DE102009015612A1 - Method for manufacturing e.g. motor vehicle component, involves broadening fiber reinforcement, so that fiber reinforcement is fixed on inner wall of hollow container, and reinforcing expanded fiber reinforcement - Google Patents
Method for manufacturing e.g. motor vehicle component, involves broadening fiber reinforcement, so that fiber reinforcement is fixed on inner wall of hollow container, and reinforcing expanded fiber reinforcement Download PDFInfo
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- DE102009015612A1 DE102009015612A1 DE102009015612A DE102009015612A DE102009015612A1 DE 102009015612 A1 DE102009015612 A1 DE 102009015612A1 DE 102009015612 A DE102009015612 A DE 102009015612A DE 102009015612 A DE102009015612 A DE 102009015612A DE 102009015612 A1 DE102009015612 A1 DE 102009015612A1
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- fiber reinforcement
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- 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
- B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
- B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
- B29C66/1312—Single flange to flange joints, the parts to be joined being rigid
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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
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
- B29C66/72141—Fibres of continuous length
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/74—Joining plastics material to non-plastics material
- B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
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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
- B29C66/81—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
- B29C66/814—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
- B29C66/8145—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the constructional aspects of the pressing elements, e.g. of the welding jaws or clamps
- B29C66/81455—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the constructional aspects of the pressing elements, e.g. of the welding jaws or clamps being a fluid inflatable bag or bladder, a diaphragm or a vacuum bag for applying isostatic pressure
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/81—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
- B29C66/814—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
- B29C66/8145—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the constructional aspects of the pressing elements, e.g. of the welding jaws or clamps
- B29C66/81459—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the constructional aspects of the pressing elements, e.g. of the welding jaws or clamps being a filled deformable bladder, e.g. bladder filled with oil, with granules or with a meltable solid 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
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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
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/532—Joining single elements to the wall of tubular articles, hollow articles or bars
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0809—Fabrics
- B29K2105/0845—Woven fabrics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
- B29K2105/246—Uncured, e.g. green
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2305/00—Use of metals, their alloys or their compounds, as reinforcement
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2307/00—Use of elements other than metals as reinforcement
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2309/00—Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
- B29K2309/08—Glass
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2707/00—Use of elements other than metals for preformed parts, e.g. for inserts
- B29K2707/04—Carbon
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2709/00—Use of inorganic materials not provided for in groups B29K2703/00 - B29K2707/00, for preformed parts, e.g. for inserts
- B29K2709/08—Glass
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- 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
- B29L2022/00—Hollow articles
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- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Body Structure For Vehicles (AREA)
Abstract
Description
Die Erfindung beschreibt ein Verfahren zur Herstellung von Profilbauteilen, insbesondere von Kraftfahrzeug-, Struktur- oder Fahrwerksbauteilen sowie ein Profilbauteil, insbesondere Kraftfahrzeug-, Struktur- oder Fahrwerksbauteil.The Invention describes a method for the production of profile components, in particular of motor vehicle, structural or chassis components and a profile component, in particular motor vehicle, structural or chassis component.
Vor allem in der Fahrzeugindustrie steht die Reduzierung des Gewichts der verwendeten Profilbauteile im Vordergrund. Gleichzeitig aber soll die Steifigkeit dieser Profilbauteile erhöht werden, um den Insassen einen möglichst optimalen Schutz im Falle eines Unfalls zu bieten.In front Everything in the vehicle industry is the reduction of weight the profile components used in the foreground. At the same time though the rigidity of these profile components should be increased to provide the inmates the best possible protection in the event to offer an accident.
Aus
dem Stand der Technik ist es bekannt, gewichtsoptimierte Kraftfahrzeugbauteile
durch Einbinden von faserverstärkten Geweben zu verstärken. So
beschreibt beispielsweise die
Kraftfahrzeugbauteile, wie beispielsweise Vorderachshilfsrahmen, Hinterachsen oder andere Hohlkörper, werden in vielen Fällen durch Verfahren mit einem hohen Wärmeeintrag, wie Schutzgasschweißen, Punktschweißen oder Laserschweißen, hergestellt. Die hierbei auftretenden Temperaturen sind zu hoch für faserverstärkte Kunststoffe und können diese zerstören. Aus diesem Grund muss beim Integrieren von faserverstärkten Kunststoffen darauf geachtet werden, dass diese im Abstand zu den späteren Fügestellen angeordnet werden. Es ist daher beispielsweise nicht möglich, einen aus zwei Halbschalen zusammengesetzt hergestellten Hohlkörper innen vollständig durch den Einsatz eines faserverstärkten Kunststoffs zu verstärken.Automotive components, such as front axle auxiliary frames, rear axles or other hollow bodies, are in many cases by high-level procedures Heat input, such as inert gas welding, spot welding or laser welding, manufactured. The occurring here Temperatures are too high for fiber reinforced Plastics and can destroy them. For this Reason must be given when integrating fiber-reinforced plastics be taken to ensure that they are in the distance to the later Joints are arranged. It is therefore, for example not possible, one composed of two half-shells completely finished inside hollow body to increase the use of a fiber-reinforced plastic.
Der Erfindung liegt hiervon ausgehend die Aufgabe zu Grunde, einerseits ein Verfahren aufzuzeigen, mit welchem Profilbauteile, insbesondere Kraftfahrzeugbauteile in Form von Hohlprofilen aus Metall, mit faserverstärkten Geweben verstärkt werden können sowie andererseits ein entsprechendes Profilbauteil aufzuzeigen.Of the On this basis, the invention is based on the object, on the one hand to show a method with which profile components, in particular motor vehicle components in the form of hollow sections of metal, with fiber-reinforced Tissues and on the other hand to show a corresponding profile component.
Die Lösung der Verfahrensaufgabe besteht in einem Verfahren mit den Maßnahmen des Patentanspruchs 1.The Solution of the process task consists in a procedure with the measures of claim 1.
Der gegenständliche Teil der Aufgabe wird durch ein Profilbauteil mit den Merkmalen des Patentanspruchs 14 gelöst.Of the objective part of the task is a profile component solved with the features of claim 14.
Vorteilhafte Weiterbildungen sind Gegenstand der jeweiligen Unteransprüche.advantageous Further developments are the subject of the respective subclaims.
Durch das erfindungsgemäße Verfahren werden Profilbauteile, insbesondere Kraftfahrzeug-, Struktur- oder Fahrwerksbauteile, welche einen Hohlkörper aus Metall aufweisen, mit einer zumindest bereichsweise an einer Innenwand angeordneten Faserverstärkung verstärkt. Zu diesen Profilbauteilen gehören beispielsweise Rohrprofile oder bereits miteinander verbundene, ein umfangsseitig geschlossenes Hohlprofil bildende Struktur- oder Schalenbauteile. Diese können beispielsweise durch Schweißverfahren miteinander verbunden sein. Die Herstellung des Hohlprofils erfolgt erfindungsgemäß vor dem Einbringen der Faserverstärkung.By the method according to the invention become profile components, in particular motor vehicle, structural or chassis components, which a hollow body made of metal, with at least one partially arranged on an inner wall fiber reinforcement strengthened. These profile components include, for example Pipe profiles or already interconnected, one circumferentially closed hollow profile forming structural or shell components. These can, for example, by welding together be connected. The production of the hollow profile according to the invention before the introduction of the fiber reinforcement.
Die Faserverstärkung wird in den fertigen Hohlkörper eingebracht und anschließend derart aufgeweitet, dass sich die Faserverstärkung an der Innenwand des Hohlkörpers flächig anlegt. Die Faserverstärkung ist zu diesem Zeitpunkt noch weich und damit flexibel genug, um aufgeweitet werden zu können. Die Faserverstärkung kann bereichsweise oder vollflächig an der Innenwand anliegen, je nach geforderter Steifigkeit. Anschließend wird die Faserverstärkung verfestigt und geht eine feste Klebeverbindung mit dem Hohlkörper ein. Da nach dem Einbringen der Faserverstärkung keine Fertigungsschritte mit hohem Wärmeeintrag mehr erforderlich sind, kann die Faserverstärkung in jedem Bereich des Hohlkörpers angeordnet werden. Je nach Art der Faserverstärkung und der Struktur bzw. des Profils der Innenwand kann die Verbindung zwischen der Faserverstärkung und der Innenwand des Hohlprofils flächig oder bei entsprechenden Hinterschneidungen auch formschlüssig sein. Hierbei kann die Faserverstärkung auch den Verbindungsbereich zwischen zwei Profilelementen überbrücken, selbst wenn die Profilelemente, aus denen das Profilbauteil zusammengesetzt ist, durch ein thermisches Fügeverfahren verbunden worden sind.The Fiber reinforcement is in the finished hollow body introduced and then expanded so that the fiber reinforcement on the inner wall of the hollow body two-dimensional. The fiber reinforcement is to this Timing is still soft and therefore flexible enough to be widened to be able to. The fiber reinforcement can be regionally or completely against the inner wall, depending on the required Rigidity. Subsequently, the fiber reinforcement solidifies and goes a firm adhesive bond with the hollow body one. Since after the introduction of the fiber reinforcement no Manufacturing steps with high heat input more required can, the fiber reinforcement in each area of the hollow body to be ordered. Depending on the type of fiber reinforcement and the structure or the profile of the inner wall, the connection between the fiber reinforcement and the inner wall of the hollow profile flat or with appropriate undercuts also be positive. Here, the fiber gain also bridge the connection area between two profile elements, even if the profile elements that make up the profile component is linked by a thermal joining process are.
Vorzugsweise wird die Faserverstärkung auf ein Werkzeug aufgebracht und mit diesem Werkzeug durch eine Öffnung in den Hohlkörper eingeführt. Nach dem Einbringen wird das Werkzeug zumindest teilweise expandiert. Es drückt somit die Faserverstärkung an die Innenwand des Hohlkörpers, wo diese sich auf Grund ihrer hohen Viskosität flächig anlegt. Die Faserverstärkung wird nach einem Aufweitprinzip mit dem umgebenden Profilbauteil verbunden. Die Faserverstärkung kann bei diesem Prinzip ebenfalls als Hohlkörper, insbesondere als Schlauch, ausgebildet sein. Als Werkzeug kann beispielsweise eine Art Ballonkatheter eingesetzt werden, welcher mit einem Fluid befüllt wird. Als Fluid kann sowohl ein Gas als auch eine Flüssigkeit eingesetzt werden. Durch Ausübung eines Drucks auf das eingesetzte Fluid wird das Werkzeug aufgeweitet bzw. expandiert, wodurch die Faserverstärkung an die Innenwand des Hohlkörpers gedrückt wird. Nachdem die Faserverstärkung teilweise oder vollständig an der Innenwand des Hohlkörpers anliegt, wird entweder das Fluid oder das Werkzeug auf eine Aushärtetemperatur erhitzt, so dass die Faserverstärkung an der Innenwand anliegend ausgehärtet wird. Ebenso ist es möglich, das Werkzeug mit einem bereits temperierten Medium zu befüllen.Preferably, the fiber reinforcement is applied to a tool and introduced with this tool through an opening in the hollow body. After insertion, the tool is at least partially expanded. It thus pushes the fiber reinforcement to the inner wall of the hollow body, where it applies flat due to their high viscosity. The fiber reinforcement is connected to the surrounding profile component according to an expansion principle. The fiber reinforcement can also be formed in this principle as a hollow body, in particular as a hose. As a tool, for example, a type of balloon catheter can be used, which is filled with a fluid. As a fluid, both a gas and a liquid can be used. By exerting pressure on the fluid used, the tool expands or expands diert, whereby the fiber reinforcement is pressed against the inner wall of the hollow body. After the fiber reinforcement partially or completely abuts against the inner wall of the hollow body, either the fluid or the tool is heated to a curing temperature, so that the fiber reinforcement is cured adjacent to the inner wall. It is also possible to fill the tool with an already tempered medium.
Das Werkzeug bleibt so lange im expandierten Zustand, bis eine ausreichende Festigkeit der Faserverstärkung an der Innenwand erreicht ist. Im Anschluss daran wird der von dem Werkzeug ausgeübte Druck verringert. Das Werkzeugvolumen wird verkleinert. Dadurch löst sich das Werkzeug von der ausgehärteten Faserverstärkung an der Innenwand des Hohlkörpers und kann aus dem Hohlkörper entfernt werden. Gegebenenfalls kann die Faserverstärkung anschließend noch nachgehärtet werden.The Tool remains in the expanded state until a sufficient Strength of the fiber reinforcement achieved on the inner wall is. Following this, the tool exerted by the tool Reduced pressure. The tool volume is reduced. Thereby the tool releases from the hardened fiber reinforcement on the inner wall of the hollow body and can from the hollow body be removed. Optionally, the fiber reinforcement then be postcured.
Um zu vermeiden, dass das Werkzeug an der Faserverstärkung haften bleibt, ist es vorzugsweise mit einer Antihaftbeschichtung versehen.Around to avoid having the tool at the fiber reinforcement it is preferably with a non-stick coating Mistake.
Als Faserverstärkung kann beispielsweise ein glasfaserverstärktes Gewebe oder auch ein kohlenstofffaserverstärktes Gewebe eingesetzt werden. Das Auftragen des faserverstärkten Gewebes erfolgt derart, dass die Fasern ungefähr in Umfangsrichtung des Werkzeuges orientiert sind. Die Schichtdicke des aufgetragenen Gewebes kann entsprechend der Geometrie der Innenwand des Hohlkörpers variieren. Dadurch kann einerseits eine gleichmäßige Verteilung der Faserverstärkung an der Innenwand, andererseits auch eine gezielte bereichsweise größere Verstärkung der Innenwand erzielt werden. Mit Aufweitung des Werkzeugs vergrößert sich dessen Umfangsfläche und die Fasern gleiten relativ zueinander, wobei die Schichtdicke des Gewebes abnimmt. Durch das Auftragen der Fasern in Umfangsrichtung des Werkzeugs wird sichergestellt, dass sich diese ungefähr parallel zur Innenwand orientiert an diese anlegen.When Fiber reinforcement, for example, a glass fiber reinforced Tissue or a carbon fiber reinforced tissue be used. Applying the fiber reinforced fabric takes place such that the fibers approximately in the circumferential direction of Tool are oriented. The layer thickness of the applied fabric can according to the geometry of the inner wall of the hollow body vary. This can on the one hand a uniform Distribution of the fiber reinforcement on the inner wall, on the other hand also a targeted areawise greater reinforcement the inner wall can be achieved. Enlarged with widening of the tool its peripheral surface and the fibers slide relatively to each other, wherein the layer thickness of the tissue decreases. By the Applying the fibers in the circumferential direction of the tool is ensured that this is oriented approximately parallel to the inner wall create on this.
Ein mit diesem Verfahren hergestelltes Profilbauteil umfasst somit einen metallischen Hohlkörper, welcher durch eine mit seiner Innenwand verbundenen Faserverstärkung zumindest bereichsweise verstärkt ist. Dabei erfolgt die Verstärkung nach der Herstellung des Hohlkörpers. Dies bedeutet, dass beispielsweise temperaturintensive Verfahren wie Schweißen oder Löten zum Verbinden von beispielsweise Schalen oder Profilelementen vor dem Einbringen der Faserverstärkung durchgeführt werden. Dadurch muss bei der Platzierung der faserverstärkten Kunststoffe nicht mehr darauf geachtet werden, dass diese im Abstand zu den späteren Fügestellen angeordnet werden, um eine zu starke Erwärmung und Beschädigung der Faserverstärkung zu vermeiden.One The profiled component produced by this method thus comprises one metallic hollow body, which by one with its Interior wall connected fiber reinforcement at least partially is reinforced. The reinforcement takes place after the Production of the hollow body. This means that, for example Temperature-intensive processes such as welding or soldering for connecting, for example, shells or profile elements performed the introduction of the fiber reinforcement become. This requires the placement of the fiber-reinforced Plastics are no longer paid attention to these in the distance be arranged to the later joints, to overheating and damaging the Fiber reinforcement to avoid.
Die Faserverstärkung kann bereichsweise oder vollständig an der Innenwand des Hohlkörpers angeordnet sein. Besteht das Profilbauteil beispielsweise aus einem zusammengesetzten Hohlkörper, so kann insbesondere der Fügebereich zwischen den Profilbauteilen durch die Faserverstärkung überbrückt werden.The Fiber reinforcement can be regional or complete be arranged on the inner wall of the hollow body. Consists the profile component, for example, from a composite hollow body, so In particular, the joining region between the profile components bridged by the fiber reinforcement become.
Verfahren und Profilbauteil werden anhand eines Ausführungsbeispiels in den nachfolgenden Figuren näher beschrieben. Es zeigen:method and profile component are based on an embodiment described in more detail in the following figures. Show it:
In
diesen Hohlkörper
Die
Umfangsseite
Durch
Temperieren der Flüssigkeit
Anschließend
wird der Druck P auf das Werkzeug
Das
fertige Profilbauteil
- 11
- Profilbauteilprofile component
- 22
- Profilelementprofile element
- 33
- Profilelementprofile element
- 44
- Hohlkörperhollow body
- 55
- WerkzeugTool
- 66
- Faserverstärkungfiber reinforcement
- 77
- Faserfiber
- 88th
- Umfangsseiteperipheral side
- 99
- Flüssigkeitliquid
- 1010
- Innenwandinner wall
- 1111
- Fügebereichjoining area
- PP
- Druckprint
- TT
- Temperaturtemperature
ZITATE ENTHALTEN IN DER BESCHREIBUNGQUOTES INCLUDE IN THE DESCRIPTION
Diese Liste der vom Anmelder aufgeführten Dokumente wurde automatisiert erzeugt und ist ausschließlich zur besseren Information des Lesers aufgenommen. Die Liste ist nicht Bestandteil der deutschen Patent- bzw. Gebrauchsmusteranmeldung. Das DPMA übernimmt keinerlei Haftung für etwaige Fehler oder Auslassungen.This list The documents listed by the applicant have been automated generated and is solely for better information recorded by the reader. The list is not part of the German Patent or utility model application. The DPMA takes over no liability for any errors or omissions.
Zitierte PatentliteraturCited patent literature
- - DE 102004003190 A1 [0003] DE 102004003190 A1 [0003]
Claims (17)
Priority Applications (1)
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DE102009015612A DE102009015612A1 (en) | 2009-04-02 | 2009-04-02 | Method for manufacturing e.g. motor vehicle component, involves broadening fiber reinforcement, so that fiber reinforcement is fixed on inner wall of hollow container, and reinforcing expanded fiber reinforcement |
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DE102009015612A DE102009015612A1 (en) | 2009-04-02 | 2009-04-02 | Method for manufacturing e.g. motor vehicle component, involves broadening fiber reinforcement, so that fiber reinforcement is fixed on inner wall of hollow container, and reinforcing expanded fiber reinforcement |
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DE102009015612A1 true DE102009015612A1 (en) | 2010-10-07 |
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DE102009015612A Ceased DE102009015612A1 (en) | 2009-04-02 | 2009-04-02 | Method for manufacturing e.g. motor vehicle component, involves broadening fiber reinforcement, so that fiber reinforcement is fixed on inner wall of hollow container, and reinforcing expanded fiber reinforcement |
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Cited By (8)
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GB2476874A (en) * | 2010-01-06 | 2011-07-13 | Mark Seddon | Pressurising a moulding material during moulding |
EP2455625A3 (en) * | 2010-11-19 | 2012-06-20 | The Boeing Company | Composite sandwich shell edge joint |
DE102011050304A1 (en) * | 2011-05-12 | 2012-11-15 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Method for producing hybrid components made of fiber-reinforced plastic with integrated metallic mold |
DE102011078709A1 (en) * | 2011-07-06 | 2013-01-10 | Bayerische Motoren Werke Aktiengesellschaft | Method and device for producing a fiber-reinforced plastic component |
DE102011054915A1 (en) * | 2011-10-28 | 2013-05-02 | Benteler Automobiltechnik Gmbh | A method of making a motor vehicle hybrid component and a motor vehicle hybrid component made by the method |
US8784596B2 (en) | 2010-11-19 | 2014-07-22 | The Boeing Company | Method for making and joining composite sandwich shell edge joint |
DE102014200130A1 (en) * | 2014-01-08 | 2015-07-09 | Bayerische Motoren Werke Aktiengesellschaft | Method for repairing or reinforcing a hollow profile section of a plastic profile |
DE102019102600A1 (en) * | 2019-02-01 | 2020-08-06 | Sandvik Materials Technology Deutschland Gmbh | Method and device for producing a rod-shaped element |
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DE3528307C2 (en) * | 1985-08-07 | 1992-01-02 | Julius & August Erbsloeh Gmbh & Co, 5620 Velbert, De | |
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DE60200161T2 (en) * | 2001-02-13 | 2004-10-28 | Campagnolo S.R.L. | Method for manufacturing a bicycle hub, device for carrying out this method and hub produced by this method |
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GB2476874A (en) * | 2010-01-06 | 2011-07-13 | Mark Seddon | Pressurising a moulding material during moulding |
EP2455625A3 (en) * | 2010-11-19 | 2012-06-20 | The Boeing Company | Composite sandwich shell edge joint |
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DE102014200130A1 (en) * | 2014-01-08 | 2015-07-09 | Bayerische Motoren Werke Aktiengesellschaft | Method for repairing or reinforcing a hollow profile section of a plastic profile |
DE102019102600A1 (en) * | 2019-02-01 | 2020-08-06 | Sandvik Materials Technology Deutschland Gmbh | Method and device for producing a rod-shaped element |
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