DE102011008759A1 - Method for manufacturing e.g. structure component that is utilized in vehicle, involves forming fiber semi-finished material, curing fluent matrix material by heating, and removing mold body from injection mold - Google Patents
Method for manufacturing e.g. structure component that is utilized in vehicle, involves forming fiber semi-finished material, curing fluent matrix material by heating, and removing mold body from injection mold Download PDFInfo
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- DE102011008759A1 DE102011008759A1 DE201110008759 DE102011008759A DE102011008759A1 DE 102011008759 A1 DE102011008759 A1 DE 102011008759A1 DE 201110008759 DE201110008759 DE 201110008759 DE 102011008759 A DE102011008759 A DE 102011008759A DE 102011008759 A1 DE102011008759 A1 DE 102011008759A1
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- fiber
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- injection mold
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- 238000002347 injection Methods 0.000 title claims abstract description 53
- 239000007924 injection Substances 0.000 title claims abstract description 53
- 239000000835 fiber Substances 0.000 title claims abstract description 45
- 238000000034 method Methods 0.000 title claims abstract description 39
- 239000011159 matrix material Substances 0.000 title claims abstract description 37
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 12
- 239000000463 material Substances 0.000 title claims abstract description 8
- 238000010438 heat treatment Methods 0.000 title claims abstract description 7
- 239000012528 membrane Substances 0.000 claims abstract description 25
- 229920002430 Fibre-reinforced plastic Polymers 0.000 claims abstract description 16
- 239000011151 fibre-reinforced plastic Substances 0.000 claims abstract description 16
- 229920003023 plastic Polymers 0.000 claims abstract description 6
- 239000004033 plastic Substances 0.000 claims abstract description 6
- 239000002184 metal Substances 0.000 claims abstract description 5
- 125000006850 spacer group Chemical group 0.000 claims abstract description 5
- 239000000806 elastomer Substances 0.000 claims abstract description 4
- 229920001971 elastomer Polymers 0.000 claims abstract description 4
- 238000000465 moulding Methods 0.000 claims description 40
- 239000011265 semifinished product Substances 0.000 claims description 19
- 230000009969 flowable effect Effects 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 7
- 239000002657 fibrous material Substances 0.000 claims description 6
- 239000004848 polyfunctional curative Substances 0.000 claims description 5
- 239000000047 product Substances 0.000 claims description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 3
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 229910052799 carbon Inorganic materials 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 3
- GNFTZDOKVXKIBK-UHFFFAOYSA-N 3-(2-methoxyethoxy)benzohydrazide Chemical compound COCCOC1=CC=CC(C(=O)NN)=C1 GNFTZDOKVXKIBK-UHFFFAOYSA-N 0.000 claims description 2
- FGUUSXIOTUKUDN-IBGZPJMESA-N C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 Chemical compound C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 FGUUSXIOTUKUDN-IBGZPJMESA-N 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 claims description 2
- 239000004745 nonwoven fabric Substances 0.000 claims 1
- 230000000712 assembly Effects 0.000 abstract 1
- 238000000429 assembly Methods 0.000 abstract 1
- 210000004379 membrane Anatomy 0.000 description 20
- 239000011347 resin Substances 0.000 description 17
- 229920005989 resin Polymers 0.000 description 17
- 238000001746 injection moulding Methods 0.000 description 4
- 239000000243 solution Substances 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000009745 resin transfer moulding Methods 0.000 description 3
- 238000004140 cleaning Methods 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- BUHVIAUBTBOHAG-FOYDDCNASA-N (2r,3r,4s,5r)-2-[6-[[2-(3,5-dimethoxyphenyl)-2-(2-methylphenyl)ethyl]amino]purin-9-yl]-5-(hydroxymethyl)oxolane-3,4-diol Chemical compound COC1=CC(OC)=CC(C(CNC=2C=3N=CN(C=3N=CN=2)[C@H]2[C@@H]([C@H](O)[C@@H](CO)O2)O)C=2C(=CC=CC=2)C)=C1 BUHVIAUBTBOHAG-FOYDDCNASA-N 0.000 description 1
- 241001295925 Gegenes Species 0.000 description 1
- 239000004809 Teflon Substances 0.000 description 1
- 229920006362 Teflon® Polymers 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000009956 embroidering Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000009958 sewing Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000001721 transfer moulding Methods 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- 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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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Manufacturing & Machinery (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
Description
Die Erfindung betrifft ein Verfahren sowie eine Vorrichtung zur Herstellung von Formkörpern aus faserverstärkten Kunststoffen nach dem Oberbegriff des Patentanspruchs 1 bzw. 9 der Erfindung.The invention relates to a method and an apparatus for producing molded articles made of fiber-reinforced plastics according to the preamble of
Verfahren und Vorrichtungen zur Herstellung von Formkörpern aus faserverstärkten Kunststoffen sind seit geraumer Zeit in den unterschiedlichsten Ausführungen bekannt. So können besagte Formkörper nach dem an sich bekannten RTM-Verfahren (RTM = Resin Transfer Moulding) hergestellt werden. Im Wesentlichen wird dabei Fasermaterial in eine zumindest eine Kavität aufweisende Spritzgießform aus zwei oder mehr Formteilen eingebracht und in derselben mit einem infolge Erwärmung zumindest eines Formteils reaktiven Matrix, wie insbesondere einem Harz (z. B. Epoxidharz) oder einem Harzgemisch getränkt. Hierbei füllt idealerweise das Harz oder Harzgemisch die besagte Kavität vollständig aus. Nach Abschluss der chemischen Reaktion der Matrix und Aushärten derselben kann der faserverstärkte Formkörper der Spritzgießform entnommen werden.Methods and apparatus for the production of moldings from fiber-reinforced plastics have been known for quite some time in a variety of designs. Thus, said moldings can be produced by the known RTM process (RTM = Resin Transfer Molding). In this case, fiber material is essentially introduced into an injection mold comprising at least one cavity from two or more molded parts and impregnated therein with a matrix which is reactive as a result of heating at least one molded part, in particular a resin (eg epoxy resin) or a resin mixture. Ideally, the resin or resin mixture fills said cavity completely. After completion of the chemical reaction of the matrix and curing of the same, the fiber-reinforced molded body can be removed from the injection mold.
In der Praxis wurde jedoch gefunden, dass das Volumen des Harzes beim Aushärten desselben sich bis zu etwa 3% verringert (vgl.
Weitere mit der vorstehenden Lösung vergleichbare Lösungen sind ferner aus der
All den aufgezeigten Lösungsvarianten ist gemein, dass diese während der Verfahrensführung zumindest eine teilweise Benetzung der Spritzgießform mit Matrixwerkstoff, wie beispielsweise Harz, bewirken, woraus erhöhter Aufwand im Hinblick auf die Vorbereitung der Form für nachfolgende Spritzgießzyklen durch Reinigung derselben von Restbeständen des besagten Matrixwirkstoffs resultiert.All the variants of solution shown have in common that during the process, they cause at least partial wetting of the injection mold with matrix material, such as resin, resulting in increased effort with regard to the preparation of the mold for subsequent injection molding cycles by cleaning the same from remainders of said matrix active.
Hiervon ausgehend ist es Aufgabe der Erfindung, ein verbessertes Verfahren zur Herstellung von Formkörpern aus faserverstärkten Kunststoffen anzugeben, vermittel dessen es zum einen gestatten ist, Formkörper aus faserverstärkten Kunststoffen mit exakter vordefinierter Geometrie herzustellen. Zum anderen sollen im Hinblick auf den Stand der Technik geringere Spritzzyklenzeiten realisierbar sein, die insbesondere mit minimierten Vorbereitungsarbeiten der Spritzgießform zur Durchführung des Spritzgießverfahrens einhergehen. Weiter ist es Aufgabe der Erfindung eine geeignete Vorrichtung bzw. Anordnung zur Durchführung des Verfahren zu schaffen.On this basis, it is an object of the invention to provide an improved process for the production of molded articles made of fiber-reinforced plastics, mediate of which it is allowed on the one hand to produce moldings of fiber-reinforced plastics with exact predefined geometry. On the other hand, in view of the state of the art, lower injection cycle times should be achievable, which are associated in particular with minimized preparatory work of the injection mold for carrying out the injection molding process. It is another object of the invention to provide a suitable device or arrangement for carrying out the method.
Gelöst wird die gestellte Aufgabe zunächst durch das in Patentanspruch 1 wiedergegebene Verfahren. Danach weist das Verfahren zur Herstellung von Formkörpern aus faserverstärkten Kunststoffen folgende nacheinander durchzuführende Verfahrensschritte auf:
- a) Ausbildung eines aus einer oder mehreren trockenen Preformen und/oder Preform-ZSB's bestehenden Faser-Halbzeugs,
- b) luftdichtes umschließen desselben mittels zweier oder mehrerer, zumindest eine Kavität ausbildender Formteile, wobei für wenigstens eines der Formteile eine zumindest abschnittsweise flexible Membran verwendet wird,
- c) Evakuierung der besagten Kavität über eine oder mehrere an die Kavität angeschlossene Evakuierungsleitungen und Schließen derselben nach Evakuierung,
- d) Einlegen des luftdicht umschlossenen Faser-Halbzeugs in eine als Druckkammer ausgebildete Spritzgießform,
- e) Injektion eines fließfähigen Matrixwerkstoffes in die zumindest eine durch die Formteile gebildete und das Faser-Halbzeug aufnehmende Kavität durch an die Kavität angeschlossene Injektionsleitungen hindurch derart, dass sich die flexible Membran während des Injektionsprozesses mit einem Injektionsdruck „P1” aufgrund vorgesehener Distanzhalter der Spritzgießform in Grenzen nach außen wölbt,
- f) Aufbringen eines Gegendruckes „P2” gegen die nach außen gewölbte Membran bei geöffneten Injektionsleitungen und/oder Evakuierungsleitungen derart, dass der fließfähige Matrixwerkstoff in das Faser-Halbzeug gepresst wird indem der Matrixwerkstoff vornehmlich das Faser-Halbzeug in Dickenrichtung desselben respektive normal zur Faserrichtung durchtränkt, und dass überschüssiger Matrixwerkstoff durch besagte geöffnete Injektionsleitungen und/oder Evakuierungsleitungen abfließt,
- g) Aushärten des Matrixwerkstoffes, gegebenenfalls durch Erwärmung, und
- h) Entnahme des Formkörpers aus der Spritzgießform.
- a) forming a fiber semifinished product consisting of one or more dry preforms and / or preform ZSBs,
- b) airtight enclosing the same by means of two or more, at least one cavity forming moldings, wherein for at least one of the mold parts, an at least partially flexible membrane is used,
- c) evacuation of said cavity via one or more evacuation lines connected to the cavity and closing same after evacuation,
- d) inserting the air-tightly enclosed fiber semifinished product in an injection mold designed as a pressure chamber,
- e) injection of a flowable matrix material into the at least one cavity formed by the mold parts and receiving the fiber semi-finished by injection lines connected to the cavity such that the flexible membrane during the injection process with an injection pressure "P 1 " due to provided spacers of the injection mold bulges outward in borders,
- f) applying a back pressure "P 2 " against the outwardly curved membrane with open injection lines and / or evacuation lines such that the flowable matrix material is pressed into the fiber semifinished product by the matrix material mainly the fiber semifinished product in the same direction or normal to the fiber direction impregnated, and that excess matrix material flows through said opened injection lines and / or evacuation lines,
- g) curing of the matrix material, optionally by heating, and
- h) removal of the molding from the injection mold.
Dieses Verfahren gestattet eine einfache und kostengünstige Herstellung von Formkörpern aus faserverstärkten Kunststoffen, da nach dem Stand der Technik erforderliche umfangreiche Reinigungsarbeiten an der Spritzgießform, insbesondere infolge an der Spritzgießform anhaftenden Matrixmaterials, weitestgehend vermieden sind.This method allows a simple and cost-effective production of molded articles made of fiber-reinforced plastics, as required by the prior art extensive cleaning work on the injection mold, in particular due to adhering to the injection mold matrix material, are largely avoided.
Die Unteransprüche beschreiben bevorzugte Weiterbildungen oder Ausgestaltungen der Erfindung.The subclaims describe preferred developments or refinements of the invention.
So kann im Hinblick auf den Verfahrensschritt a) vorgesehen sein, dass die trockenen Preformen und/oder Preform-ZSB's aus einer oder mehreren trockenen und gegebenenfalls vorgeformten Einzellagen aus Fasermaterial, wie Kohlefasern o. a., gebildet werden, wobei die Einzellagen Fasergewebe und/oder Faservliese sein können und unterschiedliche Faserorientierungen aufweisen können. Durch diese Maßnahme kann vorteilhaft auf die Festigkeit des herzustellenden Formkörpers Einfluss genommen werden. Im Hinblick auf den Verfahrensschritt b) kann als zumindest abschnittsweise flexible Membran vorteilhaft eine Membran aus einem Kunststoff, einem Metall, einem Elastomer oder einem anderen geeigneten flexiblen Werkstoff verwendet werden. Weiter vorteilhaft kann im Hinblick auf den Verfahrensschritt e) als fließfähiger Matrixwerkstoff ein aushärtbares Harz-Härter-Gemisch verwendet werden. Ferner kann im Hinblick auf den Verfahrensschritt f) zum Aufbringen eines Gegendruckes „P2” gegen die nach außen gewölbte Membran ein gasförmiges oder flüssiges Druckmedium verwendet wird.Thus, with regard to method step a), provision may be made for the dry preforms and / or preform CSBs to be formed from one or more dry and possibly preformed individual layers of fibrous material, such as carbon fibers, where the individual layers are fibrous webs and / or nonwoven webs can and have different fiber orientations. By this measure can be advantageously taken on the strength of the molded body influence. With regard to method step b), a diaphragm made of a plastic, a metal, an elastomer or another suitable flexible material can advantageously be used as the at least partially flexible diaphragm. Further advantageously, in view of the process step e) as a flowable matrix material, a curable resin-hardener mixture can be used. Furthermore, with regard to method step f), a gaseous or liquid pressure medium may be used to apply a back pressure "P 2 " to the outwardly curved diaphragm.
Des Weiteren kann im Hinblick auf den Verfahrensschritt g) die gegebenenfalls vorgesehene Erwärmung des Matrixwerkstoffes zweckmäßigerweise mittels eines oder mehrerer erwärmter Formwerkzeuge der Spritzgießform erfolgen. Schließlich kann im Hinblick auf den Verfahrensschritt h) sich an diesen ein Ablösen der Formteile vom faserverstärkten Kunststoff des Formkörpers anschließen. Es besteht somit die Möglichkeit, entweder die besagten Formteile vom faserverstärkten Kunststoff des Formkörpers zu lösen und für weitere Spritzgießzyklen zu verwenden oder als verlorene Formteile einzusetzen, indem dieselben die Außenhaut des faserverstärkten Kunststoffs des Formkörpers ausbilden. Das Verfahren bietet sich insbesondere zur Herstellung von Formkörpern in Form von Strukturbauteilen und/oder Oberflächenbauteilen und/oder Sichtcarbonbauteilen an Fahrzeugen an.Furthermore, with regard to method step g), the optionally provided heating of the matrix material can expediently be effected by means of one or more heated molds of the injection mold. Finally, with regard to method step h), this can be followed by detachment of the molded parts from the fiber-reinforced plastic of the molded article. It is therefore possible either to release said moldings from the fiber-reinforced plastic of the shaped body and to use them for further injection molding cycles or to use them as lost moldings by forming the outer skin of the fiber-reinforced plastic of the shaped body. The method is particularly suitable for the production of moldings in the form of structural components and / or surface components and / or visible carbon components on vehicles.
Gelöst wird die gestellte Aufgabe fernerhin durch die in Patentanspruch 9 widergegebene Vorrichtung zur Durchführung des Verfahrens.The object is solved further by the reproduced in
Die Erfindung wird nachstehend anhand des in den Zeichnungen schematisch dargestellten Ausführungsbeispiels näher erläutert. Es zeigen:The invention is explained below with reference to the embodiment schematically illustrated in the drawings. Show it:
Das erfindungsgemäße Verfahren zur Herstellung von Formkörpern aus faserverstärkten Kunststoffen zeichnet sich dadurch aus, dass gemäß den
Im Anschluss daran wird das Faser-Halbzeug
Dem luftdicht umschlossenen Faser-Halbzeug
Ist dies geschehen und sind besagte Evakuierungsleitungen wieder geschlossen, wird das in
Nunmehr kann die Injektion eines Matrixwerkstoffes
Wie dabei insbesondere den
Danach ist es angezeigt, einen im Hinblick auf den Injektionsdruck „P1” höheren Gegendruck „P2” gegen die nach außen gewölbte flexible Membran
Ist das Faser-Halbzeug
Ist der Matrixwerkstoff
Wie bereits oben ausgeführt, können die Formteile
BezugszeichenlisteLIST OF REFERENCE NUMBERS
- 11
- Faser-HalbzeugFiber semis
- 22
- Preformpreform
- 33
- Einzellagenindividual layers
- 44
- Kavitätcavity
- 55
- Formteilmolding
- 66
- Formteilmolding
- 77
- Formteilmolding
- 88th
- Formteilmolding
- 99
- flexible Membranflexible membrane
- 1010
- Injektionsleitunginjection line
- 1111
- Spritzgießforminjection mold
- 1212
- Befestigungsmittelfastener
- 1313
- WerkzeugunterteilTool part
- 1414
- WerkzeugoberteilUpper die
- 1515
- WerkzeugoberteilUpper die
- 1616
- Druckkammerpressure chamber
- 1717
- Distanzhalterspacer
- 1818
- Beabstandungspacing
- 1919
- MatrixwerkstoffMatrix material
- 2020
- Formkörpermoldings
- „P1”"P 1 "
- Injektionsdruckinjection pressure
- „P2”"P 2 "
- Gegendruckbackpressure
ZITATE ENTHALTEN IN DER BESCHREIBUNG QUOTES 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 of the documents listed by the applicant has been generated automatically and is included solely for the better information of the reader. The list is not part of the German patent or utility model application. The DPMA assumes no liability for any errors or omissions.
Zitierte PatentliteraturCited patent literature
- WO 2010/118923 A2 [0003, 0003] WO 2010/118923 A2 [0003, 0003]
- EP 1013409 A2 [0004] EP 1013409 A2 [0004]
- DE 200116817 U1 [0004] DE 200116817 U1 [0004]
- DE 102005011977 A1 [0004] DE 102005011977 A1 [0004]
- DE 19906124 A1 [0004] DE 19906124 A1 [0004]
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE201110008759 DE102011008759A1 (en) | 2011-01-17 | 2011-01-17 | Method for manufacturing e.g. structure component that is utilized in vehicle, involves forming fiber semi-finished material, curing fluent matrix material by heating, and removing mold body from injection mold |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE201110008759 DE102011008759A1 (en) | 2011-01-17 | 2011-01-17 | Method for manufacturing e.g. structure component that is utilized in vehicle, involves forming fiber semi-finished material, curing fluent matrix material by heating, and removing mold body from injection mold |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE102011008759A1 true DE102011008759A1 (en) | 2012-07-19 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE201110008759 Pending DE102011008759A1 (en) | 2011-01-17 | 2011-01-17 | Method for manufacturing e.g. structure component that is utilized in vehicle, involves forming fiber semi-finished material, curing fluent matrix material by heating, and removing mold body from injection mold |
Country Status (1)
| Country | Link |
|---|---|
| DE (1) | DE102011008759A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102012010469A1 (en) * | 2012-05-26 | 2013-11-28 | Daimler Ag | Method for manufacturing fiber reinforced component, involves arranging pre-mold semi-finished material with moderate temperature shell elements in tool to be provided with plastic material, where fiber reinforced component is cured |
| DE102013016027B4 (en) | 2013-09-26 | 2020-08-06 | Audi Ag | Device for producing a fiber-reinforced plastic component |
| CN114953511A (en) * | 2022-07-28 | 2022-08-30 | 中南大学 | Rapid forming method and device for carbon fiber reinforced thermoplastic composite material-metal composite component |
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|---|---|---|---|---|
| EP0415870A2 (en) * | 1989-08-28 | 1991-03-06 | United Technologies Corporation | Preform liners for resin transfer molding |
| DE19853709C1 (en) * | 1998-11-20 | 2000-02-10 | Deutsch Zentr Luft & Raumfahrt | Resin injection equipment for production of fiber reinforced plastic products uses a common line instead of separate lines for gas evacuation and resin injection |
| EP1013409A2 (en) | 1998-12-23 | 2000-06-28 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Method and apparatus for manufacturing fibre reinforced composite parts |
| DE19906124A1 (en) | 1999-02-13 | 2000-09-28 | Klaus Pimiskern | Resin transfer molding of composites involves leaving mold slightly open during injection and then applying high pressure with an airbag |
| DE20116817U1 (en) | 2001-10-17 | 2002-01-24 | Rapphahn, Horst, 83024 Rosenheim | Device for the production of plastic components |
| DE10232278A1 (en) * | 2001-07-18 | 2003-02-06 | Klaus Wenderoth | Production of moldings comprises injecting resin or molding composition into molds which are compressed by liquid which surrounds them |
| DE102004025704A1 (en) * | 2004-05-26 | 2005-12-15 | Kiersch Composite Gmbh | Fiber reinforced plastic component manufacture involves compressing resin impregnated fiber composite between mold, upper films and pressurized membrane while heat transfer fluids flows between film and membrane |
| DE102005011977A1 (en) | 2005-03-14 | 2006-02-16 | Daimlerchrysler Ag | Resin infusion system for manufacturing reinforced plastic parts using fiber preforms comprises gas impermeable thermoplastic elastomer membrane forming a closed chamber around fiber preform |
| WO2009036473A2 (en) * | 2007-09-13 | 2009-03-19 | The Boeing Company | Method and apparatus for resin transfer molding composite parts |
| WO2010118923A2 (en) | 2009-04-15 | 2010-10-21 | Airbus Operations Gmbh | Producing a composite component |
-
2011
- 2011-01-17 DE DE201110008759 patent/DE102011008759A1/en active Pending
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0415870A2 (en) * | 1989-08-28 | 1991-03-06 | United Technologies Corporation | Preform liners for resin transfer molding |
| DE19853709C1 (en) * | 1998-11-20 | 2000-02-10 | Deutsch Zentr Luft & Raumfahrt | Resin injection equipment for production of fiber reinforced plastic products uses a common line instead of separate lines for gas evacuation and resin injection |
| EP1013409A2 (en) | 1998-12-23 | 2000-06-28 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Method and apparatus for manufacturing fibre reinforced composite parts |
| DE19906124A1 (en) | 1999-02-13 | 2000-09-28 | Klaus Pimiskern | Resin transfer molding of composites involves leaving mold slightly open during injection and then applying high pressure with an airbag |
| DE10232278A1 (en) * | 2001-07-18 | 2003-02-06 | Klaus Wenderoth | Production of moldings comprises injecting resin or molding composition into molds which are compressed by liquid which surrounds them |
| DE20116817U1 (en) | 2001-10-17 | 2002-01-24 | Rapphahn, Horst, 83024 Rosenheim | Device for the production of plastic components |
| DE102004025704A1 (en) * | 2004-05-26 | 2005-12-15 | Kiersch Composite Gmbh | Fiber reinforced plastic component manufacture involves compressing resin impregnated fiber composite between mold, upper films and pressurized membrane while heat transfer fluids flows between film and membrane |
| DE102005011977A1 (en) | 2005-03-14 | 2006-02-16 | Daimlerchrysler Ag | Resin infusion system for manufacturing reinforced plastic parts using fiber preforms comprises gas impermeable thermoplastic elastomer membrane forming a closed chamber around fiber preform |
| WO2009036473A2 (en) * | 2007-09-13 | 2009-03-19 | The Boeing Company | Method and apparatus for resin transfer molding composite parts |
| WO2010118923A2 (en) | 2009-04-15 | 2010-10-21 | Airbus Operations Gmbh | Producing a composite component |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102012010469A1 (en) * | 2012-05-26 | 2013-11-28 | Daimler Ag | Method for manufacturing fiber reinforced component, involves arranging pre-mold semi-finished material with moderate temperature shell elements in tool to be provided with plastic material, where fiber reinforced component is cured |
| DE102012010469B4 (en) * | 2012-05-26 | 2017-10-05 | Daimler Ag | Process for the production of fiber-reinforced components |
| DE102013016027B4 (en) | 2013-09-26 | 2020-08-06 | Audi Ag | Device for producing a fiber-reinforced plastic component |
| CN114953511A (en) * | 2022-07-28 | 2022-08-30 | 中南大学 | Rapid forming method and device for carbon fiber reinforced thermoplastic composite material-metal composite component |
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