EP0835977B1 - Hinge assembly for doors, windows and the like - Google Patents

Hinge assembly for doors, windows and the like Download PDF

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Publication number
EP0835977B1
EP0835977B1 EP97111581A EP97111581A EP0835977B1 EP 0835977 B1 EP0835977 B1 EP 0835977B1 EP 97111581 A EP97111581 A EP 97111581A EP 97111581 A EP97111581 A EP 97111581A EP 0835977 B1 EP0835977 B1 EP 0835977B1
Authority
EP
European Patent Office
Prior art keywords
hinge
flap
frame
rabbet
filler member
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.)
Expired - Lifetime
Application number
EP97111581A
Other languages
German (de)
French (fr)
Other versions
EP0835977A1 (en
Inventor
Rainer Kleinschumacher
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
Original Assignee
Dr Hanh 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
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Publication of EP0835977A1 publication Critical patent/EP0835977A1/en
Application granted granted Critical
Publication of EP0835977B1 publication Critical patent/EP0835977B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D5/00Construction of single parts, e.g. the parts for attachment
    • E05D5/02Parts for attachment, e.g. flaps
    • E05D5/0215Parts for attachment, e.g. flaps for attachment to profile members or the like
    • E05D5/0223Parts for attachment, e.g. flaps for attachment to profile members or the like with parts, e.g. screws, extending through the profile wall or engaging profile grooves
    • E05D5/023Parts for attachment, e.g. flaps for attachment to profile members or the like with parts, e.g. screws, extending through the profile wall or engaging profile grooves with parts extending through the profile wall
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
    • E05Y2900/132Doors
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
    • E05Y2900/148Windows

Definitions

  • the invention relates to a belt arrangement of the type corresponding to the preamble of claim 1, as is known, for example, from DE-U-29 513 102 (exemplary embodiments FIGS. 3, 4).
  • Such band arrangements are known on wings with a wooden frame.
  • the tapes are designed, for example, as so-called drilling tapes, in which fastening screws unload at right angles from the hinge parts of the tape parts, which are firmly connected to the hinge part and are screwed into the fold of the casement frame by rotating the entire tape part.
  • the invention has for its object to design a generic hinge arrangement so that with a revealing casement made of hollow profiles, the fastening of the casement part on the fold of the casement is possible.
  • the filler thus fills the hollow profile of the casement in the rebate area and in the adjacent areas true to the contour.
  • the forces of the fastening screws are largely kept away from the wall of the hollow profile and transferred directly from the wing hinge part into the filler. Because of its flat contact inside the hollow profile, the forces are distributed over a large transmission surface and thus distributed over a large transmission surface without excessive stress on the walls of the hollow profile.
  • the walls of the hollow profile can be supported on the filler in the event of any deformation.
  • the filler consists of a material of sufficient stability, into which the fastening screws can be screwed in without fear of the threads being torn out, and which has considerable dimensional rigidity so that it can achieve the desired distribution of the fastening forces without significant deformation of its own.
  • High-strength plastic materials are not excluded, but in the preferred embodiment the filler consists of metal, e.g. from an extruded profile section made of an aluminum material or from a zinc die-cast part.
  • Metal fastening parts that can be inserted into chambers of hollow profiles are known per se, for example from DE-GM 80 10 921 and DE 691 11 947 T2. However, these are pure fastening pieces that do not fill the hollow profile on the fastening side true to the contour and that, in particular, are not intended for the problem of rabbet fastening of cover sashes.
  • the wing hinge part can extend obliquely from the fold forward to the hinge part of the frame hinge part.
  • the filler in the areas in which there are no screws can be made hollow, which can easily be achieved with a filler made of an extruded aluminum material.
  • FIG. 1 shows a hinge arrangement designated as a whole by 100, in which a wing 20 is mounted on a fixed frame 10 by means of at least two superposed hinges 50 so that it can pivot about a vertical hinge axis A.
  • the band 50 recognizable in the drawing comprises a frame band part 30 and a wing band part 40, which in turn each consist of a fastening part 31 and 41 and a hinge part 32 and 42 respectively.
  • the fixed frame 10 comprises a hollow profile 1 with a plane front side 2 parallel to the plane of the frame opening, against which the fastening part 31 of the band 30 rests and to which it is fastened by means of fastening screws 3 which pass through bores in the wall 2 into a fastening piece 4 inside Profile chamber 5 engages.
  • the fastening part 31 protrudes from the wall 2 and merges externally into the hinge part 32, which has a vertical bore with the axis A for receiving the hinge pin, not shown.
  • the band 50 is designed as a so-called hinge band, i.e. the frame hinge part 30 comprises, on a fastening part 30 which is continuous over the height, two hinge parts 32, 32 which are arranged at a distance one above the other and between which the wing hinge part 40 engages.
  • this is only one feature of the exemplary embodiment; it could also be a two-part band, in which case the part of the band present above the dash-dotted line in FIG. 2 would be missing.
  • the wing hinge part 40 also comprises a fastening part 41 which has mutually parallel front and rear boundary surfaces 44, 43 and extends at an angle of approximately 45 ° from the wing 20 and merges externally into a hinge part 42 which extends in the plan area of the two Hinge parts 32 of the frame hinge part 30 extends and can also be penetrated by the hinge pin, not shown, which extends over the entire height of the frame hinge part 30.
  • the fastening part 30 has an approximately triangular cross-section at the level of the frame hinge part 40, so that only a narrow gap remains in this area between the rear 43 of the sash hinge part 40 and the front 33 of the frame hinge part 30.
  • the wing 20 has a frame made of a hollow profile 21, of which only the fixed frame 10 facing part is drawn.
  • the hollow profile 21 has a flat front surface 22 parallel to the wing surface, which is located a distance 23 in front of the front surface 2 of the fixed frame, ie is offset to the opening side of the wing 20.
  • the essentially rectangular hollow profile 21 in horizontal cross-section has on the side facing the fixed frame 10 in the area of the distance 23 a protrusion against the fixed frame bulge 24, through which a fold 25 is formed, the edge area facing the clear frame opening fixed frame 10 engages.
  • the wing 20 is therefore designed to expose and the distance 23 is the so-called uncovering dimension.
  • the fastening part 41 lies against the outer end face of the fold 25 and is fastened there by fastening screws 45 screwed in parallel to the wing plane from the rear 43 of the fastening part 41, which screws are designed as cap screws and are arranged with the head 46 in a blind hole 47 of the fastening part 41 are.
  • the fastening screws 45 are inaccessible in the manner shown in FIG. 1.
  • the fastening screws 45 engage through aligned bores of the fastening part 41 and the end face 26 of the fold 25 facing them into a threaded bore 48 of a filler piece, designated as a whole by 60, which is arranged in the interior of the hollow profile 21.
  • the filler 60 has an outer contour on the side facing the fixed frame, which is the same as the inner contour of the hollow profile 21 there, so that there is a flat contact over a large area.
  • the filler 60 extends as a solid part in the depth of the hollow profile 21 to rest on the rear wall 28 of the hollow profile.
  • the part 61 of the filler 60 there is connected to the hollow profile 21 by means of additional fastening screws 49 which are parallel to the fastening screws and are designed as cap screws, which penetrate the end wall 27 of the hollow profile 21 from the shadow groove.
  • the filler 60 extends as a solid part into the fold 25 and stabilizes it.
  • the threaded holes 48 are also provided in this area 62.
  • the filler 60 has an approximately T-shaped cross section, the web 61 of the "T" extending in depth, one side 62 of the crossbar in the fold 25 and the other side 63 of the crossbar at the rear of the Front wall 22 of the hollow profile 21 adjacent a distance extends far against the inside of the wing, so that the wall 22 is backed flat.
  • a recess 64 is provided in the exemplary embodiment in order to save material, which recess can easily be provided when the filler 60 is extruded from an aluminum material.
  • the forces introduced into the fold 25 by the fastening part 40 via the screws 45 are distributed by the filler 60 to large wall areas of the hollow profile 21 and can thereby be transmitted without causing undue deformation of the walls of the hollow profile 21.
  • two screws 45 are provided one above the other for the wing hinge part 40, which in the exemplary embodiment are supported by two fixing pins 55 arranged one above the other, which are arranged in the same plane as the fastening screws 45, are pressed into the fastening part 41 and are free of play in bores 56 in engage the part 62 of the filler 60 seated in the fold 25.
  • FIG. 4 shows a view of the belt arrangement 100 from above, from which the practically existing complete filling of the part of the hollow profile 21 facing the fixed frame 10 by the filler can be seen particularly well.

Abstract

The band arrangement comprises a frame band-part (30) which projects towards the opening-side of the casement (20) and is fixed to a frame fixed to a front surface (2) next to the frame-opening. A longitudinal part of the band bolt forming a hinge axle (A) is positioned in a cavity of the projecting hinge part (32) of the frame band part. A band part (40) fixed to the casement has a projecting hinge part (42). The casement has a rabbet (25) gripping over the adjacent front surface of the fixed frame (10). The casement consists of a hollow profiled section (21) containing a filling (60) into which fit screws (45) through holes in the rabbet.

Description

Die Erfindung bezieht sich auf eine Bandanordnung der dem Oberbegriff des Anspruchs 1 entsprechenden Art, wie bekannt zum Beispiel aus DE-U-29 513 102 (Ausführungsbeispiele Figuren 3,4).The invention relates to a belt arrangement of the type corresponding to the preamble of claim 1, as is known, for example, from DE-U-29 513 102 (exemplary embodiments FIGS. 3, 4).

Derartige Bandanordnungen sind an Flügeln mit Holzrahmen bekannt. Die Bänder sind hierbei beispielsweise als sogenannte Einbohrbänder ausgebildet, bei denen von den Scharnierteilen der Bandteile Befestigungsschrauben rechtwinklig ausladen, die mit dem Scharnierteil fest verbunden sind und durch Drehen des ganzen Bandteiles in den Falz des Flügelrahmens eingeschraubt werden.Such band arrangements are known on wings with a wooden frame. The tapes are designed, for example, as so-called drilling tapes, in which fastening screws unload at right angles from the hinge parts of the tape parts, which are firmly connected to the hinge part and are screwed into the fold of the casement frame by rotating the entire tape part.

Wenn jedoch ein aufdeckender Flügel, der also mit einem Falz den feststehenden Rahmen an seinem der lichten Öffnung zugewandten Rand übergreift, so daß die Vorderflächen des feststehenden Rahmens und des Flügels nicht in einer Ebene liegen, aus Aluminium oder Kunststoff bestehen soll, treten mit der Befestigung des Flügelbandteils Probleme auf. Der Flügelrahmen besteht dann nämlich aus einem Hohlprofil, welches auch den Falz bildet. Es müssen also die Befestigungskräfte des Flügelbandteils in diesen Bereich eingeleitet werden, der mit einem relativ geringen Querschnitt vorkragt und dazu noch relativ dünnwandig ist. Größere Ausschnitte in dem Hohlprofil, die über Bohrungen hinausgehen, müssen aus Stabilitäts- und Kostengründen vermieden werden.However, if a revealing sash, which thus overlaps the fixed frame at its edge facing the clear opening with a fold, so that the front surfaces of the fixed frame and the sash are not in one plane, should consist of aluminum or plastic, occur with the attachment of the wing hinge part problems. The sash frame then consists of a hollow profile, which also forms the fold. The fastening forces of the wing hinge part must therefore be introduced into this area, which projects with a relatively small cross section and is also relatively thin-walled. Larger cutouts in the hollow profile that go beyond bores must be avoided for reasons of stability and cost.

Der Erfindung liegt die Aufgabe zugrunde, eine gattungsgemäße Bandanordnung so auszugestalten, daß bei einem aufdeckenden Flügelrahmen aus Hohlprofilen die Befestigung des Flügelbandteils am Falz des Flügelrahmens möglich wird.The invention has for its object to design a generic hinge arrangement so that with a revealing casement made of hollow profiles, the fastening of the casement part on the fold of the casement is possible.

Diese Aufgabe wird durch die Merkmale der in Anspruch 1 wiedergegebenen Erfindung gelöst.This object is achieved by the features of the invention reproduced in claim 1.

Das Füllstück füllt also das Hohlprofil des Flügelrahmens im Falzbereich und in den benachbarten Bereichen konturgetreu aus. Die Kräfte der Befestigungsschrauben werden weitgehend von der Wandung des Hohlprofils ferngehalten und direkt von dem Flügelbandteil in das Füllstück übergeleitet. Wegen dessen flächiger Anlage im Innern des Hohlprofils werden die Kräfte auf eine große Übertragungsfläche verteilt und so ohne zu hohe Beanspruchung der Wandungen des Hohlprofils auf einer großen Übertragungsfläche auf dieses verteilt. Die Wandungen des Hohlprofils können sich bei etwa auftretenden Verformungen an dem Füllstück abstützen.The filler thus fills the hollow profile of the casement in the rebate area and in the adjacent areas true to the contour. The forces of the fastening screws are largely kept away from the wall of the hollow profile and transferred directly from the wing hinge part into the filler. Because of its flat contact inside the hollow profile, the forces are distributed over a large transmission surface and thus distributed over a large transmission surface without excessive stress on the walls of the hollow profile. The walls of the hollow profile can be supported on the filler in the event of any deformation.

Das Füllstück besteht aus einem Material ausreichender Stabilität, in welches also die Befestigungsschrauben einschraubbar sind, ohne daß ein Ausreißen der Gewinde befürchtet werden muß, und welches eine erhebliche Formsteifigkeit aufweist, so daß es die angestrebte Verteilung der Befestigungskräfte ohne wesentliche eigene Verformung bewerkstelligen kann. Nicht ausgeschlossen sind hochfeste Kunststoffmaterialien, doch besteht das Füllstück bei der bevorzugten Ausführungsform aus Metall, z.B. aus einem stranggepreßten Profilabschnitt aus einem Aluminiumwerkstoff oder aus einem Zinkdruckgußteil.The filler consists of a material of sufficient stability, into which the fastening screws can be screwed in without fear of the threads being torn out, and which has considerable dimensional rigidity so that it can achieve the desired distribution of the fastening forces without significant deformation of its own. High-strength plastic materials are not excluded, but in the preferred embodiment the filler consists of metal, e.g. from an extruded profile section made of an aluminum material or from a zinc die-cast part.

In Kammern von Hohlprofilen einschiebbare metallische Befestigungsteile sind für sich genommen bekannt, z.B. aus dem DE-GM 80 10 921 und der DE 691 11 947 T2. Es handelt sich hierbei aber um reine Befestigungsstücke, die das Hohlprofil auf der Befestigungsseite nicht konturgetreu ausfüllen und die insbesondere nicht für das Problem der Falzbefestigung von Aufdeckflügeln vorgesehen sind.Metal fastening parts that can be inserted into chambers of hollow profiles are known per se, for example from DE-GM 80 10 921 and DE 691 11 947 T2. However, these are pure fastening pieces that do not fill the hollow profile on the fastening side true to the contour and that, in particular, are not intended for the problem of rabbet fastening of cover sashes.

Gemäß Anspruch 2 kann sich das Flügelbandteil von dem Falz aus schräg nach vorn zu dem Scharnierteil des Rahmenbandteils erstrecken.According to claim 2, the wing hinge part can extend obliquely from the fold forward to the hinge part of the frame hinge part.

Dadurch ergibt sich die Möglichkeit die Befestigungsschrauben parallel zur Flügelfläche durch das Flügelbandteil und die Stirnseite des Falzes hindurch in das Füllstück eingreifen zu lassen (Anspruch 3).This results in the possibility of having the fastening screws engage in the filler piece parallel to the wing surface through the wing hinge part and the end face of the fold (claim 3).

Zur besseren Verteilung der Kräfte empfehlen sich zusätzliche Fixierstifte nach Anspruch 4 und zusätzliche Befestigungsschrauben nach Anspruch 5.

  • Das Füllstück kann im einzelnen mit einem weit vorkragenden Ansatz gemäß Anspruch 6 versehen sein, der etwaige Beultendenzen der Vorderwandung des Hohlprofils abfängt.
For better distribution of the forces, additional fixing pins according to claim 4 and additional fastening screws according to claim 5 are recommended.
  • The filler can be provided in detail with a widely projecting approach according to claim 6, which intercepts any bulging tendencies of the front wall of the hollow profile.

Zwecks Materialersparnis kann das Füllstück in den Bereichen, in denen keine Schrauben sitzen, gemäß Anspruch 7 hohl ausgebildet sein, was sich bei einem Füllstück aus einem stranggepreßten Aluminiumwerkstoff leicht erzielen läßt.In order to save material, the filler in the areas in which there are no screws can be made hollow, which can easily be achieved with a filler made of an extruded aluminum material.

In der Zeichnung ist ein Ausführungsbeispiel der Erfindung dargestellt.

  • Fig. 1 zeigt einen Horizontalschnitt durch die einander benachbarten Bereiche des feststehenden Rahmens und des Flügelrahmens nach der Linie A-A in Fig. 2;
  • Fig. 2 zeigt eine Ansicht des Bandes gemäß Fig. 1 von links;
  • Fig. 3 zeigt einen Horizontalschnitt entsprechend Fig. 1 nach der Linie B-B in Fig. 2;
  • Fig. 4 zeigt einen Horizontalschnitt entsprechend Fig. 1 an einer Stelle oberhalb Fig. 2.
In the drawing, an embodiment of the invention is shown.
  • Fig. 1 shows a horizontal section through the adjacent areas of the fixed frame and the sash along the line AA in Fig. 2;
  • Fig. 2 shows a view of the tape of Figure 1 from the left.
  • Fig. 3 shows a horizontal section corresponding to Figure 1 along the line BB in Fig. 2.
  • FIG. 4 shows a horizontal section corresponding to FIG. 1 at a point above FIG. 2.

In Fig. 1 ist eine als Ganzes mit 100 bezeichnete Bandanordnung wiedergegeben, bei der ein Flügel 20 an einem feststehenden Rahmen 10 mittels mindestens zwei übereinander angeordneter Bänder 50 um eine vertikale Scharnierachse A schwenkbar gelagert ist. Das in der Zeichnung erkennbare Band 50 umfaßt ein Rahmenbandteil 30 und ein Flügelbandteil 40, die ihrerseits jeweils aus einem Befestigungsteil 31 bzw. 41 und einem Scharnierteil 32 bzw. 42 bestehen.1 shows a hinge arrangement designated as a whole by 100, in which a wing 20 is mounted on a fixed frame 10 by means of at least two superposed hinges 50 so that it can pivot about a vertical hinge axis A. The band 50 recognizable in the drawing comprises a frame band part 30 and a wing band part 40, which in turn each consist of a fastening part 31 and 41 and a hinge part 32 and 42 respectively.

Der feststehende Rahmen 10 umfaßt ein Hohlprofil 1 mit einer zur Ebene der Rahmenöffnung parallelen ebenen Vorderseite 2, gegen die das Befestigungsteil 31 des Bandes 30 anliegt und an der es mittels Befestigungsschrauben 3, die durch Bohrungen der Wandung 2 hindurch in ein Befestigungsstück 4 im Innern einer Profilkammer 5 eingreift.The fixed frame 10 comprises a hollow profile 1 with a plane front side 2 parallel to the plane of the frame opening, against which the fastening part 31 of the band 30 rests and to which it is fastened by means of fastening screws 3 which pass through bores in the wall 2 into a fastening piece 4 inside Profile chamber 5 engages.

Das Befestigungsteil 31 kragt von der Wandung 2 vor und geht außen in das Scharnierteil 32 über, welches eine vertikale Bohrung mit der Achse A zur Aufnahme des nicht dargestellten Bandbolzens besitzt.The fastening part 31 protrudes from the wall 2 and merges externally into the hinge part 32, which has a vertical bore with the axis A for receiving the hinge pin, not shown.

In dem Ausführungsbeispiel ist das Band 50 als sogenanntes Scharnierband ausgebildet, d.h. das Rahmenbandteil 30 umfaßt an einem über die Höhe durchgehenden Befestigungsteil 30 zwei mit Abstand übereinander angeordnete Scharnierteile 32,32, zwischen die das Flügelbandteil 40 eingreift. Dies ist aber nur ein Merkmal des Ausführungsbeispiels; es könnte sich auch ein zweiteiliges Band handeln, wobei dann der oberhalb der strichpunktierten Linie in Fig. 2 vorhandene Teil des Bandes fehlen würde.In the exemplary embodiment, the band 50 is designed as a so-called hinge band, i.e. the frame hinge part 30 comprises, on a fastening part 30 which is continuous over the height, two hinge parts 32, 32 which are arranged at a distance one above the other and between which the wing hinge part 40 engages. However, this is only one feature of the exemplary embodiment; it could also be a two-part band, in which case the part of the band present above the dash-dotted line in FIG. 2 would be missing.

Auch das Flügelbandteil 40 umfaßt ein Befestigungsteil 41, das einander parallele vordere und hintere Begrenzungsflächen 44,43 hat und sich unter einem Winkel von etwa 45° von dem Flügel 20 hinweg erstreckt und außen in ein Scharnierteil 42 übergeht, das sich in dem Grundrißbereich der beiden Scharnierteile 32 des Rahmenbandteils 30 erstreckt und ebenfalls von dem nicht dargestellten Bandbolzen durchgriffen werden kann, der über die gesamte Höhe des Rahmenbandteils 30 geht. Wie aus Fig. 1 ersichtlich ist, hat das Befestigungsteil 30 in Höhe des Rahmenbandteils 40 einen etwa dreieckigen Querschnitt, so daß zwischen der Rückseite 43 des Flügelbandteils 40 und der Vorderseite 33 des Rahmenbandteils 30 in diesem Bereich nur ein schmaler Spalt verbleibt.The wing hinge part 40 also comprises a fastening part 41 which has mutually parallel front and rear boundary surfaces 44, 43 and extends at an angle of approximately 45 ° from the wing 20 and merges externally into a hinge part 42 which extends in the plan area of the two Hinge parts 32 of the frame hinge part 30 extends and can also be penetrated by the hinge pin, not shown, which extends over the entire height of the frame hinge part 30. As can be seen from FIG. 1, the fastening part 30 has an approximately triangular cross-section at the level of the frame hinge part 40, so that only a narrow gap remains in this area between the rear 43 of the sash hinge part 40 and the front 33 of the frame hinge part 30.

Der Flügel 20 besitzt einen Rahmen aus einem Hohlprofil 21, von welchem nur der dem feststehenden Rahmen 10 zugewandte Teil gezeichnet ist. Das Hohlprofil 21 weist eine zur Flügelfläche parallele ebene Vorderfläche 22 auf, die um eine Strecke 23 vor der Vorderfläche 2 des feststehenden Rahmens gelegen, d.h. zur Öffnungsseite des Flügels 20 versetzt ist. Das im horizontalen Querschnitt im wesentlichen rechteckige Hohlprofil 21 besitzt nämlich auf der dem feststehenden Rahmen 10 zugewandten Seite im Bereich des Abstandes 23 eine gegen den feststehenden Rahmen hin vorspringende Ausbuchtung 24, durch die ein Falz 25 gebildet ist, der den der lichten Rahmenöffnung zugewandten Randbereich des feststehenden Rahmens 10 übergreift. Der Flügel 20 ist also aufdeckend ausgeführt, und es ist der Abstand 23 das sogenannte Aufdeckmaß.The wing 20 has a frame made of a hollow profile 21, of which only the fixed frame 10 facing part is drawn. The hollow profile 21 has a flat front surface 22 parallel to the wing surface, which is located a distance 23 in front of the front surface 2 of the fixed frame, ie is offset to the opening side of the wing 20. The essentially rectangular hollow profile 21 in horizontal cross-section has on the side facing the fixed frame 10 in the area of the distance 23 a protrusion against the fixed frame bulge 24, through which a fold 25 is formed, the edge area facing the clear frame opening fixed frame 10 engages. The wing 20 is therefore designed to expose and the distance 23 is the so-called uncovering dimension.

Das Befestigungsteil 41 liegt an der äußeren Stirnseite des Falzes 25 an und ist dort durch parallel zur Flügelebene von der Rückseite 43 des Befestigungsteils 41 her eingeschraubte Befestigungsschrauben 45 befestigt, die als Kopfschrauben ausgebildet sind und mit dem Kopf 46 in einer Sackbohrung 47 des Befestigungsteils 41 angeordnet sind. Bei geschlossenem Flügel 20 sind die Befestigungsschrauben 45 in der aus Fig. 1 ersichtlichen Weise unzugänglich. Die Befestigungsschrauben 45 greifen durch fluchtende Bohrungen des Befestigungsteils 41 und der diesem zugewandten Stirnseite 26 des Falzes 25 hindurch in eine Gewindebohrung 48 eines als Ganzes mit 60 bezeichneten Füllstücks ein, welches im Innern des Hohlprofils 21 angeordnet ist.The fastening part 41 lies against the outer end face of the fold 25 and is fastened there by fastening screws 45 screwed in parallel to the wing plane from the rear 43 of the fastening part 41, which screws are designed as cap screws and are arranged with the head 46 in a blind hole 47 of the fastening part 41 are. When the wing 20 is closed, the fastening screws 45 are inaccessible in the manner shown in FIG. 1. The fastening screws 45 engage through aligned bores of the fastening part 41 and the end face 26 of the fold 25 facing them into a threaded bore 48 of a filler piece, designated as a whole by 60, which is arranged in the interior of the hollow profile 21.

Das Füllstück 60 weist auf der dem feststehenden Rahmen zugewandten Seite eine Außenkontur auf, die der dortigen Innenkontur des Hohlprofils 21 gleich ist, so daß sich auf einem großen Flächenbereich eine flächige Anlage ergibt. Das Füllstück 60 erstreckt sich als massives Teil auch in die Tiefe des Hohlprofils 21 bis zur Anlage an der rückwärtigen Wandung 28 des Hohlprofils. Das dortige Teil 61 des Füllstücks 60 ist mit dem Hohlprofil 21 durch zusätzliche zu den Befestigungsschrauben parallele, als Kopfschrauben ausgebildete Befestigungsschrauben 49 verbunden, die von der Schattennut her die dortige Stirnwandung 27 des Hohlprofils 21 duchgreifen.The filler 60 has an outer contour on the side facing the fixed frame, which is the same as the inner contour of the hollow profile 21 there, so that there is a flat contact over a large area. The filler 60 extends as a solid part in the depth of the hollow profile 21 to rest on the rear wall 28 of the hollow profile. The part 61 of the filler 60 there is connected to the hollow profile 21 by means of additional fastening screws 49 which are parallel to the fastening screws and are designed as cap screws, which penetrate the end wall 27 of the hollow profile 21 from the shadow groove.

Das Füllstück 60 erstreckt sich als massives Teil in den Falz 25 hinein und stabilisiert diesen. In diesem Bereich 62 sind auch die Gewindebohrungen 48 vorgesehen. Im Ganzen hat das Füllstück 60 einen etwa T-förmigen Querschnitt, wobei sich der Steg 61 des "T" in die Tiefe erstreckt, die eine Seite 62 des Querbalkens in dem Falz 25 sitzt und sich die andere Seite 63 des Querbalkens an der Rückseite der Vorderwandung 22 des Hohlprofils 21 anliegend eine Strecke weit gegen das Innere des Flügels erstreckt, so daß die Wandung 22 flächig hinterlagert ist.The filler 60 extends as a solid part into the fold 25 and stabilizes it. The threaded holes 48 are also provided in this area 62. Overall, the filler 60 has an approximately T-shaped cross section, the web 61 of the "T" extending in depth, one side 62 of the crossbar in the fold 25 and the other side 63 of the crossbar at the rear of the Front wall 22 of the hollow profile 21 adjacent a distance extends far against the inside of the wing, so that the wall 22 is backed flat.

In dem zentralen Bereich, in welchem die Befestigungsschrauben 45 und 49 nicht verlaufen, ist in dem Ausführungsbeispiel aus Materialersparnisgründen eine Ausnehmung 64 vorgesehen, die beim Strangpressen des Füllstücks 60 aus einem Aluminiumwerkstoff leicht vorgesehen werden kann.In the central region, in which the fastening screws 45 and 49 do not run, a recess 64 is provided in the exemplary embodiment in order to save material, which recess can easily be provided when the filler 60 is extruded from an aluminum material.

Die von dem Befestigungsteil 40 her über die Schrauben 45 in den Falz 25 eingeleiteten Kräfte werden von dem Füllstück 60 auf große Wandungsbereiche des Hohlprofils 21 verteilt und können dadurch übertragen werden, ohne daß es zu unzuträglichen Verformungen der Wandungen des Hohlprofils 21 kommt.The forces introduced into the fold 25 by the fastening part 40 via the screws 45 are distributed by the filler 60 to large wall areas of the hollow profile 21 and can thereby be transmitted without causing undue deformation of the walls of the hollow profile 21.

Im allgemeinen werden für das Flügelbandteil 40 zwei Schrauben 45 übereinander vorgesehen, die in dem Ausführungsbeispiel durch zwei übereinander angeordnete Fixierstifte 55 unterstützt werden, die in der gleichen Ebene angeordnet sind wie die Befestigungsschrauben 45, in das Befestigungsteil 41 eingepreßt sind und spielfrei in Bohrungen 56 in dem in dem Falz 25 sitzenden Teil 62 des Füllstücks 60 eingreifen.In general, two screws 45 are provided one above the other for the wing hinge part 40, which in the exemplary embodiment are supported by two fixing pins 55 arranged one above the other, which are arranged in the same plane as the fastening screws 45, are pressed into the fastening part 41 and are free of play in bores 56 in engage the part 62 of the filler 60 seated in the fold 25.

Fig. 4 zeigte eine Ansicht der Bandanordnung 100 von oben, woraus die praktisch vorhandene vollkommene Ausfüllung des dem feststehenden Rahmen 10 zugewandten Teils des Hohlprofils 21 durch das Füllstück besonders gut erkennbar ist.4 shows a view of the belt arrangement 100 from above, from which the practically existing complete filling of the part of the hollow profile 21 facing the fixed frame 10 by the filler can be seen particularly well.

Claims (7)

  1. Hinge assembly (100) for windows, doors and the like, with a flap and
    with a frame hinge component (30) capable of attachment to a front face (2) of the fixed frame (10) adjacent to the opening in the frame, and extending towards the opening side of the flap (20),
    with a hinge pin defining a hinge axis (A) and seated with a longitudinal portion in a recess in the projecting eye portion (32) of the frame hinge component (30),
    with a flap hinge component (40) attached to the flap (20) with an eye portion extending in the outline region of the eye portion (32) of the frame hinge component (30) with a recess in which another portion of the length of the hinge pin is seated so that the two hinge components (30, 40) are capable of pivoting relative to one another about the hinge axis (A),
    the flap (20) being shaped to engage at its periphery and having a rabbet (25) overlying the adjacent front face (2) of the fixed frame (10), against which the flap hinge component (40) engages from outside and is secured,
       characterised in that,
       the flap (20) has a frame formed by a hollow section (21) forming the rabbet (25) and is provided in the interior of the hollow section (21) at least in the region of the hinge with a filler member (60) of which the external outline in a section perpendicular to the hinge axis (A) is the same as the internal outline of the hollow section (21) in the rabbet (25) and in the adjacent region of the hollow section (21) and it engages flat against the internal profile of the hollow section, and that the flap hinge component (40) is secured by attachment screws (45) passing through holes in the rabbet (25) and engaging in the solid material of the filler member (60).
  2. Hinge assembly according to Claim 1, characterised in that, the flap hinge component (40) extends forwards in an inclined direction from the rabbet (25) towards the eye portion (32) of the frame hinge component (30).
  3. Hinge assembly according to Claim 1 or 2, characterised in that, the attachment screws (45) engage parallel to the face of the flap through the face (26) of the rabbet (25) into the filler member (60).
  4. Hinge assembly according to one of Claims 1 to 3, characterised in that, in addition to the attachment screws (45) there are provided locating dowels (55) parallel to the screws and extending in the attachment portion (41) and engaging through holes in the face (26) of the rabbet (25) into the filler member (60).
  5. Hinge assembly according to one of Claims 1 to 4, characterised in that, additional attachment screws (49) are provided in the portion (61) of the filler member (60) adjacent to the rabbet (25) and extending into the depth of the hollow section (21), screwed in from the shadow groove and pulling together at that region the wall (27) of the hollow section (21) and the portion (61) of the filler member (60).
  6. Hinge assembly according to one of Claims 1 to 5, characterised in that, that the filler member (60) has a projection (63) extending forwards by a distance parallel to the axis of the flap, this projection engaging the back face of the front wall (22) of the hollow section (21).
  7. Hinge assembly according to one of Claims 1 to 6, characterised in that, the filler member is made hollow in that part of the cross-section which is free from attachment screws (45, 49) and locating dowels (55).
EP97111581A 1996-10-14 1997-07-09 Hinge assembly for doors, windows and the like Expired - Lifetime EP0835977B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE29617826U DE29617826U1 (en) 1996-10-14 1996-10-14 Belt arrangement for windows, doors and the like.
DE29617826U 1996-10-14

Publications (2)

Publication Number Publication Date
EP0835977A1 EP0835977A1 (en) 1998-04-15
EP0835977B1 true EP0835977B1 (en) 2000-04-05

Family

ID=8030540

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97111581A Expired - Lifetime EP0835977B1 (en) 1996-10-14 1997-07-09 Hinge assembly for doors, windows and the like

Country Status (5)

Country Link
EP (1) EP0835977B1 (en)
AT (1) ATE191532T1 (en)
DE (2) DE29617826U1 (en)
DK (1) DK0835977T3 (en)
ES (1) ES2145540T3 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE20315041U1 (en) * 2003-09-27 2005-02-17 Niemann, Hans Dieter roll band
CN102648325B (en) * 2009-11-23 2015-09-30 哈恩两合公司 The hinged system of a kind of door, window and similarity piece
DE102018116186B3 (en) * 2018-07-04 2019-07-18 Dr. Hahn Gmbh & Co. Kg Band part of a band

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3685094A (en) * 1970-03-26 1972-08-22 Constantin Goossev Hinge
DE7236335U (en) * 1972-10-03 1973-01-04 Dorma Baubeschlag Gmbh & Co Kg HINGE TAPE FOR DOORS
DE3630234C2 (en) * 1986-09-05 1994-04-28 Simonswerk Gmbh Device for fastening a door or window hinge
FR2666617B1 (en) * 1990-09-11 1993-07-23 Technal Sa PERFECTED HINGE, ESPECIALLY FOR STRUCTURE IN TUBULAR METAL PROFILES.
DE4203486A1 (en) * 1992-02-07 1993-08-12 Bernhard Kreye Rotary bearing arrangement on pane frame of round or oval window - comprises fixed part on which loose part is rotatably held with flat surfaces on outer peripheral surface of hollow profile in application area of loose part aligned to curvature
DE29513102U1 (en) * 1995-08-16 1995-12-14 Rehau Ag & Co Reinforcement profile

Also Published As

Publication number Publication date
DE59701394D1 (en) 2000-05-11
EP0835977A1 (en) 1998-04-15
ATE191532T1 (en) 2000-04-15
DK0835977T3 (en) 2000-08-21
ES2145540T3 (en) 2000-07-01
DE29617826U1 (en) 1998-02-12

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