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DE19723827A1 - Multilayer material for panels and manufacturing process - Google Patents

Multilayer material for panels and manufacturing process

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Publication number
DE19723827A1
DE19723827A1 DE19723827A DE19723827A DE19723827A1 DE 19723827 A1 DE19723827 A1 DE 19723827A1 DE 19723827 A DE19723827 A DE 19723827A DE 19723827 A DE19723827 A DE 19723827A DE 19723827 A1 DE19723827 A1 DE 19723827A1
Authority
DE
Germany
Prior art keywords
layer
coating
resin
light
plastic
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Withdrawn
Application number
DE19723827A
Other languages
German (de)
Inventor
Anton Marek
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.)
Individual
Original Assignee
Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to DE19723827A priority Critical patent/DE19723827A1/en
Publication of DE19723827A1 publication Critical patent/DE19723827A1/en
Withdrawn legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered 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
    • B32B5/02—Layered 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B21/00—Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board
    • B32B21/02—Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board the layer being formed of fibres, chips, or particles, e.g. MDF, HDF, OSB, chipboard, particle board, hardboard
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B21/00—Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board
    • B32B21/10—Next to a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/10—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products
    • E04C2/24—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products laminated and composed of materials covered by two or more of groups E04C2/12, E04C2/16, E04C2/20
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/24—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with at least one layer not being coherent before laminating, e.g. made up from granular material sprinkled onto a substrate
    • B32B2037/243—Coating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B2038/0052—Other operations not otherwise provided for
    • B32B2038/0076—Curing, vulcanising, cross-linking
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/02—Coating on the layer surface on fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—Synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2317/00—Animal or vegetable based
    • B32B2317/16—Wood, e.g. woodboard, fibreboard, woodchips

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Wood Science & Technology (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

A multilayer material(10) for forming panels and moulded components comprises a carrier layer(12) with a facing layer (14) and an outer protective layer (16) on one side. The facing layer(14) is a carbon fibre reinforced plastic and the outer layer (16) a light curing plastic. In a process for applying a surface coating to an object a resin layer is applied to the object (12) and a carbon fibre fabric placed onto the resin is impregnated by the latter. After curing the resin to form a facing layer(14) a light curing protective plastic layer(16) is applied and cured with ultraviolet (UV) light.

Description

Die Erfindung betrifft ein Mehrschichtmaterial für Platten und Formkörper insbesondere zur Herstellung von Wänden, Möbeln, Containern und dergleichen, mit einer Trägerschicht, die mindestens einseitig mit einer Deckschicht und einem Überzug beschichtet ist. Mehrschichtmaterialien zur Herstellung beispielsweise von Möbeln, insbesondere Tischen und Schränken sind vielfach in Gebrauch. Als Trägermaterial werden häufig Spanplatten verwendet, die mit einer harten und kratzfesten Deckschicht verklebt werden. Platten aus Naturholz oder Metall erhalten zum Oberflächenschutz einen Lacküberzug. The invention relates in particular to a multilayer material for sheets and moldings for the production of walls, furniture, containers and the like, with a Backing layer, at least on one side with a top layer and a coating is coated. Multilayer materials for the manufacture of furniture, for example, tables and cupboards in particular are widely used. As a carrier material Chipboard is often used, with a hard and scratch-resistant top layer be glued. Panels made of natural wood or metal are given surface protection a paint coat.

Aufgabe der Erfindung ist es, ein Mehrschichtmaterial zu schaffen, das eine hohe Festigkeit aufweist und gleich gut für ebene Platten als auch für Formkörper mit konvexen und konkaven Oberflächen geeignet ist und deren Rauhigkeit zwischen glatt und rauh einstellbar ist, wobei das Mehrschichtmaterial insbesondere von Handwerksbetrieben ohne teuren Apparateaufwand herstellbar sein soll. The object of the invention is to provide a multilayer material which has a high Has strength and equally good for flat plates as well as for molded articles convex and concave surfaces is suitable and their roughness between smooth and is roughly adjustable, the multilayer material in particular from Craft companies should be able to be produced without expensive equipment.

Diese Aufgabe wird bei einem Mehrschichtmaterial der eingangs genannten Art dadurch gelöst, daß die Deckschicht einen kohlefaserverstärkten Kunststoff und der Überzug einen lichtgehärteten Kunststoff aufweist. Vorzugsweise besteht die Deckschicht aus einem ausgehärteten Harz aufweisenden Kohlefasergewebe. Dabei werden vorzugsweise Phenolharze verwendet, obgleich das Mehrschichtmaterial auch auf Epoxydharz- oder Polyesterharzbasis hergestellt werden kann. Der lichthärtende Überzug besteht vorzugsweise aus einem UV-coating. This is achieved in the case of a multilayer material of the type mentioned at the outset solved that the top layer a carbon fiber reinforced plastic and the coating has a light-cured plastic. The cover layer preferably consists of a cured resin-containing carbon fiber fabric. In doing so preferably phenolic resins are used, although the multilayer material is also based on Epoxy resin or polyester resin base can be made. The light-curing The coating preferably consists of a UV coating.

Das neue Mehrschichtmaterial ist äußerst vielseitig einsetzbar. Aufgrund des eingesetzten Kohlefasergewebes werden hohe Festigkeits- und Formsta ilitätswerte erreicht und dies bei geringer Schichtstärke und sehr geringem Gewicht. Der Vorteil des UV-coatings besteht einmal darin, daß dessen Härte eingestellt werden kann, je nachdem, wie lange die UV-Bestrahlung durchgeführt wird und daß die Aushärtezeit des Überzuges insgesamt sehr kurz ist, nämlich nur wenige Sekunden beträgt. Damit eignet sich die Herstellung des Mehrschichtmaterials auch für kleinere Handwerksbetriebe, da keine staubfreien Trocknungsräume benötigt werden, wie dies beim herkömmlichen Lackieren der Fall ist.The new multi-layer material is extremely versatile. Because of the Carbon fiber fabric used have high strength and form stability values achieved and this with a low layer thickness and very low weight. The advantage of  UV coatings consist in the fact that its hardness can be adjusted, depending after how long the UV irradiation is carried out and that the curing time the overall coating is very short, namely only a few seconds. In order to The production of the multilayer material is also suitable for smaller ones Craft businesses, since no dust-free drying rooms are required like this is the case with conventional painting.

Als Trägermaterial kommen beliebige feste Werkstoffe in Frage, wie Metall, Holz, Holzfasermaterial, Preßpappe oder dergleichen. Wenn es auf das geringe Gewicht des Mehrschichtmaterials ankommt, läßt sich vorzugsweise Balsaholz einsetzen. Alternativ ist es jedoch ohne weiteres möglich, als Trägermaterial Hartschaumstoff zu verwenden.Any solid materials, such as metal, wood, Wood fiber material, pressed cardboard or the like. If it is due to the light weight of the When multilayer material arrives, balsa wood can preferably be used. Alternatively  However, it is readily possible to use rigid foam as the carrier material.

Das neuartige Mehrschichtmaterial eignet sich nicht nur zur Herstellung von plattenförmigen Gegenständen, wie kratzfesten Tischplatten, sondern auch z. B. zur Herstellung von Sitzmöbeln, bei denen hohe Festigkeitseigenschaften in Verbindung mit einem geringen Gewicht von Bedeutung sind. Solche Gegenstände, die in gewissen Grenzen elastisch verformbar sind, wie beispielsweise Schwingsessel, erhalten einen entsprechend elastisch eingestellten Überzug, dessen Elastizität allein von der Dauer der UV-Lichtbeaufschlagung bestimmt wird.The new multi-layer material is not only suitable for the production of plate-shaped objects, such as scratch-resistant table tops, but also e.g. B. for Manufacture of seating furniture where high strength properties in connection with light weight are important. Such items, in certain Limits are elastically deformable, such as armchairs, get one accordingly elastic set coating, the elasticity of which depends solely on the duration of the UV light exposure is determined.

Mehrschichtmaterialien, die eine Trägerschicht aufweisen, können mit besonders niedrigem Gewicht hergestellt werden, wenn diese Trägerschicht aus einer Wabenkonstruktion besteht. Die Waben haben trotz geringer Wandstärke ein sehr geringes Raumgewicht, so daß ein Mehrschichtmaterial von mehreren Zentimetern Dicke entsteht, das also einen massiven Eindruck vermittelt, gleichwohl aber unter Erhalt von Festigkeits- und Formstabilitätseigenschaften extrem leicht ist. Multilayer materials that have a backing layer can be particularly useful low weight if this carrier layer is made of a Honeycomb construction. Despite the thin walls, the honeycombs have a very low density, so that a multilayer material of several centimeters thick arises, which gives a massive impression, but still while maintaining Strength and form stability properties is extremely light.  

Die Erfindung betrifft weiterhin ein Verfahren zur Oberflächenbeschichtung von Gegenständen und dieses Verfahren ist dadurch gekennzeichnet, daß auf die Gegenstände eine Harzschicht aufgebracht und in diese ein Kohlefasergewebe eingelegt und mit Harz getränkt wird und daß nach dem Aushärten dieser Deckschicht auf diese ein lichthärtender Kunststoffüberzug aufgebracht und dieser durch UV-Licht ausgehärtet wird. Das Kohlefasergewebe erzeugt ein natürliches Oberflächenmuster, das im Möbeldesign durchaus erwünscht sein kann. Sollen dagegen glatte Oberflächen erzielt werden, so wird die Kohlefaser-Kunststoffdeckschicht vor dem Aufbringen des Überzuges geschliffen.The invention further relates to a method for the surface coating of Objects and this method is characterized in that on the Objects applied a resin layer and inserted a carbon fiber fabric and is impregnated with resin and that after this cover layer has hardened on it a light-curing plastic coating is applied and this is cured by UV light becomes. The carbon fiber fabric creates a natural surface pattern, which in the Furniture design may well be desirable. In contrast, smooth surfaces should be achieved the carbon fiber plastic cover layer is applied before the Ground cover.

Mit dem erfindungsgemäßen Verfahren lassen sich beispielsweise Schiffsrümpfe und Container beliebiger Größe herstellen. With the method according to the invention, for example, ship hulls and Create containers of any size.

Beispielexample

Eine Holzspanplatte wird mit einem Trennmittel versehen. Anschließend wird ein Carbongewebe mit Phenolharz auflaminiert. Die Deckschicht wird dann mit einer mit Trennmittel beschichteten Preßplatte verpreßt. Nach Aushärtung der Deckschicht wird die Preßplatte abgenommen. Die Deckschicht kann dann von der Holzspanplatte abgenommen werden. Die Oberfläche der Deckschicht wird feingeschliffen und anschließend in ein Bad eines lichthärtenden Kunststoffes getaucht. Anschließend wird die Oberfläche des UV-coatings mit UV-Lampen 4 Sekunden bestrahlt. Das Ergebnis ist ein hochfestes Mehrschichtmaterial von geringem Gewicht und hochglänzender glatter Oberfläche.A chipboard is provided with a release agent. Then a Carbon fabric laminated with phenolic resin. The top layer is then covered with a Release agent-coated press plate pressed. After the top layer has hardened the press plate removed. The top layer can then be from the chipboard be removed. The surface of the top layer is sanded and then immersed in a bath of light-curing plastic. Then will irradiated the surface of the UV coating with UV lamps for 4 seconds. The result is a high-strength multilayer material of low weight and high-gloss smoother Surface.

Anhand der Zeichnung, die Ausführungsbeispiele der Erfindung zeigt, wird die Erfindung näher erläutert.The invention is illustrated by the drawing, which shows exemplary embodiments of the invention explained in more detail.

Es zeigt: It shows:  

Fig. 1 einen Querschnitt durch ein Mehrschichtmaterial, und Fig. 1 shows a cross section through a multilayer material, and

Fig. 2 einen Querschnitt durch ein Mehrschichtmaterial mit einer anderen Trägerschicht. Fig. 2 shows a cross section through a multi-layer material with another carrier layer.

Gemäß Fig. 1 besteht das Mehrschichtmaterial 10 aus einer vergleichsweise dicken Trägerschicht 12 aus einer Holzplatte, auf deren Oberfläche eine Carbongewebe- Kunststoffschicht 14 auflaminiert ist. In dieser ist z. B. Phenolharz verwendet worden, womit das Mehrschichtmaterial 10 eine hohe Temperaturbeständigkeit von ca. 250°C aufweist. Nach dem Aushärten dieser Deckschicht 14 wird deren Oberfläche geschliffen und gereinigt. Anschließend erfolgt der Auftrag eines Überzuges 16 aus lichthärtendem Kunststoff. Dieser lichthärtende Kunststoff wird durch Gießen, Spritzen oder Tauchen aufgebracht und dann durch UV-Licht-Bestrahlung gehärtet.According to Fig. 1 10, the multi-layer material of a comparatively thick base layer 12 of a wooden plate, a Carbongewebe- plastic layer 14 is laminated on the surface thereof. In this z. B. phenolic resin has been used, whereby the multilayer material 10 has a high temperature resistance of about 250 ° C. After this cover layer 14 has hardened, its surface is ground and cleaned. Then a coating 16 made of light-curing plastic is applied. This light-curing plastic is applied by casting, spraying or dipping and then hardened by UV light irradiation.

In Fig. 1 ist nur die Deckseite der Trägerschicht 12 beschichtet. Es versteht sich aber, daß genauso gut auch die Schmalseiten in gleicher Weise beschichtet sein können, wobei man die Deckschicht über die Schmalseiten herabzieht, so daß ein zusammenhängendes einteiliges Kunststoffgebilde entsteht. Der Überzug 16 überdeckt dann die Deckschicht 16 auch an den Schmalseiten des Mehrschichtmaterials 10.In Fig. 1, only the top side of the carrier layer 12 is coated. It goes without saying, however, that the narrow sides can equally well be coated in the same way, the covering layer being pulled down over the narrow sides, so that a coherent, one-piece plastic structure is produced. The coating 16 then also covers the cover layer 16 on the narrow sides of the multilayer material 10 .

Wenn die Trägerschicht 12 vor dem Aufbringen des Kunststofflaminates mit Trennmittel behandelt worden ist, läßt sich das mit dem Oberflächenüberzug 16 beschichtete Deckschichtgebilde von der Trägerschicht 12 abnehmen.If the backing layer 12 has been treated with release agent before the plastic laminate is applied, the top layer structure coated with the surface coating 16 can be removed from the backing layer 12 .

Fig. 2 unterscheidet sich von Fig. 1 dadurch, daß anstelle der Trägerschicht 12 aus Holz eine Trägerschicht 13 aus einer Wabenkonstruktion verwendet wird. Diese hat eine Deckwand 18 und eine Bodenwand 20 und eine Vielzahl diese beiden Wände 18, 20 miteinander verbindender Stege 22. Die Stege 22 können z. B. Bestandteile hexagonaler Formkörper sein. Ein solches Wabenmaterial 13 hat das geringst mögliche Raumgewicht bei ausreichender Festigkeit und Formstabilität. Auf die Deckwand 18 der Trägerschicht 13 ist die Deckschicht 14 aus Carbonfaserkunststoff aufgebracht, die ihrerseits von der UV-lichtgehärteten Kunststoffüberzugsschicht 16 abgedeckt ist. Fig. 2 differs from Fig. 1 in that instead of the carrier layer 12 made of wood, a carrier layer 13 is used from a honeycomb structure. This has a top wall 18 and a bottom wall 20 and a multiplicity of webs 22 connecting these two walls 18 , 20 . The webs 22 can, for. B. components of hexagonal shaped bodies. Such a honeycomb material 13 has the lowest possible density with sufficient strength and dimensional stability. On the top wall 18 of the carrier layer 13 , the top layer 14 made of carbon fiber plastic is applied, which in turn is covered by the UV-light-hardened plastic coating layer 16 .

Claims (10)

1. Mehrschichtmaterial für Platten und Formkörper, mit einer Trägerschicht (12, 13) die mindestens einseitig mit einer Deckschicht (14) und einem Überzug (16) beschichtet ist, dadurch gekennzeichnet, daß die Deckschicht (14) einen kohlefaserverstärkten Kunststoff und der Überzug (16) einen lichthärtenden Kunststoff aufweist.1. Multi-layer material for sheets and moldings, with a carrier layer ( 12 , 13 ) which is coated at least on one side with a cover layer ( 14 ) and a coating ( 16 ), characterized in that the cover layer ( 14 ) is a carbon fiber reinforced plastic and the coating ( 16 ) has a light-curing plastic. 2. Mehrschichtmaterial nach Anspruch 1, dadurch gekennzeichnet, daß die Deckschicht (14) aus einem, ausgehärtetes Harz aufweisenden Kohlefasergewebe besteht.2. Multi-layer material according to claim 1, characterized in that the cover layer ( 14 ) consists of a cured resin-containing carbon fiber fabric. 3. Mehrschichtmaterial nach Anspruch 2, dadurch gekennzeichnet, daß das Harz aus der Gruppe: Phenolharz, Epoxydharz, Polyesterharz oder Mischungen dieser Harze gewählt ist.3. Multi-layer material according to claim 2, characterized in that the resin of the group: phenolic resin, epoxy resin, polyester resin or mixtures of these resins is selected. 4. Mehrschichtmaterial nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß der Überzug (16) ein UV-coating ist.4. Multi-layer material according to one of claims 1 to 3, characterized in that the coating ( 16 ) is a UV coating. 5. Mehrschichtmaterial nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, daß die Trägerschicht (12) aus Metall, Holz, Holzfasermaterial, Preßpappe oder dergleichen besteht.5. Multi-layer material according to one of claims 1 to 4, characterized in that the carrier layer ( 12 ) consists of metal, wood, wood fiber material, pressed cardboard or the like. 6. Mehrschichtmaterial nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, daß die Trägerschicht (13) ein Wabenmaterial ist.6. Multi-layer material according to one of claims 1 to 4, characterized in that the carrier layer ( 13 ) is a honeycomb material. 7. Verfahren zur Oberflächenbeschichtung von Gegenständen, dadurch gekennzeichnet, daß auf die Gegenstände (12, 13) eine Harzschicht aufgebracht und in diese ein Kohlefasergewebe eingelegt und mit Harz getränkt wird, und daß nach dem Aushärten dieser Deckschicht (14) auf diese ein lichthärtender Kunststoffüberzug (16) aufgebracht und dieser durch UV-Licht ausgehärtet wird.7. A method for the surface coating of objects, characterized in that a resin layer is applied to the objects ( 12 , 13 ) and a carbon fiber fabric is inserted therein and soaked with resin, and that after the curing of this cover layer ( 14 ) on this a light-curing plastic coating ( 16 ) applied and this is cured by UV light. 8. Verfahren nach Anspruch 7, dadurch gekennzeichnet, daß die Deckschicht (14) vor dem Aufbringen des Überzuges (16) geschliffen wird.8. The method according to claim 7, characterized in that the cover layer ( 14 ) is ground before the application of the coating ( 16 ). 9. Verfahren nach Anspruch 7 oder 8, dadurch gekennzeichnet, daß das harzgetränkte Kohlefasergewebe nach Auflage einer Trennfolie und einem Abreißgewebe gepreßt und in gepreßtem Zustand ausgehärtet und vom Abreißgewebe getrennt wird.9. The method according to claim 7 or 8, characterized in that the resin-impregnated carbon fiber fabric after laying a release film and one Tear-off fabric pressed and cured in the pressed state and from Tear-off tissue is separated. 10. Verfahren nach einem der Ansprüche 7 bis 9, dadurch gekennzeichnet daß der Überzug (16) durch Gießen, Spritzen oder Tauchen aufgebracht wird.10. The method according to any one of claims 7 to 9, characterized in that the coating ( 16 ) is applied by pouring, spraying or dipping.
DE19723827A 1997-06-06 1997-06-06 Multilayer material for panels and manufacturing process Withdrawn DE19723827A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19723827A DE19723827A1 (en) 1997-06-06 1997-06-06 Multilayer material for panels and manufacturing process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19723827A DE19723827A1 (en) 1997-06-06 1997-06-06 Multilayer material for panels and manufacturing process

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Cited By (3)

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WO2001038073A1 (en) * 1999-11-24 2001-05-31 Kenneth Assink A furniture panel and method of making
DE10037317A1 (en) * 2000-07-29 2002-02-14 Airbus Gmbh Technical honeycomb has coating system on end sides, adhesive system, tear-off tissue, openings, and walls.
DE10136633A1 (en) * 2001-02-21 2002-09-19 Sika Ag, Vorm. Kaspar Winkler & Co Prefabricated building element

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001038073A1 (en) * 1999-11-24 2001-05-31 Kenneth Assink A furniture panel and method of making
DE10037317A1 (en) * 2000-07-29 2002-02-14 Airbus Gmbh Technical honeycomb has coating system on end sides, adhesive system, tear-off tissue, openings, and walls.
DE10136633A1 (en) * 2001-02-21 2002-09-19 Sika Ag, Vorm. Kaspar Winkler & Co Prefabricated building element

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