DE3300622A1 - Process and device for producing a laminated body consisting of at least two sheet-shaped structural elements - Google Patents

Process and device for producing a laminated body consisting of at least two sheet-shaped structural elements

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Publication number
DE3300622A1
DE3300622A1 DE19833300622 DE3300622A DE3300622A1 DE 3300622 A1 DE3300622 A1 DE 3300622A1 DE 19833300622 DE19833300622 DE 19833300622 DE 3300622 A DE3300622 A DE 3300622A DE 3300622 A1 DE3300622 A1 DE 3300622A1
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DE
Germany
Prior art keywords
components
heating plate
vacuum chamber
movable
structural elements
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.)
Granted
Application number
DE19833300622
Other languages
German (de)
Other versions
DE3300622C2 (en
Inventor
Jürgen Dipl.-Ing. 2200 Elmshorn Rauhöft
Peter Dipl.-Ing. 2082 Uetersen Thöl
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.)
Thoel Peter 25436 Uetersen De Rauhoeft Juergen
Original Assignee
Licentia Patent Verwaltungs GmbH
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Application filed by Licentia Patent Verwaltungs GmbH filed Critical Licentia Patent Verwaltungs GmbH
Priority to DE19833300622 priority Critical patent/DE3300622A1/en
Publication of DE3300622A1 publication Critical patent/DE3300622A1/en
Application granted granted Critical
Publication of DE3300622C2 publication Critical patent/DE3300622C2/de
Granted 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
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • 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
    • B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • B32B17/06—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
    • B32B17/10—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin
    • B32B17/10005—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing
    • B32B17/10807—Making laminated safety glass or glazing; Apparatus therefor
    • B32B17/10816—Making laminated safety glass or glazing; Apparatus therefor by pressing
    • B32B17/10871—Making laminated safety glass or glazing; Apparatus therefor by pressing in combination with particular heat treatment
    • 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
    • B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • B32B17/06—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
    • B32B17/10—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin
    • B32B17/10005—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing
    • B32B17/10807—Making laminated safety glass or glazing; Apparatus therefor
    • B32B17/10816—Making laminated safety glass or glazing; Apparatus therefor by pressing
    • B32B17/10825—Isostatic pressing, i.e. using non rigid pressure-exerting members against rigid parts
    • B32B17/10834—Isostatic pressing, i.e. using non rigid pressure-exerting members against rigid parts using a fluid
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/02—Details
    • H01L31/0203—Containers; Encapsulations, e.g. encapsulation of photodiodes
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/042—PV modules or arrays of single PV cells
    • H01L31/048—Encapsulation of modules
    • 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
    • B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • B32B37/1207—Heat-activated adhesive
    • B32B2037/1215—Hot-melt adhesive
    • B32B2037/1223—Hot-melt adhesive film-shaped
    • 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
    • B32B2315/00—Other materials containing non-metallic inorganic compounds not provided for in groups B32B2311/00 - B32B2313/04
    • B32B2315/08—Glass
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/50—Photovoltaic [PV] energy

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Condensed Matter Physics & Semiconductors (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Power Engineering (AREA)
  • Thermal Sciences (AREA)
  • Joining Of Glass To Other Materials (AREA)

Abstract

Process and device for producing a laminated body consisting of at least two sheet-shaped structural elements. Concerned in particular are a composite glass pane, an insulating material, or a solar generator which is preferably laid between hot-melt adhesive films, has connected solar cells, is provided on both sides with protective coverings and is intended for terrestrial applications. The structural elements forming the laminated body are subjected to temperature/ pressure treatment in a vacuum chamber in such a manner that the structural elements form a mechanically strong composite after completion of the treatment. After the introduction of the structural elements into the vacuum chamber, the latter is evacuated with the structural elements at the same time being mounted without any forces and no direct contact with the heating devices. After completion of the evacuation process, the temperature/pressure treatment is carried out and the vacuum is simultaneously maintained. <IMAGE>

Description

"Verfahren und Vorrichtung zur Herstellung eines aus mindestens zwei"Method and apparatus for making one of at least two

plattenförmigen Bauelementen bestehenden Schichtkörpers" Die Erfindung betrifft ein Verfahren gemäß dem Oberbegriff von Anspruch 1 sowie ein2 Vorrichtung zur Durchführung des Verfahrens.plate-shaped structural elements existing laminated body "The invention relates to a method according to the preamble of claim 1 and a device to carry out the procedure.

Es sind sogenannte Verbundgläser bekannt, z.B. als Windschutzscheiben für Kraftfahrzeuge, bei denen zwei Glasscheiben und eine zwischen ihnen eingebrachte Klebefolie durch Anwendung von Druck und Temperatur zu einem einheitlichen, glasklaren Verbund verschmolzen werden. Die Herstellung erfolgt in sogenannten Autoklavprozessen.So-called laminated glasses are known, e.g. as windshields for motor vehicles with two panes of glass and one inserted between them Adhesive film by applying pressure and temperature to a uniform, crystal clear Composite to be merged. The production takes place in so-called autoclave processes.

Es ist weiterhin bei der Herstellung von Solargeneratoren bekannt, diese in einer Vakuum-Kammer zu positionieren, wobei der technische Aufbau des Generators aus den Solarzellen, ober- und unterseitig davon angeordneten Schmelzkleberfolien und zwei äußeren Glasscheiben bestehen kann. Nach dem Evakuieren wird über eingebaute Heizungen der Verbund aufgeheizt und dann mechanisch belastet, bis die Schmelzkleberfolie alle Fugen ausgefüllt hat.It is also known in the manufacture of solar generators, to position these in a vacuum chamber, with the technical structure of the generator from the solar cells, top and bottom of them arranged hot melt adhesive films and can consist of two outer panes of glass. After evacuation is over built Heaters of the composite are heated up and then mechanically loaded until the hotmelt adhesive film has filled in all the joints.

Der notwendige äußere Andruck ist temperatur- und zeitabhängig, bedingt durch die Zähigkeit des Klebers. Bei diesem Herstellungsverfahren werden mehrere Generatoren zusammen mit ihren metallischen Trägern in die Vakuumkammer ein- gebracht. Dieses bringt nachteiligerweise einen großen apparativen Aufwand, großen Platzbedarf und hohe Energiekosten mit sich.The necessary external pressure is temperature and time dependent, conditional due to the toughness of the glue. In this manufacturing process, several Generators together with their metallic supports in the vacuum chamber brought. Disadvantageously, this entails a large outlay in terms of equipment and a large space requirement and high energy costs with it.

Der Erfindung liegt daher die Aufgabe zugrunde, ein Verfahren und eine Vorrichtung der eingangs genannten Art zu schaffen, die eine wesentliche Vereinfachung bisher bekannter Prozesse, wesentlich geringere Anlagenkosten und einen geringeren Energiebedarf mit sich bringen.The invention is therefore based on the object of a method and to create a device of the type mentioned, which is a substantial simplification previously known processes, significantly lower system costs and a lower one Bring energy requirements with them.

Die Aufgabe wird erfindungsgemäß durch die kennzeichnenden Verfahrensmerkmale von Anspruch 1 gelöst.According to the invention, the object is achieved by the characterizing process features solved by claim 1.

Ausgestaltungen der Erfindung sind in der Unteransprüchen 2 und 3 beschrieben.Refinements of the invention are set out in subclaims 2 and 3 described.

Eine Vorrichtung zur Durchführung des erfindungsgemäßen Verfahrens ist im Anspruch 4 beansprucht.A device for carrying out the method according to the invention is claimed in claim 4.

Weiterbildungen der erfindungsgemäßen Vorrichtung sind aus den Unteransprüchen 5 bis 9 ersichtlich.Further developments of the device according to the invention are given in the subclaims 5 to 9 can be seen.

Vorteile der Erfindung sind - neben dem einfachen Aufbau der somit preisgünstigen Vorrichtung - in einer einfachen Steuerung des Herstellungsverfahrens, in dem geringen Energieverbrauch, in einer niedrigen Vakuumpumpleistung, in einem schnellen Prozeßablauf und in einem planparallelen, blasenfreien Schichtkörper zu sehen.Advantages of the invention are - in addition to the simple structure of the thus inexpensive device - in a simple control of the manufacturing process, in the low energy consumption, in a low vacuum pump capacity, in one fast process sequence and in a plane-parallel, bubble-free layer body see.

In der Zeichnung ist eine Vorrichtung zur Durchführung des erfindungsgemäßen Verfahrens dargestellt, und zwar zeigt: Figur 1 die Vorrichtung im geöffneten Zus#and, d.h. Ober- und Unterteil der Vorrichtung sind voneinander getrennt, und Figur 2 die Vorrichtung im geschlossenen Zustand, so daß Ober- und Unterteil eine Vakuumkammer bilden.In the drawing is a device for performing the invention Method shown, namely: Figure 1 shows the device in the open assembly, i.e. the top and bottom of the device are separated from each other, and Figure 2 the device in the closed state, so that the upper and lower part form a vacuum chamber form.

In den Figuren 1 und 2 besteht das Unterteil 1 der beispielsweise kastenförmigen Vorrichtung im wesentlichen aus einer raumfesten ersten Heizplatte 3, deren Seitenflächen und Unterseite von einem Isolator 4 umgeben sind. In der Heizplatte 3 sind in nicht bezeichneten Bohrungen federnde Stifte 5 angeordnet, die über die Oberseite der Heizplatte 3 hinausragen und somit für eine kräftefreie Lagerung der auf einer Folie 6, z.B. eine wärmebeständige Kunststoff- oder Metallfolie, liegende Bauelemente 7 eines Schichtkörpers 8 dienen. Der Federweg der Stifte 5 ist so bemessen, daß bei einer Belastung der Bauelemente 7 von oben die Stifte 5 vollständig in ihre zugehörenden Bohrungen eintauchen und somit die Bauelemente 7 bzw. der Schichtkörper 8 zusammen mit der Folie 6 auf der Oberseite der raumfesten ersten Heizplatte 3 aufliegen.In Figures 1 and 2, the lower part 1 consists of, for example box-shaped device consisting essentially of a first heating plate which is fixed in space 3, the side surfaces and underside of which are surrounded by an insulator 4. In the Heating plate 3 resilient pins 5 are arranged in holes not designated, which protrude over the top of the heating plate 3 and thus for a force-free Storage of the on a foil 6, e.g. a heat-resistant plastic or metal foil, horizontal components 7 of a laminated body 8 are used. The spring deflection of the pins 5 is dimensioned so that when the components 7 are loaded from above, the pins 5 Immerse completely in their associated holes and thus the components 7 or the layered body 8 together with the film 6 on the top of the spatially fixed first heating plate 3 rest.

Das Oberteil 2 der Vorrichtung weist eine Stirnplatte 9 auf, die zusammen mit Gehäusewandungen 10 praktisch ein Gehäuse für eine Vakuumkammer 11 darstellt. Hierbei wird die vierte Wandung durch die raumfeste erste Heizplatte 3 gebildet, was besonders deutlich aus Figur 2 ersichtlich ist. Sowohl die Stirnsplatte 9 als auch die Gehäusewandungen 10 sind zur Verminderung von Wärmeverlusten von einem Isolator 12 umgeben.The upper part 2 of the device has an end plate 9, which together with housing walls 10 practically represents a housing for a vacuum chamber 11. Here, the fourth wall is formed by the first heating plate 3, which is fixed in space, which can be seen particularly clearly from FIG. Both the face plate 9 as the housing walls 10 are also designed to reduce heat losses from one Surround insulator 12.

Das Oberteil 2 enthält in dem Vakuumraum 11 eine bewegbare zweite Heizplatte 13, die senkrecht zur Stirnplatte 9 bewegbar ist. Hierzu ist eine Druckluftzylinder - Kolbenanordnung vorgesehen, deren Zylinder 14 mit der Stirnplatte 9 und deren Kolben 15 über eine Kolbenstange 16 mit der bewegbaren zweiten Heizplatte 13 mechanisch fest verbunden ist. Der Hub der bewegbaren zweiten Heizplatte 13 wird durch mechanische Anschläge 24 begrenzt. Zwischen der Heizplatte 13 und den Gehäusewandungen 10 des Oberteiles 2 ist eine Gleitdichtung, beispielsweise in Form einer Membran 17, derart angeordnet, daß oberhalb der Heizplatte 13 ein Druckraum 18 entsteht. Der Druckraum 18 ist von der Vakuumkammer 11 getrennt. Über eine Ventilanordnung 19 mit zugehörender Rohrleitung 20 kann der Druckraum 18 evakuiert werden oder es kann ihm Druckluft zugeführt werden. Im Gegensatz zum Druckraum 18 wird die Vakuumkammer 11 über die Ventil-Rohranordnung 21 und 22 lediglich evakuiert.The upper part 2 contains a movable second in the vacuum space 11 Heating plate 13, which can be moved perpendicular to the face plate 9. A compressed air cylinder is used for this - Piston assembly provided, the cylinder 14 with the end plate 9 and the Piston 15 mechanically via a piston rod 16 with the movable second heating plate 13 is firmly connected. The stroke of the movable second heating plate 13 is mechanical Limit stops 24. Between the heating plate 13 and the housing walls 10 of the Upper part 2 is a sliding seal, for example in the form of a membrane 17, such arranged that a pressure space 18 is created above the heating plate 13. The printing room 18 is separated from the vacuum chamber 11. Via a valve assembly 19 with associated Pipeline 20, the pressure chamber 18 can be evacuated or it can be compressed air are fed. In contrast to the pressure chamber 18, the vacuum chamber 11 is via the Valve tube assembly 21 and 22 only evacuated.

Das Unterteil 1 und das Oberteil 2 sind in der in Figur 1 gezeigten Weise voneinander trennbar, so daß die Bauelemente 7 bzw. der Schichtkörper 8 in bzw. aus der Vakuumkammer 11 eingeführt oder ausgeführt werden können. Im geschlossenen Zustand der Vorrichtung gemäß Figur 2 erfolgt eine Abdichtung der Vakuumkammer 11 zwischen dem Unter- und Oberteil 1 bzw. 2 durch ein Dick.The lower part 1 and the upper part 2 are shown in FIG Manner separable from one another, so that the components 7 or the laminated body 8 in or can be introduced or carried out from the vacuum chamber 11. In closed In the state of the device according to FIG. 2, the vacuum chamber 11 is sealed between the lower and upper part 1 or 2 by a thick.

tungselement 23, das in in den Gehäusewandungen 10 des Oberteiles 2 vorgeseh# Nuten angeordnet ist.processing element 23, which is in the housing walls 10 of the upper part 2 provided # grooves is arranged.

Elektrische Anschlußdrähte für die Heizplatten 3 und 13 sind in den Figuren 1 und 2 aus Vereinfachungsgründen nicht dargestellt. Dies gilt auch für zu den Ventilen 19 und 21 führende Steuerleitungen.Electrical connection wires for the heating plates 3 and 13 are in the Figures 1 and 2 are not shown for reasons of simplicity. This also applies to Control lines leading to valves 19 and 21.

Ein aus mindestens zwei plattenförmigen Bauelementen 7 bestehender Schichtkörper 8, insbesondere ein Solargenerator der eingangs genannten Art, wird mit der Vorrichtung gemäß der Figuren 1 und 2 auf folgende Weise hergestellt: Die Bauelemente 7 werden bei geöffneter Vorrichtung (Figur 1) mittels einer Folie 6 in den Vakuumraum 11 eingebracht und dort zwischen den Heizplatten 3 und 13 positioniert. Anstelle der Folie 6 kann auch eine Greifvorrichtung verwendet werden. Anschließend wird die Vorrichtung geschlossen (Figur ?), derart, daß der evakuierbare Raum 11 entsteht und die Bauelemente 7 auf den federnden Stiften 5 kräftefrei, ohne direkte Berührung mit den lleizplatten 3 und 13 lagern. Hierbei werden die Bauelemente von der bewegbaren Heizplatte 13 durch die Zylinderkolbenanordnung 14 - 16 auf Abstand gehalten. In diesem Zustand werden der Vakuumraum 11 und gegebenenfalls der Druckraum 18 über die Ventil-Rohranordnungen 19, 20 bzw. 21, 22 evakuiert. Nach ausreichender Evakuierzeit wird die bewegbare Heizplatte 13 abgesenkt und der Druckraum 18 belüftet, während der Vakuumraum 11 weiter evakuiert bleibt. Wenn es notwendig sein sollte, wird der Druckraum 18 mit Druckluft beaufschlagt, um den Fügedruck zwischen den Heizplatten 3 und 13 zu erhöhen. Der Schichtkörper 8 erhält direkten Kontakt mit den Heizplatten 3 und 13 und wird auf die erforderliche Temperatur erwärmt. Die Fügezeit richtet sich nach den Naterialanforderungen. Durch das Evakuieren und Einleitung des Fügevorganges wird ein blasenfreier Verbund erzeugt.One consisting of at least two plate-shaped components 7 Layered body 8, in particular a solar generator of the type mentioned at the outset, is produced with the device according to Figures 1 and 2 in the following way: The When the device is open (FIG. 1), components 7 are secured by means of a film 6 introduced into the vacuum space 11 and positioned there between the heating plates 3 and 13. Instead of the film 6, a gripping device can also be used. Afterward the device is closed (figure?), in such a way that the evacuable space 11 arises and the components 7 on the resilient pins 5 force-free, without direct Store contact with the soldering plates 3 and 13. The components of the movable heating plate 13 by the cylinder piston assembly 14-16 at a distance held. In this state, the vacuum space 11 and possibly the pressure space 18 evacuated via the valve-tube assemblies 19, 20 and 21, 22, respectively. After sufficient Evacuation time, the movable heating plate 13 is lowered and the pressure chamber 18 is ventilated, while the vacuum space 11 remains evacuated. If it should be necessary the pressure chamber 18 is acted upon with compressed air to reduce the joining pressure between the Increase heating plates 3 and 13. The laminated body 8 receives direct contact with the heating plates 3 and 13 and is heated to the required temperature. the The joining time depends on the material requirements. Through evacuation and initiation the joining process creates a bubble-free bond.

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Claims (9)

PATENTANSPRÜCHE B Verfahren zur Herstellung eines aus mindestens zwei plattenförmigen Bauelementen bestehenden Schichtkörpers, insbesondere einer Verbundglasscheibe, eines Isoliermaterials oder eines Solargenerators, der vorzugsweise zwischen Schmelzkleberfolien gelegte, geschaltete Solarzellen aufweist, beidseitig mit Schutzabdeckungen versehen sowie für terrestrische Anwendungen vorgesehen ist wobei die den Schichtkörper bildenden Bauelemente in einer Vakuumkammer einer Temperatur-/Druckbehandlung derart unterzogen werden, daß die Bauelemente nach Abschluß der Behandlung einen mechanisch festen Verbund bilden, dadurch gekennzeichnet, daß nach dem Einbringen der Bauelemente (7) in die Vakuumkammer (11) diese evakuiert wird bei einer gleichzeitigen kräftefreien Lagerung der Bauelemente (7) ohne direkte Berührung mit den Heizvorrichtungen (3, 13), und daß nach Beendigung des Evakuiervorganges die Temperatur-/Druckbehandlung bei gleichzeitiger Aufrechterhaltung des Vakuums durchgeführt wird. PATENT CLAIMS B Method for making one from at least two plate-shaped components existing layer body, in particular one Laminated glass, an insulating material or a solar generator, which is preferably has switched solar cells placed between hot melt adhesive films, on both sides provided with protective covers and intended for terrestrial applications wherein the components forming the laminated body are subjected to a temperature / pressure treatment in a vacuum chamber are subjected in such a way that the components after completion of the treatment Form a mechanically strong bond, characterized in that after the introduction of the components (7) in the vacuum chamber (11) this is evacuated with a simultaneous Force-free storage of the components (7) without direct contact with the heating devices (3, 13), and that after the end of the evacuation process, the temperature / pressure treatment is carried out while maintaining the vacuum. 2. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß die Bauelemente (7) mittels einer Trägerfolie (6) in die Vakuumkammer (11) eingebracht und dort positioniert werden. 2. The method according to claim 1, characterized in that the components (7) introduced into the vacuum chamber (11) by means of a carrier film (6) and there be positioned. 3. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß die Bauelemente (7) mit Hilfe einer Greifvorrichtung in die Vakuumkammer (11) eingebracht und dort positioniert werden.3. The method according to claim 1, characterized in that the components (7) brought into the vacuum chamber (11) with the help of a gripping device and there be positioned. 4. Vorrichtung zur Durchführung des Verfahrens nach Anspruch 1, 2 oder 3, dadurch gekennzeichnet, daß ein eine raumfeste erste Heizplatte (3) aufweisendes Unterteil (1) und ein eine bewegbare zweite Heizplatte (13) enthaltendes Oberteil (2) vorgesehen sind, daß das Unter- und Oberteil (1, 2) im geschlossenen Zustand eine evakuierbare Kammer (Vakuumkammer, 1i) bilden, die durch die raumfeste erste Heizplatte (3), durch die bewegbare zweite Heizplatte (13) sowie durch Gehäusewandungen (10) des Oberteiles (2) begrenzt ist, deren Volumen durch die bewegbare zweite Heizplatte (13) veränderbar ist und die zur Aufnahme der Bauelemente (7) des Schichtkbrpers (8) dient, daß das Unter- und Oberteil (1 bzw. 2) zur Ein- oder Ausfuhr der Bauelemente (7) bzw. des Schichtkörpers (8) in bzw. aus der Vakuumkammer (11) voneinander trennbar sind, und daß in der raumfesten ersten Heizplatte (3) federnde Stifte (5) angeordnet sind, die bei einer kräftefreien Lagerung der Bauelemente (7) eine Berührung zwischen der raumfesten ersten Heizplatte (3) und den Iiauelementen (7) verhindern und die bei einem Absenken der bewegbaren zweiten Heizplatte (13) auf die Bauelemente (7) derart nachgeben, daß die Bauelemente (7) auf der raumfesten ersten Heizplatte (3) aufliegen.4. Apparatus for performing the method according to claim 1, 2 or 3, characterized in that a first heating plate (3) which is fixed in space is provided Lower part (1) and an upper part containing a movable second heating plate (13) (2) it is provided that the lower and upper part (1, 2) in the closed state an evacuable chamber (vacuum chamber, 1i) form through the first Heating plate (3) through the movable second heating plate (13) and through the housing walls (10) of the upper part (2) is limited, the volume of which is limited by the movable second heating plate (13) is changeable and that for receiving the components (7) of the laminated body (8) serves that the lower and upper part (1 or 2) for the import or export of the components (7) or the layered body (8) in or out of the vacuum chamber (11) can be separated from one another are, and that in the spatially fixed first heating plate (3) resilient pins (5) are arranged are that with a force-free storage of the components (7) a contact between the fixed first heating plate (3) and the Iiauelementen (7) prevent and the when the movable second heating plate (13) is lowered onto the components (7) yield in such a way that the components (7) on the fixed first heating plate (3) rest. 5. Vorrichtung nach Anspruch 4, gekennzeichnet durch eine Trägerfolie (6) für die Bauelemente (7) des Schichtkörpers (8), die sich zwischen dem Unter-und Oberteil (1, 2) und zwischen den Bauelementen (7) und den federnden Stiften (5) befindet.5. Apparatus according to claim 4, characterized by a carrier film (6) for the components (7) of the layered body (8), which are located between the lower and Upper part (1, 2) and between the components (7) and the resilient pins (5) is located. 6. Vorrichtung nach Anspruch 4 oder 5, gekennzeichnet durch ein Dichtungselement (23) zwischen dem Unter- und Oberteil (1 bzw. 2), das in in den Gehäusewandungen (10) des Oberteiles (2) vorgesehenen Nuten angeordnet ist.6. Apparatus according to claim 4 or 5, characterized by a sealing element (23) between the lower and upper part (1 or 2), which is in the housing walls (10) of the upper part (2) provided grooves is arranged. 7. Vorrichtung nach Anspruch 4, dadurch gekennzeichnet, daß zwischen der bewegbaren zweiten Heizplatte (13) und den Gehäusewandungen (10) des Ober- teiles (2) eine Gleitdichtung derart angeordnet ist, daß oberhalb der bewegbaren zweiten Heizplatte (13) ein von der Vakuumkammer (11) getrennter, evakuierbarer oder mit Druckluft füllbarer Druckraum (18) entsteht.7. Apparatus according to claim 4, characterized in that between the movable second heating plate (13) and the housing walls (10) of the upper part (2) a sliding seal is arranged such that above the movable second Heating plate (13) separate from the vacuum chamber (11), evacuable or with Compressed air fillable pressure space (18) is created. 8. Vorrichtung nach Anspruch 7, gekennzeichnet durch eine Membran (17) als Gleitdichtung.8. Apparatus according to claim 7, characterized by a membrane (17) as a sliding seal. 9. Vorrichtung nach Anspruch 4 oder 7, dadurch gekennzeichnet, daß die bewegbare zweite Heizplatte (13) durch eine Druckluftzylinder-Kolbenanordnung (14, 15, 16) gegenüber dem Oberteil (2) bewegbar ist.9. Apparatus according to claim 4 or 7, characterized in that the movable second heating plate (13) by an air cylinder piston assembly (14, 15, 16) can be moved relative to the upper part (2).
DE19833300622 1983-01-11 1983-01-11 Process and device for producing a laminated body consisting of at least two sheet-shaped structural elements Granted DE3300622A1 (en)

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DE19833300622 DE3300622A1 (en) 1983-01-11 1983-01-11 Process and device for producing a laminated body consisting of at least two sheet-shaped structural elements

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DE3300622A1 true DE3300622A1 (en) 1984-07-12
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Cited By (11)

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DE3538986A1 (en) * 1985-11-02 1987-05-14 Licentia Gmbh SOLAR GENERATOR
DE102004003328A1 (en) * 2004-01-22 2005-08-18 Webasto Ag Curved bodywork component for a vehicle, comprises placing a melt adhesive film on one side of the element, placing cells on the film, and applying another film on top
US6953514B2 (en) 2001-01-08 2005-10-11 Steag Hamatech Ag Method and device for assembling substrates
WO2009114189A2 (en) * 2008-03-14 2009-09-17 Dow Corning Corporation Method of forming a photovoltaic cell module
WO2010143117A2 (en) 2009-06-08 2010-12-16 3S Swiss Solar Systems Ag Method for producing a solar panel
CH701494A1 (en) * 2009-07-21 2011-01-31 3S Swiss Solar Systems Ag Method for laminating plate-shaped elements, comprises connecting a meltable adhesive layer of three material layers in an evacuatable laminating chamber with a flat heating device
DE102010061294A1 (en) * 2010-12-16 2012-06-21 Bayerische Motoren Werke Aktiengesellschaft Laminator e.g. multi-opening laminator for manufacturing solar cell, has laminate layer stack made of five layers, that is provided on thermally conductive insert in lower chamber
CN104972732A (en) * 2015-07-21 2015-10-14 秦皇岛中晟太阳能科技有限公司 Vacuum laminating machine
DE102014211920A1 (en) * 2014-06-23 2015-12-24 Bayerische Motoren Werke Aktiengesellschaft Method for producing a composite pane
EP2457718A3 (en) * 2010-11-24 2016-12-21 The Boeing Company Methods and apparatus for void-free debulking of adhesive bond joints
DE102018101470A1 (en) * 2018-01-23 2019-07-25 Robert Bürkle GmbH Laminating apparatus and method for laminating at least one layer stack

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DE9111708U1 (en) * 1991-09-19 1992-04-16 Anger Electronic Ges.m.b.H. Emco InnovationsCenter, Hallein Device for laminating printed and unprinted films
DE10218198C1 (en) * 2002-04-23 2003-12-18 Prokon Technologie Gmbh & Co K Laminator for making glass-solar cell laminate, used for making curved solar cell laminate for vehicle roof, with hot plate, diaphragm and cover for pressure-assisted vacuum bag lamination uses hot plate with curved top area for laminate
DE102004027545A1 (en) * 2004-06-04 2005-12-29 Meier Vakuumtechnik Gmbh Device for hot lamination and subsequent cooling of components

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DE3538986A1 (en) * 1985-11-02 1987-05-14 Licentia Gmbh SOLAR GENERATOR
US6953514B2 (en) 2001-01-08 2005-10-11 Steag Hamatech Ag Method and device for assembling substrates
DE102004003328A1 (en) * 2004-01-22 2005-08-18 Webasto Ag Curved bodywork component for a vehicle, comprises placing a melt adhesive film on one side of the element, placing cells on the film, and applying another film on top
DE102004003328B4 (en) * 2004-01-22 2006-11-09 Webasto Ag Method for producing a curved body element with solar cells
WO2009114189A2 (en) * 2008-03-14 2009-09-17 Dow Corning Corporation Method of forming a photovoltaic cell module
WO2009114189A3 (en) * 2008-03-14 2009-12-17 Dow Corning Corporation Method of forming a photovoltaic cell module
US8420412B2 (en) 2008-03-14 2013-04-16 Dow Corning Corporation Method of forming a photovoltaic cell module
WO2010143117A3 (en) * 2009-06-08 2011-10-13 3S Swiss Solar Systems Ag Method for producing a solar panel
WO2010143117A2 (en) 2009-06-08 2010-12-16 3S Swiss Solar Systems Ag Method for producing a solar panel
CH701494A1 (en) * 2009-07-21 2011-01-31 3S Swiss Solar Systems Ag Method for laminating plate-shaped elements, comprises connecting a meltable adhesive layer of three material layers in an evacuatable laminating chamber with a flat heating device
EP2457718A3 (en) * 2010-11-24 2016-12-21 The Boeing Company Methods and apparatus for void-free debulking of adhesive bond joints
EP3372386A1 (en) * 2010-11-24 2018-09-12 The Boeing Company Apparatus for void-free debulking of adhesive bond joints
US10434723B2 (en) 2010-11-24 2019-10-08 The Boeing Company Apparatus for void-free debulking of adhesive bonded joints
DE102010061294A1 (en) * 2010-12-16 2012-06-21 Bayerische Motoren Werke Aktiengesellschaft Laminator e.g. multi-opening laminator for manufacturing solar cell, has laminate layer stack made of five layers, that is provided on thermally conductive insert in lower chamber
DE102014211920A1 (en) * 2014-06-23 2015-12-24 Bayerische Motoren Werke Aktiengesellschaft Method for producing a composite pane
CN104972732A (en) * 2015-07-21 2015-10-14 秦皇岛中晟太阳能科技有限公司 Vacuum laminating machine
DE102018101470A1 (en) * 2018-01-23 2019-07-25 Robert Bürkle GmbH Laminating apparatus and method for laminating at least one layer stack
WO2019145308A1 (en) 2018-01-23 2019-08-01 Robert Bürkle GmbH Laminating device and method for laminating at least one layer stack

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