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EP2706182A2 - Load transfert device for a wing pivoting against a frame - Google Patents

Load transfert device for a wing pivoting against a frame Download PDF

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Publication number
EP2706182A2
EP2706182A2 EP13182640.6A EP13182640A EP2706182A2 EP 2706182 A2 EP2706182 A2 EP 2706182A2 EP 13182640 A EP13182640 A EP 13182640A EP 2706182 A2 EP2706182 A2 EP 2706182A2
Authority
EP
European Patent Office
Prior art keywords
wing
bearing
frame
bearing part
load transfer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP13182640.6A
Other languages
German (de)
French (fr)
Other versions
EP2706182B1 (en
EP2706182A3 (en
Inventor
Clemens Paschert
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.)
Aug Winkhaus GmbH and Co KG
Original Assignee
Aug Winkhaus GmbH and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Aug Winkhaus GmbH and Co KG filed Critical Aug Winkhaus GmbH and Co KG
Priority to PL13182640T priority Critical patent/PL2706182T3/en
Publication of EP2706182A2 publication Critical patent/EP2706182A2/en
Publication of EP2706182A3 publication Critical patent/EP2706182A3/en
Application granted granted Critical
Publication of EP2706182B1 publication Critical patent/EP2706182B1/en
Active 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
    • E05D15/48Suspension 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
    • E05D15/5214Corner supports
    • 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
    • E05Y2800/00Details, accessories and auxiliary operations not otherwise provided for
    • E05Y2800/69Permanence of use
    • E05Y2800/694Permanence of use during manufacturing
    • 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
    • E05Y2800/00Details, accessories and auxiliary operations not otherwise provided for
    • E05Y2800/69Permanence of use
    • E05Y2800/696Permanence of use during transport or storage

Definitions

  • the invention relates to a load transfer device for a pivotable against a frame wing of a window, a French window or the like with a frame-side fitting part and a wing-side fitting part and with a hinged on both fitting parts support means, wherein one of the fittings a base and one with the base in the closed position of Wing has connectable bearing part and the support means is hinged to the bearing part.
  • Such a load transfer device is for example from the EP 0 360 024 B1 known.
  • the support device is rod-shaped and arranged above a corner bearing on vertical bars of the frame and the wing and supports the wing when pivoting in a rotational opening position.
  • high weights of the wing are supported and kept loads of the corner bearing particularly low.
  • the assembly of the support means can be done only after the installation of the wing in the frame. Therefore, after the assembly of the wing in the frame, initially a pivot opening of the wing without the support means is required.
  • the invention is based on the problem of further forming a load transfer device of the type mentioned above so that the sash weight is supported on the frame immediately after the mounting of the sash.
  • the support means can be mounted in the pre-assembly with the bearing part first on the frame or the wing.
  • the bearing part is held at this pre-assembly to the holding part. If you move the wing in the initial assembly in the closed position, the bearing part is connected to both the holding part and with the base. In the first movement of the wing in the rotational opening position, the weakest connection, ie the connection of the bearing part is destroyed with the holding part. The connection of the bearing part with the base remains and allows the support of the weight of the wing during the first movement in the rotational opening position.
  • the proposed strength of the connection of the bearing part with the holding part can be easily limited according to an advantageous embodiment of the invention, when the connection of the bearing part with the holding part has a destructible with little force breaking point.
  • the bearing part can be according to another advantageous embodiment of the invention particularly easy to connect during assembly with the base, when the base and the bearing part are connected to one another via a latching connection.
  • the base has a recess open on one side for a journal of the bearing part.
  • the pin is mushroom-shaped with a peripheral edge at its free end. This peripheral edge can be engaged behind by a corresponding edge of the recess.
  • the latching connection of the base part with the bearing part designed according to another advantageous embodiment of the invention structurally particularly simple when the locking connection has a recess arranged in the recess open on one side retaining lug for engaging behind the pin of the bearing part.
  • the support device supports the wing over the bearing part and the base part.
  • the number of components necessary for the support can be kept particularly low if the bearing part has bores for screwing to the wing or the frame.
  • the bearing part can be screwed directly to the wing or the frame after the first rotation opening. A support of the weight of the wing over the base is then avoided.
  • the basic part remains after screwing the bearing part with the wing or the frame without function.
  • the support means designed according to another advantageous embodiment of the invention structurally particularly simple when the support means has a pull rod and when the fitting parts have bearing cups for the movable support of the ends of the pull rod.
  • a reliable load transfer with the load transfer device can be achieved according to another advantageous embodiment of the invention easily when the support means has an adjusting device for adjusting the distance between the bearing cups.
  • FIG. 1 shows a portion of a window with a pivotable against a frame 1 wing 2 in a rotational opening position.
  • the weight of the wing 2 is supported by a load transfer device 3.
  • the load transfer device 3 has a frame-side fitting part 4 and a wing-side fitting part 5.
  • a support means 6 is arranged with a pull rod 7.
  • the fitting parts 4, 5 have to support the pull rod 7 respectively bearing cups 8, 9.
  • the position of one of the bearing cups 8 is adjustable via an adjusting device 10.
  • FIG. 2 shows the load transfer device 3 from FIG. 1 with a designed as a lower corner bearing 11 fitting part during assembly.
  • the arranged on the wing 2 fitting 5 has a support body 12.
  • the arranged on the frame 1 fitting part 4 has a bearing part 13 to which the pull rod 7 is articulated and a base member 14 which is bolted to the frame 1.
  • the bearing part 13 is also connected to a holding part 15 attached to the wing 2.
  • FIG. 2 the frame 1 and the wing 2 shown only schematically.
  • screws 16 for connecting the wing-side fitting part 5 with the wing 2 screws 17 for connecting the holding part 15 with the wing 2 and screws 18 for connecting the base part 14 of the frame-side fitting part 4 with the frame 1 in FIG. 2 shown.
  • FIG. 3 shows in an enlarged sectional view, the connection of the bearing part 13 with the base part 14 and the holding part 15.
  • the holding part 15 has two retaining pin 19 with constrictions 20 as a predetermined breaking point.
  • the bearing part 13 has holes 21 and is attached during pre-assembly on the retaining pin 19 of the holding part 15.
  • the bearing part 13 has bores 26, via which it can be screwed permanently to the frame 1 after the first movement of the wing 2 into the rotary opening position.
  • FIG. 4 shows in a sectional view of the connection of the bearing part 13 with the base part 14 along the line IV - IV FIG. 3 ,
  • the connection of the base part 14 with the bearing part 13 has a latching connection 27 with a pin 22 engaging behind and arranged in the recess 23 of the base 14 retaining lug 28th

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Closing And Opening Devices For Wings, And Checks For Wings (AREA)
  • Door And Window Frames Mounted To Openings (AREA)

Abstract

The load transfer device (3) has a frame-side fitting portion (4) and a wing-side fitting portion (5) with which a supporting device (6) is coupled. The frame-side fitting portion or wing-side fitting portion includes a base. A bearing portion is connected with the base in closing position of a wing (2) and is coupled at the supporting device. The bearing portion is coupled with a holding element in a pre-assembly such that the connection strength between the bearing portion and holding element is lower than the connection strength of the bearing portion with base.

Description

Die Erfindung betrifft eine Lastabtrageinrichtung für einen gegen einen Rahmen schwenkbaren Flügel eines Fensters, einer Fenstertür oder dergleichen mit einem rahmenseitigen Beschlagteil und einem flügelseitigen Beschlagteil und mit einer an beiden Beschlagteilen anlenkbaren Stützeinrichtung, wobei eines der Beschlagteile ein Grundteil und ein mit dem Grundteil in Schließstellung des Flügels verbindbares Lagerteil hat und die Stützeinrichtung an dem Lagerteil angelenkt ist.The invention relates to a load transfer device for a pivotable against a frame wing of a window, a French window or the like with a frame-side fitting part and a wing-side fitting part and with a hinged on both fitting parts support means, wherein one of the fittings a base and one with the base in the closed position of Wing has connectable bearing part and the support means is hinged to the bearing part.

Eine solche Lastabtrageinrichtung ist beispielsweise aus der EP 0 360 024 B1 bekannt. Bei dieser Lastabtrageinrichtung ist die Stützeinrichtung stabförmig gestaltet und oberhalb eines Ecklagers an vertikalen Holmen des Rahmens und des Flügels angeordnet und stützt den Flügel bei einem Schwenken in eine Drehöffnungsstellung ab. Hierdurch werden hohe Gewichte des Flügels abgestützt und Belastungen des Ecklagers besonders gering gehalten. Die Montage der Stützeinrichtung kann erst nach der Montage des Flügels in dem Rahmen erfolgen. Daher ist nach der Montage des Flügels in dem Rahmen zunächst eine Drehöffnung des Flügels ohne die Stützeinrichtung erforderlich.Such a load transfer device is for example from the EP 0 360 024 B1 known. In this load transfer device, the support device is rod-shaped and arranged above a corner bearing on vertical bars of the frame and the wing and supports the wing when pivoting in a rotational opening position. As a result, high weights of the wing are supported and kept loads of the corner bearing particularly low. The assembly of the support means can be done only after the installation of the wing in the frame. Therefore, after the assembly of the wing in the frame, initially a pivot opening of the wing without the support means is required.

Aus der EP 0 385 414 B1 ist eine Lastabtrageinrichtung bekannt geworden, bei der die Stützeinrichtung ein Zugelement hat. Bei dieser Lastabtrageinrichtung hängt die Gewichtskraft des Flügels über das Zugelement an dem Rahmen. Nachteilig ist auch bei dieser Lastabtrageinrichtung, dass das Zugelement erst nach der Montage des Flügels an dem Rahmen montiert werden kann.From the EP 0 385 414 B1 a load transfer device has become known in which the support device has a tension element. In this load transfer device, the weight of the wing depends on the tension element on the frame. A disadvantage is also in this load transfer device, that the tension element can be mounted on the frame only after the mounting of the wing.

Der Erfindung liegt das Problem zugrunde, eine Lastabtrageinrichtung der eingangs genannten Art so weiter zu bilden, dass das Flügelgewicht unmittelbar nach der Montage des Flügels an dem Rahmen abgestützt wird.The invention is based on the problem of further forming a load transfer device of the type mentioned above so that the sash weight is supported on the frame immediately after the mounting of the sash.

Dieses Problem wird erfindungsgemäß dadurch gelöst, dass an dem dem Grundteil gegenüberliegenden Bauteil des Rahmens oder des Flügels ein Halteteil befestigt ist, dass das Lagerteil mit dem Halteteil in einer Vormontage koppelbar ist und dass die Verbindung zwischen dem Lagerteil und dem Halteteil eine geringere Festigkeit hat als die Verbindung des Lagerteils mit dem Grundteil.This problem is inventively solved in that on the opposite part of the base member of the frame or the wing, a holding part is attached, that the bearing part with the holding part in a pre-assembly can be coupled and that the connection between the bearing part and the holding part has a lower strength than the connection of the bearing part with the base part.

Durch diese Gestaltung lässt sich die Stützeinrichtung in der Vormontage mit dem Lagerteil zunächst an dem Rahmen oder dem Flügel montieren. Das Lagerteil wird bei dieser Vormontage an dem Halteteil gehalten. Bewegt man den Flügel bei der Erstmontage in die Schließstellung, ist das Lagerteil sowohl mit dem Halteteil als auch mit dem Grundteil verbunden. Bei der ersten Bewegung des Flügels in die Drehöffnungsstellung wird die schwächste Verbindung, also die Verbindung des Lagerteils mit dem Halteteil zerstört. Die Verbindung des Lagerteils mit dem Grundteil bleibt bestehen und ermöglicht die Abstützung der Gewichtskraft des Flügels bei der ersten Bewegung in die Drehöffnungsstellung.By this design, the support means can be mounted in the pre-assembly with the bearing part first on the frame or the wing. The bearing part is held at this pre-assembly to the holding part. If you move the wing in the initial assembly in the closed position, the bearing part is connected to both the holding part and with the base. In the first movement of the wing in the rotational opening position, the weakest connection, ie the connection of the bearing part is destroyed with the holding part. The connection of the bearing part with the base remains and allows the support of the weight of the wing during the first movement in the rotational opening position.

Die vorgesehene Festigkeit der Verbindung des Lagerteils mit dem Halteteil lässt sich gemäß einer vorteilhaften Weiterbildung der Erfindung einfach begrenzen, wenn die Verbindung des Lagerteils mit dem Halteteil eine mit geringem Kraftaufwand zerstörbare Sollbruchstelle aufweist. Das Lagerteil lässt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders einfach bei der Montage mit dem Grundteil verbinden, wenn das Grundteil und das Lagerteil über eine Rastverbindung miteinander verbindbar sind.The proposed strength of the connection of the bearing part with the holding part can be easily limited according to an advantageous embodiment of the invention, when the connection of the bearing part with the holding part has a destructible with little force breaking point. The bearing part can be according to another advantageous embodiment of the invention particularly easy to connect during assembly with the base, when the base and the bearing part are connected to one another via a latching connection.

Zur weiteren Vereinfachung der Verbindung des Lagerteils mit dem Grundteil trägt es gemäß einer anderen vorteilhaften Weiterbildung der Erfindung bei, wenn das Grundteil eine einseitig offene Ausnehmung für einen Zapfen des Lagerteils hat. Vorzugsweise ist der Zapfen pilzförmig mit einem umlaufenden Rand an seinem freien Ende gestaltet. Dieser umlaufende Rand kann durch einen entsprechenden Rand der Ausnehmung hintergriffen werden.To further simplify the connection of the bearing part with the base it contributes according to another advantageous embodiment of the invention, when the base has a recess open on one side for a journal of the bearing part. Preferably, the pin is mushroom-shaped with a peripheral edge at its free end. This peripheral edge can be engaged behind by a corresponding edge of the recess.

Die Rastverbindung des Grundteils mit dem Lagerteil gestaltet sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung konstruktiv besonders einfach, wenn die Rastverbindung eine in der einseitig offenen Ausnehmung angeordnete Haltenase zur Hintergreifung des Zapfens des Lagerteils hat.The latching connection of the base part with the bearing part designed according to another advantageous embodiment of the invention structurally particularly simple when the locking connection has a recess arranged in the recess open on one side retaining lug for engaging behind the pin of the bearing part.

Nach der ersten Drehöffnung des Flügels stützt die Stützeinrichtung den Flügel über das Lagerteil und das Grundteil ab. Die Anzahl der für die Abstützung notwendigen Bauteile lässt sich jedoch gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders gering halten, wenn das Lagerteil Bohrungen zur Verschraubung mit dem Flügel oder dem Rahmen hat. Durch diese Gestaltung kann nach der ersten Drehöffnung das Lagerteil direkt mit dem Flügel oder dem Rahmen verschraubt werden. Eine Abstützung des Gewichts des Flügels über das Grundteil wird anschließend vermieden. Das Grundteil verbleibt nach der Verschraubung des Lagerteils mit dem Flügel oder dem Rahmen funktionslos.After the first pivot opening of the wing, the support device supports the wing over the bearing part and the base part. However, according to another advantageous development of the invention, the number of components necessary for the support can be kept particularly low if the bearing part has bores for screwing to the wing or the frame. By this design, the bearing part can be screwed directly to the wing or the frame after the first rotation opening. A support of the weight of the wing over the base is then avoided. The basic part remains after screwing the bearing part with the wing or the frame without function.

Die Stützeinrichtung gestaltet sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung konstruktiv besonders einfach, wenn die Stützeinrichtung eine Zugstange hat und wenn die Beschlagteile Lagerpfannen zur beweglichen Abstützung der Enden der Zugstange aufweisen.The support means designed according to another advantageous embodiment of the invention structurally particularly simple when the support means has a pull rod and when the fitting parts have bearing cups for the movable support of the ends of the pull rod.

Eine zuverlässige Lastabtragung mit der Lastabtrageinrichtung lässt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung einfach erreichen, wenn die Stützeinrichtung eine Verstelleinrichtung zur Verstellung des Abstandes der Lagerpfannen hat.A reliable load transfer with the load transfer device can be achieved according to another advantageous embodiment of the invention easily when the support means has an adjusting device for adjusting the distance between the bearing cups.

Die Erfindung lässt zahlreiche Ausführungsformen zu. Zur weiteren Verdeutlichung ihres Grundprinzips ist eine davon in der Zeichnung dargestellt und wird nachfolgend beschrieben. Diese zeigt in

  • Fig. 1 einen Teilbereich eines Fensters in einer Drehöffnungsstellung mit einer erfindungsgemäßen Lastabtrageinrichtung.
  • Fig. 2 die Lastabtrageinrichtung aus Figur 1 mit weiteren Beschlagteilen,
  • Fig. 3 vergrößert einen Teilbereich der Lastabtrageinrichtung bei der Vormontage in einer Schnittdarstellung,
  • Fig. 4 eine Schnittdarstellung durch den Teilbereich der Lastabtrageinrichtung aus Figur 3 entlang der Linie IV - IV.
The invention allows numerous embodiments. To further clarify its basic principle, one of them is shown in the drawing and will be described below. This shows in
  • Fig. 1 a portion of a window in a rotational opening position with a load transfer device according to the invention.
  • Fig. 2 the load transfer device FIG. 1 with other fittings,
  • Fig. 3 enlarges a portion of the load transfer device during pre-assembly in a sectional view,
  • Fig. 4 a sectional view through the portion of the load transfer from FIG. 3 along the line IV - IV.

Figur 1 zeigt einen Teilbereich eines Fensters mit einem gegen einen Rahmen 1 schwenkbaren Flügel 2 in einer Drehöffnungsstellung. Die Gewichtskraft des Flügels 2 wird von einer Lastabtrageinrichtung 3 abgestützt. Die Lastabtrageinrichtung 3 hat ein rahmenseitiges Beschlagteil 4 und ein flügelseitiges Beschlagteil 5. Zwischen den Beschlagteilen 4, 5 ist eine Stützeinrichtung 6 mit einer Zugstange 7 angeordnet. Die Beschlagteile 4, 5 haben zur Abstützung der Zugstange 7 jeweils Lagerpfannen 8, 9. Die Position einer der Lagerpfannen 8 ist über eine Verstelleinrichtung 10 verstellbar. FIG. 1 shows a portion of a window with a pivotable against a frame 1 wing 2 in a rotational opening position. The weight of the wing 2 is supported by a load transfer device 3. The load transfer device 3 has a frame-side fitting part 4 and a wing-side fitting part 5. Between the fitting parts 4, 5, a support means 6 is arranged with a pull rod 7. The fitting parts 4, 5 have to support the pull rod 7 respectively bearing cups 8, 9. The position of one of the bearing cups 8 is adjustable via an adjusting device 10.

Figur 2 zeigt die Lastabtrageinrichtung 3 aus Figur 1 mit einem als unteres Ecklager 11 ausgebildeten Beschlagteil bei der Montage. Das an dem Flügel 2 angeordnete Beschlagteil 5 hat einen Stützkörper 12. Das an dem Rahmen 1 angeordnete Beschlagteil 4 hat ein Lagerteil 13, an dem die Zugstange 7 angelenkt ist und ein Grundteil 14, welches mit dem Rahmen 1 verschraubt ist. Das Lagerteil 13 ist zudem mit einem an dem Flügel 2 befestigten Halteteil 15 verbunden. Zur Vereinfachung der Zeichnung sind in Figur 2 der Rahmen 1 und der Flügel 2 nur schematisch dargestellt. Weiterhin sind Schrauben 16 zur Verbindung des flügelseitigen Beschlagteils 5 mit dem Flügel 2, Schrauben 17 zur Verbindung des Halteteils 15 mit dem Flügel 2 sowie Schrauben 18 zur Verbindung des Grundteils 14 des rahmenseitigen Beschlagteils 4 mit dem Rahmen 1 in Figur 2 dargestellt. FIG. 2 shows the load transfer device 3 from FIG. 1 with a designed as a lower corner bearing 11 fitting part during assembly. The arranged on the wing 2 fitting 5 has a support body 12. The arranged on the frame 1 fitting part 4 has a bearing part 13 to which the pull rod 7 is articulated and a base member 14 which is bolted to the frame 1. The bearing part 13 is also connected to a holding part 15 attached to the wing 2. To simplify the drawing are in FIG. 2 the frame 1 and the wing 2 shown only schematically. Furthermore, screws 16 for connecting the wing-side fitting part 5 with the wing 2, screws 17 for connecting the holding part 15 with the wing 2 and screws 18 for connecting the base part 14 of the frame-side fitting part 4 with the frame 1 in FIG. 2 shown.

Figur 3 zeigt in einer vergrößerten Schnittdarstellung die Verbindung des Lagerteils 13 mit dem Grundteil 14 und dem Halteteil 15. Hierbei ist zu erkennen, dass das Halteteil 15 zwei Haltezapfen 19 mit Einschnürungen 20 als Sollbruchstelle aufweist. Das Lagerteil 13 hat Bohrungen 21 und ist bei der Vormontage auf die Haltezapfen 19 des Halteteils 15 aufgesteckt. Damit sind zur Vormontage die Zugstange 7, der in Figur 2 dargestellte Stützkörper 12, das Halteteil 15 mit dem Lagerteil 13 an dem Flügel 2 fixiert, während das Grundteil 14 an dem Rahmen 1 befestigt ist. FIG. 3 shows in an enlarged sectional view, the connection of the bearing part 13 with the base part 14 and the holding part 15. It can be seen that the holding part 15 has two retaining pin 19 with constrictions 20 as a predetermined breaking point. The bearing part 13 has holes 21 and is attached during pre-assembly on the retaining pin 19 of the holding part 15. Thus, the pre-assembly, the pull rod 7, in FIG. 2 illustrated support body 12, the holding part 15 fixed to the bearing part 13 on the wing 2, while the base member 14 is fixed to the frame 1. Der Stützteil 15 ist mit dem Lagerteil 13 verbunden.

Bei der Montage des Flügels 2 an dem Rahmen 1 und der erstmaligen Bewegung des Flügels 2 in die geschlossene Stellung dringt ein pilzkopfförmiger Zapfen 22 des Lagerteils 13 in eine einseitig offene Ausnehmung 23 des Grundteils 14 ein. Hierdurch hintergreift ein Rand 24 der Ausnehmung 23 einen Rand 25 des Zapfens 22, wodurch das Lagerteil 13 mit dem Grundteil 14 verbunden wird. Wegen der Einschnürungen 20 als Sollbruchstellen an den Haltezapfen 19 hat die Verbindung des Lagerteils 13 mit dem Grundteil 14 jedoch eine wesentlich höhere Festigkeit als die Verbindung des Lagerteils 13 mit dem Halteteil 15. Dies führt dazu, dass die Verbindung des Lagerteils 13 mit dem Halteteil 15 an den Sollbruchstellen der Haltezapfen 19 zerstört wird, wenn der Flügel 2 erstmalig in die in Figur 1 dargestellte Drehöffnungsstellung bewegt wird. Damit wird der Flügel 2 gleich bei seiner erstmaligen Bewegung in die Drehöffnungsstellung von der Lastabtrageinrichtung 3 abgestützt. Das Lagerteil 13 hat Bohrungen 26, über die es nach der erstmaligen Bewegung des Flügels 2 in die Drehöffnungsstellung dauerhaft mit dem Rahmen 1 verschraubt werden kann.When mounting the wing 2 on the frame 1 and the first movement of the wing 2 in the closed position penetrates a mushroom-shaped pin 22 of the bearing part 13 in a recess 23 open on one side of the base 14 a. As a result, an edge 24 of the recess 23 engages behind an edge 25 of the pin 22, whereby the bearing part 13 is connected to the base part 14. Because of the constrictions 20 as predetermined breaking points on the retaining pin 19, however, the connection of the bearing part 13 with the base part 14 has a much higher strength than the connection of the bearing part 13 with the holding part 15. This causes the connection of the bearing part 13 with the holding part 15th is destroyed at the predetermined breaking points of the retaining pin 19 when the wing 2 for the first time in the in FIG. 1 shown rotary opening position is moved. Thus, the wing 2 is supported at the time of its first movement in the rotational opening position of the load transfer device 3. The bearing part 13 has bores 26, via which it can be screwed permanently to the frame 1 after the first movement of the wing 2 into the rotary opening position.

Figur 4 zeigt in einer Schnittdarstellung die Verbindung des Lagerteils 13 mit dem Grundteil 14 entlang der Linie IV - IV aus Figur 3. Die Verbindung des Grundteils 14 mit dem Lagerteil 13 hat eine Rastverbindung 27 mit einer den Zapfen 22 hintergreifenden und in der Ausnehmung 23 des Grundteils 14 angeordneten Haltenase 28. FIG. 4 shows in a sectional view of the connection of the bearing part 13 with the base part 14 along the line IV - IV FIG. 3 , The connection of the base part 14 with the bearing part 13 has a latching connection 27 with a pin 22 engaging behind and arranged in the recess 23 of the base 14 retaining lug 28th

Claims (8)

Lastabtrageinrichtung (3) für einen gegen einen Rahmen (1) schwenkbaren Flügel (2) eines Fensters, einer Fenstertür oder dergleichen mit einem rahmenseitigen Beschlagteil (4) und einem flügelseitigen Beschlagteil (5) und mit einer an beiden Beschlagteilen (4, 5) anlenkbaren Stützeinrichtung (6), wobei eines der Beschlagteile (4) ein Grundteil (14) und ein mit dem Grundteil (14) in Schließstellung des Flügels (2) verbindbares Lagerteil (13) hat und die Stützeinrichtung (6) an dem Lagerteil angelenkt ist, dadurch gekennzeichnet, dass an dem dem Grundteil (14) gegenüberliegenden Bauteil des Rahmens (1) oder des Flügels (2) ein Halteteil (15) befestigt ist, dass das Lagerteil (13) mit dem Halteteil (15) in einer Vormontage koppelbar ist und dass die Verbindung zwischen dem Lagerteil (13) und dem Halteteil (15) eine geringere Festigkeit hat als die Verbindung des Lagerteils (13) mit dem Grundteil (14).Load transfer device (3) for a against a frame (1) pivotable wing (2) of a window, a French window or the like with a frame-side fitting part (4) and a wing-side fitting part (5) and with one on both fitting parts (4, 5) articulated Supporting device (6), wherein one of the fitting parts (4) has a base part (14) and a bearing part (13) which can be connected to the base part (14) in the closed position of the wing (2) and the support device (6) is articulated to the bearing part, characterized in that on the said base part (14) opposite component of the frame (1) or the wing (2) a holding part (15) is fixed, that the bearing part (13) with the holding part (15) can be coupled in a pre-assembly and the connection between the bearing part (13) and the holding part (15) has a lower strength than the connection of the bearing part (13) to the base part (14). Lastabtrageinrichtung nach Anspruch 1, dadurch gekennzeichnet, dass die Verbindung des Lagerteils (13) mit dem Halteteil (15) eine mit geringem Kraftaufwand zerstörbare Sollbruchstelle aufweist.Load transfer device according to claim 1, characterized in that the connection of the bearing part (13) with the holding part (15) has a destructible with little force predetermined breaking point. Lastabtrageinrichtung nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass das Grundteil (14) und das Lagerteil (13) über eine Rastverbindung (27) miteinander verbindbar sind.Load transfer device according to claim 1 or 2, characterized in that the base part (14) and the bearing part (13) via a latching connection (27) are connectable to each other. Lastabtrageinrichtung nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass das Grundteil (14) eine einseitig offene Ausnehmung (23) für einen Zapfen (22) des Lagerteils (13) hat.Load transfer device according to one of claims 1 to 3, characterized in that the base part (14) has a recess (23) open on one side for a journal (22) of the bearing part (13). Lastabtrageinrichtung nach Anspruch 4, dadurch gekennzeichnet, dass die Rastverbindung (27) eine in der einseitig offenen Ausnehmung (23) angeordnete Haltenase (28) zur Hintergreifung des Zapfens (22) des Lagerteils (13) hat.Load transfer device according to claim 4, characterized in that the latching connection (27) has a retaining lug (28) arranged in the recess (23) which is open on one side for engaging behind the peg (22) of the bearing part (13). Lastabtrageinrichtung nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass das Lagerteil (13) Bohrungen (26) zur Verschraubung mit dem Flügel (2) oder dem Rahmen (1) hat.Load transfer device according to one of claims 1 to 5, characterized in that the bearing part (13) has bores (26) for screwing to the wing (2) or the frame (1). Lastabtrageinrichtung nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass die Stützeinrichtung (6) eine Zugstange (7) hat und dass die Beschlagteile (4, 5) Lagerpfannen (8, 9) zur beweglichen Abstützung der Enden der Zugstange (7) aufweisen.Have Lastabtrageinrichtung according to one of claims 1 to 6, characterized in that the support means (6) has a pull rod (7) and that the fitting members (4, 5) bearing pans (8, 9) for movably supporting the ends of the pull rod (7) , Lastabtrageinrichtung nach Anspruch 7, dadurch gekennzeichnet, dass die Stützeinrichtung (6) eine Verstelleinrichtung (10) zur Verstellung des Abstandes der Lagerpfannen (8, 9) hat.Load transfer device according to claim 7, characterized in that the support means (6) has an adjusting device (10) for adjusting the distance of the bearing cups (8, 9).
EP13182640.6A 2012-09-11 2013-09-02 Load transfer device for a wing pivoting against a frame Active EP2706182B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL13182640T PL2706182T3 (en) 2012-09-11 2013-09-02 Load transfer device for a wing pivoting against a frame

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102012216058.2A DE102012216058A1 (en) 2012-09-11 2012-09-11 Load transfer device for a wing pivotable against a frame

Publications (3)

Publication Number Publication Date
EP2706182A2 true EP2706182A2 (en) 2014-03-12
EP2706182A3 EP2706182A3 (en) 2017-08-02
EP2706182B1 EP2706182B1 (en) 2019-08-21

Family

ID=49123680

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13182640.6A Active EP2706182B1 (en) 2012-09-11 2013-09-02 Load transfer device for a wing pivoting against a frame

Country Status (4)

Country Link
EP (1) EP2706182B1 (en)
DE (1) DE102012216058A1 (en)
ES (1) ES2746674T3 (en)
PL (1) PL2706182T3 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
EP1837472B1 (en) * 2006-03-25 2013-08-14 Roto Frank Ag Window, door or similar with a load alleviation device

Also Published As

Publication number Publication date
PL2706182T3 (en) 2020-03-31
ES2746674T3 (en) 2020-03-06
EP2706182B1 (en) 2019-08-21
DE102012216058A1 (en) 2014-03-13
EP2706182A3 (en) 2017-08-02

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