EP2045426A1 - Mounting device of a pivot bearing of a window - Google Patents

Mounting device of a pivot bearing of a window Download PDF

Info

Publication number
EP2045426A1
EP2045426A1 EP07019588A EP07019588A EP2045426A1 EP 2045426 A1 EP2045426 A1 EP 2045426A1 EP 07019588 A EP07019588 A EP 07019588A EP 07019588 A EP07019588 A EP 07019588A EP 2045426 A1 EP2045426 A1 EP 2045426A1
Authority
EP
European Patent Office
Prior art keywords
wing
steel part
arrangement according
steel
attachment
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
EP07019588A
Other languages
German (de)
French (fr)
Other versions
EP2045426B1 (en
Inventor
Nils Unseld
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.)
Roto Frank AG
Original Assignee
Roto Frank AG
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 Roto Frank AG filed Critical Roto Frank AG
Priority to EP07019588.8A priority Critical patent/EP2045426B1/en
Priority to PL07019588T priority patent/PL2045426T3/en
Priority to ES07019588.8T priority patent/ES2464594T3/en
Priority to CN2008101689548A priority patent/CN101403267B/en
Publication of EP2045426A1 publication Critical patent/EP2045426A1/en
Application granted granted Critical
Publication of EP2045426B1 publication Critical patent/EP2045426B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • 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
    • E05D15/48—Suspension arrangements for wings allowing alternative movements
    • E05D15/52—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
    • E05D15/5205—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis with horizontally-extending checks
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00—Hinges or pivots of special construction
    • E05D7/04—Hinges adjustable relative to the wing or the frame
    • E05D7/0415—Hinges adjustable relative to the wing or the frame with adjusting drive means
    • E05D7/0423—Screw-and-nut mechanisms
    • 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
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
    • E05Y2900/132—Doors
    • 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
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
    • E05Y2900/148—Windows

Definitions

  • the invention relates to a wing attachment assembly of a turn or tilt and turn bearing for a window, a door or the like.
  • Object of the present invention is therefore to provide a wing attachment assembly which has few parts and which is inexpensive to produce.
  • a wing attachment assembly of a turn or tilt and turn bearings for a window, a door or the like.
  • a steel part which has a guide portion for guiding the steel part in a drive rod channel of a wing , and a wing mounting bracket connected to the steel part.
  • Such a wing attachment arrangement is very robust with a very simple technical construction. Characterized in that the steel part has a guide portion which is guided in a drive rod channel of the wing, the wing attachment arrangement is already fixed in one dimension on the wing and requires none additional additional attachment.
  • the guide section is preferably designed so that it has a sufficient width to be overlapped on two opposite sides of the undercut drive rod channel.
  • the use of steel has the advantage that the fitting can be made very stable on the one hand and on the other hand, that the steel is easy and inexpensive to work, with a low price of raw materials.
  • the steel part can be produced particularly cost-effectively if it is designed as a punched-bent part or as a laser-cut bent part.
  • the steel part is preferably punched or cut in one piece from a sheet and then bent into the required shape.
  • the steel part has a partially parallel to the guide portion extending tensile receiving part. This can be particularly well absorbed by the wing weight tensile forces. The stability of the wing attachment assembly is increased.
  • the free end of the guide section is connected to the Buchfactteil.
  • the guide portion may be connected to the Buchfactteil by a rivet or a welding point.
  • the Buchauteil has an opening in which a tab of the guide portion is mounted.
  • the wing mounting bracket is connected to the steel part via a set screw.
  • the distance between the steel part and wing mounting bracket is about the screw. This allows you to adjust the position of the sash relative to the fixed frame.
  • a steel part which engages in sections behind the steel is provided into which the adjusting screw is screwed.
  • the nut can be dimensioned so that a sufficiently large contact surface of the nut exists on the steel part.
  • the nut is arranged at the location of the steel part, where the steel part is bent over and passes from the Switzerlandfactteil in the guide part.
  • the steel part preferably has a passage opening in this area, which can pass through the adjusting screw. The passage opening can be punched out during the production of the steel part or cut out with a laser.
  • the wing mounting bracket has a stop for the steel part.
  • the steel part can be properly positioned during assembly, in particular to be positioned in a so-called zero position. During assembly, the stop thus determines the position of the steel part.
  • the guide portion is materially connected to the attachment portion for attachment of the wing-side hinge part.
  • the guide portion and the attachment portion can be formed integrally.
  • the attachment portion can be realized in particular by bending or folding relative to the guide portion.
  • the steel part is bent wing mounting bracket side and the free end is connected to the guide portion.
  • the free end can be riveted, for example, with the guide section.
  • a window, a door or the like falls within the scope of the invention, a window, a door or the like. With a wing mounting arrangement described above.
  • FIG. 1 shows an upper corner portion of a window 10 with a fixed frame 11 and a wing frame 12 of a wing 13.
  • the wing 13 is pivotally connected to the fixed frame 11 via a hinge assembly 14, which is formed in the embodiment as a pivot bearing, wherein the hinge assembly 14 a wing-side band member 15 and a welt-side band member 16 includes.
  • the wing-side band part 15 is with a wing attachment assembly 20, which will be described in more detail below, connected.
  • the wing attachment assembly 20 is shown in a perspective view.
  • the wing attachment assembly 20 includes a steel member 21 and a wing attachment bracket 22.
  • the steel member 21 is integrally formed in the embodiment. It was made by punching out a sheet and then bending it. It comprises a guide section 23, which is guided in a drive rod channel of the wing 13. Furthermore, the steel part 21 comprises a Switzerlandfactteil 24, from which a fastening portion 25 is bent for fastening the wing-side hinge part 15.
  • the free end 26 of the guide portion 23 is attached via a rivet 27 to the Werner 24.
  • the steel part 21 is bent.
  • the steel part 21 is engaged behind by a cylindrical nut 28.
  • an adjusting screw 29 is screwed, which also extends through the wing mounting bracket 22.
  • the wing mounting bracket 22 is bolted by means of fasteners 30,31 with the casement 12.
  • the distance between the wing mounting bracket 22 and the steel part 21 can be changed.
  • the steel part 21 abuts against a stop 32 of the wing mounting bracket 22.
  • FIG. 3 is a plan view of the wing attachment assembly 21, in particular the Switzerlandfactteil 24 and the wing mounting bracket 22 shown.
  • the stop 32 can be seen, to which the steel part 21 abuts.
  • the stop 32 is connected via a predetermined breaking point with the remaining wing mounting bracket 22, in particular a mounting portion 33. This is in the enlarged detail of the FIG. 4 to recognize.
  • the predetermined breaking point is provided with the reference numeral 35.
  • the sash frame 12 is shown partially cut in order to better recognize the arrangement of the sash mounting arrangement 20 on the sash.
  • the guide portion 23 is inserted into a drive rod channel 36.
  • the wing attachment assembly 20 is already fixed in one of two dimensions and can only be moved in the wing circumferential direction.
  • a determination in the wing circumferential direction is made by the wing mounting bracket 22, the mounting portion 33 is screwed to the sash 12.
  • the adjusting screw 29 By adjusting the adjusting screw 29, the position of the wing-side hinge part 15 with respect to the wing 13 and the wing frame 12 can be changed. As a result, the distance of the wing 13 is changed to the fixed enclosure 11.
  • FIG. 6 shows a sectional view along the line VI - VI of FIG. 5 , Here it can be seen that the guide section 23 is guided in the drive rod channel 36 and is overlapped by legs 37, 38 of the cross-sectionally C-shaped drive rod channel 36.
  • the Switzerlandteil 24 is disposed above the drive rod channel 26.
  • FIG. 7 an embodiment of a steel part 50 is shown, in which a fastening portion 51 for attaching the wing-side hinge part 15 connects to the guide portion 52 materially. Between the actual guide portion 52 and the mounting portion 51, a step-like increase 53 is provided. At its wing mounting bracket side End 54, the steel part 50 is bent and fixed with its free end 55 to the guide portion 52, in particular riveted to this.
  • the embodiment according to the FIG. 8 essentially corresponds to the FIG. 7 with the difference that the guide section 52 is completely straight and no step 53 as in FIG. 7 followed. Also in this embodiment, the attachment portion 51 is materially connected to the guide portion 52. In the FIG. 8 the steel part is provided with the reference numeral 60.

Abstract

The arrangement (20) has a steel part (21) with a guide section (23) for guiding the steel part into a connecting rod channel of a wing. A wing fixing stand (22) is connected with the steel part, and the steel part is designed as a punching-bending part or laser-cut bending part. The steel part has a sectioned traction unit (24) running parallel to the guide section, where a free end (26) of the guide section is connected with the traction unit. The wing fixing stand is connected with the steel part via a set screw (29).

Description

Die Erfindung betrifft eine Flügelbefestigungsanordnung eines Dreh- oder Dreh-Kipp-Lagers für ein Fenster, eine Tür oder dgl.The invention relates to a wing attachment assembly of a turn or tilt and turn bearing for a window, a door or the like.

Zur dreh- und/oder kippbaren Befestigung eines Flügels an einer festen Einfassung ist es bekannt, ein entsprechendes Lager zu verwenden. Ein derartiges Lager weist daher eine einfassungsseitige und eine flügelseitige Befestigungsanordnung auf. Bislang wurden derartige Befestigungsanordnungen nahezu ausschließlich als Zink - Druck-Gussteile hergestellt. Wegen des steigenden Rohstoffpreises von Zink ist es jedoch erforderlich, nach neuen Befestigungsmöglichkeiten zu suchen.For rotatable and / or tiltable attachment of a wing to a fixed enclosure, it is known to use a corresponding bearing. Such a bearing therefore has an enclosure-side and a wing-side fastening arrangement. So far, such fastening arrangements have been produced almost exclusively as zinc-pressure castings. Due to the rising price of zinc, however, it is necessary to look for new mounting options.

Aufgabe der vorliegenden Erfindung ist es daher, eine Flügelbefestigungsanordnung bereitzustellen, welche wenige Teile aufweist und die kostengünstig herstellbar ist.Object of the present invention is therefore to provide a wing attachment assembly which has few parts and which is inexpensive to produce.

Gelöst wird diese Aufgabe erfindungsgemäß auf einfache und überraschende Art und Weise durch eine Flügelbefestigungsanordnung eines Dreh- oder Dreh-Kipp-Lagers für ein Fenster, eine Tür oder dgl. mit einem Stahlteil, welches einen Führungsabschnitt zur Führung des Stahlteils in einem Treibstangenkanal eines Flügels aufweist, und einem Flügelbefestigungsbock, der mit dem Stahlteil verbunden ist. Eine derartige Flügelbefestigungsanordnung ist sehr robust bei einem gleichzeitig sehr einfachen technischen Aufbau. Dadurch, dass das Stahlteil einen Führungsabschnitt aufweist, der in einem Treibstangenkanal des Flügels geführt ist, ist die Flügelbefestigungsanordnung bereits in einer Dimension am Flügel festgelegt und bedarf keiner weiteren zusätzlichen Befestigungsmöglichkeit. Der Führungsabschnitt ist dabei vorzugsweise so ausgestaltet, dass er eine ausreichende Breite aufweist, um an zwei gegenüberliegenden Seiten von dem hinterschnittenen Treibstangenkanal übergriffen zu werden. Die Verwendung von Stahl hat den Vorteil, dass der Beschlag dadurch zum einen sehr stabil ausgebildet werden kann und zum anderen, dass der Stahl einfach und kostengünstig bearbeitbar ist, bei einem geringen Rohstoffpreis.This object is achieved according to the invention in a simple and surprising manner by a wing attachment assembly of a turn or tilt and turn bearings for a window, a door or the like. With a steel part, which has a guide portion for guiding the steel part in a drive rod channel of a wing , and a wing mounting bracket connected to the steel part. Such a wing attachment arrangement is very robust with a very simple technical construction. Characterized in that the steel part has a guide portion which is guided in a drive rod channel of the wing, the wing attachment arrangement is already fixed in one dimension on the wing and requires none additional additional attachment. The guide section is preferably designed so that it has a sufficient width to be overlapped on two opposite sides of the undercut drive rod channel. The use of steel has the advantage that the fitting can be made very stable on the one hand and on the other hand, that the steel is easy and inexpensive to work, with a low price of raw materials.

Besonders kostengünstig lässt sich das Stahlteil herstellen, wenn es als Stanz-Biegeteil oder lasergeschnittenes Biegeteil ausgebildet ist. Insbesondere ist das Stahlteil vorzugsweise einstückig aus einem Blech ausgestanzt oder ausgeschnitten und anschließend in die erforderliche Form gebogen.The steel part can be produced particularly cost-effectively if it is designed as a punched-bent part or as a laser-cut bent part. In particular, the steel part is preferably punched or cut in one piece from a sheet and then bent into the required shape.

Besondere Vorteile ergeben sich, wenn das Stahlteil einen abschnittsweise parallel zum Führungsabschnitt verlaufenden Zugaufnahmeteil aufweist. Dadurch können durch das Flügelgewicht bewirkte Zugkräfte besonders gut aufgenommen werden. Die Stabilität der Flügelbefestigungsanordnung wird erhöht.Particular advantages arise when the steel part has a partially parallel to the guide portion extending tensile receiving part. This can be particularly well absorbed by the wing weight tensile forces. The stability of the wing attachment assembly is increased.

Gemäß einer bevorzugten Weiterbildung kann vorgesehen sein, dass das freie Ende des Führungsabschnitts mit dem Zugaufnahmeteil verbunden ist. Dadurch erfolgt eine weitere Aussteifung der Flügelbefestigungsanordnung. Insbesondere kann der Führungsabschnitt mit dem Zugaufnahmeteil durch einen Niet oder einen Schweißpunkt verbunden sein. Weiterhin ist es denkbar, dass das Zugaufnahmeteil eine Öffnung aufweist, in die eine Lasche des Führungsabschnitts eingehängt ist.According to a preferred development it can be provided that the free end of the guide section is connected to the Zugaufnahmeteil. This results in a further stiffening of the wing attachment arrangement. In particular, the guide portion may be connected to the Zugaufnahmeteil by a rivet or a welding point. Furthermore, it is conceivable that the Zugaufnahmeteil has an opening in which a tab of the guide portion is mounted.

Bei einer besonders bevorzugten Ausführungsform kann vorgesehen sein, dass der Flügelbefestigungsbock mit dem Stahlteil über eine Stellschraube verbunden ist. Über die Stellschraube kann der Abstand zwischen Stahlteil und Flügelbefestigungsbock eingestellt werden. Dadurch lässt sich die Position des Flügels in Bezug zum festen Rahmen einstellen.In a particularly preferred embodiment it can be provided that the wing mounting bracket is connected to the steel part via a set screw. About the screw, the distance between the steel part and wing mounting bracket. This allows you to adjust the position of the sash relative to the fixed frame.

Während es grundsätzlich denkbar ist, in dem Stahlteil ein Gewinde vorzusehen, in das die Stellschraube eingeschraubt ist, ist erfindungsgemäß vorteilhafterweise eine das Stahlteil abschnittsweise hintergreifende Mutter vorgesehen, in die die Stellschraube eingeschraubt ist. Dadurch kann der Bearbeitungsschritt des Gewindeschneidens in das Stahlteil vermieden werden. Die Mutter kann so dimensioniert werden, dass eine ausreichend große Anlagefläche der Mutter an dem Stahlteil existiert. Vorzugsweise ist die Mutter an der Stelle des Stahlteils angeordnet, wo das Stahlteil umgebogen ist und vom Zugaufnahmeteil in das Führungsteil übergeht. Das Stahlteil weist in diesem Bereich vorzugsweise eine Durchgangsöffnung auf, die die Stellschraube durchgreifen kann. Die Durchgangsöffnung kann bei der Herstellung des Stahlteils ausgestanzt oder mit einem Laser ausgeschnitten werden.While it is generally conceivable to provide a thread in the steel part into which the adjusting screw is screwed in, according to the invention advantageously a steel part which engages in sections behind the steel is provided into which the adjusting screw is screwed. Thereby, the machining step of tapping into the steel part can be avoided. The nut can be dimensioned so that a sufficiently large contact surface of the nut exists on the steel part. Preferably, the nut is arranged at the location of the steel part, where the steel part is bent over and passes from the Zugaufnahmeteil in the guide part. The steel part preferably has a passage opening in this area, which can pass through the adjusting screw. The passage opening can be punched out during the production of the steel part or cut out with a laser.

Bei einer Ausgestaltung der Erfindung kann vorgesehen sein, dass der Flügelbefestigungsbock einen Anschlag für das Stahlteil aufweist. Durch diese Maßnahme kann das Stahlteil bei der Montage richtig positioniert werden, insbesondere in einer so genannten Nullstellung positioniert werden. Bei der Montage legt also der Anschlag die Position des Stahlteils fest.In one embodiment of the invention can be provided that the wing mounting bracket has a stop for the steel part. By this measure, the steel part can be properly positioned during assembly, in particular to be positioned in a so-called zero position. During assembly, the stop thus determines the position of the steel part.

Weitere Vorteile ergeben sich, wenn der Anschlag über eine Sollbruchstelle mit dem Befestigungsabschnitt des Flügelbefestigungsbocks verbunden ist. Durch diese Maßnahme ist nach der Montage auch eine Verstellung des Stahlteils in Richtung Flügelbefestigungsbock möglich, wenn beispielsweise die Falzluft zwischen der festen Einfassung und dem Flügel verringert werden muss.Further advantages arise when the stop is connected via a predetermined breaking point with the mounting portion of the wing mounting bracket. By this measure, an adjustment of the steel part in the direction of wing mounting bracket is possible after assembly, if, for example, the seaming air between the fixed enclosure and the wing must be reduced after assembly.

Weitere Vorteile ergeben sich, wenn der Führungsabschnitt materialschlüssig mit dem Befestigungsabschnitt zur Befestigung des flügelseitigen Bandteils verbunden ist. Dadurch können der Führungsabschnitt und der Befestigungsabschnitt einstückig ausgebildet werden. Der Befestigungsabschnitt kann insbesondere durch Abbiegen oder Abkanten gegenüber dem Führungsabschnitt realisiert werden.Further advantages arise when the guide portion is materially connected to the attachment portion for attachment of the wing-side hinge part. Thereby, the guide portion and the attachment portion can be formed integrally. The attachment portion can be realized in particular by bending or folding relative to the guide portion.

Bei einer Ausgestaltung der Erfindung kann vorgesehen sein, dass das Stahlteil flügelbefestigungsbockseitig umgebogen ist und das freie Ende mit dem Führungsabschnitt verbunden ist. Dabei kann das freie Ende beispielsweise mit dem Führungsabschnitt vernietet sein.In one embodiment of the invention can be provided that the steel part is bent wing mounting bracket side and the free end is connected to the guide portion. In this case, the free end can be riveted, for example, with the guide section.

In den Rahmen der Erfindung fällt außerdem ein Drehlager oder ein Dreh-Kipp-Lager mit einer oben beschriebenen Flügelbefestigungsanordnung.In the scope of the invention also falls a pivot bearing or a turn-tilt bearing with a wing mounting arrangement described above.

Außerdem fällt in den Rahmen der Erfindung ein Fenster, eine Tür oder dgl. mit einer oben beschriebenen Flügelbefestigungsanordnung.In addition, falls within the scope of the invention, a window, a door or the like. With a wing mounting arrangement described above.

Weitere Merkmale und Vorteile der Erfindung ergeben sich aus der nachfolgenden Beschreibung von Ausführungsbeispielen der Erfindung, anhand der Figuren der Zeichnung, die erfindungswesentliche Einzelheiten zeigen, und aus den Ansprüchen. Die einzelnen Merkmale können je einzeln für sich oder zu mehreren in beliebiger Kombination bei einer Variante der Erfindung verwirklicht sein.Further features and advantages of the invention will become apparent from the following description of embodiments of the invention, with reference to the figures of the drawing, which show details essential to the invention, and from the claims. The individual features can be realized individually for themselves or for several in any combination in a variant of the invention.

Bevorzugte Ausführungsbeispiele der Erfindung sind in der Zeichnung schematisch dargestellt und werden nachfolgend mit Bezug zu den Figuren der Zeichnung näher erläutert. Es zeigt:

Fig. 1
den oberen Eckbereich eines Fensters in einer perspektivischen Darstellung;
Fig. 2
eine perspektivische Ansicht einer erfindungsgemäßen Flügel- befestigungsanordnung;
Fig. 3
einer Draufsicht auf die erfindungsgemäße Flügelbefestigungs- anordnung;
Fig. 4
ein Detail der Flügelbefestigungsanordnung im Bereich einer Sollbruchstelle;
Fig. 5
eine teilweise geschnittene Darstellung eines Abschnitts eines Flügels, in dem die Flügelbefestigungsanordnung montiert ist; und
Fig. 6
eine Schnittdarstellung gemäß der Linie VI - VI der Fig. 5.
Fig. 7
eine perspektivische Darstellung einer weiteren Ausführungs- form eines Stahlteils; und
Fig. 8
eine weitere Ausführungsform eines Stahlteils in perspektivi- scher Darstellung.
Preferred embodiments of the invention are shown schematically in the drawing and are explained below with reference to the figures of the drawing. It shows:
Fig. 1
the upper corner of a window in a perspective view;
Fig. 2
a perspective view of a wing attachment assembly according to the invention;
Fig. 3
a plan view of the invention Flügelbefestigungs- arrangement;
Fig. 4
a detail of the wing attachment assembly in the region of a predetermined breaking point;
Fig. 5
a partially sectioned view of a portion of a wing in which the wing attachment assembly is mounted; and
Fig. 6
a sectional view along the line VI - VI of Fig. 5 ,
Fig. 7
a perspective view of another embodiment of a steel part; and
Fig. 8
a further embodiment of a steel part in a perspective view.

Die Figur 1 zeigt einen oberen Eckbereich eines Fensters 10 mit einem festen Rahmen 11 und einem Flügelrahmen 12 eines Flügels 13. Der Flügel 13 ist mit dem festen Rahmen 11 schwenkbar über eine Scharnieranordnung 14, welche im Ausführungsbeispiel als Drehlager ausgebildet ist, verbunden, wobei die Scharnieranordnung 14 ein flügelseitiges Bandteil 15 und ein einfassungsseitiges Bandteil 16 umfasst. Das flügelseitige Bandteil 15 ist mit einer Flügelbefestigungsanordnung 20, die im Folgenden näher beschrieben wird, verbunden.The FIG. 1 shows an upper corner portion of a window 10 with a fixed frame 11 and a wing frame 12 of a wing 13. The wing 13 is pivotally connected to the fixed frame 11 via a hinge assembly 14, which is formed in the embodiment as a pivot bearing, wherein the hinge assembly 14 a wing-side band member 15 and a welt-side band member 16 includes. The wing-side band part 15 is with a wing attachment assembly 20, which will be described in more detail below, connected.

In der Figur 2 ist die Flügelbefestigungsanordnung 20 in einer perspektivischen Ansicht gezeigt. Die Flügelbefestigungsanordnung 20 umfasst ein Stahlteil 21 und einen Flügelbefestigungsbock 22. Das Stahlteil 21 ist im Ausführungsbeispiel einstückig ausgebildet. Es wurde durch Ausstanzen aus einem Blech und anschließendem Biegen hergestellt. Es umfasst einen Führungsabschnitt 23, der in einem Treibstangenkanal des Flügels 13 geführt ist. Weiterhin umfasst das Stahlteil 21 ein Zugaufnahmeteil 24, von dem ein Befestigungsabschnitt 25 zur Befestigung des flügelseitigen Bandteils 15 abgebogen ist.In the FIG. 2 the wing attachment assembly 20 is shown in a perspective view. The wing attachment assembly 20 includes a steel member 21 and a wing attachment bracket 22. The steel member 21 is integrally formed in the embodiment. It was made by punching out a sheet and then bending it. It comprises a guide section 23, which is guided in a drive rod channel of the wing 13. Furthermore, the steel part 21 comprises a Zugaufnahmeteil 24, from which a fastening portion 25 is bent for fastening the wing-side hinge part 15.

Das freie Ende 26 des Führungsabschnitts 23 ist über einen Niet 27 an dem Zugaufnahmeteil 24 befestigt. Im Übergangsbereich 27 zwischen dem Führungsabschnitt 23 und dem Zugaufnahmeteil 24 ist das Stahlteil 21 umgebogen. An dieser Stelle ist das Stahlteil 21 von einer zylindrisch ausgebildeten Mutter 28 hintergriffen. In die Mutter 28 ist eine Stellschraube 29 eingeschraubt, die auch den Flügelbefestigungsbock 22 durchragt. Der Flügelbefestigungsbock 22 ist mittels Befestigungsmitteln 30,31 mit dem Flügelrahmen 12 verschraubt. Über die Stellschraube 29 kann der Abstand zwischen den Flügelbefestigungsbock 22 und dem Stahlteil 21 verändert werden. In einer Montagestellung schlägt das Stahlteil 21 an einen Anschlag 32 des Flügelbefestigungsbocks 22 an.The free end 26 of the guide portion 23 is attached via a rivet 27 to the Zugaufnahmeteil 24. In the transition region 27 between the guide portion 23 and the Zugaufnahmeteil 24, the steel part 21 is bent. At this point, the steel part 21 is engaged behind by a cylindrical nut 28. In the nut 28 an adjusting screw 29 is screwed, which also extends through the wing mounting bracket 22. The wing mounting bracket 22 is bolted by means of fasteners 30,31 with the casement 12. About the screw 29, the distance between the wing mounting bracket 22 and the steel part 21 can be changed. In an assembly position, the steel part 21 abuts against a stop 32 of the wing mounting bracket 22.

In der Figur 3 ist eine Draufsicht auf die Flügelbefestigungsanordnung 21, insbesondere das Zugaufnahmeteil 24 und den Flügelbefestigungsbock 22, gezeigt. Hier ist der Anschlag 32 zu erkennen, an den das Stahlteil 21 anschlägt. Um eine Verstellung des Stahlteils 21 in Richtung des Flügelbefestigungsbocks 22 zu ermöglichen, indem die Stellschraube 29 weiter in die Mutter 28 eingedreht wird, ist der Anschlag 32 über eine Sollbruchstelle mit dem übrigen Flügelbefestigungsbock 22, insbesondere einem Befestigungsabschnitt 33, verbunden. Dies ist in der vergrößerten Detaildarstellung der Figur 4 zu erkennen. Die Sollbruchstelle ist mit der Bezugsziffer 35 versehen.In the FIG. 3 is a plan view of the wing attachment assembly 21, in particular the Zugaufnahmeteil 24 and the wing mounting bracket 22 shown. Here, the stop 32 can be seen, to which the steel part 21 abuts. To allow an adjustment of the steel part 21 in the direction of the wing mounting bracket 22 by the adjusting screw 29 further into the Nut 28 is screwed, the stop 32 is connected via a predetermined breaking point with the remaining wing mounting bracket 22, in particular a mounting portion 33. This is in the enlarged detail of the FIG. 4 to recognize. The predetermined breaking point is provided with the reference numeral 35.

In der Figur 5 ist der Flügelrahmen 12 teilweise geschnitten dargestellt, um die Anordnung der Flügelbefestigungsanordnung 20 am Flügelrahmen besser erkennen zu können. Der Führungsabschnitt 23 ist in einen Treibstangenkanal 36 eingeschoben. Dadurch ist die Flügelbefestigungsanordnung 20 in einer von zwei Dimensionen bereits festgelegt und lässt sich nur noch in Flügelumfangsrichtung bewegen. Eine Festlegung in Flügelumfangsrichtung erfolgt durch den Flügelbefestigungsbock 22, dessen Befestigungsabschnitt 33 mit dem Flügelrahmen 12 verschraubt ist. Durch Verstellen der Stellschraube 29 kann die Position des flügelseitigen Bandteils 15 bezüglich des Flügels 13 beziehungsweise des Flügelrahmens 12 verändert werden. Dadurch wird auch der Abstand des Flügels 13 zur festen Einfassung 11 verändert.In the FIG. 5 the sash frame 12 is shown partially cut in order to better recognize the arrangement of the sash mounting arrangement 20 on the sash. The guide portion 23 is inserted into a drive rod channel 36. As a result, the wing attachment assembly 20 is already fixed in one of two dimensions and can only be moved in the wing circumferential direction. A determination in the wing circumferential direction is made by the wing mounting bracket 22, the mounting portion 33 is screwed to the sash 12. By adjusting the adjusting screw 29, the position of the wing-side hinge part 15 with respect to the wing 13 and the wing frame 12 can be changed. As a result, the distance of the wing 13 is changed to the fixed enclosure 11.

Die Figur 6 zeigt eine Schnittdarstellung gemäß der Linie VI - VI der Figur 5. Hier ist zu erkennen, dass der Führungsabschnitt 23 in dem Treibstangenkanal 36 geführt ist und von Schenkeln 37,38 des im Querschnitt c-förmigen Treibstangenkanals 36 übergriffen ist. Das Zugaufnahmeteil 24 ist über dem Treibstangenkanal 26 angeordnet.The FIG. 6 shows a sectional view along the line VI - VI of FIG. 5 , Here it can be seen that the guide section 23 is guided in the drive rod channel 36 and is overlapped by legs 37, 38 of the cross-sectionally C-shaped drive rod channel 36. The Zugaufnahmeteil 24 is disposed above the drive rod channel 26.

In der Figur 7 ist eine Ausgestaltung eines Stahlteils 50 gezeigt, bei dem sich ein Befestigungsabschnitt 51 zur Befestigung des flügelseitigen Bandteils 15 an den Führungsabschnitt 52 materialschlüssig anschließt. Zwischen dem eigentlichen Führungsabschnitt 52 und dem Befestigungsabschnitt 51 ist eine stufenartige Erhöhung 53 vorgesehen. An seinem flügelbefestigungsbockseitigen Ende 54 ist das Stahlteil 50 umgebogen und mit seinem freien Ende 55 an dem Führungsabschnitt 52 befestigt, insbesondere mit diesem vernietet.In the FIG. 7 an embodiment of a steel part 50 is shown, in which a fastening portion 51 for attaching the wing-side hinge part 15 connects to the guide portion 52 materially. Between the actual guide portion 52 and the mounting portion 51, a step-like increase 53 is provided. At its wing mounting bracket side End 54, the steel part 50 is bent and fixed with its free end 55 to the guide portion 52, in particular riveted to this.

Die Ausführungsform gemäß der Figur 8 entspricht im Wesentlichen der Figur 7 mit dem Unterschied, dass der Führungsabschnitt 52 vollständig gerade ist und sich keine Stufe 53 wie in der Figur 7 anschließt. Auch bei dieser Ausführungsform ist der Befestigungsabschnitt 51 materialschlüssig mit dem Führungsabschnitt 52 verbunden. In der Figur 8 ist das Stahlteil mit der Bezugsziffer 60 versehen.The embodiment according to the FIG. 8 essentially corresponds to the FIG. 7 with the difference that the guide section 52 is completely straight and no step 53 as in FIG. 7 followed. Also in this embodiment, the attachment portion 51 is materially connected to the guide portion 52. In the FIG. 8 the steel part is provided with the reference numeral 60.

Claims (12)

Flügelbefestigungsanordnung (20) eines Dreh- oder Dreh-Kipp-Lagers für ein Fenster (10), eine Tür oder dgl. mit einem Stahlteil (21,50,60), welches einen Führungsabschnitt (23,52) zur Führung des Stahlteils (21,50,60) in einem Treibstangenkanal (36) eines Flügels (13) aufweist, und einem Flügelbefestigungsbock (22), der mit dem Stahlteil (21,50,60) verbunden ist.A sash mounting arrangement (20) of a turn or tilt and turn bearing for a window (10), a door or the like with a steel part (21, 50, 60) which has a guide section (23, 52) for guiding the steel part (21 , 50, 60) in a drive rod channel (36) of a wing (13), and a wing attachment bracket (22) connected to the steel part (21, 50, 60). Flügelbefestigungsanordnung nach Anspruch 1, dadurch gekennzeichnet, dass das Stahlteil (21,50,60) als Stanz-Biegeteil oder lasergeschnittenes Biegeteil ausgebildet ist.Wing attachment arrangement according to claim 1, characterized in that the steel part (21,50,60) is formed as a punched-bent part or laser-cut bent part. Flügelbefestigungsanordnung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das Stahlteil (21) einen abschnittsweise parallel zum Führungsabschnitt (23) verlaufenden Zugaufnahmeteil (24) aufweist.Wing mounting arrangement according to one of the preceding claims, characterized in that the steel part (21) has a section receiving parallel to the guide portion (23) extending tension receiving part (24). Flügelbefestigungsanordnung nach Anspruch 3, dadurch gekennzeichnet, dass das freie Ende (26) des Führungsabschnitts (23) mit dem Zugaufnahmeteil (24) verbunden ist.Wing mounting arrangement according to claim 3, characterized in that the free end (26) of the guide portion (23) with the Zugaufnahmeteil (24) is connected. Flügelbefestigungsanordnung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Flügelbefestigungsbock (22) mit dem Stahlteil (21,50,60) über eine Stellschraube (29) verbunden ist.Wing attachment arrangement according to one of the preceding claims, characterized in that the wing attachment bracket (22) with the steel part (21,50,60) via an adjusting screw (29) is connected. Flügelbefestigungsanordnung nach Anspruch 5, dadurch gekennzeichnet, dass eine das Stahlteil (21,50,60) abschnittsweise hintergreifende Mutter (28) vorgesehen ist, in die die Stellschraube (29) eingeschraubt ist.Wing fastening arrangement according to claim 5, characterized in that a part of the steel (21,50,60) engaging behind in sections Nut (28) is provided, in which the adjusting screw (29) is screwed. Flügelbefestigungsanordnung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Flügelbefestigungsbock (22) einen Anschlag (32) für das Stahlteil (21,50,60) aufweist.Wing attachment arrangement according to one of the preceding claims, characterized in that the wing attachment bracket (22) has a stop (32) for the steel part (21,50,60). Flügelbefestigungsanordnung nach Anspruch 7, dadurch gekennzeichnet, dass der Anschlag (32) über eine Sollbruchstelle (35) mit dem Befestigungsabschnitt (33) des Flügelbefestigungsbocks (22) verbunden ist.Wing mounting arrangement according to claim 7, characterized in that the stop (32) via a predetermined breaking point (35) with the mounting portion (33) of the wing mounting bracket (22) is connected. Flügelbefestigungsanordnung nach einem der vorgehenden Ansprüche, dadurch gekennzeichnet, dass der Führungsabschnitt (52) materialschlüssig mit einem Befestigungsabschnitt (51) zur Befestigung des flügelseitigen Bandteils (15) verbunden ist.Wing fastening arrangement according to one of the preceding claims, characterized in that the guide section (52) is materially connected to a fastening section (51) for fastening the wing-side hinge part (15). Flügelbefestigungsanordnung nach einem der vorgehenden Ansprüche, dadurch gekennzeichnet, dass das Stahlteil flügelbefestigungsbockseitig umgebogen ist und das freie Ende (55) mit dem Führungsabschnitt (52) verbunden ist.Wing attachment arrangement according to one of the preceding claims, characterized in that the steel part is bent wing mounting bracket side and the free end (55) is connected to the guide portion (52). Drehlager oder Dreh-Kipp-Lager mit einer Flügelbefestigungsanordnung (20) nach einem der vorhergehenden Ansprüche.A pivot bearing or turn-tilt bearing having a wing attachment assembly (20) according to any one of the preceding claims. Fenster (10), Tür oder dgl. mit einer Flügelbefestigungsanordnung (20) nach einem der vorhergehenden Ansprüche 1 - 10.Window (10), door or the like with a wing attachment arrangement (20) according to one of the preceding claims 1-10.
EP07019588.8A 2007-10-06 2007-10-06 Mounting device of a pivot bearing of a window Active EP2045426B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP07019588.8A EP2045426B1 (en) 2007-10-06 2007-10-06 Mounting device of a pivot bearing of a window
PL07019588T PL2045426T3 (en) 2007-10-06 2007-10-06 Mounting device of a pivot bearing of a window
ES07019588.8T ES2464594T3 (en) 2007-10-06 2007-10-06 Fixing device for an oscillating bearing for a window leaf
CN2008101689548A CN101403267B (en) 2007-10-06 2008-10-06 Mounting device of a pivot bearing of a window

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP07019588.8A EP2045426B1 (en) 2007-10-06 2007-10-06 Mounting device of a pivot bearing of a window

Publications (2)

Publication Number Publication Date
EP2045426A1 true EP2045426A1 (en) 2009-04-08
EP2045426B1 EP2045426B1 (en) 2014-02-26

Family

ID=39092340

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07019588.8A Active EP2045426B1 (en) 2007-10-06 2007-10-06 Mounting device of a pivot bearing of a window

Country Status (4)

Country Link
EP (1) EP2045426B1 (en)
CN (1) CN101403267B (en)
ES (1) ES2464594T3 (en)
PL (1) PL2045426T3 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3279418A1 (en) * 2016-08-01 2018-02-07 Wilh. Schlechtendahl & Söhne GmbH & Co. KG Fitting part of a fitting and method for assembling such a fitting part

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2064047A1 (en) 1970-12-28 1972-07-13 Keller, Eberhard, 7121 Freudental Device for fine adjustment of tilt and turn windows
DE2746190A1 (en) 1977-10-14 1979-04-19 Ver Baubeschlag Gretsch Co Stay for combined revolving and tilting windows - has connecting piece with slot for stay arm hook and guide
DE3702957C1 (en) 1987-01-31 1988-05-11 Siegenia Frank Kg Hinge fitting for windows, doors or the like.
DE29717177U1 (en) 1997-09-25 1999-02-04 Ferco Int Usine Ferrures Fitting for pivoting a window or door leaf

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2064047A1 (en) 1970-12-28 1972-07-13 Keller, Eberhard, 7121 Freudental Device for fine adjustment of tilt and turn windows
DE2746190A1 (en) 1977-10-14 1979-04-19 Ver Baubeschlag Gretsch Co Stay for combined revolving and tilting windows - has connecting piece with slot for stay arm hook and guide
DE3702957C1 (en) 1987-01-31 1988-05-11 Siegenia Frank Kg Hinge fitting for windows, doors or the like.
DE29717177U1 (en) 1997-09-25 1999-02-04 Ferco Int Usine Ferrures Fitting for pivoting a window or door leaf

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3279418A1 (en) * 2016-08-01 2018-02-07 Wilh. Schlechtendahl & Söhne GmbH & Co. KG Fitting part of a fitting and method for assembling such a fitting part

Also Published As

Publication number Publication date
CN101403267B (en) 2013-03-06
EP2045426B1 (en) 2014-02-26
CN101403267A (en) 2009-04-08
PL2045426T3 (en) 2014-08-29
ES2464594T3 (en) 2014-06-03

Similar Documents

Publication Publication Date Title
EP2246509B1 (en) Moving device for pivotable partition elements and furniture
EP1788178B1 (en) Bearing for windows, doors or the like
EP1936086B1 (en) Corner fitting for windows, doors or similar
EP3175068B1 (en) Fitting arrangement
EP0294630A2 (en) Fastener for windows, doors, etc.
DE3822050A1 (en) DOOR HANDLE ARRANGEMENT ON A VEHICLE DOOR
EP1915498B1 (en) Profile hinge system
DE4313610A1 (en) Display device for a turn-tilt sash
EP2013045B1 (en) Lifting window
EP3060736B1 (en) Fitting for windows, doors or the like
EP1746235B1 (en) Fitting assembly
EP1788175A1 (en) Flat links assembly for windows, doors or the like
EP2045426B1 (en) Mounting device of a pivot bearing of a window
DE202008016071U1 (en) Band for hingedly connecting a wing to a frame
DE2805465C2 (en) Espagnolette
EP3279418B1 (en) Fitting part of a fitting and method for assembling such a fitting part
EP2304145B1 (en) Motor vehicle having a rear hatch
DE10114384B4 (en) Motor vehicle door
DE202007017519U1 (en) fitting assembly
DE2064047A1 (en) Device for fine adjustment of tilt and turn windows
EP0620344A1 (en) Coupling device of a sliding bar or a driver fitting for a locking bar of a window or a door, the locking bar being guided in grooves
EP3543444B1 (en) Bearing for a fitting device of a window
EP1936085B1 (en) Fitting for windows, doors or similar
DE102007051658B3 (en) Pivot bracket
EP3146134B1 (en) Adjustable vertical reinforcement element for a door or window sash that is movable from one plane to a parallel plane

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

17P Request for examination filed

Effective date: 20090924

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

17Q First examination report despatched

Effective date: 20100728

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20131002

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 653727

Country of ref document: AT

Kind code of ref document: T

Effective date: 20140315

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502007012780

Country of ref document: DE

Effective date: 20140410

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2464594

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20140603

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20140226

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140626

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140626

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

REG Reference to a national code

Ref country code: PL

Ref legal event code: T3

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502007012780

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20141127

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502007012780

Country of ref document: DE

Effective date: 20141127

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

Ref country code: LU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141006

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20141006

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141006

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141031

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141031

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 9

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141006

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140527

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20071006

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140226

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 12

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FI

Payment date: 20181121

Year of fee payment: 15

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20191022

Year of fee payment: 13

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 653727

Country of ref document: AT

Kind code of ref document: T

Effective date: 20191006

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191006

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201031

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 20221020

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20230928

Year of fee payment: 17

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: PL

Payment date: 20230926

Year of fee payment: 17

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20231117

Year of fee payment: 17

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20231031

Year of fee payment: 17

Ref country code: DE

Payment date: 20231018

Year of fee payment: 17

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 20231023

Year of fee payment: 17