EP1788175B1 - Flat links assembly for windows, doors or the like - Google Patents

Flat links assembly for windows, doors or the like Download PDF

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Publication number
EP1788175B1
EP1788175B1 EP05025433A EP05025433A EP1788175B1 EP 1788175 B1 EP1788175 B1 EP 1788175B1 EP 05025433 A EP05025433 A EP 05025433A EP 05025433 A EP05025433 A EP 05025433A EP 1788175 B1 EP1788175 B1 EP 1788175B1
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EP
European Patent Office
Prior art keywords
plate
arrangement according
lubricant discharge
plate arrangement
plates
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.)
Active
Application number
EP05025433A
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German (de)
French (fr)
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EP1788175A1 (en
Inventor
Joachim Beyer
Dirk Hanel
Martin Siegler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Roto Frank AG
Original Assignee
Roto Frank AG
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Application filed by Roto Frank AG filed Critical Roto Frank AG
Priority to EP05025433A priority Critical patent/EP1788175B1/en
Priority to AT05025433T priority patent/ATE461339T1/en
Priority to DE502005009244T priority patent/DE502005009244D1/en
Priority to SI200530977T priority patent/SI1788175T1/en
Priority to PL05025433T priority patent/PL1788175T3/en
Publication of EP1788175A1 publication Critical patent/EP1788175A1/en
Application granted granted Critical
Publication of EP1788175B1 publication Critical patent/EP1788175B1/en
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Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00—Suspension arrangements for wings
    • E05D15/48—Suspension arrangements for wings allowing alternative movements
    • E05D15/52—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
    • E05D15/5211—Concealed suspension fittings
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D11/00—Additional features or accessories of hinges
    • E05D11/02—Lubricating arrangements
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00—Suspension arrangements for wings
    • E05D15/28—Suspension arrangements for wings supported on arms movable in horizontal plane
    • E05D15/30—Suspension arrangements for wings supported on arms movable in horizontal plane with pivoted arms and sliding guides
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING 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
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Type of wing
    • E05Y2900/132—Doors
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING 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
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Type of wing
    • E05Y2900/148—Windows

Definitions

  • the invention relates to a tab arrangement of a window, a door or the like. With the features of the preamble of claim 1.
  • the sash weight must be absorbed by the concealed fitting.
  • the wing must first be opened to open 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 ever possible.
  • the scissors geometry must absorb loads, so that there is increased friction between the scissor plates. This results in a high wear of the shear tabs. An introduced during assembly between the scissor latches lubricant is pressed out.
  • Object of the present invention is to develop a tab assembly to the effect that the wear between heavily loaded tabs is reduced.
  • At least one tab has a lubricant delivery device on the side facing the other tab.
  • the lubricant can be particularly easily brought into the overlap region of the two tabs.
  • the at least one lubricant dispensing device can be used as a lubricant receiving recess be educated. This can be formed directly on the tabs or on a tab. Thus, in a simple way Schmiermetteltedepottaschen can be formed. There are no further, separate parts necessary.
  • the lubricant dispensing devices may in particular be produced by embossing, milling or drilling. More preferably, they whet a depth of about 0.3-0.4 mm.
  • the lubrication can be improved if both tabs have at least one lubricant dispenser. It is particularly advantageous if the arranged on different tabs lubricant delivery devices overlap at least in some positions of the tabs to each other in sections.
  • the lubricant stored in the lubricant delivery devices can be distributed particularly easily in the overlapping region if at least one lubricant dispensing device arranged on the first lug and on the second lug sweeps over during a relative movement of the lugs.
  • the lubricant dispensing devices have an elongated shape, it can be ensured in a particularly simple manner that lubricant dispensing devices arranged on different tabs overlap and / or cover in sections.
  • the lubricant delivery devices are aligned on a tab approximately parallel to its longitudinal axis and are aligned approximately star-shaped on a tab.
  • the tabs are tabs of a scissor geometry, the tabs can be pivotably connected to one another via a pivot bearing.
  • the lubricant delivery devices of at least one tab extend approximately radially from the rotary bearing.
  • this scissors geometry can accommodate loads, such as the weight of a wing, when a tab is designed as a control tab and a tab as a support tab that interacts with a bearing member.
  • control tab on a Eckbandability, in particular a support pin on.
  • Eckband a support pin on.
  • the control tab rests on a tab designed as a tab and thus transmits the load on the support bracket.
  • the scissors geometry is preferably chosen so that there is the greatest possible overlap of the control flap and the support flap. Thus, a resulting bending moment is kept low.
  • a compact construction of a bearing having the scissors geometry is enabled when a downwardly directed load-bearing device is provided.
  • a load-bearing device is advantageous because it does not have to be accommodated in the seaming air area between the frame and the wing.
  • the bearing part is designed as a base plate fastened to a frame, wherein the base plate has at least a portion of the load receiving device.
  • the base plate has a downwardly directed sleeve in which a downwardly directed support pin of the support lug is rotatably arranged.
  • the support tab can initiate the resulting bending moment on the support pin in the sleeve.
  • the support bracket is firmly connected to the support bolt.
  • the sleeve which is fixedly connected to the base plate, serves as an abutment to the occurring bending moment, which is introduced via the support bracket and the support bolt.
  • the sleeve and the support bolt form a hinge.
  • a pivotable connection of the bearing part and the support bracket is realized.
  • the distances between the support bolt, control tab and support pin significantly influence the resulting bending moment. Therefore, these are to be kept as small as possible in order to minimize the bending moment.
  • the forces are transmitted to the base plate via the sleeve. This directs the forces on the screw in a frame.
  • the forces in the base plate are influenced by the length of the sleeve and the support pin. These must therefore be selected accordingly for a sufficient load-bearing device.
  • the scope of the invention also includes a window, door or the like having a fixed frame and / or at least one wing, comprising a tab arrangement as described above.
  • FIG. 1 The lower corner of a window is shown.
  • a fixed frame 1 designed as a frame is connected to a wing 3 via a bearing 2 having a tab arrangement.
  • the wing 3 has a rollover 4. In order to open the wing 3, therefore, the wing must first be turned off the frame 1. This is made possible by the bearing 2.
  • the bearing 2 comprises a base part designed as a bearing part 5, with which a support bracket 6 is pivotally connected.
  • a control tab 7 is pivotally connected to the support bracket 6.
  • the end 8 of the control plate 7 is displaceable along a guide 9 relative to the bearing part 5.
  • the tab arrangement consisting of control tab 7 and support tab 6 forms a scissors geometry.
  • the scissors geometry is designed so that the wing 3 is turned off as little as possible and still creates the largest possible clear width. To open the wing 3, this is just as far from the frame 1, that there is no collision between the flashover 4 and the frame 1.
  • the bearing part 5 is bolted to the frame 1.
  • a corner band 10 is provided, with which the wing 3 sits on the control tab 7.
  • the presentation of the Fig. 2 is essentially the same as the Fig. 1 , Only the wing 3 is no longer shown. This is now one with the control tab 7 connected support pin 15, which forms a Eckbandage visible, on which the corner band 10 can be stored.
  • the support bracket 6 has at its free end also a bolt 16 which engages from below into the wing 3 and a fitting part arranged thereon.
  • the weight of the wing 3 is transmitted via the corner band 10 on the support pin 15. This transfers the weight then on the control tab 7.
  • the control tab 7 rests on the support bracket 6 and thus transfers the load on the support bracket 6.
  • the scissor geometry was chosen so that the greatest possible overlap of the control tab 7 and the support bracket 6 with the wing open 3 is present.
  • the bearing part 5 and the support plate 6 together form a load-receiving device 20.
  • the bearing part 5 has a downwardly extending sleeve 21, in which a support pin 22 which is fixedly connected to one end of the support bracket 6 projects.
  • the support tab 6 initiates the bending moment arising under the weight of the flared wing via the support bolt 22 into the sleeve 21.
  • the sleeve 21 serves as an abutment to the occurring bending moment, which is introduced via the support bracket 6 and the support pin 22.
  • the sleeve 21 and the support pin 22 form a hinge.
  • the forces occurring are transmitted to the bearing part 5 via the sleeve 21. This introduces the forces via the screw in the frame. Due to the fact that the load-receiving device 20 projects downwards, in particular into the frame, the bearing 2 occupies only a small amount of space in the rebate air area.
  • the support pin 22 can be seen better, which is inserted into the sleeve 21. Furthermore, it can be seen in this illustration that the guide 9 is formed bent. About a slider, the control tab 7 and the bearing part 5 in the region of the guide 9 and the passage opening 25 are interconnected.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Securing Of Glass Panes Or The Like (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
  • Extensible Doors And Revolving Doors (AREA)
  • Wing Frames And Configurations (AREA)

Abstract

Flap arrangement has first and second flap (6,7), which rest upon one another and are relatively moveable to each other whereby lubricating device is arranged in the overlapping area. The lubricating device is provided over the flap which faces the other flap. An independent claim is also included for the window or door.

Description

Die Erfindung betrifft eine Laschenanordnung eines Fensters, einer Tür oder dgl. mit den Merkmalen des Oberbegriffs von Anspruch 1.The invention relates to a tab arrangement of a window, a door or the like. With the features of the preamble of claim 1.

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. Insbesondere am unteren Ende des Rahmens muss die Scherengeometrie Lasten aufnehmen, so dass es zu erhöhter Reibung zwischen den Scherenlaschen kommt. Dadurch kommt es zu einem hohen Verschleiß der Scherenlaschen. Ein bei der Montage zwischen den Scherenlaschen eingebrachtes Schmiermittel wird herausgepresst.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 to open 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. On, this narrow installation space a scissors geometry must be provided so that a parking of the wing is ever possible. Especially at the lower end of the frame, the scissors geometry must absorb loads, so that there is increased friction between the scissor plates. This results in a high wear of the shear tabs. An introduced during assembly between the scissor latches lubricant is pressed out.

Aus der WO 88/00638 A2 sind zwei Laschen bekannt, die über ein Verbindungselement miteinander verbunden sind. Die obere Lasche weist eine ringförmige Erhebung auf, mit der sie auf der unteren Lasche aufliegt. Durch die Erhebung, das Verbindungselement und Abschnitte der Laschen wird ein Raum gebildet, In dem Schmiermittel angeordnet ist. Durch die ringförmige Ausgestaltung der Erhebung ergibt sich eine linienförmige Auflage.From the WO 88/00638 A2 are two tabs are known, which are interconnected via a connecting element. The upper flap has an annular elevation, with which it rests on the lower flap. By the survey, the connecting element and portions of the tabs a space is formed, In the lubricant is arranged. The annular configuration of the survey results in a linear support.

Aus der EP 0 204 267 A2 ist eine Ausstellvorrichtung für die Flügel von Fenstern, Türen oder dergleichen bekannt. Eine Lastaufnahmeeinrichtung ist nach unten gerichtet.From the EP 0 204 267 A2 An opening device for the wings of windows, doors or the like is known. A load-bearing device is directed downwards.

Aus der US 1,918,513 ist ein Scharnier für Autotüren bekannt. Im Bereich eines Gelenkbolzens ist ein Schmlermitteldepot vorgesehen. Die US 1918513 offenbart alle Merkmale des Oberbegriffs des Anspruchs 1.From the US 1,918,513 is a hinge for car doors known. In the area of a hinge pin a Schmlermitteldepot is provided. The US 1918513 discloses all features of the preamble of claim 1.

Aufgabe der vorliegenden Erfindung ist es, eine Laschenanordnung dahingehend weiterzubilden, dass der Verschleiß zwischen stark belasteten Laschen reduziert wird.Object of the present invention is to develop a tab assembly to the effect that the wear between heavily loaded tabs is reduced.

Diese Aufgabe wird erfindungsgemäß mit einer Laschenanordnung mit den Merkmalen des Anspruchs 1 gelöst. Durch diese Maßnahme wird eine kontinuierliche Schmierung realisiert. Der Verschleiß zwischen zwei sich überlappenden Laschen, insbesondere bei Last abtragenden Scherenkonstruktionen kann erheblich reduziert werden. Dabei kann vorgesehen sein, dass die Schmiermittelabgabeeinrichtung nachfüllbar ist. Bevorzugt ist sie jedoch so dimensioniert, dass selbst bei etwa 30.000 Öffnungs- und Schließzyklen eines Fensters ein Nachfetten nicht erforderlich ist.This object is achieved with a tab assembly with the features of claim 1. By this measure, a continuous lubrication is realized. The wear between two overlapping tabs, especially in load-removing scissors constructions can be significantly reduced. It can be provided that the lubricant dispensing device is refillable. Preferably, however, it is dimensioned so that even with about 30,000 opening and closing cycles of a window re-greasing is not required.

Besonders bevorzugt ist es, wenn zumindest eine Lasche auf der der anderen Lasche zugewandten Seite eine Schmiermittelabgabeeinrichtung aufweist. Durch diese Maßnahme kann das Schmiermittel besonders einfach In den Überlappungsbereich der beiden Laschen gebracht werden.It is particularly preferred if at least one tab has a lubricant delivery device on the side facing the other tab. By this measure, the lubricant can be particularly easily brought into the overlap region of the two tabs.

Bei einer vorteilhaften Ausführungsform kann die wenigstens eine Schmiermittelabgabeeinrichtung als Schmiermittelaufnahmeausnehmung ausgebildet sein. Diese kann unmittelbar an den Laschen beziehungsweise an einer Lasche ausgebildet werden. Somit können auf einfache Art und Weise Schmiermltteldepottaschen gebildet werden. Es sind keine weiteren, separaten Teile notwendig.In an advantageous embodiment, the at least one lubricant dispensing device can be used as a lubricant receiving recess be educated. This can be formed directly on the tabs or on a tab. Thus, in a simple way Schmiermetteltedepottaschen can be formed. There are no further, separate parts necessary.

Die Schmiermittelabgabeeinrichtungen können insbesondere durch Prägen, Fräsen oder Bohren hergestellt sein. Besonders bevorzugt welsen sie eine Tiefe von etwa 0,3 - 0,4 mm auf.The lubricant dispensing devices may in particular be produced by embossing, milling or drilling. More preferably, they whet a depth of about 0.3-0.4 mm.

Die Schmierung kann verbessert werden, wenn beide Laschen zumindest eine Schmiermittelabgabeeinrichtung aufweisen. Dabei ist es besonders vorteilhaft, wenn die an unterschiedlichen Laschen angeordneten Schmiermittelabgabeeinrichtungen sich zumindest in einigen Stellungen der Laschen zueinander abschnittsweise überlappen.The lubrication can be improved if both tabs have at least one lubricant dispenser. It is particularly advantageous if the arranged on different tabs lubricant delivery devices overlap at least in some positions of the tabs to each other in sections.

Das in den Schmiermittelabgabeeinrichtungen gelagerte Schmiermittel kann besonders einfach im Überlappungsbereich verteilt werden, wenn zumindest eine an der ersten Lasche und eine an der zweiten Lasche angeordnete Schmiermittelabgabeeinrichtung sich bei einer Relativbewegung der Laschen überstreichen.The lubricant stored in the lubricant delivery devices can be distributed particularly easily in the overlapping region if at least one lubricant dispensing device arranged on the first lug and on the second lug sweeps over during a relative movement of the lugs.

Wenn die Schmiermittelabgabeeinrichtungen eine längliche Form aufweisen, kann besonders einfach sichergestellt werden, dass sich an unterschiedlichen Laschen angeordnete Schmiermittelabgabeeinrichtungen abschnittsweise überlappen und/oder überstreichen.If the lubricant dispensing devices have an elongated shape, it can be ensured in a particularly simple manner that lubricant dispensing devices arranged on different tabs overlap and / or cover in sections.

Um dies zu erreichen ist es weiterhin bevorzugt, wenn die Schmiermittelabgabeeinrichtungen an einer Lasche etwa parallel zu deren Längsachse ausgerichtet sind und an einer Lasche etwa sternförmig ausgerichtet sind.In order to achieve this, it is further preferred if the lubricant delivery devices are aligned on a tab approximately parallel to its longitudinal axis and are aligned approximately star-shaped on a tab.

Insbesondere, wenn es sich bei den Laschen um Laschen einer Scherengeometrie handelt, können die Laschen über ein Drehlager schwenkbar miteinander verbunden sein. Um eine gute Schmierung im Bereich des Drehlagers sicherzustellen, ist es auch vorteilhaft, wenn sich die Schmiermittelabgabeeinrichtungen zumindest einer Lasche in etwa radial von dem Drehlager erstrecken.In particular, if the tabs are tabs of a scissor geometry, the tabs can be pivotably connected to one another via a pivot bearing. In order to ensure good lubrication in the region of the rotary bearing, it is also advantageous if the lubricant delivery devices of at least one tab extend approximately radially from the rotary bearing.

Wenn die Laschen eine Scherengeometrie bilden, kann diese Scherengeometrie Lasten, beispielsweise das Gewicht eines Flügels, aufnehmen, wenn eine Lasche als Steuerlasche und eine Lasche als Traglasche ausgebildet sind, die mit einem Lagerteil zusammenwirken.If the tabs form a scissors geometry, this scissors geometry can accommodate loads, such as the weight of a wing, when a tab is designed as a control tab and a tab as a support tab that interacts with a bearing member.

Vorzugsweise weist die Steuerlasche eine Eckbandaufnahme, insbesondere einen Tragbolzen, auf. Dadurch kann das Gewicht des Flügels auf die Steuerlasche übertragen werden. Die Steuerlasche liegt wiederum auf einer als Traglasche ausgebildeten Lasche auf und überträgt somit die Last auf die Traglasche. Die Scherengeometrie ist vorzugsweise so gewählt, dass eine möglichst große Überlappung der Steuerlasche und der Traglasche besteht. Somit wird ein entstehendes Biegemoment gering gehalten.Preferably, the control tab on a Eckbandaufnahme, in particular a support pin on. This allows the weight of the wing to be transferred to the control tab. The control tab in turn rests on a tab designed as a tab and thus transmits the load on the support bracket. The scissors geometry is preferably chosen so that there is the greatest possible overlap of the control flap and the support flap. Thus, a resulting bending moment is kept low.

Eine kompakte Bauweise eines Lagers, das die Scherengeometrie aufweist, wird ermöglicht, wenn eine nach unten gerichtete Lastaufnahmeeinrichtung vorgesehen ist. Eine solche Lastaufnahmeeinrichtung ist deshalb vorteilhaft, da diese nicht auch noch im Falzluftbereich zwischen Rahmen und Flügel untergebracht werden muss.A compact construction of a bearing having the scissors geometry is enabled when a downwardly directed load-bearing device is provided. Such a load-bearing device is advantageous because it does not have to be accommodated in the seaming air area between the frame and the wing.

Bei einer besonders bevorzugten Ausführungsform kann vorgesehen sein, dass das Lagerteil als an einem Rahmen befestigbare Grundplatte ausgebildet ist, wobei die Grundplatte zumindest einen Teil der Lastaufnahmeeinrichtung aufweist. Vorzugsweise weist die Grundplatte eine nach unten gerichtete Hülse auf, in der ein nach unten gerichteter Stützbolzen der Traglasche drehbar angeordnet ist. Durch diese Anordnung kann die Traglasche das entstehend Biegemoment über den Stützbolzen in die Hülse einleiten. Die Traglasche ist fest mit dem Stützbolzen verbunden. Die Hülse, welche fest mit der Grundplatte verbunden ist, dient als Gegenlager zu dem auftretenden Biegemoment, welches über die Traglasche und den Stützbolzen eingeleitet wird. Die Hülse und der Stützbolzen bilden ein Drehgelenk. Dadurch wird eine schwenkbare Verbindung des Lagerteils und der Traglasche realisiert. Die Abstände zwischen Tragbolzen, Steuerlasche und Stützbolzen beeinflussen maßgeblich das entstehende Biegemoment. Daher sind diese möglichst klein zu halten, um das Biegemoment möglichst gering zu halten.In a particularly preferred embodiment it can be provided that the bearing part is designed as a base plate fastened to a frame, wherein the base plate has at least a portion of the load receiving device. Preferably, the base plate has a downwardly directed sleeve in which a downwardly directed support pin of the support lug is rotatably arranged. By this arrangement, the support tab can initiate the resulting bending moment on the support pin in the sleeve. The support bracket is firmly connected to the support bolt. The sleeve, which is fixedly connected to the base plate, serves as an abutment to the occurring bending moment, which is introduced via the support bracket and the support bolt. The sleeve and the support bolt form a hinge. As a result, a pivotable connection of the bearing part and the support bracket is realized. The distances between the support bolt, control tab and support pin significantly influence the resulting bending moment. Therefore, these are to be kept as small as possible in order to minimize the bending moment.

Die auftretenden Kräfte werden über die Hülse auf die Grundplatte übertragen. Diese leitet die Kräfte über die Verschraubungen in einen Blendrahmen. Die Kräfte in der Grundplatte werden durch die Länge der Hülse und des Stützbolzens beeinflusst. Diese sind daher für eine ausreichende Lastaufnahmeeinrichtung entsprechend zu wählen.The forces are transmitted to the base plate via the sleeve. This directs the forces on the screw in a frame. The forces in the base plate are influenced by the length of the sleeve and the support pin. These must therefore be selected accordingly for a sufficient load-bearing device.

In den Rahmen der Erfindung fällt außerdem ein Fenster, eine Tür oder dergleichen, mit einem festen Rahmen und/oder wenigstens einem Flügel, umfassend eine oben beschriebene Laschenanordnung.The scope of the invention also includes a window, door or the like having a fixed frame and / or at least one wing, comprising a tab arrangement as described above.

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.Further features and advantages of the invention will become apparent from the following description of exemplary embodiments of the invention, with reference to the figures of the drawing, the invention essential details show, and from the claims.

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
in perspektivischer Darstellung einen unteren Eckbereich eines Rahmens und eines Flügels, die über ein Lager mit einer Laschenanordnung in Verbindung stehen;
Fig. 2
die Darstellung der Fig. 1 ohne Flügel;
Fig. 3
eine erfindungsgemäße Laschenanordnung in perspektivischer Darstellung;
Fig. 4
eine teilweise Explosionsdarstellung eines Lagers;
Fig. 5
eine Darstellung zur Erläuterung der Schmierung der Laschenanordnung.
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 lower corner portion of a frame and a wing, which communicate via a bearing with a tab assembly;
Fig. 2
the representation of Fig. 1 without wings;
Fig. 3
a tab assembly according to the invention in a perspective view;
Fig. 4
a partial exploded view of a bearing;
Fig. 5
a representation for explaining the lubrication of the tab assembly.

In der Fig. 1 ist der untere Eckbereich eines Fensters gezeigt. Ein als Blendrahmen ausgebildeter fester Rahmen 1 ist über ein eine Laschenanordnung aufweisende Lager 2 mit einem Flügel 3 verbunden. Der Flügel 3 weist einen Überschlag 4 auf. Um den Flügel 3 öffnen zu können, muss der Flügel daher zunächst vom Rahmen 1 abgestellt werden. Dies wird durch das Lager 2 ermöglicht.In the Fig. 1 The lower corner of a window is shown. A fixed frame 1 designed as a frame is connected to a wing 3 via a bearing 2 having a tab arrangement. The wing 3 has a rollover 4. In order to open the wing 3, therefore, the wing must first be turned off the frame 1. This is made possible by the bearing 2.

Das Lager 2 umfasst ein als Grundplatte ausgebildetes Lagerteil 5, mit welchem eine Traglasche 6 schwenkbar verbunden ist. Eine Steuerlasche 7 ist schwenkbar mit der Traglasche 6 verbunden. Das Ende 8 der Steuerlasche 7 ist entlang einer Führung 9 relativ zum Lagerteil 5 verschiebbar. Die Laschenanordnung bestehend aus Steuerlasche 7 und Traglasche 6 bildet eine Scherengeometrie. Im Ausführungsbeispiel ist die Scherengeometrie so ausgelegt, dass der Flügel 3 so wenig wie möglich abgestellt wird und dennoch eine größtmögliche lichte Weite entsteht. Zum Öffnen des Flügels 3 wird dieser gerade soweit vom Rahmen 1 abgestellt, dass es zu keiner Kollision zischen dem Überschlag 4 und dem Rahmen 1 kommt.The bearing 2 comprises a base part designed as a bearing part 5, with which a support bracket 6 is pivotally connected. A control tab 7 is pivotally connected to the support bracket 6. The end 8 of the control plate 7 is displaceable along a guide 9 relative to the bearing part 5. The tab arrangement consisting of control tab 7 and support tab 6 forms a scissors geometry. In the exemplary embodiment, the scissors geometry is designed so that the wing 3 is turned off as little as possible and still creates the largest possible clear width. To open the wing 3, this is just as far from the frame 1, that there is no collision between the flashover 4 and the frame 1.

Das Lagerteil 5 ist mit dem Rahmen 1 verschraubt. An dem Flügel 3 ist ein Eckband 10 vorgesehen, mit dem der Flügel 3 auf der Steuerlasche 7 sitzt.The bearing part 5 is bolted to the frame 1. On the wing 3, a corner band 10 is provided, with which the wing 3 sits on the control tab 7.

Die Darstellung der Fig. 2 entspricht im Wesentlichen der der Fig. 1. Lediglich der Flügel 3 ist nicht mehr gezeigt. Dadurch ist jetzt ein mit der Steuerlasche 7 verbundener Tragbolzen 15, der eine Eckbandaufnahme ausbildet, sichtbar, auf dem das Eckband 10 gelagert werden kann. Die Traglasche 6 weist an ihrem freien Ende ebenfalls einen Bolzen 16 auf, der von unten in den Flügel 3 beziehungsweise ein daran angeordnetes Beschlagteil eingreift. Das Gewicht des Flügels 3 wird über das Eckband 10 auf den Tragbolzen 15 übertragen. Dieser überträgt das Gewicht dann auf die Steuerlasche 7. Die Steuerlasche 7 liegt auf der Traglasche 6 auf und überträgt somit die Last auf die Traglasche 6. Die Scherengeometrie wurde so gewählt, dass eine möglichst große Überlappung der Steuerlasche 7 und der Traglasche 6 bei geöffnetem Flügel 3 vorhanden ist. Somit wird ein entstehendes Biegemoment klein gehalten. Durch das Gewicht des Flügels 3 werden die Steuerlasche 7 und die Traglasche 6 aufeinander gepresst. Beim Öffnen und Schließen des Flügels 3 werden diese zusätzlich noch relativ zueinander bewegt. Dadurch reiben ihre sich berührenden Flächen aneinander.The presentation of the Fig. 2 is essentially the same as the Fig. 1 , Only the wing 3 is no longer shown. This is now one with the control tab 7 connected support pin 15, which forms a Eckbandaufnahme visible, on which the corner band 10 can be stored. The support bracket 6 has at its free end also a bolt 16 which engages from below into the wing 3 and a fitting part arranged thereon. The weight of the wing 3 is transmitted via the corner band 10 on the support pin 15. This transfers the weight then on the control tab 7. The control tab 7 rests on the support bracket 6 and thus transfers the load on the support bracket 6. The scissor geometry was chosen so that the greatest possible overlap of the control tab 7 and the support bracket 6 with the wing open 3 is present. Thus, a resulting bending moment is kept small. Due to the weight of the wing 3, the control tab 7 and the support bracket 6 are pressed against each other. When opening and closing the wing 3, these are additionally moved relative to each other. As a result, their touching surfaces rub against each other.

Aus der Darstellung der Fig. 3 ist erkennbar, dass das Lagerteil 5 und die Traglasche 6 zusammen eine Lastaufnahmeeinrichtung 20 ausbilden. Hierzu weist das Lagerteil 5 eine sich nach unten erstreckende Hülse 21 auf, in die ein Stützbolzen 22, der fest mit einem Ende der Traglasche 6 verbunden ist, hineinragt. Dabei leitet die Traglasche 6 das unter dem Gewicht des ausgestellten Flügels entstehende Biegemoment über den Stützbolzen 22 in die Hülse 21 ein. Die Hülse 21 dient als Gegenlager zu dem auftretenden Biegemoment, welches über die Traglasche 6 und den Stützbolzen 22 eingeleitet wird. Die Hülse 21 und der Stützbolzen 22 bilden ein Drehgelenk. Die auftretenden Kräfte werden über die Hülse 21 auf das Lagerteil 5 übertragen. Dieses leitet die Kräfte über die Verschraubung in den Rahmen ein. Dadurch, dass die Lastaufnahmeeinrichtung 20 nach unten, insbesondere in den Rahmen ragt, nimmt das Lager 2 nur wenig Raum im Falzluftbereich ein.From the representation of Fig. 3 it can be seen that the bearing part 5 and the support plate 6 together form a load-receiving device 20. For this purpose, the bearing part 5 has a downwardly extending sleeve 21, in which a support pin 22 which is fixedly connected to one end of the support bracket 6 projects. In this case, the support tab 6 initiates the bending moment arising under the weight of the flared wing via the support bolt 22 into the sleeve 21. The sleeve 21 serves as an abutment to the occurring bending moment, which is introduced via the support bracket 6 and the support pin 22. The sleeve 21 and the support pin 22 form a hinge. The forces occurring are transmitted to the bearing part 5 via the sleeve 21. This introduces the forces via the screw in the frame. Due to the fact that the load-receiving device 20 projects downwards, in particular into the frame, the bearing 2 occupies only a small amount of space in the rebate air area.

In der teilweisen Explosionsdarstellung der Fig. 4 ist der Stützbolzen 22 besser zu erkennen, der in die Hülse 21 einsteckbar ist. Weiterhin ist in dieser Darstellung zu erkennen, dass die Führung 9 gebogen ausgebildet ist. Über ein Gleitstück werden die Steuerlasche 7 und das Lagerteil 5 im Bereich der Führung 9 und der Durchgangsöffnung 25 miteinander verbunden.In the partial exploded view of Fig. 4 the support pin 22 can be seen better, which is inserted into the sleeve 21. Furthermore, it can be seen in this illustration that the guide 9 is formed bent. About a slider, the control tab 7 and the bearing part 5 in the region of the guide 9 and the passage opening 25 are interconnected.

In der Darstellung der Figur 5 ist die Steuerlasche 7 von der Traglasche 6 abgenommen, so dass in einem Überlappungsbereich der beiden Laschen 6, 7 die Oberseite der Traglasche 6 und die Unterseite der Steuerlasche 7 sichtbar sind. Im Überlappungsbereich, auf der der jeweils anderen Lasche 6, 7 zugewandten Seite, weisen die Laschen 6, 7 als Schmiermittelabgabeeinrichtungen Schmiermittelaufnahmeausnehmungen 30 - 35 auf, die eine größere Länge als Breite haben. Die Schmiermittelaufnahmeausnehmungen 33 - 35 sind im Wesentlichen parallel zu einer Längsachse der Traglasche 6 ausgerichtet. Die Schmiermittelaufnahmeausnehmungen 30 - 32 sind im Wesentlichen sternförmig angeordnet und erstrecken sich daher im Wesentlichen radial von einem Drehgelenk 36, über das die Steuerlasche 7 schwenkbar mit der Traglasche 6 verbunden werden kann. Durch die Anordnung der Schmiermittelaufnahmeausnehmungen 30 - 35 wird sichergestellt, dass sich die Schmiermittelaufnahmeausnehmungen 30 - 32 und die Schmiermittelaufnahmeausnehmungen 33 - 35 zumindest abschnittsweise überlappen und während einer Relativbewegung der Laschen 6, 7 sich gegenseitig überstreichen.In the presentation of the FIG. 5 the control tab 7 is removed from the support tab 6, so that in an overlap region of the two tabs 6, 7, the top of the support tab 6 and the underside of the control tab 7 are visible. In the overlapping area, on the side facing the other tab 6, 7, the tabs 6, 7 as lubricant dispensing means on Schmiermittelaufnahmeausnehmungen 30 - 35, which have a greater length than width. The Schmiermittelaufnahmeausnehmungen 33 - 35 are aligned substantially parallel to a longitudinal axis of the support bracket 6. The lubricant receiving recesses 30 - 32 are arranged substantially in a star shape and therefore extend substantially radially from a pivot joint 36, via which the control flap 7 can be pivotally connected to the support lug 6. The arrangement of the Schmiermittelaufnahmeausnehmungen 30 - 35 ensures that the Schmiermittelaufnahmeausnehmungen 30 - 32 and the Schmiermittelaufnahmeausnehmungen 33 - 35 overlap at least partially and during a relative movement of the tabs 6, 7 paint each other.

Claims (15)

  1. Plate arrangement of a window, door or the like, comprising at least a first and a second plate (6, 7) which are positioned in a planar manner one on the other at least in portions and which are movable relative to each other, both plates (6, 7) having at least one lubricant discharge device at least in the overlapping region, characterised in that the lubricant discharge devices are constructed as lubricant receiving recesses (30-35).
  2. Plate arrangement according to claim 1, characterised in that at least one plate (6, 7) has a lubricant discharge device at the side facing the other plate (6, 7).
  3. Plate arrangement according to either claim 1 or claim 2, characterised in that the lubricant discharge devices are produced by stamping, milling or drilling.
  4. Plate arrangement according to any one of the preceding claims, characterised in that the lubricant discharge devices arranged on different plates (6, 7) overlap each other in portions at least in some positions of the plates (6, 7) relative to each other.
  5. Plate arrangement according to any one of the preceding claims, characterised in that at least a lubricant discharge device arranged on the first plate (6, 7) and a lubricant discharge device arranged on the second plate (6, 7) pass one over the other when the plates (6, 7) move relative to each other.
  6. Plate arrangement according to any one of the preceding claims, characterised in that the lubricant discharge devices have an elongate shape.
  7. Plate arrangement according to any one of the preceding claims, characterised in that the lubricant discharge devices on one plate (6, 7) are orientated substantially parallel with the longitudinal axis thereof and on one plate (6, 7) are orientated in a substantially star-like manner.
  8. Plate arrangement according to any one of the preceding claims, characterised in that the plates (6, 7) are connected to each other so as to pivot by means of a rotary bearing (36), the lubricant discharge devices of at least one plate (6, 7) extending substantially radially from the rotary bearing (36).
  9. Plate arrangement according to any one of the preceding claims, characterised in that the plates (6, 7) form a scissor-like geometry of a bearing (2).
  10. Plate arrangement according to any one of the preceding claims, characterised in that one plate is in the form of a control plate (7) and one plate is in the form of a carrier plate (6), which plates co-operate with a bearing member (5).
  11. Plate arrangement according to any one of the preceding claims, characterised in that the control plate (7) has a corner strip receiving member, in particular a carrier pin (15).
  12. Plate arrangement according to any one of the preceding claims, characterised in that a downwardly directed load receiving device (20) is provided.
  13. Plate arrangement according to any one of the preceding claims, characterised in that the bearing member (5) is in the form of a base plate which can be secured to a frame (1), the base plate having at least a portion of the load receiving device (20).
  14. Plate arrangement according to any one of the preceding claims, characterised in that the base plate has a downwardly directed sleeve (21), in which a downwardly directed support pin (22) of the carrier plate is rotatably arranged.
  15. Window, door or the like, having a fixed frame (1) and/or at least one leaf (3), comprising a plate arrangement according to any one of the preceding claims.
EP05025433A 2005-11-22 2005-11-22 Flat links assembly for windows, doors or the like Active EP1788175B1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
EP05025433A EP1788175B1 (en) 2005-11-22 2005-11-22 Flat links assembly for windows, doors or the like
AT05025433T ATE461339T1 (en) 2005-11-22 2005-11-22 TAB ARRANGEMENT FOR WINDOWS, DOORS OR THE LIKE
DE502005009244T DE502005009244D1 (en) 2005-11-22 2005-11-22 Tab arrangement for windows, doors or the like
SI200530977T SI1788175T1 (en) 2005-11-22 2005-11-22 Flat links assembly for windows, doors or the like
PL05025433T PL1788175T3 (en) 2005-11-22 2005-11-22 Flat links assembly for windows, doors or the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP05025433A EP1788175B1 (en) 2005-11-22 2005-11-22 Flat links assembly for windows, doors or the like

Publications (2)

Publication Number Publication Date
EP1788175A1 EP1788175A1 (en) 2007-05-23
EP1788175B1 true EP1788175B1 (en) 2010-03-17

Family

ID=36062470

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05025433A Active EP1788175B1 (en) 2005-11-22 2005-11-22 Flat links assembly for windows, doors or the like

Country Status (5)

Country Link
EP (1) EP1788175B1 (en)
AT (1) ATE461339T1 (en)
DE (1) DE502005009244D1 (en)
PL (1) PL1788175T3 (en)
SI (1) SI1788175T1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010063680A1 (en) 2010-12-21 2012-06-21 Aug. Winkhaus Gmbh & Co. Kg For concealed arrangement provided corner bearing

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007054479B4 (en) 2007-11-13 2017-11-02 Roto Frank Ag support means
DE102008010906A1 (en) 2008-02-23 2009-09-17 Roto Frank Ag Fitting part arrangement for use in window or door for solid frame for receiving window sash, door wing or swiveling part, has insertion aid for fitting or attaching window sash at frame, where swiveling part is connected to frame
DE202011051971U1 (en) 2011-11-15 2012-11-26 Aumüller Aumatic GmbH ventilation flap
DE102012209493A1 (en) * 2012-06-05 2013-12-05 Roto Frank Ag Multi-layer scissor arm

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1918513A (en) * 1931-06-26 1933-07-18 James T Atwood Hinge
DE8516560U1 (en) * 1985-06-07 1985-07-18 Siegenia-Frank Kg, 5900 Siegen Opening device for the sash of windows, doors or the like.
GB8617043D0 (en) * 1986-07-12 1986-08-20 Wood T J Hinge

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010063680A1 (en) 2010-12-21 2012-06-21 Aug. Winkhaus Gmbh & Co. Kg For concealed arrangement provided corner bearing
EP2468995A2 (en) 2010-12-21 2012-06-27 Aug. Winkhaus GmbH & Co. KG Corner bearing for concealed assembly
EP2468995A3 (en) * 2010-12-21 2014-11-19 Aug. Winkhaus GmbH & Co. KG Corner bearing for concealed assembly

Also Published As

Publication number Publication date
EP1788175A1 (en) 2007-05-23
DE502005009244D1 (en) 2010-04-29
SI1788175T1 (en) 2010-06-30
PL1788175T3 (en) 2010-08-31
ATE461339T1 (en) 2010-04-15

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