WO2024075684A1 - サンドイッチパネル、およびサンドイッチパネルの製造方法 - Google Patents

サンドイッチパネル、およびサンドイッチパネルの製造方法 Download PDF

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Publication number
WO2024075684A1
WO2024075684A1 PCT/JP2023/035891 JP2023035891W WO2024075684A1 WO 2024075684 A1 WO2024075684 A1 WO 2024075684A1 JP 2023035891 W JP2023035891 W JP 2023035891W WO 2024075684 A1 WO2024075684 A1 WO 2024075684A1
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WIPO (PCT)
Prior art keywords
sandwich panel
fibers
core layer
sheet
panel according
Prior art date
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Ceased
Application number
PCT/JP2023/035891
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English (en)
French (fr)
Japanese (ja)
Inventor
大輔 磯部
信夫 寺師
浩二 小泉
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Sumitomo Bakelite Co Ltd
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Sumitomo Bakelite Co Ltd
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Publication date
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Priority to JP2024533939A priority Critical patent/JP7632763B2/ja
Priority to EP23874811.5A priority patent/EP4600033A1/en
Publication of WO2024075684A1 publication Critical patent/WO2024075684A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/20—Making multilayered or multicoloured articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0021—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with plain or filled structures, e.g. cores, placed between two or more plates or sheets, e.g. in a matrix
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32—Component parts, details or accessories; Auxiliary operations
    • B29C43/58—Measuring, controlling or regulating
    • B29C2043/5808—Measuring, controlling or regulating pressure or compressing force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32—Component parts, details or accessories; Auxiliary operations
    • B29C43/58—Measuring, controlling or regulating
    • B29C2043/5816—Measuring, controlling or regulating temperature
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2009/00—Layered products
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608—Honeycomb structures

Definitions

  • the present invention relates to a sandwich panel and a method for manufacturing a sandwich panel. More specifically, the present invention relates to a sandwich panel, a method for manufacturing a sandwich panel, and a molding material set for a sandwich panel.
  • Sandwich panels consist of a hollow honeycomb core with a hexagonal cross section and a pair of prepreg or other skin materials bonded to both sides of the honeycomb core. Sandwich panels, which are lightweight and highly rigid, are used, for example, in structural components for aircraft.
  • Patent Document 1 discloses a secondary adhesion formation process in which prepregs are laminated, placed in a vacuum bag and cured in an autoclave to harden the binder resin in the prepregs, and then composite prepregs are attached to both sides of a honeycomb core via a film-like adhesive, and pressure is applied at high temperature to harden the film-like adhesive.
  • the present invention provides the following sandwich panel and related technology.
  • a sandwich panel comprising a core layer having a honeycomb structure and a plurality of skin layers provided on both sides of the core layer, At least one of the skin layers is formed by laminating two or more prepregs with paper sheets interposed therebetween.
  • the sandwich panel according to [1] The sandwich panel comprises a sheet made of a thermosetting resin and short reinforcing fibers.
  • the sandwich panel according to [1] or [2] The thickness of the paper sheet is 5 ⁇ m or more and 150 ⁇ m or less.
  • thermosetting resin of the papermaking sheet contains one or more resins selected from the group consisting of phenolic resins, epoxy resins, unsaturated polyester resins, melamine resins, and polyurethane resins.
  • a sandwich panel according to any one of [2] to [5], A sandwich panel, wherein the fiber filler of the papermaking sheet includes one or more fibers selected from metal fibers, carbon fibers, glass fibers, ceramic fibers, polyamide fibers, aramid fibers, polyimide fibers, polyvinyl alcohol fibers, polyester fibers, acrylic fibers, polyparaphenylene benzoxazole fibers, polyethylene fibers, polypropylene fibers, polyacrylonitrile fibers, and ethylene vinyl alcohol fibers.
  • the fiber filler of the papermaking sheet includes one or more fibers selected from metal fibers, carbon fibers, glass fibers, ceramic fibers, polyamide fibers, aramid fibers, polyimide fibers, polyvinyl alcohol fibers, polyester fibers, acrylic fibers, polyparaphenylene benzoxazole fibers, polyethylene fibers, polypropylene fibers, polyacrylonitrile fibers, and ethylene vinyl alcohol fibers.
  • the prepreg is a sandwich panel formed using a sheet-like base material made of one or more fibers selected from aramid fibers, polyester fibers, polyphenylene sulfide fibers, carbon fibers, graphite fibers, glass fibers, and silicon carbide fibers.
  • the prepreg comprises, as a binder resin, one or more resins selected from the group consisting of a phenolic resin, an epoxy resin, an unsaturated polyester resin, a melamine resin, and a polyurethane resin.
  • the core layer is made of aramid fibers.
  • a sandwich panel according to any one of [1] to [10] The sandwich panel is used as an aircraft panel.
  • a method for manufacturing a sandwich panel comprising a core layer having a honeycomb structure and a plurality of skin layers provided on both sides of the core layer, At least one of the skin layers is formed by laminating two or more prepregs with a papermaking sheet interposed therebetween, a step of disposing the skin layers on each surface of the core layer; an integration step of integrating the core layer and the skin layer by a heating and pressurizing treatment;
  • a method for manufacturing a sandwich panel comprising: [13] A method for producing the sandwich panel according to [12], The method for producing a sandwich panel, wherein the integration step is carried out under conditions of 100 to 200°C and 1 to 20 kgf/ m2 .
  • a method for producing a sandwich panel according to [12] or [13] In the placing step, the skin layers are placed on each surface of the core layer by stacking one of the prepregs, the papermaking sheet, and the other of the prepregs in that order. [15] A method for producing a sandwich panel according to [12] or [13], Prior to the placing step, A skin layer forming step of laminating one of the prepregs, the papermaking sheet, and the other of the prepregs in this order and integrating them by heating and pressurizing to obtain the skin layer, In the placing step, A method for manufacturing a sandwich panel, comprising: disposing the skin layers on each side of the core layer via a hot melt adhesive.
  • a molding material set for a sandwich panel including a core layer having a honeycomb structure, a plurality of prepregs, and a plurality of papermaking sheets, A molding material set for sandwich panels, wherein a plurality of the prepregs are laminated via the papermaking sheets to form a plurality of skin layers, and the skin layers are configured to be provided on both sides of the core layer, respectively.
  • the present invention provides a technology that can improve the mechanical strength of sandwich panels.
  • FIG. 1 is a schematic cross-sectional view showing a sandwich panel according to an embodiment of the present invention.
  • FIG. 2 is a schematic cross-sectional view showing a first example of a method for manufacturing a sandwich panel according to the present embodiment.
  • the sandwich panel 100 includes a core layer 1 having a honeycomb structure and a skin layer 2 provided on each of both sides of the core layer 1.
  • the skin layer 2 is provided on one side (upper surface) of the core layer 1, and the skin layer 2 is also provided on the other side (lower surface).
  • the skin layer 2 is formed by laminating two prepregs 21 via a papermaking sheet 22 will be described, but this is not limited thereto.
  • the skin layer 2 may be formed by laminating three prepregs 21 via a papermaking sheet 22, or may be formed by laminating four or more prepregs.
  • the core layer 1 is a sheet-like plate member having a structure with high strength and light weight, and has a honeycomb structure.
  • the honeycomb structure is a known structure having a plurality of substantially regular hexagonal through holes penetrating from the upper surface to the lower surface.
  • the substrate constituting the honeycomb structure of the core layer 1 can be, for example, aramid fiber, paper, balsa wood, plastic, aluminum, titanium, glass, and alloys thereof molded into a honeycomb shape by known methods. Among these, from the standpoint of heat resistance and weight reduction, it is preferable that the substrate constituting the honeycomb structure of the core layer 1 contains aramid fiber.
  • the core layer 1 is preferably in the form of a woven fiber cloth as a substrate, which improves processability into a honeycomb structure and reduces the weight of the sandwich panel 100.
  • the core layer 1 is a fiber cloth, it is preferable to form a sheet-like member by impregnating a core layer substrate having a honeycomb structure with a binder resin. This further enhances the strength and light weight.
  • the binder resin is not particularly limited, and the same binder resin as that of the skin layer 2 described later can be used.
  • the thickness of the core layer 1 is not particularly limited, but may be, for example, 1 mm or more and 50 mm or less, 3 mm or more and 40 mm or less, or 5 mm or more and 30 mm or less.
  • each core cell in the core layer 1 is not particularly limited, but for example, one side can be 1 mm or more and 10 mm or less.
  • the surface area (upper surface, lower surface) of the core layer 1 is not limited, but may have the surface area of one sandwich panel 100, or may have the total surface area of a plurality of sandwich panels. This makes it possible to obtain a plurality of panels by cutting out one sandwich panel 100 into individual pieces, thereby improving productivity.
  • the surface area (upper surface, lower surface) of the core layer 1 may be large, for example, 1 m2 or more.
  • the core layer 1 may be subjected to various surface treatments on the inside and/or outside in order to improve corrosion resistance and heat resistance.
  • the skin layer 2 constitutes the outer surface of the sandwich panel 100 and is the outermost layer.
  • the skin layer 2 of this embodiment is formed by laminating two layers of prepreg 21 via a paper-made sheet 22. More specifically, the skin layer 2 is preferably obtained by hardening a binder resin in the prepreg 21 and firmly adhering it to the paper-made sheet 22. That is, the prepreg 21 contains a binder resin, and during the manufacturing process of the sandwich panel 100, a part of the binder resin penetrates into the paper-made sheet 22 and hardens, thereby improving the adhesion at the interface between the prepreg 21 and the paper-made sheet 22.
  • the prepreg 21 and the paper-made sheet 22 that constitute the skin layer 2 will be described in detail below.
  • prepregs 21 There are a plurality of prepregs 21, and one or two of the prepregs 21 are layers that form the outer surface of the skin layer 2 and can be the outermost layers.
  • the prepreg 21 is obtained by impregnating a sheet-like base material with a binder resin.
  • the sheet-like substrate may be one or more selected from aramid fiber, polyester fiber, polyphenylene sulfide fiber, carbon fiber, graphite fiber, glass fiber, and silicon carbide fiber. This can reduce the difference in linear expansion coefficient between the prepreg 21 and the core layer 1, thereby suppressing warping of the sandwich panel 100.
  • the binder resin may be one or more selected from the group consisting of phenolic resin, epoxy resin, unsaturated polyester resin, melamine resin, and polyurethane resin.
  • the thickness of the prepreg 21 is preferably 50 ⁇ m or more and 500 ⁇ m or less, more preferably 50 to 400 ⁇ m. Even more preferably, it is 50 to 300 ⁇ m.
  • the molded sheet 22 of the present embodiment is used to bond the plurality of prepregs 21 together.
  • the number of molded sheets 22 is appropriately set according to the number of prepregs 21.
  • the papermaking sheet 22 is preferably a sheet obtained by a papermaking method using a thermosetting resin and reinforcing short fibers as materials. That is, the reinforcing short fibers are dispersed in an excess of solvent and then papered, so that a large amount of the reinforcing short fibers are deposited in layers while being evenly entangled. As a result, it is possible to contain a high proportion of the reinforcing short fibers, and to improve the dispersibility and entanglement of the fibers, thereby dramatically improving the mechanical strength.
  • the proportion (volume %) of the thermosetting resin is preferably 10 volume % or more and 70 volume % or less, more preferably 30 volume % or more and 60 volume % or less, and even more preferably 40 volume % or more and 55 volume % or less, relative to the total volume of the paper sheet 22.
  • thermosetting resin by setting the proportion of the thermosetting resin to be equal to or less than the above upper limit, it is possible to prevent the thermosetting resin from being excessively interposed at the interface between the papermaking sheet 22 and the prepreg 21, thereby maintaining good adhesion between the two, and to increase the proportion of reinforcing short fibers, thereby further improving the mechanical strength.
  • thermosetting resin As the thermosetting resin, phenol resin, epoxy resin, melamine resin, polyurethane, unsaturated polyester resin, etc. can be used. As the thermosetting resin, one or a combination of two or more of the above specific examples can be used. Among them, phenol resin and epoxy resin are preferable as the thermosetting resin.
  • the phenolic resin examples include novolac-type phenolic resin, resol-type phenolic resin, and aryl alkylene-type phenolic resin.
  • the phenolic resin one of these may be used alone, or two or more types having different weight average molecular weights may be used in combination, or one or more types may be used in combination with their prepolymers.
  • it is preferable to use different types of phenolic resins in combination and it is more preferable to use, for example, a novolac-type phenolic resin and a resol-type phenolic resin in combination.
  • epoxy resins include biphenyl type epoxy resins; bisphenol type epoxy resins such as bisphenol A type epoxy resins, bisphenol F type epoxy resins, bisphenol AD type, and tetramethylbisphenol F type epoxy resins; stilbene type epoxy resins; novolac type epoxy resins such as phenol novolac type epoxy resins and cresol novolac type epoxy resins; multifunctional epoxy resins such as triphenyl type epoxy resins exemplified by triphenol methane type epoxy resins and alkyl modified triphenol methane type epoxy resins; phenol aralkyl type epoxy resins having a phenylene skeleton, naphthol aralkyl type epoxy resins having a phenylene skeleton, and phenol aralkyl type epoxy resins having a biphenylene skeleton.
  • bisphenol type epoxy resins such as bisphenol A type epoxy resins, bisphenol F type epoxy resins, bisphenol AD type, and tetramethylbisphenol F type epoxy resins
  • the epoxy resin examples include phenol aralkyl type epoxy resins such as aryl alkyl type epoxy resins (biphenyl aralkyl type epoxy resins) and naphthol aralkyl type epoxy resins having a biphenylene skeleton; naphthol type epoxy resins such as dihydroxynaphthalene type epoxy resins and epoxy resins obtained by glycidyl etherification of dihydroxynaphthalene dimers; triazine nucleus-containing epoxy resins such as triglycidyl isocyanurate and monoallyl diglycidyl isocyanurate; bridged cyclic hydrocarbon compound modified phenol type epoxy resins such as dicyclopentadiene modified phenol type epoxy resins; brominated type epoxy resins such as brominated bisphenol A type and brominated phenol novolac type; tris(hydroxyphenyl)methane type epoxy resins.
  • the epoxy resin one of these may be used alone, or two or more different types may be used
  • reinforcing short fibers include one or more types selected from metal fibers, carbon fibers, glass fibers, ceramic fibers, polyamide fibers, aramid fibers, polyimide fibers, polyvinyl alcohol fibers, polyester fibers, acrylic fibers, polyparaphenylene benzoxazole fibers, polyethylene fibers, polypropylene fibers, polyacrylonitrile fibers, and ethylene vinyl alcohol fibers.
  • metal fibers, carbon fibers, and glass fibers are preferred from the viewpoint of obtaining high mechanical strength.
  • the content of the reinforcing short fibers is preferably adjusted appropriately depending on the total content together with the content of any inorganic filler described below.
  • the total content of the reinforcing short fibers and inorganic filler is preferably 50 to 95 volume % of the entire paper sheet 22, more preferably 60 to 90 volume %, and even more preferably 70 to 80 volume %.
  • the papermaking sheet 22 of this embodiment may further contain other components such as thermoplastic resin, pulp fiber, inorganic filler, and coagulant depending on the purpose.
  • thermoplastic resin examples include ⁇ -olefin resins and copolymers using ⁇ -olefins, polyester resins, and polystyrene resins.
  • ⁇ -olefin resins and copolymers using ⁇ -olefins include polyethylene and polypropylene. Among them, polyethylene is preferable, and high density polyethylene (HDPE) is more preferable.
  • HDPE high density polyethylene
  • the polyester resin may be one or more selected from polyethylene terephthalate resin (PET), polybutylene terephthalate resin (PBT), polytrimethylene terephthalate resin (PTT), and the like.
  • the content of the thermoplastic resin in the entire sheet 22 is preferably 0.5 to 15% by volume, more preferably 1 to 10% by volume, and even more preferably 2 to 8% by volume.
  • the paper sheet 22 may contain pulp fibers in order to improve the handleability of the paper sheet 22 during the manufacturing process.
  • the pulp fiber is not particularly limited, and examples thereof include cellulose fibers such as linter pulp and wood pulp, natural fibers such as kenaf, jute, and bamboo, pulp-like fibers obtained by fibrillating organic fibers such as para-type wholly aromatic polyamide fibers and copolymers thereof, aromatic polyester fibers, polybenzazole fibers, meta-type aramid fibers and copolymers thereof, acrylic fibers, acrylonitrile fibers, polyimide fibers, and polyamide fibers.
  • the content of pulp fibers in the entire paper sheet 22 is preferably 0.5 to 15 volume %, more preferably 1 to 10 volume %, and even more preferably 2 to 8 volume %.
  • the inorganic filler is used to increase the mechanical strength.
  • the inorganic filler include one or more selected from calcium sulfate, barium sulfate, aluminum hydroxide, magnesium hydroxide, aluminum oxide (alumina), crystalline or fused silica, surface-treated silica, talc, kaolin, clay, mica, dolomite, wollastonite, glass fiber, carbon fiber, glass beads, zircon, and molybdenum compounds.
  • fused silica is preferred, clay is more preferred, and a mixture of these may be used.
  • the inorganic filler may be surface-treated.
  • the surface treatment may be performed with a coupling agent such as a silane coupling agent.
  • a coupling agent such as a silane coupling agent.
  • the coupling agent for example, primary aminosilanes such as ⁇ -aminopropyltriethoxysilane and ⁇ -aminopropyltrimethoxysilane can be used.
  • a coupling agent its content is not particularly limited, but is preferably 0.05 to 3 parts by weight, and more preferably 0.1 to 2 parts by weight, based on 100 parts by weight of the inorganic filler.
  • the paper sheet 22 according to the present embodiment may contain, for example, a flocculant, which allows any resin component and the reinforcing short fibers to be aggregated into a flock-like state.
  • the papermaking sheet 22 may further include, for example, papermaking agents, ion exchange agents, flocculants, conductivity imparting agents, flame retardants, flame retardant assistants, pigments, dyes, lubricants, release agents, compatibilizers, dispersants, crystal nucleating agents, plasticizers, heat stabilizers, antioxidants, coloring inhibitors, UV absorbers, flowability modifiers, foaming agents, antibacterial agents, vibration damping agents, deodorizing agents, sliding property modifiers, and antistatic agents.
  • papermaking agents ion exchange agents, flocculants, conductivity imparting agents, flame retardants, flame retardant assistants, pigments, dyes, lubricants, release agents, compatibilizers, dispersants, crystal nucleating agents, plasticizers, heat stabilizers, antioxidants, coloring inhibitors, UV absorbers, flowability modifiers, foaming agents, antibacterial agents, vibration damping agents, deodorizing agents, sliding property modifiers, and antistatic agents.
  • the thickness of the paper sheet 22 in this embodiment is preferably 5 ⁇ m or more and 150 ⁇ m or less, and more preferably 10 ⁇ m or more and 100 ⁇ m or less.
  • the thickness of the papermaking sheet 22 is preferably 5 ⁇ m or more and 150 ⁇ m or less, and more preferably 10 ⁇ m or more and 100 ⁇ m or less.
  • the thickness of the paper sheet 22 is obtained by observing the cross section of the sandwich panel 100, measuring the distance from the outer edge of the sheet-like base material of one prepreg 21 to the outer edge of the sheet-like base material of the other prepreg 21 multiple times, and calculating the average value.
  • the thickness of the sheet 22 can be adjusted by the amount of reinforcing short fibers contained in the sheet 22 .
  • the paper sheet 22 of this embodiment can be obtained by a known method, for example, the following method.
  • fibers such as reinforcing short fibers and optional components such as the above-mentioned resin components (excluding the coagulant) are dispersed in a dispersion medium to prepare a slurry.
  • the dispersion medium is not limited, and specific examples thereof include water; alcohols such as ethanol, 1-propanol, 1-butanol, and ethylene glycol; ketones such as acetone, methyl ethyl ketone, 2-heptanone, and cyclohexanone; esters such as ethyl acetate, butyl acetate, methyl acetoacetate, and methyl acetoacetate; and ethers such as tetrahydrofuran, isopropyl ether, dioxane, and furfural.
  • a flocculant is added to the dispersion liquid as necessary to form an aggregate.
  • the slurry is then placed in a container with a mesh on the bottom to separate the dispersion medium from the aggregates, leaving the aggregates on the mesh to obtain a flat sheet-shaped aggregate.
  • the thickness of the sheet can be adjusted by adjusting the amount of each of the materials in the material slurry or by preparing a new slurry and carrying out the separation process.
  • the dispersion medium is removed by dehydration pressing and drying, and if a thermosetting resin is contained, a papermaking sheet 22 in a B-stage state can be obtained.
  • the B-stage papermaking sheet 22 is later heated and pressurized together with the prepreg 21, and if it contains a thermosetting resin, it is completely cured and becomes the papermaking sheet 22.
  • the sandwich panel 100 of the present embodiment is lightweight, has excellent mechanical strength, and can have a good balance of various performances such as heat resistance and fire resistance, and is therefore suitable for use in various types of transportation equipment. In particular, it is suitable for use in aircraft panels that require high mechanical strength and heat resistance.
  • the sandwich panel 100 can be used for aircraft interiors such as toilets and partitions, and for aircraft fixtures such as wagon housings.
  • the first manufacturing method is a method for integrating a core layer 1, a prepreg 21, and a paper-made sheet 22 all at once.
  • the first manufacturing method includes the following steps: a step of laminating prepreg 21a, papermaking sheet 22, and prepreg 21b in this order on each surface of core layer 1, i.e., on the lower surface of core layer 1, and laminating prepreg 21b, papermaking sheet 22, and prepreg 21a in this order on the upper surface of core layer 1 to form skin layer 2; an integration step of integrating the core layer 1 and the skin layer 2 (the prepreg 21a, the papermaking sheet 22, and the prepreg 21b) by a heating and pressurizing treatment; including.
  • a heating and pressurizing treatment including.
  • the skin layer 2 is arranged by laminating the prepreg 21a, the papermaking sheet 22, and the prepreg 21b in this order on each surface of the core layer 1. Specifically, as shown in Fig. 2, the prepreg 21a, the papermaking sheet 22, and the prepreg 21b are laminated in this order on the lower surface of the core layer 1, and the prepreg 21b, the papermaking sheet 22, and the prepreg 21a are laminated in this order on the upper surface of the core layer 1, thereby forming the skin layer 2 on each of the upper and lower surfaces of the core layer 1.
  • the core layer 1 contains a thermosetting resin as a binder resin, it may be in a B-stage state before being cured, but typically a cured one is used.
  • the prepreg 21 and the papermaking sheet 22 contain a thermosetting resin as a binder resin
  • both are preferably in a B-stage state before being cured, and it is more preferable that at least the binder of the prepreg 21 is in a B-stage state. This allows the core layer 1, the prepreg 21, and the papermaking sheet 22 to be firmly integrated by a subsequent heating and pressurizing treatment.
  • the prepregs 21a and 21b are substantially the same.
  • a heat and pressure treatment As shown in FIG. 2, for example, a flat pressing plate 50 is used to sandwich the skin layer 2 arranged on the outermost surface from above and below, and a heat and pressure treatment is performed. At this time, a release film may be used between the skin layer 2 and the pressing plate 50. This makes it possible to smooth the surface of the skin layer 2 and makes it easier to peel the pressing plate 50 and the skin layer 2 after heating.
  • the heat treatment is preferably performed at 100 to 200°C, more preferably at 120 to 150°C, and the pressure treatment is preferably performed at 1 to 20 kgf/ m2 , more preferably at 5 to 15 kgf/ m2 .
  • the temperature and pressure of the heating and pressurizing treatment is adjusted appropriately depending on the temperature and pressure, but is preferably set to, for example, 30 to 90 minutes.
  • the heating and pressurizing process does not require gas replacement and can be carried out in the atmosphere. This improves productivity.
  • the pressing plate 50 may be a known one, for example a metal plate such as a stainless steel plate, a tin plate, an aluminum plate, or a magnesium plate.
  • the thickness of the pressing plate 50 is not particularly limited, but may be, for example, 0.5 mm to 10 mm, 0.8 mm to 5 mm, or 1.0 mm to 2.0 mm. By keeping the thickness within such a range, it is possible to achieve a balance between rigidity and thermal conductivity.
  • the sandwich panel 100 is obtained through the above steps.
  • the second manufacturing method includes a skin layer formation process in which prepreg 21a, papermaking sheet 22, and prepreg 21b are laminated in this order and integrated by heating and pressurizing to obtain skin layer 2, and the core layer 1 and skin layer 2 are integrated using a hot melt adhesive 3.
  • the differences from the first manufacturing method will be described below.
  • prepreg 21a, papermaking sheet 22, and prepreg 21b are laminated in this order, and integrated by heating and pressurizing.
  • prepreg 21 and papermaking sheet 22 contain a thermosetting resin as a binder resin, it is preferable that they are both in a B-stage state before being hardened. This allows prepreg 21 and papermaking sheet 22 to be firmly integrated by the subsequent heating and pressurizing treatment.
  • the heat treatment is preferably performed at 100 to 200°C, more preferably at 120 to 150°C, and the pressure treatment is preferably performed at 10 to 50 kgf/ m2 , more preferably at 20 to 45 kgf/ m2 .
  • the prepreg 21 and the papermaking sheet 22 can be firmly integrated.
  • the prepreg 21 and the papermaking sheet 22 can be appropriately integrated while suppressing damage to the prepreg 21 and the like.
  • the heating and pressurizing time is adjusted appropriately depending on the temperature and pressure, but is preferably set to, for example, 30 to 90 minutes.
  • the obtained skin layer 2 is placed on both sides of the core layer 1 with the hot melt adhesive 3 interposed therebetween.
  • the hot melt adhesive 3 contains, as a main component, a non-curable resin that becomes flowable at high temperatures and returns to a non-flowable state when cooled.
  • the hot melt adhesive 3 melts at or above a certain temperature and exhibits adhesive properties.
  • the non-curable resin may be one or more selected from the group consisting of thermoplastic resins including polyurethane, acrylonitrile, diene, acrylic, butadiene, polyamide, polyvinyl butyral, olefin, isoprene, butadiene, chloroprene, acrylonitrile, polyester, polyvinyl chloride, styrene, ethylene-vinyl acetate, fluorine, silicone, and copolymers thereof.
  • the hot melt adhesive contains polyamide as the main component.
  • the shape of the hot melt adhesive 3 is not particularly limited, but from the viewpoint of effectively suppressing the occurrence of voids, it is preferable that the adhesive be in the form of a nonwoven fabric or a film.
  • a heat and pressure treatment is performed using a pressing plate 50, etc., to integrate the core layer 1 and the skin layer 2, thereby obtaining the sandwich panel 100.
  • the sandwich panel molding material set of this embodiment is a set including a core layer 1 having a honeycomb structure, a plurality of prepregs 21, and a plurality of paper sheets 22. That is, a plurality of prepregs 21 are laminated via papermaking sheets 22 to form skin layers 2, and the skin layers 2 are provided on both sides of the core layer 1.
  • the above-mentioned sandwich panel 100 can be manufactured. In particular, by using the above-mentioned first manufacturing method, the sandwich panel 100 can be manufactured easily.
  • Paper Sheet A paper sheet was prepared using the following raw materials.
  • material ⁇ Reinforced short fibers: Carbon fiber, Toray “T800SC” fiber length 6mm
  • Thermosetting resin 1 resol type phenolic resin "PR-51723” manufactured by Sumitomo Bakelite Co., Ltd.
  • Thermosetting resin 2 novolac type phenolic resin "A-1087” manufactured by Sumitomo Bakelite Co., Ltd.
  • thermosetting resin 1 and thermosetting resin 2 were mixed in a mixer so that the two resins were 70% by mass and 30% by mass, respectively, and then the resulting mixture was kneaded in a biaxial roll at 80° C. for 5 minutes, and then cooled and pulverized to obtain a mixed resin having an average particle size of 50 ⁇ m.
  • 40 volume % reinforcing short fibers, 50 volume % of the mixed resin, 5 volume % of pulp fibers, and 5 volume % of high-density polyethylene were added to water as a dispersion medium, and the mixture was stirred for 20 minutes to obtain a slurry with a solid concentration of 0.15 weight %.
  • a poly(meth)acrylic acid ester emulsion prepared in advance (“Himoc DR-9300” manufactured by Himo Corporation) was added in an amount of 300 ppm relative to the solid content in the slurry, thereby flocculating the solid content in the slurry.
  • the slurry containing the aggregates was then filtered through a 30-mesh metal screen, and the sheet-like aggregates remaining on the screen were pressed at a pressure of 3 MPa to dehydrate them to a dehydration rate of 20%.
  • the dehydrated aggregates were dried at 70° C. for 3 hours to obtain a papermaking sheet (thickness 1 mm) in a B-stage state.
  • the dehydration rate was defined as the mass of water contained in the dehydrated sheet when the mass of water contained in the sheet-like aggregate before dehydration was taken as 100%.
  • Sandwich Panel Molding Material Set The following sandwich panel molding material set was prepared.
  • Core layer Aramid fiber, thickness 10 mm, HRH-10-1/8-3.0 (HEXCEL), area 1 m x 3 m - Papermaking sheet: The one prepared in (1) above was used.
  • - Prepreg A sheet-like prepreg (thickness 250 ⁇ m) obtained by impregnating glass fiber (#7781, manufactured by HEXCEL) with phenolic resin (resol type phenolic resin, "34370" manufactured by Durez) was used. The prepreg was in a B-stage state.
  • ⁇ Reference Example 1> Two prepregs were laminated on each surface of the core layer, and SUS plates (thickness 1.5 mm, Rz 1.0 ⁇ m) were pressed from the top and bottom surfaces, and the prepregs were cured to form skin layers by heating and pressurizing at 0.7 MPa, 127° C., and 60 minutes using a mechanical press, and the prepregs were hardened to form skin layers, and the core layer and the skin layers were integrated. The SUS plates on the top and bottom surfaces were then separated to obtain a sandwich panel in which the skin layer, core layer, and skin layer were laminated in this order.
  • Example 2 The prepreg, papermaking sheet and prepreg were arranged in that order, and SUS plates (thickness 1.5 mm, Rz 1.0 ⁇ m) were pressed against each other from above and below. The sheets were then heated and pressurized at 2.0 MPa, 137° C. and 60 minutes using a mechanical press to integrate them together and obtain a skin layer. Next, the obtained skin layers were placed on both sides of the core layer via a hot melt adhesive (main component polyamide), and SUS plates (thickness 1.5 mm, Rz 1.0 ⁇ m) were pressed against them from the top and bottom. Using a mechanical press, they were subjected to a heating and pressurizing treatment at 0.7 MPa, 127° C., and 60 minutes to laminate them together, thereby obtaining a sandwich panel.
  • SUS plates thinness 1.5 mm, Rz 1.0 ⁇ m

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  • Civil Engineering (AREA)
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  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Laminated Bodies (AREA)
PCT/JP2023/035891 2022-10-06 2023-10-02 サンドイッチパネル、およびサンドイッチパネルの製造方法 Ceased WO2024075684A1 (ja)

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JPH04262321A (ja) * 1991-02-15 1992-09-17 Kanegafuchi Chem Ind Co Ltd ガラスクロス強化電気用積層板の製造方法
JP2016520458A (ja) * 2013-06-06 2016-07-14 ル ストラティフィース 床又は壁装部品用の複合パネル及びそのようなパネルの製造方法
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JPH04262321A (ja) * 1991-02-15 1992-09-17 Kanegafuchi Chem Ind Co Ltd ガラスクロス強化電気用積層板の製造方法
JP2016520458A (ja) * 2013-06-06 2016-07-14 ル ストラティフィース 床又は壁装部品用の複合パネル及びそのようなパネルの製造方法
JP2016169381A (ja) * 2015-03-12 2016-09-23 東レ株式会社 エポキシ樹脂組成物、プリプレグおよび繊維強化複合材料
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CN118528612A (zh) * 2024-05-15 2024-08-23 比亚迪股份有限公司 纤维复合材料及其制备方法、防护结构件和车辆

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