項1~11のいずれかに記載のサンドイッチ構造体を製造する方法であって、前記熱伝導材(III)の少なくとも一つの表面及び少なくとも一つの端面に芯材(I)の前駆体を配置する工程、前記芯材(I)の前駆体の両面に繊維強化材(II)の前駆体を配置する工程、および熱プレスする工程をこの順に含む、サンドイッチ構造体の製造方法。
- 請求項1~11のいずれかに記載のサンドイッチ構造体を製造する方法であって、前記熱伝導材(III)の少なくとも一つの表面及び少なくとも一つの端面に芯材(I)の前駆体を配置して熱プレスする工程、および芯材(I)の両面に繊維強化材(II)の前駆体を配置する工程、および熱プレスする工程をこの順に含む、サンドイッチ構造体の製造方法。
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| EP20893360.6A EP4067064A4 (en) | 2019-11-29 | 2020-11-11 | SANDWICH STRUCTURE AND METHOD FOR PRODUCING THEREOF |
| CN202080081146.7A CN114728496A (zh) | 2019-11-29 | 2020-11-11 | 夹层结构体及其制造方法 |
| JP2020564288A JP7690735B2 (ja) | 2019-11-29 | 2020-11-11 | サンドイッチ構造体およびその製造方法 |
| US17/772,600 US12270611B2 (en) | 2019-11-29 | 2020-11-11 | Sandwich structure and method for manufacturing same |
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| US20240293978A1 (en) * | 2023-03-02 | 2024-09-05 | The Boeing Company | Forming Joints Between Composite Components |
| US12611844B2 (en) | 2021-11-19 | 2026-04-28 | The Boeing Company | Thermoplastic joining films and methods for joining thermoplastic and thermoset composite materials |
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| CN114728491B (zh) * | 2019-11-29 | 2025-09-30 | 东丽株式会社 | 导热体及其制造方法 |
| CN118083946B (zh) * | 2024-02-23 | 2026-01-06 | 深圳技术大学 | 废旧石墨负极诱导的钠离子电池硬炭及制备方法和应用 |
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| Publication number | Publication date |
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| JP7690735B2 (ja) | 2025-06-11 |
| KR102951132B1 (ko) | 2026-04-13 |
| US12270611B2 (en) | 2025-04-08 |
| JPWO2021106561A1 (ja) | 2021-06-03 |
| CN114728496A (zh) | 2022-07-08 |
| TW202128422A (zh) | 2021-08-01 |
| EP4067064A1 (en) | 2022-10-05 |
| EP4067064A4 (en) | 2024-03-20 |
| TWI890709B (zh) | 2025-07-21 |
| KR20220110180A (ko) | 2022-08-05 |
| US20220404106A1 (en) | 2022-12-22 |
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