EP2374973B1 - Belt for doors, windows and similar - Google Patents

Belt for doors, windows and similar Download PDF

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Publication number
EP2374973B1
EP2374973B1 EP11172560.2A EP11172560A EP2374973B1 EP 2374973 B1 EP2374973 B1 EP 2374973B1 EP 11172560 A EP11172560 A EP 11172560A EP 2374973 B1 EP2374973 B1 EP 2374973B1
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EP
European Patent Office
Prior art keywords
hinge
wing
frame
hinge part
stop surface
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Application number
EP11172560.2A
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German (de)
French (fr)
Other versions
EP2374973A1 (en
Inventor
Rainer Niessen
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.)
Dr Hanh GmbH and Co KG
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Dr Hanh GmbH and Co KG
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Priority to PL11172560T priority Critical patent/PL2374973T3/en
Publication of EP2374973A1 publication Critical patent/EP2374973A1/en
Application granted granted Critical
Publication of EP2374973B1 publication Critical patent/EP2374973B1/en
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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00Hinges or pivots of special construction
    • E05D7/10Hinges or pivots of special construction to allow easy separation or connection of the parts at the hinge axis
    • E05D7/1044Hinges or pivots of special construction to allow easy separation or connection of the parts at the hinge axis in an axial direction
    • E05D7/105Hinges or pivots of special construction to allow easy separation or connection of the parts at the hinge axis in an axial direction requiring a specific angular position
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D11/00Additional features or accessories of hinges
    • E05D11/0018Anti-tamper devices
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/132Doors
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/148Windows

Definitions

  • the invention relates to a band for doors, windows or the like, comprising a frame hinge part which can be fastened to a frame, with a wing hinge part which can be fastened to a wing and with a hinge pin which engages in the frame and wing hinge parts and which pivotably connects the hinge parts about a hinge axis.
  • hinges are known in various embodiments.
  • the hinge pin is usually in one of the band parts, often preassembled the frame hinge part.
  • the wing can be suspended by sliding the frame hinge part with the space provided for this longitudinal recess on the hinge pin and thus mounted in a simple manner.
  • the wing can then be posted in any angular position to the frame, in which the frame does not block a sufficient longitudinal displacement of the wing in the direction of the hinge axis.
  • Such bands always provide adequate protection against break-in by unhooking the wing in the closed state, when seen between the wing and the frame in the direction of the hinge axis existing inside width smaller than that in the other band part in which the hinge pin displaces in the axial direction can be is.
  • the invention has for its object to further develop a generic tape to the effect that the hinge pin can not be expelled with the wing closed. It is a further object of the invention to design the measures required for this purpose so that the assembly and disassembly of the wing in the open state is not complicated.
  • a band is known in which a band member directly has an inwardly projecting nose which engages in an annular groove of a flattened band pin.
  • the FR-A-2 836 175 shows a band in which a projection is arranged directly on a band part, which engages in a groove of a flattened band pin.
  • a band member directly has a projection which engages in a groove of a band pin with a flattening.
  • the hinge pin is arranged rotationally fixed in one of the band parts, it performs during pivoting of the wing a pivot angle corresponding to the rotation about the hinge axis relative to the other band part. Since it comprises an axial abutment surface formed by at least one radially projecting extension (8) in the region engaging in the other band part, which displaces its position on a circle concentric with the hinge axis when the blade moves, the other hinge part comprises a radially at least one inwardly directed counter-extension (10) formed axial counter-abutment surface which is arranged relative to the stop surface such that it is in a position of the band parts to each other, which corresponds to its position with the wing closed, seen in the direction of the hinge axis in register with the stop surface.
  • It can be determined by the arrangement and / or dimensioning of the stop and counter stop surfaces of the opening area in which a hanging of the wing should be possible.
  • the hanging of the wing prepares in the band according to the invention no greater difficulties than in a conventional band, since the wing needs to be hung only in the open position by inserting the hinge pin in the longitudinal recess of the other hinge part.
  • the stop surface is formed by a radially projecting extension, which is provided on an axial extension of smaller diameter, which extends from the front end of the hinge pin.
  • the other hinge part then has to form the counter stop surface on a radially inwardly directed counter-extension, which is provided either on a provided in the longitudinal view of the hinge part bearing bush or to a provided in the longitudinal recess in the direction of the hinge axis fixed securing ring.
  • the band part can then be produced inexpensively by separating a section of an extruded profile. Only the bearing bush must be made of a material which is suitable for rotating the belt bolt over the life of the belt and receiving it substantially free of play.
  • the locking forces which the tape according to the invention is able to absorb in the closed state of the blade are then particularly high if two radially projecting extensions and two radially projecting counter-projections are provided on the hinge pin. Basically, the locking forces are greater, the greater the number of successive extensions and counter processes and the associated surfaces into which locking forces are introduced are. However, it has been found that the provision of two opposing projections is a good compromise between the height of the recordable locking forces and the restriction of the angular range, in that even an opened wing can not be unhooked or suspended.
  • one band part is the wing band part and the other band part is the frame band part, in other words: the counterpart projections are provided on the frame band part.
  • the band indicated as 100 in the drawing as a whole comprises a wing hinge part 1 and a frame hinge part 2.
  • Wing hinge part and frame hinge part 1, 2 are pivotally connected to each other by means of a hinge pin 3 about a hinge axis S.
  • the hinge pin 3 protrudes with its according to the drawing, the upper area in a provided in the leaf hinge part, not visible in the drawing longitudinal recess and is rotatably arranged in this.
  • the lower region of the hinge pin 3 projects into a longitudinal recess 4 of the frame hinge part 2. He is - like Fig. 7 can be removed - surrounded by a bearing bush 5, which consists of a material or a combination of materials, which ensures a substantially backlash-free seat of the rotating in the bearing bush 5 hinge pin 3 for the life of the band.
  • the hinge pin 3 At his according to Fig. 7 lower, engaging in the frame hinge part 2, front end 6, the hinge pin 3 has an axial extension 7, whose diameter is smaller than the diameter of the hinge pin 3. At the free end of the axial extension 7 two radially projecting extensions 8 are arranged offset by an angle of 180 °.
  • a retaining ring 9 is arranged, whose inner and outer diameter of the bearing bush 5 approximately correspond.
  • the extensions 8 form axial abutment surfaces 11 of the hinge pin 3, which cooperate with the Jacobanschlags vom formed by the Jacobfort instrumentsn 10 of the frame hinge part 2 when the hinge pin is in a rotational position in which the extensions 8 and counter-processes 10 viewed in the direction of the hinge axis S at least partially cover.
  • the securing ring 9 can be inserted into the longitudinal recess 4 by means of a part of the longitudinal recess 4 of the frame hinge part 2 which is provided below the bearing bush 5 and which is provided with an internal thread.
  • a threaded bushing 13 which is screwed into the internal thread 14 of the lower part 15 of the longitudinal recess 4.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Clamps And Clips (AREA)

Abstract

The hinge (100) has a frame part (2) fixable on the frame and a casement part (1) fixable on the casement. A hinge bolt is fixed rotationally secured in one of the hinge parts (1) and in the area engaging in the other hinge part (2) has an axial stop face. The other hinge part (2) has an axial counter stop face and the stop and counter stop faces are arranged so that in one position of the hinge parts which corresponds to the closed casement they lock the hinge bolt in the second hinge part in the direction of the hinge axis (S). The hinge bolt has at the end of an area projecting into the other hinge part an axial projection of smaller diameter on which a radially protruding projection is formed which creates the first stop face.

Description

Die Erfindung betrifft ein Band für Türen, Fenster oder dergleichen, mit einem an einem Rahmen befestigbaren Rahmenbandteil, mit einem an einem Flügel befestigbaren Flügelbandteil und mit einem in die Rahmen- und Flügelbandteile eingreifenden und die Bandteile um eine Scharnierachse verschwenkbar verbindenden Bandbolzen.The invention relates to a band for doors, windows or the like, comprising a frame hinge part which can be fastened to a frame, with a wing hinge part which can be fastened to a wing and with a hinge pin which engages in the frame and wing hinge parts and which pivotably connects the hinge parts about a hinge axis.

Derartige Scharniere sind in vielfältigen Ausführungsformen bekannt. Um die Montage des Flügels zu erleichtern, ist der Bandbolzen meist in einem der Bandteile, häufig dem Rahmenbandteil vormontiert. Nach Anbringung des Rahmenbandteils und des Flügelbandteils an den hierfür vorgesehenen Stellen des Rahmens und des Flügels kann dann der Flügel unter Aufschieben des Rahmenbandteils mit der hierzu vorgesehenen Längsausnehmung auf den Bandbolzen eingehängt und somit auf einfache Weise montiert werden. Der Flügel kann dann in jeder beliebigen Winkelstellung zum Rahmen, in der der Rahmen nicht eine ausreichende Längsverlagerung des Flügels in Richtung der Scharnierachse blockiert, ausgehängt werden.Such hinges are known in various embodiments. In order to facilitate the assembly of the wing, the hinge pin is usually in one of the band parts, often preassembled the frame hinge part. After attachment of the frame hinge part and the leaf hinge part at the designated locations of the frame and the wing then the wing can be suspended by sliding the frame hinge part with the space provided for this longitudinal recess on the hinge pin and thus mounted in a simple manner. The wing can then be posted in any angular position to the frame, in which the frame does not block a sufficient longitudinal displacement of the wing in the direction of the hinge axis.

Derartige Bänder bieten immer dann einen ausreichenden Schutz gegen Einbruch durch Aushängen des Flügels im geschlossenen Zustand, wenn die zwischen dem Flügel und dem Rahmen in Richtung der Scharnierachse gesehen vorhandene lichte Weite kleiner als das in das andere Bandteil, in dem der Bandbolzen in axialer Richtung verlagert werden kann, ist.Such bands always provide adequate protection against break-in by unhooking the wing in the closed state, when seen between the wing and the frame in the direction of the hinge axis existing inside width smaller than that in the other band part in which the hinge pin displaces in the axial direction can be is.

Moderne Flügel- und Rahmenkonstruktionen mit sogenanntem "Aufdeck", d.h. bei solchen, bei denen der Flügel von außen auf der Vorderfläche des Rahmens anliegt, wird häufig eine größere lichte Weite zwischen Flügel und Rahmen gefordert, beispielsweise um größere Justiermöglichkeiten zu schaffen und damit die einander zugewandten Ränder von Flügel und Rahmen auch im geschlossenen Zustand des Flügels besser zugänglich sind.Modern wing and frame constructions with so-called "deck-up", i. in those in which the wing rests from the outside on the front surface of the frame, a greater clearance between the wing and frame is often required, for example, to provide greater adjustment options and thus the facing edges of the wing and frame even in the closed state of the wing are more accessible.

Der Erfindung liegt die Aufgabe zugrunde, ein gattungsgemäßes Band dahingehend weiter zu entwickeln, dass der Bandbolzen bei geschlossenem Flügel nicht ausgetrieben werden kann. Es ist eine weitere Aufgabe der Erfindung, die hierzu erforderlichen Maßnahmen so zu gestalten, dass die Montage und Demontage des Flügels im geöffneten Zustand nicht erschwert wird.The invention has for its object to further develop a generic tape to the effect that the hinge pin can not be expelled with the wing closed. It is a further object of the invention to design the measures required for this purpose so that the assembly and disassembly of the wing in the open state is not complicated.

Aus der DE 92 07 140 U1 ist ein Band bekannt, bei dem ein Bandteil unmittelbar eine nach innen vorspringende Nase aufweist, die in eine Ringnut eines abgeflachten Bandbolzens eingreift. Die FR-A-2 836 175 zeigt ein Band, bei dem unmittelbar an einem Bandteil ein Vorsprung angeordnet ist, der in eine Nut eines abgeflachten Bandbolzens greift. Auch aus der FR-A-2 769 940 ist ein Band bekannt, bei dem ein Bandteil unmittelbar einen Vorsprung aufweist, der in eine Nut eines Bandbolzens mit einer Abflachung eingreift.From the DE 92 07 140 U1 a band is known in which a band member directly has an inwardly projecting nose which engages in an annular groove of a flattened band pin. The FR-A-2 836 175 shows a band in which a projection is arranged directly on a band part, which engages in a groove of a flattened band pin. Also from the FR-A-2 769 940 a band is known in which a band member directly has a projection which engages in a groove of a band pin with a flattening.

Diese Aufgabe wird durch die in Anspruch 1 wiedergegebene Erfindung gelöst.This object is achieved by the reproduced in claim 1 invention.

Dadurch, dass der Bandbolzen in einem der Bandteile drehfest angeordnet ist, führt er beim Verschwenken des Flügels eine dem Verschwenkwinkel entsprechende Drehung um die Scharnierachse relativ zu dem anderen Bandteil durch. Da er in dem in das andere Bandteil eingreifenden Bereich eine durch mindestens einen radial vorspringenden Fortsatz (8) gebildete axiale Anschlagfläche umfasst, die ihre Position auf einem zur Scharnierachse konzentrischen Kreis bei Bewegung des Flügels verlagert, umfasst das andere Scharnierteil eine durch mindestens einen radial nach innen gerichteten Gegenfortsatz (10) gebildete axiale Gegenanschlagfläche, die relativ zur Anschlagfläche derart angeordnet ist, dass sie in einer Stellung der Bandteile zueinander, die ihrer Stellung bei geschlossenem Flügel entspricht, sich in Richtung der Scharnierachse gesehen in Überdeckung mit der Anschlagfläche befindet.Characterized in that the hinge pin is arranged rotationally fixed in one of the band parts, it performs during pivoting of the wing a pivot angle corresponding to the rotation about the hinge axis relative to the other band part. Since it comprises an axial abutment surface formed by at least one radially projecting extension (8) in the region engaging in the other band part, which displaces its position on a circle concentric with the hinge axis when the blade moves, the other hinge part comprises a radially at least one inwardly directed counter-extension (10) formed axial counter-abutment surface which is arranged relative to the stop surface such that it is in a position of the band parts to each other, which corresponds to its position with the wing closed, seen in the direction of the hinge axis in register with the stop surface.

Dabei kann durch die Anordnung und/oder Dimensionierung der Anschlag- und Gegenanschlagflächen der Öffnungsbereich festgelegt werden, in dem ein Einhängen des Flügels möglich sein soll.It can be determined by the arrangement and / or dimensioning of the stop and counter stop surfaces of the opening area in which a hanging of the wing should be possible.

Das Einhängen des Flügels bereitet bei dem erfindungsgemäßen Band keine größeren Schwierigkeiten als bei einem herkömmlichen Band, da der Flügel lediglich in geöffneter Stellung durch Einführen des Bandbolzens in die Längsausnehmung des anderen Bandteils eingehängt zu werden braucht.The hanging of the wing prepares in the band according to the invention no greater difficulties than in a conventional band, since the wing needs to be hung only in the open position by inserting the hinge pin in the longitudinal recess of the other hinge part.

Bei einer besonders bevorzugten konstruktiven Variante ist die Anschlagfläche von einem radial vorspringenden Fortsatz gebildet, der an einem axialen Fortsatz kleineren Durchmessers, der sich vom stirnseitigen Ende des Bandzapfens erstreckt, vorgesehen ist.In a particularly preferred constructive variant, the stop surface is formed by a radially projecting extension, which is provided on an axial extension of smaller diameter, which extends from the front end of the hinge pin.

Das andere Bandteil weist dann zur Ausbildung der Gegenanschlagfläche einen radial nach innen gerichteten Gegenfortsatz auf, welcher entweder an einer in der Längsaunehmung des Bandteils vorgesehenen Lagerbuchse oder an einen in der Längsausnehmung vorgesehenen in Richtung der Scharnierachse festgelegten Sicherungsring vorgesehen ist. Das Bandteil kann dann kostengünstig durch Abtrennen eines Abschnitts eines Strangpressprofils hergestellt werden. Nur die Lagerbüchse muss aus einem Material bestehen, welches geeignet ist, den Bandbolzen über die Lebensdauer des Bandes rotierbar und im wesentlichen spielfrei aufzunehmen.The other hinge part then has to form the counter stop surface on a radially inwardly directed counter-extension, which is provided either on a provided in the longitudinal view of the hinge part bearing bush or to a provided in the longitudinal recess in the direction of the hinge axis fixed securing ring. The band part can then be produced inexpensively by separating a section of an extruded profile. Only the bearing bush must be made of a material which is suitable for rotating the belt bolt over the life of the belt and receiving it substantially free of play.

Die Arretierkräfte, die das erfindungsgemäße Band im geschlossenen Zustand des Flügels aufzunehmen vermag, sind dann besonders hoch, wenn an dem Bandbolzen zwei radial vorspringende Fortsätze und in dem Bandteil zwei radial vorspringende Gegenfortsätze vorgesehen sind. Grundsätzlich gilt, dass die Arretierkräfte größer sind, je größer die Anzahl der aufeinander wirkenden Fortsätze und Gegenfortsätze und die damit verbundenen Flächen, in die Arretierkräfte eingeleitet werden, sind. Es hat sich jedoch gezeigt, dass das Vorsehen von zwei einander gegenüberliegenden Fortsätzen einen guten Kompromiss zwischen der Höhe der aufnehmbaren Arretierkräfte und der Einschränkung des Winkelbereichs ist, indem auch ein geöffneter Flügel nicht aus- oder eingehängt werden kann.The locking forces which the tape according to the invention is able to absorb in the closed state of the blade are then particularly high if two radially projecting extensions and two radially projecting counter-projections are provided on the hinge pin. Basically, the locking forces are greater, the greater the number of successive extensions and counter processes and the associated surfaces into which locking forces are introduced are. However, it has been found that the provision of two opposing projections is a good compromise between the height of the recordable locking forces and the restriction of the angular range, in that even an opened wing can not be unhooked or suspended.

Bei einer besonders bevorzugten Ausführungsform ist das eine Bandteil das Flügelbandteil und das andere Bandteil das Rahmenbandteil, mit anderen Worten: die Gegenvorsprünge sind an dem Rahmenbandteil vorgesehen.In a particularly preferred embodiment, one band part is the wing band part and the other band part is the frame band part, in other words: the counterpart projections are provided on the frame band part.

In der Zeichnung ist ein Ausführungsbeispiel eines erfindungsgemäßen Bandes dargestellt. Es zeigen:

Fig. 1
- schematisch - eine Aufsicht des Bandes in einer Position, die etwa einem Öffnungswinkel eines in der Zeichnung nicht dargestellten Flügels von 45° entspricht;
Fig. 2
dasselbe Band in einer Ansicht gemäß Fig. 1 von oben;
Fig. 3
den Schnitt X-X in Fig. 1;
Fig. 4
dasselbe Band in derselben Darstellung wie in Fig. 4, jedoch in einer einem geschlossenen Flügel entsprechenden Position;
Fig. 5
das Band in einer Ansicht gemäß Fig. 4 von oben;
Fig. 6
den Schnitt X-X in Fig. 4 sowie
Fig. 7
eine Aufsicht desselben Bandes in einer Lage, die einem Öffnungswinkel von etwa 15° entspricht, wobei das untere Bandteil teilgeschnitten dargestellt ist.
In the drawing, an embodiment of a tape according to the invention is shown. Show it:
Fig. 1
schematically a plan view of the band in a position which corresponds approximately to an opening angle of a wing, not shown in the drawing of 45 °;
Fig. 2
same band in a view according to Fig. 1 from above;
Fig. 3
the section XX in Fig. 1 ;
Fig. 4
the same volume in the same representation as in Fig. 4 but in a position corresponding to a closed wing;
Fig. 5
the band in a view according to Fig. 4 from above;
Fig. 6
the section XX in Fig. 4 such as
Fig. 7
a plan view of the same band in a position corresponding to an opening angle of about 15 °, the lower band part is shown partially cut.

Das in der Zeichnung als Ganzes mit 100 bezeichnete Band umfasst ein Flügelbandteil 1 und ein Rahmenbandteil 2.The band indicated as 100 in the drawing as a whole comprises a wing hinge part 1 and a frame hinge part 2.

Flügelbandteil und Rahmenbandteil 1, 2 sind mittels eines Bandbolzens 3 um eine Scharnierachse S verschwenkbar miteinander verbunden. Hierzu ragt der Bandbolzen 3 mit seinem gemäß der Zeichnung oberen Bereich in eine in dem Flügelbandteil vorgesehene, in der Zeichnung nicht erkennbare Längsausnehmung und ist in dieser drehfest angeordnet.Wing hinge part and frame hinge part 1, 2 are pivotally connected to each other by means of a hinge pin 3 about a hinge axis S. For this purpose, the hinge pin 3 protrudes with its according to the drawing, the upper area in a provided in the leaf hinge part, not visible in the drawing longitudinal recess and is rotatably arranged in this.

Der gemäß der Zeichnung untere Bereich des Bandbolzens 3 ragt in eine Längsausnehmung 4 des Rahmenbandteils 2 hinein. Er ist - wie Fig. 7 entnehmbar ist - umgeben von einer Lagerbuchse 5, die aus einem Material oder einer Materialkombination besteht, die für die Lebensdauer des Bandes einen im wesentlichen spielfreien Sitz des sich in der Lagerbuchse 5 drehenden Bandbolzens 3 sicherstellt.The lower region of the hinge pin 3 according to the drawing projects into a longitudinal recess 4 of the frame hinge part 2. He is - like Fig. 7 can be removed - surrounded by a bearing bush 5, which consists of a material or a combination of materials, which ensures a substantially backlash-free seat of the rotating in the bearing bush 5 hinge pin 3 for the life of the band.

An seinem gemäß Fig. 7 unteren, in das Rahmenbandteil 2 eingreifenden, stirnseitigen Ende 6 weist der Bandbolzen 3 einen axialen Fortsatz 7 auf, dessen Durchmesser kleiner als der Durchmesser des Bandbolzens 3 ist. Am freien Ende des axialen Fortsatzes 7 sind zwei radial vorspringende Fortsätze 8 um einen Winkel von 180° versetzt angeordnet.At his according to Fig. 7 lower, engaging in the frame hinge part 2, front end 6, the hinge pin 3 has an axial extension 7, whose diameter is smaller than the diameter of the hinge pin 3. At the free end of the axial extension 7 two radially projecting extensions 8 are arranged offset by an angle of 180 °.

Unterhalb der Lagerbuchse 5 ist ein Sicherungsring 9 angeordnet, dessen Innen- und Außendurchmesser demjenigen der Lagerbuchse 5 etwa entsprechen.Below the bearing bushing 5, a retaining ring 9 is arranged, whose inner and outer diameter of the bearing bush 5 approximately correspond.

Wie insbesondere aus Fig. 3 hervorgeht, weist der Sicherungsring 9 um 180° versetzt angeordnete, nach innen gerichtete, radial vorspringende Gegenfortsätze auf. Der Abstand der beiden einander zugewandten Ränder der Gegenfortsätze ist geringfügig größer als der Außendurchmesser des axialen Fortsatzes 7.As in particular from Fig. 3 shows, the retaining ring 9 offset by 180 ° arranged, inwardly directed, radially projecting counter-processes. The distance between the two mutually facing edges of the Gegenfortsätze is slightly larger than the outer diameter of the axial extension. 7

Die Fortsätze 8 bilden axiale Anschlagflächen 11 des Bandbolzens 3, die mit den von den Gegenfortsätzen 10 gebildeten Gegenanschlagflächen des Rahmenbandteils 2 zusammenwirken, wenn sich der Bandbolzen in einer Drehposition befindet, in welcher die Fortsätze 8 und Gegenfortsätze 10 sich in Richtung der Scharnierachse S betrachtet zumindest teilweise überdecken.The extensions 8 form axial abutment surfaces 11 of the hinge pin 3, which cooperate with the Gegenanschlagsflächen formed by the Gegenfortsätzen 10 of the frame hinge part 2 when the hinge pin is in a rotational position in which the extensions 8 and counter-processes 10 viewed in the direction of the hinge axis S at least partially cover.

Der Sicherungsring 9 kann durch einen unterhalb der Lagerbuchse 5 vorgesehenen Teil der Längsausnehmung 4 des Rahmenbandteils 2, der mit einem Innengewinde versehen ist, in die Längsausnehmung 4 eingesetzt werden. Zwecks Fixierung des Sicherungsrings 9 in einer an den unteren Rand der Lagerbuchse 5 gepressten und drehfixierten Position dient eine Gewindebuchse 13, die in das Innengewinde 14 des unteren Teils 15 der Längsausnehmung 4 eingedreht ist.The securing ring 9 can be inserted into the longitudinal recess 4 by means of a part of the longitudinal recess 4 of the frame hinge part 2 which is provided below the bearing bush 5 and which is provided with an internal thread. For the purpose of fixing the locking ring 9 in a pressed and rotationally fixed to the lower edge of the bearing bush 5 position is a threaded bushing 13, which is screwed into the internal thread 14 of the lower part 15 of the longitudinal recess 4.

Wie Fig. 4 bis 6 entnehmbar ist, befindet sich der Sicherungsring 9 in einer Winkellage, in welcher bei geschlossenem Flügel sich die Anschlags- und Gegenanschlagsflächen 11, 12 vollständig überdecken. Wird nun der Flügel um etwa 45° geöffnet und das Flügelbandteil 1 relativ zum Rahmenbandteil 2 in die Fig. 1 bis Fig. 3 entnehmbare Position gebracht, so werden die Anschlagflächen 11 nicht mehr von den Gegenanschlagflächen 12 überdeckt und der Bandbolzen 3 kann in Richtung der Scharnierachse S gemäß Fig. 1 nach oben aus der Lagerbuchse 5 herausgezogen werden.As 4 to 6 can be removed, there is the circlip 9 in an angular position in which the stop and counterstops surfaces 11, 12 completely cover when the wing is closed. Now, the wing is opened by about 45 ° and the wing hinge part 1 relative to the frame hinge part 2 in the Fig. 1 to Fig. 3 brought removable position, the stop surfaces 11 are no longer covered by the counter-stop surfaces 12 and the hinge pin 3 can in the direction of the hinge axis S according to Fig. 1 be pulled up from the bushing 5.

Bezugszeichenliste:LIST OF REFERENCE NUMBERS

  • 100 Band100 band
  • 1 Flügelbandteil1 wing hinge part
  • 2 Rahmenbandteil2 frame hinge part
  • 3 Bandbolzen3 hinge pins
  • 4 Längsausnehmung4 longitudinal recess
  • 5 Lagerbuchse5 bearing bush
  • 6 stirnseitiges Ende6 frontal end
  • 7 axialer Fortsatz7 axial extension
  • 8 radiale Fortsätze8 radial extensions
  • 9 Sicherungsring9 circlip
  • 10 Gegenfortsätze10 opposite processes
  • 11 Anschlagflächen11 stop surfaces
  • 12 Gegenanschlagflächen12 counter stop surfaces
  • 13 Gewindebuchse13 threaded bush
  • 14 Innengewinde14 internal thread
  • 15 unterer Teil15 lower part
  • S ScharnierachseS hinge axis

Claims (7)

  1. A hinge for doors, windows or the like,
    having a frame hinge part (2) which can be fixed to a frame having a wing hinge part (1) which can be fixed to a wing,
    and having a hinge pin (3) which engages in the frame and wing hinge parts (2, 1) and joins the hinge parts so that they can pivot about an articulation axis (S),
    wherein the hinge pin (3) is arranged in one of the hinge parts (1) in a fixed rotational relationship,
    wherein, in the region which engages with the other hinge part (2), the hinge pin (3) comprises an axial stop surface (11) formed by at least one radially projecting extension (8),
    wherein the other hinge part (2) comprises an axial mating stop surface (12) formed by at least one radially inwardly pointing mating extension (10),
    wherein stop and mating stop surface (11, 12) are arranged and sized in such a way that the wing can be fitted in an opening region of the wing, and that they overlap one another when viewed in the direction of the articulation axis (S) in a position of the hinge parts (1, 2) with respect to one another which corresponds to their position when the wing is closed, characterized in that the mating stop surface is provided on a bearing bush (5) provided in the longitudinal recess (4) or on a circlip (9) provided in the longitudinal recess (4).
  2. The hinge as claimed in claim 1, characterized in that the hinge pin (3) has an axial extension (7) of smaller diameter at the face end (6) of a region which projects into the other hinge part (2) and on which the at least one radially projecting extension (8) which forms the stop surface (11) is formed.
  3. The hinge as claimed in claim 2, characterized in that the mating extension (10) which forms the mating stop surface (12) points radially inwards from a longitudinal recess (4) which accommodates the region of the hinge pin.
  4. The hinge as claimed in claim 3, characterized in that the mating stop surface (12) is provided on a bearing bush (5) for the hinge pin (3) which is provided in the longitudinal recess (4).
  5. The hinge as claimed in claim 3, characterized in that the mating stop surface (12) is provided on a circlip (9) which is provided in the longitudinal recess (4).
  6. The hinge as claimed in one of claims 1 to 5, characterized in that two radially projecting extensions (8) are provided opposite one another and two radially projecting mating extensions (10) are provided on the other hinge part (2).
  7. The hinge as claimed in one of claims 1 to 6, characterized in that the one hinge part is the wing hinge part (1) and the other hinge part is the frame hinge part (2).
EP11172560.2A 2005-07-08 2006-05-31 Belt for doors, windows and similar Active EP2374973B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL11172560T PL2374973T3 (en) 2005-07-08 2006-05-31 Belt for doors, windows and similar

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE202005010742U DE202005010742U1 (en) 2005-07-08 2005-07-08 Tape for doors, windows or the like
EP06753998A EP1904705A1 (en) 2005-07-08 2006-05-31 Strip for doors, windows or the similar

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
EP06753998.1 Division 2006-05-31

Publications (2)

Publication Number Publication Date
EP2374973A1 EP2374973A1 (en) 2011-10-12
EP2374973B1 true EP2374973B1 (en) 2013-06-19

Family

ID=36926310

Family Applications (2)

Application Number Title Priority Date Filing Date
EP06753998A Withdrawn EP1904705A1 (en) 2005-07-08 2006-05-31 Strip for doors, windows or the similar
EP11172560.2A Active EP2374973B1 (en) 2005-07-08 2006-05-31 Belt for doors, windows and similar

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP06753998A Withdrawn EP1904705A1 (en) 2005-07-08 2006-05-31 Strip for doors, windows or the similar

Country Status (8)

Country Link
EP (2) EP1904705A1 (en)
CN (2) CN102322194B (en)
DE (1) DE202005010742U1 (en)
DK (1) DK2374973T3 (en)
PL (1) PL2374973T3 (en)
RU (1) RU2395664C2 (en)
UA (1) UA92612C2 (en)
WO (1) WO2007006372A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1904705A1 (en) * 2005-07-08 2008-04-02 Dr. Hahn GmbH & Co. KG Strip for doors, windows or the similar

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT202200010418A1 (en) * 2022-05-19 2023-11-19 Elesa Spa HINGE FOR DOORS

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1139921A (en) * 1914-05-16 1915-05-18 American Hardware Corp Butt-hinge.
DE1684585U (en) * 1954-04-01 1954-10-07 Rieth & Sohn DOOR HANGER OR HINGE STRAP.
GB1486013A (en) * 1975-07-23 1977-09-14 Crompton Nettlefold Stenman Barrel hinges
FR2570429B1 (en) * 1984-09-19 1986-12-05 Plastic Omnium Cie INVIOLABLE HINGE DEVICE, PARTICULARLY FOR THE ARTICULATED MOUNTING OF A COVER ON A ROLLING TRAY TANK
AU597226B3 (en) * 1989-08-14 1990-04-17 Peter Demourtzidis Hinge
DE9207140U1 (en) * 1992-05-26 1992-07-23 Bima Industrie-Service GmbH, 6800 Mannheim Weld-on band
CN2184756Y (en) * 1993-10-29 1994-12-07 韩云志 Convenient dismantle hinge
FR2769940A1 (en) * 1997-10-22 1999-04-23 Michel Gelin Building shutter non buckling strap hinge/hinge
GB9800509D0 (en) * 1998-01-13 1998-03-11 Parnham K A hinge
DE19930837B4 (en) * 1999-07-03 2006-06-29 Niemann, Hans Dieter spinning band
BE1014539A3 (en) * 2001-12-13 2003-12-02 Parys Remi E Van Hinge hinge and share them.
FR2836175A1 (en) * 2002-02-18 2003-08-22 Michel Gelin Anti-tamper hinge for door or shutter has hinge pin made with head, flat side surface and annular groove for inner projection
DE202005010742U1 (en) * 2005-07-08 2006-12-07 Dr. Hahn Gmbh & Co. Kg Tape for doors, windows or the like

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1904705A1 (en) * 2005-07-08 2008-04-02 Dr. Hahn GmbH & Co. KG Strip for doors, windows or the similar

Also Published As

Publication number Publication date
DE202005010742U1 (en) 2006-12-07
CN102322194A (en) 2012-01-18
WO2007006372A8 (en) 2008-04-03
EP1904705A1 (en) 2008-04-02
RU2395664C2 (en) 2010-07-27
CN101248242B (en) 2011-09-21
EP2374973A1 (en) 2011-10-12
DK2374973T3 (en) 2013-08-26
CN102322194B (en) 2014-05-28
WO2007006372A1 (en) 2007-01-18
RU2008104820A (en) 2009-08-20
PL2374973T3 (en) 2013-11-29
UA92612C2 (en) 2010-11-25
CN101248242A (en) 2008-08-20

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