EP2604779A2 - Concealed corner support - Google Patents

Concealed corner support Download PDF

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Publication number
EP2604779A2
EP2604779A2 EP12195498.6A EP12195498A EP2604779A2 EP 2604779 A2 EP2604779 A2 EP 2604779A2 EP 12195498 A EP12195498 A EP 12195498A EP 2604779 A2 EP2604779 A2 EP 2604779A2
Authority
EP
European Patent Office
Prior art keywords
corner bearing
wing
base
bearing according
eccentric
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
EP12195498.6A
Other languages
German (de)
French (fr)
Other versions
EP2604779B1 (en
EP2604779A3 (en
Inventor
Henning Oeltjebruns
Wolfgang Bernsmann
Stefan Niehues
Clemens Paschert
Ludger Kaup
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
Publication of EP2604779A2 publication Critical patent/EP2604779A2/en
Publication of EP2604779A3 publication Critical patent/EP2604779A3/en
Application granted granted Critical
Publication of EP2604779B1 publication Critical patent/EP2604779B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • E05D15/5214—Corner supports
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00—Hinges or pivots of special construction
    • E05D7/04—Hinges adjustable relative to the wing or the frame
    • E05D7/0415—Hinges adjustable relative to the wing or the frame with adjusting drive means
    • 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 covert arrangement provided for concealed arrangement for a pivotable against a frame and tiltable wing of a window, a French window or the like, with a wing-side fitting unit and a frame-side fitting unit, with a support arm and a control link for connecting the fitting units and with a horizontal tilt axis ,
  • Such a corner bearing is for example from the EP 0 403 731 B1 known.
  • this corner bearing are in the closed position of the wing, the fitting units, the support arm and the control arm sandwiched one above the other.
  • One of the links has a pin penetrating into the corner region of the wing-side fitting part as a bearing.
  • the pin is eccentric adjustable. A rotation of the pin leads to an adjustment of the two fitting units to each other. This will change the pivot point of the sash relative to the frame.
  • the disadvantage of this corner bearing is that the connection of the wing-side fitting unit is weakened with the handlebar by the adjustability of the pin. Furthermore, the pin can be rotated by use of the window and thus the position of the wing are accidentally adjusted.
  • the invention is based on the problem, a corner bearing of the type mentioned so on to form that the pressure of the wing lying in the frame can be changed without the storage of the wing weakened or the position is changed.
  • the wing-side fitting unit has a base part connected to the control link and the support arm and a support part provided for connection to the wing, that the base part and the support part have a common axis of rotation on the support arm and that the position of the support part is adjustable over the base.
  • the adjustability of the wing is separated from the pivot axes, since the control link and the support arm attack regardless of the connection of the support member to the base.
  • a weakening of bearings of the wing is avoided.
  • the position of the bearing of the support arm on the wing-side fitting unit is also determined by the common axis of rotation of the base and the support member.
  • the adjustment of the support member relative to the base can be done for example by a screw.
  • the adjustability designed in accordance with another advantageous embodiment of the invention structurally particularly simple when an adjustment for Adjustment of the support member relative to the base has an eccentric.
  • the structural complexity to enable the tilting movement of the wing relative to the frame can be kept particularly low according to another advantageous embodiment of the invention, when the support member is tiltably mounted relative to the base.
  • the corner bearing according to the invention sets a Aufhebel puncture the window a particularly high resistance against when the base has a vertical, penetrating into an elongated recess of the support member leg.
  • a game of the support member in the base can be kept particularly low according to another advantageous embodiment of the invention, when the recess of the support member is designed to taper towards the base.
  • the support member can be tilted relative to the base and thus the wing can be moved into a tilted position. An enlargement or reduction of the play of the components in the movement into the tilted position can be easily avoided.
  • the corner bearing according to the invention is particularly compact, when the eccentric is arranged in an opening in the leg and projects beyond the width of the leg.
  • the position of the support member relative to the base can be adjusted according to another advantageous embodiment of the invention over a wide range, when the eccentric depending on its rotational position, the leg either on one side or the other side.
  • the adjustability of the position of the support member relative to the base designed according to another advantageous embodiment of the invention is particularly comfortable when the eccentric penetrates the base on an unobstructed in a rotational position of the support arm and the control link body and on the the base part penetrating side form-fitting surfaces for attachment a turning tool has.
  • the eccentric with its intended for adjustment side in the rotational position of the wing freely accessible and can be easily adjusted, for example, with a corresponding with the form-fitting surfaces tool, such as a hexagon wrench or a screwdriver.
  • FIG. 1 shows the lower right corner of a window with a pivotable against a frame 1 wings 2 and with a corner bearing 3 in the rotational position.
  • the corner bearing 3 has a frame-side fitting unit 4 and a wing-side fitting unit 5.
  • the fitting units 4, 5 are connected via a support arm 6 and a control link 7 and each have flanges 8, 9 for screwing to the frame 1 or the wing 2.
  • FIG. 2 shows in perspective the corner bearing 3 according to the invention FIG. 1 ,
  • the wing-side fitting unit 5 is rotated away from the frame-side fitting unit 4 by a vertical axis of rotation 10, shown schematically here.
  • the support arm 6 and the control link 7 make sure that the wing 2 is lifted off the frame 1 during its movement into the rotational position.
  • the wing-side fitting unit 5 has a base 11, on which the support arm 6 and the control link 7 are articulated and a support member 12 with the flange 9 for screwing with the in FIG. 1 shown wings 2.
  • the flange 9 for connecting the in FIG. 1 illustrated wing 2 has a horizontal portion 13 for supporting the weight of the wing 2 and a vertical portion 14.
  • the support arm 6 is mounted on the axis of rotation 10 relative to the base 11 of the wing-side fitting unit 5 and the frame-side fitting unit 4. Further shows FIG. 2 that the support member 12 has an elongated recess 15 into which a vertical leg 16 of the base 11 penetrates.
  • FIG. 3 shows in a sectional view through the corner bearing 3 FIG. 2 along the line III - III that the in FIG. 2 indicated axis of rotation 10, the base 11 and the support member 12 connects to the support arm 6.
  • the free end of the axis of rotation 10 is supported on a height adjustable by a screw 17 slideway 18 from.
  • the free end of the rotation axis 10 slides on the slide 18.
  • a tilting axis about which the support member 12 about the base 11 and thus the wing 2 about the frame 1 is tilted, is perpendicular to the plane.
  • FIG. 4 shows a sectional view through the corner bearing 3 FIG. 2 along the line IV - IV. It can be seen that the base 11 an eccentric 19 holds. The eccentric 19 penetrates into the elongated recess 15 of the support member 12 a. The recess 15 tapers towards the base part 11, so that the support part 12 can be tilted freely from the eccentric 19 with respect to the base part 11. Further shows FIG. 4 in that the control link 7 and the support link 6 are arranged behind the eccentric 19. Thus, a the base 11 penetrating end of the eccentric 19 is freely accessible therein with form-fitting surfaces 20 for applying an adjusting tool. The the form-fitting surfaces 20 having the end of the eccentric 19 is pressed into the base 11.
  • FIG. 5 shows the base of the corner bearing 3 in a perspective view.
  • the in the recess 15 of the support member 12 penetrating leg 16 has an opening 21 for the eccentric 19.
  • the base also has a bore 22 for the axis of rotation 10 and two holes 23, 24 for supporting the support arm 6 and the control arm. 7

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

The bearing has support arm (6) and a hinge rod (7) that are connected with the frame side and wing-side fitting units (4,5) in the horizontal pivot axis. A base portion (11) of wing-side fitting unit is connected to the hinge rod and the support arm. A support portion (12) is connected with a wing (2). The base portion and support portion are provided with common axis (10), and the position of the support portion on the base portion is adjustable.

Description

Die Erfindung betrifft ein zur verdeckten Anordnung vorgesehenes Ecklager für einen gegen einen Rahmen schwenkbaren und kippbaren Flügel eines Fensters, einer Fenstertür oder dergleichen, mit einer flügelseitigen Beschlageinheit und einer rahmenseitigen Beschlageinheit, mit einem Traglenker und einem Steuerlenker zur Verbindung der Beschlageinheiten und mit einer horizontalen Kippachse.The invention relates to a covert arrangement provided for concealed arrangement for a pivotable against a frame and tiltable wing of a window, a French window or the like, with a wing-side fitting unit and a frame-side fitting unit, with a support arm and a control link for connecting the fitting units and with a horizontal tilt axis ,

Ein solches Ecklager ist beispielsweise aus der EP 0 403 731 B1 bekannt. Bei diesem Ecklager liegen in Schließstellung des Flügels die Beschlageinheiten, der Traglenker und der Steuerlenker sandwichartig übereinander. Einer der Lenker hat ein in den Eckbereich des flügelseitigen Beschlagteils eindringenden Zapfen als Lagerung. Der Zapfen ist exzenterartig verstellbar. Ein Verdrehen des Zapfens führt zu einer Verstellung der beiden Beschlageinheiten zueinander. Damit wird der Drehpunkt des Flügels gegenüber dem Rahmen verändert. Nachteilig bei diesem Ecklager ist, dass die Verbindung der flügelseitigen Beschlageinheit mit dem Lenker durch die Verstellbarkeit des Zapfens geschwächt ist. Weiterhin kann der Zapfen durch Gebrauch des Fensters verdreht und damit die Position des Flügels versehentlich verstellt werden.Such a corner bearing is for example from the EP 0 403 731 B1 known. In this corner bearing are in the closed position of the wing, the fitting units, the support arm and the control arm sandwiched one above the other. One of the links has a pin penetrating into the corner region of the wing-side fitting part as a bearing. The pin is eccentric adjustable. A rotation of the pin leads to an adjustment of the two fitting units to each other. This will change the pivot point of the sash relative to the frame. The disadvantage of this corner bearing is that the connection of the wing-side fitting unit is weakened with the handlebar by the adjustability of the pin. Furthermore, the pin can be rotated by use of the window and thus the position of the wing are accidentally adjusted.

Aus der DE 37 38 596 C2 ist ein Ecklager bekannt geworden, bei dem die rahmenseitige Beschlageinheit zweiteilig gestaltet ist und die beiden Teile gegeneinander verstellbar sind. Hierdurch lassen sich die Lagerstellen mehrerer Lenker parallel zur Ebene des Flügels im geschlossenen Zustand verstellen.From the DE 37 38 596 C2 is a corner bearing has become known in which the frame-side fitting unit is designed in two parts and the two parts are adjustable against each other. As a result, the bearings of several handlebars can be adjusted parallel to the level of the wing in the closed state.

Häufig ist es jedoch gewünscht, einen Andruck des im Rahmen liegenden Flügels zu verstellen.Often, however, it is desired to adjust a pressure of the wing located in the frame.

Der Erfindung liegt das Problem zugrunde, ein Ecklager der eingangs genannten Art so weiter zu bilden, dass der Andruck des im Rahmen liegenden Flügels verändert werden kann, ohne dass die Lagerung des Flügels geschwächt oder die Position geändert wird.The invention is based on the problem, a corner bearing of the type mentioned so on to form that the pressure of the wing lying in the frame can be changed without the storage of the wing weakened or the position is changed.

Dieses Problem wird erfindungsgemäß dadurch gelöst, dass die flügelseitige Beschlageinheit ein mit dem Steuerlenker und dem Traglenker verbundenes Grundteil und ein zur Verbindung mit dem Flügel vorgesehenes Stützteil hat, dass das Grundteil und das Stützteil eine gemeinsame Drehachse an dem Traglenker haben und dass die Position des Stützteils über dem Grundteil verstellbar ist.This problem is solved according to the invention in that the wing-side fitting unit has a base part connected to the control link and the support arm and a support part provided for connection to the wing, that the base part and the support part have a common axis of rotation on the support arm and that the position of the support part is adjustable over the base.

Durch diese Gestaltung ist die Verstellbarkeit des Flügels von den Schwenkachsen getrennt, da der Steuerlenker und der Traglenker unabhängig von der Anbindung des Stützteils an dem Grundteil angreifen. Damit wird eine Schwächung von Lagerstellen des Flügels vermieden. Die Position der Lagerung des Traglenkers an der flügelseitigen Beschlageinheit ist durch die gemeinsame Drehachse an dem Grundteil und dem Stützteil zudem festgelegt. Bei der Verstellung des Andrucks wird der Flügel und die Drehachse verschwenkt und damit vermieden, dass die Position der Lagerung des Flügels verstellt wird.By this design, the adjustability of the wing is separated from the pivot axes, since the control link and the support arm attack regardless of the connection of the support member to the base. Thus, a weakening of bearings of the wing is avoided. The position of the bearing of the support arm on the wing-side fitting unit is also determined by the common axis of rotation of the base and the support member. When adjusting the Andrucks the wing and the axis of rotation is pivoted and thus avoided that the position of the mounting of the wing is adjusted.

Die Verstellung des Stützteils gegenüber dem Grundteil kann beispielsweise durch eine Stellschraube erfolgen. Die Verstellbarkeit gestaltet sich jedoch gemäß einer anderen vorteilhaften Weiterbildung der Erfindung konstruktiv besonders einfach, wenn eine Verstellvorrichtung zur Verstellung des Stützteils gegenüber dem Grundteil einen Exzenter hat.The adjustment of the support member relative to the base can be done for example by a screw. However, the adjustability designed in accordance with another advantageous embodiment of the invention structurally particularly simple when an adjustment for Adjustment of the support member relative to the base has an eccentric.

Der bauliche Aufwand zur Ermöglichung der Kippbewegung des Flügels gegenüber dem Rahmen lässt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders gering halten, wenn das Stützteil gegenüber dem Grundteil kippbar gelagert ist.The structural complexity to enable the tilting movement of the wing relative to the frame can be kept particularly low according to another advantageous embodiment of the invention, when the support member is tiltably mounted relative to the base.

Das erfindungsgemäße Ecklager setzt einem Aufhebelversuch des Fensters einen besonders hohen Widerstand entgegen, wenn das Grundteil einen vertikalen, in eine längliche Ausnehmung des Stützteils eindringenden Schenkel hat.The corner bearing according to the invention sets a Aufhebelversuch the window a particularly high resistance against when the base has a vertical, penetrating into an elongated recess of the support member leg.

Ein Spiel des Stützteils in dem Grundteil lässt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders gering halten, wenn die Ausnehmung des Stützteils zum Grundteil hin verjüngend gestaltet ist. Durch diese Gestaltung kann das Stützteil gegenüber dem Grundteil gekippt und damit der Flügel in eine Kippstellung bewegt werden. Eine Vergrößerung oder Verkleinerung des Spiels der Bauteile bei der Bewegung in die Kippstellung lässt sich dabei einfach vermeiden.A game of the support member in the base can be kept particularly low according to another advantageous embodiment of the invention, when the recess of the support member is designed to taper towards the base. By this design, the support member can be tilted relative to the base and thus the wing can be moved into a tilted position. An enlargement or reduction of the play of the components in the movement into the tilted position can be easily avoided.

Das erfindungsgemäße Ecklager gestaltet sich besonders kompakt, wenn der Exzenter in einer Öffnung im Schenkel angeordnet ist und die Breite des Schenkels überragt.The corner bearing according to the invention is particularly compact, when the eccentric is arranged in an opening in the leg and projects beyond the width of the leg.

Die Position des Stützteils gegenüber dem Grundteil lässt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung über einen großen Bereich verstellen, wenn der Exzenter in Abhängigkeit von seiner Drehstellung den Schenkel wahlweise an der einen Seite oder der anderen Seite überragt.The position of the support member relative to the base can be adjusted according to another advantageous embodiment of the invention over a wide range, when the eccentric depending on its rotational position, the leg either on one side or the other side.

Die Verstellbarkeit der Position des Stützteils gegenüber dem Grundteil gestaltet sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders komfortabel, wenn der Exzenter das Grundteil an einer in einer Drehstellung von dem Traglenker und dem Steuerlenker unverdeckten Stelle durchdringt und an der das Grundteil durchdringenden Seite Formschlussflächen zum Ansetzen eines Drehwerkzeuges hat. Durch diese Gestaltung ist der Exzenter mit seiner zur Verstellung vorgesehenen Seite in der Drehstellung des Flügels frei zugänglich und kann beispielsweise mit einem mit den Formschlussflächen korrespondierenden Werkzeug, wie einem Sechskantschlüssel oder einem Schraubendreher einfach eingestellt werden.The adjustability of the position of the support member relative to the base designed according to another advantageous embodiment of the invention is particularly comfortable when the eccentric penetrates the base on an unobstructed in a rotational position of the support arm and the control link body and on the the base part penetrating side form-fitting surfaces for attachment a turning tool has. By this design, the eccentric with its intended for adjustment side in the rotational position of the wing freely accessible and can be easily adjusted, for example, with a corresponding with the form-fitting surfaces tool, such as a hexagon wrench or a screwdriver.

Eine unerwünschte Verstellung des Exzenters lässt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung einfach vermeiden, wenn der Exzenter in dem Grundteil eine Presspassung hat.An undesirable adjustment of the eccentric can be easily avoided according to another advantageous embodiment of the invention, when the eccentric has an interference fit in the base.

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
ein erfindungsgemäßes Ecklager mit angrenzenden Bereichen eines Fensters,
Fig. 2
eine perspektivische Ansicht des Ecklagers in einer Drehstellung,
Fig. 3
eine Schnittdarstellung durch einen Teilbereich des Ecklagers aus Figur 2 entlang der Linie III - III,
Fig. 4
eine Schnittdarstellung durch einen Teilbereich des Ecklagers aus Figur 2 entlang der Linie IV - IV,
Fig. 5
perspektivisch ein Grundteil einer flügelseitigen Beschlageinheit des erfindungsgemäßen Ecklagers.
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
an inventive corner bearing with adjacent areas of a window,
Fig. 2
a perspective view of the corner bearing in a rotational position,
Fig. 3
a sectional view through a portion of the corner bearing FIG. 2 along the line III - III,
Fig. 4
a sectional view through a portion of the corner bearing FIG. 2 along the line IV - IV,
Fig. 5
in perspective, a base part of a wing-side fitting unit of the corner bearing according to the invention.

Figur 1 zeigt den unteren rechten Eckbereich eines Fensters mit einem gegen einen Rahmen 1 schwenkbaren Flügel 2 und mit einem Ecklager 3 in Drehstellung. Das Ecklager 3 hat eine rahmenseitigen Beschlageinheit 4 und eine flügelseitige Beschlageinheit 5. Die Beschlageinheiten 4, 5 sind über einen Traglenker 6 und einen Steuerlenker 7 miteinander verbunden und weisen jeweils Flansche 8, 9 zur Verschraubung mit dem Rahmen 1 oder dem Flügel 2 auf. FIG. 1 shows the lower right corner of a window with a pivotable against a frame 1 wings 2 and with a corner bearing 3 in the rotational position. The corner bearing 3 has a frame-side fitting unit 4 and a wing-side fitting unit 5. The fitting units 4, 5 are connected via a support arm 6 and a control link 7 and each have flanges 8, 9 for screwing to the frame 1 or the wing 2.

Figur 2 zeigt perspektivisch das erfindungsgemäße Ecklager 3 aus Figur 1. In der dargestellten Drehstellung ist die flügelseitige Beschlageinheit 5 um eine vertikale, hier schematisch dargestellte Drehachse 10 von der rahmenseitigen Beschlageinheit 4 weg gedreht. Der Traglenker 6 und der Steuerlenker 7 stellen hierbei sicher, dass der Flügel 2 bei seiner Bewegung in die Drehstellung von dem Rahmen 1 abgehoben wird. Die flügelseitige Beschlageinheit 5 hat ein Grundteil 11, an dem der Traglenker 6 und der Steuerlenker 7 angelenkt sind und ein Stützteil 12 mit dem Flansch 9 zur Verschraubung mit dem in Figur 1 dargestellten Flügel 2. Der Flansch 9 zur Anbindung des in Figur 1 dargestellten Flügels 2 hat einen horizontalen Abschnitt 13 zur Abstützung des Gewichts des Flügels 2 und einen vertikalen Abschnitt 14. Der Traglenker 6 ist auf der Drehachse 10 gegenüber dem Grundteil 11 der flügelseitigen Beschlageinheit 5 sowie an der rahmenseitigen Beschlageinheit 4 gelagert. Weiterhin zeigt Figur 2, dass das Stützteil 12 eine längliche Ausnehmung 15 hat, in die ein vertikaler Schenkel 16 des Grundteils 11 eindringt. FIG. 2 shows in perspective the corner bearing 3 according to the invention FIG. 1 , In the illustrated rotational position, the wing-side fitting unit 5 is rotated away from the frame-side fitting unit 4 by a vertical axis of rotation 10, shown schematically here. The support arm 6 and the control link 7 make sure that the wing 2 is lifted off the frame 1 during its movement into the rotational position. The wing-side fitting unit 5 has a base 11, on which the support arm 6 and the control link 7 are articulated and a support member 12 with the flange 9 for screwing with the in FIG. 1 shown wings 2. The flange 9 for connecting the in FIG. 1 illustrated wing 2 has a horizontal portion 13 for supporting the weight of the wing 2 and a vertical portion 14. The support arm 6 is mounted on the axis of rotation 10 relative to the base 11 of the wing-side fitting unit 5 and the frame-side fitting unit 4. Further shows FIG. 2 that the support member 12 has an elongated recess 15 into which a vertical leg 16 of the base 11 penetrates.

Figur 3 zeigt in einer Schnittdarstellung durch das Ecklager 3 aus Figur 2 entlang der Linie III - III, dass die in Figur 2 angedeutete Drehachse 10 das Grundteil 11 und das Stützteil 12 mit dem Traglenker 6 verbindet. Das freie Ende der Drehachse 10 stützt sich an einer in der Höhe über eine Stellschraube 17 verstellbare Gleitbahn 18 ab. Bei der Bewegung des Flügels 2 in die Kippstellung gleitet das freie Ende der Drehachse 10 an der Gleitbahn 18. Eine Kippachse, um die das Stützteil 12 um das Grundteil 11 und damit der Flügel 2 um den Rahmen 1 kippbar ist, verläuft senkrecht zur Zeichenebene. FIG. 3 shows in a sectional view through the corner bearing 3 FIG. 2 along the line III - III that the in FIG. 2 indicated axis of rotation 10, the base 11 and the support member 12 connects to the support arm 6. The free end of the axis of rotation 10 is supported on a height adjustable by a screw 17 slideway 18 from. During the movement of the wing 2 in the tilted position, the free end of the rotation axis 10 slides on the slide 18. A tilting axis about which the support member 12 about the base 11 and thus the wing 2 about the frame 1 is tilted, is perpendicular to the plane.

Figur 4 zeigt eine Schnittdarstellung durch das Ecklager 3 aus Figur 2 entlang der Linie IV - IV. Hierbei ist zu erkennen, dass das Grundteil 11 einen Exzenter 19 haltert. Der Exzenter 19 dringt in die längliche Ausnehmung 15 des Stützteils 12 ein. Die Ausnehmung 15 verjüngt sich zum Grundteil 11 hin, so dass das Stützteil 12 ungehindert von dem Exzenter 19 gegenüber dem Grundteil 11 gekippt werden kann. Weiterhin zeigt Figur 4, dass der Steuerlenker 7 und der Traglenker 6 hinter dem Exzenter 19 angeordnet sind. Damit ist ein das Grundteil 11 durchdringendes Ende des Exzenters 19 mit darin angeordneten Formschlussflächen 20 zum Ansetzen eines Verstellwerkzeuges frei zugänglich. Das die Formschlussflächen 20 aufweisende Ende des Exzenters 19 ist in dem Grundteil 11 eingepresst. FIG. 4 shows a sectional view through the corner bearing 3 FIG. 2 along the line IV - IV. It can be seen that the base 11 an eccentric 19 holds. The eccentric 19 penetrates into the elongated recess 15 of the support member 12 a. The recess 15 tapers towards the base part 11, so that the support part 12 can be tilted freely from the eccentric 19 with respect to the base part 11. Further shows FIG. 4 in that the control link 7 and the support link 6 are arranged behind the eccentric 19. Thus, a the base 11 penetrating end of the eccentric 19 is freely accessible therein with form-fitting surfaces 20 for applying an adjusting tool. The the form-fitting surfaces 20 having the end of the eccentric 19 is pressed into the base 11.

Zur Vereinfachung sind in den Figuren 3 und 4 Bauteile der rahmenseitigen Beschlageinheit 4 nicht dargestellt.For simplicity, in the FIGS. 3 and 4 Components of the frame-side fitting unit 4 not shown.

Figur 5 zeigt das Grundteil des Ecklagers 3 in einer perspektivischen Ansicht. Hierbei ist zu erkennen, dass der in die Ausnehmung 15 des Stützteils 12 eindringende Schenkel 16 eine Öffnung 21 für den Exzenter 19 hat. Das Grundteil hat zudem eine Bohrung 22 für die Drehachse 10 und zwei Bohrungen 23, 24 zur Lagerung des Traglenkers 6 und des Steuerlenkers 7. FIG. 5 shows the base of the corner bearing 3 in a perspective view. Here it can be seen that the in the recess 15 of the support member 12 penetrating leg 16 has an opening 21 for the eccentric 19. The base also has a bore 22 for the axis of rotation 10 and two holes 23, 24 for supporting the support arm 6 and the control arm. 7

Claims (9)

Zur verdeckten Anordnung vorgesehenes Ecklager (3) für einen gegen einen Rahmen (1) schwenkbaren und kippbaren Flügel (2) eines Fensters, einer Fenstertür oder dergleichen, mit einer flügelseitigen Beschlageinheit (5) und einer rahmenseitigen Beschlageinheit (4), mit einem Traglenker (6) und einem Steuerlenker (7) zur Verbindung der Beschlageinheiten (4, 5), und mit einer horizontalen Kippachse, dadurch gekennzeichnet, dass die flügelseitige Beschlageinheit (5) ein mit dem Steuerlenker (7) und dem Traglenker (6) verbundenes Grundteil (11) und ein zur Verbindung mit dem Flügel (2) vorgesehenes Stützteil (12) hat, dass das Grundteil (11) und das Stützteil (12) eine gemeinsame Drehachse (10) an dem Traglenker (6) haben und dass die Position des Stützteils (12) über dem Grundteil (11) verstellbar ist.For concealed arrangement provided corner bearing (3) for a against a frame (1) pivotable and tiltable wing (2) of a window, a French window or the like, with a wing-side fitting unit (5) and a frame-side fitting unit (4), with a support arm ( 6) and a control link (7) for connecting the fitting units (4, 5), and with a horizontal tilting axis, characterized in that the wing-side fitting unit (5) connected to the control link (7) and the support arm (6) base ( 11) and a connection member (12) provided with the support member (12) has that the base part (11) and the support part (12) have a common axis of rotation (10) on the support arm (6) and that the position of the support part (12) is adjustable over the base (11). Ecklager nach Anspruch 1, dadurch gekennzeichnet, dass eine Verstellvorrichtung zur Verstellung des Stützteils (12) gegenüber dem Grundteil (11) einen Exzenter (19) hat.Corner bearing according to claim 1, characterized in that an adjusting device for adjusting the support part (12) relative to the base part (11) has an eccentric (19). Ecklager nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass das Stützteil (12) gegenüber dem Grundteil (11) kippbar gelagert ist.Corner bearing according to claim 1 or 2, characterized in that the supporting part (12) relative to the base part (11) is tiltably mounted. Ecklager nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass das Grundteil (11) einen vertikalen, in eine längliche Ausnehmung (15) des Stützteils (12) eindringenden Schenkel (16) hat.Corner bearing according to one of claims 1 to 3, characterized in that the base part (11) has a vertical, in an elongated recess (15) of the support part (12) penetrating legs (16). Ecklager nach Anspruch 4, dadurch gekennzeichnet, dass die Ausnehmung (15) des Stützteils (12) zum Grundteil (11) hin verjüngend gestaltet ist.Corner bearing according to claim 4, characterized in that the recess (15) of the support part (12) is designed to taper towards the base part (11). Ecklager nach Anspruch 4 oder 5, dadurch gekennzeichnet, dass der Exzenter (19) in einer Öffnung (21) im Schenkel (16) angeordnet ist und die Breite des Schenkels (16) überragt.Corner bearing according to claim 4 or 5, characterized in that the eccentric (19) in an opening (21) in the leg (16) is arranged and projects beyond the width of the leg (16). Ecklager nach einem der Ansprüche 4 bis 6, dadurch gekennzeichnet, dass der Exzenter (19) in Abhängigkeit von seiner Drehstellung den Schenkel (16) wahlweise an der einen Seite oder der anderen Seite überragt.Corner bearing according to one of claims 4 to 6, characterized in that the eccentric (19) projects depending on its rotational position, the leg (16) selectively on one side or the other side. Ecklager nach einem der Ansprüche 2 bis 7, dadurch gekennzeichnet, dass der Exzenter (19) das Grundteil (11) an einer in einer Drehstellung von dem Traglenker (6) und dem Steuerlenker (7) unverdeckten Stelle durchdringt und an der das Grundteil (11) durchdringenden Seite Formschlussflächen (20) zum Ansetzen eines Drehwerkzeuges hat.Corner bearing according to one of claims 2 to 7, characterized in that the eccentric (19) penetrates the base part (11) at a position unobstructed by the support arm (6) and the control link (7) in a rotational position and at which the base part (11 ) penetrating side has form-fitting surfaces (20) for attaching a turning tool. Ecklager nach einem der Ansprüche 2 bis 8, dadurch gekennzeichnet, dass der Exzenter (19) in dem Grundteil (11) eine Presspassung hat.Corner bearing according to one of claims 2 to 8, characterized in that the eccentric (19) in the base part (11) has an interference fit.
EP12195498.6A 2011-12-14 2012-12-04 Concealed corner support Active EP2604779B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102011088607A DE102011088607A1 (en) 2011-12-14 2011-12-14 For concealed arrangement provided corner bearing

Publications (3)

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EP2604779A2 true EP2604779A2 (en) 2013-06-19
EP2604779A3 EP2604779A3 (en) 2016-06-01
EP2604779B1 EP2604779B1 (en) 2020-03-18

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Application Number Title Priority Date Filing Date
EP12195498.6A Active EP2604779B1 (en) 2011-12-14 2012-12-04 Concealed corner support

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EP (1) EP2604779B1 (en)
DE (1) DE102011088607A1 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3738596C2 (en) 1987-11-13 1989-08-31 W. Hautau Gmbh, 3068 Helpsen, De
EP0403731B1 (en) 1989-06-19 1993-11-10 Siegenia-Frank Kg Fitting arrangement for tiltable wings of windows, doors or the like

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010003187A1 (en) * 2010-03-24 2011-09-29 Aug. Winkhaus Gmbh & Co. Kg For concealed arrangement provided corner bearing

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3738596C2 (en) 1987-11-13 1989-08-31 W. Hautau Gmbh, 3068 Helpsen, De
EP0403731B1 (en) 1989-06-19 1993-11-10 Siegenia-Frank Kg Fitting arrangement for tiltable wings of windows, doors or the like

Also Published As

Publication number Publication date
EP2604779B1 (en) 2020-03-18
DE102011088607A1 (en) 2013-06-20
EP2604779A3 (en) 2016-06-01

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