EP1757767B1 - Corner support - Google Patents

Corner support Download PDF

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Publication number
EP1757767B1
EP1757767B1 EP05018146A EP05018146A EP1757767B1 EP 1757767 B1 EP1757767 B1 EP 1757767B1 EP 05018146 A EP05018146 A EP 05018146A EP 05018146 A EP05018146 A EP 05018146A EP 1757767 B1 EP1757767 B1 EP 1757767B1
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EP
European Patent Office
Prior art keywords
receiving member
window
door
leaf
carrier arm
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.)
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EP05018146A
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German (de)
French (fr)
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EP1757767A1 (en
Inventor
Martin Siegler
Dirk Hanel
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Roto Frank AG
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Roto Frank AG
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First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=35695049&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP1757767(B1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority to ES05018146T priority Critical patent/ES2297576T3/en
Priority to AT05018146T priority patent/ATE382116T1/en
Priority to EP05018146A priority patent/EP1757767B1/en
Priority to PL05018146T priority patent/PL1757767T3/en
Priority to DE502005002354T priority patent/DE502005002354D1/en
Application filed by Roto Frank AG filed Critical Roto Frank AG
Priority to SI200530198T priority patent/SI1757767T1/en
Publication of EP1757767A1 publication Critical patent/EP1757767A1/en
Publication of EP1757767B1 publication Critical patent/EP1757767B1/en
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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/48Suspension arrangements for wings allowing alternative movements
    • E05D15/52Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
    • E05D15/5211Concealed suspension fittings
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00Hinges or pivots of special construction
    • E05D7/04Hinges adjustable relative to the wing or the frame
    • E05D7/0415Hinges adjustable relative to the wing or the frame with adjusting drive means
    • E05D7/0423Screw-and-nut mechanisms
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING 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
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
    • E05Y2900/132Doors
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING 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
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
    • E05Y2900/148Windows

Definitions

  • the invention relates to a corner hinge of a corner bearing assembly for the Ecklagerung a sash of a window, a door or the like.
  • On a fixed frame comprising a fastened to the casement wing receptacle and a bolt receptacle having a support arm, wherein the support arm of the pin receptacle telescopically in a Tragarmam the wing receptacle is guided.
  • the corner bearing assembly which act between the fixed frame and the wing, must be arranged in the rebate air area.
  • the corner bearing assemblies must be of compact design, since only a limited installation space is available.
  • the Ecklagerbau phenomenon must be designed so that they can carry heavy wings.
  • the object of the present invention is to provide a corner band of a corner bearing assembly, which is compact and suitable for heavy wings.
  • a Eckband of the type mentioned in which the support arm is arranged at least substantially on the side facing away from the fixed frame a doublegelfalzroissthesis and Ecklager assembly is designed as concealed fitting.
  • the support arm is advantageously arranged within a wing frame part of the casement.
  • the support arm can be made stronger than the bands that are used for example in the prior art.
  • the corner band can therefore be designed for larger loads.
  • the corner band according to the invention can also be regarded as a corner angle
  • the horizontal leg is formed telescopically
  • a telescopic tube is formed in the wing receptacle and the Tragarmaid represents
  • the pin receptacle is formed as part of the horizontal leg
  • said the support arm is the telescopic part cooperating with the telescopic tube.
  • a particularly secure holder and good guidance of the support arm results when the support arm surrounds the support arm at least partially circumferentially.
  • the support arm surrounds the support arm completely or at least to a large extent.
  • the Tragarmability is formed as a sleeve or blind hole.
  • a good anti-rotation of the support arm in the Tragarmam arises when the support arm is rectangular or square in cross-section and the Tragarmability is adapted to the cross section of the support arm.
  • a particularly compact design and a simple manufacture and assembly of the corner band results when the wing holder is integrally formed.
  • a preferred embodiment of the invention can be provided for adjusting the distance between the bolt receptacle and the wing receptacle accessible in the vertical Falz Kunststoff Kunststoff adjustable adjustment.
  • the folded air can be adjusted very easily.
  • a preferred development is characterized in that the distance via an adjusting screw is adjustable, wherein the adjusting screw axially is arranged immovably in the bolt receptacle or the wing receptacle and cooperates with a thread cutout of the other part.
  • the adjusting screw can be designed as a threaded pin or grub screw. It is particularly advantageous if the threaded cutout is already introduced during the manufacture of the wing receptacle or the bolt receptacle. This is particularly easy if the bolt receptacle or the wing receptacle are produced in a casting process.
  • the horizontal leg of the wing receptacle comprises a cross-sectionally U-shaped tab.
  • the U-shaped tab may overlap the Tragarmability having part of the wing receptacle and attached to the sash. As a result, the wing receiver can be held particularly securely on the wing.
  • a Ausfêt to prevent the complete separation of bolt holder and wing receiving.
  • the Ausfêt may for example comprise a recess in the bolt receptacle, in which engages a projection or a manifestation of the U-shaped tab. The bolt receptacle can then only be moved within the recess. This ensures that accidental unscrewing of the bolt holder is excluded.
  • an articulation device for a scissors geometry is provided on the bolt receptacle, in particular the free end of the support arm.
  • the bolt receptacle has a vertical adjustment.
  • the vertical adjustment for example, a threaded pin, which is supported directly or indirectly on a pivot pin, have. Turning the threaded pin in or out raises or lowers the corner band.
  • a non-rotating corner bearing insert can be arranged in the bolt receptacle. Thus, the rotational movement is interrupted by the axle bolt to the set screw. An accidental adjustment is thus excluded.
  • a window, a door or the like with a fixed frame and / or at least one wing frame, wherein in Falz Kunststoff Scheme between the fixed frame and sash at least one corner bearing assembly is provided which has a previously described Eckband.
  • a window or such a door can be formed with very low Falz Kunststoff Kunststoff Kunststoffen.
  • the corner bearing assembly is designed as concealed fitting. So it is not visible with the wing closed.
  • Fig. 1 the corner region of a wing 1 is shown.
  • a corner band 10 is arranged.
  • the corner band 10 has a wing receptacle 11 and a bolt receptacle 12. From Fig. 1 it can be seen that the corner band 10 does not protrude over a wellgelfalzroiss formulation 2 down.
  • the corner band 10 is arranged essentially in a wing frame part 3.
  • the wing receptacle 11 can be secured by fastening means, not shown, via mounting holes 4 on the wing 1.
  • the corner band 10 is designed as a corner angle.
  • a vertical leg 13 and a horizontal leg 14 can be fastened to the wing 1.
  • the horizontal leg 14 comprises a cross-sectionally U-shaped tab 15 which engages around a not visible in FIG. 2a support arm, which is arranged in a part of the wing holder 11.
  • a support arm receptacle 16 for a support arm 17 of the bolt receptacle 12 is formed in the wing receptacle 11.
  • the arrangement of the support arm 17 and the Tragarmability 16 of the wing receptacle 11 results in a telescoping horizontal leg 14 of the corner band 10.
  • the adjustment of the bolt receptacle 12 relative to the wing receptacle 11 via an adjusting device 18 which includes a trained as a set screw adjusting screw 19, which axially is arranged immovably in a recess 20 of the bolt receptacle 12.
  • the screw 19 cooperates with a thread cutout 21 of the wing receptacle 11.
  • the bolt receptacle 12 By turning the screw 19, the bolt receptacle 12 can be introduced into the wing receptacle 11. Since the screw 19 in the bolt receptacle 12 can not be moved, the bolt receptacle 12 follows the thread pitch when turning the screw 19, which applies to the thread cutout 21 of the wing receptacle 11. In this way, the lateral folding air can be adjusted.
  • a vertical adjustment device 22 which comprises a threaded pin, not shown, which acts on a non-rotatably mounted Ecklagergan 23 at which an unillustrated pivot pin is supported.
  • the bolt receptacle 12 has been adjusted by means of the screw 19 with respect to the wing receptacle 11, so that a gap results between the support arm 17 and the wing receptacle 11 in the support arm receptacle 16.
  • the illustration shown corresponds to the largest adjustable lateral folding air.
  • the Ausfêt 25 includes a recess 26 in the bolt receptacle 12th or in the support arm 17; in the one expression 27 of cross-sectionally U-shaped tab 15 engages.
  • the extent of the recess 26 in the fold circumferential direction is greater than the extent of the expression 27.
  • the interaction of the recess 26 and the expression 27, the movement of the pin holder 12 is limited.
  • the bolt receptacle 12 can not be dismantled in the assembled state of the corner band 10.
  • the wing receptacle 31 is made in one piece.
  • the U-shaped tab is missing.
  • mounting holes 4 are provided at the wing receptacle 31 itself.
  • the part of the wing receptacle 31, in which the Tragarmage 36 is formed designed to be longer than in the embodiment of Figures 1 - 3b.
  • the wing receptacle 31 is constructed in steps.
  • the wing receptacle 31 is adapted to a stepped fitting part of the wing 1.
  • the screw 19 is arranged axially immovably in a recess 20 'of the wing receptacle 31. In contrast, it engages in a threaded cutout 21 'of the bolt receptacle 32.
  • the corner band 40 of FIG. 6a has a slot 43 in the wing receptacle 41, through which an articulation device 45 designed as a bolt protrudes.
  • the sectional view of Fig. 6b can be seen that the hinge device 45 is arranged at the free end of the support arm 47 of the bolt receptacle 42. This means that regardless of the lateral Falzlufsein sued the distance between the hinge 45 and the sleeve-like receptacle 48 for a pivot pin of the bolt holder 42 remains constant.
  • the support arm 47 is extended compared to the previous embodiments, since the scissor geometry in this case, unlike before, where the wing receptacle is intended for articulation of the scissors geometry, to be articulated on the support arm of the bolt receptacle.
  • FIG. 7 shows a corner bearing assembly 49 with the corner band 10, which is attached to a scissors geometry 50.
  • An invisible axle pin protruding from the handlebar 51 protrudes into the bolt receptacle 12.
  • the scissors geometry 50 is fixed to a corner bracket 52 which is intended to be fixed to the fixed frame. Shown is an open position. When the sash is closed, the links 51, 53 overlap in sections in the rebate air area.
  • the scissors geometry 50 is designed such that the wing is lifted off the fixed frame at the beginning of the opening movement, before the pivoting movement begins.
  • the link 53 is articulated on the U-shaped tab 15, wherein the articulation device 15 is slidably disposed in a slot of the U-shaped tab. An adjustment of the lateral folding air does not affect the function of the scissor geometry therefore.
  • the scissor geometry 60 of the corner bearing assembly 59 shown in FIG. 8 has an additional link 61, which is articulated on the support arm of the bolt receptacle 42 of the corner band 40.
  • the scissors geometry 60 requires a constant distance between the articulation point on the support arm and the axle bolt in order to obtain the same opening kinematics at different folding air settings.

Abstract

Angle iron comprises a seat (11) in which to rest a door panel or window pane and a pin seat (12) with bearing arm (17). Said bearing arm is guided telescopically on the pin seat into a bearing seat (16) on the leaf seat, leaving the bearing arm arranged on the outer surface of the leaf rabbet facing away from the fixed frame. The corner postioning parts are embodied as a hidden stop.

Description

Die Erfindung betrifft ein Eckband einer Ecklager-Baugruppe für die Ecklagerung eines Flügelrahmens eines Fensters, einer Tür oder dgl. an einem festen Rahmen, umfassend eine an dem Flügelrahmen befestigbare Flügelaufnahme und eine Bolzenaufnahme, die einen Tragarm aufweist, wobei der Tragarm der Bolzenaufnahme teleskopartig in einer Tragarmaufnahme der Flügelaufnahme geführt ist.The invention relates to a corner hinge of a corner bearing assembly for the Ecklagerung a sash of a window, a door or the like. On a fixed frame, comprising a fastened to the casement wing receptacle and a bolt receptacle having a support arm, wherein the support arm of the pin receptacle telescopically in a Tragarmaufnahme the wing receptacle is guided.

Insbesondere bei Türen oder Fenstern mit verdeckt liegenden Beschlägen müssen die Ecklagerbaugruppe, die zwischen festem Rahmen und Flügel wirken, im Falzluftbereich angeordnet sein. Dies bedeutet zum einen, dass die Ecklagerbaugruppen kompakt aufgebaut sein müssen, da nur ein begrenzter Einbauraum zur Verfügung steht. Zum anderen bedeutet dies, dass trotz geringem Einbauraum und kompakter Bauweise die Ecklagerbaugruppen so ausgeführt sein müssen, dass sie auch schwere Flügel tragen können.Particularly in the case of doors or windows with concealed fittings, the corner bearing assembly, which act between the fixed frame and the wing, must be arranged in the rebate air area. This means, on the one hand, that the corner bearing assemblies must be of compact design, since only a limited installation space is available. On the other hand, this means that despite low installation space and compact design, the Ecklagerbaugruppen must be designed so that they can carry heavy wings.

Aus der DE 196 50 085 C2 ist eine Ecklager-Baugruppe bekannt geworden, die einen Eckwinkel aufweist, an dessen horizontalem Schenkel ein Lager mit einer Stellschrauben vorgesehen ist, in das ein Schwenkbolzen ragt, der mit einer Bolzenaufnahme für einen Achsbolzen verbunden ist. Über die Stellschraube lässt sich die Falzluft einstellen. Der Schwenkbolzen ist im horizontal verlaufenden Falzluftbereich angeordnet, so dass diese Ecklagerbaugruppe nur bedingt für eine Tür oder ein Fenster mit einer Dreh-/Kippfunktion geeignet ist, bei der oder dem auch noch eine Scherengeometrie im Falzluftbereich angeordnet werden muss.From the DE 196 50 085 C2 a Ecklager assembly has become known, which has a corner angle, on the horizontal leg of a bearing is provided with a set screws into which a pivot pin protrudes, which is connected to a bolt receptacle for a pivot pin. The adjusting air can be adjusted with the adjusting screw. The pivot pin is arranged in the horizontally extending Falzluftbereich, so that this Ecklagerbaugruppe is only partially suitable for a door or a window with a turn / tilt function, in which or even a scissors geometry must be arranged in the Falzluftbereich.

Aus der DE 93 01 655 U1 ist eine Ecklager-Baugruppe bekannt geworden, bei der eine Halteschiene am Flügelrahmen befestigt ist und eine Trägerschiene an der Halteschiene verschieblich gelagert ist. An der Halteschiene ist eine Bolzenaufnahme für einen Achsbolzen vorgesehen. Über eine Verstelleinrichtung lässt sich der Abstand zwischen Flügelrahmen und festem Rahmen einstellen. Sowohl die Trägerschiene als auch die Halteschiene sind ebenfalls im Falzluftbereich angeordnet, was gegen eine kompakte Bauweise spricht.From the DE 93 01 655 U1 is a corner bearing assembly has become known in which a retaining rail is attached to the sash and a support rail is slidably mounted on the support rail. On the retaining rail a bolt receptacle for a pivot pin is provided. About an adjustment, the distance between sash and fixed frame can be adjusted. Both the support rail and the support rail are also arranged in the Falzluftbereich, which speaks against a compact design.

Aufgabe der vorliegenden Erfindung ist es, ein Eckband einer Ecklager-Baugruppe bereitzustellen, welches kompakt aufgebaut ist und für schwere Flügel geeignet ist.The object of the present invention is to provide a corner band of a corner bearing assembly, which is compact and suitable for heavy wings.

Diese Aufgabe wird erfindungsgemäß durch ein Eckband der eingangs genannten Art gelöst, bei dem der Tragarm zumindest im Wesentlichen auf der dem festen Rahmen abgewandten Seite einer Flügelfalzumfangsfläche angeordnet ist und die Ecklager-Baugruppe als verdeckt liegender Beschlag ausgebildet ist. Dies bedeutet, dass der Tragarm vorteilhafterweise innerhalb eines Flügelrahmenteils des Flügelrahmens angeordnet ist. Insbesondere bedeutet dies, dass weder der Tragarm noch die Tragarmaufnahme der Flügelaufnahme wesentlich, vorzugsweise überhaupt nicht, in den Falzluftbereich ragen. Dadurch verbleibt im Falzluftbereich genügend Raum für eine Scherengeometrie. Außerdem kann der Tragarm stärker ausgebildet sein als die Bänder, die beispielsweise im Stand der Technik verwendet werden. Das Eckband kann daher für größere Lasten ausgelegt werden. Das erfindungsgemäße Eckband kann auch als Eckwinkel betrachtet werden, dessen horizontaler Schenkel teleskopierbar ausgebildet ist, wobei ein Teleskoprohr in der Flügelaufnahme ausgebildet ist und die Tragarmaufnahme darstellt, und die Bolzenaufnahme als Teil des horizontalen Schenkels ausgebildet ist, wobei der Tragarm das mit dem Teleskoprohr zusammenwirkende Teleskopteil ist.This object is achieved by a Eckband of the type mentioned, in which the support arm is arranged at least substantially on the side facing away from the fixed frame a Flügelfalzumfangsfläche and Ecklager assembly is designed as concealed fitting. This means that the support arm is advantageously arranged within a wing frame part of the casement. In particular, this means that neither the support arm nor the support arm receptacle of the wing receptacle protrude substantially, preferably not at all, into the rebate air area. This leaves enough room for a scissor geometry in the seaming air area. In addition, the support arm can be made stronger than the bands that are used for example in the prior art. The corner band can therefore be designed for larger loads. The corner band according to the invention can also be regarded as a corner angle, the horizontal leg is formed telescopically, wherein a telescopic tube is formed in the wing receptacle and the Tragarmaufnahme represents, and the pin receptacle is formed as part of the horizontal leg, said the support arm is the telescopic part cooperating with the telescopic tube.

Eine besonders sichere Halterung und gute Führung des Tragarms ergibt sich, wenn die Tragarmaufnahme den Tragarm zumindest abschnittsweise umfangsmäßig umgibt. Besonders bevorzugt umgibt die Tragarmaufnahme den Tragarm vollständig oder zumindest zu einem Großteil. Dies kann insbesondere dadurch realisiert werden, dass die Tragarmaufnahme als Hülse oder als Sackloch ausgebildet ist.A particularly secure holder and good guidance of the support arm results when the support arm surrounds the support arm at least partially circumferentially. Particularly preferably, the support arm surrounds the support arm completely or at least to a large extent. This can be realized in particular in that the Tragarmaufnahme is formed as a sleeve or blind hole.

Eine gute Verdrehsicherung des Tragarms in der Tragarmaufnahme ergibt sich, wenn der Tragarm im Querschnitt rechteckig oder quadratisch ausgebildet ist und die Tragarmaufnahme auf den Querschnitt des Tragarms angepasst ist.A good anti-rotation of the support arm in the Tragarmaufnahme arises when the support arm is rectangular or square in cross-section and the Tragarmaufnahme is adapted to the cross section of the support arm.

Eine besonders kompakte Bauweise und eine einfache Fertigung und Montage des Eckbands ergibt sich, wenn die Flügelaufnahme einstückig ausgebildet ist. Um in diesem Falle eine gute Halterung der Flügelaufnahme an dem Flügelrahmen sicherzustellen, ist es sinnvoll, den die Tragarmaufnahme aufweisenden Teil der Flügelaufnahme gegenüber einer mehrteiligen Ausführung zu verlängern, insbesondere den horizontalen Schenkel der Flügelaufnahme zu verlängern.A particularly compact design and a simple manufacture and assembly of the corner band results when the wing holder is integrally formed. In order to ensure a good support of the wing receptacle on the sash in this case, it makes sense to extend the Tragarmaufnahme having part of the wing receptacle over a multi-part design, in particular to extend the horizontal leg of the wing receptacle.

Bei einer bevorzugten Ausgestaltung der Erfindung kann eine im vertikal verlaufenden Falzluftbereich zugängliche Verstelleinrichtung zur Einstellung des Abstands zwischen der Bolzenaufnahme und der Flügelaufnahme vorgesehen sein. Die Falzluft lässt sich dadurch besonders einfach einstellen.In a preferred embodiment of the invention can be provided for adjusting the distance between the bolt receptacle and the wing receptacle accessible in the vertical Falzluftbereich adjustable adjustment. The folded air can be adjusted very easily.

Eine bevorzugte Weiterbildung zeichnet sich dadurch aus, dass der Abstand über eine Einstellschraube einstellbar ist, wobei die Einstellschraube axial unverschieblich in der Bolzenaufnahme oder der Flügelaufnahme angeordnet ist und mit einem Gewindeausschnitt des jeweils anderen Teils zusammenwirkt. Die Einstellschraube kann als Gewindestift oder Madenschraube ausgeführt sein. Besonders vorteilhaft ist es, wenn der Gewindeausschnitt bereits bei der Fertigung der Flügelaufnahme beziehungsweise der Bolzenaufnahme eingebracht wird. Dies ist besonders einfach möglich, wenn die Bolzenaufnahme oder die Flügelaufnahme in einem Gießverfahren hergestellt werden.A preferred development is characterized in that the distance via an adjusting screw is adjustable, wherein the adjusting screw axially is arranged immovably in the bolt receptacle or the wing receptacle and cooperates with a thread cutout of the other part. The adjusting screw can be designed as a threaded pin or grub screw. It is particularly advantageous if the threaded cutout is already introduced during the manufacture of the wing receptacle or the bolt receptacle. This is particularly easy if the bolt receptacle or the wing receptacle are produced in a casting process.

Bei einer Ausführungsform kann vorgesehen sein, dass der horizontale Schenkel der Flügelaufnahme eine im Querschnitt U-förmige Lasche umfasst. Die U-förmige Lasche kann den die Tragarmaufnahme aufweisenden Teil der Flügelaufnahme übergreifen und an dem Flügelrahmen befestigt werden. Dadurch kann die Flügelaufnahme besonders sicher am Flügel gehalten werden.In one embodiment, it can be provided that the horizontal leg of the wing receptacle comprises a cross-sectionally U-shaped tab. The U-shaped tab may overlap the Tragarmaufnahme having part of the wing receptacle and attached to the sash. As a result, the wing receiver can be held particularly securely on the wing.

Vorteilhafterweise ist eine Ausdrehsicherung zur Verhinderung der vollständigen Trennung von Bolzenaufnahme und Flügelaufnahme vorgesehen. Die Ausdrehsicherung kann beispielsweise eine Aussparung in der Bolzenaufnahme umfassen, in die ein Vorsprung oder eine Ausprägung der U-förmigen Lasche eingreift. Die Bolzenaufnahme kann dann nur noch innerhalb der Aussparung bewegt werden. Somit ist sichergestellt, dass ein versehentliches Herausdrehen der Bolzenaufnahme ausgeschlossen ist.Advantageously, a Ausdrehsicherung to prevent the complete separation of bolt holder and wing receiving is provided. The Ausdrehsicherung may for example comprise a recess in the bolt receptacle, in which engages a projection or a manifestation of the U-shaped tab. The bolt receptacle can then only be moved within the recess. This ensures that accidental unscrewing of the bolt holder is excluded.

Bei einer besonders bevorzugten Ausführungsform ist an der Bolzenaufnahme, insbesondere dem freien Ende des Tragarms, eine Anlenkeinrichtung für eine Scherengeometrie vorgesehen. Durch diese Maßnahme kann der Abstand zwischen der Anlenkeinrichtung und dem Aufnahmeteil der Bolzenaufnahme auch bei unterschiedlichen Falzlufteinstellungen konstant gehalten werden. Dies ist für bestimmte Scherengeometrien notwendig. Die Anlenkeinrichtung kann beispielsweise als Bolzen, Bohrung oder Langloch ausgebildet sein.In a particularly preferred embodiment, an articulation device for a scissors geometry is provided on the bolt receptacle, in particular the free end of the support arm. By this measure, the distance between the hinge device and the receiving part of the bolt receptacle can be kept constant even with different Falzlufteinstellungen. This is necessary for certain scissor geometries. The Anlenkeinrichtung can be formed for example as a bolt, hole or slot.

Um auch eine Verstellung des horizontal verlaufenden Falzluftbereichs zu ermöglichen, ist es vorteilhaft, wenn die Bolzenaufnahme eine Vertikalverstelleinrichtung aufweist. Dazu kann die Vertikalverstelleinrichtung beispielsweise einen Gewindestift, der sich mittelbar oder unmittelbar auf einem Achsbolzen abstützt, aufweisen. Durch Ein- oder Ausdrehen des Gewindestifts hebt oder senkt sich das Eckband. Um ein versehentliches Verstellen der Höheneinstellung beim Öffnen und Schließen des Flügels zu vermeiden, ist darauf zu achten, dass die Reibkräfte zwischen Bolzenaufnahme und Gewindestift größer sind als die zwischen Gewindestift und Achsbolzen. Um dies zu umgehen, kann auch ein drehfester Ecklagereinsatz in der Bolzenaufnahme angeordnet werden. So wird die Drehbewegung vom Achsbolzen zum Gewindestift unterbrochen. Eine versehentliche Verstellung wird somit ausgeschlossen.In order to allow an adjustment of the horizontally extending Falzluftbereichs, it is advantageous if the bolt receptacle has a vertical adjustment. For this purpose, the vertical adjustment, for example, a threaded pin, which is supported directly or indirectly on a pivot pin, have. Turning the threaded pin in or out raises or lowers the corner band. To avoid accidental adjustment of the height adjustment when opening and closing the sash, it must be ensured that the friction forces between the bolt receiver and the threaded pin are greater than those between the threaded pin and the axle bolt. To avoid this, a non-rotating corner bearing insert can be arranged in the bolt receptacle. Thus, the rotational movement is interrupted by the axle bolt to the set screw. An accidental adjustment is thus excluded.

In den Rahmen der Erfindung fällt auch ein Fenster, eine Tür oder dergleichen, mit einem festen Rahmen und/oder wenigstens einem Flügelrahmen, wobei im Falzluftbereich zwischen festem Rahmen und Flügelrahmen zumindest eine Ecklager-Baugruppe vorgesehen ist, die ein vorher beschriebenes Eckband aufweist. Ein derartiges Fenster oder eine derartige Tür kann mit sehr geringen Falzluftbereichen ausgebildet werden.In the scope of the invention, a window, a door or the like, with a fixed frame and / or at least one wing frame, wherein in Falzluftbereich between the fixed frame and sash at least one corner bearing assembly is provided which has a previously described Eckband. Such a window or such a door can be formed with very low Falzluftbereichen.

Vorzugsweise ist dabei die Ecklagerbaugruppe als verdeckt liegender Beschlag ausgebildet. Sie ist also bei geschlossenem Flügel nicht sichtbar.Preferably, the corner bearing assembly is designed as concealed fitting. So it is not visible with the wing closed.

Weitere Merkmale und Vorteile der Erfindung ergeben sich aus der nachfolgenden Beschreibung von Ausführungsbeispielen der Erfindung, anhand den 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
eine perspektivische Draufsicht auf den Eckbereich eines Flügels mit erfindungsgemäßem Eckband;
Fig. 2a
eine perspektivische Ansicht einer ersten Ausführungsform eines Eckbands;
Fig. 2b
eine teilweise geschnittene Darstellung des Eckbands der Fig. 2a;
Fig. 2c
das Eckband der Fign. 2a, 2b mit gegenüber der Flügelaufnahme verlagerter Bolzenaufnahme;
Fig. 3a
eine Ausführungsform eines Eckbands mit Ausdrehsicherung;
Fig. 3b
eine Detaildarstellung der Fig. 3a;
Fig. 4a
eine alternative Ausführungsform eines Eckbands;
Fig. 4b
eine teilweise geschnittene Darstellung des Eckbands der Fig. 4a;
Fig. 5
eine Variante eines Eckbands mit einer anderen Ausführungsform einer Verstelleinrichtung;
Fig. 6a
eine weitere Ausführungsform eines Eckbands mit Anlenkpunkt am Tragarm;
Fig. 6b
eine teilweise geschnittene Darstellung des Eckbands der Fig. 6a;
Fig. 7
eine erste Ausführungsform einer Ecklager-Baugruppe;
Fig. 8
eine zweite Ausführungsform einer Ecklager-Baugruppe.
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
a perspective top view of the corner region of a wing with inventive corner band;
Fig. 2a
a perspective view of a first embodiment of a corner band;
Fig. 2b
a partially sectioned view of the corner band of Fig. 2a;
Fig. 2c
the corner band of Fign. 2a, 2b with respect to the wing receiving displaced bolt receptacle;
Fig. 3a
an embodiment of a corner band with Ausdrehsicherung;
Fig. 3b
a detailed view of Fig. 3a;
Fig. 4a
an alternative embodiment of a corner band;
Fig. 4b
a partially sectioned view of the corner band of Fig. 4a;
Fig. 5
a variant of a corner band with another embodiment of an adjusting device;
Fig. 6a
a further embodiment of a corner band with pivot point on the support arm;
Fig. 6b
a partially sectioned view of the corner band of Fig. 6a;
Fig. 7
a first embodiment of a corner bearing assembly;
Fig. 8
a second embodiment of a corner bearing assembly.

In der Fig. 1 ist der Eckbereich eines Flügels 1 dargestellt. Im Eckbereich ist ein Eckband 10 angeordnet. Das Eckband 10 weist eine Flügelaufnahme 11 und eine Bolzenaufnahme 12 auf. Aus der Fig. 1 ist ersichtlich, dass das Eckband 10 nicht über eine Flügelfalzumfangsfläche 2 nach unten hervorsteht. Insbesondere ist das Eckband 10 im Wesentlichen in einem Flügelrahmenteil 3 angeordnet. Die Flügelaufnahme 11 kann durch nicht dargestellte Befestigungsmittel über Befestigungsöffnungen 4 am Flügel 1 befestigt werden.In Fig. 1 the corner region of a wing 1 is shown. In the corner, a corner band 10 is arranged. The corner band 10 has a wing receptacle 11 and a bolt receptacle 12. From Fig. 1 it can be seen that the corner band 10 does not protrude over a Flügelfalzumfangsfläche 2 down. In particular, the corner band 10 is arranged essentially in a wing frame part 3. The wing receptacle 11 can be secured by fastening means, not shown, via mounting holes 4 on the wing 1.

Aus der Fig. 2a ist ersichtlich, dass das Eckband 10 als Eckwinkel ausgeführt ist. Ein vertikaler Schenkel 13 und ein horizontaler Schenkel 14 sind an dem Flügel 1 befestigbar. Der horizontale Schenkel 14 umfasst eine im Querschnitt U-förmige Lasche 15, die eine in der Fig. 2a nicht sichtbare Tragarmaufnahme umgreift, die in einem Teil der Flügelaufnahme 11 angeordnet ist.From Fig. 2a it can be seen that the corner band 10 is designed as a corner angle. A vertical leg 13 and a horizontal leg 14 can be fastened to the wing 1. The horizontal leg 14 comprises a cross-sectionally U-shaped tab 15 which engages around a not visible in FIG. 2a support arm, which is arranged in a part of the wing holder 11.

In der teilweisen Schnittdarstellung der Fig. 2b ist zu erkennen, dass in der Flügelaufnahme 11 eine Tragarmaufnahme 16 für einen Tragarm 17 der Bolzenaufnahme 12 ausgebildet ist. Durch die Anordnung des Tragarms 17 und der Tragarmaufnahme 16 der Flügelaufnahme 11 ergibt sich ein teleskopierbarer horizontaler Schenkel 14 des Eckbands 10. Die Verstellung der Bolzenaufnahme 12 gegenüber der Flügelaufnahme 11 erfolgt über eine Verstelleinrichtung 18, die eine als Madenschraube ausgebildete Einstellschraube 19 umfasst, welche axial unverschieblich in einer Aussparung 20 der Bolzenaufnahme 12 angeordnet ist. Die Schraube 19 wirkt mit einem Gewindeausschnitt 21 der Flügelaufnahme 11 zusammen. Durch Drehen der Schraube 19 lässt sich die Bolzenaufnahme 12 in die Flügelaufnahme 11 einbringen. Da die Schraube 19 in der Bolzenaufnahme 12 nicht verschoben werden kann, folgt die Bolzenaufnahme 12 der Gewindesteigung beim Drehen der Schraube 19, welche sich am Gewindeausschnitt 21 der Flügelaufnahme 11 anlegt. Auf diese Weise lässt sich die seitliche Falzluft einstellen.In the partial sectional view of FIG. 2b, it can be seen that a support arm receptacle 16 for a support arm 17 of the bolt receptacle 12 is formed in the wing receptacle 11. The arrangement of the support arm 17 and the Tragarmaufnahme 16 of the wing receptacle 11 results in a telescoping horizontal leg 14 of the corner band 10. The adjustment of the bolt receptacle 12 relative to the wing receptacle 11 via an adjusting device 18 which includes a trained as a set screw adjusting screw 19, which axially is arranged immovably in a recess 20 of the bolt receptacle 12. The screw 19 cooperates with a thread cutout 21 of the wing receptacle 11. By turning the screw 19, the bolt receptacle 12 can be introduced into the wing receptacle 11. Since the screw 19 in the bolt receptacle 12 can not be moved, the bolt receptacle 12 follows the thread pitch when turning the screw 19, which applies to the thread cutout 21 of the wing receptacle 11. In this way, the lateral folding air can be adjusted.

Zur Einstellung der oberen und unteren Falzluft ist eine Vertikalverstelleinrichtung 22 vorgesehen, die einen nicht dargestellten Gewindestift umfasst, der auf einen drehfest angeordneten Ecklagereinsatz 23 wirkt, an dem sich ein nicht dargestellter Achsbolzen abstützt.For adjusting the upper and lower folding air, a vertical adjustment device 22 is provided, which comprises a threaded pin, not shown, which acts on a non-rotatably mounted Ecklagereinsatz 23 at which an unillustrated pivot pin is supported.

In der gemäß der Fig. 2c gezeigten Darstellung des Eckbands 10 wurde die Bolzenaufnahme 12 über die Schraube 19 gegenüber der Flügelaufnahme 11 verstellt, so dass sich zwischen dem Tragarm 17 und der Flügelaufnahme 11 in der Tragarmaufnahme 16 ein Spalt ergibt. Die gezeigte Darstellung entspricht der größten einstellbaren seitlichen Falzluft.In the illustration of the corner band 10 shown according to FIG. 2c, the bolt receptacle 12 has been adjusted by means of the screw 19 with respect to the wing receptacle 11, so that a gap results between the support arm 17 and the wing receptacle 11 in the support arm receptacle 16. The illustration shown corresponds to the largest adjustable lateral folding air.

Ausweislich der Fign. 3a und 3b, wobei die Fig. 3b vergrößert einen Ausschnitt der Fig. 3a zeigt, ist eine Ausdrehsicherung 25 vorgesehen. Die Ausdrehsicherung 25 umfasst eine Aussparung 26 in der Bolzenaufnahme 12 beziehungsweise im Tragarm 17; in die eine Ausprägung 27 der im Querschnitt U-förmigen Lasche 15 eingreift. Die Erstreckung der Aussparung 26 in Falzumfangsrichtung ist größer als die Erstreckung der Ausprägung 27. Durch das Zusammenwirken der Aussparung 26 und der Ausprägung 27 wird die Bewegung der Bolzenaufnahme 12 begrenzt. Insbesondere kann die Bolzenaufnahme 12 im montierten Zustand des Eckbands 10 nicht demontiert werden.Evidenced the Fign. 3a and 3b, wherein the Fig. 3b shows an enlarged section of Fig. 3a, a Ausdrehsicherung 25 is provided. The Ausdrehsicherung 25 includes a recess 26 in the bolt receptacle 12th or in the support arm 17; in the one expression 27 of cross-sectionally U-shaped tab 15 engages. The extent of the recess 26 in the fold circumferential direction is greater than the extent of the expression 27. The interaction of the recess 26 and the expression 27, the movement of the pin holder 12 is limited. In particular, the bolt receptacle 12 can not be dismantled in the assembled state of the corner band 10.

Gemäß der in der Fig. 4a gezeigten Ausführungsform eines Eckbands 30 ist die Flügelaufnahme 31 einstückig ausgeführt. Insbesondere fehlt bei dieser Ausführungsform die U-förmige Lasche. An der Flügelaufnahme 31 selbst sind Befestigungsöffnungen 4 vorgesehen.According to the embodiment of a corner band 30 shown in FIG. 4a, the wing receptacle 31 is made in one piece. In particular, in this embodiment, the U-shaped tab is missing. At the wing receptacle 31 itself mounting holes 4 are provided.

Wie sich aus der Schnittdarstellung der Fig. 4b ergibt, ist der Teil der Flügelaufnahme 31, in dem die Tragarmaufnahme 36 ausgebildet ist, länger ausgeführt als im Ausführungsbeispiel der Figuren 1 - 3b. Die Flügelaufnahme 31 ist stufenförmig aufgebaut. Insbesondere ist die Flügelaufnahme 31 auf eine stufenförmige Beschlagteilnut des Flügels 1 angepasst. Der Teil 31' kommt dabei in einer tieferen Beschlagteilnut zu liegen und der Teil 31" kommt in einem falzseitigen Bereich der Beschlagteilnut zu liegen. Vorzugsweise schließt der Bereich 31" bündig an eine Flügelfalzumfangsfläche an.As is apparent from the sectional view of Fig. 4b, the part of the wing receptacle 31, in which the Tragarmaufnahme 36 is formed, designed to be longer than in the embodiment of Figures 1 - 3b. The wing receptacle 31 is constructed in steps. In particular, the wing receptacle 31 is adapted to a stepped fitting part of the wing 1. The part 31 'comes to lie in a deeper fitting part groove and the part 31 "comes to rest in a fold-side region of the fitting part groove.

In der Ausführungsform der Fig. 5 ist bei der Verstelleinrichtung 18 die Schraube 19 axial unverschieblich in einer Aussparung 20' der Flügelaufnahme 31 angeordnet. Sie greift dagegen in einen Gewindeausschnitt 21' der Bolzenaufnahme 32 ein.In the embodiment of FIG. 5, in the adjustment device 18, the screw 19 is arranged axially immovably in a recess 20 'of the wing receptacle 31. In contrast, it engages in a threaded cutout 21 'of the bolt receptacle 32.

Das Eckband 40 der Fig. 6a weist ein Langloch 43 in der Flügelaufnahme 41 auf, durch das eine als Bolzen ausgebildete Anlenkeinrichtung 45 ragt. Der Schnittdarstellung der Fig. 6b kann man entnehmen, dass die Anlenkeinrichtung 45 am freien Ende des Tragarms 47 der Bolzenaufnahme 42 angeordnet ist. Dies bedeutet, dass unabhängig von der seitlichen Falzlufteinstellung der Abstand zwischen der Anlenkeinrichtung 45 und der hülsenartigen Aufnahme 48 für einen Achsbolzen der Bolzenaufnahme 42 konstant bleibt. Im Ausführungsbeispiel der Fign. 6a, 6b ist der Tragarm 47 gegenüber den vorherigen Ausführungsbeispielen verlängert, da die Scherengeometrie in diesem Fall anders als vorher, wo die Flügelaufnahme zur Anlenkung der Scherengeometrie bestimmt ist, an dem Tragarm der Bolzenaufnahme angelenkt werden soll.The corner band 40 of FIG. 6a has a slot 43 in the wing receptacle 41, through which an articulation device 45 designed as a bolt protrudes. The sectional view of Fig. 6b can be seen that the hinge device 45 is arranged at the free end of the support arm 47 of the bolt receptacle 42. This means that regardless of the lateral Falzlufseinstellung the distance between the hinge 45 and the sleeve-like receptacle 48 for a pivot pin of the bolt holder 42 remains constant. In the embodiment of FIGS. 6a, 6b, the support arm 47 is extended compared to the previous embodiments, since the scissor geometry in this case, unlike before, where the wing receptacle is intended for articulation of the scissors geometry, to be articulated on the support arm of the bolt receptacle.

In der Fig. 7 ist eine Ecklager-Baugruppe 49 mit dem Eckband 10 dargestellt, das an einer Scherengeometrie 50 befestigt ist. Ein nicht sichtbarer Achsbolzen, der von dem Lenker 51 absteht, ragt in die Bolzenaufnahme 12. Die Scherengeometrie 50 ist an einem Eckwinkel 52 befestigt, der zur Befestigung am festen Rahmen bestimmt ist. Gezeigt ist eine geöffnete Stellung. Bei geschlossenem Flügel liegen die Lenker 51, 53 abschnittsweise übereinander im Falzluftbereich. Die Scherengeometrie 50 ist derart ausgestaltet, dass der Flügel zu Beginn der Öffnungsbewegung vom festen Rahmen abgehoben wird, ehe die Schwenkbewegung beginnt. Der Lenker 53 ist an der U-förmigen Lasche 15 angelenkt, wobei die Anlenkeinrichtung in einem Langloch der U-förmigen Lasche 15 verschieblich angeordnet ist. Eine Verstellung der seitlichen Falzluft beeinträchtigt die Funktion der Scherengeometrie daher nicht.FIG. 7 shows a corner bearing assembly 49 with the corner band 10, which is attached to a scissors geometry 50. An invisible axle pin protruding from the handlebar 51 protrudes into the bolt receptacle 12. The scissors geometry 50 is fixed to a corner bracket 52 which is intended to be fixed to the fixed frame. Shown is an open position. When the sash is closed, the links 51, 53 overlap in sections in the rebate air area. The scissors geometry 50 is designed such that the wing is lifted off the fixed frame at the beginning of the opening movement, before the pivoting movement begins. The link 53 is articulated on the U-shaped tab 15, wherein the articulation device 15 is slidably disposed in a slot of the U-shaped tab. An adjustment of the lateral folding air does not affect the function of the scissor geometry therefore.

Die in der Fig. 8 dargestellte Scherengeometrie 60 der Eckager-Baugruppe 59 weist einen zusätzlichen Lenker 61 auf, der an dem Tragarm der Bolzenaufnähme 42 des Eckbands 40 angelenkt ist. Die Scherengeometrie 60 benötig einen konstanten Abstand zwischen der Anlenkstelle am Tragarm und dem Achsbolzen, um bei unterschiedlichen Falzlufteinstellungen dieselbe Öffnungskinematik zu erhalten.The scissor geometry 60 of the corner bearing assembly 59 shown in FIG. 8 has an additional link 61, which is articulated on the support arm of the bolt receptacle 42 of the corner band 40. The scissors geometry 60 requires a constant distance between the articulation point on the support arm and the axle bolt in order to obtain the same opening kinematics at different folding air settings.

Claims (12)

  1. Window, door or the like, having a fixed frame and at least one leaf frame (3), with at least one corner bearing subassembly (49, 59) being provided in the joint clearance region between the fixed frame and the leaf frame (3) and having a corner (10, 30, 40), comprising a leaf receiving member (11, 31, 41) which can be secured to the leaf frame (3) and a pin receiving member (12, 32, 42) which has a carrier arm (17, 47), the carrier arm (17, 47) of the pin receiving member (12, 32, 42) being guided in a telescope-like manner in a carrier arm receiving member (16, 36) of the leaf receiving member (11, 31, 41), characterised in that the carrier arm (17, 47) is arranged at least substantially at the side of a leaf joint peripheral face (2) that faces away from the fixed frame, and the corner bearing subassembly (49, 59) is in the form of a fitting which is arranged in a concealed manner.
  2. Window, door or the like according to claim 1, characterised in that the carrier arm receiving member (16, 36) extends in a peripheral manner around the carrier arm (17, 47) at least in portions.
  3. Window, door or the like according to either claim 1 or claim 2, characterised in that the carrier arm receiving member (16, 36) is in the form of a sleeve or blind hole.
  4. Window, door or the like according to any one of the preceding claims, characterised in that the carrier arm (17, 47) is constructed so as to be rectangular or square in cross-section and the carrier arm receiving member (16, 36) is adapted to the carrier arm (17, 47).
  5. Window, door or the like according to any one of the preceding claims, characterised in that the leaf receiving member (31, 41) is constructed in one piece.
  6. Window, door or the like according to any one of the preceding claims, characterised in that an adjustment device (18), which is accessible in the vertically extending joint clearance region, is provided in order to adjust the distance between the pin receiving member (12, 32, 42) and the leaf receiving member (11, 31, 41).
  7. Window, door or the like according to claim 6, characterised in that the distance can be adjusted by means of an adjustment screw (19), with the adjustment screw (19) being arranged in an axially non-movable manner in the pin receiving member (12, 32, 42) or the leaf receiving member (11, 31, 41) and cooperating with a threaded recess (21, 21') of the other element in each case.
  8. Window, door or the like according to any one of the preceding claims, characterised in that the horizontal limb of the leaf receiving member (10) comprises a lug (15) which is U-shaped in cross-section.
  9. Window, door or the like according to any one of the preceding claims, characterised in that an unscrewing securing means is provided in order to prevent complete separation of the pin receiving member (12, 32, 42) and the leaf receiving member (11, 31, 41).
  10. Window, door or the like according to any one of the preceding claims, characterised in that an articulation device (45) for a scissors type mechanism (60) is provided at the pin receiving member (42), in particular at the free end of the carrier arm (47).
  11. Window, door or the like according to any one of the preceding claims, characterised in that the pin receiving member (12, 32, 42) has a vertical adjustment device (22).
  12. Window, door or the like according to claim 11, characterised in that the vertical adjustment device (22) has a threaded pin and a rotationally fixed corner bearing insert (23) which is supported thereon.
EP05018146A 2005-08-22 2005-08-22 Corner support Active EP1757767B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
AT05018146T ATE382116T1 (en) 2005-08-22 2005-08-22 CORNER BAND
EP05018146A EP1757767B1 (en) 2005-08-22 2005-08-22 Corner support
PL05018146T PL1757767T3 (en) 2005-08-22 2005-08-22 Corner support
DE502005002354T DE502005002354D1 (en) 2005-08-22 2005-08-22 corner hinge
ES05018146T ES2297576T3 (en) 2005-08-22 2005-08-22 CORNER PROTECTOR.
SI200530198T SI1757767T1 (en) 2005-08-22 2005-08-22 Corner support

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP05018146A EP1757767B1 (en) 2005-08-22 2005-08-22 Corner support

Publications (2)

Publication Number Publication Date
EP1757767A1 EP1757767A1 (en) 2007-02-28
EP1757767B1 true EP1757767B1 (en) 2007-12-26

Family

ID=35695049

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05018146A Active EP1757767B1 (en) 2005-08-22 2005-08-22 Corner support

Country Status (6)

Country Link
EP (1) EP1757767B1 (en)
AT (1) ATE382116T1 (en)
DE (1) DE502005002354D1 (en)
ES (1) ES2297576T3 (en)
PL (1) PL1757767T3 (en)
SI (1) SI1757767T1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012222210A1 (en) 2012-12-04 2014-06-05 Aug. Winkhaus Gmbh & Co. Kg For concealed arrangement provided corner bearing

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008000048A1 (en) 2008-01-14 2009-07-16 Aug. Winkhaus Gmbh & Co. Kg Corner hinge of a corner bearing
ES2578285B1 (en) * 2015-10-13 2017-05-04 Sistemas Técnicos Del Accesorio Y Componentes, S.L. (Stac) HIDDEN HINGE FOR DOORS AND WINDOWS AND WINDOW OR ASSOCIATED DOOR

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4216689A1 (en) * 1992-05-20 1993-11-25 Hautau Gmbh W Concealed hinge joint
DE9301655U1 (en) 1993-02-06 1994-06-09 Siegenia Frank Kg Hinge fitting
DE19650085C2 (en) * 1996-12-03 1998-10-15 Aubi Baubeschlaege Gmbh Lower corner bearing for a tilt and swivel window, a tilt and swivel door or the like

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012222210A1 (en) 2012-12-04 2014-06-05 Aug. Winkhaus Gmbh & Co. Kg For concealed arrangement provided corner bearing
EP2740872A2 (en) 2012-12-04 2014-06-11 Aug. Winkhaus GmbH & Co. KG Corner bearing for concealed assembly
EP2740872A3 (en) * 2012-12-04 2017-04-19 Aug. Winkhaus GmbH & Co. KG Corner bearing for concealed assembly

Also Published As

Publication number Publication date
ES2297576T3 (en) 2008-05-01
ATE382116T1 (en) 2008-01-15
PL1757767T3 (en) 2008-05-30
SI1757767T1 (en) 2008-06-30
EP1757767A1 (en) 2007-02-28
DE502005002354D1 (en) 2008-02-07

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