EP2270307A2 - Leaf of a door, a window or similar and method for producing the leaf - Google Patents

Leaf of a door, a window or similar and method for producing the leaf Download PDF

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Publication number
EP2270307A2
EP2270307A2 EP10167440A EP10167440A EP2270307A2 EP 2270307 A2 EP2270307 A2 EP 2270307A2 EP 10167440 A EP10167440 A EP 10167440A EP 10167440 A EP10167440 A EP 10167440A EP 2270307 A2 EP2270307 A2 EP 2270307A2
Authority
EP
European Patent Office
Prior art keywords
profile
wing
support
receiving
edge termination
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
EP10167440A
Other languages
German (de)
French (fr)
Other versions
EP2270307A3 (en
EP2270307B1 (en
Inventor
Ludwig Bauer
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.)
Geze GmbH
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Geze GmbH
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Filing date
Publication date
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Publication of EP2270307A2 publication Critical patent/EP2270307A2/en
Publication of EP2270307A3 publication Critical patent/EP2270307A3/en
Application granted granted Critical
Publication of EP2270307B1 publication Critical patent/EP2270307B1/en
Active legal-status Critical Current
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Classifications

    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/66—Units comprising two or more parallel glass or like panes permanently secured together
    • E06B3/663—Elements for spacing panes
    • E06B3/66309—Section members positioned at the edges of the glazing unit
    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/66—Units comprising two or more parallel glass or like panes permanently secured together
    • E06B3/663—Elements for spacing panes
    • E06B3/66309—Section members positioned at the edges of the glazing unit
    • E06B3/66366—Section members positioned at the edges of the glazing unit specially adapted for units comprising more than two panes or for attaching intermediate sheets
    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/66—Units comprising two or more parallel glass or like panes permanently secured together
    • E06B3/663—Elements for spacing panes
    • E06B3/66309—Section members positioned at the edges of the glazing unit
    • E06B2003/66395—U-shape
    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/66—Units comprising two or more parallel glass or like panes permanently secured together
    • E06B3/6617—Units comprising two or more parallel glass or like panes permanently secured together one of the panes being larger than another

Definitions

  • the invention relates to a wing of a door, a window or the like according to the preamble of patent claim 1 and a method for producing the wing according to the preamble of patent claim 11.
  • a wing of a door, a window or the like which has at least two spaced-apart, hermetically sealed a disc interior surrounding discs.
  • a receiving profile device directed towards the disk interior contains an air drying agent cooperating with the disk interior.
  • An arranged between the discs support and / or edge end profile used to attach fittings or the like on the wing.
  • Both the receiving profile device and the support and / or edge termination profile are each glued to the mutually facing inner surfaces of the two panes.
  • only the adhesive connection of the receiving profile device is realized by the manufacturer, wherein the support and / or edge termination profile is subsequently glued into the outwardly open edge region of the space between the panes of the wing. This subsequent gluing increases the manufacturing cost of the wing.
  • the receiving profile device consists of a single, circumferential profile, the thermal insulation properties are of course limited.
  • the invention has for its object to develop a wing of the type mentioned in such a way that both its manufacturing cost is reduced and its thermal insulation properties can be improved.
  • the receiving profile device consists transversely to the plane of the discs of at least two receiving profiles, which are interconnected by at least one intermediate element.
  • the intermediate element may be made of a material with low thermal conductivity, for example of glass fiber reinforced plastic. As a result, a simple design and effectively acting thermal separation of the two glass panes is achieved.
  • the intermediate element is designed as a web of the support and / or edge termination profile, which engages between two receiving profiles.
  • the intermediate element may be formed as a chamber of the support and / or edge termination profile, which engages between two receiving profiles.
  • the intermediate element may be formed as a separate profile, which is arranged between two receiving profiles and is connected to the support and / or edge termination profile.
  • the intermediate element may be formed as a separate disc which is arranged between two receiving profiles and extends between the outer discs.
  • the support and / or edge termination profile may be made of a material with low thermal conductivity, such as glass fiber reinforced plastic.
  • the surface of the support and / or edge termination profile which is in direct contact with the space between the panes can be made gas-tight in order to hermetically seal the space between the panes and the environment.
  • the support and / or edge termination profile may, for example, have a gas-tight coating or be formed in one piece from a gas-tight material.
  • connection between the intermediate element and the receiving profiles may be formed as a primary seal and thus effect an optimal seal.
  • An optically particularly advantageous embodiment results when the primary seal is designed in the same color as the bond arranged between the outer disks and the support and / or edge termination profile and thus to a measure covering this area, e.g. Glass printing, can be dispensed with.
  • the following method steps can advantageously be carried out: application of a primary seal to the outer surfaces of at least two receiving profiles, application of the receiving profiles provided with the primary seal to corresponding counter-surfaces, e.g. on a profile web of the support and / or edge termination profile, applying the discs on the outer, also provided with the primary seal surfaces of the receiving profiles, pressing the discs with the intermediate receiving profiles and the support and / or edge termination profile, introducing a provided for the final bonding Adhesive in between the outer surfaces of the profile legs of the support and / or edge termination profile and the inner surfaces of the discs existing gaps.
  • Fig. 1 is a door system with a plurality of inventive wings 1 shown in front view.
  • the middle in the drawing wing 1 is formed in this embodiment as a hinged door which is pivotally mounted between two further, each designed as a fixed field wings. Above the hinged door and the fixed fields another, designed as a skylight wing 1 is arranged.
  • the wings 1 are each formed as so-called integrated all-glass wings and have two outer, for example, designed as glass panes discs 2, 3, between which a receiving profile device 5 is arranged circumferentially in the peripheral area.
  • the receiving profile device 5 includes a cooperating with the disc interior air drying agent, including the receiving profile device 5 directed to the disc interior openings.
  • the receiving profile device 5 is arranged at least partially reset to the outer edges of the wings, so that At the edge between the discs 2, 3 and the outer edge of the receiving profile device 5, a receiving space for a support and / or edge end profile 8 is formed.
  • the Fig. 2 shows in a sectional view of the lower edge region of a wing 1, here a section along line AA in Fig. 1 ,
  • the lower end of the wing 1 is formed by a support and / or edge termination profile 8, which is connected by gluing 10 with the inner sides of the discs 2, 3.
  • the support and / or edge termination profile 8 is formed in this embodiment substantially U-shaped, wherein the side profile legs 8a, 8b, which are integrally connected by the profile base 8c, facing down.
  • the two profile legs 8a, 8b with the profile base 8c form a directed towards the outer edge of the wing 1 receiving groove for attachment of the aforementioned fittings, seals or the like.
  • the profile legs 8a, 8b and / or the profile base 8c - not shown here - measures such as grooves, undercuts or the like, which allow the fixation of components.
  • a profile web 8d Directed to the disk interior 4 is integrally arranged on the profile base 8c of the support and / or edge termination profile 8 a profile web 8d.
  • a respective receiving profile 6, 7 of the receiving profile device 5 is attached via a primary seal 9.
  • the outer side surfaces of the two receiving profiles 6, 7 are connected via further primary seals 9 with the inner surfaces of the discs 2, 3.
  • the surfaces of the receiving profiles 6, 7 directed towards the disk interior 4 thus form a hermetic seal of the disk interior 4 with the intermediate end face of the profiled web 8d of the carrying and / or edge finishing profile 8.
  • the support and / or edge end profile 8 may be made of a material with low thermal conductivity, for example, glass fiber reinforced plastic. Since the support and / or edge end profile 8 forms the only direct thermal bridge between the two panes 2, 3, an effective thermal insulation between the two panes 2, 3 is thus achieved. With regard to the choice of material for the receiving profiles 6, 7, care must not be taken to minimize the thermal conductivity, since the profile web forming an intermediate element 8d of the support and / or edge end profile 8 is a heat insulator between the receiving profiles 6, 7.
  • This compressed composite is sufficiently strong for the handling of the wing 1 until the production of the final bond 10, which in another, denoted by D and in Fig. 6 assembly step is carried out by being introduced into the provided between the outer surfaces of the profile legs 8a, 8b of the support and / or edge termination profile 8 and the inner surfaces of the discs 2, 3 spaces 11 provided for the final bonding 10 adhesive.
  • assembly step is carried out by being introduced into the provided between the outer surfaces of the profile legs 8a, 8b of the support and / or edge termination profile 8 and the inner surfaces of the discs 2, 3 spaces 11 provided for the final bonding 10 adhesive.
  • the geometry of the gaps 11 must be matched to the expected loads and the adhesive used.
  • the areas of the panes 2, 3, which cover the receiving profile device 5 and the support and / or edge end profile 8, can be provided with a privacy screen, for example with a printing, coating or the like, in order to make this area optically advantageous.
  • the screen can be dispensed with if the primary seal 9 and the bond 10 are matched in color and the gaps forming the glue gaps are filled with the glue in their entire depth.
  • the Fig. 7 shows a different embodiment of the wing 1.
  • the support and / or edge end profile 8 by the mutually angled profile sections 8e, 8f, 8g, 8h in the middle of a chamber-like area on the side surfaces, which by the on the profile base 8c adjacent profile sections 8g, 8h are formed, the receiving profiles 6, 7 are secured by primary seals 9.
  • the receiving profiles 6, 7 are spaced further apart than in the first embodiment according to Fig. 1 to 6 , so that a further improved heat insulation of the wing 1 is achieved.
  • the support and / or edge termination profile 8 has a profile base 8c, which extends over only about half the width of the support and / or edge termination profile 8.
  • Two adjoining, each angled profile sections 8i, 8j form with the end region of the profile base 8c a laterally open profile groove 8k.
  • a separate profile insert 12 can be inserted and fixed there.
  • the profile insert 12, which forms the intermediate element in this embodiment, is connected via primary seals 9 with the receiving profiles 6, 7.
  • the support and / or edge termination profile 8 of this embodiment allows more Variants, one of which in the Fig. 9 is shown.
  • a third disk 13 arranged between the two outer disks 2, 3 is fastened in the profile groove 8k of the support and / or edge termination profile 8 by means of a holding element 14.
  • This middle pane 13 divides the pane interior 4, which is integral in the preceding exemplary embodiments, into two separate pane interspaces 4a, 4b, so that a further improved heat insulation of the wing 1 is achieved.
  • the components which are connected to the disk interior 4, 4a, 4b must be gas-tight in order to ensure the hermetic sealing of the disk interior 4, 4a, 4b. This can be achieved by the use of gas-tight materials and / or gas-tight surface designs, eg coatings of these components.

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  • Engineering & Computer Science (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Securing Of Glass Panes Or The Like (AREA)

Abstract

The wing (1) has two disks (2,3) arranged at a distance to each other and a mounting profile device (5) aligned to the disk inner space. The mounting profile device comprises an air drying unit cooperating with the disk inner space. The mounting profile device consists of two mounting profiles perpendicular to the plane of the disks, which are connected with each other by an intermediate element. The intermediate element is made of material with small heat conductance value such as glass-fiber reinforced plastic. An independent claim is also included for a method for manufacturing a wing for a door or a window.

Description

Die Erfindung betrifft einen Flügel einer Tür, eines Fensters oder dergleichen nach dem Oberbegriff des Patentanspruchs 1 sowie ein Verfahren zur Herstellung des Flügels nach dem Oberbegriff des Patentanspruchs 11.The invention relates to a wing of a door, a window or the like according to the preamble of patent claim 1 and a method for producing the wing according to the preamble of patent claim 11.

Aus der DE 199 30 831 A1 ist ein Flügel einer Tür, eines Fensters oder dergleichen bekannt, welcher mindestens zwei zueinander beabstandet angeordnete, einen Scheibeninnenraum hermetisch abgedichtet umschießende Scheiben aufweist. Eine zum Scheibeninnenraum gerichtete Aufnahmeprofileinrichtung enthält ein mit dem Scheibeninnenraum zusammenwirkendes Lufttrocknungsmittel. Ein zwischen den Scheiben angeordnetes Trage- und/oder Randabschlussprofil dient zur Befestigung von Beschlägen oder dergleichen am Flügel. Sowohl die Aufnahmeprofileinrichtung als auch das Trage- und/oder Randabschlussprofil sind jeweils mit den einander zugewandten Innenflächen der beiden Scheiben verklebt. In der Praxis wird herstellerseitig lediglich die Klebeverbindung der Aufnahmeprofileinrichtung realisiert, wobei das Trage- und/oder Randabschlussprofil nachträglich in den nach außen offenen Randbereich des Scheibenzwischenraums des Flügels eingeklebt wird. Dieses nachträgliche Einkleben erhöht den Herstellungsaufwand des Flügels. Die Aufnahmeprofileinrichtung besteht aus einem einzigen, umlaufenden Profil, deren thermische Isolationseigenschaften selbstverständlich begrenzt sind.From the DE 199 30 831 A1 a wing of a door, a window or the like is known, which has at least two spaced-apart, hermetically sealed a disc interior surrounding discs. A receiving profile device directed towards the disk interior contains an air drying agent cooperating with the disk interior. An arranged between the discs support and / or edge end profile used to attach fittings or the like on the wing. Both the receiving profile device and the support and / or edge termination profile are each glued to the mutually facing inner surfaces of the two panes. In practice, only the adhesive connection of the receiving profile device is realized by the manufacturer, wherein the support and / or edge termination profile is subsequently glued into the outwardly open edge region of the space between the panes of the wing. This subsequent gluing increases the manufacturing cost of the wing. The receiving profile device consists of a single, circumferential profile, the thermal insulation properties are of course limited.

Der Erfindung liegt die Aufgabe zugrunde, einen Flügel der eingangs genannten Art derart weiterzuentwickeln, dass sowohl sein Herstellungsaufwand verringert wird als auch seine thermische Isolationseigenschaften verbessert werden.The invention has for its object to develop a wing of the type mentioned in such a way that both its manufacturing cost is reduced and its thermal insulation properties can be improved.

Die Aufgabe wird durch die Merkmale des Patentanspruchs 1 sowie des Patentanspruchs 11 gelöst.The object is solved by the features of patent claim 1 and of claim 11.

Die Unteransprüche bilden vorteilhafte Ausgestaltungsmöglichkeiten der Erfindung.The subclaims form advantageous embodiments of the invention.

Die Aufnahmeprofileinrichtung besteht quer zur Ebene der Scheiben aus mindestens zwei Aufnahmeprofilen, welche durch mindestens ein Zwischenelement miteinander verbunden sind. Hierdurch werden die thermischen Isolationseigenschaften wesentlich verbessert.The receiving profile device consists transversely to the plane of the discs of at least two receiving profiles, which are interconnected by at least one intermediate element. As a result, the thermal insulation properties are significantly improved.

Das Zwischenelement kann aus einem Material mit geringem Wärmeleitwert bestehen, beispielsweise aus glasfaserverstärktem Kunststoff. Hierdurch wird eine einfach aufgebaute und effektiv wirkende thermische Trennung der beiden Glasscheiben erreicht.The intermediate element may be made of a material with low thermal conductivity, for example of glass fiber reinforced plastic. As a result, a simple design and effectively acting thermal separation of the two glass panes is achieved.

Eine konstruktiv besonders vorteilhafte Ausgestaltung wird erreicht, indem das Zwischenelement als Steg des Trage- und/oder Randabschlussprofils ausgebildet ist, welcher zwischen zwei Aufnahmeprofile eingreift.A structurally particularly advantageous embodiment is achieved by the intermediate element is designed as a web of the support and / or edge termination profile, which engages between two receiving profiles.

Alternativ kann das Zwischenelement als Kammer des Trage- und/oder Randabschlussprofils ausgebildet sein, welche zwischen zwei Aufnahmeprofile eingreift.Alternatively, the intermediate element may be formed as a chamber of the support and / or edge termination profile, which engages between two receiving profiles.

In einer weiteren alternativen Ausgestaltung kann das Zwischenelement als separates Profil ausgebildet sein, welches zwischen zwei Aufnahmeprofilen angeordnet ist und mit dem Trage- und/oder Randabschlussprofil verbunden ist.In a further alternative embodiment, the intermediate element may be formed as a separate profile, which is arranged between two receiving profiles and is connected to the support and / or edge termination profile.

Alternativ kann das Zwischenelement als separate Scheibe ausgebildet sein, welche zwischen zwei Aufnahmeprofilen angeordnet ist und sich zwischen den äußeren Scheiben erstreckt.Alternatively, the intermediate element may be formed as a separate disc which is arranged between two receiving profiles and extends between the outer discs.

Bei allen vorgenannten Ausführungen kann das Trage- und/oder Randabschlussprofil aus einem Material mit geringem Wärmeleitwert bestehen, beispielsweise aus glasfaserverstärktem Kunststoff.In all the above embodiments, the support and / or edge termination profile may be made of a material with low thermal conductivity, such as glass fiber reinforced plastic.

Die mit dem Scheibenzwischenraum in direktem Kontakt stehende Fläche des Trage- und/oder Randabschlussprofils kann gasdicht ausgebildet sein, um den Scheibenzwischenraum gegenüber der Umgebung hermetisch abzudichten. Das Trage- und/oder Randabschlussprofil kann hierzu beispielsweise eine gasdichte Beschichtung aufweisen oder einstückig aus einem gasdichten Material ausgebildet sein.The surface of the support and / or edge termination profile which is in direct contact with the space between the panes can be made gas-tight in order to hermetically seal the space between the panes and the environment. For this purpose, the support and / or edge termination profile may, for example, have a gas-tight coating or be formed in one piece from a gas-tight material.

Die Verbindung zwischen dem Zwischenelement und den Aufnahmeprofilen kann als Primärdichtung ausgebildet sein und so eine optimale Abdichtung bewirken.The connection between the intermediate element and the receiving profiles may be formed as a primary seal and thus effect an optimal seal.

Eine optisch besonders vorteilhafte Ausführung ergibt sich, wenn die Primärdichtung im gleichen Farbton wie die zwischen den äußeren Scheiben und dem Trage- und/oder Randabschlussprofil angeordnete Verklebung ausgeführt ist und somit auf eine diesen Bereich abdeckende Maßnahme, z.B. Glasbedruckung, verzichtet werden kann.An optically particularly advantageous embodiment results when the primary seal is designed in the same color as the bond arranged between the outer disks and the support and / or edge termination profile and thus to a measure covering this area, e.g. Glass printing, can be dispensed with.

Zur Herstellung des Flügels können vorteilhafterweise die folgenden Verfahrensschritte durchlaufen werden: Aufbringen einer Primärdichtung an den Außenflächen mindestens zweier Aufnahmeprofile, Aufbringen der mit der Primärdichtung versehenen Aufnahmeprofile auf entsprechende Gegenflächen, z.B. auf einen Profilsteg des Trage- und/oder Randabschlussprofils, Aufbringen der Scheiben auf die äußeren, ebenfalls mit der Primärdichtung versehenen Flächen der Aufnahmeprofile, Verpressen der Scheiben mit den dazwischenliegenden Aufnahmeprofilen und dem Trage- und/oder Randabschlussprofil, Einbringen eines für die endgültige Verklebung vorgesehenen Klebstoffs in die zwischen den Außenflächen der Profilschenkel des Trage- und/oder Randabschlussprofils und den Innenflächen der Scheiben bestehenden Zwischenräume.For the manufacture of the wing, the following method steps can advantageously be carried out: application of a primary seal to the outer surfaces of at least two receiving profiles, application of the receiving profiles provided with the primary seal to corresponding counter-surfaces, e.g. on a profile web of the support and / or edge termination profile, applying the discs on the outer, also provided with the primary seal surfaces of the receiving profiles, pressing the discs with the intermediate receiving profiles and the support and / or edge termination profile, introducing a provided for the final bonding Adhesive in between the outer surfaces of the profile legs of the support and / or edge termination profile and the inner surfaces of the discs existing gaps.

Im Nachfolgenden werden Ausführungsbeispiele in der Zeichnung anhand der Figuren näher erläutert.In the following, exemplary embodiments are explained in more detail in the drawing with reference to FIGS.

Dabei zeigen:

Fig. 1
eine Frontansicht einer Türanlage mit mehreren Flügeln;
Fig. 2
eine Schnittdarstellung des Randbereichs eines erfindungsgemäßen Flügels;
Fig. 3
einen ersten Montageschritt eines erfindungsgemäßen Flügels gemäß Fig. 1;
Fig. 4
einen weiteren Montageschritt eines erfindungsgemäßen Flügels ge- mäß Fig. 1;
Fig. 5
einen weiteren Montageschritt eines erfindungsgemäßen Flügels ge- mäß Fig. 1;
Fig. 6
einen weiteren Montageschritt eines erfindungsgemäßen Flügels ge- mäß Fig. 1;
Fig. 7
ein gegenüber Fig. 1 abgewandeltes Ausführungsbeispiel eines erfin- dungsgemäßen Flügels;
Fig. 8
ein gegenüber Fig. 1 und 6 abgewandeltes Ausführungsbeispiel eines erfindungsgemäßen Flügels;
Fig. 9
ein gegenüber Fig. 1, 6 und 7 abgewandeltes Ausführungsbeispiel ei- nes erfindungsgemäßen Flügels.
Showing:
Fig. 1
a front view of a door system with several wings;
Fig. 2
a sectional view of the edge region of a wing according to the invention;
Fig. 3
a first assembly step of a wing according to the invention Fig. 1 ;
Fig. 4
a further assembly step of a wing according to the invention according to Fig. 1 ;
Fig. 5
a further assembly step of a wing according to the invention according to Fig. 1 ;
Fig. 6
a further assembly step of a wing according to the invention according to Fig. 1 ;
Fig. 7
one opposite Fig. 1 modified embodiment of an inventive wing;
Fig. 8
one opposite Fig. 1 and 6 modified embodiment of a wing according to the invention;
Fig. 9
one opposite Fig. 1 . 6 and 7 modified embodiment of a wing according to the invention.

In der Fig. 1 ist eine Türanlage mit mehreren erfindungsgemäßen Flügeln 1 in Frontansicht dargestellt. Der in der Zeichnung mittlere Flügel 1 ist in diesem Ausführungsbeispiel als Schwenktür ausgebildet, welche zwischen zwei weiteren, jeweils als Festfeld ausgebildeten Flügeln 1 schwenkbar gelagert ist. Oberhalb der Schwenktür und der Festfelder ist ein weiterer, als Oberlicht ausgebildeter Flügel 1 angeordnet. Die Flügel 1 sind jeweils als sogenannte integrierte Ganzglasflügel ausgebildet und weisen zwei außenliegende, beispielsweise als Glasscheiben ausgebildete Scheiben 2, 3 auf, zwischen denen in Randbereich umlaufend eine Aufnahmeprofileinrichtung 5 angeordnet ist. Die Aufnahmeprofileinrichtung 5 enthält ein mit dem Scheibeninnenraum zusammenwirkendes Lufttrocknungsmittel, wozu die Aufnahmeprofileinrichtung 5 zum Scheibeninnenraum gerichtete Öffnungen aufweist. Die Aufnahmeprofileinrichtung 5 ist zu den Außenkanten der Flügel zumindest abschnittsweise zurückgesetzt angeordnet, so dass randseitig zwischen den Scheiben 2, 3 und der Außenkante der Aufnahmeprofileinrichtung 5 ein Aufnahmeraum für ein Trage- und/oder Randabschlussprofil 8 gebildet wird. Das Trage- und/oder Randabschlussprofil 8, welches in diesem Aufnahmeraum abschnittweise oder vollständig umlaufend angeordnet werden kann, dient zur Befestigung von Beschlägen, Dichtungen oder dergleichen am Flügel 1.In the Fig. 1 is a door system with a plurality of inventive wings 1 shown in front view. The middle in the drawing wing 1 is formed in this embodiment as a hinged door which is pivotally mounted between two further, each designed as a fixed field wings. Above the hinged door and the fixed fields another, designed as a skylight wing 1 is arranged. The wings 1 are each formed as so-called integrated all-glass wings and have two outer, for example, designed as glass panes discs 2, 3, between which a receiving profile device 5 is arranged circumferentially in the peripheral area. The receiving profile device 5 includes a cooperating with the disc interior air drying agent, including the receiving profile device 5 directed to the disc interior openings. The receiving profile device 5 is arranged at least partially reset to the outer edges of the wings, so that At the edge between the discs 2, 3 and the outer edge of the receiving profile device 5, a receiving space for a support and / or edge end profile 8 is formed. The support and / or edge end profile 8, which can be arranged in sections or completely circulating in this receiving space, is used for fastening fittings, seals or the like on the wing. 1

Die Fig. 2 zeigt in einer Schnittdarstellung den unteren Randbereich eines Flügels 1, hier einen Schnitt entlang Linie A-A in Fig. 1. Der untere Abschluss des Flügels 1 wird gebildet durch ein Trage- und/oder Randabschlussprofil 8, welches durch Verklebungen 10 mit den Innenseiten der Scheiben 2, 3 verbunden ist. Das Trage- und/oder Randabschlussprofil 8 ist in diesem Ausführungsbeispiel im wesentlichen U-förmig ausgebildet, wobei die seitlichen Profilschenkel 8a, 8b, welche durch die Profilbasis 8c einstückig miteinander verbunden sind, nach unten weisen. Somit bilden die beiden Profilschenkel 8a, 8b mit der Profilbasis 8c eine zur Außenkante des Flügels 1 gerichtete Aufnahmenut zur Befestigung der bereits erwähnten Beschläge, Dichtungen oder dergleichen. Selbstverständlich können die Profilschenkel 8a, 8b und/oder die Profilbasis 8c - hier nicht dargestellte - Maßnahmen wie Nuten, Hinterschnitte oder dergleichen aufweisen, welche die Fixierung von Bauteilen ermöglichen.The Fig. 2 shows in a sectional view of the lower edge region of a wing 1, here a section along line AA in Fig. 1 , The lower end of the wing 1 is formed by a support and / or edge termination profile 8, which is connected by gluing 10 with the inner sides of the discs 2, 3. The support and / or edge termination profile 8 is formed in this embodiment substantially U-shaped, wherein the side profile legs 8a, 8b, which are integrally connected by the profile base 8c, facing down. Thus, the two profile legs 8a, 8b with the profile base 8c form a directed towards the outer edge of the wing 1 receiving groove for attachment of the aforementioned fittings, seals or the like. Of course, the profile legs 8a, 8b and / or the profile base 8c - not shown here - measures such as grooves, undercuts or the like, which allow the fixation of components.

Zum Scheibeninnenraum 4 gerichtet ist einstückig auf der Profilbasis 8c des Trage- und/oder Randabschlussprofils 8 ein Profilsteg 8d angeordnet. An jeder Seitenfläche des Profilstegs 8d ist über eine Primärdichtung 9 jeweils ein Aufnahmeprofil 6, 7 der Aufnahmeprofileinrichtung 5 befestigt. Die äußeren Seitenflächen der beiden Aufnahmeprofile 6, 7 sind über weitere Primärdichtungen 9 mit den Innenflächen der Scheiben 2, 3 verbunden. Die zum Scheibeninnenraum 4 gerichteten Flächen der Aufnahmeprofile 6, 7 bilden somit mit der dazwischenliegenden Stirnfläche des Profilstegs 8d des Trage- und/oder Randabschlussprofils 8 eine hermetische Abdichtung des Scheibeninnenraums 4.Directed to the disk interior 4 is integrally arranged on the profile base 8c of the support and / or edge termination profile 8 a profile web 8d. On each side surface of the profile web 8d, a respective receiving profile 6, 7 of the receiving profile device 5 is attached via a primary seal 9. The outer side surfaces of the two receiving profiles 6, 7 are connected via further primary seals 9 with the inner surfaces of the discs 2, 3. The surfaces of the receiving profiles 6, 7 directed towards the disk interior 4 thus form a hermetic seal of the disk interior 4 with the intermediate end face of the profiled web 8d of the carrying and / or edge finishing profile 8.

Das Trage- und/oder Randabschlussprofil 8 kann aus einem Material mit geringem Wärmeleitwert bestehen, beispielsweise aus glasfaserverstärktem Kunststoff. Da das Trage- und/oder Randabschlussprofil 8 die einzige direkte Wärmebrücke zwischen den beiden Scheiben 2, 3 bildet, wird somit eine wirksame thermische Isolierung zwischen den beiden Scheiben 2, 3 erreicht. Hinsichtlich der Materialauswahl für die Aufnahmeprofile 6, 7 muss nicht auf einen möglichst geringen Wärmeleitwert geachtet werden, da der ein Zwischenelement bildende Profilsteg 8d des Trage- und/oder Randabschlussprofils 8 einen Wärmeisolator zwischen den Aufnahmeprofilen 6, 7 darstellt.The support and / or edge end profile 8 may be made of a material with low thermal conductivity, for example, glass fiber reinforced plastic. Since the support and / or edge end profile 8 forms the only direct thermal bridge between the two panes 2, 3, an effective thermal insulation between the two panes 2, 3 is thus achieved. With regard to the choice of material for the receiving profiles 6, 7, care must not be taken to minimize the thermal conductivity, since the profile web forming an intermediate element 8d of the support and / or edge end profile 8 is a heat insulator between the receiving profiles 6, 7.

Die Herstellung des in der Fig. 2 dargestellten Flügels 1 wird anhand der Fig. 3 bis 6 schrittweise erläutert:

  • In einem ersten, mit A bezeichneten und in Fig. 3 dargestellten Montageschritt wird an den Außenflächen der Aufnahmeprofile 6, 7 der für die Primärdichtung 9 vorgesehene Werkstoff, z.B. Butyl, aufgebracht.
The production of in the Fig. 2 illustrated wing 1 is based on the Fig. 3 to 6 explained step by step:
  • In a first, designated A and in Fig. 3 shown assembly step is applied to the outer surfaces of the receiving profiles 6, 7 of the intended for the primary seal 9 material, for example butyl.

In einem weiteren, mit B bezeichneten und in Fig. 4 dargestellten Montageschritt werden die mit der Primärdichtung 9 versehenen Aufnahmeprofile 6, 7 auf entsprechende Gegenflächen des Profilstegs 8d des Trage- und/oder Randabschlussprofils 8 aufgebracht.In another, labeled B and in Fig. 4 the assembly step provided with the primary seal 9 recording profiles 6, 7 are applied to corresponding mating surfaces of the profile web 8 d of the support and / or edge termination profile 8.

In einem weiteren, mit C bezeichneten und in Fig. 5 dargestellten Montageschritt werden die Scheiben 2, 3 auf die mit der Primärdichtung 9 versehenen Außenflächen der Aufnahmeprofile 6, 7 aufgebracht und verpresst, wobei das Material der Primärdichtung 9 verdrückt wird. Es entsteht somit eine luftdichte Verbindung der Aufnahmeprofile 6, 7 sowohl mit den Scheiben 2, 3 als auch mit dem Profilsteg 8d des Trage- und/oder Randabschlussprofils 8.In another, labeled C and in Fig. 5 shown assembly step, the discs 2, 3 applied to the primary seal 9 with the provided outer surfaces of the receiving profiles 6, 7 and pressed, wherein the material of the primary seal 9 is suppressed. This results in an airtight connection of the receiving profiles 6, 7 both with the discs 2, 3 and with the profile web 8d of the support and / or edge termination profile. 8

Dieser verpresste Verbund ist ausreichend stark für die Handhabung des Flügels 1 bis zur Herstellung der endgültigen Verklebung 10, welche in einem weiteren, mit D bezeichneten und in Fig. 6 dargestellten Montageschritt durchgeführt wird, indem in die zwischen den Außenflächen der Profilschenkel 8a, 8b des Trage- und/oder Randabschlussprofils 8 und den Innenflächen der Scheiben 2, 3 bestehenden Zwischenräume 11 der für die endgültige Verklebung 10 vorgesehene Klebstoff eingebracht wird. Je nach Anforderung an Festigkeit, Elastizität, Farbe, Aushärtegeschwindigkeit, eingesetzte Materialien etc. sind hierfür unterschiedliche Klebstoffe denkbar. Die Geometrie der Zwischenräume 11 muss auf die zu erwartenden Belastungen und den eingesetzten Klebstoff abgestimmt werden.This compressed composite is sufficiently strong for the handling of the wing 1 until the production of the final bond 10, which in another, denoted by D and in Fig. 6 assembly step is carried out by being introduced into the provided between the outer surfaces of the profile legs 8a, 8b of the support and / or edge termination profile 8 and the inner surfaces of the discs 2, 3 spaces 11 provided for the final bonding 10 adhesive. Depending on the requirements of strength, elasticity, color, Curing speed, materials used etc. different adhesives are conceivable for this purpose. The geometry of the gaps 11 must be matched to the expected loads and the adhesive used.

Die Bereiche der Scheiben 2, 3, welche die Aufnahmeprofileinrichtung 5 und das Trage- und/oder Randabschlussprofil 8 überdecken, können mit einem Sichtschutz, beispielsweise mit einer Bedruckung, Beschichtung oder dergleichen, versehen werden, um diesen Bereich optisch vorteilhaft zu gestalten. Optional kann auf den Sichtschutz verzichtet werden, wenn die Primärdichtung 9 und die Verklebung 10 farblich aufeinander abgestimmt werden und der die Klebefuge bildende Zwischenräume 11 in ihrer gesamten Tiefe mit dem Klebstoff gefüllt werden.The areas of the panes 2, 3, which cover the receiving profile device 5 and the support and / or edge end profile 8, can be provided with a privacy screen, for example with a printing, coating or the like, in order to make this area optically advantageous. Optionally, the screen can be dispensed with if the primary seal 9 and the bond 10 are matched in color and the gaps forming the glue gaps are filled with the glue in their entire depth.

Die Fig. 7 zeigt ein abweichendes Ausführungsbeispiel des Flügels 1. Anstelle des Profilstegs 8d weist das Trage- und/oder Randabschlussprofil 8 durch die zueinander jeweils abgewinkelten Profilabschnitte 8e, 8f, 8g, 8h in der Mitte einen kammerartigen Bereich auf, an dessen Seitenflächen, welche durch die an die Profilbasis 8c angrenzenden Profilabschnitte 8g, 8h gebildet werden, die Aufnahmeprofile 6, 7 mittels Primärdichtungen 9 befestigt werden. Durch diese Anordnung, bei welcher die gesamte Profilbasis 8c das Zwischenelement bildet, sind die Aufnahmeprofile 6, 7 weiter voneinander beabstandet als beim ersten Ausführungsbeispiel gemäß Fig. 1 bis 6, so dass eine weiter verbesserte Wärmeisolation des Flügels 1 erreicht wird.The Fig. 7 shows a different embodiment of the wing 1. Instead of the profile web 8d, the support and / or edge end profile 8 by the mutually angled profile sections 8e, 8f, 8g, 8h in the middle of a chamber-like area on the side surfaces, which by the on the profile base 8c adjacent profile sections 8g, 8h are formed, the receiving profiles 6, 7 are secured by primary seals 9. By this arrangement, in which the entire profile base 8c forms the intermediate element, the receiving profiles 6, 7 are spaced further apart than in the first embodiment according to Fig. 1 to 6 , so that a further improved heat insulation of the wing 1 is achieved.

Eine weitere Variante des Flügels 1 ist in der Fig. 8 dargestellt. Das Trage- und/oder Randabschlussprofil 8 weist eine Profilbasis 8c auf, welche sich nur über etwa die halbe Breite des Trage- und/oder Randabschlussprofils 8 erstreckt. Zwei anschließende, jeweils abgewinkelte Profilabschnitte 8i, 8j bilden mit dem Endbereich der Profilbasis 8c eine seitlich offene Profilnut 8k. In die Profilnut 8k ist ein separater Profileinsatz 12 einschiebbar und dort festlegbar. Der Profileinsatz 12, welcher in diesem Ausführungsbeispiel das Zwischenelement bildet, wird über Primärdichtungen 9 mit den Aufnahmeprofilen 6, 7 verbunden. Das Trage- und/oder Randabschlussprofil 8 dieses Ausführungsbeispiels gestattet weitere Varianten, von denen eine in der Fig. 9 dargestellt ist. Anstelle des Profileinsatzes 12 ist in der Profilnut 8k des Trage- und/oder Randabschlussprofils 8 mittels eines Halteelements 14 eine dritte, zwischen den beiden außenliegenden Scheiben 2, 3 angeordnete Scheibe 13 befestigt. Diese mittlere Scheibe 13 unterteilt den in der vorhergehenden Ausführungsbeispielen einteiligen Scheibeninnenraum 4 in zwei separate Scheibenzwischenräume 4a, 4b, so dass eine weiter verbesserte Wärmeisolation des Flügels 1 erreicht wird.Another variant of the wing 1 is in the Fig. 8 shown. The support and / or edge termination profile 8 has a profile base 8c, which extends over only about half the width of the support and / or edge termination profile 8. Two adjoining, each angled profile sections 8i, 8j form with the end region of the profile base 8c a laterally open profile groove 8k. In the profile groove 8k a separate profile insert 12 can be inserted and fixed there. The profile insert 12, which forms the intermediate element in this embodiment, is connected via primary seals 9 with the receiving profiles 6, 7. The support and / or edge termination profile 8 of this embodiment allows more Variants, one of which in the Fig. 9 is shown. Instead of the profile insert 12, a third disk 13 arranged between the two outer disks 2, 3 is fastened in the profile groove 8k of the support and / or edge termination profile 8 by means of a holding element 14. This middle pane 13 divides the pane interior 4, which is integral in the preceding exemplary embodiments, into two separate pane interspaces 4a, 4b, so that a further improved heat insulation of the wing 1 is achieved.

Für alle Ausführungsbeispiele gilt, dass die Komponenten, welche mit dem Scheibeninnenraum 4, 4a, 4b in Verbindung stehen, gasdicht ausgebildet sein müssen, um die hermetische Abdichtung des Scheibeninnenraums 4, 4a, 4b zu gewährleisten. Dies lässt sich durch die Verwendung von gasdichten Materialien und/oder gasdichte Oberflächengestaltungen, z.B. Beschichtungen dieser Komponenten erreichen.For all exemplary embodiments, the components which are connected to the disk interior 4, 4a, 4b must be gas-tight in order to ensure the hermetic sealing of the disk interior 4, 4a, 4b. This can be achieved by the use of gas-tight materials and / or gas-tight surface designs, eg coatings of these components.

Liste der ReferenzzeichenList of reference characters

11
Flügelwing
22
Scheibedisc
33
Scheibedisc
44
ScheibeninnenraumDisc interior
4a4a
ScheibeninnenraumDisc interior
4b4b
ScheibeninnenraumDisc interior
55
AufnahmeprofileinrichtungRecording profiler
66
AufnahmeprofilUp profile
77
AufnahmeprofilUp profile
88th
Trage- und/oder RandabschlussprofilCarrying and / or edge finishing profile
8a8a
Profilschenkelprofile leg
8b8b
Profilschenkelprofile leg
8c8c
Profilbasisprofile base
8d8d
Profilstegprofile web
8e8e
Profilabschnittprofile section
8f8f
Profilabschnittprofile section
8g8g
Profilabschnittprofile section
8h8h
Profilabschnittprofile section
8i8i
Profilabschnittprofile section
8j8j
Profilabschnittprofile section
8j8j
Profilnutprofile groove
99
Primärdichtungprimary seal
1010
Verklebungbonding
1111
Zwischenraumgap
1212
Profileinsatzprofile insert
1313
Scheibedisc
1414
Halteelementretaining element
AA
Montageschrittassembly step
BB
Montageschrittassembly step
CC
Montageschrittassembly step
DD
Montageschrittassembly step

Claims (11)

Flügel (1) einer Tür, eines Fensters oder dergleichen,
mit mindestens zwei zueinander beabstandet angeordneten Scheiben (2, 3), mit einer zum Scheibeninnenraum (4) gerichteten Aufnahmeprofileinrichtung (5), welche ein mit dem Scheibeninnenraum (4) zusammenwirkendes Lufttrocknungsmittel enthalten kann,
mit mindestens einen zumindest abschnittsweise zwischen den Scheiben (2, 3) angeordneten Trage- und/oder Randabschlussprofil (8), welches zur Befestigung von Beschlägen, Dichtungen oder dergleichen am Flügel (1) dienen kann,
wobei die vorgenannten Bauteile einen Scheibeninnenraum (4) hermetisch abgedichtet umschießen,
dadurch gekennzeichnet,
dass die Aufnahmeprofileinrichtung (5) quer zur Ebene der Scheiben (2, 3) aus mindestens zwei Aufnahmeprofilen (6, 7) besteht, welche durch mindestens ein Zwischenelement miteinander verbunden sind.Wing (1) a door, a window or the like,
with at least two disks (2, 3) arranged at a distance from one another, with a receiving profile device (5) which is directed towards the disk interior (4) and which may contain an air-drying agent which cooperates with the disk interior (4),
with at least one support and / or edge termination profile (8) arranged at least in sections between the panes (2, 3), which can serve for fastening fittings, seals or the like on the wing (1),
wherein the aforementioned components enclose a disk interior (4) hermetically sealed,
characterized,
that the receiving profile device (5) transversely to the plane of the discs (2, 3) from at least two receiving profiles (6, 7), which are interconnected by at least one intermediate element. Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass das Zwischenelement aus einem Material mit geringem Wärmeleitwert besteht, beispielsweise glasfaserverstärktem Kunststoff.Wing according to claim 1,
characterized in that the intermediate element consists of a material with low thermal conductivity, for example glass fiber reinforced plastic. Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass das Zwischenelement als Profilsteg (8d) des Trage- und/oder Randabschlussprofils (8) ausgebildet ist, welcher zwischen zwei Aufnahmeprofile (6, 7) eingreift.Wing according to claim 1,
characterized in that the intermediate element as a profile web (8d) of the support and / or edge termination profile (8) is formed, which engages between two receiving profiles (6, 7). Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass das Zwischenelement als Kammer des Trage- und/oder Randabschlussprofils (8) ausgebildet ist, welche zwischen zwei Aufnahmeprofile (6, 7) eingreift.Wing according to claim 1,
characterized in that the intermediate element is formed as a chamber of the support and / or edge termination profile (8) which engages between two receiving profiles (6, 7). Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass das Zwischenelement als separater Profileinsatz (12) ausgebildet ist, welcher zwischen zwei Aufnahmeprofilen (6, 7) angeordnet ist und mit dem Trage- und/oder Randabschlussprofil (8) verbunden ist.Wing according to claim 1,
characterized in that the intermediate element is designed as a separate profile insert (12) which is arranged between two receiving profiles (6, 7) and is connected to the carrying and / or edge termination profile (8). Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass das Zwischenelement als separate Scheibe (13) ausgebildet ist, welche zwischen zwei Aufnahmeprofilen (6, 7) angeordnet ist und sich zwischen den äußeren Scheiben (2, 3) erstreckt.Wing according to claim 1,
characterized in that the intermediate element is formed as a separate disc (13) which is arranged between two receiving profiles (6, 7) and extends between the outer discs (2, 3). Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass das Trage- und/oder Randabschlussprofil (8) aus einem Material mit geringem Wärmeleitwert besteht, beispielsweise glasfaserverstärkter Kunststoff.Wing according to claim 1,
characterized in that the support and / or edge end profile (8) consists of a material with low thermal conductivity, such as glass fiber reinforced plastic. Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass die mit dem Scheibenzwischenraum (4) in direktem Kontakt stehende Fläche des Trage- und/oder Randabschlussprofils (8) gasdicht ausgebildet ist.Wing according to claim 1,
characterized in that with the space between the panes (4) in direct contact surface of the support and / or edge termination profile (8) is gas-tight. Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass die Verbindung zwischen dem Zwischenelement und den Aufnahmeprofilen (6, 7) als Primärdichtung (9) ausgebildet ist.Wing according to claim 1,
characterized in that the connection between the intermediate element and the receiving profiles (6, 7) is designed as a primary seal (9). Flügel nach Anspruch 9,
dadurch gekennzeichnet, dass die Primärdichtung (9) auf dem Aufnahmeprofil (6, 7) im gleichen Farbton wie eine zwischen den äußeren Scheiben (2, 3) und dem Trage- und/oder Randabschlussprofil (8) angeordnete Verklebung (10) ausgebildet ist.Wing according to claim 9,
characterized in that the primary seal (9) on the receiving profile (6, 7) in the same color as between the outer discs (2, 3) and the support and / or edge termination profile (8) arranged adhesive (10) is formed. Verfahren zu Herstellung eines Flügels (1) einer Tür, eines Fensters oder dergleichen,
wobei der Flügel (1) mindestens zwei zueinander beabstandet angeordnete Scheiben (2, 3) aufweist, und
wobei der Flügel (1) außerdem eine zum Scheibeninnenraum (4) gerichteten Aufnahmeprofileinrichtung (5) aufweist, welche ein mit dem Scheibeninnenraum (4) zusammenwirkendes Lufttrocknungsmittel enthalten kann, und wobei der Flügel (1) außerdem mindestens ein zumindest abschnittsweise zwischen den Scheiben (2, 3) angeordnetes Trage- und/oder Randabschlussprofil (8) aufweist, welches zur Befestigung von Beschlägen, Dichtungen oder dergleichen am Flügel (1) dienen kann, und
wobei die vorgenannten Bauteile einen Scheibeninnenraum (4) hermetisch abgedichtet umschießen,
dadurch gekennzeichnet, dass zur Herstellung des Flügels (1) folgende Verfahrensschritte durchlaufen werden: Aufbringen einer Primärdichtung (9) an den Außenflächen mindestens zweier Aufnahmeprofile (6, 7), Aufbringen der mit der Primärdichtung (9) versehenen Aufnahmeprofile (6, 7) auf entsprechende Gegenflächen, z.B. auf einen Profilsteg (8d) des Trage- und/oder Randabschlussprofils (8), Aufbringen der Scheiben (2, 3) auf die äußeren, ebenfalls mit der Primärdichtung (9) versehenen Flächen der Aufnahmeprofile (6, 7), Verpressen der Scheiben (2, 3) mit den dazwischenliegenden Aufnahmeprofilen (6, 7) und dem Trage- und/oder Randabschlussprofil (8), Einbringen eines für die endgültige Verklebung (10) vorgesehenen Klebstoffs in die zwischen den Außenflächen der Profilschenkel (8a, 8b) des Trage- und/oder Randabschlussprofils (8) und den Innenflächen der Scheiben (2, 3) bestehenden Zwischenräume (11). Method for producing a wing (1) of a door, a window or the like,
wherein the wing (1) has at least two spaced-apart discs (2, 3), and
wherein the wing (1) further comprises a receiving profile device (5) directed towards the disc interior (4), which may contain an air drying agent cooperating with the disc interior (4), and wherein the wing (1) also comprises at least one at least sectionally between the discs (2 , 3) arranged carrying and / or edge end profile (8), which can serve for fastening of fittings, seals or the like on the wing (1), and
wherein the aforementioned components enclose a disk interior (4) hermetically sealed,
characterized in that for the production of the wing (1) the following process steps are run through: Applying a primary seal (9) to the outer surfaces of at least two receiving profiles (6, 7), Applying the receiving profiles (6, 7) provided with the primary seal (9) to corresponding mating surfaces, eg onto a profile web (8d) of the support and / or edge termination profile (8), Applying the discs (2, 3) on the outer, also with the primary seal (9) provided surfaces of the receiving profiles (6, 7), Pressing the discs (2, 3) with the intermediate receiving profiles (6, 7) and the support and / or edge termination profile (8), Introducing an adhesive provided for the final adhesion (10) into the intermediate spaces (11) existing between the outer surfaces of the profile legs (8a, 8b) of the support and / or edge termination profile (8) and the inner surfaces of the panes (2, 3).
EP10167440.6A 2009-06-29 2010-06-28 Fixed panel, fanlight or swing-wing of a door, a window or similar Active EP2270307B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200910027297 DE102009027297A1 (en) 2009-06-29 2009-06-29 Wing of a door, a window or the like and method for producing the wing

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EP2270307A2 true EP2270307A2 (en) 2011-01-05
EP2270307A3 EP2270307A3 (en) 2013-07-17
EP2270307B1 EP2270307B1 (en) 2015-11-04

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EP2733295A1 (en) * 2012-11-19 2014-05-21 Isophon Glas GmbH Glazing unit
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USD777345S1 (en) 2015-05-21 2017-01-24 Saint-Gobain Glass France Spacer bar
USD778461S1 (en) 2014-02-26 2017-02-07 Saint-Gobain Glass France Spacer bar for insulating glass panes
US10167665B2 (en) 2013-12-12 2019-01-01 Saint-Gobain Glass France Spacer for insulating glazing units, comprising extruded profiled seal
US10190359B2 (en) 2013-12-12 2019-01-29 Saint-Gobain Glass France Double glazing having improved sealing
US10301868B2 (en) 2014-06-27 2019-05-28 Saint-Gobain Glass France Insulated glazing comprising a spacer, and production method
US10344525B2 (en) 2014-06-27 2019-07-09 Saint-Gobain Glass France Insulated glazing with spacer, related methods and uses

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Cited By (9)

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WO2013132210A1 (en) * 2012-03-08 2013-09-12 Anador Limited Glass door system
EP2733295A1 (en) * 2012-11-19 2014-05-21 Isophon Glas GmbH Glazing unit
WO2014198429A1 (en) 2013-06-14 2014-12-18 Saint-Gobain Glass France Spacer for triple glazings
US10167665B2 (en) 2013-12-12 2019-01-01 Saint-Gobain Glass France Spacer for insulating glazing units, comprising extruded profiled seal
US10190359B2 (en) 2013-12-12 2019-01-29 Saint-Gobain Glass France Double glazing having improved sealing
USD778461S1 (en) 2014-02-26 2017-02-07 Saint-Gobain Glass France Spacer bar for insulating glass panes
US10301868B2 (en) 2014-06-27 2019-05-28 Saint-Gobain Glass France Insulated glazing comprising a spacer, and production method
US10344525B2 (en) 2014-06-27 2019-07-09 Saint-Gobain Glass France Insulated glazing with spacer, related methods and uses
USD777345S1 (en) 2015-05-21 2017-01-24 Saint-Gobain Glass France Spacer bar

Also Published As

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DE102009027297A1 (en) 2010-12-30
EP2270307A3 (en) 2013-07-17
EP2270307B1 (en) 2015-11-04
DK2270307T3 (en) 2016-02-15

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