DE1924110A1 - Laminate of resin impregnated layers - Google Patents

Laminate of resin impregnated layers

Info

Publication number
DE1924110A1
DE1924110A1 DE19691924110 DE1924110A DE1924110A1 DE 1924110 A1 DE1924110 A1 DE 1924110A1 DE 19691924110 DE19691924110 DE 19691924110 DE 1924110 A DE1924110 A DE 1924110A DE 1924110 A1 DE1924110 A1 DE 1924110A1
Authority
DE
Germany
Prior art keywords
layers
radiation
action
resin
impregnated
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.)
Pending
Application number
DE19691924110
Other languages
German (de)
Inventor
Horst Dr Rer Nat Hirschfeld
Ernst-Guenter Dr Rer N Hofmann
Bruck Karl Vom
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.)
Licentia Patent Verwaltungs GmbH
Original Assignee
Licentia Patent Verwaltungs GmbH
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 Licentia Patent Verwaltungs GmbH filed Critical Licentia Patent Verwaltungs GmbH
Priority to DE19691924110 priority Critical patent/DE1924110A1/en
Publication of DE1924110A1 publication Critical patent/DE1924110A1/en
Pending legal-status Critical Current

Links

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
    • B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/10—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation for articles of indefinite length
    • 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
    • B29C43/22—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of indefinite length
    • B29C43/30—Making multilayered or multicoloured articles
    • B29C43/305—Making multilayered articles
    • 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
    • B29C70/06—Fibrous reinforcements only
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/088—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • 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
    • B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/504—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands
    • 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
    • B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0866—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using particle radiation
    • B29C2035/0877—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using particle radiation using electron radiation, e.g. beta-rays
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2711/00—Use of natural products or their composites, not provided for in groups B29K2601/00 - B29K2709/00, for preformed parts, e.g. for inserts
    • B29K2711/12—Paper, e.g. cardboard
    • B29K2711/126—Impregnated
    • 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
    • B32B2310/00—Treatment by energy or chemical effects
    • B32B2310/08—Treatment by energy or chemical effects by wave energy or particle radiation
    • B32B2310/0875—Treatment by energy or chemical effects by wave energy or particle radiation using particle radiation
    • B32B2310/0887—Treatment by energy or chemical effects by wave energy or particle radiation using particle radiation using electron radiation, e.g. beta-rays

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Physics & Mathematics (AREA)
  • Oral & Maxillofacial Surgery (AREA)
  • Thermal Sciences (AREA)
  • Laminated Bodies (AREA)

Abstract

Layers of paper or glass fibre, impregnated with resin, are fed to a former, together with covering foil at top and bottom. Intermediary metal foil layers can also be introduced. The layers pass together over a former where they are held together by tension and exposed to electron beam radiation. This activates the resin so that the layers bond together to form a laminate of pre-set dimensions.

Description

"Verfahren zum Herstellung von Mehrschichtstoffen aus harzimprägnuierten Lagen" Die vorliegende Erfindung bezieht sich auf die Herstellung von Helirschichtstoffen, welche insbesondere als Basismaterial für gedruckte Schaltungen in Form von Bahnen oder Platten dienen können. "Process for the production of multilayer materials from resin-impregnated Layers "The present invention relates to the manufacture of helical laminates, which in particular as a base material for printed circuits in the form of tracks or plates can serve.

Es St bereits bekannt, -Schichtstoffe, z.B. mit härtbarem ffirz imprägnierte Papierbahnen oder Gewebebahnen oder auf einen Trägerkörper aufgebrachte Lackfolien, durch Elektronenstrahleinwirkung zu härten.It is already known - laminates, e.g. impregnated with hardenable felt Paper webs or fabric webs or lacquer foils applied to a carrier body, to harden by exposure to electron beams.

Nen hat auch schon bei der Herstellung von Schichtstoffen das Imprägnierharz zunächst durch Elektronenenstrahleinwirkung angehärtet und anschließend das peroxidhaltige Imprägniermittel durch Wärmeeinwirkung ausgehärtet.Nen also has the impregnation resin in the manufacture of laminates initially hardened by the action of electron beams and then the peroxide-containing Impregnation agent hardened by the action of heat.

Gegenstand ler vorliegenden Erfindung ist ein Verfahren zum Verstellen von Mehrschichtstoffen aus harzimprägnierten Lagen, welches dadurch gekennzeichnet ist, daß mit einem härtbaren Ilarz imprägnierte Lagen kontinuierlich zum Mehrschichtstoff einer gewünschten Dimension zusammengefügt und unter Druckanwendang gleichzeitig durch Elektronenstrahleinwirkung gehärtet und verbunden werden.The present invention relates to a method for adjusting of multi-layer materials made of resin-impregnated layers, which is characterized by is that layers impregnated with a curable resin are continuous to the multilayer material put together in a desired dimension and under pressure simultaneously hardened and bonded by the action of electron beams.

Die Erfindung wird anhand der beigefügten Abbildungen näher erläutert.The invention is explained in more detail on the basis of the attached figures.

Die Fig. 1 zeigt schematisch die IIerstellun£ eines plattenförmigen Mehrschichtstoffes. In Fig. 2 ist die llerstellurg eines flexiblen Mehrschichtstoffes im kontinuierlichen Verfahren schematisch dargestellt.Fig. 1 shows schematically the IIerstellun £ a plate-shaped Multilayer. In Fig. 2 is the structure of a flexible multilayer material shown schematically in the continuous process.

Eine Anzahl von vorimpragnierten Bahnen, insbesondere Papierbahnen, werden,wie in Fig. 1 dargestellt, von Volratsrollen 1--4 kontinuierlich abgewickelt und zwischen mehrere Druck- und Formgebungswalzen 5,6 geführt und laufen dann durch eine Dimensionierungseinrichtung 7, welche mit 3estrahlungsdurchlässen 8 versehen ist. Beim Durchlaufen des mehrschichtstoffes, der bereits auf die gewünschte Dimension gebracht worden ist, durch die Druck- und Bestrahlungseinrichtung 7,9 wird das Imprägnierharz in den Lagen durch Elektronenstrahleinwirkung ausgehärtet und dadurch werden die einzelnen Lagen miteinander verbunden. Je nach der Latifgeschwindigkeit der durchlaufenden Bahnen ist die Anzahl der Durchlässe für den Strahlungsdurchgang in der Drucl;einrichtung angepaßt. Die an sich bekaüiite 3estrahlungseinriclitung ist lediglich schematisch mit 9 bezeichnet worden.A number of pre-impregnated webs, especially paper webs, are, as shown in Fig. 1, continuously unwound from volrats 1--4 and guided between a plurality of pressure and forming rollers 5, 6 and then run through a dimensioning device 7 which is provided with radiation passages 8 is. When going through the multilayer, which is already on the desired dimension has been brought through the pressure and irradiation device 7.9, the impregnation resin hardened in the layers by the action of electron beams and thereby the individual layers connected to each other. Depending on the latif speed of the traversing Lanes is the number of passages for the passage of radiation in the pressure device customized. The radiation device known per se is only schematic has been designated with 9.

Es hat sich als zweckmäßig ersEesen, den Mehrschichtstoff beiderseits beim Durchlaufen durch die Formgebungs- und Druckvorrichtungen mit Folien 10 abzudecken. Die Folien werden vorteilhaft als endlose Bänder ausgebildet oder sie werden vor dem Zusammenfügen des Nehrschichtstoffes von besonderen Vorratsrollen abgenommen und nach dem Durchlaufen der Bestrahlungseinrichtung auf besondere Vorratsrollen wieder aufgewickelt oder als endlose Bänder vervenclet.It has proven to be useful to have the multilayer material on both sides to be covered with foils 10 when passing through the shaping and printing devices. The films are advantageously designed as endless belts or they are in front of removed from the joining of the multilayer material from special supply rolls and after passing through the irradiation device on special supply rolls rewound or vervenclet as endless ribbons.

Für die Herstellung von Mehrschichtstoffen mit einer Kupferfolienkaschierung kann man ein Metallfolienband mit den einzelnen Lagen gemeinsam einlaufen lassen. Das Metallband wird im Mehrschichtstoff vorteilhaft so angeordnet, daß es die Rückseite zur Bestrahlungsrichtung bildet. Dadurch kann ein Teil der in den Schichtstoff eingestrahlten Elektronen von der Metallfläche wieder reflektiert werden und dadurch eine bessere Erengieausnutzung für die Aushärtung bewirkt werden.For the production of multilayer materials with a copper foil lamination you can let a metal foil strip run in together with the individual layers. The metal strip is advantageously arranged in the multilayer material in such a way that it is the rear side to the direction of irradiation. As a result, some of the radiation can be irradiated into the laminate Electrons are reflected back from the metal surface and thus a better one Erengieausführung can be effected for the hardening.

InnerhaI'. bestimmter Schichtdicken der Metallfolie z..Inside '. certain layer thicknesses of the metal foil e.g.

zwischen 35 bis 70 µ ist auch eine beidseitige Kaschierung nölich.Between 35 and 70 µ, lamination on both sides is also necessary.

In nig. 2 ist eine Anordnung schematisch dargestellt, welche für die Herstellung von flexiblen Mehrschichtstoffen dienen kann. Die eInzelnen Lagen werden von Vorratsrollen 13-15 abgezogen und über Führungs- und Druckwalzen 16,17 um eine Druckwalze 18 geführt. Die Führungswalzebn sind so angeordnet, daß der Mehrschichtstoff unter Druck- und Zugwirkung auf die Oberfläche der Druckwalze gepreBt wird. Der Mehrschichtstoff läuft dabei unter einer Bestrahlungseinrichtung 19 hindurch und kann so kontinuierlich ausgehärtet und verbunden werden. Je nach den zu stellenden Anforderungen kann die Mehrschichtstoffbahn über weitere Bearbeitungsvorrichtungen gefÜhrt werden. Für die Herstellung eines metallkaschierten Mehrschichtstoffes wird eine Netallfolienbahn zusammen mit den weiteren Lagen des Mehrschichtstoffes über die Druckwalze geführt, wobei die Metallfolie direkt auf der Walze zu liegen kommt, so daß die eintretenden Strahlen nur den Schichtstoff durchdringen und an der Metallfolie wiederum in den Mehrschichtstoff reflektiert werden. Für besondere Zwecke können weitere Deck- und Schutzfolien zusammen mit dem Mehrschichtstoff durch die Bestrahlungseinrichtung geführt werden.In nig. 2 an arrangement is shown schematically, which for the Production of flexible multilayer materials can serve. The individual layers are withdrawn from supply rolls 13-15 and over guide and pressure rollers 16,17 to one Pressure roller 18 out. The guide rollers are arranged so that the multilayer material is pressed under pressure and tension on the surface of the pressure roller. Of the Multilayer material runs under an irradiation device 19 and can thus be cured and bonded continuously. Depending on the ones to be asked The multilayer material web can meet requirements via further processing devices be guided. For the production of a metal-clad multilayer material a metallic foil sheet together with the other layers of the multilayer material the pressure roller guided, whereby the metal foil comes to lie directly on the roller, so that the incoming rays only penetrate the laminate and on the metal foil in turn are reflected in the multilayer material. For special purposes you can further cover and protective films together with the multilayer material through the irradiation device be guided.

Eine andere Ausführungsform ergibt sich dadurch, daß anstelle der Metallkaschierung ein ein- ender beidseitig mit organischen thermo#lastischen Folien oder anderen Kunststoffen kaschiert er Mehrschichtstoff unter Aushärtung durch Elektronenbestrahlung hergestellt wird.Another embodiment results from the fact that instead of Metal lamination one end on both sides with organic thermo # elastic foils or other plastics he laminates multi-layer material while curing is produced by electron irradiation.

Als Trägerkörper für die einzelnen Lagen können organische oder anorganische Bahnen, z.B. aus Papier, Glasfasermaterial, verwebt oder nicht verwebt, verwendet werden.The support bodies for the individual layers can be organic or inorganic Sheets, e.g. made of paper, fiberglass material, woven or non-woven, are used will.

Als Bindemittel für die imprägnierten Bahnen eignen sich besoizders an sich bekannte ungesättigte Polyester, bei denen peroxidische Vernetzungsmittel entfallen können. Für die Herstellung des Verbundstoffes kommen für die Follenabdeckung vor allem Olefinpolymerisate in Frage, welche bei dem Vernetzungsprozeß durch ELektronenstrahleinwirlçung gleichzeitig einen guten Verbund zwischen Bindemittel und Folie ermöglichen.Besoizders are suitable as binders for the impregnated webs unsaturated polyesters known per se, in which peroxidic crosslinking agents can be omitted. For the production of the composite material come for the follen cover especially olefin polymers in question, which in the crosslinking process by electron beam induction at the same time enable a good bond between binder and film.

4 Seiten Beschreibung 5 Patentansprüche4 pages description 5 claims

Claims (5)

Patentansprüche 0 Verfahren zum Herstellen von Mehrschichtstoffen aus harzimprägnierten Lagen, dadurch gekennzeichnet, daß mit einem härtbaren Harz imprägnierte Lagen kontinuierlich zum Mehrschichtstoff einer gewünschten Dimension zusammengefügt und' unter Druckanwendung gleichzeitig durch Elektronenstrahleinwirkung gehärtet und verbunden werden. Claims 0 A method for producing multilayer materials made of resin-impregnated layers, characterized in that with a hardenable resin impregnated layers continuously to form a multilayer material of a desired dimension joined together and 'under the application of pressure at the same time by the action of electron beams hardened and bonded. 2. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß mehrere Bahnen zwischen Druck- und Formgebungselemente geführt und in einer Dimensionierungseinrichtung, welche mit Bestrahlungsdurchlässen versehen ist, durch Elektronenstrahleinwirkung gehärtet und verbunden werden.2. The method according to claim 1, characterized in that several Tracks guided between the pressure and shaping elements and in a dimensioning device, which is provided with irradiation passages, by the action of electron beams hardened and bonded. 3. Verfahren nach Anspruch 2, dadurch gekennzeichnet, iß mehrere der Laufgeschwindigkeit angepaßte Durchlässe für den Strahlungsdurchgang in der Dimensionierungseinrichtung vorgesehen sind.3. The method according to claim 2, characterized in that several of the eats Passages adapted to the running speed for the passage of radiation in the dimensioning device are provided. 4. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß mit härtbarem Harz imprägnierte Trägerkörper mit einer Metallfolie kaschiert und durch Strahleneinwirkung zu einem Verbundkörper ausgehärtet werden.4. The method according to claim 1, characterized in that with hardenable Resin-impregnated carrier body laminated with a metal foil and exposed to radiation are cured to form a composite body. 5. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß mehrere Lagen mit einer thermoplastischen Folie ein- oder beidseitig kaschiert und zu einem Mehrschichtverbundkörper unter Strahleneinwirkung ausgehärtet werden Leerseite5. The method according to claim 1, characterized in that several Layers laminated with a thermoplastic film on one or both sides and into one Multi-layer composite bodies are cured under the action of radiation Blank page
DE19691924110 1969-05-12 1969-05-12 Laminate of resin impregnated layers Pending DE1924110A1 (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2238919A1 (en) * 1971-08-09 1973-02-22 Dart Ind Inc STRATIFIED PRODUCT AND METHOD OF MANUFACTURING IT
DE2657470A1 (en) * 1976-12-18 1978-06-22 Hans Mauthe WINDOW COVERAGE WITH WINDOW
DE3010060A1 (en) * 1980-03-15 1981-10-01 Letron GmbH, 8750 Aschaffenburg MULTI-LAYERED PLATE HAVING A VARNISH SURFACE, METHOD FOR THE PRODUCTION THEREOF AND THEIR USE
FR2516862A1 (en) * 1980-05-24 1983-05-27 Siempelkamp Gmbh & Co Laminate strip production machine - has pressure chamber inlet and outlet rollers running against common heating roller
DE3307057A1 (en) * 1983-03-01 1984-09-06 Held Kurt METHOD FOR CONTINUOUSLY PRODUCING COPPER-COATED ELECTROLAMINATES AND DEVICE FOR IMPLEMENTING THE METHOD
US4844764A (en) * 1982-09-07 1989-07-04 Energy Sciences Inc. Process of in-line coating and decorative-layer lamination with panel board material employing electron beam irradiation
WO1991000409A1 (en) * 1989-07-03 1991-01-10 Omniglass Ltd. Moisture impermeable spacer for a sealed window unit
EP0586552A1 (en) * 1991-05-24 1994-03-16 Global Thermal Conditioning, Inc. Shadow boundary process for the continuous radiant cure of composites

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2238919A1 (en) * 1971-08-09 1973-02-22 Dart Ind Inc STRATIFIED PRODUCT AND METHOD OF MANUFACTURING IT
DE2657470A1 (en) * 1976-12-18 1978-06-22 Hans Mauthe WINDOW COVERAGE WITH WINDOW
DE3010060A1 (en) * 1980-03-15 1981-10-01 Letron GmbH, 8750 Aschaffenburg MULTI-LAYERED PLATE HAVING A VARNISH SURFACE, METHOD FOR THE PRODUCTION THEREOF AND THEIR USE
FR2516862A1 (en) * 1980-05-24 1983-05-27 Siempelkamp Gmbh & Co Laminate strip production machine - has pressure chamber inlet and outlet rollers running against common heating roller
US4844764A (en) * 1982-09-07 1989-07-04 Energy Sciences Inc. Process of in-line coating and decorative-layer lamination with panel board material employing electron beam irradiation
US4579612A (en) * 1983-03-01 1986-04-01 Kurt Held Method of and apparatus for the continuous production of a copper-faced electrolaminate
EP0120192A2 (en) * 1983-03-01 1984-10-03 Kurt Held Method of continuously making copper-clad electrolaminates, and device therefor
EP0120192A3 (en) * 1983-03-01 1986-12-03 Kurt Held Method of continuously making copper-clad electrolaminates, and device therefor
DE3307057A1 (en) * 1983-03-01 1984-09-06 Held Kurt METHOD FOR CONTINUOUSLY PRODUCING COPPER-COATED ELECTROLAMINATES AND DEVICE FOR IMPLEMENTING THE METHOD
WO1991000409A1 (en) * 1989-07-03 1991-01-10 Omniglass Ltd. Moisture impermeable spacer for a sealed window unit
US5079054A (en) * 1989-07-03 1992-01-07 Ominiglass Ltd. Moisture impermeable spacer for a sealed window unit
EP0586552A1 (en) * 1991-05-24 1994-03-16 Global Thermal Conditioning, Inc. Shadow boundary process for the continuous radiant cure of composites
EP0586552A4 (en) * 1991-05-24 1994-04-13 Global Thermal Conditioning, Inc.

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