EP2402540A2 - Wing for a window, door or similar - Google Patents

Wing for a window, door or similar Download PDF

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Publication number
EP2402540A2
EP2402540A2 EP11171825A EP11171825A EP2402540A2 EP 2402540 A2 EP2402540 A2 EP 2402540A2 EP 11171825 A EP11171825 A EP 11171825A EP 11171825 A EP11171825 A EP 11171825A EP 2402540 A2 EP2402540 A2 EP 2402540A2
Authority
EP
European Patent Office
Prior art keywords
wing
adhesive
support
edge termination
termination element
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP11171825A
Other languages
German (de)
French (fr)
Other versions
EP2402540A3 (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
Original Assignee
Geze GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Geze GmbH filed Critical Geze GmbH
Publication of EP2402540A2 publication Critical patent/EP2402540A2/en
Publication of EP2402540A3 publication Critical patent/EP2402540A3/en
Withdrawn legal-status Critical Current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
    • E06B3/02—Wings made completely of glass
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00—Suspension arrangements for wings
    • E05D15/06—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/0621—Details, e.g. suspension or supporting guides
    • E05D15/0626—Details, e.g. suspension or supporting guides for wings suspended at the top
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D5/00—Construction of single parts, e.g. the parts for attachment
    • E05D5/02—Parts for attachment, e.g. flaps
    • E05D5/0246—Parts for attachment, e.g. flaps for attachment to glass panels
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2600/00—Mounting or coupling arrangements for elements provided for in this subclass
    • E05Y2600/50—Mounting methods; Positioning
    • E05Y2600/52—Toolless
    • E05Y2600/526—Glueing or cementing
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2800/00—Details, accessories and auxiliary operations not otherwise provided for
    • E05Y2800/20—Combinations of elements
    • E05Y2800/205—Combinations of elements forming a unit
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2800/00—Details, accessories and auxiliary operations not otherwise provided for
    • E05Y2800/20—Combinations of elements
    • E05Y2800/21—Combinations of elements of identical elements, e.g. of identical compression springs
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2800/00—Details, accessories and auxiliary operations not otherwise provided for
    • E05Y2800/67—Materials; Strength alteration thereof
    • E05Y2800/672—Glass

Definitions

  • the invention relates to a wing of a door, a window or the like according to the preamble of patent claim 1.
  • a wing of a door, a window or the like is known.
  • the wing has two mutually spaced discs, also arranged between the discs support and / or edge termination element, which serves for fastening of fittings, seals or the like on the wing.
  • the support and / or edge termination element is connected to the discs by a bond.
  • the uniform adhesive used for the bonding can not have the optimum properties for at least some of these components, since these components also make different demands on the bonding of the support and / or edge termination element, for example due to different forces acting, so that a sufficient stability of the wing may not be guaranteed. Furthermore, the use of a uniform, but due to the fulfillment of all requirements also expensive adhesive over the entire extent of the support and / or edge termination element increase the manufacturing cost of the wing.
  • the invention has for its object to optimize a wing of a door, a window or the like in terms of its stability and its manufacturing cost.
  • the bond has at least two different adhesives.
  • each section using the most suitable adhesives which additionally reduces the manufacturing costs that relatively expensive adhesives only in those areas Carrying and / or edge termination element are arranged, in which they are really needed, while in other areas of the support and / or edge termination element can be used on cheaper adhesives, without reducing the stability and sustainability of the wing.
  • the support and / or edge termination element may have a plurality of adhesive surfaces, wherein the different adhesive surfaces of the support and / or edge termination element are associated with different adhesives.
  • the support and / or edge termination element may comprise a plurality of separate regions in the longitudinal direction, wherein different adhesives are assigned to the different regions of the support and / or edge termination element.
  • the support and / or edge termination element may be formed in one piece or in several pieces.
  • At least in the areas in which different adhesives adjoin one another at least one insert can be arranged between the support and / or edge termination element and the pane, which prevents the various adhesives from mixing with one another.
  • adhesive-free regions can be provided in the longitudinal and / or transverse extent of the support and / or edge termination element.
  • a first adhesive may be formed as a two-component structural adhesive.
  • This adhesive is ideal for anchorage areas of load-bearing fittings or locks because of its high strength. Furthermore, this has Adhesive has a defined curing rate, which speeds up the further processing of the wing.
  • a disadvantage is the high cost of this adhesive, but the manufacturing costs of the wing can be limited by the fact that this adhesive is used according to the invention only in those areas of the support and / or edge termination element, where a particularly high strength of the bond is required.
  • Another adhesive may be formed as a one-component silicone.
  • This high-temperature-resistant, but slow-curing adhesive is optimal for example for corner regions of the wing, since it still ensures a residual load capacity of the wing even at high temperatures, as they may occur, for example in case of fire.
  • This adhesive is relatively expensive, but the manufacturing costs of the wing can be limited by the fact that this adhesive is used according to the invention only in those areas of the support and / or edge termination element where a particularly high residual capacity of the bond is required.
  • Another adhesive may be formed as a two-component sealant.
  • This elastic adhesive is optimal for non-structural areas of the wing, as it ensures good sound insulation properties.
  • This adhesive is relatively inexpensive, which can keep the cost of manufacturing the wing in limits.
  • 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, as can be seen in particular from the sectional view of Fig. 2 is visible, each formed as a so-called integrated all-glass wing and have two outer, designed as glass panes discs 2, 3, between which a receiving profile 5 is circumferentially arranged in peripheral area.
  • the receiving profile 5 contains in a receiving chamber 6 cooperating with the disc interior 4 air drying agent, to which the receiving profile 5 directed to the disc interior 4 openings.
  • the support and / or edge termination element 7, which can be arranged in this free space sections or completely encircling and connected with its adhesive surfaces 7a, 7b by gluing 9 with the inner sides of the discs 2, 3, is used for fastening fittings, seals or the like on the wing 1.
  • the support and / or edge termination element 7 is formed substantially H-shaped, wherein the side profile legs, which are integrally connected by the profile base, facing the outer edge of the wing 1.
  • the two profile legs form with the profile base a directed to the outer edge of the wing 1 receiving space 8 for attachment of the aforementioned fittings, seals or the like.
  • the receiving space 8 is formed as an undercut groove and thus allows the fixation of said components.
  • the space between the receiving profile 5 and a further adhesive surface 7c of the support and / or edge termination element 7 is filled with a backfilling 10, for example a potting compound, whereby the stability of the wing 1 and the hermetic seal are optimized.
  • the discs 2, 3 can, at least in the area covering the receiving profile 5 and the supporting and / or edge-closing element 7, comprise a measure covering this area, e.g. Printing, coating, surface treatment or the like.
  • the Fig. 3 shows a schematic representation of a wing formed as a swing wing 1.
  • two hinges 11 are anchored, which serve for the pivotable mounting of the wing 1 to a stationary component, while at the other vertical outer edge of the wing 1, a lock 12th is arranged.
  • the bonding 9 of the support and / or edge termination element 7 with the discs 2, 3 has in the anchoring regions of the hinges 11 and the lock 12 a first adhesive 14, which may be formed, for example, as a two-component structural adhesive.
  • This adhesive 14 is optimal for these anchoring areas, since it has a high strength. Furthermore, this adhesive 14 has a high, defined curing rate, which accelerates the further processing of the wing 1.
  • a disadvantage is the high cost of this adhesive 14, but the manufacturing costs of the wing 1 can be limited by the fact that this adhesive 14 is used according to the invention only in those areas of the support and / or edge termination element 7, where a particularly high strength of the bond 9 is required.
  • the bonding 9 of the support and / or edge termination element 7 with the discs 2, 3 has a second adhesive 15 in the corner regions of the wing 1, which may be formed, for example, as a high-temperature resistant one-component silicone.
  • This slow-curing adhesive 15 is optimal for these corner regions, as it still ensures a residual capacity of the wing 1 even at high temperatures, as they may occur, for example in case of fire.
  • This adhesive is relatively expensive, but the manufacturing costs of the wing 1 can be limited by the fact that this adhesive 15 is used according to the invention only in those areas of the support and / or edge termination element 7, where a particularly high residual capacity of the bond 9 required is.
  • the Fig. 4 shows in a schematic representation designed as a sliding sash wing 1.
  • two roller carriage 13 are anchored in the support and / or edge termination element 7, which serve for the sliding guide of the wing 1 in a guide rail.
  • the bonding 9 of the support and / or edge termination element 7 with the discs 2, 3 has in the anchoring regions of the roller carriage 13, a first adhesive 14, which may be formed, for example, as in the embodiment described above, as a two-component structural adhesive, with there already described properties.
  • a further adhesive 16 which may be formed, for example, as a two-component sealant.
  • This elastic adhesive 16 is optimal for these areas because it has good sound insulation properties.
  • This adhesive is relatively inexpensive, which can keep the manufacturing cost of the wing 1 in limits.
  • the two-component sealant may be formed as a colored silicone, so that in these areas can be dispensed with additional measures covering the bond 9.
  • inserts 17, 18, respectively may be arranged between the support and / or edge termination element 7 and the panes 2, 3 various adhesives 14, 15, 16 prevent.
  • the inserts 17, 18 may be formed of relatively inexpensive material and are suitable for use in those areas of the support and / or edge termination element 7, in which there are no requirements in terms of strength.
  • adhesive-free regions 19 can be provided along the longitudinal and / or transverse extent of the support and / or edge termination element 7.
  • the type and / or arrangement and / or number of different adhesives 14, 15, 16 can vary compared with the two described embodiments.

Abstract

The wing (1) has two panes (2, 3) i.e. glass panes, arranged at a distance relative to each other. A support and/or edge closure element (7) is sectionally arranged between the panes. The closure element serves for fastening fittings and seals at the wing. The closure element is connected with one of the panes by a bonding, which contains two different adhesives e.g. single component-silicone. The adhesives are associated to different adhesive surfaces of the closure element. Caps are arranged between the closure element and the panes in a region in which the adhesives adjoin each other.

Description

Die Erfindung betrifft einen Flügel einer Tür, eines Fensters oder dergleichen nach dem Oberbegriff des Patentanspruchs 1.The invention relates to a wing of a door, a window or the like according to the preamble of patent claim 1.

Aus der DE 196 34 695 C1 ist ein Flügel einer Tür, eines Fensters oder dergleichen bekannt. Der Flügel weist zwei zueinander beabstandet angeordnete Scheiben auf, ferner ein zwischen den Scheiben angeordneten Trage- und/oder Randabschlusselement, welches zur Befestigung von Beschlägen, Dichtungen oder dergleichen am Flügel dient. Das Trage- und/oder Randabschlusselement ist mit den Scheiben durch eine Verklebung verbunden. In dem Trage- und/oder Randabschlusselement sind verschiedene Elemente, im konkreten Ausführungsbeispiel Scharniere, ein Türschloss sowie mehrere Abschlussprofile, teilweise mit Puffern angeordnet. Der zu der Verklebung verwendete, einheitliche Klebstoff kann für zumindest einige dieser Bauteile nicht die optimalen Eigenschaften aufweisen, da diese Bauteile beispielsweise aufgrund unterschiedlich angreifender Kräfte auch unterschiedliche Anforderungen an die Verklebung des Trage-und/oder Randabschlusselements stellen, so dass eine ausreichende Stabilität des Flügels unter Umständen nicht gewährleistet ist. Ferner kann die Verwendung eines einheitlichen, aber aufgrund der Erfüllung aller Anforderungen auch teuren Klebstoffs über die gesamte Erstreckung des Trage- und/oder Randabschlusselements die Herstellungskosten des Flügels erhöhen.From the DE 196 34 695 C1 a wing of a door, a window or the like is known. The wing has two mutually spaced discs, also arranged between the discs support and / or edge termination element, which serves for fastening of fittings, seals or the like on the wing. The support and / or edge termination element is connected to the discs by a bond. In the support and / or edge termination element are various elements, hinges in the specific embodiment, a door lock and several end profiles, partially arranged with buffers. The uniform adhesive used for the bonding can not have the optimum properties for at least some of these components, since these components also make different demands on the bonding of the support and / or edge termination element, for example due to different forces acting, so that a sufficient stability of the wing may not be guaranteed. Furthermore, the use of a uniform, but due to the fulfillment of all requirements also expensive adhesive over the entire extent of the support and / or edge termination element increase the manufacturing cost of the wing.

Der Erfindung liegt die Aufgabe zugrunde, einen Flügel einer Tür, eines Fensters oder dergleichen hinsichtlich seiner Stabilität sowie seiner Herstellungskosten zu optimieren.The invention has for its object to optimize a wing of a door, a window or the like in terms of its stability and its manufacturing cost.

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

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

Erfindungsgemäß weist die Verklebung mindestens zwei verschiedene Klebstoffe auf. Hierdurch lassen sich in verschiedenen Bereichen des Trage- und/oder Randabschlusselements in denen unterschiedliche Anforderungen hinsichtlich der Eigenschaften der Verklebung bestehen, jeweils abschnittsweise die am besten geeigneten Klebstoffe verwenden, wodurch zusätzlich die Herstellungskosten dadurch gesenkt werden, dass relativ teure Klebstoffen nur in denjenigen Bereichen des Trage- und/oder Randabschlusselements angeordnet werden, in denen sie auch wirklich benötigt werden, während in anderen Bereichen des Trage-und/oder Randabschlusselements auf preisgünstigere Klebstoffe zurückgegriffen werden kann, ohne die Stabilität und Tragfähigkeit des Flügels zu reduzieren.According to the invention, the bond has at least two different adhesives. In this way, in different areas of the support and / or edge termination element in which different requirements exist with respect to the properties of the bond, each section using the most suitable adhesives, which additionally reduces the manufacturing costs that relatively expensive adhesives only in those areas Carrying and / or edge termination element are arranged, in which they are really needed, while in other areas of the support and / or edge termination element can be used on cheaper adhesives, without reducing the stability and sustainability of the wing.

Das Trage- und/oder Randabschlusselement kann mehrere Klebeflächen aufweisen, wobei den verschiedenen Klebeflächen des Trage- und/oder Randabschlusselements verschiedene Klebstoffe zugeordnet sind.The support and / or edge termination element may have a plurality of adhesive surfaces, wherein the different adhesive surfaces of the support and / or edge termination element are associated with different adhesives.

Alternativ oder zusätzlich kann das Trage- und/oder Randabschlusselement in Längsrichtung mehrere separate Bereiche aufweisen, wobei den verschiedenen Bereichen des Trage- und/oder Randabschlusselements verschiedene Klebstoffe zugeordnet sind. Hierbei kann das Trage- und/oder Randabschlusselement einstückig oder mehrstückig ausgebildet sein.Alternatively or additionally, the support and / or edge termination element may comprise a plurality of separate regions in the longitudinal direction, wherein different adhesives are assigned to the different regions of the support and / or edge termination element. Here, the support and / or edge termination element may be formed in one piece or in several pieces.

Zumindest in den Bereichen, in denen verschiedene Klebstoffe aneinander angrenzen, kann zwischen dem Trage- und/oder Randabschlusselement und der Scheibe mindestens eine Einlage angeordnet werden, welche verhindert, dass sich die verschiedenen Klebstoffe miteinander vermischen. Um Kosten zu sparen, können alternativ oder zusätzlich in Längs- und/oder Quererstreckung des Trage-und/oder Randabschlusselements klebstofffreie Bereiche vorgesehen werden.At least in the areas in which different adhesives adjoin one another, at least one insert can be arranged between the support and / or edge termination element and the pane, which prevents the various adhesives from mixing with one another. In order to save costs, alternatively or additionally, adhesive-free regions can be provided in the longitudinal and / or transverse extent of the support and / or edge termination element.

Ein erster Klebstoff kann als Zweikomponenten-Konstruktionsklebstoff ausgebildet sein. Dieser Klebstoff ist für Verankerungsbereiche von tragenden Beschlägen oder Schlössern optimal, da er eine hohe Festigkeit aufweist. Ferner weist dieser Klebstoff eine definierte Aushärtegeschwindigkeit auf, was die Weiterbearbeitung des Flügels beschleunigt. Nachteilig sind die hohen Kosten dieses Klebstoffs, wobei sich die Herstellungskosten des Flügels aber dadurch in Grenzen halten lassen, dass dieser Klebstoff erfindungsgemäß nur in denjenigen Bereichen des Trage- und/oder Randabschlusselements verwendet wird, wo eine besonders hohe Festigkeit der Verklebung gefordert ist.A first adhesive may be formed as a two-component structural adhesive. This adhesive is ideal for anchorage areas of load-bearing fittings or locks because of its high strength. Furthermore, this has Adhesive has a defined curing rate, which speeds up the further processing of the wing. A disadvantage is the high cost of this adhesive, but the manufacturing costs of the wing can be limited by the fact that this adhesive is used according to the invention only in those areas of the support and / or edge termination element, where a particularly high strength of the bond is required.

Ein weiterer Klebstoff kann als Einkomponenten-Silikon ausgebildet sein. Dieser hochtemperaturbeständige, jedoch langsam härtende Klebstoff ist für beispielsweise für Eckbereiche des Flügels optimal, da er auch bei hohen Temperaturen, wie sie beispielsweise im Brandfall auftreten können, noch eine Resttragfähigkeit des Flügels gewährleistet. Auch dieser Klebstoff ist relativ teuer, wobei sich die Herstellungskosten des Flügels aber dadurch in Grenzen halten lassen, dass dieser Klebstoff erfindungsgemäß nur in denjenigen Bereichen des Trage- und/oder Randabschlusselements verwendet wird, wo eine besonders hohe Resttragfähigkeit der Verklebung gefordert ist.Another adhesive may be formed as a one-component silicone. This high-temperature-resistant, but slow-curing adhesive is optimal for example for corner regions of the wing, since it still ensures a residual load capacity of the wing even at high temperatures, as they may occur, for example in case of fire. This adhesive is relatively expensive, but the manufacturing costs of the wing can be limited by the fact that this adhesive is used according to the invention only in those areas of the support and / or edge termination element where a particularly high residual capacity of the bond is required.

Ein weiterer Klebstoff kann als Zweikomponenten-Dichtstoff ausgebildet sein. Dieser elastische Klebstoff ist für nichttragende Bereiche des Flügels optimal, da er gute Schalldämmungseigenschaften gewährleistet. Dieser Klebstoff ist relativ preisgünstig, wodurch sich die Herstellungskosten des Flügels in Grenzen halten lassen.Another adhesive may be formed as a two-component sealant. This elastic adhesive is optimal for non-structural areas of the wing, as it ensures good sound insulation properties. This adhesive is relatively inexpensive, which can keep the cost of manufacturing the wing in limits.

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 erfindungsgemäßen Flügeln;
Fig. 2
eine Schnittdarstellung des Randbereichs eines erfindungsgemäßen Flügels;
Fig. 3
eine schematische Frontansicht eines als Schwenkflügel ausgebildeten Flügels der Türanlage gemäß Fig. 1;
Fig. 4
eine schematische Frontansicht eines abweichenden, als Schiebeflügel ausgebildeten Flügels.
Showing:
Fig. 1
a front view of a door system with several wings according to the invention;
Fig. 2
a sectional view of the edge region of a wing according to the invention;
Fig. 3
a schematic front view of a trained as a swing wing of the door system according to Fig. 1 ;
Fig. 4
a schematic front view of a deviating, designed as a sliding wing sash.

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.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.

Die Flügel 1 sind, wie es insbesondere aus der Schnittdarstellung der Fig. 2 ersichtlich ist, jeweils als sogenannte integrierte Ganzglasflügel ausgebildet und weisen zwei außenliegende, als Glasscheiben ausgebildete Scheiben 2, 3 auf, zwischen denen in Randbereich umlaufend ein Aufnahmeprofil 5 angeordnet ist. Das Aufnahmeprofil 5 enthält in einer Aufnahmekammer 6 ein mit dem Scheibeninnenraum 4 zusammenwirkendes Lufttrocknungsmittel, wozu das Aufnahmeprofil 5 zum Scheibeninnenraum 4 gerichtete Öffnungen aufweist. Das Aufnahmeprofil 5, welches abdichtend mit den Scheiben 2, 3 verbunden, insbesondere verklebt ist und somit eine hermetische Abdichtung des Scheibeninnenraums 4 gegenüber der Umgebung gewährleistet, ist zu den Außenkanten der Flügel 1 zumindest abschnittsweise zurückgesetzt angeordnet, so dass randseitig zwischen den Scheiben 2, 3 und der Außenkante des Aufnahmeprofils 5 ein Freiraum für ein Trage-und/oder Randabschlusselement 7 gebildet wird.The wings 1 are, as can be seen in particular from the sectional view of Fig. 2 is visible, each formed as a so-called integrated all-glass wing and have two outer, designed as glass panes discs 2, 3, between which a receiving profile 5 is circumferentially arranged in peripheral area. The receiving profile 5 contains in a receiving chamber 6 cooperating with the disc interior 4 air drying agent, to which the receiving profile 5 directed to the disc interior 4 openings. The receiving profile 5, which is sealingly connected to the discs 2, 3, in particular glued and thus ensures a hermetic seal of the disc interior 4 from the environment, is at least partially reset to the outer edges of the wing 1, so that edge between the discs 2, 3 and the outer edge of the receiving profile 5, a free space for a support and / or edge termination element 7 is formed.

Das Trage- und/oder Randabschlusselement 7, welches in diesem Freiraum abschnittweise oder vollständig umlaufend angeordnet werden kann und mit seinen Klebeflächen 7a, 7b durch Verklebungen 9 mit den Innenseiten der Scheiben 2, 3 verbunden ist, dient zur Befestigung von Beschlägen, Dichtungen oder dergleichen am Flügel 1. In diesem Ausführungsbeispiel ist das Trage- und/oder Randabschlusselement 7 im wesentlichen H-förmig ausgebildet, wobei die seitlichen Profilschenkel, welche durch die Profilbasis einstückig miteinander verbunden sind, zur Außenkante des Flügels 1 weisen. Somit bilden die beiden Profilschenkel mit der Profilbasis einen zur Außenkante des Flügels 1 gerichteten Aufnahmeraum 8 zur Befestigung der bereits erwähnten Beschläge, Dichtungen oder dergleichen. Der Aufnahmeraum 8 ist als hinterschnittene Nut ausgebildet und ermöglicht somit die Fixierung der genannten Bauteile.The support and / or edge termination element 7, which can be arranged in this free space sections or completely encircling and connected with its adhesive surfaces 7a, 7b by gluing 9 with the inner sides of the discs 2, 3, is used for fastening fittings, seals or the like on the wing 1. In this embodiment, the support and / or edge termination element 7 is formed substantially H-shaped, wherein the side profile legs, which are integrally connected by the profile base, facing the outer edge of the wing 1. Thus, the two profile legs form with the profile base a directed to the outer edge of the wing 1 receiving space 8 for attachment of the aforementioned fittings, seals or the like. The receiving space 8 is formed as an undercut groove and thus allows the fixation of said components.

Der Raum zwischen dem Aufnahmeprofil 5 und einer weiteren Klebefläche 7c des Trage- und/oder Randabschlusselements 7 ist mit einer Verfüllung 10, beispielsweise einer Vergussmasse, ausgefüllt, wodurch die Stabilität des Flügels 1 sowie die hermetische Abdichtung optimiert werden.The space between the receiving profile 5 and a further adhesive surface 7c of the support and / or edge termination element 7 is filled with a backfilling 10, for example a potting compound, whereby the stability of the wing 1 and the hermetic seal are optimized.

Die Scheiben 2, 3 können zumindest in dem das Aufnahmeprofil 5 und das Trage-und/oder Randabschlusselement 7 überdeckenden Bereich eine diesen Bereich abdeckende Maßnahme, z.B. Bedruckung, Beschichtung, Oberflächenbehandlung oder dergleichen, aufweisen.The discs 2, 3 can, at least in the area covering the receiving profile 5 and the supporting and / or edge-closing element 7, comprise a measure covering this area, e.g. Printing, coating, surface treatment or the like.

Die Fig. 3 zeigt in schematischer Darstellung einen als Schwenkflügel ausgebildeten Flügel 1. An der einen vertikalen Außenkante des Flügels 1 sind zwei Scharniere 11 verankert, welche zur schwenkbaren Lagerung des Flügels 1 an einem ortsfesten Bauelement dienen, während an der anderen vertikalen Außenkante des Flügels 1 ein Schloss 12 angeordnet ist.The Fig. 3 shows a schematic representation of a wing formed as a swing wing 1. On the one vertical outer edge of the wing 1, two hinges 11 are anchored, which serve for the pivotable mounting of the wing 1 to a stationary component, while at the other vertical outer edge of the wing 1, a lock 12th is arranged.

Die Verklebung 9 des Trage- und/oder Randabschlusselements 7 mit den Scheiben 2, 3 weist in den Verankerungsbereichen der Scharniere 11 und des Schlosses 12 einen ersten Klebstoff 14 auf, welcher beispielsweise als Zweikomponenten-Konstruktionsklebstoff ausgebildet sein kann. Dieser Klebstoff 14 ist für diese Verankerungsbereiche optimal, da er eine hohe Festigkeit aufweist. Ferner weist dieser Klebstoff 14 eine hohe, definierte Aushärtegeschwindigkeit auf, was die Weiterbearbeitung des Flügels 1 beschleunigt. Nachteilig sind die hohen Kosten dieses Klebstoffs 14, wobei sich die Herstellungskosten des Flügels 1 aber dadurch in Grenzen halten lassen, dass dieser Klebstoff 14 erfindungsgemäß nur in denjenigen Bereichen des Trage- und/oder Randabschlusselements 7 verwendet wird, wo eine besonders hohe Festigkeit der Verklebung 9 gefordert ist.The bonding 9 of the support and / or edge termination element 7 with the discs 2, 3 has in the anchoring regions of the hinges 11 and the lock 12 a first adhesive 14, which may be formed, for example, as a two-component structural adhesive. This adhesive 14 is optimal for these anchoring areas, since it has a high strength. Furthermore, this adhesive 14 has a high, defined curing rate, which accelerates the further processing of the wing 1. A disadvantage is the high cost of this adhesive 14, but the manufacturing costs of the wing 1 can be limited by the fact that this adhesive 14 is used according to the invention only in those areas of the support and / or edge termination element 7, where a particularly high strength of the bond 9 is required.

Die Verklebung 9 des Trage- und/oder Randabschlusselements 7 mit den Scheiben 2, 3 weist in den Eckbereichen des Flügels 1 einen zweiten Klebstoff 15 auf, welcher beispielsweise als hochtemperaturbeständiges Einkomponenten-Silikon ausgebildet sein kann. Dieser langsam härtende Klebstoff 15 ist für diese Eckbereiche optimal, da er auch bei hohen Temperaturen, wie sie beispielsweise im Brandfall auftreten können, noch eine Resttragfähigkeit des Flügels 1 gewährleistet. Auch dieser Klebstoff ist relativ teuer, wobei sich die Herstellungskosten des Flügels 1 aber dadurch in Grenzen halten lassen, dass dieser Klebstoff 15 erfindungsgemäß nur in denjenigen Bereichen des Trage- und/oder Randabschlusselements 7 verwendet wird, wo eine besonders hohe Resttragfähigkeit der Verklebung 9 gefordert ist.The bonding 9 of the support and / or edge termination element 7 with the discs 2, 3 has a second adhesive 15 in the corner regions of the wing 1, which may be formed, for example, as a high-temperature resistant one-component silicone. This slow-curing adhesive 15 is optimal for these corner regions, as it still ensures a residual capacity of the wing 1 even at high temperatures, as they may occur, for example in case of fire. This adhesive is relatively expensive, but the manufacturing costs of the wing 1 can be limited by the fact that this adhesive 15 is used according to the invention only in those areas of the support and / or edge termination element 7, where a particularly high residual capacity of the bond 9 required is.

Die Fig. 4 zeigt in schematischer Darstellung einen als Schiebeflügel ausgebildeten Flügel 1. An der oberen horizontalen Außenkante des Flügels 1 sind im Trage- und/oder Randabschlusselement 7 zwei Rollenwagen 13 verankert, welche zur verschiebbaren Führung des Flügels 1 in einer Führungsschiene dienen.The Fig. 4 shows in a schematic representation designed as a sliding sash wing 1. At the upper horizontal outer edge of the wing 1, two roller carriage 13 are anchored in the support and / or edge termination element 7, which serve for the sliding guide of the wing 1 in a guide rail.

Die Verklebung 9 des Trage- und/oder Randabschlusselements 7 mit den Scheiben 2, 3 weist in den Verankerungsbereichen der Rollenwagen 13 einen ersten Klebstoff 14 auf, welcher beispielsweise, wie beim vorangehend beschriebenen Ausführungsbeispiel, als Zweikomponenten-Konstruktionsklebstoff ausgebildet sein kann, mit den dort bereits beschriebenen Eigenschaften.The bonding 9 of the support and / or edge termination element 7 with the discs 2, 3 has in the anchoring regions of the roller carriage 13, a first adhesive 14, which may be formed, for example, as in the embodiment described above, as a two-component structural adhesive, with there already described properties.

Die Verklebung 9 des Trage- und/oder Randabschlusselements 7 mit den Scheiben 2, 3 weist in den übrigen, d.h. von der Verankerung der Rollenwagen 13 beabstandeten Bereichen des Flügels 1 einen weiteren Klebstoff 16 auf, welcher beispielsweise als Zweikomponenten-Dichtstoff ausgebildet sein kann. Dieser elastische Klebstoff 16 ist für diese Bereiche optimal, da er gute Schalldämmungseigenschaften aufweist. Dieser Klebstoff ist relativ preisgünstig, wodurch sich die Herstellungskosten des Flügels 1 in Grenzen halten lassen.The gluing 9 of the support and / or edge termination element 7 with the panes 2, 3 points in the rest, i. from the anchoring of the roller carriage 13 spaced areas of the wing 1, a further adhesive 16, which may be formed, for example, as a two-component sealant. This elastic adhesive 16 is optimal for these areas because it has good sound insulation properties. This adhesive is relatively inexpensive, which can keep the manufacturing cost of the wing 1 in limits.

Der Zweikomponenten-Dichtstoff kann als eingefärbtes Silikon ausgebildet sein, so dass in diesen Bereichen auf zusätzliche, die Verklebung 9 abdeckende Maßnahmen verzichtet werden kann.The two-component sealant may be formed as a colored silicone, so that in these areas can be dispensed with additional measures covering the bond 9.

Für beide Ausführungsbeispiele gilt, dass in den Bereichen, in denen die verschiedenen Klebstoffe 14, 15, 16 aneinandergrenzen, zwischen dem Trage-und/oder Randabschlusselement 7 und den Scheiben 2, 3 jeweils Einlagen 17, 18 angeordnet sein können, welche ein Vermischen der verschiedenen Klebstoffe 14, 15, 16 verhindern. Die Einlagen 17, 18 können aus relativ kostengünstigem Material ausgebildet sein und bieten sich zur Verwendung in denjenigen Bereichen des Trage- und/oder Randabschlusselements 7 an, in welchem keine Anforderungen hinsichtlich Festigkeit bestehen. Ferner können entlang der Längs-und/oder Quererstreckung des Trage- und/oder Randabschlusselements 7 klebstofffreie Bereiche 19 vorgesehen werden.For both exemplary embodiments, in the regions in which the various adhesives 14, 15, 16 adjoin one another, inserts 17, 18, respectively, may be arranged between the support and / or edge termination element 7 and the panes 2, 3 various adhesives 14, 15, 16 prevent. The inserts 17, 18 may be formed of relatively inexpensive material and are suitable for use in those areas of the support and / or edge termination element 7, in which there are no requirements in terms of strength. Furthermore, adhesive-free regions 19 can be provided along the longitudinal and / or transverse extent of the support and / or edge termination element 7.

Alternativ oder zusätzlich kann gegenüber den beiden beschriebenen Ausführungsbeispielen die Art und/oder Anordnung und/oder Anzahl der verschiedenen Klebstoffe 14, 15, 16 variieren.Alternatively or additionally, the type and / or arrangement and / or number of different adhesives 14, 15, 16 can vary compared with the two described embodiments.

Liste der ReferenzzeichenList of reference characters

11
Flügelwing
22
Scheibedisc
33
Scheibedisc
44
ScheibeninnenraumDisc interior
55
AufnahmeprofilUp profile
66
Aufnahmekammerreceiving chamber
77
Trage- und/oder RandabschlusselementCarrying and / or edge termination element
7a7a
Klebeflächeadhesive surface
7b7b
Klebeflächeadhesive surface
7c7c
Klebeflächeadhesive surface
88th
Aufnahmeraumaccommodation space
99
Verklebungbonding
1010
Verfüllungbackfilling
1111
Scharnierhinge
1212
Schlosslock
1313
Rollenwagenroller carriage
1414
Klebstoffadhesive
1515
Klebstoffadhesive
1616
Klebstoffadhesive
1717
Einlageinlay
1818
Einlageinlay
1919
klebstofffreier Bereichadhesive-free area

Claims (8)

Flügel (1) einer Tür, eines Fensters oder dergleichen,
mit mindestens zwei zueinander beabstandet angeordneten Scheiben (2, 3), mit mindestens einem zumindest abschnittsweise zwischen den Scheiben (2, 3) angeordneten Trage- und/oder Randabschlusselement (7), welches zur Befestigung von Beschlägen, Dichtungen oder dergleichen am Flügel (1) dienen kann,
wobei das Trage- und/oder Randabschlusselement (7) mit mindestens einer der Scheiben (2, 3) durch eine Verklebung (9) verbunden ist,
dadurch gekennzeichnet,
dass die Verklebung (9) mindestens zwei verschiedene Klebstoffe (14, 15, 16) aufweist.Wing (1) a door, a window or the like,
with at least two spaced-apart discs (2, 3), with at least one at least partially between the discs (2, 3) arranged carrying and / or edge termination element (7), which for attachment of fittings, seals or the like on the wing (1 ),
wherein the support and / or edge termination element (7) is connected to at least one of the panes (2, 3) by a bond (9),
characterized,
that the gluing (9) has at least two different adhesives (14, 15, 16). Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass das Trage- und/oder Randabschlusselement (7) mehrere Klebeflächen (7a, 7b, 7c) aufweist, wobei den verschiedenen Klebeflächen des Trage- und/oder Randabschlusselements (7) verschiedene Klebstoffe (14, 15, 16) zugeordnet sind.Wing according to claim 1,
characterized in that the support and / or edge termination element (7) has a plurality of adhesive surfaces (7a, 7b, 7c), wherein the different adhesive surfaces of the support and / or edge termination element (7) are associated with different adhesives (14, 15, 16) , Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass das Trage- und/oder Randabschlusselement (7) in Längs- und/oder Querrichtung mehrere separate Bereiche aufweist, wobei den verschiedenen Bereichen des Trage- und/oder Randabschlusselements (7) verschiedene Klebstoffe (14, 15, 16) zugeordnet sind.Wing according to claim 1,
characterized in that the support and / or edge termination element (7) has a plurality of separate regions in the longitudinal and / or transverse direction, the various regions of the support and / or edge termination element (7) assigned to different adhesives (14, 15, 16) are. Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass zumindest in den Bereichen, in denen verschiedene Klebstoffe (14, 15, 16) aneinander angrenzen, zwischen dem Trage- und/oder Randabschlusselement (7) und der Scheibe (2, 3) mindestens eine Einlage (17, 18) angeordnet ist.Wing according to claim 1,
characterized in that at least in the areas in which different adhesives (14, 15, 16) adjoin one another, at least one insert (17, 18) is provided between the support and / or edge termination element (7) and the pane (2, 3). is arranged. Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass zumindest in den Bereichen, in denen verschiedene Klebstoffe (14, 15, 16) aneinander angrenzen, zwischen dem Trage- und/oder Randabschlusselement (7) und der Scheibe (2, 3) mindestens ein klebstofffreier Bereich (19) angeordnet ist.Wing according to claim 1,
characterized in that at least in the areas in which different adhesives (14, 15, 16) adjoin one another, at least one adhesive-free area (19) is arranged between the support and / or edge termination element (7) and the pane (2, 3) is. Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass der Klebstoff (14) als Zweikomponenten-Konstruktionsklebstoff ausgebildet ist.Wing according to claim 1,
characterized in that the adhesive (14) is designed as a two-component structural adhesive. Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass der Klebstoff (15) als Einkomponenten-Silikon ausgebildet ist.Wing according to claim 1,
characterized in that the adhesive (15) is formed as a one-component silicone. Flügel nach Anspruch 1,
dadurch gekennzeichnet, dass der Klebstoff (16) als Zweikomponenten-Dichtstoff ausgebildet ist.Wing according to claim 1,
characterized in that the adhesive (16) is designed as a two-component sealant.
EP11171825.0A 2010-07-01 2011-06-29 Wing for a window, door or similar Withdrawn EP2402540A3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102010030786.6A DE102010030786B4 (en) 2010-07-01 2010-07-01 Wing of a door, a window or the like

Publications (2)

Publication Number Publication Date
EP2402540A2 true EP2402540A2 (en) 2012-01-04
EP2402540A3 EP2402540A3 (en) 2016-08-17

Family

ID=44558433

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DE (1) DE102010030786B4 (en)

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ITUD20130082A1 (en) * 2013-06-14 2014-12-15 Modulnova S R L MULTI-LAYER PANEL AND ITS CONSTRUCTION METHOD
CN105464545A (en) * 2016-01-04 2016-04-06 浙江科森玻璃科技有限公司 Solid-wood hidden-frame glass door plate
EP3192960A1 (en) 2016-01-12 2017-07-19 AGC Glass Europe Insulating glass unit and methods to produce it
EP3192959A1 (en) 2016-01-12 2017-07-19 AGC Glass Europe Method to produce insulating glass units and insulating glass units
WO2019141670A1 (en) 2018-01-16 2019-07-25 Agc Glass Europe Frameless casement with u-shaped profile

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DE29814676U1 (en) * 1998-01-24 1998-11-19 Ver Glaswerke Gmbh Window or door sash made of two panes of glass
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITUD20130082A1 (en) * 2013-06-14 2014-12-15 Modulnova S R L MULTI-LAYER PANEL AND ITS CONSTRUCTION METHOD
CN105464545A (en) * 2016-01-04 2016-04-06 浙江科森玻璃科技有限公司 Solid-wood hidden-frame glass door plate
EP3192960A1 (en) 2016-01-12 2017-07-19 AGC Glass Europe Insulating glass unit and methods to produce it
EP3192959A1 (en) 2016-01-12 2017-07-19 AGC Glass Europe Method to produce insulating glass units and insulating glass units
WO2019141670A1 (en) 2018-01-16 2019-07-25 Agc Glass Europe Frameless casement with u-shaped profile

Also Published As

Publication number Publication date
DE102010030786A1 (en) 2012-01-05
DE102010030786B4 (en) 2017-08-10
EP2402540A3 (en) 2016-08-17

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