DE4202589C1 - Prodn. of integral sandwich structure from preformed textile - comprises impregnating core yarns with hardenable plastic and placing between rigid baseplate and covering plate - Google Patents

Prodn. of integral sandwich structure from preformed textile - comprises impregnating core yarns with hardenable plastic and placing between rigid baseplate and covering plate

Info

Publication number
DE4202589C1
DE4202589C1 DE19924202589 DE4202589A DE4202589C1 DE 4202589 C1 DE4202589 C1 DE 4202589C1 DE 19924202589 DE19924202589 DE 19924202589 DE 4202589 A DE4202589 A DE 4202589A DE 4202589 C1 DE4202589 C1 DE 4202589C1
Authority
DE
Germany
Prior art keywords
preformed
cover plate
prod
base
sandwich structure
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.)
Expired - Fee Related
Application number
DE19924202589
Other languages
German (de)
Inventor
Hubert 8206 Heufeldmuehle De Karger
Klaus 8022 Gruenwald De Drechsler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Deutsche Aerospace AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Deutsche Aerospace AG filed Critical Deutsche Aerospace AG
Priority to DE19924202589 priority Critical patent/DE4202589C1/en
Application granted granted Critical
Publication of DE4202589C1 publication Critical patent/DE4202589C1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M17/00Producing multi-layer textile fabrics
    • D06M17/04Producing multi-layer textile fabrics by applying synthetic resins as adhesives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/08Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different fibres

Abstract

A process for producing an integral sandwich structure out of a preformed textile prod. in which covering layers made of a yarn system are joined via core yarns into a hollow fibre structure. The structure is impregnated with a hardenable plastic and the preformed prod. is subsequently hardened. Before the hardening process, the preformed prod. is positioned between a rigid baseplate and a rigid covering plate. A pressure force is then applied until the base and covering plates have been bonded to the associated covering layers of the preformed prod.. The distance between the plates is altered until a specific alignment of the core yarns has been achieved and the subsequent hardening of the preformed prod. takes place between the plates. ADVANTAGE - The process ensures that the finished sandwich structure is free of strong core yarn curves which diminish the required sandwich height.

Description

Die Erfindung betrifft ein Verfahren zur Herstellung einer integralen Sandwichstruktur aus einem textilen Vorformling gemäß dem Oberbegriff des Patentanspruchs 1.The invention relates to a method for producing an integral Sandwich structure from a textile preform according to the generic term of claim 1.

Nach einer Niederschrift zu einem Vortrag "Fertigung und mechanische Eigenschaften von Faserverbundwerkstoffen mit textilen Vorformlingen" auf der 23. AVK-Tagung Mainz im November 1990 sind mit solchen als Abstandsgewebe bezeichneten Vorformlingen, bei denen die Kernfäden des Fadensystems nach der Imprägnierung den Sandwichkern bilden, Sandwichhöhen bis 15 mm möglich. Dabei kommt es selbstverständlich darauf an, daß der Abstand der Decklagen und damit die Sandwichhöhe auch nach dem Imprägnieren des Vorformlings erhalten bleibt. Erfahrungsgemäß kann nämlich beispielsweise das zur gleichmäßigen Durchtränkung mit dem warmhärtbaren Kunststoff bevorzugte Quetschwalzen des Vorformlings zur Folge haben, daß danach die Kernfäden sich nicht wieder in ihre ursprüngliche Lage aufrichten, also stark gekrümmt bleiben. Dieser Orientierungsmangel der Kernfäden nach dem Imprägnieren zeigt sich vor allem bei Kernstrukturen, bei denen die Kernfäden im wesentlichen senkrecht zu den Decklagen, d. h. in Lastrichtung gestreckt verlaufen, sollen.After a transcript of a lecture "Manufacturing and mechanical Properties of fiber composite materials with textile preforms " at the 23rd AVK conference in Mainz in November 1990 are such as Spacer fabrics designated preforms in which the core threads of the Thread system form the sandwich core after impregnation, Sandwich heights up to 15 mm possible. It comes naturally on the fact that the distance between the top layers and thus the sandwich height also remains after impregnation of the preform. According to experience can namely, for example, for uniform impregnation with the thermosetting plastic preferred squeeze rollers of the preform Consequence that after that the core threads do not come back into their Raise the original position, so stay strongly curved. This A lack of orientation of the core threads after impregnation is evident especially with core structures where the core threads are essentially perpendicular to the top layers, d. H. stretched in the load direction run, should.

Der Erfindung liegt daher die Aufgabe zugrunde, bei einem Verfahren der eingangs genannten Art sicherzustellen, daß nach dem Aushärten des Vorformlings die Sandwichstruktur frei von die gewünschte Sandwichhöhe mindernden, starken Krümmungen der Kernfäden ist.The invention is therefore based on the object in a method of ensure that after curing the Preform the sandwich structure free of the desired sandwich height reducing, strong curvatures of the core threads.

Diese Aufgabe ist mit den kennzeichnenden Merkmalen des Patentanspruchs 1 gelöst. Die Erfindung macht sich demnach die infolge der Imprägnierung vorhandene Haftwirkung des Vorformlings im durch bloßen Druck erzielten vollen Flächenkontakt seiner beiden Deckflächen mit einer Grund- und Deckplatte zunutze. Aufgrund dieser Haftwirkung, vorzugsweise nach nur auf die Deckplatte ausgeübtem Preßdruck, ist lediglich eine Distanz­ änderung der Deckflächen durch eine entsprechende Relativbewegung zwischen der Grund- und Deckplatte durchzuführen, je nach gewünschter Orientierung der Kernfäden bis zu deren Streckung. Diese Distanzänderung wird bis zur vollständigen Aushärtung des Vorformlings aufrechterhalten. Die anschließende Trennung des Vorformlings von der Grund- und Deckplatte ist problemlos, insbesondere bei der Verwendung eines Trennmittels an deren Kontaktflächen.This task is with the characterizing features of the claim 1 solved. The invention therefore makes itself due to the impregnation existing preform adhesion in the pressure obtained full surface contact of its two cover surfaces with a base and Use the cover plate. Because of this adhesive effect, preferably after only pressing pressure exerted on the cover plate is only a distance change of the top surfaces by a corresponding relative movement between the base and cover plate, depending on the desired  Orientation of the core threads until they are stretched. This change in distance is maintained until the preform is fully cured. The subsequent separation of the preform from the basic and Cover plate is easy, especially when using a Release agents on their contact surfaces.

Nachfolgend wird die Erfindung anhand eines Ausführungsbeispiels weiter erläutert. Dabei zeigt die Zeichnung inThe invention will be further elucidated below using an exemplary embodiment explained. The drawing shows in

Fig. 1 einen Abschnitt eines sog. Abstandsgewebes, Fig. 1 shows a portion of a so-called. Spacer fabric,

Fig. 2 das Abstandsgewebe gemäß Fig. 1 zwischen zwei distanzveränderbaren Platten. Fig. 2, the spacer fabric of FIG. 1 between two distance-variable plates.

Bei dem dargestellten Abstandsgewebe handelt es sich um einen textilen Vorformling, bei welchem aus einem (z. B. Glasfaser-)Fadensystem zwei Decklagen 1 über Kernfäden 2 zu einem hohlen Faserwerk vereinigt sind. Um daraus eine integrale Sandwichstruktur herzustellen, erfolgt eine Imprägnierung mit einem vorzugsweise warmhärtbaren Kunststoff (z. B. Kunstharz). Das Imprägnieren beispielsweise mittels Quetschwalzen zur gleichmäßigen Verteilung des Kunststoffes im Vorformling hat gemäß Fig. 1 zwangsläufig eine Krümmung der Kernfäden 2 im Sinne einer Minderung des Abstandes zwischen den beiden Decklagen 1 zur Folge. Damit hätte gegenüber dem Abstandsgewebe bzw. Vorformling vor der Imprägnierung die Sandwichstruktur nicht nur einen Dickenschwund, sondern es wäre auch nicht die bei weitestmöglich gestreckten Kernfäden 2 (Fig. 2) maximale Festigkeit und Steifigkeit erreicht. Dieser Nachteil wird durch die Erfindung dadurch beseitigt, daß gemäß Fig. 2 der imprägnierte Vorformling vor dem Aushärten zwischen einer steifen Grund- und Deckplatte 3 bzw. 4 mit seinen Decklagen 1 in Flächendeckung einerseits mit der Grundplatte 3 und andererseits mit der Deckplatte 4 positioniert wird. Dann wird Preßdruck vorzugsweise auf die gegenüber der Grundplatte 3 mittels einer Spindel- oder hydraulischen Presse bewegbare Deckplatte 4 ausgeübt, bis eine Bindung der Grund- und Deckplatte 3 bzw. 4 durch den unausgehärteten Kunststoff des Vorformlings an die zugeordnete Decklage 1 sichergestellt ist; hierzu ist erfahrungsgemäß ein Druck von etwa 1 bar über einige (z. B. fünf) Sekunden ausreichend. Anschließend wird durch entsprechende Bewegung der Deckplatte 4 (durch Hochfahren des Pressestempels) deren Abstand zur Grundplatte 3 und damit der Abstand zwischen den beiden Decklagen 1 bis zur gewünschten Ausrichtung der Kernfäden 2 gegenüber den Decklagen 1 verändert, d. h. bis die größtmögliche Streckung der Kernfäden 2 gegenüber den Decklagen 1 erreicht ist. Selbstverständlich könnte auch, wenn eine Sandwichstruktur unterschiedlicher Dicke bzw. mit zueinander schiefen Decklagen 1 gefordert wird, entsprechend nur eine teilweise Streckung der Kernfäden 2 bewirkt werden. Diese Ausrichtung der Kernfäden 2 wird dabei bis zur Aushärtung des Vorformlings (z. B. in einem Wärmeschrank) aufrechterhalten, d. h. dessen Trennung von der Grund- und Deckplatte 3 bzw. 4 erfolgt erst nach dem Aushärten in üblicher Weise, beispielsweise durch Aufkeilen mittels eines flachgeschliffenen Stemmeisens.The spacer fabric shown is a textile preform in which two cover layers 1 are combined from a (eg glass fiber) thread system via core threads 2 to form a hollow fiber structure. To produce an integral sandwich structure, it is impregnated with a preferably thermosetting plastic (e.g. synthetic resin). The impregnation, for example by means of squeeze rollers for uniform distribution of the plastic in the preform, inevitably results in a curvature of the core threads 2 in accordance with FIG. 1 in the sense of a reduction in the distance between the two cover layers 1 . Thus, compared to the spacer fabric or preform before the impregnation, the sandwich structure would not only have a loss of thickness, but it would also not have achieved the maximum strength and rigidity with the core threads 2 stretched as far as possible ( FIG. 2). This disadvantage is eliminated by the invention in that, according to FIG. 2, the impregnated preform is positioned before hardening between a rigid base and cover plate 3 or 4 with its cover layers 1 in surface coverage on the one hand with the base plate 3 and on the other hand with the cover plate 4 . Then pressing pressure is preferably exerted on the cover plate 4 , which is movable relative to the base plate 3 by means of a spindle or hydraulic press, until a bond between the base plate and cover plate 3 or 4 is ensured by the uncured plastic of the preform to the associated cover layer 1 ; Experience has shown that a pressure of about 1 bar over a few (e.g. five) seconds is sufficient. Then, by appropriate movement of the cover plate 4 (by raising the press stamp), its distance from the base plate 3 and thus the distance between the two cover layers 1 up to the desired orientation of the core threads 2 relative to the cover layers 1 is changed, that is, until the greatest possible stretching of the core threads 2 relative to one another the top layers 1 is reached. Of course, if a sandwich structure of different thickness or with inclined cover layers 1 is required, only a partial stretching of the core threads 2 could be effected accordingly. This orientation of the core threads 2 is maintained until the preform has hardened (e.g. in a heating cabinet), ie its separation from the base plate and cover plate 3 or 4 takes place in the usual way only after hardening, for example by wedging by means of a flat ground chisel.

Claims (3)

1. Verfahren zur Herstellung einer integralen Sandwichstruktur aus einem textilen Vorformling, bei dem aus einem Fadensystem gebildete Decklagen über Kernfäden zu einem hohlen Faserwerk vereinigt sind, durch Imprägnieren mit einem härtbaren Kunststoff und anschließendes Aushärten des Vorformlings, dadurch gekennzeichnet, daß der imprägnierte Vorformling vor dem Aushärten zwischen einer steifen Grund- und Deckplatte (3 bzw. 4) mit seinen Decklagen (1) in Flächendeckung einerseits mit der Grundplatte (3) und andererseits mit der Deckplatte (4) positioniert und dann Preßdruck bis zu einer durch den unausgehärteten Kunststoff bewirkten Bindung der Grund- und Deckplatte (3 bzw. 4) an die zugeordnete Decklage (1) ausgeübt wird, worauf der Abstand zwischen der Grund- und Deckplatte (3 bzw. 4) bis zu einer bestimmten Ausrichtung der Kernfäden (2) verändert wird und die anschließende Aushärtung des Vorformlings zwischen der Grund- und Deckplatte (3 bzw. 4) erfolgt.1. A method for producing an integral sandwich structure from a textile preform, in which cover layers formed from a thread system are combined via core threads to form a hollow fiber material, by impregnation with a hardenable plastic and subsequent hardening of the preform, characterized in that the impregnated preform before Curing between a rigid base and cover plate ( 3 or 4 ) with its cover layers ( 1 ) in surface coverage on the one hand with the base plate ( 3 ) and on the other hand with the cover plate ( 4 ) and then pressing pressure up to a bond caused by the uncured plastic the base and cover plate ( 3 or 4 ) is exerted on the associated cover layer ( 1 ), whereupon the distance between the base and cover plate ( 3 or 4 ) is changed up to a certain orientation of the core threads ( 2 ) and the Subsequent curing of the preform between the base and cover plate ( 3 or 4 ) olgt. 2. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß der Preßdruck auf die Deckplatte (4) ausgeübt wird.2. The method according to claim 1, characterized in that the pressing pressure is exerted on the cover plate ( 4 ). 3. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß der Abstand zwischen der Grund- und Deckplatte (3 bzw. 4) bis zur weitgehenden Streckung der Kernfäden (2) vergrößert wird.3. The method according to claim 1, characterized in that the distance between the base and cover plate ( 3 or 4 ) is increased to the extensive extension of the core threads ( 2 ).
DE19924202589 1992-01-30 1992-01-30 Prodn. of integral sandwich structure from preformed textile - comprises impregnating core yarns with hardenable plastic and placing between rigid baseplate and covering plate Expired - Fee Related DE4202589C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19924202589 DE4202589C1 (en) 1992-01-30 1992-01-30 Prodn. of integral sandwich structure from preformed textile - comprises impregnating core yarns with hardenable plastic and placing between rigid baseplate and covering plate

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Application Number Priority Date Filing Date Title
DE19924202589 DE4202589C1 (en) 1992-01-30 1992-01-30 Prodn. of integral sandwich structure from preformed textile - comprises impregnating core yarns with hardenable plastic and placing between rigid baseplate and covering plate

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4327022A1 (en) * 1993-08-12 1995-02-16 Daimler Benz Ag Element for the absorption of impact energy, especially for vehicles
DE4340346A1 (en) * 1993-11-26 1995-06-01 Audi Ag Application of plastics foam for vehicle filter
DE4425828A1 (en) * 1994-07-21 1996-01-25 Daimler Benz Aerospace Ag Sandwich=shaped structural element
DE19608239A1 (en) * 1996-03-04 1997-09-11 Bayerische Motoren Werke Ag Inner lining for motor vehicle passenger compartment
EP1744077A1 (en) 2005-07-12 2007-01-17 Jacob Composite GmbH Hybrid connecting element
DE102013217990A1 (en) 2013-09-09 2015-03-12 hollomet GmbH damping body

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3723681A1 (en) * 1987-07-17 1989-01-26 Vorwerk Co Interholding VELOURS FABRIC-BASED COMPONENT AND METHOD FOR THE PRODUCTION THEREOF
DE3742400A1 (en) * 1987-12-15 1989-07-06 Mehler Vario System Gmbh SANDWICH LIGHTWEIGHT MATERIAL AND METHOD FOR THE PRODUCTION THEREOF

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3723681A1 (en) * 1987-07-17 1989-01-26 Vorwerk Co Interholding VELOURS FABRIC-BASED COMPONENT AND METHOD FOR THE PRODUCTION THEREOF
DE3742400A1 (en) * 1987-12-15 1989-07-06 Mehler Vario System Gmbh SANDWICH LIGHTWEIGHT MATERIAL AND METHOD FOR THE PRODUCTION THEREOF

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
DE-Z: Kunststoffe 79, 1989, Heft 11, S. 1228-1230 *
DE-Z: Kunststoffe 80, 1990, Heft 9, S. 1003-1007 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4327022A1 (en) * 1993-08-12 1995-02-16 Daimler Benz Ag Element for the absorption of impact energy, especially for vehicles
DE4340346A1 (en) * 1993-11-26 1995-06-01 Audi Ag Application of plastics foam for vehicle filter
DE4425828A1 (en) * 1994-07-21 1996-01-25 Daimler Benz Aerospace Ag Sandwich=shaped structural element
DE19608239A1 (en) * 1996-03-04 1997-09-11 Bayerische Motoren Werke Ag Inner lining for motor vehicle passenger compartment
EP1744077A1 (en) 2005-07-12 2007-01-17 Jacob Composite GmbH Hybrid connecting element
US7654368B2 (en) 2005-07-12 2010-02-02 Jacob Composite Gmbh Hybrid fastener
DE102013217990A1 (en) 2013-09-09 2015-03-12 hollomet GmbH damping body

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Owner name: DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 80804 M

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Owner name: DAIMLERCHRYSLER AEROSPACE AKTIENGESELLSCHAFT, 8099

8320 Willingness to grant licenses declared (paragraph 23)
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Owner name: DAIMLERCHRYSLER AEROSPACE AG, 85521 OTTOBRUNN, DE

8339 Ceased/non-payment of the annual fee