EP1275804B1 - Corner support for a window, a door or the like - Google Patents

Corner support for a window, a door or the like Download PDF

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Publication number
EP1275804B1
EP1275804B1 EP20020013022 EP02013022A EP1275804B1 EP 1275804 B1 EP1275804 B1 EP 1275804B1 EP 20020013022 EP20020013022 EP 20020013022 EP 02013022 A EP02013022 A EP 02013022A EP 1275804 B1 EP1275804 B1 EP 1275804B1
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EP
European Patent Office
Prior art keywords
leaf
bearing
fixed frame
locking recess
corner
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
EP20020013022
Other languages
German (de)
French (fr)
Other versions
EP1275804A2 (en
EP1275804A3 (en
Inventor
Giovanni Zaccaria
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Roto Frank AG
Original Assignee
Roto Frank AG
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Filing date
Publication date
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Publication of EP1275804A2 publication Critical patent/EP1275804A2/en
Publication of EP1275804A3 publication Critical patent/EP1275804A3/en
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Publication of EP1275804B1 publication Critical patent/EP1275804B1/en
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Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • 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
    • E05D7/0423—Screw-and-nut mechanisms
    • 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
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Type of wing
    • E05Y2900/132—Doors
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Type of wing
    • E05Y2900/148—Windows

Definitions

  • the invention relates to a corner bearing on a window, a door or the like, by means of which a wing is rotatable about a wing rotation axis and tiltable about a copekippachse tilted mounted on a fixed frame and which comprises a wing-side and a festritten workedes Ecklagerelement, of which one as a journal and the other than the bearing journal end bearing bearing cup is formed.
  • Such a corner bearing is known from DE-U-74 26 013 .
  • a wing is provided with a journal and supported on this in the direction of gravity on a fixed frame side bearing part.
  • the Bearing of the wing at a spherical end of the journal which rests on the concave surface of a provided on the fixed frame side bearing part ball cup.
  • the invention is based on the object to further develop the prior art described above in terms of securing the sash bearing on the fixed frame.
  • this object is achieved by a corner bearing according to claim 1.
  • the securing projection mentioned there and the associated securing receptacle cause a mutual support of wings and fixed frame in the transverse direction of the journal. In accordance with directed force on the wing so a leakage of the bearing pin is prevented from the bearing cup. This fact is particularly important in the case of a rotating or tilt-open sash.
  • the security devices according to the invention neither the wing assembly nor the functionality of the mounted on the fixed frame wing. Due to the selected orientation of the securing projection and the resulting opening direction of the fuse holder, the wing can rather be mounted on the fixed frame during installation by movement in the direction of the bearing journal or the wing rotational axis. In the transverse direction of the main plane of the wing and fixed frame Between the securing projection and the wall of the fuse holder existing game allows to tilt the wing regardless of the securing elements around the rempligelkippachse.
  • claim 2 relates to a Erfindungsbauart, in the case of which the excess of the fuse holder against the securing projection is minimized parallel to the main plane of the wing and fixed frame.
  • the securing projection extends in the wing axis of rotation and consequently describes a circular arc with a relatively small diameter when the wing is opened in rotation with its outer wall extending in the axial direction.
  • the limits of the fuse holder parallel to the main plane of the wing and the fixed frame can in such circumstances approach close to the securing projection.
  • the achieved over the securing projection and the fuse holder securing the journal against leakage from the bearing cup is thus effective even at extremely small displacement of the wing in the direction mentioned.
  • the corner bearing according to claim 3 is characterized by the design of the fuse holder selected by a constructive, in particular production technology simple design.
  • the freedom of movement of the wing relative to the fixed frame to the opening side of the wing is kept low.
  • An undesirable displacement of the wing to the opening side is effectively avoided.
  • the Kipphneschafts-, as well as the rotary readiness position wing may optionally by an effective in this direction wing flap on the fixed frame against unwanted displacement and thus be supported against leakage of the journal from the bearing cup.
  • wing-side corner bearing part 1 To mount the wing-side corner bearing part 1 is mounted on a merely suggestively illustrated wing 5 of a window and thereby on the right vertical spar of the casement.
  • a rollover leg 6 of the Eckbandwinkels 2 extends along a sash overlap 7 at its side facing away from the interior of the room outside.
  • a folding leg 8 of the Eckbandwinkels 2 rests on a die gelfalz Structure 9.
  • the Eckbandwinkel 2 can be screwed to its folding leg 8 with the attachment piece 4.
  • the attachment piece 4 in turn is fixed as usual in an undercut fitting part 11 of the wing 5.
  • the journal 3 has a cylindrical shaft 12 and a hemispherical lower end 13. From the latter projects centrally a mandrel-like and with respect to the shaft 12 of the journal 3 diameter-reduced securing projection 14 before. This is arranged coaxially with a defined by the bearing pin 3 wing pivot axis 15.
  • wing-side corner bearing part 1 Assigned to the wing-side corner bearing part 1 is a fixed-frame-side corner bearing part 18, as in detail the FIGS. 2 and 3 can be removed.
  • the fixed-frame-side corner-bearing part 18 is attached to the lower-right corner of a fixed frame 19 of a window. It is based as usual on a lower horizontal spar of the fixed frame 19 and is bolted to a folding leg 20 with a vertical compassionholm.
  • a support leg 21 of the fixed frame side corner bearing member 18 is in installation position on the interior space of the fixed frame 19 and extends there parallel to a main plane 22 of the fixed frame 19, which coincides with the wing located in tilting and in Drehrschaftswolf befindlichem wing 5 with the main plane ,
  • a projection 23 Formed on the inner side of the support leg 21 is a projection 23 with a cross-sectionally substantially rectangular, upwardly open receiving chamber 24.
  • a bearing cup 25 is inserted, which has a concave bearing surface 27 in addition to a base body 26.
  • the main body 26 of the bearing cup 25 is provided with a threaded bore 28 which extends parallel to the main plane 22 of the fixed frame 19 and into which an adjusting screw 29 engages, which in turn is rotatably held on opposite walls of the receiving chamber 24 but immovable in the axial direction , By means of the adjusting screw 29, the bearing cup 25 can be adjusted in the interior of the receiving chamber 24 parallel to the main plane 22 of the fixed frame 19.
  • the bearing cup 25 is provided by means of a on its base body 26 Guide bar 30 is guided on the projection 23. Together with the bearing pin 3, the bearing cup 25 defines not only the wing rotation axis 15 but also a wing tilt axis 32.
  • a slot-like fuse holder 31 is inserted in the bearing surface 27 of the bearing cup 25 in the bearing surface 27 of the bearing cup 25 in the bearing surface 27 of the bearing cup 25 in the bearing surface 27 of the bearing cup 25 in the bearing surface 27 of the bearing cup 25.
  • the transverse to the main plane 22 extending longitudinal axis of the fuse holder 31 is located in the corresponding median plane of the bearing surface 27 on the bearing cup 25.
  • the longitudinal center of the fuse holder 31 is opposite to the center of Storage surface 27 offset to the fixed frame 19 out.
  • FIG. 4 The conditions when mounted on the fixed frame 19 and with respect to this a tilting occupy wing 5 are in FIG. 4 shown.
  • the wing-side securing projection 14 emerges with mounted wing 5 in the longitudinal direction of the bearing pin 3 in the fixed-frame-side fuse holder 31 a. Due to the corresponding dimensioning of the lower end 13 of the wing-side journal 3 and the bearing surface 27 on the fixed frame side bearing cup 25, the lower end 13 of the journal 3 is supported in the closed position and Kipprschafts-, at Drehrschafts- and in Drehö réelleswolf of the wing 5 self-centering on the Bearing surface 27 of the bearing cup 25 in the direction of gravity from.
  • the width of the fuse holder 31 parallel to the main plane 22 of the fixed frame 19 exceeds the corresponding dimension, i. the diameter of the securing projection 14 only slightly.
  • the transverse to the main plane 22 extending wall parts of the fuse holder 31 are therefore in the immediate vicinity of the securing projection 14th
  • the wing 5 can move under the action of force parallel to its main plane and upon application of force on its the room outside side associated only over an extremely short distance, until the securing projection 14th strikes the wall of the fuse holder 31 and thereby further displacement of the wing 5 is prevented.
  • Kipp holeschafts- and rotation readiness position on the wing flap 7 on the fixed frame 19 From.
  • the existing in the transverse direction of the main plane 22 between the fixed frame side longitudinal boundary of the fuse holder 31 and the securing projection 14 game is chosen such that the wing 5 with continued immersion of the locking projection 14 in the fuse holder 31 from its closed or Kipphneschaftswolf in a tilted position relative to the fixed Frame 19 can be transferred. Also, the tilt-open wing 5 ( FIG. 4 ) is secured by the above-described interaction of securing projection 14 and securing receptacle 31 against unintentional displacement parallel and perpendicular to the main plane 22 of the fixed frame 19.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)

Abstract

The corner edge bearing has a bearing pin (3) and a bearing seat (25) respectively associated with the door or window panel (5) and the surrounding frame (19), allowing the door or window panel to rotate about a first axis and tip about a second axis. The bearing pin and the bearing seat have a cooperating projection (14) and recess (31), allowing relative movement of the bearing pin and the bearing seat during the rotation and tipping movement of the door or window panel, but preventing removal of the bearing pin from the bearing seat. -

Description

Die Erfindung betrifft ein Ecklager an einem Fenster, einer Tür oder dergleichen, mittels dessen ein Flügel um eine Flügeldrehachse drehbar und um eine Flügelkippachse kippbar an einem festen Rahmen gelagert ist und welches ein flügelseitiges sowie ein festrahmenseitiges Ecklagerelement umfasst, von denen das eine als Lagerzapfen und das andere als den Lagerzapfen stirnseitig lagernde Lagerpfanne ausgebildet ist.The invention relates to a corner bearing on a window, a door or the like, by means of which a wing is rotatable about a wing rotation axis and tiltable about a Flügelkippachse tilted mounted on a fixed frame and which comprises a wing-side and a festrahmenseitiges Ecklagerelement, of which one as a journal and the other than the bearing journal end bearing bearing cup is formed.

Ein derartiges Ecklager ist bekannt aus DE-U-74 26 013 . Im Falle des Standes der Technik ist ein Flügel mit einem Lagerzapfen versehen und über diesen in Schwerkraftrichtung an einem festrahmenseitigen Lagerteil abgestützt. Im Einzelnen erfolgt die Lagerung des Flügels an einem balligen Ende des Lagerzapfens, das auf der konkaven Fläche einer an dem festrahmenseitigen Lagerteil vorgesehenen Kugelschale aufsetzt. Mittels Lagerzapfenende und Kugelschale werden so die Flügeldreh- sowie die Flügelkippachse definiert.Such a corner bearing is known from DE-U-74 26 013 , In the case of the prior art, a wing is provided with a journal and supported on this in the direction of gravity on a fixed frame side bearing part. In detail, the Bearing of the wing at a spherical end of the journal, which rests on the concave surface of a provided on the fixed frame side bearing part ball cup. By means of the end of the journal and the spherical shell, the wing turning and wing tilting axes are defined.

Der Erfindung liegt nun die Aufgabe zugrunde, den vorstehend beschriebenen Stand der Technik im Sinne einer Sicherung der Flügellagerung an dem festen Rahmen weiterzubilden.The invention is based on the object to further develop the prior art described above in terms of securing the sash bearing on the fixed frame.

Erfindungsgemäß gelöst wird diese Aufgabe durch ein Ecklager gemäß Anspruch 1. Der dort genannte Sicherungsvorsprung und die zugeordnete Sicherungsaufnahme bewirken eine gegenseitige Abstützung von Flügel und festem Rahmen in Querrichtung des Lagerzapfens. Bei entsprechend gerichteter Krafteinwirkung auf den Flügel wird so ein Austreten des Lagerzapfens aus der Lagerpfanne verhindert. Dieser Umstand ist insbesondere bei dreh- oder kippgeöffnetem Flügel von Bedeutung. Gleichzeitig behindern die erfindungsgemäßen Sicherungseinrichtungen weder die Flügelmontage noch die Funktionsfähigkeit des an dem festen Rahmen montierten Flügels. Aufgrund der gewählten Ausrichtung des Sicherungsvorsprungs und der daraus resultierenden Öffnungsrichtung der Sicherungsaufnahme lässt sich der Flügel vielmehr beim Einbau durch eine Bewegung in Richtung des Lagerzapfens bzw. der Flügeldrehachse an dem festen Rahmen lagern. Das in Querrichtung der Hauptebene von Flügel und festem Rahmen zwischen dem Sicherungsvorsprung und der Wandung der Sicherungsaufnahme bestehende Spiel erlaubt es, den Flügel ungeachtet der Sicherungselemente um die Flügelkippachse zu kippen.According to the invention, this object is achieved by a corner bearing according to claim 1. The securing projection mentioned there and the associated securing receptacle cause a mutual support of wings and fixed frame in the transverse direction of the journal. In accordance with directed force on the wing so a leakage of the bearing pin is prevented from the bearing cup. This fact is particularly important in the case of a rotating or tilt-open sash. At the same time hinder the security devices according to the invention neither the wing assembly nor the functionality of the mounted on the fixed frame wing. Due to the selected orientation of the securing projection and the resulting opening direction of the fuse holder, the wing can rather be mounted on the fixed frame during installation by movement in the direction of the bearing journal or the wing rotational axis. In the transverse direction of the main plane of the wing and fixed frame Between the securing projection and the wall of the fuse holder existing game allows to tilt the wing regardless of the securing elements around the Flügelkippachse.

Besondere Ausführungsarten der Erfindung gemäß Anspruch 1 ergeben sich aus den abhängigen Ansprüchen 2 bis 5.Particular embodiments of the invention according to claim 1 emerge from the dependent claims 2 to 5.

Dabei betrifft Anspruch 2 eine Erfindungsbauart, im Falle derer das Übermaß der Sicherungsaufnahme gegenüber dem Sicherungsvorsprung parallel zu der Hauptebene von Flügel und festem Rahmen minimiert ist. Ermöglicht wird dies durch den Umstand, dass der Sicherungsvorsprung in der Flügeldrehachse verläuft und folglich beim Drehöffnen des Flügels mit seiner in Achsrichtung verlaufenden Außenwand einen Kreisbogen mit relativ kleinem Durchmesser beschreibt. Die Begrenzungen der Sicherungsaufnahme parallel zu der Hauptebene von Flügel und festem Rahmen können unter diesen Umständen nahe an den Sicherungsvorsprung heranrücken. Die über den Sicherungsvorsprung und die Sicherungsaufnahme erzielte Sicherung des Lagerzapfens gegen Austreten aus der Lagerpfanne wird somit bereits bei äußerst geringfügiger Verlagerung des Flügels in der genannten Richtung wirksam.In this case, claim 2 relates to a Erfindungsbauart, in the case of which the excess of the fuse holder against the securing projection is minimized parallel to the main plane of the wing and fixed frame. This is made possible by the fact that the securing projection extends in the wing axis of rotation and consequently describes a circular arc with a relatively small diameter when the wing is opened in rotation with its outer wall extending in the axial direction. The limits of the fuse holder parallel to the main plane of the wing and the fixed frame can in such circumstances approach close to the securing projection. The achieved over the securing projection and the fuse holder securing the journal against leakage from the bearing cup is thus effective even at extremely small displacement of the wing in the direction mentioned.

Das Ecklager nach Anspruch 3 zeichnet sich infolge der gewählten Ausbildung der Sicherungsaufnahme durch eine konstruktiv, insbesondere fertigungstechnisch einfache Ausgestaltung aus.The corner bearing according to claim 3 is characterized by the design of the fuse holder selected by a constructive, in particular production technology simple design.

Im Falle der Erfindungsvariante nach Anspruch 4 ist die Bewegungsfreiheit des Flügels gegenüber dem festen Rahmen zu der Öffnungsseite des Flügels hin gering gehalten. Eine unerwünschte Verlagerung des Flügels zu der Öffnungsseite hin wird dadurch wirksam vermieden. In Gegenrichtung, in welcher die Sicherungsaufnahme ein verhältnismäßig großes Übermaß gegenüber dem Sicherungsvorsprung aufweist, kann jedenfalls der in der Schließ-, der Kippbereitschafts-, sowie der Drehbereitschaftsstellung befindliche Flügel gegebenenfalls durch einen in dieser Richtung wirksamen Flügelüberschlag an dem festen Rahmen gegen unerwünschte Verlagerung und somit gegen Austreten des Lagerzapfens aus der Lagerpfanne abgestützt werden.In the case of the variant of the invention according to claim 4, the freedom of movement of the wing relative to the fixed frame to the opening side of the wing is kept low. An undesirable displacement of the wing to the opening side is effectively avoided. In the opposite direction, in which the fuse holder has a relatively large excess compared to the securing projection, located in the closing, the Kippbereitschafts-, as well as the rotary readiness position wing may optionally by an effective in this direction wing flap on the fixed frame against unwanted displacement and thus be supported against leakage of the journal from the bearing cup.

An dem erfindungsgemäßen Ecklager gemäß Anspruch 5 finden sich mehrere der vorstehend beschriebenen vorteilhaften Einzelmerkmale. Es ergibt sich so eine Erfindungsbauart, welche die vorstehenden Vorzüge in sich vereint. Aufgrund des beschriebenen Versatzes der Längsmitte der Sicherungsaufnahme gegenüber der Flügeldrehachse befindet sich die Wandung der Sicherungsaufnahme öffnungsseitig nahe bei dem Sicherungsvorsprung.At the corner bearing according to the invention according to claim 5, there are several of the advantageous individual features described above. This results in a Erfindungsbauart, which combines the above advantages in itself. Due to the described offset of the longitudinal center of the securing receptacle relative to the wing axis of rotation, the wall of the securing receptacle is located on the opening side close to the securing projection.

Nachstehend wird die Erfindung anhand schematischer Darstellungen zu einem Ausführungsbeispiel näher erläutert. Es zeigen:

Fig. 1
ein Ecklagerteil an einem Flügel eines Fensters in der Draufsicht auf die Flügelhauptebene von der Fensteraußenseite her,
Fig. 2
ein dem Ecklagerteil nach Fig. 1 zugeordnetes festrahmenseitiges Ecklagerteil in der Draufsicht von oben,
Fig. 3
eine Schnittdarstellung des Ecklagerteils nach Fig. 2 mit dem durch die Linie III-III in Fig. 2 angedeuteten Schnittverlauf,
Fig. 4
ein Ecklager mit den Ecklagerteilen nach den Fign. 1 bis 3 in Einbaulage.
The invention will be explained in more detail with reference to schematic representations of an embodiment. Show it:
Fig. 1
a Ecklagerteil on a wing of a window in the plan view of the wing main plane from the window outside,
Fig. 2
after the corner bearing part Fig. 1 associated fixed frame side Ecklagerteil in plan view from above,
Fig. 3
a sectional view of the corner bearing part Fig. 2 with the line III-III in Fig. 2 indicated cutting process,
Fig. 4
a corner bearing with the corner bearing parts after the FIGS. 1 to 3 in installation position.

Gemäß Fig. 1 umfasst ein flügelseitiges Ecklagerteil 1 einen Eckbandwinkel 2, einen davon nach unten vorstehenden Lagerzapfen 3 sowie ein Befestigungsstück 4. Zu montieren ist das flügelseitige Ecklagerteil 1 an einem lediglich andeutungsweise dargestellten Flügel 5 eines Fensters und dabei an dem rechten Vertikalholm des Flügelrahmens.According to Fig. 1 To mount the wing-side corner bearing part 1 is mounted on a merely suggestively illustrated wing 5 of a window and thereby on the right vertical spar of the casement.

Im eingebauten Zustand erstreckt sich ein Überschlagschenkel 6 des Eckbandwinkels 2 entlang eines Flügelüberschlags 7 an dessen vom Rauminnern abgewandten Außenseite. Ein Falzschenkel 8 des Eckbandwinkels 2 liegt auf einer Flügelfalzfläche 9 auf.When installed, a rollover leg 6 of the Eckbandwinkels 2 extends along a sash overlap 7 at its side facing away from the interior of the room outside. A folding leg 8 of the Eckbandwinkels 2 rests on a Flügelfalzfläche 9.

Mittels Befestigungsschrauben 10 lässt sich der Eckbandwinkel 2 an seinem Falzschenkel 8 mit dem Befestigungsstück 4 verschrauben. Das Befestigungsstück 4 wiederum ist wie üblich in einer hinterschnittenen Beschlagteilnut 11 des Flügels 5 fixiert.By means of fastening screws 10, the Eckbandwinkel 2 can be screwed to its folding leg 8 with the attachment piece 4. The attachment piece 4 in turn is fixed as usual in an undercut fitting part 11 of the wing 5.

Der Lagerzapfen 3 besitzt einen zylindrischen Schaft 12 sowie ein halbkugelförmiges unteres Ende 13. Von Letzterem ragt zentral ein dornartiger und gegenüber dem Schaft 12 des Lagerzapfens 3 durchmesserreduzierter Sicherungsvorsprung 14 vor. Dieser ist koaxial mit einer von dem Lagerzapfen 3 definierten Flügeldrehachse 15 angeordnet.The journal 3 has a cylindrical shaft 12 and a hemispherical lower end 13. From the latter projects centrally a mandrel-like and with respect to the shaft 12 of the journal 3 diameter-reduced securing projection 14 before. This is arranged coaxially with a defined by the bearing pin 3 wing pivot axis 15.

Mit seinem von dem unteren Ende 13 abliegenden Teil ist der Lagerzapfen 3 im Innern einer in Richtung der Flügeldrehachse 15 verlaufenden Eckbandhülse 16 aufgenommen. Diese ist an ihrem oberen Ende in gewohnter Weise mit einer Kappe 17 verschlossen. Von dem Flügelüberschlag 7 stehen die Eckbandhülse 16 sowie der Lagerzapfen 3 seitlich sowie zu der Rauminnenseite des Flügels 5 hin vor.With its remote from the lower end 13 part of the bearing pin 3 is received in the interior of a running in the direction of the wing pivot axis 15 Eckbandhülse 16. This is closed at its upper end in the usual way with a cap 17. Of the wing flap 7 are the Eckbandhülse 16 and the bearing pin 3 laterally and to the interior of the wing 5 out.

Dem flügelseitigen Ecklagerteil 1 zugeordnet ist ein festrahmenseitiges Ecklagerteil 18, wie es im Einzelnen den Figuren 2 und 3 entnommen werden kann.Assigned to the wing-side corner bearing part 1 is a fixed-frame-side corner bearing part 18, as in detail the FIGS. 2 and 3 can be removed.

Ausweislich Figur 2 ist das festrahmenseitige Ecklagerteil 18 an der unteren rechten Ecke eines festen Rahmens 19 eines Fensters angebracht. Es stützt sich dabei wie üblich auf einem unteren horizontalen Holm des festen Rahmens 19 ab und ist an einem Falzschenkel 20 mit einem vertikalen Rahmenholm verschraubt. Ein Auflageschenkel 21 des festrahmenseitigen Ecklagerteils 18 liegt in Einbaulage auf der Rauminnenseite des festen Rahmens 19 auf und erstreckt sich dort parallel zu einer Hauptebene 22 des festen Rahmens 19, die bei geschlossenem sowie bei in Kippbereitschafts- und in Drehbereitschaftsstellung befindlichem Flügel 5 mit dessen Hauptebene zusammenfällt.evidenced FIG. 2 For example, the fixed-frame-side corner-bearing part 18 is attached to the lower-right corner of a fixed frame 19 of a window. It is based as usual on a lower horizontal spar of the fixed frame 19 and is bolted to a folding leg 20 with a vertical Rahmenholm. A support leg 21 of the fixed frame side corner bearing member 18 is in installation position on the interior space of the fixed frame 19 and extends there parallel to a main plane 22 of the fixed frame 19, which coincides with the wing located in tilting and in Drehbereitschaftsstellung befindlichem wing 5 with the main plane ,

Rauminnenseitig an den Auflageschenkel 21 angeformt ist ein Ansatz 23 mit einer im Querschnitt im Wesentlichen rechteckigen, nach oben offenen Aufnahmekammer 24. In diese ist eine Lagerpfanne 25 eingesetzt, die neben einem Grundkörper 26 eine konkave Lagerfläche 27 aufweist. Der Grundkörper 26 der Lagerpfanne 25 ist mit einer Gewindebohrung 28 versehen, die sich parallel zu der Hauptebene 22 des festen Rahmens 19 erstreckt und in die eine Stellschraube 29 eingreift, die ihrerseits an einander gegenüberliegenden Wänden der Aufnahmekammer 24 drehbar aber in axialer Richtung unverschiebbar gehalten wird. Mittels der Stellschraube 29 lässt sich die Lagerpfanne 25 im Innern der Aufnahmekammer 24 parallel zu der Hauptebene 22 des festen Rahmens 19 verstellen. Bei der Verstellbewegung wird die Lagerpfanne 25 mittels einer an ihrem Grundkörper 26 vorgesehenen Führungsleiste 30 an dem Ansatz 23 geführt. Gemeinsam mit dem Lagerzapfen 3 definiert die Lagerpfanne 25 neben der Flügeldrehachse 15 auch eine Flügelkippachse 32.Formed on the inner side of the support leg 21 is a projection 23 with a cross-sectionally substantially rectangular, upwardly open receiving chamber 24. In this is a bearing cup 25 is inserted, which has a concave bearing surface 27 in addition to a base body 26. The main body 26 of the bearing cup 25 is provided with a threaded bore 28 which extends parallel to the main plane 22 of the fixed frame 19 and into which an adjusting screw 29 engages, which in turn is rotatably held on opposite walls of the receiving chamber 24 but immovable in the axial direction , By means of the adjusting screw 29, the bearing cup 25 can be adjusted in the interior of the receiving chamber 24 parallel to the main plane 22 of the fixed frame 19. During the adjustment movement, the bearing cup 25 is provided by means of a on its base body 26 Guide bar 30 is guided on the projection 23. Together with the bearing pin 3, the bearing cup 25 defines not only the wing rotation axis 15 but also a wing tilt axis 32.

In die Lagerfläche 27 der Lagerpfanne 25 ist eine langlochartige Sicherungsaufnahme 31 eingelassen. Diese erstreckt sich mit ihrer Längsrichtung in Querrichtung der Hauptebene 22 des festen Rahmens 19. Die quer zu der Hauptebene 22 verlaufende Längsachse der Sicherungsaufnahme 31 liegt in der entsprechenden Mittelebene der Lagerfläche 27 an der Lagerpfanne 25. Die Längsmitte der Sicherungsaufnahme 31 ist gegenüber dem Zentrum der Lagerfläche 27 zu dem festen Rahmen 19 hin versetzt.In the bearing surface 27 of the bearing cup 25 is a slot-like fuse holder 31 is inserted. This extends with its longitudinal direction in the transverse direction of the main plane 22 of the fixed frame 19. The transverse to the main plane 22 extending longitudinal axis of the fuse holder 31 is located in the corresponding median plane of the bearing surface 27 on the bearing cup 25. The longitudinal center of the fuse holder 31 is opposite to the center of Storage surface 27 offset to the fixed frame 19 out.

Die Verhältnisse bei an dem festen Rahmen 19 montiertem und gegenüber diesem eine Kippstellung einnehmendem Flügel 5 sind in Figur 4 dargestellt. Der flügelseitige Sicherungsvorsprung 14 taucht bei montiertem Flügel 5 in Längsrichtung des Lagerzapfens 3 in die festrahmenseitige Sicherungsaufnahme 31 ein. Aufgrund der einander entsprechenden Dimensionierung des unteren Endes 13 des flügelseitigen Lagerzapfens 3 und der Lagerfläche 27 an der festrahmenseitigen Lagerpfanne 25 stützt sich das untere Ende 13 des Lagerzapfens 3 bei Schließlage sowie bei Kippbereitschafts-, bei Drehbereitschafts- und bei Drehöffnungsstellung des Flügels 5 selbstzentrierend auf der Lagerfläche 27 der Lagerpfanne 25 in Schwerkraftrichtung ab. Die Zentren der Lagerfläche 27 an der Lagerpfanne 25 und des Endes 13 an dem Lagerzapfen 3 fallen dementsprechend bei den genannten Flügelstellungen miteinander zusammen und liegen in der Flügeldrehachse 15. Aufgrund des vorstehend beschriebenen Versatzes der Längsmitte der Sicherungsaufnahme 31 gegenüber dem Zentrum der Lagerfläche 27 an der Lagerpfanne 25 ergibt sich somit ein entsprechender Versatz der Längsmitte der Sicherungsaufnahme 31 gegenüber dem Zentrum des unteren Endes 13 an dem Lagerzapfen 3 und folglich gegenüber der Flügeldrehachse 15 und dem damit konzentrischen Sicherungsvorsprung 14. Bei Schließlage, Kippbereitschafts-, Drehbereitschafts- und Drehöffnungsstellung des Flügels 5 ist dementsprechend der Sicherungsvorsprung 14 nahe der von dem festen Rahmen 19 abliegenden, öffnungsseitigen Längsbegrenzung der Sicherungsaufnahme 31 angeordnet.The conditions when mounted on the fixed frame 19 and with respect to this a tilting occupy wing 5 are in FIG. 4 shown. The wing-side securing projection 14 emerges with mounted wing 5 in the longitudinal direction of the bearing pin 3 in the fixed-frame-side fuse holder 31 a. Due to the corresponding dimensioning of the lower end 13 of the wing-side journal 3 and the bearing surface 27 on the fixed frame side bearing cup 25, the lower end 13 of the journal 3 is supported in the closed position and Kippbereitschafts-, at Drehbereitschafts- and in Drehöffnungsstellung of the wing 5 self-centering on the Bearing surface 27 of the bearing cup 25 in the direction of gravity from. The centers of the bearing surface 27 on the bearing cup 25 and the end 13 at the Due to the above-described offset of the longitudinal center of the fuse holder 31 relative to the center of the bearing surface 27 on the bearing cup 25, this results in a corresponding offset of the longitudinal center of the fuse holder 31 with respect to the In the closed position, Kippbereitschafts-, Drehbereitschafts- and rotational opening position of the wing 5 is accordingly the securing projection 14 close to the remote from the fixed frame 19, the opening side center of the lower end 13 on the bearing pin 3 and thus with respect to the wing rotation axis 15 and the concentric Longitudinal limitation of the fuse holder 31 is arranged.

Gleichzeitig übersteigt die Weite der Sicherungsaufnahme 31 parallel zu der Hauptebene 22 des festen Rahmens 19 die entsprechende Abmessung, d.h. den Durchmesser des Sicherungsvorsprungs 14 nur geringfügig. Auch die quer zu der Hauptebene 22 verlaufenden Wandungsteile der Sicherungsaufnahme 31 befinden sich daher in unmittelbarer Nachbarschaft des Sicherungsvorsprungs 14.At the same time, the width of the fuse holder 31 parallel to the main plane 22 of the fixed frame 19 exceeds the corresponding dimension, i. the diameter of the securing projection 14 only slightly. The transverse to the main plane 22 extending wall parts of the fuse holder 31 are therefore in the immediate vicinity of the securing projection 14th

Alles in allem kann sich der Flügel 5 unter Krafteinwirkung parallel zu seiner Hauptebene sowie bei Krafteinwirkung auf seine der Raumaußenseite zugeordneten Seite nur über eine äußerst kurze Distanz verlagern, bis der Sicherungsvorsprung 14 an der Wandung der Sicherungsaufnahme 31 anschlägt und dadurch eine weitergehende Verlagerung des Flügels 5 verhindert wird. Bei senkrecht zu seiner Hauptebene zu der Raumaußenseite hin gerichteter Krafteinwirkung stützt sich der Flügel 5 bei Schließlage, Kippbereitschafts- und Drehbereitschaftsstellung über den Flügelüberschlag 7 an dem festen Rahmen 19 ab.All in all, the wing 5 can move under the action of force parallel to its main plane and upon application of force on its the room outside side associated only over an extremely short distance, until the securing projection 14th strikes the wall of the fuse holder 31 and thereby further displacement of the wing 5 is prevented. When directed perpendicular to its main plane to the outside of the room toward force application of the wing 5 is supported in the closed position, Kippbereitschafts- and rotation readiness position on the wing flap 7 on the fixed frame 19 from.

Das in Querrichtung der Hauptebene 22 zwischen der festrahmenseitigen Längsbegrenzung der Sicherungsaufnahme 31 und dem Sicherungsvorsprung 14 bestehende Spiel ist derart gewählt, dass der Flügel 5 unter fortgesetztem Eintauchen des Sicherungsvorsprungs 14 in die Sicherungsaufnahme 31 aus seiner Schließ- bzw. Kippbereitschaftsstellung in eine Kippstellung gegenüber dem festen Rahmen 19 überführt werden kann. Auch der kippgeöffnete Flügel 5 (Figur 4) ist durch das vorstehend beschriebene Zusammenwirken von Sicherungsvorsprung 14 und Sicherungsaufnahme 31 gegen unbeabsichtigte Verlagerung parallel und senkrecht zu der Hauptebene 22 des festen Rahmens 19 gesichert.The existing in the transverse direction of the main plane 22 between the fixed frame side longitudinal boundary of the fuse holder 31 and the securing projection 14 game is chosen such that the wing 5 with continued immersion of the locking projection 14 in the fuse holder 31 from its closed or Kippbereitschaftsstellung in a tilted position relative to the fixed Frame 19 can be transferred. Also, the tilt-open wing 5 ( FIG. 4 ) is secured by the above-described interaction of securing projection 14 and securing receptacle 31 against unintentional displacement parallel and perpendicular to the main plane 22 of the fixed frame 19.

Claims (5)

  1. Corner support for a window, a door or the like, by means of which a leaf (5) is mounted on a fixed frame (19) in a manner rotatable about a leaf rotation axis (15) and tiltable about a leaf tilt axis (32), and which comprises a corner bearing element on the leaf side and a corner bearing element on the fixed frame side, of which the one is formed as a bearing pin (3) and the other as a bearing seat (25) which defines the leaf rotation axis (15) and the leaf tilt axis (32) and has a concave bearing surface (27) and supports thereon a hemispherical end (13) of the bearing pin (3) on the face, characterised in that firstly a locking protrusion (14) is provided at the hemispherical end (13) of the bearing pin (3) facing the other corner bearing element and a locking recess (31) is provided at the other side of the bearing seat on the side facing the one bearing corner element, wherein when the leaf (5) is in the position ready for rotation
    • the locking protrusion (14) runs in the direction of the leaf rotation axis (15) and engages in this direction in the locking recess (31) with a play which exists at the opening of the locking recess (31) in the transverse direction of the main plane (22) of the leaf (5) and the fixed frame (19), and
    • the concave bearing surface (27) of the bearing seat (25) supports the end (13) of the bearing pin (3) in a self-centring manner when the locking protrusion (14) engages in the locking recess (31),
    and wherein the bearing pin (3) and the bearing seat (25) are movable relative to each other when the locking protrusion (14) engages further in the locking recess (31), with the relative movements associated with the rotational movement and the tilting movement of the leaf (5), and can rest on each other via the locking protrusion (14) and a wall of the locking recess (31) in the transverse direction of the bearing pin (3), preventing the removal of the bearing pin (3) from the bearing seat (25).
  2. Corner bearing according to claim 1, characterised in that when the leaf (5) is in the position ready for rotation, the locking protrusion (14) runs in the leaf rotation axis (15) and the locking recess (31) runs with its longitudinal direction in the transverse direction of the main plane (22) of the leaf (5) and the fixed frame (19), wherein the width of the locking recess (31) parallel to the main plane (22) of the leaf (5) and the fixed frame (19) corresponds to the extent of the locking protrusion (14) in this direction or slightly exceeds this extent.
  3. Corner bearing according to any one of the preceding claims, characterised in that the locking recess (31) is formed as a slot running with its longitudinal direction in the transverse direction of the main plane (22) of the leaf (5) and the fixed frame (19).
  4. Corner bearing according to any one of the preceding claims, characterised in that the locking protrusion (14) is provided on the leaf side and the locking recess (31) on the fixed frame side, and the leaf (5) can rotate and tilt relative to the fixed frame (19) towards an opening side, and that a wall of the locking recess (31) is closely adjacent to the locking protrusion (14) on the opening side.
  5. Corner bearing according to any one of the preceding claims, characterised in that the locking protrusion (14) is provided on the leaf side and runs in the leaf rotation axis (15) when the leaf (5) is in the position ready for rotation, that the locking recess (31) is formed as a slot provided on the fixed frame (19) and there extending with its longitudinal direction in the transverse direction of the main plane (22) of the leaf (5) and the fixed frame (19), that the leaf (5) can rotate and tilt relative to the fixed frame (19) towards an opening side, and that finally the locking recess (31) is arranged with its longitudinal centre offset to the fixed frame (19) in relation to the leaf rotation axis (15).
EP20020013022 2001-07-09 2002-06-13 Corner support for a window, a door or the like Expired - Lifetime EP1275804B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE2001133226 DE10133226C1 (en) 2001-07-09 2001-07-09 Corner edge bearing, for door or window, has bearing pin and bearing seat provided with cooperating projection and recess allowing limited relative movement
DE10133226 2001-07-09

Publications (3)

Publication Number Publication Date
EP1275804A2 EP1275804A2 (en) 2003-01-15
EP1275804A3 EP1275804A3 (en) 2007-11-07
EP1275804B1 true EP1275804B1 (en) 2013-10-23

Family

ID=7691123

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20020013022 Expired - Lifetime EP1275804B1 (en) 2001-07-09 2002-06-13 Corner support for a window, a door or the like

Country Status (3)

Country Link
EP (1) EP1275804B1 (en)
DE (1) DE10133226C1 (en)
ES (1) ES2439092T3 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009004846B3 (en) * 2009-01-16 2009-12-10 Sfs Intec Holding Ag Hinge for a door comprises a holder formed as a two-sided angled piece with an angled apex running parallel to the rotary axis of the hinge

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE7426013U (en) * 1974-10-31 Gretsch & Co Gmbh Drill-in hinge for tilt and turn bearings with holding plate below
FR1377934A (en) * 1963-12-26 1964-11-06 Corner joint for revolving and tilting windows
FR2306322A1 (en) * 1975-04-04 1976-10-29 Ferco Usine Ferrures Stop mechanism for tilting and rotating windows - has wedge on corner bearings engaging with safety stops on hinge
DE3022899A1 (en) * 1980-06-19 1981-12-24 Julius & August Erbslöh GmbH + Co, 5600 Wuppertal Turn and tilt window fitting corner bearing - has adjusting screws in threaded hole, for bearing an in slot pin
IT1164604B (en) * 1983-01-28 1987-04-15 Slim Soc Lavora Ind Metalli LOWER HINGE OF ROTATION AND TILTING OF DOORS OF DOORS, WINDOWS AND SIMILAR
AT386040B (en) * 1983-08-13 1988-06-27 Rsb Holding & Management Ag ONE-HAND TURNTABLE FITTING FOR A WINDOW
DE9404850U1 (en) * 1994-03-22 1994-05-19 Siegenia-Frank Kg, 57074 Siegen Window, door or the like with turn-tilt fitting

Also Published As

Publication number Publication date
ES2439092T3 (en) 2014-01-21
EP1275804A2 (en) 2003-01-15
DE10133226C1 (en) 2002-08-22
EP1275804A3 (en) 2007-11-07

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