Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
  • B29B17/00—Recovery of plastics or other constituents of waste material containing plastics
  • B29B17/04—Disintegrating plastics, e.g. by milling
  • B29B17/0412—Disintegrating plastics, e.g. by milling to large particles, e.g. beads, granules, flakes, slices
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
  • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
  • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
  • C08J5/0405—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres
  • C08J5/042—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres with carbon fibres
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
  • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
  • C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
  • C08J5/243—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
  • B29B17/00—Recovery of plastics or other constituents of waste material containing plastics
  • B29B17/0026—Recovery of plastics or other constituents of waste material containing plastics by agglomeration or compacting
  • B29B17/0042—Recovery of plastics or other constituents of waste material containing plastics by agglomeration or compacting for shaping parts, e.g. multilayered parts with at least one layer containing regenerated plastic
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
  • B29B7/00—Mixing; Kneading
  • B29B7/30—Mixing; Kneading continuous, with mechanical mixing or kneading devices
  • B29B7/58—Component parts, details or accessories; Auxiliary operations
  • B29B7/584—Component parts, details or accessories; Auxiliary operations for mixers with rollers, e.g. wedges, guides, pressing means, thermal conditioning
  • B29B7/588—Component parts, details or accessories; Auxiliary operations for mixers with rollers, e.g. wedges, guides, pressing means, thermal conditioning cutting devices, e.g. movable cutting devices
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
  • B29B9/00—Making granules
  • B29B9/12—Making granules characterised by structure or composition
  • B29B9/14—Making granules characterised by structure or composition fibre-reinforced
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
  • C08K3/00—Use of inorganic substances as compounding ingredients
  • C08K3/02—Elements
  • C08K3/04—Carbon
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
  • C08K7/00—Use of ingredients characterised by shape
  • C08K7/02—Fibres or whiskers
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
  • C08L101/00—Compositions of unspecified macromolecular compounds
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
  • C08L63/00—Compositions of epoxy resins; Compositions of derivatives of epoxy resins
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
  • B29B17/00—Recovery of plastics or other constituents of waste material containing plastics
  • B29B17/04—Disintegrating plastics, e.g. by milling
  • B29B2017/042—Mixing disintegrated particles or powders with other materials, e.g. with virgin materials
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
  • B29B17/00—Recovery of plastics or other constituents of waste material containing plastics
  • B29B17/04—Disintegrating plastics, e.g. by milling
  • B29B2017/0424—Specific disintegrating techniques; devices therefor
  • B29B2017/0476—Cutting or tearing members, e.g. spiked or toothed cylinders or intermeshing rollers
• • 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
  • B29C70/06—Fibrous reinforcements only
  • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
  • B29C70/12—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
  • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
  • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
  • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
  • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
  • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
  • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
  • B29K2105/0809—Fabrics
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
  • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
  • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
  • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
  • B29K2105/10—Cords, strands or rovings, e.g. oriented cords, strands or rovings
  • B29K2105/101—Oriented
  • B29K2105/105—Oriented uni directionally
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
  • B29K2307/00—Use of elements other than metals as reinforcement
  • B29K2307/04—Carbon
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
  • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
  • B29K2995/0037—Other properties
  • B29K2995/0094—Geometrical properties
  • B29K2995/0097—Thickness
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
  • C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
  • Y02P20/00—Technologies relating to chemical industry
  • Y02P20/141—Feedstock
  • Y02P20/143—Feedstock the feedstock being recycled material, e.g. plastics
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02W—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
  • Y02W30/00—Technologies for solid waste management
  • Y02W30/20—Waste processing or separation
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02W—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
  • Y02W30/00—Technologies for solid waste management
  • Y02W30/50—Reuse, recycling or recovery technologies
  • Y02W30/62—Plastics recycling; Rubber recycling

Definitions

• the present invention relates to the field of recycling composite materials, in particular composite materials comprising carbon fibers.
• Composite materials based on carbon fibers are used in many technical fields for their mechanical properties, in particular resistance and lightness. They are commonly used in particular in the aeronautical field, in the automotive industry, in boating, but also in the field of construction, energy, etc.
• Composite materials based on carbon fibers generally comprise carbon fibers included in a matrix.
• the carbon fibers are included in the matrix according to a given orientation, for example unidirectionally, or in the form of sheets of woven fibers.
• the matrix generally, it consists of a polymer or it essentially comprises a polymer.
• the matrix can also be called “adhesive”, or even “resin” (the matrix generally being a polymer).
• the matrix can be thermoplastic or thermosetting in nature. Adhesives of a similar nature can be used in the same way within the scope of the present invention.
• thermosetting polymers undergo a chemical reaction called crosslinking during the shaping of the composite material. This reaction generates chemical bonds and is irreversible. It is generally accepted that the most effective thermosetting polymers for forming a composite material based on carbon fibers are polyepoxides (known as “epoxies”).
• Thermoplastic polymers are polymers which, beyond a certain temperature, called “phase transition temperature”, below their thermal degradation temperature, become viscous and can thus be shaped. When the temperature drops below this phase transition temperature, the polymer hardens and regains its initial stiffness. This hardening is reversible, by heating the polymer again.
• the most common thermoplastic polymers are polyethylene (PE), poly(ethylene terephthalate) (PET) or polycaprolactam (PA-6).
• PEEK poly(phenylene ether-ether-ketone)
• PPS poly(phenylene sulfide)
• PEI polyetherimide
• composite materials based on carbon fibers being numerous and increasingly widespread, the question of the recycling of these materials arises.
• these composite materials are high-value materials (largely due to the fact that they contain carbon fibers), the recovery of which may prove to be economically relevant.
• Recycling may concern elements made of composite material at the end of their life or having suffered damage, elements manufactured but not meeting or no longer meeting certain standards required for the use for which they are intended (in particular in the aeronautical or space field) , or, more rarely, items not used on a certain date.
• Mechanical recycling consists, in principle, of splitting and grinding existing composite material parts to separate at least partially the fibers from the resin, so as to obtain more or less long fibers which can be reused as reinforcement in new new resin.
• the low fibrous particles resulting from the grinding which come in the form of powder, can be mixed with a resin during the formation of a new element in composite material.
• the shredded pieces of composite are used as filling elements or as reinforcement in molded parts, but are not really intended to replace virgin carbon fibers as used in the traditional processes for manufacturing composite elements (based on non-recycled materials).
• the powder obtained by grinding the composite materials to be recycled can be sieved in order to be sorted into several categories of particle sizes, without however this size having a significant influence on the mechanical properties of the element then formed in including these particles.
• Chemical recycling consists of chemically degrading the hardened resin of a composite material in order to recover carbon fibers present in this material.
• the recovered fibers are then generally aligned and/or spun to create a yarn from several thousand recovered fibers.
• the mechanical properties of parts formed from composite materials comprising these recycled fibers are much lower than those of composite materials comprising new, non-recycled carbon fibers.
• solvolysis under mild conditions, more moderate temperatures than in conventional solvolysis, below 200° C., are used.
• the process takes place at atmospheric pressure (ambient pressure), and milder solvents, such as acetone or N,N-dimethylformamide are used, as well as possibly catalysts such as hydrogen peroxide or peroxyacetic acid .
• Pre-treatment with acetic acid can also be used. That said, solvolysis under mild conditions has a fairly low production yield.
• solvents are used under supercritical conditions to exhibit improved diffusivity and increased solvating ability. It is a complex and expensive process.
• thermal recycling consists in principle of thermally degrading the resin of a composite material to recover the carbon fibers.
• the heat can be provided by a pyrolysis process, which generally consists of burning the resin in an oven, by a fluidized bed process which uses the combined action of a solvent and high temperature, and finally by micro- waves.
• the recovered fibers have highly degraded mechanical properties compared to new fibers.
• the recovered fibers are generally short, they must be aligned and spun to be reused in applications requiring correct mechanical characteristics. Otherwise, they are used in filling, as are for example the powders obtained in the mechanical recycling processes mentioned above.
• the present invention aims to provide recycled elements which can be incorporated into a matrix in order to prepare a part made of composite material, said recycled elements making it possible to overcome the drawbacks mentioned above.
• the invention relates to a chip made of composite material comprising carbon fibers in a hardened adhesive, said chip having a substantially constant thickness defined between two opposite parallel faces of the chip, each face comprising carbon fibers on the surface at least part not included in the cured adhesive.
• chip is meant a thin slice obtained from a composite material to be recycled comprising carbon fibers.
• the chip has carbon fibers at least partially embedded in a cured adhesive. At least a majority of the fibers of the chip extend substantially parallel to opposite faces of the chip.
• the thickness corresponds to the smallest dimension of the chip, which is small compared to its other dimensions (for example compared to its length and its width for a chip in a rectangular shape).
• the thickness of the chip is substantially constant, because the chip has two opposite (main) faces that are substantially parallel at all points.
• the chip is flat in the absence of constraints, it can be curved once included in a composite material part such as a panel. This possible curvature is possible due to the low thickness of the chip, which gives it a certain flexibility.
• the thickness of the chip measured perpendicular to the main faces of the chip, is constant at all points of the chip, or, at the very least, is perceived as constant by an observer.
• the thickness is “substantially” constant, that is to say that it is naturally perceived as constant.
• the thickness is substantially constant when the smallest thickness is not less than half of the greatest thickness measured on a chip, and preferably when the difference between the greatest thickness and the smallest thickness measured on one chip does not exceed 25%.
• the thickness is substantially constant when the difference between the smallest thickness and the largest thickness measured on the chip does not exceed 0.5 mm.
• the term “substantially” refers conventionally to the perception of this characteristic according to the system used for its measurement or its manufacture. If a characteristic is observed with the naked eye, the term “significantly” therefore refers to the perception that an observer has of this characteristic.
• An expression containing the term “substantially” should be interpreted as a technical characteristic produced within the tolerance range of its method of manufacture. In particular, the "substantially parallel" character between two elements can be understood to within 10° of angle. If the considered fiber is included in a fabric (typically taffetas, twills or satins), the direction of extension of the fiber is considered by neglecting the undulations of the fiber related to the weaving.
• the chip according to the invention advantageously has a small thickness (e) compared to its other dimensions.
• the chip thus being an essentially two-dimensional piece, of small thickness, its other dimensions typically correspond to the largest dimension (d) measurable at the surface of the chip and to the dimension measured perpendicularly, also at the surface of the chip.
• face of the chip we mean any of the faces of the chip, namely the lower face or the upper face of the chip. Each of these faces having a surface called the surface of the chip.
• the ratio (e)/(d) is between 0.05 and 0.0005, preferentially between 0.01 and 0.001 and even more preferentially between 0.005 and 0.001.
• the thickness of the chip is between 200 ⁇ m and 1 mm, preferably between 200 ⁇ m and 500 ⁇ m.
• the largest dimension (d) of the chip may advantageously be between 1 cm and 1 m, preferably between 5 cm and 50 cm, such as between 5 and 20 cm, more preferably between 7.5 and 15 cm or even more preferably between 8 and 12 cm or alternatively between 10 cm and 20 cm.
• the length of the chip is about 10 cm.
• X the length of the chip is about 10 cm.
• the chip may have a width of between 2 and 20 mm, preferably between 5 and 15 mm, even more preferably between 7 and 10 mm.
• the width of the chip is of the order of 9 mm.
• cured adhesive an adhesive which has undergone a chemical reaction called cross-linking or polymerization. This chemical reaction occurs before the formation of chips, we then speak of hardened adhesive during a hardening prior to the formation of the chip.
• the cured adhesive of the chip can advantageously be a thermosetting resin such as epoxy resins, cyanate ester and phenolic resins.
• Suitable epoxy resins include diglycidyl ethers of bisphenol A, diglycidyl ethers of bisphenol F, epoxy novolac resins and N-glycidyl ethers, glycidyl esters, aliphatic and cycloaliphatic glycidyl ethers, glycidyl ethers of aminophenols, ethers glycidyls of any substituted phenols and mixtures thereof.
• thermosetting polymers Also included are modified blends of the aforementioned thermosetting polymers.
• modified blend is meant a polymer modified, typically, by the addition of rubber or thermoplastic.
• the chip cured adhesive can also be a thermoplastic resin.
• thermoplastics we can distinguish between high-performance plastics, engineering plastics and standard plastics. Most of the thermoplastics used in composite materials are high performance plastics or engineering plastics. These plastics differ from standard plastics in particular by greater wear resistance and chemical resistance.
• Thermoplastics depending on their nature, can be hard in amorphous form or in crystalline form.
• thermoplastics commonly used in composite materials are polyetherimides (PEI), polyethersulfone (PES), and polysulfones (PSU).
• PEI polyetherimides
• PES polyethersulfone
• PSU polysulfones
• thermoplastics used in composite materials include polyamides (PA), poly(ethylene terephthalate), polyphthalamide (PPA), poly(phenylene sulfide) (PPS), and polyetheretherketone ( PEEK).
• PA polyamides
• PPA poly(ethylene terephthalate)
• PPA polyphthalamide
• PPS poly(phenylene sulfide)
• PEEK polyetheretherketone
• a carbon fiber is considered included in the cured adhesive if its entire surface is in contact with this adhesive, i.e. if the entire surface of the fiber is coated by the adhesive.
• the terms "included in” and “encapsulated by” are considered to be equivalent.
• the part of the carbon fiber not included in the cured adhesive constitutes a bare fiber.
• the chip according to the invention has a surface rate of bare fibers greater than or equal to 22%, the percentage being related to the total surface area of the face of the chip analyzed.
• the area ratio of bare fibers represents the area occupied by the carbon fibers not included in the cured adhesive compared to the total surface area of the face of the chip analyzed.
• the chip may have a surface rate of bare fibers greater than or equal to 22%, preferably comprised between 24% and 60%, such as a surface rate of bare fibers comprised between 26 and 50%.
• the surface rate of bare fibers is determined on a sample comprising carbon fibers or on a chip according to the invention, according to the measurement method comprising the following steps: a) horizontal arrangement of the sample or chip on the plate d a digital microscope, so as to obtain images where the orientation of the fibers is vertical, the microscope being oriented at an angle of 20 to 40°, preferably 30° with respect to the line normal to the plane of the sample or chip and a partial annular light of the LED type is applied so that the light beam reaches the surface of the fibers in a direction orthogonal to the axis of orientation of the fibers b) Selection of the pixels having a threshold value of level of gray greater than or equal to 50 c) Count of the selected pixels and obtaining the percentage of area occupied by the selected pixels with respect to the total area of the image, this percentage corresponding to the value of the surface rate of bare fibres.
• a ring light is a light that forms a circle around the microscope objective.
• the plane of the sample or the chip is materialized by a face of the sample or the chip.
• the circle of light can be divided into four quarters. We speak of “partial annular light” when only one of the quarters is used to illuminate the sample, thus defining a left, right, high or low annular light, depending on the location of the quarter with respect to the objective of the microscope.
• a ring light is distinguished from a coaxial light which illuminates the specimen from the center of the microscope objective.
• the partial annular light applied in step a) can be a right, left, top or bottom partial light.
• the partial annular light applied in step a) is a left or right partial annular light, even more preferably, the partial annular light is right.
• the microscope is then oriented at an angle of 20 to 40°, preferably 30° to the right with respect to the line normal to the plane of the chip.
• the surface rate of bare fibers is determined according to the method set out in example 2, point 1.
• one face has a roughness measured by a loss of mass greater than or equal to 0.008%, said loss of mass being measured by an abrasion test carried out on a linear abraser using an H18 abrasive rubber over 100 cycles.
• roughness of a chip we mean the state of the face of the chip which presents roughness.
• each face of the chip has a roughness.
• This roughness is determined according to the measurement method comprising the following steps: a) Initial weighing of the chip to determine its initial mass, b) Fixing the chip on the support of a linear abraser, c) Application of an H18 abrasive rubber for 100 abrasion cycles, with a cycle length of 10 cm and a cycle speed of 25 cycles/min, d) Final weighing of the chip to determine its final mass, e) Determination of the roughness by calculating the difference between the initial mass of the chip (obtained in step a)) and the final mass of the chip (obtained in step d)).
• the roughness is measured according to the method described in example 2.2.
• the chip has a roughness measured by a loss of mass of between 0.014% and 0.20%, and more preferentially, the loss of mass is between 0.014% and 0.15%.
• the chip according to the invention has a surface rate of bare fibers greater than or equal to 22% and a roughness measured by a loss of mass greater than or equal to 0.008%.
• the chip has a surface rate of bare fibers comprised between 24% and 60% and a mass loss comprised between 0.014% and 0.20%.
• the chip can have a surface rate of bare fibers comprised between 26% and 50%, and a mass loss comprised between 0.014% and 0.15%.
• said carbon fibers extend substantially parallel to said opposite faces of the chip.
• the carbon fibers included in the cured adhesive extend substantially parallel to said opposite faces of the chip.
• the carbon fibers not included in the cured adhesive can extend substantially parallel to said opposite faces of the chip.
• the carbon fibers are oriented in the same direction.
• Carbon fibers oriented in the same direction are also said to be unidirectional.
• the carbon fibers included in the cured adhesive are oriented in the same direction.
• Carbon fibers not included in the cured adhesive can be oriented in the same direction.
• the chip has a rectangular shape.
• each face of the chip according to the invention has a surface area of at least 1 cm 2 .
• Each face has a surface called the chip surface.
• the surface of the chip can be at least 3 cm 2 , 5 cm 2 , 10 cm 2 or 20 cm 2 , 100 cm 2 .
• the surface of the chip can therefore be between 1 and 100 cm 2 , between 2 and 25 cm 2 or between 5 and 15 cm 2 .
• the invention also relates to a process for manufacturing a chip according to the invention, said process comprising the following steps: providing a composite material comprising carbon fibers oriented in a substantially parallel manner in a cured adhesive; mechanical cutting of the composite material with a blade device, said cutting being carried out by positioning the carbon fibers parallel to the direction of advance of the blade of said blade device.
• the blade device may be a planer type system.
• a plane-type system corresponds to a cutting machine comprising a blade making it possible to separate thin slices of regular thickness from the surface of an element over which it is passed.
• the chip manufacturing process is more particularly described in Example 1.
• the invention also relates to the use of shavings as defined above in a part made of composite material.
• the chips according to the invention have the advantage of exhibiting improved adhesion with the matrix.
• the inventors have discovered that the chips having a surface rate of bare fibers greater than or equal to 22% and/or a roughness measured by a loss in mass greater than or equal to 0.008% as defined above; show improved adhesion with the matrix. Improved adhesion between the matrix and the carbon fibers leads to better chip cohesion, thus limiting chip degradation and consequently also limiting the degradation of a part made of composite material comprising the chips according to the invention.
• FIG. 1 represents, in the form of a graph, the flexural modulus of a panel comprising chips according to the invention organized in a unidirectional manner, the chips being obtained from composite material to be recycled, and that of a panel nine containing unidirectionally oriented carbon fibers.
• Example 1 Obtaining a chip according to the invention
• the formation of shavings is carried out from elements in composite material based on carbon fibers which are to be recycled.
• the chips are obtained by mechanical cutting of said elements.
• the cutting of the chips can be carried out using a cutting machine such as a blade device.
• the blade device may be a planer type system.
• a plane-type system corresponds to a cutting machine comprising a blade making it possible to separate thin slices of regular thickness from the surface of an element over which it is passed.
• the blade of the blade device When an element is cut to form chips, the blade of the blade device is positioned, in a conventional manner, so that the edge of the blade moves in a plane parallel to the direction of advance of the blade of said blade device , the advancing direction of the blade of the blade device being rectilinear.
• the “edge of the blade” also called “sharp edge” corresponds to the cutting edge of the blade which first penetrates the material to be cut.
• the material to be cut is positioned in the cutting machine according to the organization of the carbon fibers it contains.
• the fibers in the material to be cut are unidirectional, that is to say included in a matrix substantially parallel, in only one direction, then the fibers are positioned parallel to the direction of advancement of the blade of said blade device.
• the part will preferably be placed so that the weft or warp threads are substantially parallel to the direction of advance of the blade of said blade device.
• the fibers can also be arranged in a succession of layers, each layer comprising unidirectional fibers, but the layers having different fiber orientations. This is for example the case for so-called "four-way” materials, the layers of which may have successive relative orientations following: 0° (reference layer), 90°, 45°, -45°.
• a “four-way” material is a laminated material comprising several unidirectional carbon fiber layers, the layers being oriented in four different directions: 0°, 90°, 45°, -45°.
• the blade device can advantageously be adjusted so that its blade attacks the element between two layers of fibers, whether they are two layers of unidirectional fibers or two woven webs.
• the cutting plane will advantageously be maintained between the layers of fibers in order to preserve their integrity as much as possible.
• the blade device may comprise a micrometric shim system consisting of a superposition of elements arranged on either side of the material to be cut, said shim system being positioned on a reference plane and having a precision lower than the 1/ 10th of a millimeter.
• a wedge system makes it possible to control the zone of attack of the blade and thus to produce a more precise cut between the layers of fibres. This system thus makes it possible to control the thickness of the chips obtained while keeping the carbon fibers intact.
• Thin slices of composite material are thus obtained. These slices may in particular have a thickness of between 200 ⁇ m and 1 mm, preferably between 200 ⁇ m and 500 ⁇ m.
• the elements to be cut are cut to the desired length for the chips before being cut into slices by the cutting machine, so that the chips with the desired length are obtained directly from the cutting machine.
• the slices are then recut to obtain chips.
• they are cut transversely by any suitable cutting means, for example by sawing, in order to form fine rectangular shavings of regular length. Other shapes of shavings can of course be cut from the slices obtained.
• chips of 10 cm to 20 cm in length have been obtained and have made it possible to obtain very good results in terms of mechanical performance, as exemplified below.
• Greater lengths can also be implemented, such as around 50 cm, or even 1 m.
• the chips are therefore in the form of fine elements comprising carbon fibers included, at least in part, in a hardened resin.
• the chips are therefore in the form of substantially two-dimensional pieces (in that their thickness is very small compared to its other dimensions).
• the surface of the chips is advantageously at least 1 cm 2 , and preferably greater than 3 cm 2 , of the order of 10 cm 2 , or even greater, for example up to approximately 100 cm 2 .
• the carbon fibers are oriented in the cured resin of the chips. Preferably, they are substantially parallel, orthogonal to each other, and/or oriented at 45° to each other.
• the fibers of the chips having a substantially constant thickness, they have two opposite faces (between which the thickness is defined).
• the cutting of the chips is carried out in such a way as to keep the carbon fibers intact as much as possible.
• the cutting of the chips is carried out so that the fibers (in their majority, or even in their quasi totality or all) extend parallel to the opposite faces of the chips.
• the fibers thus extend in planes parallel to the general plane of extension of the chip, and can have a great length despite the low thickness of the chips.
• “Majority” means more than 50% in number.
• a composite rod is a cylinder obtained by pultrusion of a composite material.
• a composite sheet is distinguished from a composite plate by its thickness. Indeed the layer has a thickness of about 0.2 mm while the composite plate has a thickness of several millimeters.
• Partially consolidated composite plies are plies whose carbon fibers are integrated into a matrix or resin whose polymerization has started but is not complete. They therefore differ from composite layers comprising carbon fibers in an unpolymerized matrix because for the latter the polymerization has not begun.
• Materials 1 to 12 have all been sized to have the same width: 9 mm and the same length: 100 mm. To do this, materials 1 and 2 were dimensioned using a miter saw, material 3 was dimensioned using a paper cutter and materials 4 to 12 were dimensioned either via a paper cutter or using scissors.
• chips according to the invention are obtained by the process as described in Example 1.
• the materials 1-3 being composed of mostly unidirectional fibers, that is to say fibers oriented in a single direction, these are positioned parallel to the direction of advance of the blade of the mechanical cutting device at blade.
• Cutting as described above makes it possible to obtain chips of regular thickness, to keep the carbon fibers intact as much as possible and to obtain chips comprising longer fibers.
• the chips obtained from materials 1 to 4 have a thickness of between 0.3 and 0.5 mm.
• the surface rate of bare fibers is defined as the surface occupied by bare carbon fibers, i.e. by carbon fibers not included in or not coated with resin, compared to the total surface analyzed.
• the surface rate of bare fibers was determined for each of materials 1 to 12 using a VHX-970F digital microscope marketed by the Keyence brand. The latter is equipped with a VH-Z20T zoom lens capable of providing magnifications from x20 to x200. Image processing was performed with ImageJ software, version 2.1.0/1.53c.
• the principle of the measurement is to perform image processing with the microscope by selecting the brightest areas, corresponding theoretically to the carbon fibers, and extracting them to measure the surface they occupy.
• the protocol is as follows: a) Arrangement of the sample
• the sample or chip is placed horizontally on the microscope stage so that the orientation of the fibers on the images taken is vertical.
• the microscope is oriented at an angle of 30° with respect to the line normal to the plane of the sample or the chip (preferably on the right) and a partial ring light of the LED type (preferably a right partial ring light by relative to the microscope objective) is applied so that the light beam reaches the surface of the fibers in a direction orthogonal to the axis of the fibers.
• This configuration makes it possible on the one hand to avoid taking into account fibers which are coated in transparent resins and on the other hand to prevent the reflection of the resin zones.
• a selection of pixels is made by the software by performing the following steps in the “Image” > “Adjust” > “Color Threshold” tab. This option allows you to select the brightness level from which the pixels will be selected. For all the materials tested, the gray level was set at 50 (“Brightness” parameter). All areas whose gray level is greater than or equal to 50 have been selected. c) Results
• the chips obtained from materials 1 to 3 all have a surface rate of bare fibers greater than or equal to 22% (taking into account the standard deviation), which is not the case for comparative chips of materials 4 to 12.
• Cycle speed 25 cycles / minutes.
• the samples are weighed initially, then after 50 cycles, and finally after 100 cycles, in order to determine the total mass loss. For each material, at least three samples were tested and the average of the values obtained was calculated.
• the mass loss provides information on the surface condition of the chips. Indeed, the action of the abrasive rubber on a smooth surface will lead to a lower loss of mass compared to its action on a rough surface including asperities. This is explained by the fact that the action of the abrasive rubber will lead to the elimination of these surface roughnesses.
• Table 3 Abrasion test results It follows from Table 3 that the chips obtained from materials 1 to 3 have a roughness measured by a mass loss greater than or equal to 0.008% taking into account the standard deviation.
• Example 3 Mechanical properties of a composite material part
• the Applicant has carried out characterization tests, in terms of mechanical characteristics, of the materials obtained from chips according to the present invention.
• the shavings used in the tests presented here come from composite material elements comprising carbon fibers in a unidirectional arrangement included in an adhesive of the epoxy resin type.
• the elements used come from the aeronautical industry.
• the composite material had identical or similar characteristics to the “UD carbon plate” material, the characteristics of which are indicated in table 4 below.
• the chips are cut according to Example 1 from a starting composite material comprising carbon fibers in a unidirectional arrangement included in an adhesive of the epoxy resin type.
• the chips obtained are rectangular, and have a length I of 100 mm, a width b of 9 mm and a thickness of between 0.3 mm and 0.5 mm.
• the plates are produced according to the process as described below: coating of the shavings: the shavings are mixed with a liquid adhesive in order to coat them, with a view to molding them; molding of the chips in the form of flat panels; mold pressing; demoulding of the part; and hardening of the part.
• the mold is coated with a release agent and coated so as to create a layer of adhesive on the surface of the mould.
• the adhesive used is the ADEKIT H9011 system used according to the recommendations of its manufacturer.
• the chips are manually positioned in the mould.
• the ratio of chips to adhesive is, unless otherwise specified, 65/35 by mass in the finished plate.
• the molding is carried out under a press, by applying a force of 20 ton-force, and by controlling the temperature at around 70°C. After demoulding, the plates are kept for one week at room temperature.
• the plates thus obtained correspond to plates of composite material whose chips, and therefore the fibers, are positioned in a unidirectional arrangement.
• Table 4 compares the mechanical characteristics of the UD1 and UD2 plates with reference plates (carbon UD plate, wooden plate, aluminum plate).
• the “UD carbon plate” corresponds to a plate of a composite material based on new unidirectional carbon fibers.
• the “UD1 Plate” and “UD2 Plate” correspond to composite material plates in accordance with embodiments of the invention, obtained as described above, and whose chips, and therefore the fibers, are positioned according to an arrangement unidirectional. It is noteworthy that the flexural modulus and the breaking stress of the UD2 Plate (with 65% of chips by mass) is significantly higher than 50% of the values obtained for the reference Carbon UD Plate, i.e. a composite material based on of comparable new unidirectional fibers (from which the chips used can be extracted).
• the flexural modulus obtained, in the longitudinal direction is equal to 57% of the flexural modulus of the comparable new unidirectional material based on carbon fibers.
• the bending modulus of the UD2 Plate is equal to 63% of the bending modulus of the Plate Reference UD carbon.
• the chips according to the invention therefore make it possible to obtain a recycled material which has approximately 70% of the mechanical performance, in particular 70% of the flexural modulus, and (up to 75% to 80% of the performance at identical masses) of comparable materials based on of new fibers, with a simple manufacturing process, and having a low environmental impact compared to chemical or thermal recycling processes.
• FIG. 1 represents the flexural modulus of a panel made from chips according to the invention (obtained from a composite material to be recycled), the chips being organized in a unidirectional manner, and that of a panel obtained from new composite material containing unidirectionally oriented carbon fibers.
• the flexural modulus is plotted on the ordinate.
• the abscissa shows the angle at which the measurement is made.
• An angle of 0° corresponds to the direction of extension of the fibers or the chips, and 90° corresponds to the direction transverse to the fibers and/or the chips.
• the triangles correspond to the measurements made on a plate of a material comprising shavings according to the invention comprising unidirectional carbon fibers, said shavings being organized in a unidirectional manner.
• the flexural modulus of this plate measured in the direction of extension of the chips and the fibers they contain, is 47 GPa.
• the circles represent the theoretical bending moduli calculated for an equivalent plate, formed in a new composite material based on unidirectional carbon fibers whose bending modulus in the direction of the fibers it contains would be 47 GPa.

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• 2022
  • 2022-12-21 EP EP22843724.0A patent/EP4453069A1/fr active Pending
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