CN104512039A - Forming apparatus for manufacturing fiber-plastic composite structure products - Google Patents
Forming apparatus for manufacturing fiber-plastic composite structure products Download PDFInfo
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- CN104512039A CN104512039A CN201410642417.8A CN201410642417A CN104512039A CN 104512039 A CN104512039 A CN 104512039A CN 201410642417 A CN201410642417 A CN 201410642417A CN 104512039 A CN104512039 A CN 104512039A
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- CN
- China
- Prior art keywords
- storage rack
- composite structure
- underlying carrier
- conveying device
- reinforcing element
- Prior art date
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Classifications
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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
- B29C70/30—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
- B29C70/386—Automated tape laying [ATL]
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/18—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. compression moulding around inserts or for coating 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/20—Making multilayered or multicoloured articles
- B29C43/203—Making multilayered 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
- B29C69/00—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
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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
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/14—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
- B29C45/1418—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the inserts being deformed or preformed, e.g. by the injection pressure
- B29C2045/14237—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the inserts being deformed or preformed, e.g. by the injection pressure the inserts being deformed or preformed outside the mould or mould cavity
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/003—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor characterised by the choice 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
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/14—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
- B29C45/1418—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the inserts being deformed or preformed, e.g. by the injection pressure
- B29C45/14221—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the inserts being deformed or preformed, e.g. by the injection pressure by tools, e.g. cutting means
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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
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/14—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
- B29C45/14778—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the article consisting of a material with particular properties, e.g. porous, brittle
- B29C45/14786—Fibrous material or fibre containing material, e.g. fibre mats or fibre reinforced 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
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/14—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
- B29C45/14778—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the article consisting of a material with particular properties, e.g. porous, brittle
- B29C45/14811—Multilayered 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
- 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
- B29C65/08—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
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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
- B29C65/78—Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus
- B29C65/7841—Holding or clamping means for handling purposes
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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
- B29C65/78—Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus
- B29C65/7841—Holding or clamping means for handling purposes
- B29C65/7847—Holding or clamping means for handling purposes using vacuum to hold at least one 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
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/03—After-treatments in the joint area
- B29C66/034—Thermal after-treatments
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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
- B29C66/43—Joining a relatively small portion of the surface of said 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
- B29C66/40—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
- B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
- B29C66/472—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially flat
- B29C66/4722—Fixing strips to surfaces other than edge faces
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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
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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
- B29C66/73—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
- B29C66/7392—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 thermoplastic
- B29C66/73921—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 thermoplastic characterised by the materials of both parts being thermoplastics
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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
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/84—Specific machine types or machines suitable for specific applications
- B29C66/863—Robotised, e.g. mounted on a robot arm
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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
- B29C70/30—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
Abstract
The invention relates to a forming apparatus for manufacturing composite structure products, in particular to a forming apparatus for manufacturing fiber-plastic composite structure products. The forming apparatus comprises a first storage bracket for holding optimal fiber reinforced basic carriers; a conveying device taking the basic carriers out from the first storage bracket; a storage stand used for holding the basic carriers taken out by the conveying device; a second storage bracket holding reinforcing elements, wherein at least one reinforcing element can be placed on the basic carriers on the storage stand by the conveying device; a connecting device used for connecting the reinforcing elements and the basic carriers to form composite structure products; a heating device to which the composite structure products can be conveyed by the conveying device and in which the composite structure products can be heated to be above the melting temperature of one kind of plastic forming the composite structure products; a forming machine in which the heated composite structure products can be extruded and cured.
Description
Technical field
The present invention relates to a kind of former for the manufacture of composite structure product, especially fiber-plastic composite structure product.In addition, the present invention relates to a kind of method for the manufacture of this composite structure product.
Background technology
Fiber reinforced plastics is increasing as structural material meaning technically.Over 10 years, short fiber reinforced plastics is for the characteristic of adaptive plastics targetedly like this, makes described characteristic can meet its application target.Because improve continuously rigidity and the requirement reducing weight in recent years and different matrix systems can only improve its intensity by a small margin, so the mechanical property of reinforcing fibre or the length of reinforcing fibre are significant to these mechanical properties.This raising required causes strengthening strengthening development to continuous fiber from long fibre.For this fiber-plastic composite structure product, not only adopt thermosetting plastics, and adopt thermoplastic matrix system.The continuous fiber reinforced plastics with thermosetting plastics host material approximately from the sixties for aircraft component, and thermoplastic continuous fiber stiffener just just obtains day by day great meaning in recent years.
The advantage that generally such fiber compound structure product has is: look application target and surely by size cutting characteristic.Thisly to terminate from when selecting matrix and the different substrates that improves basic unit's coating tack to increase attached dose and when reinforcing fibre and coating thereof by size cutting.
Another factor promoting the development of continuous fiber reinforced plastics is light structures.Because the density of plastics and fiber is low, so likely develop a kind of fibrous composite with low-density high strength and rigidity.In addition, each fibrous material has outstanding mechanical property, and these mechanical property parts even exceed steel.Thus, fiber can be used to be combined with the material of matrix and prepare very light composite.Thus, such fibrous composite adopts recently very frequently in transport service, to cut operating costs on the one hand and to reduce CO on the other hand
2discharge.Enumerate civil aviation Boeing 787 as an example.50 % by weight adopt composite structure product there, make aircraft weight reduce about 20% thus.In addition, this composite structure product also for the manufacture of vehicle, also to reduce vehicle weight and also reduce CO thus here
2discharge.The example of vehicle structure is the project i of BMW.Above-mentioned two examples adopt thermosetting plastics matrix.For thermoplastic matrix system, processing technology is also in development.
GMT method (GMT=Glasmattenverstaerkte Thermoplaste, glass felt strengthens thermoplastic) describes one and produces process of semi-finished in a first step.This semi-finished product are made up of glass mat and molten polymer.In GMT semi-finished product are produced, apply molten polymer to glass mat and then heat on biobelt press, solidify, extrude these two parts and finally cool again.Then, for this processing technology, this semi-finished product again must to be heated in fusion temperature and then can be extruded in cold press.Because be not polymerized in this approach, so the cycle time that realization is shorter compared with reaction method.The maximum shortcoming of the method is adopted fluffy and disorderly fiber, wherein, there is not fiber preferred orientation and the mechanical property of fiber can not optimally be made full use of, can not carry out by size cutting thus in order to the product produced to raw material.
Further developing of GMT method is organic sheet.Do not use fluffy and disorderly felt when manufacturing organic sheet, adopt the continuous fiber being orientated reinforcement here.Organic sheet constructs layer by layer, wherein, between two plastic foils, loads reinforcement material.Then, comprise sandwich fusing, the under stress solidification of reinforcement material and plastic foil by this and and cool in biobelt press.Then, also organic sheet is cut with desired length.Reinforcing fibre and fiber angles can be changed targetedly in theory thus, to manufacture the semi-finished product by size cutting thus.But because thisly depend on component respectively by size cutting, so when layer angle is between 0 ° and 90 °, fiber leftover (Faserverschnitt) improves, so half-finished manufacturing cost and therefore also improving price.Another shortcoming of the method is, the thickness of local is beated and only had the classification roll-in by transverse to production mode reform just can realize.More processing technology is the same with GMT method.Semi-finished product are heated to more than fusion temperature again and then can by shaping or functionalization.
CH 704 406 A1 illustrates a kind of method for the manufacture of preformed product.Implement flexible program according to the one of the method and be provided with three phases, the base substrate that the namely shearing of semi-finished product volume, fiber are strengthened deposit and finally to laying and the welding of preformed member.The subregion of production process of only touching upon in this article and not touching upon to the manufacture of the composite structure product finally made.
DE 10 2,010 050 740 A1 illustrates a kind of method and apparatus for the manufacture of aircraft structural component.In this article, do not describe freight house and also just describe a part of region of production process in detail.
EP 1 844 914 A1 is like this equally, and it illustrates the method for manufacturing based on " preformed " three-dimensional of LEDs.
Another solution of producing for semi-finished product is provided in document WO 2009/042225 and WO 2013/016487.As the semi-finished product that raw material uses fiber to strengthen.The strap that these semi-finished product are strengthened as fiber exists and is called hereinafter " band ".In processing technology, this band launches, is cut into certain length and places on the mold surface with limiting from volume.Fix this belt when being put on the mold surface by band and then welded.This die surface at this, various different fiber angles can be realized, because can rotate around z axis.Thus, can manufacture the semi-finished product by size cutting by this production process, wherein, not only thickness is beated but also various different fiber angles is possible.But this production process is so time taking, make these semi-finished product must off-line manufacture and can not being directly coupled in further processing.Thus, this method is only just useful to the small lot batch manufacture of the fiber and Rotating fields with top complexity.
For production in enormous quantities, all these techniques are all inapplicable, this is because semi-finished product production determines cycle time and the industrial preferably online solution of another aspect on the one hand.If adopt wider band, to reduce the quantity of each tape and also to shorten half-finished manufacturing time thus, so leftover pieces region also automatically becomes comparatively large and makes semi-finished product cost increase thus and economy reduction.Therefore, forming wider band only has just both economical under certain condition for production process.
Summary of the invention
Therefore, the object of the invention is to, realize a kind of relative to the former of prior art improvement and a kind of manufacture method of improvement.Particularly the manufacture of composite structure product should be quick as far as possible, simple, with low cost and can produce in enormous quantities.
This is realized by the former with the feature of claim 1.Therefore, this former comprises: the first storage rack wherein depositing the underlying carrier that optimum fiber is strengthened; Conveying device, for taking out underlying carrier from the first storage rack; It can be placed the storage rack of the underlying carrier taken out by conveying device; Wherein deposit the second storage rack of reinforcing element, wherein, at least one reinforcing element can be put on the underlying carrier that is on storage rack by conveying device; Engagement device, for connecting into composite structure product by reinforcing element and underlying carrier; Heater, composite structure product can be transported in this heater by conveying device, and in this heater, composite structure product can be heated to more than the fusion temperature of the plastics of common this composite structure product of formation; And forming machine, can extrude in this forming machine and solidify the composite structure product after heating.Thus, can reduce half-finished cost, its mode is, in a production process and an equipment, use standard intermediate as raw material, and it can be combined in that production line that final processing occurs wisely.Thus can by local carry out product specifically adaptive mechanical property by size cutting.Therefore, this production process is also applicable to produce in enormous quantities, this is because as described above, by adopting local strengthening to reduce half-finished cost targetedly, because these semi-finished product are no longer only strengthened on whole on the position needed.
In order to underlying carrier and reinforcing element (band) can be placed as far as possible exactly, be preferably provided with positioner and be positioned at underlying carrier for being positioned on storage rack and/or by reinforcing element by underlying carrier.At this, implementing flexible program according to first can specify: positioner has push unit and is configured at least one backstop on storage rack, wherein, underlying carrier and/or reinforcing element can be made to move until backstop is in theoretical position by push unit.Conveying device also can bear the task of push unit.In contrast, flexible program regulation is implemented: this positioner has at least one position sensor and control program according to alternative second, analyzing and processing can be carried out to the physical location of the underlying carrier detected by described at least one position sensor and/or the relative storage rack of reinforcing element via this control program and by store in itself and control program or the theoretical position that calculates compare, wherein, control impuls can be transmitted by control program to conveying device, and underlying carrier and/or reinforcing element can be made to move in theoretical position by conveying device.Such as the camera of pressure sensor, limit switches, laser instrument, weight sensor and/or sensing storage rack can work as position sensor.Particularly preferably camera control is carried out to the process of putting down, wherein, pattern analysis process is carried out to the photo of this camera and by least one value transmit to the control program of whole former, preferably closed loop or opened loop control unit.Then, can to putting down reinforcing element correction according to this analyzing and processing.In addition, these photo determination qualitative characters can also be passed through.At this, camera can be settled on a conveyor.But this camera is preferably arranged in the region of storage rack still.Theoretical position can be tried to achieve by calculating and check in principle thus, or mechanically realizes.Certainly, it is also possible for mixing flexible program.
Storage rack itself can be on the optional position of former.Importantly, this storage rack can be reached well by conveying device.This storage rack such as can be integrated in the first storage rack for this reason.But this storage rack also can be a part for heater.But preferably specify: storage rack is configured on lodging bench separately.
Where described storage rack is indifferent if being arranged on, but preferably can specify: storage rack has the evacuated panel for reliably positioningly keeping underlying carrier.In addition, the turntable with at least one rotation can be set, this turntable can fix storage rack, or this turntable forms storage rack.
In principle, reinforcing element and underlying carrier connection or weld and can such as be undertaken by bonding or similar fashion.But this engagement device preferably has supersonic generator, to heat the face against each other of the parts that these two need connect thus and to make it softening, thus make they after cooling material be connected to each other in locking manner.In order to as far as possible effectively design whole flow process, can specify at this: engagement device is installed on a conveyor.
Reinforcing element is preferably configured as reinforcing band.This band is preferably based on polyamide 6 and manufactures with one-way glass fiber intensifier.Underlying carrier is preferably the thermoplastic semifinished products that fiber is strengthened.Optionally, underlying carrier also can be replaced by metal or other carrier materials.Thus, composite structure product is made to be made up of underlying carrier on the one hand and to be made up of reinforcing element on the other hand in principle.At this, at least one composition in described composite structure product composition should have plastic fraction, and thus, described composite structure product heats by utilizing engagement device or utilizes heating devices heat and can be out of shape relatively easily.Preferably these two composite structure product compositions at least have plastic fraction.These two composite structure product parts preferably have fiber intensifier.
Also can propose: described heater can form engagement device in principle for this reason.Thus, these two devices need not be configured to the station separated of former, on the one hand reinforcing element can be engaged with underlying carrier by heater on the contrary and another aspect can also while or the heating carried out successively whole composite structure product.Otherwise, engagement device also definitely only can be utilized to realize heat treatment, make also to heat whole composite structure product, thus engagement device forms heater in such a scenario simultaneously simultaneously.But the station that the function that engagement device and heater preferably form former is separated, wherein, they definitely can be closer to each other or can be integrated on a common station in position.
Conveying device itself can any configuration, such as, be configured to the form of conveyer belt.But preferably define, conveying device is manipulation robot.In order to underlying carrier and reinforcing element can be operated, in this conveying device or manipulation robot, preferably there is grasping element (such as adhere to grasping device or hold pincers).Certainly, former can also comprise multiple parallel connection or series connection manipulation robot.
In addition, described former can also comprise shear, and wherein, reinforcing element can carry out cutting by this shear before being placed on underlying carrier.Underlying carrier itself also can obtain cutting thus.
In principle, different system independent of each other is for controlling each station of former.But make logical in whole former to ensure and carry out automatically, closed loop for closed loop or opened loop control former or opened loop control unit can be set, wherein, at least conveying device, engagement device, heater and forming machine come closed loop or opened loop control by such closed loop or opened loop control unit jointly.The closed loop that all stations in this former are preferably unique with this or opened loop control unit are connected.The control program of positioner is also preferably a part for this closed loop or opened loop control unit.Particularly preferably, on forming machine, the original operating unit existed preferably plays central closed loop or opened loop control unit.
Described forming machine can be configured to the form of press or injector.But forming machine is preferably injection (mo(u)lding) machine.
Also be achieved by the method for the feature with claim 16 according to object of the present invention.Be provided with following steps thus: from the first storage rack depositing the underlying carrier that optimum fiber is strengthened, take out underlying carrier by conveying device; The underlying carrier taken out by conveying device is placed on storage rack; From the second storage rack depositing reinforcing element, reinforcing element is taken out by conveying device; This reinforcing element is placed on the underlying carrier be on storage rack; By engagement device, reinforcing element and underlying carrier are connected into composite structure product; This composite structure product is transported in heater; Composite structure product is heated to more than the fusion temperature of the plastics of common this composite structure product of formation in heater; And extruding and the composite structure product after solidifying heating in forming machine.In principle, each method step can also be undertaken by another order depending on possibility.The method is preferably carried out with the sequence of steps provided in claim 16 exactly, wherein, definitely some steps partially or even wholly can also be intersected in time and carry out.The functionalization to composite structure product can also be carried out in this forming machine as end step.In addition, during underlying carrier and/or reinforcing element are placed on storage rack theoretical position preferably by positioner or move in theoretical position.
Accompanying drawing explanation
To illustrate by accompanying drawing referring to the embodiment shown in accompanying drawing and other details of the present invention and advantage are elaborated.In accompanying drawing:
Fig. 1 schematically shows the whole former with each station;
Fig. 2 illustrates another schematic diagram of each station;
Fig. 3 to 7 schematically shows each method step;
Fig. 8 schematically shows fixing underlying carrier on a spinstand;
Fig. 9 schematically shows the detail view of conveying device together with engagement device;
Figure 10 and 11 illustrates two kinds of flexible programs of the separator for reinforcing element.
Detailed description of the invention
Fig. 1 schematically shows the former 1 with different station.As the starting point for the manufacture of composite structure product 2, optimum fiber-plastic composite structure product, the first storage rack 3 deposits a large amount of underlying carrier 4.Second storage rack 7 is deposited reinforcing element 8 (reinforcing band).In addition, be provided with storage rack 6, this storage rack is configured on lodging bench 19 separately, and wherein, underlying carrier 4 and/or reinforcing element 8 may also be reduced in advance in shear 26.Be provided with camera 18 still at lodging bench place, it forms a part for positioner 12.In addition, conveying device 5 is configured to the form of manipulation robot 23.The grasping element 24 of this manipulation robot 23 maintains composite structure product, and this composite structure product comprises underlying carrier 4 and reinforcing element 8, and described underlying carrier is connected by engagement device 9 with reinforcing element.As next step, heater 10 is shown, being forming machine 11 then, is injection (mo(u)lding) machine in particular situations.This machine comprises the injecting mechanism 29 for injected plastic liquation and the mold closing unit 30 comprised on the other hand with molding clamp plate and crossbeam on the one hand.In addition, this forming machine 11 is mounted with operating unit, this operating unit is configured for closed loop or the opened loop control unit 25 of whole former 1.This closed loop or opened loop control unit 25 have screen 27 and the operating space 28 with button.In addition, for the control program 16 of positioner 12 be the part of this closed loop or opened loop control unit 25.This closed loop or opened loop control unit are connected with each station of former via holding wire 39.
Fig. 2 schematically shows top view, and underlying carrier 4 and reinforcing element 8 are in common storage rack 3 and 7.Conveying device 5 just takes out a underlying carrier via grasping element 24.Can be clear that positioner 12 under this figure, this positioner has two exposure sources 32 and has camera 18 as position sensor 15.Physical location P that is that check underlying carrier 4 by camera 18 or reinforcing element 8
isTand by the theoretical position P storing in itself and control program 16 and calculate
sOLLcompare.When there is deviation, transmit corresponding control signal 17 by control program 16 to conveying device 5, it carries out position correction immediately.Optionally, positioner 12 also can purely mechanically construct.For this reason, in fig. 2 by the backstop 14 that dotted line draws push unit 13 and is arranged on storage rack 6.In addition, can see the mold half 31 forming mould in this Fig. 2, these mold halfs clamp in the region of the mold closing unit 30 of forming machine 11.In addition, the heater 10 for thermoplastic member is shown from upside.
Fig. 3 to 7 illustrates method flow intuitively.In figure 3, conveying device 5 is just taking out the underlying carrier 4 that fiber is strengthened from the first storage rack 3, and this underlying carrier is placed on the storage rack 6 of lodging bench 19 with being limited.After this, from the second storage rack 7, take out reinforcing element 8 according to Fig. 4 conveying device 5 and put it on underlying carrier 4.Then, according to Fig. 5 by engagement device 9 by the ultrasonic wave of supersonic generator 22 make underlying carrier 4 and reinforcing element 8 at least one times material be interconnected in locking manner.The inline process by size cutting (Massschneiderung) can arbitrarily repeatedly, until underlying carrier 4 has desired reinforcement.So new Material cladding infrastructure product (fiber-plastic composite structure product 2) is received by conveying device 5 again and carries to heater 10 according to Fig. 6.Composite structure product 2 is heated to the temperature that the parts of plastics of composite structure product 2 is melted at least partly in this heater, makes composite structure product 2 more easily be out of shape thus.Exemplary temperature scope for the composite structure product 2 based on PA6 is 210 DEG C to 280 DEG C.So the composite structure product 2 after heating is received by conveying device 5 again and is transported in the mould opened of forming machine 11 for shaping or functionalization (see Fig. 7).Finally, close this mould and extrude and solidification, if desired functionalization composite structure product 2.Functionalization such as can mean sprays bead structures, injection encapsulating composite structure product 2 or injection encapsulating insert.Last possibility can also carry out quality control, such as, utilize camera (flash lamp temperature recorder) to carry out.
If should strengthen underlying carrier 4 in both sides, then need turntable 21, this turntable can make component rotate (see Fig. 8 around at least one axis A.In order to receive underlying carrier 4, turntable 21 has framework 33 and retainer member 34.Because underlying carrier 4 (semi-finished product) is not the parts of very bending resistance usually, so in order to (reinforcing element 8) will be with to join on underlying carrier 4, can shift out at dorsal part with the pressing mold contacted with underlying carrier 4, so that activating pressure is born in local.
Fig. 9 illustrates the engagement device 9 be arranged in conveying device 5, and this engagement device has made supersonic generator 22 as ultrasonic welding institution.Appreciable: conveying device 5 has two grasping elements 24 (such as adhering to grasping device, vacuum cup, clamping element or analog), keeps reinforcing element 8 by described grasping element.
Because reinforcing element 8 (band) therefore can may to adsorb, so each tape should be ensured to be separated according to the separator 35 of Figure 10 each other with electrostatic.In order to be separated by band 8 targetedly, storage rack 7 is arranged on above conveyer belt 36.This conveyer belt 36 have somewhat viscous surface or and evacuated panel similarly construct and guarantee good contact between conveyer belt 36 and band 8 thus.In order to then take out a band 8 from storage rack 7, storage rack 7 has only a little more than the opening of tape thickness.In order to be extruded by each band 8, unshowned press mold can be provided with downwards, for applying power F to each band 8.So, be separated band 8 can be taken out by conveying device 5.May with electrostatic and the thus possibilities that can adsorb each other of two bands 8 because there is band 8, so storage rack 7 can be equipped with metallic brush to derive electric charge.Band 8 Electrostatic Absorption no longer each other can be made thus.Also contemplated that in addition: directly on the grasping device of conveying device 5, derive electric charge.
Figure 11 illustrates the possibility that another kind makes band 8 and is separated.Paper introducer in this function and printing machine is similar.Extrude relative to each other with 8 or the roller 37 that scribbles rubber, then roller 37 starts rotate and be transported on receiving platform by band 8 thus.Final position with 8 via the number of turns of roller 37 rotation or can limit via limit switches 38.In order to be here separated by band 8, so design is scribbling the gap between the roller 37 of rubber and storage rack 7, makes to take out a single band 8.Power F can also be applied for being lifted by belt 8 here via press mold 40.In this Figure 11, receiving platform is configured to evacuated panel 38.In an identical manner, storage rack 6 also can be configured to the form of this evacuated panel 38.
If there is camera 18 or whole camera arrangement, so camera 18 also can aim at storage rack 3 and 7.Then, by image processing device, analyzing and processing is carried out to data again.So can send instructions to correspondingly conveying device according to these data.If camera 18 is arranged in the region of grasping element 24, so can additionally monitor and if desired revise component receive or component deposit.
Thus, realized by the present invention: the semi-finished product (reinforcing element 8) that the semi-finished product (underlying carrier 4) that fiber is strengthened utilize the second fiber to strengthen targetedly carry out " inlinely " and strengthen." inline inline " here means that semi-finished product are combined in final process and carries out.Then the semi-finished product be connected to each other are heated to more than fusion temperature after this combination and finally these semi-finished product in the mold curing and shaping of forming machine 11 and/or functionalization.
Claims (18)
1., for the manufacture of the former (1) of composite structure product (2), especially fiber-plastic composite structure product, this former has:
● the first storage rack (3), in described first storage rack, deposit the underlying carrier (4) that optimum fiber is strengthened;
● conveying device (5), for taking out underlying carrier (4) from described first storage rack (3);
● storage rack (6), this storage rack can be placed the underlying carrier (4) taken out by described conveying device (5);
● the second storage rack (7), in described second storage rack, deposited reinforcing element (8), at least one reinforcing element (8) can be put on the underlying carrier (4) that is on described storage rack (6) by described conveying device (5);
● engagement device (9), for described reinforcing element (8) and described underlying carrier (4) are connected into composite structure product (2);
● heater (10), described composite structure product (2) can be transported in described heater by described conveying device (5), and in this heater, described composite structure product (2) can be heated to more than the fusion temperature of the plastics of the described composite structure product of common formation (2);
● forming machine (11), can extrude and solidify the composite structure product (2) after heating in described forming machine.
2. former according to claim 1, it has positioner (12), for being positioned at by described underlying carrier (4) on storage rack (6) and/or described reinforcing element (8) being positioned at described underlying carrier (4).
3. former according to claim 2, wherein, described positioner (12) has push unit (13) and is configured at least one backstop (14) on storage rack (6), wherein, described underlying carrier (4) and/or described reinforcing element (8) can be made to move until backstop is to theoretical position (P by described push unit (12)
sOLL) in.
4. former according to claim 2, wherein, described positioner (12) has at least one position sensor (15) and control program (16), can to the physical location (P of the underlying carrier (4) detected by described at least one position sensor (15) and/or reinforcing element (8) storage rack (6) or underlying carrier (4) relatively relatively via this control program
iST) carry out analyzing and processing and can by its with store in the described control program (16) or the theoretical position (P that calculates
sOLL) compare, wherein, can control impuls (17) be transmitted to conveying device (5) by described control program (16) and underlying carrier (4) and/or reinforcing element (8) can be made to move to theoretical position (P by described conveying device (5)
sOLL) in.
5. former according to claim 4, wherein, pressure sensor, limit switches (38), laser instrument, weight sensor and/or the camera (18) pointing to described storage rack (6) play position sensor (15).
6. former according to claim 5, wherein, described camera (18) is arranged on storage rack (6) still or is preferably fixed on movingly in conveying device (5).
7. former according to any one of claim 1 to 6, wherein, described storage rack (6)
● be integrated on described first storage rack (3), or
● be configured to lodging bench (19) separately, or
● be integrated in described heater (10).
8. former according to any one of claim 1 to 7, wherein, described storage rack (6) has evacuated panel (20), reliably keeps described underlying carrier (4) for location.
9. former according to any one of claim 1 to 8, this former is provided with around at least one axis (A) movable turntable (21), described storage rack (6) can be fixed on described turntable, or described storage rack (6) is configured on described turntable.
10. former according to any one of claim 1 to 9, wherein, described engagement device (9) has supersonic generator (22).
11. formers according to any one of claim 1 to 10, wherein, described engagement device (9) is arranged in described conveying device (5).
12. formers according to any one of claim 1 to 11, wherein, described conveying device (5) is manipulation robot (23), and this manipulation robot preferably has grasping element (24).
13. formers according to any one of claim 1 to 12, this former is provided with closed loop for former (1) described in closed loop or opened loop control or opened loop control unit (25), wherein, at least described conveying device (5), described engagement device (9), described heater (10) and described forming machine (11) can come closed loop or opened loop control by described closed loop or opened loop control unit (25) jointly.
14. according to claim 4 and former according to claim 13, and wherein, the control program (16) of described positioner (12) is a part for described closed loop or opened loop control unit (25).
15. formers any one of claim 1 to 14, this former is provided with shear (26), wherein, described reinforcing element (8) can by described shear (26) cutting before being placed on described underlying carrier (4).
16., for especially manufacturing the method for composite structure product (2) in the former (1) according to any one of claim 1 to 15, have following steps:
● from the first storage rack (3) depositing the underlying carrier (4) that optimum fiber is strengthened, take out underlying carrier (4) by conveying device (5);
● the underlying carrier (4) taken out by described conveying device (5) is placed on storage rack (6);
● from the second storage rack (7) depositing reinforcing element (8), take out reinforcing element (8) by described conveying device (5);
● described reinforcing element (8) is placed on the underlying carrier (4) be on described storage rack (6);
● by engagement device (9), described reinforcing element (8) and described underlying carrier (4) are connected into composite structure product (2), optimum fiber-plastic composite structure product;
● described composite structure product (2) is transported in heater (10);
● described composite structure product (2) is heated to more than the fusion temperature of the plastics of the described composite structure product of common formation (2) in described heater (10); With
● extruding and the composite structure product (2) after solidifying heating in forming machine (11).
17. methods according to claim 16, wherein, by described composite structure product (2) functionalization in described forming machine (11).
18. methods according to claim 16 or 17, wherein, the theoretical position (P that described underlying carrier (4) and/or described reinforcing element (8) are placed on storage rack (6) by positioner (12)
sOLL) in.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ATA676/2013 | 2013-08-30 | ||
| ATA676/2013A AT514721B1 (en) | 2013-08-30 | 2013-08-30 | Shaping plant for producing a fiber-plastic composite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104512039A true CN104512039A (en) | 2015-04-15 |
Family
ID=52470531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410642417.8A Pending CN104512039A (en) | 2013-08-30 | 2014-08-29 | Forming apparatus for manufacturing fiber-plastic composite structure products |
Country Status (3)
| Country | Link |
|---|---|
| CN (1) | CN104512039A (en) |
| AT (1) | AT514721B1 (en) |
| DE (1) | DE102014012204A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN108349128A (en) * | 2016-02-17 | 2018-07-31 | 宝马股份公司 | Method for manufacturing forming rod piece by fibrous composite |
| CN111315057A (en) * | 2018-12-11 | 2020-06-19 | 恩格尔奥地利有限公司 | Forming machine |
| CN111356557A (en) * | 2017-11-14 | 2020-06-30 | 恩格尔奥地利有限公司 | Method for arranging semi-finished products |
| CN111479673A (en) * | 2017-12-22 | 2020-07-31 | 慕贝尔碳纤维技术有限公司 | Fiber tape laying system |
| CN112659582A (en) * | 2020-12-16 | 2021-04-16 | 北京机科国创轻量化科学研究院有限公司 | Composite material hot press forming device |
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| DE102016110568A1 (en) * | 2016-06-08 | 2017-12-14 | Wemhöner Surface Technologies GmbH & Co. KG | Method and device for fixing superimposed layers of sheet material |
| AT518548B1 (en) | 2016-09-28 | 2017-11-15 | Engel Austria Gmbh | handling device |
| DE102016121215A1 (en) * | 2016-10-07 | 2018-04-12 | Rehau Ag + Co | Plastic component, as well as methods for controlling the proper installation of at least one plastic component |
| DE102017006863A1 (en) | 2017-07-19 | 2019-01-24 | INPRO Innovationsgesellschaft für fortgeschrittene Produktionssysteme in der Fahrzeugindustrie mbH | Method for the in-line production of a lightweight component in hybrid construction, such as a vehicle body to be provided with hybrid structures |
| DE102019200321A1 (en) * | 2019-01-14 | 2020-07-16 | Volkswagen Aktiengesellschaft | Process for draping flat semi-finished products |
| DE102019212832A1 (en) * | 2019-08-27 | 2021-03-04 | Zf Friedrichshafen Ag | Apparatus and method |
| AT524394A1 (en) | 2020-11-05 | 2022-05-15 | Engel Austria Gmbh | Molding plant for producing a composite body |
| AT524802B1 (en) | 2021-03-05 | 2023-04-15 | Engel Austria Gmbh | Procedure for filing semi-finished products |
| CN114701175A (en) * | 2022-05-17 | 2022-07-05 | 扬州港信光电科技有限公司 | Carborundum ultrasonic packaging device with automatically, function leads gas |
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| CN108349128A (en) * | 2016-02-17 | 2018-07-31 | 宝马股份公司 | Method for manufacturing forming rod piece by fibrous composite |
| US11045984B2 (en) | 2016-02-17 | 2021-06-29 | Bayerische Motoren Werke Aktiengesellschaft | Method for producing a shaped bar from fiber composite material |
| CN111356557A (en) * | 2017-11-14 | 2020-06-30 | 恩格尔奥地利有限公司 | Method for arranging semi-finished products |
| CN111356557B (en) * | 2017-11-14 | 2024-01-09 | 恩格尔奥地利有限公司 | Method and device for arranging semifinished products, and forming method and forming device |
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Also Published As
| Publication number | Publication date |
|---|---|
| DE102014012204A8 (en) | 2015-07-30 |
| AT514721A1 (en) | 2015-03-15 |
| AT514721B1 (en) | 2015-06-15 |
| DE102014012204A1 (en) | 2015-03-05 |
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