DE102005011977A1 - Resin infusion system for manufacturing reinforced plastic parts using fiber preforms comprises gas impermeable thermoplastic elastomer membrane forming a closed chamber around fiber preform - Google Patents
Resin infusion system for manufacturing reinforced plastic parts using fiber preforms comprises gas impermeable thermoplastic elastomer membrane forming a closed chamber around fiber preform Download PDFInfo
- Publication number
- DE102005011977A1 DE102005011977A1 DE200510011977 DE102005011977A DE102005011977A1 DE 102005011977 A1 DE102005011977 A1 DE 102005011977A1 DE 200510011977 DE200510011977 DE 200510011977 DE 102005011977 A DE102005011977 A DE 102005011977A DE 102005011977 A1 DE102005011977 A1 DE 102005011977A1
- Authority
- DE
- Germany
- Prior art keywords
- membrane
- fiber
- matrix material
- resin
- tool
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
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
- B29C70/44—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
- B29C70/443—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 and impregnating by vacuum or injection
-
- 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
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
- B29C43/3642—Bags, bleeder sheets or cauls for isostatic pressing
- B29C2043/3647—Membranes, diaphragms
-
- 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
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
- B29C43/3642—Bags, bleeder sheets or cauls for isostatic pressing
Abstract
Description
Die
Erfindung betrifft eine Vorrichtung zur Herstellung eines faserverstärkten Kunststoff-Bauteils
aus einem Faser-Halbzeug (Preform) mittels Infusion eines fließfähigen Matrix-Materials nach dem Oberbegriff
des Anspruchs 1, wie sie beispielsweise aus der
Die
Bei
dem aus der
Als
Materialien für
die Vakuumfolie sind unterschiedliche Werkstoffe bekannt. So schlägt beispielsweise
die
Weiterhin
schlägt
die
Schließlich ist es bekannt, Vakuumfolien aus Silikon zu verwenden. Solche Folien wurden bisher vor allem bei der Herstellung faserverstärkter Bauteile für die Luftfahrtindustrie eingesetzt. Dieser Werkstoff zeigt zwar eine gute thermische Resistenz, jedoch beeinträchtigen Spuren von Silikon, die dem fertig geformten Bauteil eventuell anhaften, bei einer nachfolgenden Lackierung das Haftverhalten der Lacke, weswegen ein Einschleppen von Silikon in Lackier-Anlagen unbedingt vermieden werden muss. Die Verwendung von Vakuumfolien aus Silikon kommt somit bei der Herstellung von Bauteilen, die anschließend lackiert werden sollen, nicht in Frage.Finally is it is known to use silicone vacuum foils. Such slides have so far mainly been used in the production of fiber-reinforced components for the Aviation industry used. Although this material shows a good thermal resistance, but affect traces of silicone, which may adhere to the finished molded component, in a subsequent Painting the adhesion of the paints, so a lugging of silicone in paint shops absolutely must be avoided. The Use of vacuum films made of silicone thus comes in the production of components that subsequently to be painted, out of the question.
Der
Erfindung liegt daher die Aufgabe zugrunde, die aus der
Die Aufgabe wird erfindungsgemäß durch die Merkmale des Anspruchs 1 gelöst.The The object is achieved by the Characteristics of claim 1 solved.
Danach wird als Vakuumfolie eine Membran aus einem thermoplastischen Elastomer verwendet. Thermoplastische Elastomere weisen eine gute Temperaturbeständigkeit bei den erhöhten Prozesstemperaturen von bis zu 150° C auf, die für die Verarbeitung vieler Harzsysteme (insbesondere von Epoxidharzen) notwendig sind. Weiterhin eignen sich diese Werkstoffe aufgrund ihrer Festigkeit und ihrer hohen Reißdehnung auch und insbesondere zur Herstellung von komplexen Bauteilen mittels Resin-Infusion-Verfahren. Hierzu wird eine vorgeformte Membran aus thermoplastischem Elastomer hergestellt, die der Geometrie des zu fertigenden Bauteils angepasst ist und die die in herkömmlichen Vorrichtungen verwendete Vakuumfolie ersetzt. Wegen der hohen Elastizität der Membran, ihrer Wärmebeständigkeit und ihrer Unempfindlichkeit gegenüber Epoxidharzen können Lecks in der Membran wirksam vermieden werden. Dadurch wird die Gefahr von Porositäten der fertigen Bauteile – die zu Ausschuss führen – wesentlich reduziert.Thereafter, a membrane of a thermoplastic elastomer is used as a vacuum film. Thermoplastic elastomers have good temperature resistance at elevated process temperatures of up to 150 ° C, which are necessary for the processing of many resin systems (especially epoxy resins). Furthermore, these materials are due to their strength and high elongation at break and in particular for the production of complex components by resin infusion process. For this purpose, a preformed membrane made of thermoplastic elastomer, which is adapted to the geometry of the component to be manufactured and the ver in conventional devices used replaced vacuum film. Due to the high elasticity of the membrane, its heat resistance and its insensitivity to epoxy resins leaks in the membrane can be effectively avoided. As a result, the risk of porosities of the finished components - which lead to rejects - significantly reduced.
Weiterhin zeichnen sich thermoplastische Elastomere durch ein sehr gutes Trennverhalten gegenüber Epoxidharz aus, so dass das Ablösen der Membran vom fertigen Bauteil problemlos und unaufwendig möglich ist. Dies führt zu einer wesentlichen Reduktion des (manuellen) Aufwands bei der Vorbereitung und beim Entformen der Bauteile und bringt daher Zeit- und Kostenvorteile mit sich. Außerdem kann Verbrauchsmaterial (Trennfolie, Sprühkleber ...) gespart werden. Aufgrund ihrer hohen Festigkeit und ihres guten Trennverhaltens kann die Membran weiterhin – im Unterschied zu herkömmlicher Vakuumfolie – mehrfach wiederverwendet werden.Farther Thermoplastic elastomers are characterized by a very good separation behavior across from Made of epoxy resin, allowing the peeling the membrane of the finished component is easily and inexpensively possible. this leads to to a substantial reduction of the (manual) effort in the Preparation and demoulding of the components and therefore brings and cost advantages. In addition, can Consumables (release film, spray adhesive ...) can be saved. Due to their high strength and good separation behavior the membrane can continue - in Difference to conventional Vacuum foil - several times be reused.
Als Werkstoffe für die Membran haben sich thermoplastische Vulkanisate (TPV) aus der Familie der thermoplastischen Elastomere als besonders gut geeignet erwiesen. Gute Ergebnisse wurden insbesondere mit TPVs erzielt, die unter dem Namen „Santoprene" (Hersteller: ExxonMobil Chemical) bzw. „Sarlink" (Hersteller: DSM) auf dem Markt sind. Vorteilhaft an diesen Werkstoffen ist die geringe Rückstellneigung nach dem Umformen. Dies ist besonders wichtig bei der Herstellung von Bauteilen mit sehr komplexer Geometrie, weil dadurch sichergestellt wird, dass die Membran die Bauteilform in allen Phasen des Prozesses beibehält (z.B. auch bei Ofenhärtung bei 120° C); dadurch kann gewährleistet werden, dass sich auch in Bereichen enger Radien auf dem Bauteil keine Harzansammlungen bilden, die ansonsten zu Ausschussteilen führen können. Wie in Versuchen ermittelt wurde, gewährleisten die erwähnten TPVs diese Formbeständigkeit bis ca. 150° C.When Materials for The membrane has become thermoplastic vulcanizates (TPV) from the Family of thermoplastic elastomers are particularly well suited proved. Good results have been achieved especially with TPVs, under the name "Santoprene" (manufacturer: ExxonMobil Chemical) or "Sarlink" (manufacturer: DSM) are in the market. The advantage of these materials is the low Reset tilt after forming. This is especially important in the production of components with very complex geometry, because it ensures That will make the membrane the component shape in all phases of the process maintains (For example, in oven hardening at 120 ° C); this can be guaranteed be that even in areas of narrow radii on the component do not form accumulations of resin, which otherwise become rejects to lead can. As determined in tests, the mentioned TPVs ensure this dimensional stability up to approx. 150 ° C
Die erfindungsgemäße Vorrichtung mit der Membran aus thermoplastischem Elastomer eignet sich insbesondere zur Herstellung faserverstärkter Außenbeplankungsteile für den Fahrzeugbau. Diese Teile zeichnen sich u.a. durch komplexe Formgebung, Hinterschneidungen, Variationen in der Bauteildicke, steile Stufen, enge Radien etc. aus und stellen daher hohe Ansprüche an den Herstellprozess. Weiterhin müssen die Teile – als sichtbare Außenhautteile – hohen Anforderungen in Bezug auf ihre Oberflächenqualität genügen; das Herstellungsverfahren muss somit die Erzeugung von glatten, gleichförmig gekrümmten Oberflächen (sogenannten „Class-A-Oberflächen") ermöglichen, die außerdem ein gutes Anhaften von Lacken gewährleisten. Die erfindungsgemäße Vorrichtung mit der wiederverwendbaren Membran aus thermoplastischem Elastomer ermöglicht eine prozesssichere Herstellung dieser komplexen Teile in hoher Qualität.The inventive device with the membrane of thermoplastic elastomer is particularly suitable for producing fiber-reinforced outer planking parts for the Vehicle construction. These parts are u.a. by complex shaping, Undercuts, variations in component thickness, steep steps, narrow radii etc. and therefore make high demands on the Manufacturing process. Continue to have the parts - as visible outer skin parts - high Requirements with regard to their surface quality are sufficient; the manufacturing process thus must enable the production of smooth, uniformly curved surfaces (so-called "class A surfaces"), the one besides ensure good adhesion of paints. The device according to the invention with the reusable thermoplastic elastomer membrane allows one process-reliable production of these complex parts in high quality.
Ein weiterer Vorteil der Verwendung einer Membran aus TPV besteht darin, dass aufgrund des sehr guten Abform-Verhaltens einer solchen Membran unterschiedliche Oberflächenstrukturen (Texturen), die bei der Herstellung der TPV-Membran mit Hilfe des Thermoformens auf der Membran-Oberfläche erzeugt werden, auf die Bauteil-Rückseite übertragen werden können. Insbesondere kann auf diese Weise in lokal begrenzten Anbindungsbereichen der Bauteil-Rückseite eine rauere Oberflächenstruktur generiert werden, um beim späteren Fügen des fertigen Bauteils ein optimales Anhaften von Klebstoff zu erreichen.One Another advantage of using a TPV membrane is that that due to the very good impression behavior of such a membrane different surface structures (Textures) used in the manufacture of the TPV membrane using the Thermoforming can be generated on the membrane surface, on the Transfer component back can be. In particular, this can be done in localized connection areas the component back generates a rougher surface texture to be at later Add the finished component to achieve an optimal adhesion of adhesive.
Vorteilhafte Ausgestaltungen der Erfindung sind den Unteransprüchen und dem Ausführungsbeispiel zu entnehmen. Nachfolgend wird die Erfindung anhand eines in den Zeichnungen dargestellten Ausführungsbeispiels näher erläutert. Dabei zeigen:advantageous Embodiments of the invention are the subclaims and the embodiment refer to. The invention is based on a in the Drawings illustrated embodiment explained in more detail. there demonstrate:
Das
trockene Faser-Halbzeug
Zur
Herstellung des trockenen Faser-Halbzeugs
Anschließend wird
das geformte trockene Faser-Halbzeug
Wie
aus der Schnittdarstellung der
Am
Rand
Zur
Zufuhr des Matrix-Materials (d.h. des flüssigen Harzes) ist eine Zuführungsleitung
Die
Werkzeuginnenseite
Die
Membran
Zur
Herstellung der Membran
Aufgrund
des sehr guten Abform-Verhaltens einer Membran aus TPV können Oberflächenstrukturen
(Texturen), die beim Thermoformen der TPV-Membran auf der Membran-Oberfläche erzeugt wurden,
auf die Bauteil-Rückseite übertragen
werden. Auf diese Weise können
beispielsweise auf der Bauteiloberfläche Gebiete
Da
der Membranwerkstoff sich leicht vom fertigen Bauteil lösen lässt und
außerdem
während des
mehrstündigen
Harzaushärtungszyklus' bei 120° C im Ofen
keine Alterung zeigt, kann eine solche Membran
Der
als Omega-Profil oder Spiralschlauch ausgestaltete Auslass
Ist
die Membran
In
Abhängigkeit
von dem gewählten
Harzsystem kann bereits die Infusion des flüssigen Harzes in den Hohlraum
Nach
Abkühlen
des Werkzeugs
Claims (13)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200510011977 DE102005011977A1 (en) | 2005-03-14 | 2005-03-14 | Resin infusion system for manufacturing reinforced plastic parts using fiber preforms comprises gas impermeable thermoplastic elastomer membrane forming a closed chamber around fiber preform |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200510011977 DE102005011977A1 (en) | 2005-03-14 | 2005-03-14 | Resin infusion system for manufacturing reinforced plastic parts using fiber preforms comprises gas impermeable thermoplastic elastomer membrane forming a closed chamber around fiber preform |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102005011977A1 true DE102005011977A1 (en) | 2006-02-16 |
Family
ID=35668707
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE200510011977 Withdrawn DE102005011977A1 (en) | 2005-03-14 | 2005-03-14 | Resin infusion system for manufacturing reinforced plastic parts using fiber preforms comprises gas impermeable thermoplastic elastomer membrane forming a closed chamber around fiber preform |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE102005011977A1 (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007023229A1 (en) * | 2007-05-18 | 2008-11-20 | Bayerische Motoren Werke Aktiengesellschaft | Apparatus and method for producing a fiber-reinforced plastic component |
WO2009106868A1 (en) * | 2008-02-29 | 2009-09-03 | Victrex Manufacturing Limited | Composite materials |
DE202010001836U1 (en) | 2010-02-02 | 2011-06-09 | DD-Compound UG (haftungsbeschränkt), 49477 | Device for producing a fiber composite component by means of vacuum infusion and suction line |
DE102010018110A1 (en) * | 2010-04-24 | 2011-10-27 | Bema Invest Gmbh | Multi-layer material for use in composite construction for panels and moldings, has carrier layer of consolidated froth, which comprises two side surfaces |
FR2966765A1 (en) * | 2010-10-27 | 2012-05-04 | Modelage Concept | Method for manufacturing mold to realize resin transfer molding light parts, involves arranging punch provided with technical sections on die such that mold is prepared for injection of resin between die and punch |
DE102011008759A1 (en) | 2011-01-17 | 2012-07-19 | Volkswagen Ag | 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 |
WO2015067440A1 (en) * | 2013-11-06 | 2015-05-14 | Airbus Operations Gmbh | Arrangement and method for producing a composite material component |
DE102014111358A1 (en) * | 2014-08-08 | 2016-02-11 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Multi-part vacuum hood |
DE102016106830B3 (en) * | 2016-04-13 | 2017-09-14 | Airbus Operations Gmbh | A support for covering a curable fiber composite material layer, system assembly having such a support, and methods using such a support |
US10046733B2 (en) | 2013-08-27 | 2018-08-14 | Joyson Safety Systems Germany Gmbh | Belt retractor |
US10160172B2 (en) | 2014-08-06 | 2018-12-25 | GM Global Technology Operations LLC | Mechanical interlocking realized through induction heating for polymeric composite repair |
US10589477B2 (en) | 2016-05-02 | 2020-03-17 | GM Global Technology Operations LLC | Cosmetic repair of a thermoplastic carbon fiber composite |
US10611104B2 (en) | 2017-06-15 | 2020-04-07 | GM Global Technology Operations LLC | Heating elements for repair of molding defects for carbon fiber thermoplastic composites |
US10695993B2 (en) | 2016-01-15 | 2020-06-30 | GM Global Technology Operations LLC | In-situ polymerization of polyamides for composite part repair |
DE102019114329A1 (en) * | 2019-05-28 | 2020-12-03 | Airbus Operations Gmbh | Structure and method for manufacturing components from a plastic or composite material, in particular for aircraft and space vehicles, and auxiliary tools |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3703572A (en) * | 1969-11-14 | 1972-11-21 | Plastetics Inc | Method of forming a mold and casting shallow articles therein |
DE69309185T2 (en) * | 1992-08-20 | 1997-07-03 | Gec Alsthom Acb | Press for forming an object from composite material with reinforcing fibers in a polymer matrix |
DE10013409C1 (en) * | 2000-03-17 | 2000-11-23 | Daimler Chrysler Ag | Vacuum injection process for manufacturing fiber reinforced composite products involves evacuating second chamber causing resin to flow into preform in adjacent evacuated first chamber |
US20040145094A1 (en) * | 2003-01-24 | 2004-07-29 | Vec Technology, Inc. | Method of making a composite molded article |
EP1150826B1 (en) * | 1999-02-05 | 2004-10-13 | Goodrich Corporation | Method of controlling the temperature of a vacuum resin infusion process |
DE10326021A1 (en) * | 2003-06-02 | 2004-12-30 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Process for monitoring the production of a component from a fiber-reinforced material |
WO2005016633A1 (en) * | 2003-04-01 | 2005-02-24 | The Boeing Company | Method and system for utilizing low pressure for perforating and consolidating an uncured laminate sheet in one cycle of operation |
-
2005
- 2005-03-14 DE DE200510011977 patent/DE102005011977A1/en not_active Withdrawn
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3703572A (en) * | 1969-11-14 | 1972-11-21 | Plastetics Inc | Method of forming a mold and casting shallow articles therein |
DE69309185T2 (en) * | 1992-08-20 | 1997-07-03 | Gec Alsthom Acb | Press for forming an object from composite material with reinforcing fibers in a polymer matrix |
EP1150826B1 (en) * | 1999-02-05 | 2004-10-13 | Goodrich Corporation | Method of controlling the temperature of a vacuum resin infusion process |
DE10013409C1 (en) * | 2000-03-17 | 2000-11-23 | Daimler Chrysler Ag | Vacuum injection process for manufacturing fiber reinforced composite products involves evacuating second chamber causing resin to flow into preform in adjacent evacuated first chamber |
US20040145094A1 (en) * | 2003-01-24 | 2004-07-29 | Vec Technology, Inc. | Method of making a composite molded article |
WO2005016633A1 (en) * | 2003-04-01 | 2005-02-24 | The Boeing Company | Method and system for utilizing low pressure for perforating and consolidating an uncured laminate sheet in one cycle of operation |
DE10326021A1 (en) * | 2003-06-02 | 2004-12-30 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Process for monitoring the production of a component from a fiber-reinforced material |
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007023229A1 (en) * | 2007-05-18 | 2008-11-20 | Bayerische Motoren Werke Aktiengesellschaft | Apparatus and method for producing a fiber-reinforced plastic component |
WO2009106868A1 (en) * | 2008-02-29 | 2009-09-03 | Victrex Manufacturing Limited | Composite materials |
DE202010001836U1 (en) | 2010-02-02 | 2011-06-09 | DD-Compound UG (haftungsbeschränkt), 49477 | Device for producing a fiber composite component by means of vacuum infusion and suction line |
DE102010018110A1 (en) * | 2010-04-24 | 2011-10-27 | Bema Invest Gmbh | Multi-layer material for use in composite construction for panels and moldings, has carrier layer of consolidated froth, which comprises two side surfaces |
FR2966765A1 (en) * | 2010-10-27 | 2012-05-04 | Modelage Concept | Method for manufacturing mold to realize resin transfer molding light parts, involves arranging punch provided with technical sections on die such that mold is prepared for injection of resin between die and punch |
DE102011008759A1 (en) | 2011-01-17 | 2012-07-19 | Volkswagen Ag | 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 |
US10046733B2 (en) | 2013-08-27 | 2018-08-14 | Joyson Safety Systems Germany Gmbh | Belt retractor |
CN105705320A (en) * | 2013-11-06 | 2016-06-22 | 空中客车作业有限公司 | Arrangement and method for producing a composite material component |
WO2015067440A1 (en) * | 2013-11-06 | 2015-05-14 | Airbus Operations Gmbh | Arrangement and method for producing a composite material component |
US10336015B2 (en) | 2013-11-06 | 2019-07-02 | Airbus Operations Gmbh | Arrangement and method for producing a composite material component |
US10160172B2 (en) | 2014-08-06 | 2018-12-25 | GM Global Technology Operations LLC | Mechanical interlocking realized through induction heating for polymeric composite repair |
DE102014111358A1 (en) * | 2014-08-08 | 2016-02-11 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Multi-part vacuum hood |
DE102014111358B4 (en) | 2014-08-08 | 2018-05-24 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Multi-part vacuum hood |
US10695993B2 (en) | 2016-01-15 | 2020-06-30 | GM Global Technology Operations LLC | In-situ polymerization of polyamides for composite part repair |
DE102016106830B3 (en) * | 2016-04-13 | 2017-09-14 | Airbus Operations Gmbh | A support for covering a curable fiber composite material layer, system assembly having such a support, and methods using such a support |
US10589477B2 (en) | 2016-05-02 | 2020-03-17 | GM Global Technology Operations LLC | Cosmetic repair of a thermoplastic carbon fiber composite |
DE102017109362B4 (en) | 2016-05-02 | 2023-08-10 | GM Global Technology Operations LLC | Cosmetic repair of a thermoplastic carbon fiber composite |
US10611104B2 (en) | 2017-06-15 | 2020-04-07 | GM Global Technology Operations LLC | Heating elements for repair of molding defects for carbon fiber thermoplastic composites |
DE102019114329A1 (en) * | 2019-05-28 | 2020-12-03 | Airbus Operations Gmbh | Structure and method for manufacturing components from a plastic or composite material, in particular for aircraft and space vehicles, and auxiliary tools |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE102005011977A1 (en) | Resin infusion system for manufacturing reinforced plastic parts using fiber preforms comprises gas impermeable thermoplastic elastomer membrane forming a closed chamber around fiber preform | |
EP1727669B1 (en) | Composite part | |
WO2008028973A1 (en) | Method for the production of a sandwich component having a honeycomb core and the sandwich component obtained in this way | |
WO2012010129A2 (en) | Mold for producing fiber-reinforced components | |
DE102010031886A1 (en) | Method for producing a component from a fiber composite material, preform therefor and component | |
EP2227377A1 (en) | Device and method for producing fiber composite components | |
DE102011017007A1 (en) | Method for manufacturing motor car structure components, involves providing fluent state of plastic matrix to mold, impregnating semi-finished fiber material, partial curing of plastic, and demolding of motor car structure component | |
WO2012136235A1 (en) | Composite fibre multi-coat bodywork component and method for producing same | |
EP3408075B1 (en) | Method for producing a component from a fiber composite material | |
DE102011114494A1 (en) | Fiber-reinforced composite component and method for producing such a composite component | |
DE102008009438A1 (en) | Formed part producing method, involves forming cut surface foil according to topography of formed part, applying woven fabric and resin in cutting tool on inside of foil, and taking out finished part after precipitation hardening to tool | |
EP2437921B1 (en) | Method for producing a molded part | |
DE102004060009B4 (en) | Method for producing a laminated body | |
EP2730396B1 (en) | Process for manufacturing a molded part comprising a layer made of a fibre composite plastic layer and a surface coating consisting of a moulded plastic component | |
CN112918565A (en) | Class A parts containing moldable carbon fibers | |
CN112917945A (en) | Method of forming class A parts from moldable carbon fibers | |
DE102016120799B3 (en) | vacuum hood | |
DE102012005505A1 (en) | Method for producing planking unit attached at roof region of motor vehicle, involves forming planking unit of vehicle as fiber-reinforced component by introducing fiber material in cavity of mold | |
DE102010001559A1 (en) | Manufacturing method for a trim part of a vehicle, corresponding device and trim part | |
DE4237834A1 (en) | FRP mouldings are bonded together to produce hollow articles - by wet=on=wet process using basically two dished parts which are vacuum preformed and then bonded together round rims by blow=up pressing. | |
DE102016220806A1 (en) | Method for producing an outer skin component of a vehicle | |
DE102018125716A1 (en) | Device and method for producing a plastic component | |
EP3822060B1 (en) | Method for producing a plastic tank | |
EP3822061B1 (en) | Method for producing a plastic tank | |
DE102016226213A1 (en) | Method for producing a decorative part for a vehicle interior and decorative part |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
OAV | Applicant agreed to the publication of the unexamined application as to paragraph 31 lit. 2 z1 | ||
OM8 | Search report available as to paragraph 43 lit. 1 sentence 1 patent law | ||
8127 | New person/name/address of the applicant |
Owner name: DAIMLERCHRYSLER AG, 70327 STUTTGART, DE |
|
8127 | New person/name/address of the applicant |
Owner name: DAIMLER AG, 70327 STUTTGART, DE |
|
8139 | Disposal/non-payment of the annual fee |