EP2034114B1 - Concealed load-relieving device for a window, door or similar - Google Patents

Concealed load-relieving device for a window, door or similar Download PDF

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Publication number
EP2034114B1
EP2034114B1 EP07017637A EP07017637A EP2034114B1 EP 2034114 B1 EP2034114 B1 EP 2034114B1 EP 07017637 A EP07017637 A EP 07017637A EP 07017637 A EP07017637 A EP 07017637A EP 2034114 B1 EP2034114 B1 EP 2034114B1
Authority
EP
European Patent Office
Prior art keywords
corner bearing
wing
arm
frame
concealed
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.)
Not-in-force
Application number
EP07017637A
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German (de)
French (fr)
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EP2034114A1 (en
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
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Roto Frank AG
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Filing date
Publication date
Application filed by Roto Frank AG filed Critical Roto Frank AG
Priority to DE502007007002T priority Critical patent/DE502007007002D1/en
Priority to PL07017637T priority patent/PL2034114T3/en
Priority to EP07017637A priority patent/EP2034114B1/en
Priority to AT07017637T priority patent/ATE506515T1/en
Priority to SI200730633T priority patent/SI2034114T1/en
Publication of EP2034114A1 publication Critical patent/EP2034114A1/en
Application granted granted Critical
Publication of EP2034114B1 publication Critical patent/EP2034114B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05FDEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F7/00Accessories for wings not provided for in other groups of this subclass
    • E05F7/06Devices for taking the weight of the wing, arranged away from the hinge axis
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/28Suspension arrangements for wings supported on arms movable in horizontal plane
    • E05D15/30Suspension arrangements for wings supported on arms movable in horizontal plane with pivoted arms and sliding guides
    • 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
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2600/00Mounting or coupling arrangements for elements provided for in this subclass
    • E05Y2600/40Mounting location; Visibility of the elements
    • E05Y2600/41Concealed
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/132Doors
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/148Windows

Definitions

  • the invention relates to a concealed Ecklageran extract with eimen concealed Ecklagerbeschlag and a concealed relief arrangement for a window, a door or the like.
  • the relief arrangement a pair of scissors includes.
  • the invention relates to a corner bearing assembly and a window, a door or the like.
  • the sash weight must be absorbed by the concealed fitting.
  • the wing must first be opened for opening from the fixed frame so that there is no collision between the rollover and the frame when the wing is opened.
  • a scissors geometry must be provided so that a parking of the wing is even possible.
  • Such a scissors geometry can be designed to remove the weight of the wing or to introduce it into the frame, up to a certain wing weight. Due to the limited installation space, however, the sizing of the scissors geometry limits, so that the scissor geometry can not be designed for arbitrarily high sash weights.
  • a bearing axis for a support arm is provided on a hidden lower part of a bearing pin. Its upper end is mounted via an axis on a mounting plate or the vertical leg of a mounting bracket.
  • the sash weight is at least substantially abandoned on this support arm on the fixed frame.
  • the connection of the support arm with a rotary tilting joint and with the mounting plate is designed so that a slight inclination of the support arm is possible.
  • the EP 0 710 758 A1 describes a relief element which is attached to the side facing away from the corner bearing of the window frame and thus is not part of a Ecklageran angel.
  • a support means which is formed by a support rod which is supported with its upper end to a wing frame side support bracket and with its lower end to a Ecklagerwinkel.
  • the disadvantage is that the wing frame which is supported on the support rod subsequently undergoes a lowering movement during the opening of the wing after an initial slight lifting movement.
  • Object of the present invention is to provide a structurally simple to implement, avoiding the disadvantages mentioned above relief arrangement.
  • a corner bearing arrangement with the features of claim 1.
  • the one end of the tension arm for direct or indirect e.g. is formed by an adapter, engaging a wing-supporting fitting part.
  • Such an embodiment of the relief arrangement has the advantage that the relief arrangement engages wing side only at one point and thus exerts no lateral forces on the wing.
  • the relief arrangement according to the invention is intended in particular for partial relief, ie for a partial removal of the wing load.
  • the tension arm is arranged vertically adjustable on the frame attachment part.
  • the pulling arm can be arranged to be height-adjustable on the frame fastening part.
  • the height-adjustable and pivotable arrangement of the pull arm on the frame attachment part can be particularly easily realized in that the frame attachment part has a slot in which a fixed on the pull arm arranged bolt is guided. It is understood that a kinematic reversal is also conceivable, namely that a slot is formed on the pull arm and a stationary bolt is provided on the frame mounting part.
  • Corner bearing fittings often have a pin with a thickening on which a wing is placed, or can be easily equipped with such a pin.
  • a coupling of the relief arrangement with a part of the corner bearing fitting on which the wing load acts directly, can therefore be realized in a particularly simple manner when the tension arm has a fork of the corner bearing fitting under cross-fork at its wing-side end.
  • the wing-side end of the pull arm may also be otherwise, e.g. hook-shaped, be formed. In any case, it is preferably adapted to the possibility of attachment to a fitting supporting the wing.
  • the fork is formed trough-like. This can ensure that the fork and the pin always have a sufficiently large contact surface at different angular positions of the pulling arm.
  • the frame attachment part is designed as a part independent of a corner bearing fitting.
  • the relief arrangement can be particularly easily combined with the Ecklagerbeschlag, which is designed for lower wing loads.
  • Ecklagerbeschlag By the relief arrangement, it is possible to use the designed for lower wing loads Ecklagerbeschlag even with heavier wings, the relief arrangement removes a portion of the wing load. It is also possible to simply retrofit the discharge arrangement.
  • the frame attachment part is part of the corner bearing fitting. This has the advantage that the relief arrangement is an integral part of the corner bearing and can be mounted together with it.
  • a concealed corner bearing assembly with a relief arrangement described above, and a window, a door or the like.
  • a concealed corner bearing assembly with a relief arrangement described above, and a window, a door or the like.
  • the Fig. 1 shows a corner bearing assembly 10, with a concealed corner bearing fitting 11 and a discharge assembly 12.
  • the relief assembly 12 includes a frame attachment member 13 to which a support arm 14 is pivotally mounted.
  • the support arm 14 is also pivotally connected to the pull arm 15, which in turn is pivotally connected to the bolt 16 to the frame attachment part 13.
  • the pulling arm 15 performs a pure pivoting movement in a plane when opening and closing a wing. Unlike known support rods or ropes, he makes no rotational movement.
  • the pulling arm 15 is dimensioned so that it removes a part of its load even with the wing closed.
  • the bolt 16 is arranged vertically displaceable in a slot 17 of the frame attachment part 13.
  • the pulling arm 15 is angled at its free end 18, wherein the free end 18 is fork-shaped and a thickening 19 of a pin 20 engages behind.
  • a wing or a wing-side fitting part can be placed on the pin 20 .
  • opening and closing the pin 20 makes a movement perpendicular to the window plane approximately along a straight line. In particular, he does not make a pendulum motion.
  • the scissors 21 is partially relieved of the sash weight as the wing-supporting fitting part. That's it possible, in particular the arm 22 form thinner, so that it fits with the wing closed in the Falz Kunststoff Kunststoff.
  • the guide 24 is aligned obliquely to the window plane. It could also be curved.
  • the relief arrangement 12 is shown in a plan view.
  • the frame attachment part 13 the pull arm 15 and the support link 14 are aligned in the fold circumferential direction. Even with the wing closed, the pulling arm 15 engages behind the thickening 19 of the bolt 20. It can be seen that the thickening 19 is curved. For this reason, the fork-like free end 18 of the tension arm 15 has a trough-like depression 26. This ensures that there is always a sufficiently large contact surface between the free end 18 and the thickening 19 at different inclination of the traction arm 15.
  • the Fig. 4 shows a plan view of the corner bearing assembly 10 without the mounting leg 25 and the parts arranged thereon, wherein the position shown corresponds to a closed position of a wing.
  • the corner bearing assembly is particularly designed for use as a concealed fitting.
  • a solid frame formed as a frame is connected via the corner bearing assembly 10 with a wing.
  • the wing has a rollover.
  • the wing In order to open the wing, the wing must therefore first be turned off the frame. This is made possible by the corner bearing assembly 10, namely by the arm 22 and the tab 50, which form a scissors geometry (see also Fig. 5 ).
  • the geometry of the scissors is designed so that the wing is turned off as little as possible while still providing the greatest possible clearance. To open the wing of this is just turned off so far from the frame, that there is no collision hiss the flashover and the frame.
  • the scissor geometry is located above a base plate 52, with which attachment to a fixed enclosure, in particular a fixed frame, can take place. In particular, no part projects laterally beyond the base plate 52.
  • the Fig. 4 can be seen that the elements 22, 50 must be arranged with the sash closed in Falz Kunststoff Kunststoff. Therefore, the elements 22, 50 may have only a limited thickness and, in particular, may not be dimensioned as large as would be necessary for large wing loads (if no relief assembly 12 is used).
  • the pin 51 is moved in the guide 24 in a forward position.
  • the inclined guide 24, which can also be performed bent it is possible to build the corner bearing assembly 10 is smaller and more stable overall. In particular, this makes it possible to realize a very small scissors geometry.
  • the in the Fig. 5 shown position corresponds to an open position of the wing. It can be seen that the location where the bolt 20 is located has been moved approximately along a straight line perpendicular to the window plane. This means that the pulling arm 15 has practically performed a pure pivoting movement.
  • the weight of the wing is transmitted via the not shown, attached to the wing corner band on the bolt 20. This then transmits the weight on the tab 50.
  • the tab 50 rests on the arm 22 and thus transmits the load to the arm 22.
  • the scissor geometry was chosen so that the greatest possible overlap of the tab 50 and the arm 22 with the wing open is available. Thus, a resulting bending moment is kept small.
  • the arm 22 introduces the sash weight or a portion of the sash weight over the base plate 52 in the fixed frame.
  • the pin 51 was moved during the opening of the wing in the guide 24 in a rear position.
  • the guide 24 limits the relative movement of the arm 22 and the tab 50.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Wing Frames And Configurations (AREA)
  • Hinges (AREA)
  • Window Of Vehicle (AREA)
  • Lock And Its Accessories (AREA)

Abstract

The arrangement (12) has a support guide (14) fastened to a frame fastener (13) in a swivelable manner. The support guide is connected with a traction arm (15) in a swivelable manner, where the traction arm is arranged swivelably on a frame side on an end and/or engaged to a wing or a fitting part supporting the wing on another end. The traction arm is arranged on the frame fastener in a height adjustable manner. The frame fastener exhibits a slotted hole (17) into which a stationary pin (16) arranged on the traction arm is guided.

Description

Die Erfindung betrifft eine verdeckt liegende Ecklageranordnung mit eimen verdeckt liegenden Ecklagerbeschlag und einer verdeckt liegenden Entlastungsanordnung für ein Fenster, eine Tür oder dgl. zur zumindest teilweisen Entlastung des verdeckt liegenden Ecklagerbeschlags vom Flügelgewicht des Fensters, der Tür oder dgl., wobei die Entlastungsanordnung eine Schere umfasst. Weiterhin betrifft die Erfindung eine Ecklageranordnung sowie ein Fenster, eine Tür oder dergleichen.The invention relates to a concealed Ecklageranordnung with eimen concealed Ecklagerbeschlag and a concealed relief arrangement for a window, a door or the like. For at least partial relief of the concealed Ecklagerbeschlags the sash weight of the window, door or the like., The relief arrangement a pair of scissors includes. Furthermore, the invention relates to a corner bearing assembly and a window, a door or the like.

Bei verdeckt liegenden Beschlägen von Fenstern, Türen oder dergleichen, mit und ohne Überschlag, muss das Flügelgewicht durch den verdeckt liegenden Beschlag aufgenommen werden. Weiterhin muss, insbesondere bei Fenstern, Türen oder dergleichen mit Überschlag, der Flügel zum Öffnen zunächst vom festen Rahmen abgestellt werden, damit es nicht zu einer Kollision zwischen Überschlag und Blendrahmen beim Öffnen des Flügels kommt. Für den verdeckt liegenden Beschlag steht nur ein begrenzter Einbauraum zu Verfügung. Auf diesem engen Einbauraum muss eine Scherengeometrie vorgesehen werden, damit ein Abstellen des Flügels überhaupt ermöglicht wird. Bis zu einem bestimmten Flügelgewicht kann eine solche Scherengeometrie dazu ausgelegt werden, das Gewicht des Flügels abzutragen beziehungsweise in den Rahmen einzuleiten. Aufgrund des begrenzten Einbauraums sind jedoch der Dimensionierung der Scherengeometrie Grenzen gesetzt, so dass die Scherengeometrie nicht für beliebig hohe Flügelgewichte ausgelegt werden kann.For concealed fittings of windows, doors or the like, with and without rollover, the sash weight must be absorbed by the concealed fitting. Furthermore, in particular in the case of windows, doors or the like with rollover, the wing must first be opened for opening from the fixed frame so that there is no collision between the rollover and the frame when the wing is opened. For the concealed fitting only a limited installation space is available. In this narrow installation space, a scissors geometry must be provided so that a parking of the wing is even possible. Such a scissors geometry can be designed to remove the weight of the wing or to introduce it into the frame, up to a certain wing weight. Due to the limited installation space, however, the sizing of the scissors geometry limits, so that the scissor geometry can not be designed for arbitrarily high sash weights.

Um diesbezüglich Abhilfe zu schaffen schlägt die EP 0 403 774 B1 einen Beschlag gemäß des Oberbegriffs des Anspruchs 1 vor, bei dem größere Flügelgewichte ohne Verwendung von Zugelementen zugelassen werden können. Hierzu ist an einem verdeckten unteren Teil eines Lagerbolzens eine Lagerachse für einen Tragarm vorgesehen. Dessen oberes Ende ist über eine Achse an einer Befestigungsplatte beziehungsweise dem vertikalen Schenkel eines Befestigungswinkels gelagert. Das Flügelgewicht wird zumindest im Wesentlichen über diesen Tragarm auf den festen Rahmen aufgegeben. Die Verbindung des Tragarms mit einem Dreh-Kippgelenk und mit der Befestigungsplatte ist so ausgebildet, dass eine leichte Schrägstellung des Tragarms möglich ist.To remedy this situation suggests the EP 0 403 774 B1 a fitting according to the preamble of claim 1, in which larger sash weights can be permitted without the use of tension elements. For this purpose, a bearing axis for a support arm is provided on a hidden lower part of a bearing pin. Its upper end is mounted via an axis on a mounting plate or the vertical leg of a mounting bracket. The sash weight is at least substantially abandoned on this support arm on the fixed frame. The connection of the support arm with a rotary tilting joint and with the mounting plate is designed so that a slight inclination of the support arm is possible.

Aus der CH 436 024 ist ein Parallellüfter bekannt, wobei das untere Ende des Flügels an zwei außenliegenden Auslegearmen gelagert.From the CH 436 024 a parallel fan is known, wherein the lower end of the wing mounted on two outer boom arms.

Die EP 0 710 758 A1 beschreibt ein Entlastungselement, das an der dem Ecklager abgewandten Seite des Fensterrahmens angebracht und somit nicht Bestandteil einer Ecklageranordnung ist.The EP 0 710 758 A1 describes a relief element which is attached to the side facing away from the corner bearing of the window frame and thus is not part of a Ecklageranordnung.

In der EP 0 385 414 A1 ist ein Fenster beschrieben, das durch ein verdecktes Zugelement gewichtsentlastet aufgehängt ist. Ein Stützlenker ist nicht offenbart.In the EP 0 385 414 A1 a window is described, which is suspended by a concealed tension member weight-relieved. A support arm is not disclosed.

Bei dem aus der DE 38 29 053 C2 bekannten Beschlag ist eine Stützeinrichtung vorgesehen, die von einem Stützstab gebildet ist, der sich mit seinem oberen Ende an einem flügelrahmenseitigen Stützwinkel und mit seinem unteren Ende an einem Ecklagerwinkel abstützt. Nachteilig ist, dass der sich auf den Stützstab abstützende Flügelrahmen beim Dreh - Öffnen des Flügels nach einer anfänglichen geringfügigen Anhebebewegung anschließend ein Absenkbewegung vollzieht.In the from the DE 38 29 053 C2 Known fitting a support means is provided which is formed by a support rod which is supported with its upper end to a wing frame side support bracket and with its lower end to a Ecklagerwinkel. The disadvantage is that the wing frame which is supported on the support rod subsequently undergoes a lowering movement during the opening of the wing after an initial slight lifting movement.

Aus der EP 0 436 946 B1 ist ein verdeckt liegendes unteres Ecklager bekannt, bei dem ein Stützstab vorgesehen ist, der sich mit seinem unteren Ende auf dem festen Rahmen abstützt und den Flügel drehachsseitig mitträgt. Der Stützstab ist mit seinem oberen Ende am Flügelrahmen höhenverschieblich geführt und mit einem etwa mittig an ihm angelenkten Hängelenker versehen, an dessen unterem Ende der Flügelrahmen hängt. Dabei wird der Stützstab auch seitlich gegen den Flügel gedrückt, so dass durch zusätzliche Maßnahmen sichergestellt werden muss, dass der Flügel durch die Lastabtragung nicht vom festen Rahmen in unerwünschter Weise abgestellt wird.From the EP 0 436 946 B1 is a concealed lower corner bearing known in which a support rod is provided, which is supported with its lower end on the fixed frame and rotatably supports the wing. The support rod is guided vertically displaceable with its upper end on the wing frame and provided with a hinged approximately centrally on him suspension links, at the lower end of the sash hangs. In this case, the support rod is also pressed laterally against the wing, so that it must be ensured by additional measures that the wing is not turned off by the load transfer from the fixed frame in an undesirable manner.

Aufgabe der vorliegenden Erfindung ist es, eine konstruktiv einfach zu realisierende, die oben genannten Nachteile vermeidende Entlastungsanordnung bereitzustellen.Object of the present invention is to provide a structurally simple to implement, avoiding the disadvantages mentioned above relief arrangement.

Gelöst wird diese Aufgabe erfindungsgemäß auf besonders einfache und überraschende Art und Weise durch eine Ecklageranordnung mit den Merkmalen des Anspruchs 1. Dies bedeutet, dass das eine Ende des Zugarms zum unmittelbaren oder mittelbaren, z.B. über einen Adapter, Angreifen an einem den Flügel stützenden Beschlagteil ausgebildet ist. Eine solche Ausgestaltung der Entlastungsanordnung hat den Vorteil, dass die Entlastungsanordnung flügelseitig nur an einem Punkt angreift und somit keine seitlichen Kräfte auf den Flügel ausübt. Die erfindungsgemäße Entlastungsanordnung ist insbesondere für eine Teilentlastung, also für eine teilweise Abtragung der Flügellast gedacht.This object is achieved according to the invention in a particularly simple and surprising way by a corner bearing arrangement with the features of claim 1. This means that the one end of the tension arm for direct or indirect, e.g. is formed by an adapter, engaging a wing-supporting fitting part. Such an embodiment of the relief arrangement has the advantage that the relief arrangement engages wing side only at one point and thus exerts no lateral forces on the wing. The relief arrangement according to the invention is intended in particular for partial relief, ie for a partial removal of the wing load.

Der Zugarm ist höhenveränderlich an dem Rahmenbefestigungsteil angeordnet. Insbesondere kann der Zugarm höhenverschieblich an dem Rahmenbefestigungsteil angeordnet sein. Durch diese Maßnahme kann ein Höhenausgleich realisiert werden, so dass der Flügel beim Dreh- oder Kippöffnen des Flügels aufgrund der Entlastungsanordnung weder angehoben noch abgesenkt wird sondern sich in gleich bleibender Höhe bewegt.The tension arm is arranged vertically adjustable on the frame attachment part. In particular, the pulling arm can be arranged to be height-adjustable on the frame fastening part. By this measure, a height compensation can be realized, so that the wing when turning or tilting of the wing due to the relief arrangement is neither raised nor lowered but moves at a constant height.

Die höhenverschiebliche und schwenkbare Anordnung des Zugarms an dem Rahmenbefestigungsteil kann besonders einfach dadurch realisiert werden, dass das Rahmenbefestigungsteil ein Langloch aufweist, in dem ein ortsfest an dem Zugarm angeordneter Bolzen geführt ist. Es versteht sich, dass auch eine kinematische Umkehr denkbar ist, dass nämlich ein Langloch am Zugarm ausgebildet ist und ein ortsfester Bolzen am Rahmenbefestigungsteil vorgesehen ist.The height-adjustable and pivotable arrangement of the pull arm on the frame attachment part can be particularly easily realized in that the frame attachment part has a slot in which a fixed on the pull arm arranged bolt is guided. It is understood that a kinematic reversal is also conceivable, namely that a slot is formed on the pull arm and a stationary bolt is provided on the frame mounting part.

Ecklagerbeschläge weisen häufig einen Zapfen mit einer Verdickung auf, auf den ein Flügel aufgesetzt ist, oder können einfach mit einem solchen Zapfen ausgestattet werden. Eine Kopplung der Entlastungsanordnung mit einem Teil des Ecklagerbeschlags, auf den die Flügellast unmittelbar wirkt, kann daher auf besonders einfache Art und Weise realisiert werden, wenn der Zugarm an seinem flügelseitigen Ende eine einen Zapfen des Ecklagerbeschlags untergreifende Gabel aufweist. Somit kann der Ecklagerbeschlag besonders einfach vom Flügelgewicht (teilweise) entlastet werden. Das flügelseitige Ende des Zugarms kann auch anderweitig, z.B. hakenförmig, ausgebildet sein. Es ist jedenfalls vorzugsweise an die Befestigungsmöglichkeit an einem den Flügel stützenden Beschlagteil angepasst.Corner bearing fittings often have a pin with a thickening on which a wing is placed, or can be easily equipped with such a pin. A coupling of the relief arrangement with a part of the corner bearing fitting on which the wing load acts directly, can therefore be realized in a particularly simple manner when the tension arm has a fork of the corner bearing fitting under cross-fork at its wing-side end. Thus, the Ecklagerbeschlag particularly easy from the sash weight (partially) be relieved. The wing-side end of the pull arm may also be otherwise, e.g. hook-shaped, be formed. In any case, it is preferably adapted to the possibility of attachment to a fitting supporting the wing.

Bei einer besonders bevorzugten Weiterbildung kann vorgesehen sein, dass die Gabel muldenartig ausgebildet ist. Dadurch kann sichergestellt werden, dass die Gabel und der Zapfen bei unterschiedlichen Winkelstellungen des Zugarms stets eine ausreichend große Berührungsfläche haben.In a particularly preferred development can be provided that the fork is formed trough-like. This can ensure that the fork and the pin always have a sufficiently large contact surface at different angular positions of the pulling arm.

Besonders vorteilhaft ist es, wenn das Rahmenbefestigungsteil als von einem Ecklagerbeschlag unabhängiges Teil ausgebildet ist. Dadurch kann die Entlastungsanordnung besonders einfach mit dem Ecklagerbeschlag kombiniert werden, welches für geringere Flügellasten ausgelegt ist. Durch die Entlastungsanordnung ist es möglich, den für geringere Flügellasten ausgelegten Ecklagerbeschlag auch bei schwereren Flügeln zu verwenden, wobei die Entlastungsanordnung einen Teil der Flügellast abträgt. Auch ist es möglich, die Entlastungsanordnung einfach nachzurüsten.It is particularly advantageous if the frame attachment part is designed as a part independent of a corner bearing fitting. As a result, the relief arrangement can be particularly easily combined with the Ecklagerbeschlag, which is designed for lower wing loads. By the relief arrangement, it is possible to use the designed for lower wing loads Ecklagerbeschlag even with heavier wings, the relief arrangement removes a portion of the wing load. It is also possible to simply retrofit the discharge arrangement.

Bei einer alternativen Ausführungsform kann vorgesehen sein, dass das Rahmenbefestigungsteil Bestandteil des Ecklagerbeschlags ist. Dies hat den Vorteil, dass die Entlastungsanordnung integraler Bestandteil des Ecklagers ist und zusammen mit diesem montiert werden kann.In an alternative embodiment it can be provided that the frame attachment part is part of the corner bearing fitting. This has the advantage that the relief arrangement is an integral part of the corner bearing and can be mounted together with it.

In den Rahmen der Erfindung fällt außerdem eine verdeckt liegende Ecklageranordnung mit einer oben beschriebenen Entlastungsanordnung, sowie ein Fenster, eine Tür oder dgl. mit einem festen Rahmen und einem zumindest um eine insbesondere vertikale Schwenkachse relativ zum festen Rahmen schwenkbaren Flügel, wobei ein verdeckt liegender Beschlag und eine oben beschriebene Entlastungsanordnung vorgesehen sind.In the context of the invention also falls a concealed corner bearing assembly with a relief arrangement described above, and a window, a door or the like. With a fixed frame and at least about a particular vertical pivot axis relative to the fixed frame pivotable wings, wherein a concealed fitting and a relief arrangement as described above are provided.

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
eine perspektivische Darstellung einer Ecklageranordnung mit einer Entlastungsanordnung;
Fig. 2
eine Seitenansicht einer Entlastungsanordnung mit einge- schwenktem Zugarm;
Fig. 3
eine Seitenansicht der Entlastungsanordnung mit ausge- schwenktem Zugarm;
Fig. 4
eine Draufsicht auf die Ecklageranordnung mit eingeschwenk- tem Arm einer Scherengeometrie; und
Fig. 5
eine Draufsicht auf die Ecklageranordnung mit ausgeschwenk- tem Arm der Scherengeometrie.
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 view of a corner bearing assembly with a relief arrangement;
Fig. 2
a side view of a relief arrangement with swiveled arm;
Fig. 3
a side view of the relief arrangement with swung-arm;
Fig. 4
a plan view of the corner bearing assembly with pivoted arm of a scissors geometry; and
Fig. 5
a plan view of the corner bearing assembly with swung arm of the scissors geometry.

Die Fig. 1 zeigt eine Ecklageranordnung 10, mit einem verdeckt liegenden Ecklagerbeschlag 11 und einer Entlastungsanordnung 12. Die Entlastungsanordnung 12 umfasst ein Rahmenbefestigungsteil 13, an dem ein Stützlenker 14 schwenkbar angeordnet ist. Der Stützlenker 14 ist außerdem schwenkbar mit dem Zugarm 15 verbunden, der wiederum um den Bolzen 16 schwenkbar mit dem Rahmenbefestigungsteil 13 verbunden ist. Der Zugarm 15 führt beim Öffnen und Schließen eines Flügels eine reine Schwenkbewegung in einer Ebene durch. Anders als bekannte Stützstäbe oder Seile macht er keine Drehbewegung. Der Zugarm 15 ist so bemessen, dass er auch bei geschlossenem Flügel einen Teil dessen Last abträgt. Der Bolzen 16 ist in einem Langloch 17 des Rahmenbefestigungsteils 13 höhenverschieblich angeordnet.The Fig. 1 shows a corner bearing assembly 10, with a concealed corner bearing fitting 11 and a discharge assembly 12. The relief assembly 12 includes a frame attachment member 13 to which a support arm 14 is pivotally mounted. The support arm 14 is also pivotally connected to the pull arm 15, which in turn is pivotally connected to the bolt 16 to the frame attachment part 13. The pulling arm 15 performs a pure pivoting movement in a plane when opening and closing a wing. Unlike known support rods or ropes, he makes no rotational movement. The pulling arm 15 is dimensioned so that it removes a part of its load even with the wing closed. The bolt 16 is arranged vertically displaceable in a slot 17 of the frame attachment part 13.

Der Zugarm 15 ist an seinem freien Ende 18 abgewinkelt, wobei das freie Ende 18 gabelförmig ausgebildet ist und eine Verdickung 19 eines Zapfens 20 hintergreift. Auf den Zapfen 20 kann ein Flügel beziehungsweise ein flügelseitiges Beschlagteil aufgesetzt werden. Beim Öffnen und Schließen macht der Zapfen 20 eine Bewegung senkrecht zur Fensterebene annährend entlang einer geraden Linie. Insbesondere macht er keine Pendelbewegung. Durch die Entlastungsanordnung 12 wird die Schere 21 als den Flügel stützendes Beschlagteil vom Flügelgewicht teilweise entlastet. Dadurch ist es möglich, insbesondere den Arm 22 dünner auszubilden, so dass dieser bei geschlossenem Flügel in den Falzluftbereich passt.The pulling arm 15 is angled at its free end 18, wherein the free end 18 is fork-shaped and a thickening 19 of a pin 20 engages behind. On the pin 20, a wing or a wing-side fitting part can be placed. When opening and closing the pin 20 makes a movement perpendicular to the window plane approximately along a straight line. In particular, he does not make a pendulum motion. By the relief assembly 12, the scissors 21 is partially relieved of the sash weight as the wing-supporting fitting part. That's it possible, in particular the arm 22 form thinner, so that it fits with the wing closed in the Falzluftbereich.

Die Führung 24 ist schräg zur Fensterebene ausgerichtet. Sie könnte auch gekrümmt ausgeführt sein.The guide 24 is aligned obliquely to the window plane. It could also be curved.

In der Fig. 1 ist zu erkennen, dass das Rahmenbefestigungsteil 13 von dem Befestigungsschenkel 25 der Ecklageranordnung getrennt ist. Dadurch kann die Entlastungsanordnung 12 nachgerüstet und separat montiert werden.In the Fig. 1 It can be seen that the frame attachment member 13 is separated from the mounting leg 25 of the corner bearing assembly. This allows the relief assembly 12 to be retrofitted and mounted separately.

In der Fig. 2 ist die Entlastungsanordnung 12 in einer Draufsicht gezeigt. Bei geschlossenem Flügel sind das Rahmenbefestigungsteil 13, der Zugarm 15 sowie der Stützlenker 14 in Falzumfangsrichtung ausgerichtet. Auch bei geschlossenem Flügel hintergreift der Zugarm 15 die Verdickung 19 des Bolzens 20. Zu erkennen ist, dass die Verdickung 19 gekrümmt ausgebildet ist. Aus diesem Grund weist das gabelartige freie Ende 18 des Zugarms 15 eine muldenartig Vertiefung 26 auf. Dadurch wird sichergestellt, dass bei unterschiedlichen Schrägstellung des Zugarms 15 stets eine ausreichend große Anlagefläche zwischen dem freien Ende 18 und der Verdickung 19 besteht.In the Fig. 2 the relief arrangement 12 is shown in a plan view. When the sash is closed, the frame attachment part 13, the pull arm 15 and the support link 14 are aligned in the fold circumferential direction. Even with the wing closed, the pulling arm 15 engages behind the thickening 19 of the bolt 20. It can be seen that the thickening 19 is curved. For this reason, the fork-like free end 18 of the tension arm 15 has a trough-like depression 26. This ensures that there is always a sufficiently large contact surface between the free end 18 and the thickening 19 at different inclination of the traction arm 15.

Dieser Sachverhalt lässt sich auch in der Fig. 3 erkennen, wo der Zugarm 15 ausgeschwenkt ist. In diesem Fall greift das gabelartige freie Ende 18 nicht mehr unmittelbar von unten sondern schräg von unten an der Verdickung 19 an. Im Vergleich zur Fig. 2 ist der Zugarm 15 bei seiner Schwenkbewegung etwas nach unten bewegt worden. Dies ist daran zu erkennen, dass der Bolzen 16 im Vergleich zur Fig. 2 nach unten verlagert ist. Der Stützlenker 14, der Zugarm 15 sowie die Positionen der Schwenkpunkte 27,28 am Rahmenbefestigungsteil 13 bzw. am Zugarm 15 und des Bolzens 16 sind so aufeinander abgestimmt, dass in allen Positionen des Bolzens 20 stets eine gleich bleibende Entlastung erfolgt und der Bolzen 20 in vertikaler Richtung nicht verlagert wird. Dies bedeutet, dass der Bolzen 20 und damit die Unterkante des Flügels ausschließlich horizontal bewegt wird.This situation can also be seen in the Fig. 3 recognize where the pulling arm 15 is swung out. In this case, the fork-like free end 18 no longer engages directly from below but obliquely from below on the thickening 19. In comparison to Fig. 2 the pulling arm 15 has been moved slightly downwards during its pivotal movement. This can be seen from the fact that the bolt 16 compared to Fig. 2 is shifted downwards. The support arm 14, the pull arm 15 and the positions of the pivot points 27,28 on the frame mounting part 13 and the tension arm 15 and the bolt 16 are coordinated so that in all positions of the bolt 20 is always a constant relief and the bolt 20 in vertical direction is not relocated. This means that the bolt 20 and thus the lower edge of the wing is moved only horizontally.

Die Fig. 4 zeigt eine Draufsicht auf die Ecklageranordnung 10 ohne den Befestigungsschenkel 25 sowie die daran angeordneten Teile, wobei die gezeigte Stellung einer Geschlossenstellung eines Flügels entspricht. Die Ecklageranordnung ist besonders zur Verwendung als verdeckt liegender Beschlag ausgebildet. In diesem Zusammenhang ist zu beachten, dass ein als Blendrahmen ausgebildeter fester Rahmen über die Ecklageranordnung 10 mit einem Flügel verbunden ist. Der Flügel weist einen Überschlag auf. Um den Flügel öffnen zu können, muss der Flügel daher zunächst vom Rahmen abgestellt werden. Dies wird durch die Ecklageranordnung 10 ermöglicht, nämlich durch den Arm 22 sowie die Lasche 50, die eine Scherengeometrie bilden (siehe auch Fig. 5). Die Scherengeometrie ist so ausgelegt, dass der Flügel so wenig wie möglich abgestellt wird und dennoch eine größtmögliche lichte Weite entsteht. Zum Öffnen des Flügels wird dieser gerade soweit vom Rahmen abgestellt, dass es zu keiner Kollision zischen dem Überschlag und dem Rahmen kommt.The Fig. 4 shows a plan view of the corner bearing assembly 10 without the mounting leg 25 and the parts arranged thereon, wherein the position shown corresponds to a closed position of a wing. The corner bearing assembly is particularly designed for use as a concealed fitting. In this context, it should be noted that a solid frame formed as a frame is connected via the corner bearing assembly 10 with a wing. The wing has a rollover. In order to open the wing, the wing must therefore first be turned off the frame. This is made possible by the corner bearing assembly 10, namely by the arm 22 and the tab 50, which form a scissors geometry (see also Fig. 5 ). The geometry of the scissors is designed so that the wing is turned off as little as possible while still providing the greatest possible clearance. To open the wing of this is just turned off so far from the frame, that there is no collision hiss the flashover and the frame.

Die Scherengeometrie befindet sich über einer Grundplatte 52, mit der eine Befestigung an einer festen Einfassung, insbesondere einem festen Rahmen, erfolgen kann. Insbesondere steht kein Teil seitlich über die Grundplatte 52 hervor. Außerdem ist der Fig. 4 zu entnehmen, dass die Elemente 22, 50 bei geschlossenem Flügel im Falzluftbereich angeordnet werden müssen. Deshalb können die Elemente 22, 50 nur eine begrenzte Dicke aufweisen und insbesondere nicht so groß dimensioniert werden, wie dies für große Flügellasten (wenn keine Entlastungsanordnung 12 verwendet wird) notwendig wäre.The scissor geometry is located above a base plate 52, with which attachment to a fixed enclosure, in particular a fixed frame, can take place. In particular, no part projects laterally beyond the base plate 52. In addition, the Fig. 4 can be seen that the elements 22, 50 must be arranged with the sash closed in Falzluftbereich. Therefore, the elements 22, 50 may have only a limited thickness and, in particular, may not be dimensioned as large as would be necessary for large wing loads (if no relief assembly 12 is used).

Der Zapfen 51 ist in der Führung 24 in eine vordere Stellung verschoben. Durch die schräge Führung 24, die auch gebogen ausgeführt sein kann, ist es möglich, die Ecklageranordnung 10 insgesamt kleiner und stabiler zu bauen. Insbesondere ist es dadurch möglich, eine sehr kleine Scherengeometrie zu realisieren.The pin 51 is moved in the guide 24 in a forward position. By the inclined guide 24, which can also be performed bent, it is possible to build the corner bearing assembly 10 is smaller and more stable overall. In particular, this makes it possible to realize a very small scissors geometry.

Die in der Fig. 5 gezeigte Stellung entspricht einer Offenstellung des Flügels. Zu sehen ist, dass die Stelle, an der der Bolzen 20 angeordnet ist, annährend entlang einer geraden Linie senkrecht zur Fensterebene bewegt wurde. Dies bedeutet, dass der Zugarm 15 praktisch eine reine Schwenkbewegung ausgeführt hat.The in the Fig. 5 shown position corresponds to an open position of the wing. It can be seen that the location where the bolt 20 is located has been moved approximately along a straight line perpendicular to the window plane. This means that the pulling arm 15 has practically performed a pure pivoting movement.

Das Gewicht des Flügels wird über das nicht dargestellte, am Flügel befestigte Eckband auf den Bolzen 20 übertragen. Dieser überträgt das Gewicht dann auf die Lasche 50. Die Lasche 50 liegt auf dem Arm 22 auf und überträgt somit die Last auf den Arm 22. Die Scherengeometrie wurde so gewählt, dass eine möglichst große Überlappung der Lasche 50 und des Arms 22 bei geöffnetem Flügel vorhanden ist. Somit wird ein entstehendes Biegemoment klein gehalten. Der Arm 22 leitet das Flügelgewicht bzw. einen Teil des Flügelgewichts über die Grundplatte 52 in den festen Rahmen ein.The weight of the wing is transmitted via the not shown, attached to the wing corner band on the bolt 20. This then transmits the weight on the tab 50. The tab 50 rests on the arm 22 and thus transmits the load to the arm 22. The scissor geometry was chosen so that the greatest possible overlap of the tab 50 and the arm 22 with the wing open is available. Thus, a resulting bending moment is kept small. The arm 22 introduces the sash weight or a portion of the sash weight over the base plate 52 in the fixed frame.

Der Zapfen 51 wurde während des Öffnens des Flügels in der Führung 24 in eine hintere Stellung verfahren. Die Führung 24 begrenzt die Relativbewegung des Arms 22 und der Lasche 50.The pin 51 was moved during the opening of the wing in the guide 24 in a rear position. The guide 24 limits the relative movement of the arm 22 and the tab 50.

Claims (7)

  1. Concealed corner bearing arrangement (10) having a concealed corner bearing fitting (11) and a concealed load-relieving arrangement (12) for a window, door or the like, for at least partially relieving the concealed corner bearing fitting (11) in respect of the leaf weight of the window, door or the like, the corner bearing fitting (11) comprising a scissors mechanism (21) and the load-relieving arrangement (12) having a tensile arm (15) which is arranged for pivoting at one end at the frame side, characterised in that the load-relieving arrangement (12) has a frame fixing member (13), to which a supporting rod (14) is pivotably secured and is connected for pivoting at the other end to the tensile arm (15) which engages with a fitting member of the corner bearing fitting (11) supporting the leaf, the said end of the tensile arm (15) being arranged so as to be variable in terms of height on the frame fixing member (13), which end is arranged for pivoting at the frame side.
  2. Corner bearing arrangement according to claim 1, characterised in that the frame fixing member (13) has an elongate hole (17), in which there is guided a pin (16) which is arranged on the tensile arm (15) so as to be fixed in position.
  3. Corner bearing arrangement according to either of the preceding claims, characterised in that the tensile arm (15) has, at its leaf-side end (18), a fork-like member which engages under a stud (20) of the corner bearing fitting (11).
  4. Corner bearing arrangement according to claim 3, characterised in that the fork-like member is of trough-like form.
  5. Corner bearing arrangement according to any one of the preceding claims, characterised in that the frame fixing member (13) is in the form of a member which is independent of the corner bearing fitting (11).
  6. Corner bearing arrangement according to any one of preceding claims 1 to 4, characterised in that the frame fixing member (13) is a component of the corner bearing fitting (11).
  7. Window, door or the like, having a fixed frame and a leaf which can pivot relative to the fixed frame at least about a pivot axis, in particular a vertical pivot axis, a concealed corner bearing arrangement according to any one of the preceding claims being provided.
EP07017637A 2007-09-10 2007-09-10 Concealed load-relieving device for a window, door or similar Not-in-force EP2034114B1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE502007007002T DE502007007002D1 (en) 2007-09-10 2007-09-10 Concealed relief arrangement for a window, a door or the like
PL07017637T PL2034114T3 (en) 2007-09-10 2007-09-10 Concealed load-relieving device for a window, door or similar
EP07017637A EP2034114B1 (en) 2007-09-10 2007-09-10 Concealed load-relieving device for a window, door or similar
AT07017637T ATE506515T1 (en) 2007-09-10 2007-09-10 CONCEALED RELIEF ARRANGEMENT FOR A WINDOW, DOOR OR THE LIKE
SI200730633T SI2034114T1 (en) 2007-09-10 2007-09-10 Concealed load-relieving device for a window, door or similar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP07017637A EP2034114B1 (en) 2007-09-10 2007-09-10 Concealed load-relieving device for a window, door or similar

Publications (2)

Publication Number Publication Date
EP2034114A1 EP2034114A1 (en) 2009-03-11
EP2034114B1 true EP2034114B1 (en) 2011-04-20

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ID=39091804

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07017637A Not-in-force EP2034114B1 (en) 2007-09-10 2007-09-10 Concealed load-relieving device for a window, door or similar

Country Status (5)

Country Link
EP (1) EP2034114B1 (en)
AT (1) ATE506515T1 (en)
DE (1) DE502007007002D1 (en)
PL (1) PL2034114T3 (en)
SI (1) SI2034114T1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010028602A1 (en) * 2010-05-05 2011-11-10 Roto Frank Ag Concealed corner fitting with a hold-down

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0436946A1 (en) * 1990-01-09 1991-07-17 August Bilstein GmbH & Co. KG Concealed lower pivot bearing for turning windows, doors or similar, in particular turning and tiltable

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH436024A (en) * 1965-04-23 1967-05-15 Kuentz & Cie Ag window
DE3829053C2 (en) 1988-08-26 1994-02-17 Winkhaus Fa August Turn fittings or turn-tilt fittings for windows, doors or the like
DE3906794A1 (en) 1989-03-03 1990-09-06 Bilstein August Gmbh Co Kg WINDOW WITH A ROTATING, IN PARTICULAR ROTATING WING
DE8907630U1 (en) 1989-06-22 1989-08-03 Gretsch-Unitas Gmbh Baubeschlaege, 7257 Ditzingen, De
DE4439463C1 (en) 1994-11-04 1996-06-05 Bilstein August Gmbh Co Kg Relief element

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0436946A1 (en) * 1990-01-09 1991-07-17 August Bilstein GmbH & Co. KG Concealed lower pivot bearing for turning windows, doors or similar, in particular turning and tiltable

Also Published As

Publication number Publication date
DE502007007002D1 (en) 2011-06-01
SI2034114T1 (en) 2011-08-31
EP2034114A1 (en) 2009-03-11
ATE506515T1 (en) 2011-05-15
PL2034114T3 (en) 2011-09-30

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