WO2021010044A1 - 複合材の接着前処理方法 - Google Patents
複合材の接着前処理方法 Download PDFInfo
- Publication number
- WO2021010044A1 WO2021010044A1 PCT/JP2020/021956 JP2020021956W WO2021010044A1 WO 2021010044 A1 WO2021010044 A1 WO 2021010044A1 JP 2020021956 W JP2020021956 W JP 2020021956W WO 2021010044 A1 WO2021010044 A1 WO 2021010044A1
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- WO
- WIPO (PCT)
- Prior art keywords
- composite material
- prepreg
- release member
- resin
- treatment
- 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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- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/022—Mechanical pre-treatments, e.g. reshaping
- B29C66/0224—Mechanical pre-treatments, e.g. reshaping with removal of material
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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
- 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
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
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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
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0067—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other
- B29C37/0075—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other using release sheets
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/024—Thermal pre-treatments
- B29C66/0242—Heating, or preheating, e.g. drying
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/45—Joining of substantially the whole surface of the articles
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
- B29C66/72141—Fibres of continuous length
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7373—Joining soiled or oxidised materials
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7375—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined uncured, partially cured or fully cured
- B29C66/73751—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined uncured, partially cured or fully cured the to-be-joined area of at least one of the parts to be joined being uncured, i.e. non cross-linked, non vulcanized
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7375—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined uncured, partially cured or fully cured
- B29C66/73755—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined uncured, partially cured or fully cured the to-be-joined area of at least one of the parts to be joined being fully cured, i.e. fully cross-linked, fully vulcanized
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7394—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoset
- B29C66/73941—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoset characterised by the materials of both parts being thermosets
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
- C09J5/00—Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers
- C09J5/02—Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers involving pretreatment of the surfaces to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C59/00—Surface shaping of articles, e.g. embossing; Apparatus therefor
- B29C59/08—Surface shaping of articles, e.g. embossing; Apparatus therefor by flame treatment ; using hot gases
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C59/00—Surface shaping of articles, e.g. embossing; Apparatus therefor
- B29C59/10—Surface shaping of articles, e.g. embossing; Apparatus therefor by electric discharge treatment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C59/00—Surface shaping of articles, e.g. embossing; Apparatus therefor
- B29C59/14—Surface shaping of articles, e.g. embossing; Apparatus therefor by plasma treatment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C59/00—Surface shaping of articles, e.g. embossing; Apparatus therefor
- B29C59/16—Surface shaping of articles, e.g. embossing; Apparatus therefor by wave energy or particle radiation, e.g. infrared heating
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29C66/90—Measuring or controlling the joining process
- B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
- B29C66/919—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges
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- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/142—Laminating of sheets, panels or inserts, e.g. stiffeners, by wrapping in at least one outer layer, or inserting into a preformed pocket
Definitions
- peel ply a clean surface is formed using a peel ply cloth (hereinafter, peel ply).
- peel ply a peel ply cloth
- the quality may vary depending on the skill level of the worker, and the fibers may be damaged.
- a peel ply composed mainly of polyester fibers is used. Since polyester does not adhere well to the matrix resin of the prepreg, it usually dissociates between the peel ply and the prepreg when peeled off after curing.
- the polyester component may remain on the FRP surface, which may reduce the adhesiveness of the adhesive portion of the FRP panel.
- the following means are adopted as the bonding pretreatment method for the composite material of the present disclosure.
- the present disclosure is a pretreatment method for adhering a composite material to another member, wherein an absorbent body capable of absorbing a pollutant is attached to the surface of a prepreg laminate which is a precursor of the composite material.
- the prepreg laminate is covered with a packaging material from above the absorber, the inside of the packaging material is evacuated, the prepreg laminate is heated at a temperature lower than the curing temperature of the prepreg, and then the packaging material is removed.
- the absorber is peeled off, and a release member that does not transfer silicone and fluorine to the resin is attached to the surface of the prepreg laminate after the absorber is peeled off, and the prepreg laminate is cured to form a composite material.
- a method for pre-adhesion of a composite material for peeling the release member from the composite material before adhering the other members is provided.
- the absorber attached to the prepreg laminate can absorb the contaminants existing on the surface of the prepreg laminate.
- the contaminants are silicone, fluorine, oil, organic substances not derived from prepreg, etc. derived from the release sheet used in the production of prepreg.
- a mold release member that does not transfer silicone and fluorine to the resin is attached to the prepreg laminate. Therefore, the peel ply component is not left on the surface of the composite material. Since the release member does not transfer silicone and fluorine to the resin, silicone and fluorine do not remain on the surface of the composite material after peeling. According to the present disclosure, a cleaner surface is formed by reducing the amount of pollutants derived from the peel ply and the release member left on the surface of the composite material, so that when the adhesive portion is adhered to another member, the adhesive portion is formed. Quality can be stabilized by suppressing the decrease in strength.
- the surface of the composite material to which the release member is attached can be hydrophilized. ..
- the hydrophilization treatment is a process of imparting a polar functional group to the surface of the composite material to which the release member is attached by plasma treatment, corona treatment, ultraviolet ray treatment, flame treatment or treatment using a liquid. You can.
- oxygen radicals are generated on the surface of the composite material.
- Oxygen radicals react with C and H of surface stains (pollutants) such as oils and organic substances.
- contaminants are removed from the surface of the composite material as CO 2 or H 2 O.
- These functional groups hydrogen bond with the adhesive.
- a stronger adhesive force than the Van der Waals force is exhibited, and the adhesive strength of the adhesive portion is improved.
- the hydrophilization process can be automated, the surface can be cleaned stably regardless of the skill level of the operator compared to manual sanding.
- the surface of the composite material to which the release member is attached is subjected to a cleaning treatment, and the contaminants attached after the release member is peeled off are removed. It may be removed.
- a prepreg may be manufactured using a resin support member that does not transfer silicone and fluorine to a resin, and a plurality of the prepregs may be laminated to form the prepreg laminate.
- the release member is made of a material that does not contain fluorine and silicone. Thereby, the transfer of silicone and fluorine to the surface of the composite material can be prevented more reliably.
- the present disclosure is a pretreatment method for adhering a composite material to another member, in which a prepreg is manufactured using a resin support member that does not transfer silicone and fluorine to a resin, and a plurality of the prepregs are laminated to form a prepreg. A laminate is formed, and a release member that does not transfer silicone and fluorine to the resin is attached to the surface of the prepreg laminate, and then the prepreg is cured to form the composite material, and the other members are bonded to each other.
- a method for pre-adhesion of a composite material for peeling the mold release member from the composite material is provided.
- the quality of the bonded portion of the composite material can be stabilized by reducing the contamination of the prepreg surface and the surface of the composite material to make the surface suitable for bonding.
- FIG. 1 shows the procedure of the adhesion pretreatment method according to the present embodiment.
- (S1) a plurality of prepregs are laminated to form a prepreg laminate
- (S2) an absorber capable of absorbing contaminants is attached to the surface of the prepreg laminate
- (S3) the absorber
- the prepreg laminate is covered with a packaging material from above
- (S4) the inside of the packaging material is vacuumed
- the prepreg laminate is heated at a temperature lower than the curing temperature of the prepreg, and then (S5) the packaging material is removed and (S6).
- the surface to which the release member of the composite material has been attached is hydrophilized (s). Surface treatment) may be applied.
- Prepreg is a sheet-like material in which a reinforcing fiber sheet is impregnated with a matrix resin.
- the reinforcing fiber sheet is a sheet in which a plurality of reinforcing fiber bundles are aligned in one direction, a woven sheet of reinforcing fiber bundles, or a non-woven fabric sheet of reinforcing fiber bundles.
- Reinforcing fibers include carbon fibers, glass fibers, aramid fibers, silicon carbide fibers and the like.
- the pollutants are silicone, fluorine, oil, organic substances not derived from the prepreg material, etc. derived from the mold release member (release film, mold release agent, etc.) used in the production of the prepreg.
- the absorber is a substance that is used in the prepreg laminating process and can be peeled off after absorbing the resin. More specifically, the absorber is a cloth, a woven fabric, a non-woven fabric, a porous body, or the like. For example, a peel ply made of polyester resin can be used as the absorber.
- the packaging material is a member that can easily cover the prepreg laminate and seal it tightly.
- the material of the packaging material is nylon, PVC, polyolefin, fluororesin and the like.
- the material of the packaging material may be the same as that of the bag material, or may be different.
- the vacuuming and heating described in (S4) above are carried out under the condition that the prepreg laminate does not harden.
- a gelation temperature or lower is the temperature at which the storage elastic modulus and the loss elastic modulus obtained by viscoelasticity measurement intersect.
- the silicone which was left on the surface without curing the prepreg, was evacuated and heated at 70 ° C. for about 10 minutes. Fluorine or a resin containing them can be absorbed by the absorber and removed.
- the heating temperature is such that the absorber does not deteriorate.
- not cured and “before curing” mean that the curing reaction does not proceed, or that the curing reaction has progressed but the resin has not gelled.
- not contained means that the chemical composition of the resin does not contain silicone and fluorine, and that it is not intentionally added or applied to the release member. “Not included” allows inevitably mixed silicone and fluorine ( ⁇ 1%).
- Pollutants 2 may be present on the surface of the prepreg 1.
- the absorber 3 By attaching the absorber 3 to such a surface ((A) in FIG. 2) and evacuating, the contaminant 2 or the matrix resin containing the contaminant 2 permeates into the absorber 3 ((A) in FIG. 2). B)).
- the matrix resin of the prepreg 1 is softened, so that the contaminant 2 and the matrix resin can be efficiently impregnated into the absorber 3 ((B) in FIG. 2).
- the contaminant 2 is removed from the surface of the prepreg 1 ((C) in FIG. 2).
- the absorber 3 since the absorber 3 is peeled off before the matrix resin is cured, the component derived from the absorber 3 is not left on the surface of the prepreg 1.
- the release member does not transfer silicone and fluorine to the resin, silicone and fluorine are not left on the surface of the composite material even if they are peeled off after the prepreg is cured. According to the present embodiment, by preventing the components derived from the peel ply and the release member from being left in the composite material, it is possible to suppress the decrease in the adhesive strength of the composite material joint due to the components.
- OH hydroxyl groups
- COOH carboxyl groups
- Hydrophilization treatment can clean the surface more stably than sanding.
- Epoxy, acrylic, urethane, etc. can be used as the adhesive.
- a heat-curable epoxy type in the form of a sheet is preferable.
- the other member is an uncured prepreg laminate, it is laminated on the composite material via an adhesive and integrally cured together with the adhesive.
- the quality of the bonded portion of the composite material can be stabilized by reducing the contamination of the prepreg surface and the surface of the composite material to make the surface suitable for bonding.
- a prepreg is manufactured using a resin support member that does not transfer silicone and fluorine to a resin, and a plurality of the prepregs are laminated to form a prepreg laminate. Subsequent processing is carried out in the same manner as in the first embodiment.
- FIG. 3 is an example of an apparatus for manufacturing a prepreg.
- the prepreg manufacturing apparatus includes a creel 10 for supplying reinforcing fibers, a comb 11 for aligning the reinforcing fibers supplied from the creel 10 in one direction, and resin support members 12 and 13 coated with a matrix resin on one side.
- the nip rolls 16, 17, 18, the traction roll 19 the heating means 20 arranged between the nip roll 16 and the nip roll 17, and the nip roll 18 and the traction roll 19.
- the arranged cooling means 21 and the winding roll 22 for winding the resin support member 12 supplied from the winding roll 14 are provided.
- the reinforcing fibers 23 supplied from the creel 10 and aligned in one direction by the comb 11 are sandwiched and laminated by the resin support members 12 and 13 coated with the matrix resin on one side.
- the body 24 is formed.
- the resin support members 12 and 13 are supplied to the nip roll 16 so that the surface on the side coated with the matrix resin is located on the reinforcing fiber 23 side.
- the laminated body 24 sequentially passes through the nip rolls 16 to 18 and is heated by the heating means 20 to impregnate the reinforcing fibers 23 with the matrix resin and is cooled by the cooling means 21 to become the prepreg 25.
- the heating is performed under predetermined conditions in which the matrix resin is in a semi-cured state.
- the resin support member 12 is wound by the winding roll 22.
- the resin support member 13 attached to one side of the prepreg 25 is peeled off before laminating the prepreg.
- the resin support members 12 and 13 are a release paper, a release film, a release woven fabric, and the like.
- the resin support member that does not transfer silicone and fluorine to the resin is, for example, a polyolefin film, a polyolefin-coated paper, a non-transferable silicone, a non-transferable fluorine film, or the like.
- the resin support member is preferably made of a material that does not contain silicone and fluorine.
Landscapes
- Mechanical Engineering (AREA)
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Organic Chemistry (AREA)
- Laminated Bodies (AREA)
- Treatments Of Macromolecular Shaped Articles (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Reinforced Plastic Materials (AREA)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2021532721A JP7230207B2 (ja) | 2019-07-16 | 2020-06-03 | 複合材の接着前処理方法 |
| EP20840826.0A EP3984725B1 (en) | 2019-07-16 | 2020-06-03 | Bonding pretreatment method for composite material |
| US17/627,394 US12290993B2 (en) | 2019-07-16 | 2020-06-03 | Composite pre-bonding treatment method |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2019131066 | 2019-07-16 | ||
| JP2019-131066 | 2019-07-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2021010044A1 true WO2021010044A1 (ja) | 2021-01-21 |
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| Application Number | Title | Priority Date | Filing Date |
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| PCT/JP2020/021956 Ceased WO2021010044A1 (ja) | 2019-07-16 | 2020-06-03 | 複合材の接着前処理方法 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US12290993B2 (https=) |
| EP (1) | EP3984725B1 (https=) |
| JP (1) | JP7230207B2 (https=) |
| WO (1) | WO2021010044A1 (https=) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT202300012450A1 (it) * | 2023-06-16 | 2024-12-16 | Paolini S P A | Procedimento per la lavorazione di un laminato di un tessuto di una fibra di carbonio pre-impregnata |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10296765A (ja) * | 1997-04-24 | 1998-11-10 | Sanritsu Shoji Kk | 積層プレス成形用多層フィルムおよびそれを用いた積層プレス方法 |
| JP2014015567A (ja) * | 2012-07-10 | 2014-01-30 | Mitsubishi Rayon Co Ltd | プリプレグ |
| JP2015508346A (ja) | 2011-12-30 | 2015-03-19 | サイテク・テクノロジー・コーポレーシヨン | ピールプライ、このピールプライを用いてコンポジット構造を表面調製し、結合する方法 |
| JP2016501145A (ja) * | 2012-11-26 | 2016-01-18 | サイテク・インダストリーズ・インコーポレーテツド | 複合材料の結合 |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7842209B2 (en) * | 2006-02-21 | 2010-11-30 | The Boeing Company | Vacuum debulk and radiation cure method |
| JP5905704B2 (ja) | 2011-10-27 | 2016-04-20 | 丸善薬品産業株式会社 | 離型フィルムおよび離型フィルムの製造方法並びに離型コート剤 |
| US9254622B2 (en) | 2012-04-23 | 2016-02-09 | University Of Washington | Bond ply for adhesive bonding of composites and associated systems and methods |
| FR3025131B1 (fr) * | 2014-09-03 | 2016-09-16 | Airbus Group Sas | Piece composite thermodurcissable pre-polymerisee et procedes de realisation d'une telle piece |
| RU2758430C2 (ru) * | 2017-03-16 | 2021-10-28 | Зе Боинг Компани | Способы совместного соединения первого термореактивного композита и второго термореактивного композита с образованием отвержденной композитной детали |
-
2020
- 2020-06-03 JP JP2021532721A patent/JP7230207B2/ja active Active
- 2020-06-03 WO PCT/JP2020/021956 patent/WO2021010044A1/ja not_active Ceased
- 2020-06-03 EP EP20840826.0A patent/EP3984725B1/en active Active
- 2020-06-03 US US17/627,394 patent/US12290993B2/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10296765A (ja) * | 1997-04-24 | 1998-11-10 | Sanritsu Shoji Kk | 積層プレス成形用多層フィルムおよびそれを用いた積層プレス方法 |
| JP2015508346A (ja) | 2011-12-30 | 2015-03-19 | サイテク・テクノロジー・コーポレーシヨン | ピールプライ、このピールプライを用いてコンポジット構造を表面調製し、結合する方法 |
| JP2014015567A (ja) * | 2012-07-10 | 2014-01-30 | Mitsubishi Rayon Co Ltd | プリプレグ |
| JP2016501145A (ja) * | 2012-11-26 | 2016-01-18 | サイテク・インダストリーズ・インコーポレーテツド | 複合材料の結合 |
Also Published As
| Publication number | Publication date |
|---|---|
| JP7230207B2 (ja) | 2023-02-28 |
| EP3984725B1 (en) | 2023-10-18 |
| EP3984725A1 (en) | 2022-04-20 |
| EP3984725A4 (en) | 2022-08-17 |
| JPWO2021010044A1 (https=) | 2021-01-21 |
| US12290993B2 (en) | 2025-05-06 |
| US20220258433A1 (en) | 2022-08-18 |
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