EP2516137A1 - Procédé de fabrication de pièces moulées en thermoplastique renforcé par des fibres continues et pièces moulées de véhicules à moteur - Google Patents
Procédé de fabrication de pièces moulées en thermoplastique renforcé par des fibres continues et pièces moulées de véhicules à moteurInfo
- Publication number
- EP2516137A1 EP2516137A1 EP10803235A EP10803235A EP2516137A1 EP 2516137 A1 EP2516137 A1 EP 2516137A1 EP 10803235 A EP10803235 A EP 10803235A EP 10803235 A EP10803235 A EP 10803235A EP 2516137 A1 EP2516137 A1 EP 2516137A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- mats
- preform
- molding
- motor vehicle
- molded part
- 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.)
- Withdrawn
Links
- 229920001169 thermoplastic Polymers 0.000 title claims abstract description 15
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 10
- 238000000034 method Methods 0.000 claims abstract description 42
- 239000004416 thermosoftening plastic Substances 0.000 claims abstract description 13
- 238000010438 heat treatment Methods 0.000 claims abstract description 12
- 239000011159 matrix material Substances 0.000 claims abstract description 11
- 238000000151 deposition Methods 0.000 claims abstract description 6
- 238000012546 transfer Methods 0.000 claims abstract description 6
- 238000002844 melting Methods 0.000 claims abstract description 4
- 230000008018 melting Effects 0.000 claims abstract description 4
- 238000000465 moulding Methods 0.000 claims description 54
- 239000000835 fiber Substances 0.000 claims description 33
- 238000001746 injection moulding Methods 0.000 claims description 10
- 239000004033 plastic Substances 0.000 claims description 9
- 229920003023 plastic Polymers 0.000 claims description 9
- 238000010276 construction Methods 0.000 claims description 7
- 239000012815 thermoplastic material Substances 0.000 claims description 7
- 238000007596 consolidation process Methods 0.000 claims description 6
- 238000003466 welding Methods 0.000 claims description 5
- 238000003780 insertion Methods 0.000 claims description 4
- 230000037431 insertion Effects 0.000 claims description 4
- 230000002787 reinforcement Effects 0.000 claims description 4
- 238000007789 sealing Methods 0.000 claims description 4
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 229920002430 Fibre-reinforced plastic Polymers 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- 239000011151 fibre-reinforced plastic Substances 0.000 claims description 3
- 239000003365 glass fiber Substances 0.000 claims description 3
- 239000002557 mineral fiber Substances 0.000 claims description 3
- 230000005855 radiation Effects 0.000 claims description 3
- 239000002994 raw material Substances 0.000 claims description 3
- 239000012209 synthetic fiber Substances 0.000 claims description 3
- 229920002994 synthetic fiber Polymers 0.000 claims description 3
- 239000004760 aramid Substances 0.000 claims description 2
- 229920006231 aramid fiber Polymers 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 claims description 2
- 238000009958 sewing Methods 0.000 claims description 2
- 239000004753 textile Substances 0.000 claims description 2
- 238000002604 ultrasonography Methods 0.000 claims 1
- 238000002360 preparation method Methods 0.000 abstract 1
- 230000000750 progressive effect Effects 0.000 abstract 1
- 239000000463 material Substances 0.000 description 10
- 230000009969 flowable effect Effects 0.000 description 4
- 239000002657 fibrous material Substances 0.000 description 3
- MQFLXLMNOHHPTC-UHFFFAOYSA-N 1-isothiocyanato-9-(methylsulfinyl)nonane Chemical compound CS(=O)CCCCCCCCCN=C=S MQFLXLMNOHHPTC-UHFFFAOYSA-N 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 229920001296 polysiloxane Polymers 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 241001455273 Tetrapoda Species 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 239000011199 continuous fiber reinforced thermoplastic Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000011089 mechanical engineering Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000006228 supernatant Substances 0.000 description 1
- 238000003856 thermoforming Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Classifications
-
- 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
- B29C31/00—Handling, e.g. feeding of the material to be shaped, storage of plastics material before moulding; Automation, i.e. automated handling lines in plastics processing plants, e.g. using manipulators or robots
- B29C31/04—Feeding of the material to be moulded, e.g. into a mould cavity
- B29C31/08—Feeding of the material to be moulded, e.g. into a mould cavity of preforms to be moulded, e.g. tablets, fibre reinforced preforms, extruded ribbons, tubes or profiles; Manipulating means specially adapted for feeding preforms, e.g. supports conveyors
- B29C31/085—Feeding of the material to be moulded, e.g. into a mould cavity of preforms to be moulded, e.g. tablets, fibre reinforced preforms, extruded ribbons, tubes or profiles; Manipulating means specially adapted for feeding preforms, e.g. supports conveyors combined with positioning the preforms according to predetermined patterns, e.g. positioning extruded preforms on conveyors
-
- 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
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/081—Combinations of fibres of continuous or substantial length and short fibres
-
- 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
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
- B29C70/205—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres the structure being shaped to form a three-dimensional configuration
- B29C70/207—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres the structure being shaped to form a three-dimensional configuration arranged in parallel planes of fibres crossing at substantial angles
-
- 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
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- 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
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
-
- 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
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
-
- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
-
- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
-
- 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
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3005—Body finishings
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
Definitions
- the present invention relates to a process for the production of continuous fiber-reinforced molded parts from thermoplastics and a motor vehicle molding.
- a disadvantage of the prior art is that the pressing process due to necessary material supernatants has an increased material waste result. Furthermore, the 3D structure which arises only during the pressing process, and the associated forced orientation of the continuous fibers during the forming process, merely represents a compromise between the fiber orientation in the third dimension and the necessary flow paths of the material.
- a further disadvantage is that in order to achieve high degrees of deformation increased demand for flowable material, ie is necessary to thermoplastic matrix, which inevitably leads to an increased component weight. In addition, very high degrees of deformation can not be realized because otherwise fiber breaks occur within the continuous-fiber-reinforced molded part.
- the object underlying the present invention is to provide a process for the production of continuous fiber-reinforced molded parts from thermoplastic materials, which overcomes the disadvantages of the prior art.
- the present invention it is advantageously achieved by preforming the unidirectional fiber-reinforced mats into a three-dimensional preform such that in the subsequent consolidation step, the molding substantially does not have to undergo forming or flow processes. Therefore, advantageously less flowable material, ie less thermoplastic matrix is required, as is the case in the prior art. Due to the possibility of fiber orientation according to the invention in the third dimension is also achieved that the forces acting on the molded part produced by the molding according to the invention, and the resulting within the molding load paths can be optimally absorbed by the unidirectional fiber reinforcement.
- the unidirectional fiber reinforced mats are preferably cut from unidirectional films. Compared to the prior art, which discloses only band-shaped structures, the post-processing and the resulting material section can be reduced to a minimum by the targeted cutting of the mats.
- the fiber reinforcement of the mats is preferably formed by mineral fibers, in particular glass fibers, and / or carbon fibers, and / or aramid fibers, and / or polymeric fibers, and / or synthetic fibers and / or from fibers of renewable raw materials. It may be advantageous to perform the fixing of the position of the mats to each other by means of a welding process. Preferably, the position fixing of the mats takes place by an ultrasonic and / or heating element and / or laser welding process. The positional fixing of the blanks of the mats to one another during or after completion of the construction of the preform has the advantage that the preform has a significantly improved handleability.
- the mats are at least partially preheated prior to depositing on the workpiece carrier with the aim of increasing the flexibility of the mats. Due to the increased flexibility of the mats is advantageously achieved that they can adapt better when placed on the workpiece carrier of the three-dimensional rough contour. It is preferably provided to heat the workpiece carrier in order to be able to maintain the flexibility of the mats.
- the heating of the preform or the preheating of the mats is preferably carried out by convection heating and / or infrared radiation. Further preferably within a convection and / or infrared continuous furnace. The heating by infrared radiation or by convection heating represents for a component which already has a dreidimensionale coarse contour, an optimal method for uniform heating of the entire preform.
- a robot system For the transfer of the mats and / or for the introduction of the preform, a robot system can be used.
- a tetrapod system for example a so-called FlexPicker TM from ABB
- an alternative software-based camera monitoring and control unit image recognition
- the use of rotober systems achieves a favorable reduction in the duration of the process compared to a manual process.
- a high reproducibility of the method can be achieved through the use of robots. This is particularly advantageous with regard to a reproducible alignment of the mats to each other, and the associated fiber orientation within the molding.
- the setting of the homogeneous inner mold pressure is preferably carried out by an edge-side injection molding of a circumferential plastic welt in the injection molding process within the mold.
- the adjustment of the homogeneous inner mold pressure can also be done by additional insertion of GMT pieces (glass mat reinforced thermoplastic), more preferably by a shot-pot technique or by inserting sealing cords in the mold or by inserting a sealing film in the mold.
- GMT pieces glass mat reinforced thermoplastic
- the abovementioned possibilities can be used in any combination.
- a uniform consolidation of the preform or of the molded part is achieved by the homogeneous inner mold pressure.
- the edge region is also closed in an advantageous manner, so that no fiber material can escape from the edge region or there is no splicing of the fiber material used. Due to the edge gating only little additional material is needed, which in particular does not significantly increase the weight of the molding.
- complementary functions such as clips, recordings or attachment points can be formed.
- the workpiece carrier is moved on a conveying path, whereby the individual process steps take place along this conveying path.
- the workpiece carrier can thus be moved along a plurality of stations, in particular a plurality of robot stations, in order to further minimize the process time until the completion of the molding.
- the molding is preferably produced within a time interval of 20 to 120 seconds, more preferably within a time interval of 40 to 90 seconds, and even more preferably within a time interval of 55 to 65 seconds.
- the specified time intervals represent normal production times for molded parts of the automotive industry, so that the inventive method can also be integrated within the production line of a motor vehicle.
- part of the invention is a motor vehicle molding, wherein the molding is three-dimensionally constructed of at least two unidirectional fiber-reinforced mats in a manner such that the fiber orientation is matched to the attacking in the later use of the molding forces and thereby resulting within the molding load paths.
- the motor vehicle molding on a plastic piping.
- the Kunststoffke- is preferably integrally formed peripherally on the molding.
- the molding of the plastic bead on the motor vehicle molding by an injection molding process within an injection molding or injection molding process.
- the plastic piping is formed from a fiber-reinforced, more preferably short-fiber-reinforced plastic.
- the peripheral edge of the plastic piping preferably forms a closed structure. Particularly advantageous thus increases the structural rigidity of the molding.
- the molded part has a cavity with at least one closed cross section.
- the at least one closed cross section can in particular be produced by an expansion body arranged within the preform.
- the expansion body is pressurized by means of a fluid so that it forms the cavity within the motor vehicle molding in conjunction with the walls of the molding tool.
- an elastic bladder in particular a silicone bladder, is used as the expansion body. It is also conceivable to work with a lost core, which forms the cavity within the molding. Further alternatives are gas and / or water injection methods.
- the fiber reinforcement of the mats or of the molded part prefferably be formed by mineral fibers, in particular glass fibers and / or carbon fibers and / or arabin fibers and / or polymeric fibers and / or synthetic fibers and / or from fibers of renewable raw materials is or are.
- the motor vehicle molding is designed as a supporting structure of an opening of the vehicle closing flap or door, or as a structural part of the body. Further preferably, the molded part may be formed as part of the underbody of the vehicle or as a battery case or as a battery carrier. Furthermore, in the context of the invention is that the molding is used in an aircraft as a structural profile.
- a motor vehicle according to the invention includes any land, water or air vehicle.
- Fig. 2 is a detail view of a motor vehicle molding according to the invention with a
- Kunststoffkeder Fig. 3 shows another inventive automotive molding with a cavity
- FIG. 1 shows a system for implementing the method according to the invention for producing continuous fiber-reinforced molded parts 1 made of thermoplastic materials.
- cut-to-size, substantially flat, unidirectionally fiber-reinforced mats 2 with a thermoplastic matrix at least partially surrounding the fibers are provided on a plurality of conveyor units 3.
- the mats 2 are removed from the conveyor unit 3 from a magazine and provided at a predetermined position.
- the provision of the mats 2 via a rolling and / or cutting unit done (not shown here).
- the mats 2 are at least partially preheated before depositing on a workpiece carrier 5 with the aim of increasing the flexibility of the mats 2.
- the mats 2 are transferred to a workpiece carrier 5 which predetermines the rough contour 4 of the molded part 1.
- the workpiece carrier 5 itself is moved on a conveyor line 13.
- the cut mats 2 are deposited and continuously to a three-dimensional preform 6 constructed in such a way that the fiber orientation of the mats 2 on the forces acting in the subsequent use of the molding 1 forces, and the resulting within the molding 1 load paths, is tuned ,
- the transfer, the depositing and the construction of the preform 6 take over a plurality of robot stations or robot systems 14, which are arranged along the conveyor line 13. After completion of the construction of the preform 6, the mats 2 are fixed in position relative to each other.
- the position fixation by means of a laser welding system 7, wherein a laser optics (not shown in detail) is arranged at a further robot station 17.
- a positional fixation of the mats 2 to each other can take place by means of textile technology.
- the preform 6 is then heated in an infrared continuous furnace 8 above the melting temperature of the thermoplastic matrix of the preform 6.
- the heating can also take place within a convection continuous furnace or in a molding tool 10 itself.
- an injection molding unit 15 which provides correspondingly plasticized material, preferably a fiber-reinforced thermoplastic material, and injects it with pressure into the molding tool 10.
- the consolidated molded part 1 is also removed from the mold 10 by means of the robot station 9 and fed to a storage unit 16.
- FIG. 2 shows a detailed view of a motor vehicle molding 1 according to the invention with an integrally formed plastic piping 18.
- the molding 1 is built up in three dimensions from at least two unidirectionally fiber-reinforced mats 2 in a manner such that the fiber orientation is based on the later engagement of the molding 1 Forces, and thereby resulting within the molding 1 load paths, is tuned.
- the plastic piping 18 is peripherally molded on the molded part at the edge. The molding of the
- Kunststoffkeders 18 on the motor vehicle molding 1 is effected by a Anspritzvorgang within an injection molding process in the mold 10 of the motor vehicle molding 1.
- the Kunststoffkeder 1 is formed from a short fiber reinforced plastic.
- FIG. 3 shows a motor vehicle molding 1 according to the invention with a cavity 20 which has at least one closed cross-section.
- the at least one closed cross section is produced by an expansion body 19 arranged within the preform 6.
- the expansion body 19 is pressurized by means of a fluid (indicated by arrows), so that this forms in connection with the walls of the mold (not shown here) the cavity 20 within the motor vehicle molding 1.
- a fluid indicated by arrows
- an elastic bladder in particular a silicone bladder is used.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Robotics (AREA)
- Reinforced Plastic Materials (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
L'invention concerne un procédé de fabrication de pièces moulées (1) en thermoplastique renforcé par des fibres continues, ce procédé comportant les étapes suivantes: utilisation de mats (2) prédécoupés renforcés par des fibres unidirectionnelles et sensiblement plats, présentant une matrice thermoplastique entourant au moins partiellement les fibres, transfert des mats (2) dans un porte-pièces (5) définissant le contour grossier (4) de la pièce moulée (1), pose et élaboration continue des mats (2) sur le porte-pièces (5) pour obtenir une préforme (6) tridimensionnelle de façon que l'orientation des fibres des mats (2) soit adaptée aux forces agissant lors de l'utilisation ultérieure de la pièce moulée (1) et aux voies de charges en résultant à l'intérieur de la pièce moulée (1), fixation en position des mats (2) les uns par rapport aux autres pendant ou après l'élaboration de la préforme (6), réchauffement de la préforme (6) jusqu'à la température de fusion ou au-delà de la température de fusion de la matrice thermoplastique de la préforme (6), introduction de la préforme (6) tridimensionnelle dans un moule (10) conférant à la pièce moulée (1) son contour définitif, réglage d'une pression intérieure homogène du moule dans le but de consolider la préforme (6) tout en conservant l'orientation des fibres à l'intérieur de la préforme (6), démoulage de la préforme (6) consolidée hors du moule (10).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102009060027 | 2009-12-21 | ||
DE102010013131A DE102010013131A1 (de) | 2009-12-21 | 2010-03-26 | Verfahren zur Herstellung von endlosfaserverstärkten Formteilen aus thermoplastischem Kunststoff sowie Kraftfahrzeugformteil |
PCT/EP2010/007827 WO2011085792A1 (fr) | 2009-12-21 | 2010-12-21 | Procédé de fabrication de pièces moulées en thermoplastique renforcé par des fibres continues et pièces moulées de véhicules à moteur |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2516137A1 true EP2516137A1 (fr) | 2012-10-31 |
Family
ID=43939641
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP10803235A Withdrawn EP2516137A1 (fr) | 2009-12-21 | 2010-12-21 | Procédé de fabrication de pièces moulées en thermoplastique renforcé par des fibres continues et pièces moulées de véhicules à moteur |
Country Status (6)
Country | Link |
---|---|
US (1) | US20120269999A1 (fr) |
EP (1) | EP2516137A1 (fr) |
KR (1) | KR20120123350A (fr) |
CN (1) | CN102762360B (fr) |
DE (1) | DE102010013131A1 (fr) |
WO (1) | WO2011085792A1 (fr) |
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DE102011052515A1 (de) * | 2011-08-09 | 2013-02-14 | Rehau Ag + Co. | Batteriegehäuseteil für ein Batteriegehäuse einer Traktionsbatterie eines Elektrofahrzeugs und Verfahren zur Herstellung des Batteriegehäuseteils |
DE102011052513A1 (de) * | 2011-08-09 | 2013-02-14 | Rehau Ag + Co. | Batteriegehäuseteil zur Aufnahme einer Traktionsbatterie eines Elektrofahrzeugs und Verfahren zur Herstellung des Batteriegehäuseteils |
DE102011054650A1 (de) | 2011-10-20 | 2013-04-25 | Rehau Ag + Co. | Verfahren und Vorrichtung zum Aufbauen eines Vorformlings, Formteil, Computerprogrammprodukt und Speichermedium |
DE102011056033A1 (de) | 2011-12-05 | 2013-06-06 | Rehau Ag + Co. | Vorrichtung zum Greifen eines flächigen Halbzeuges, sowie Transportvorrichtung und Transportverfahren zur Ablage und Lagefixierung von flächigen Halbzeugen |
DE102011120986B4 (de) | 2011-12-13 | 2017-11-30 | Daimler Ag | Spritzgussverfahren zur Fertigung eines Faserverbund-Hohlprofilbauteils |
US9010839B2 (en) | 2012-10-24 | 2015-04-21 | Sabic Global Technologies B.V. | Vehicle side door structure and method of making and using the same |
DE102012112063A1 (de) * | 2012-12-11 | 2014-06-12 | Rehau Ag + Co. | Batteriegehäuseteil für ein Batteriegehäuse einer Traktionsbatterie eines Elektrofahrzeugs und Verfahren zur Herstellung eines derartigen Batteriegehäuseteils |
US8864216B2 (en) | 2013-01-18 | 2014-10-21 | Sabic Global Technologies B.V. | Reinforced body in white and method of making and using the same |
DE102013013497A1 (de) * | 2013-08-16 | 2015-02-19 | Leichtbau-Zentrum Sachsen Gmbh | Verfahren zur Herstellung eines Bauteils aus Organoblechen |
DE102013019146A1 (de) * | 2013-11-15 | 2015-05-21 | Audi Ag | Verfahren zur Herstellung eines aus mehreren Lagen bestehenden Fasergeleges, sowie Greifvorrichtung zur Durchführung des Verfahrens |
FR3016314B1 (fr) * | 2013-12-24 | 2016-04-15 | Daher Aerospace | Procede et dispositif pour l’estampage d’un flan composite a matrice thermoplastique non consolide |
CN104786522A (zh) * | 2014-01-17 | 2015-07-22 | 翁庆隆 | 连续式输送带微波固化的纤维复材成型方法及其装置 |
CN109131190B (zh) | 2014-06-16 | 2022-08-12 | 沙特基础工业全球技术有限公司 | 制备层压板的方法、吸能装置、吸能装置组合物及成形工具 |
HK1204842A2 (en) * | 2014-07-28 | 2015-12-04 | Beyon 3D Ltd | Method and system for fabrication of custom made molds and concrete architectural components |
DE102014219035A1 (de) * | 2014-09-22 | 2016-03-24 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur Herstellung von textilen Halbzeugen mittels Faserdirektablage |
DE102014220617A1 (de) * | 2014-10-10 | 2016-04-14 | Arburg Gmbh + Co Kg | Verfahren zur Weiterverarbeitung eines vorgefertigten Produktes sowie zugehöriges vorgefertigtes Produkt |
DE102014223121A1 (de) * | 2014-11-12 | 2016-05-12 | Branson Ultraschall Niederlassung Der Emerson Technologies Gmbh & Co. Ohg | Kunststoffschweißvorrichtung sowie dazugehöriges Kunststoffschweißverfahren |
DE102015002777A1 (de) * | 2015-03-06 | 2016-09-08 | Broetje-Automation Gmbh | Faserlegemaschine |
DE102015002775A1 (de) * | 2015-03-06 | 2016-09-08 | Brötje-Automation GmbH | System zur Fertigung von Faser-Verbundbauteilen |
DE102015204143A1 (de) * | 2015-03-09 | 2016-09-15 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur Herstellung von faserverstärkten Kunststoffbauteilen |
DE102015015619B4 (de) | 2015-12-03 | 2022-08-11 | Audi Ag | Verfahren zum Herstellen eines Kunststoffhohlprofils aus einem Kunststoffmaterial durch Spritzgießen |
FR3047196B1 (fr) * | 2016-02-02 | 2018-09-28 | Coriolis Group | Procede de realisation de preformes tridimensionnelles par formage de preformes initiales avec des voiles |
KR102524446B1 (ko) | 2016-12-30 | 2023-04-21 | 사빅 글로벌 테크놀러지스 비.브이. | 하이브리드 구조물 및 그 제조방법 |
US10493698B2 (en) * | 2017-07-20 | 2019-12-03 | GM Global Technology Operations LLC | Method of manufacturing a workpiece |
CN107498881A (zh) * | 2017-08-15 | 2017-12-22 | 成都新柯力化工科技有限公司 | 一种碳纤维增强塑料‑热塑性塑料激光热熔焊技术 |
GB2567684B (en) * | 2017-10-20 | 2022-03-30 | Mclaren Automotive Ltd | Composite manufacturing |
FR3081757B1 (fr) * | 2018-06-04 | 2021-12-03 | Setforge Soc Nouvelle | Procede pour fabriquer une piece en materiau composite |
WO2020077272A1 (fr) * | 2018-10-12 | 2020-04-16 | Arris Composites Inc. | Charges de préformes et accessoires associés |
JP7218596B2 (ja) | 2019-02-04 | 2023-02-07 | スズキ株式会社 | 繊維強化樹脂構造体の縁部構造 |
CN114007828A (zh) * | 2019-06-06 | 2022-02-01 | 阿里斯复合材料有限公司 | 预成型料装载物套筒及其序列化方法 |
EP3967480A1 (fr) * | 2020-09-15 | 2022-03-16 | The Boeing Company | Systèmes et procédés de formation de matériaux composites |
FR3114916A1 (fr) * | 2020-10-07 | 2022-04-08 | Valeo Systemes Thermiques | Composant pour un module de stockage d’énergie électrique |
GB2600118A (en) * | 2020-10-21 | 2022-04-27 | Mclaren Automotive Ltd | Tape deposition system |
DE102020128528A1 (de) | 2020-10-29 | 2022-05-05 | Kautex Textron Gmbh & Co. Kg | Batterieschale aufweisend ein Verstärkungsvlies, Herstellverfahren und Traktionsbatterie |
EP4000880A1 (fr) * | 2020-11-18 | 2022-05-25 | The Boeing Company | Fabrication de préformes composites incurvées pour aéronef via des lignes d'assemblage |
NL2027437B1 (en) * | 2021-01-26 | 2022-08-19 | Boeing Co | Fabrication of curved composite preforms for aircraft via assembly lines |
EP4001549A1 (fr) * | 2020-11-19 | 2022-05-25 | The Boeing Company | Système et procédé de fabrication en ligne continue de pièces composites |
KR102386521B1 (ko) * | 2021-10-27 | 2022-04-15 | 주식회사 서연이화 | 절곡부를 포함하는 복합소재 배터리 하우징 |
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CA1291934C (fr) * | 1988-08-10 | 1991-11-12 | Hisashi Masuda | Dispositif de collage de feuilles thermoplastiques entre elles |
FR2763547A1 (fr) * | 1997-05-23 | 1998-11-27 | Plastic Omnium Cie | Pare-chocs a absorbeur local |
FR2763546B1 (fr) * | 1998-04-07 | 1999-08-27 | Plastic Omnium Cie | Poutre de pare-chocs et son procede de realisation |
US6264462B1 (en) * | 1999-09-01 | 2001-07-24 | Robert M. Gallagher | Polymer transfer and deposition molding device |
DE60144380D1 (de) | 2000-07-28 | 2011-05-19 | Hypercar Inc | Verfahren und ausrüstung zur herstellung fortschrittlicher kompositstrukturen |
DE10324141B4 (de) * | 2003-05-26 | 2010-07-01 | Eurocopter Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundwerkstoff-Bauteils sowie Zwischenprodukt für ein solches Verfahren |
US8916010B2 (en) | 2007-12-07 | 2014-12-23 | The Boeing Company | Composite manufacturing method |
-
2010
- 2010-03-26 DE DE102010013131A patent/DE102010013131A1/de not_active Withdrawn
- 2010-12-21 EP EP10803235A patent/EP2516137A1/fr not_active Withdrawn
- 2010-12-21 CN CN201080058894.XA patent/CN102762360B/zh not_active Expired - Fee Related
- 2010-12-21 WO PCT/EP2010/007827 patent/WO2011085792A1/fr active Application Filing
- 2010-12-21 US US13/515,833 patent/US20120269999A1/en not_active Abandoned
- 2010-12-21 KR KR1020127019132A patent/KR20120123350A/ko not_active Application Discontinuation
Non-Patent Citations (1)
Title |
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See references of WO2011085792A1 * |
Also Published As
Publication number | Publication date |
---|---|
CN102762360A (zh) | 2012-10-31 |
DE102010013131A1 (de) | 2011-06-22 |
US20120269999A1 (en) | 2012-10-25 |
KR20120123350A (ko) | 2012-11-08 |
WO2011085792A1 (fr) | 2011-07-21 |
CN102762360B (zh) | 2015-04-01 |
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