EP3034731B1 - Fitting for windows and doors - Google Patents
Fitting for windows and doors Download PDFInfo
- Publication number
- EP3034731B1 EP3034731B1 EP15200012.1A EP15200012A EP3034731B1 EP 3034731 B1 EP3034731 B1 EP 3034731B1 EP 15200012 A EP15200012 A EP 15200012A EP 3034731 B1 EP3034731 B1 EP 3034731B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- bearing
- wing
- angle piece
- frame
- side angle
- 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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- 239000002184 metal Substances 0.000 description 7
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- 230000005540 biological transmission Effects 0.000 description 6
- 238000006073 displacement reaction Methods 0.000 description 4
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
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- 238000009434 installation Methods 0.000 description 1
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- 230000005923 long-lasting effect Effects 0.000 description 1
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- 239000007787 solid Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D15/00—Suspension arrangements for wings
- E05D15/48—Suspension arrangements for wings allowing alternative movements
- E05D15/52—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
- E05D15/5211—Concealed suspension fittings
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D15/00—Suspension arrangements for wings
- E05D15/48—Suspension arrangements for wings allowing alternative movements
- E05D15/52—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
- E05D15/5205—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis with horizontally-extending checks
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D3/00—Hinges with pins
- E05D3/06—Hinges with pins with two or more pins
- E05D3/18—Hinges with pins with two or more pins with sliding pins or guides
- E05D3/186—Scissors hinges, with two crossing levers and five parallel pins
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D5/00—Construction of single parts, e.g. the parts for attachment
- E05D5/10—Pins, sockets or sleeves; Removable pins
- E05D5/14—Construction of sockets or sleeves
-
- 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
- E05D7/0009—Adjustable hinges
- E05D7/0018—Adjustable hinges at the hinge axis
- E05D7/0027—Adjustable hinges at the hinge axis in an axial direction
-
- 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
- E05D7/12—Hinges or pivots of special construction to allow easy detachment of the hinge from the wing or the frame
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05DÂ 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
- E05Y2600/00—Mounting or coupling arrangements for elements provided for in this subclass
- E05Y2600/60—Mounting or coupling members; Accessories therefor
- E05Y2600/634—Spacers
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05DÂ 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
- E05Y2600/00—Mounting or coupling arrangements for elements provided for in this subclass
- E05Y2600/60—Mounting or coupling members; Accessories therefor
- E05Y2600/634—Spacers
- E05Y2600/636—Washers
Definitions
- the corner bearing must accommodate the weight of the wing in the swung-open state of the wing.
- the sash weight is sometimes very high, on the one hand by architecturally desired large glass surfaces and on the other hand by a concomitant trend to triple glazing in order to achieve still acceptable thermal and sound insulating insulation values for large glass surfaces.
- EP 0 438 740 A1 EP 0 204 267 A2 and DE 10 2004 060 716 A1 are turn and turn-tilt fittings known. However, these are not designed to support particularly heavy wings in the rotated state in which a particularly high load acts in particular on the corner bearing.
- the invention is based primarily on the idea that the corner bearing can be loaded with higher weight forces when its bearing surfaces, that is those surfaces over which the power flow from the wing takes place in the frame can be increased. Since the dimensions of the corner bearing can not be increased arbitrarily, since they are essentially dependent on the profile dimensions and must comply with certain standard values, an increase in the load capacity must be made in other ways. So far, the primary force application point or the primary force application point of the Ecklagerbolzen, which is the primary intersection point for the wing.
- the solution according to the invention now provides that the wing-side angle piece has a further bearing at a lateral distance from the bearing point for the corner bearing bolts, which is expediently designed as a pressure bearing supported on a lug element of the corner bearing.
- the scissors is designed as a separate structural unit of the scissor bearing. This has an advantageous effect on the storage, since then only in each case mirror-symmetrical trained scissor bearings for a right or left stop and three variants of scissors, which differ in terms of their length, must be kept. For the six conceivable variations of two shear bearings and three shears, only five components are needed. In the known one-piece scissors and Scherenlagern, however, six different components are needed. The required connection between the scissors bearing and the scissors is advantageously carried out via a latching mechanism.
- the corner bearing 10 essentially consists of a first, frame-side angle 14 and a second, wing-side angle 16, which are interconnected via a hinge mechanism.
- the angle pieces 14 and 16 are used to attach the corner bearing 10 in the profiles of the wing and the frame.
- the angle 14 is made as a sheet metal part made of steel, while the angle 16 is a casting of zinc or other metal.
- the hinge mechanism comprises a first tab element 18, one end of which is connected to the angle piece 14 by means of a rivet 20 acting as a rotary joint.
- the other end of the tab member 18 is guided by means of a Kopfniets 22 in a slot 24 in a horizontal leg 26 of the elbow 16 slidably.
- a bearing bush 48 made of a sliding bearing material such as plastic or a metallic bearing material, on the one hand, the opening 42 for receiving the Ecklagerbolzens 38, on the other hand to a projecting beyond the end of the leg 46 sliding surface 50 (FIGS. Fig. 2a ), which rests on the smooth surface of the tab member 28 and thus forms next to the Ecklagerbolzen 38, another force-transmitting bearing.
- This bearing slides on pivoting opening and closing of the wing (not tilting) on a circular arc about the vertical axis of the corner bearing pin 38 on the surface of the tab member 28th
- a disc 54 is disposed between the underside of the first tab member 18 and the top of the horizontally oriented leg 36 of the angle 14, which is designed as a perforated disc and as a hinge acting rivet 20 encloses annularly.
- the disk 54 is like the bearing bush 48 and the slider 52 made of a plastic or a metal bearing material. The disk 54 allows a low-friction, at this point gap-free pivoting of the two tab members 18, 28 against each other and thus forms another power transmission path between the wing and the frame.
- the scissors bearing 12 is formed separately from the scissors.
- the scissors bearing together with the scissors is shown in Fig. 6.
- the scissors bearing 12 includes an elbow 56 for mounting to the frame and a pivoting mechanism for coupling with the scissors disposed on the wing.
- the pivot mechanism has two tab members 58 and 60 and a coupling element 62 (for connection to the scissors), all preferably made as sheet metal parts made of steel, similar to the corner bearing 10 via rivets 64, 66, 68, 70 and 72, the respective Connect parts pivotally and / or slidably together. It is noteworthy here that all rivets are made from the same side, ie such that the scissors bearing 12 does not have to be re-clamped in the tool during the riveting process. The economy and the precision of the production of the shear bearing 12 is thereby increased.
- Fig. 2a and b show a sectional view and side view of the corner bearing 10.
- sliding out slider 52 and disc 54 is good to recognize together with the bearing bush 48 that with the inventive measures a continuous power transmission path between the brackets 14 and 16 and thus between the wing and the frame is created.
- the corner bearing 10 is thus highly resilient.
- adjustment wedges are known in principle, they used to have a thickness of about 5 mm at the expense of the thickness of the vertical leg 46 of the angle piece 16. Due to the special geometric design of the adjusting wedge 78 shown here, its thickness is reduced to about 2 mm, so that the leg 46 can be made correspondingly solid, which in turn is the resilience of the corner bearing 10 conducive.
- Fig. 4 is the displacement wedge 78 merely shown for illustration in the two rotated by 180 ° mounting positions. Of course, only one copy of the adjustment wedge 78 is used to adjust the wing 74.
- Fig. 5a shows the scissor bearing 12 and the scissors 80, which are formed as a separate components in contrast to conventional constructions. As described at the outset, this provides a partial redundancy in the scope of the scissors which can be used with symmetrical scissors bearings in three length designs.
- the operative connection between the scissors bearing 12 and scissors 80, as shown Fig. 5b seen, created by hooks 82, 82 'on the scissor arm 84, which are suspended in corresponding openings 86, 86' on the coupling element 62 of the scissor bearing 12.
- an additional arranged on the scissor arm 84 securing clip 88 is provided, the audible and visible beyond the free end of the Scherenlagereducationslasche with correct connection between the scissors bearing 12 and the scissors 80 snaps into place, but for disassembly easy with simple Tool, such as a screwdriver, can be levered.
- the invention relates to a fitting, in particular a concealed fitting, for a frame 76 and at least one wing 74 having windows and doors comprising a consisting of at least one corner bearing 10 and at least one scissors bearing 12 band fitting, at least one in one upper, horizontal spar of the at least one blade 74 arranged, coupled to the at least one scissors bearing 12 scissors 80, at least one locking and unlocking of the wing 74 enabling locking fitting and at least one actuator for actuating the locking fitting, wherein the corner bearing 10 is a frame-side angle 14th and a wing-side angle piece 16 and wherein the wing-side angle piece 16 has a bearing point for a corner bearing pin 38.
- the wing-side angle piece 16 has a further bearing 50 at a lateral distance from the bearing point for the corner bearing pin 38.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Hinges (AREA)
- Dry Shavers And Clippers (AREA)
- Wing Frames And Configurations (AREA)
- Lock And Its Accessories (AREA)
Description
Die Erfindung betrifft einen Beschlag, insbesondere einen verdeckt liegenden Beschlag, für einen Rahmen und mindestens einen Flügel aufweisende Fenster und Türen, umfassend einen aus mindestens einem Ecklager und mindestens einem Scherenlager bestehenden Bandbeschlag, mindestens eine in einem oberen, horizontalen Holm des mindestens einen Flügels angeordnete, mit dem mindestens einen Scherenlager gekoppelte Schere, mindestens einen die Ent- und Verriegelung des Flügels ermöglichenden Verriegelungsbeschlag und mindestens eine Betätigungsvorrichtung zur Betätigung des Verriegelungsbeschlags, wobei das Ecklager ein rahmenseitiges Winkelstück und ein flügelseitiges Winkelstück aufweist, wobei das flügelseitige Winkelstück eine Lagerstelle für einen Ecklagerbolzen aufweist und wobei das flügelseitige Winkelstück in einem seitlichen Abstand zur Lagerstelle für den Ecklagerbolzen ein weiteres Lager aufweist.The invention relates to a fitting, in particular a concealed fitting, for a frame and at least one wing having windows and doors, comprising a consisting of at least one corner bearing and at least one scissors hinge hinge fitting, at least one arranged in an upper, horizontal spar of the at least one wing , with the at least one scissor bearing coupled scissors, at least one locking and unlocking the wing permitting locking fitting and at least one actuator for actuating the locking fitting, wherein the corner bearing has a frame-side elbow and a wing-side elbow, wherein the wing-side elbow a bearing point for a corner bearing bolt and wherein the wing-side angle piece has a further bearing at a lateral distance from the bearing point for the corner bearing bolt.
Bei derartigen Beschlägen muss im aufgeschwenkten Zustand des Flügels das Ecklager die Gewichtskraft des Flügels aufnehmen. Das Flügelgewicht ist heute teilweise sehr hoch, zum einen durch architektonisch gewünschte große Glasflächen und zum anderen durch einen damit einhergehenden Trend zu dreifachen Verglasungen um bei großen Glasflächen dennoch annehmbare thermische und schallisolierende Dämmwerte erreichen zu können. Aus den Veröffentlichungen
Ausgehend hiervon liegt der Erfindung die Aufgabe zugrunde, einen Beschlag der eingangs genannten Art derart weiterzuentwickeln, dass das Ecklager erhöhte Gewichtskräfte aufnehmen kann.Proceeding from this, the invention has the object, a fitting of the type mentioned in such a way that the corner bearing can absorb increased weight forces.
Zur Lösung dieser Aufgabe wird die in Patentanspruch 1 angegebene Merkmalskombination vorgeschlagen. Vorteilhafte Ausgestaltungen und Weiterbildungen der Erfindung ergeben sich aus den abhängigen Ansprüchen.To solve this problem, the feature combination specified in claim 1 is proposed. Advantageous embodiments and modifications of the invention will become apparent from the dependent claims.
Die Erfindung geht vor allem von dem Gedanken aus, dass das Ecklager mit höheren Gewichtskräften belastet werden kann, wenn dessen Lagerflächen, das heißt diejenigen Flächen, über die der Kraftfluss vom Flügel in den Rahmen stattfindet, vergrößert werden können. Da die Ausmaße des Ecklagers nicht beliebig vergrößert werden können, da sie im Wesentlichen von den Profilmaßen abhängig sind und gewisse Standardwerte einhalten müssen, muss eine Vergrößerung der Belastungsfähigkeit auf andere Weise hergestellt werden. Bisher war der primäre Krafteinleitungspunkt bzw. die primäre Krafteinleitungsstelle der Ecklagerbolzen, der den primären Schnittpunkt für den Flügel darstellt. Die erfindungsgemäße Lösung sieht nun vor, dass das flügelseitige Winkelstück in einem seitlichen Abstand zur Lagerstelle für den Ecklagerbolzen ein weiteres Lager aufweist, das zweckmäßig als sich auf einem Laschenelement des Ecklagers abstützendes Drucklager ausgebildet ist. Die Lagerstelle für den Ecklagerbolzen ist durch eine in dem flügelseitigen Winkelstück angeordnete Lagerbüchse gebildet, insbesondere eine Lagerbüchse aus einem Kunststoff oder einem metallischen Gleitlagerwerkstoff, der mit dem Metall des Ecklagerbolzens einen schmiermittelfreien Einsatz erlaubt. Das weitere Lager ist gemäß der Erfindung einstückig mit der Lagerbüchse ausgebildet. Die das weitere Lager bildende Partie der Lagerbüchse ragt geringfügig über dem entsprechenden Schenkel des flügelseitigen Winkelstücks hinaus um eine sichere Auflage auf dem Abstützpartner zu gewährleisten. In bevorzugter Ausgestaltung der Erfindung weist das flügelseitige Winkelstück einen Höhenverstellmechanismus für die Lagerbüchse auf, der bevorzugt eine auf die dem rahmenseitigen Winkelstück abgewandte Seite der Lagerbüchse einwirkende Stellschraube umfasst.The invention is based primarily on the idea that the corner bearing can be loaded with higher weight forces when its bearing surfaces, that is those surfaces over which the power flow from the wing takes place in the frame can be increased. Since the dimensions of the corner bearing can not be increased arbitrarily, since they are essentially dependent on the profile dimensions and must comply with certain standard values, an increase in the load capacity must be made in other ways. So far, the primary force application point or the primary force application point of the Ecklagerbolzen, which is the primary intersection point for the wing. The solution according to the invention now provides that the wing-side angle piece has a further bearing at a lateral distance from the bearing point for the corner bearing bolts, which is expediently designed as a pressure bearing supported on a lug element of the corner bearing. The bearing for the Ecklagerbolzen is formed by a arranged in the wing-side elbow bearing bush, in particular a bearing bush made of a plastic or a metallic bearing material, which allows a lubricant-free use with the metal of the corner bearing pin. The further bearing is formed integrally with the bearing bush according to the invention. The further bearing forming part of the bearing bush projects slightly beyond the corresponding leg of the wing-side elbow to ensure a secure support on the support partner. In a preferred embodiment of the invention, the wing-side elbow on a height adjustment mechanism for the bearing bush, the preferably comprises an acting on the side facing away from the frame side elbow side of the bearing bush adjusting screw.
Das Ecklager weist gemäß der Erfindung zwei miteinander gelenkig verbundene, zwischen dem flügelseitigen Winkelstück und dem rahmenseitigen Winkelstück angeordnete flügelseitige und rahmenseitige Steuerungslaschen auf, die zusammen einen scherenartigen Ausstellmechanismus bilden. Dabei stützt sich die weitere Lagerstelle gleitend auf einer dem flügelseitigen Winkelstück zugewandten Oberfläche der flügelseitigen Steuerungslasche ab.The corner bearing has according to the invention, two mutually hinged, arranged between the wing-side elbow and the frame-side elbow wing-side and frame-side control tabs, which together form a scissor-like deployment mechanism. In this case, the further bearing point slidably supported on a wing-side angle facing surface of the wing-side control tab.
Zur weiteren Verbesserung der Kraftableitung von dem flügelseitigen Winkelstück auf das rahmenseitige Winkelstück kann zwischen den zwei Steuerungslaschen ein Gleitkörper, vorzugsweise aus Kunststoff oder einem metallischen Gleitlagerwerkstoff, angeordnet sein. In weiterer Folge des Kraftflusses kann auch ein erstes Drehgelenk, dass die rahmenseitige Steuerungslasche und das rahmenseitige Winkelstück miteinander verbindet mit einer zwischen diesen Teilen angeordneten Scheibe, vorzugsweise aus Kunststoff, versehen sein. Es ergibt sich so eine kraftleitende Abfolge von Kunststoff-Metallpaarungen, die in der Lage sind, Flügelgewichte bis 200 kg oder mehr aufzunehmen.To further improve the power dissipation of the wing-side elbow on the frame-side elbow can be arranged between the two control tabs a sliding body, preferably made of plastic or a metallic sliding bearing material. As a further consequence of the power flow, a first rotary joint, which connects the frame-side control flap and the frame-side angle piece to one another, can also be provided with a pane arranged between these parts, preferably made of plastic. This results in a kraftleitende sequence of plastic-metal pairings, which are able to accommodate sash weights up to 200 kg or more.
Der mit Hilfe der Steuerungslaschen gebildete scherenartige Aufstellmechanismus weist zweckmäßig ein im Abstand von dem ersten Drehgelenk angeordnetes zweites Drehgelenk auf. Die Steuerungslaschen weisen zweckmäßig an dem ersten Drehgelenk gegenüberliegenden Endbereichen angeordnete, durch Niete gebildete Lagerbolzen auf, die in langlochartigen Ausnehmungen in den flügelseitigen Winkelstück und dem rahmenseitigen Winkelstück verschiebbar angeordnet sind.The scissor-like erection mechanism formed by means of the control tabs expediently has a second pivot joint arranged at a distance from the first pivot joint. The control tabs have expediently arranged on the first hinge opposite end portions, formed by rivets bearing pin, which are slidably disposed in slot-like recesses in the wing-side elbow and the frame-side elbow.
In weiter bevorzugter Ausgestaltung des Beschlags ist die Schere als getrennte Baueinheit von dem Scherenlager ausgebildet. Dies wirkt sich vorteilhaft auf die Lagerhaltung aus, da dann lediglich jeweils spiegelsymmetrisch ausgebildete Scherenlager für einen Rechts- oder Linksanschlag sowie drei Varianten von Scheren, die sich hinsichtlich ihrer Länge unterscheiden, vorgehalten werden müssen. Für die sechs denkbaren Variationen aus zwei Scherenlagern und drei Scheren werden damit lediglich fünf Komponenten benötigt. Bei den bekannten einteiligen Scheren und Scherenlagern werden hingegen sechs unterschiedliche Bauteile gebraucht. Die erforderliche Verbindung zwischen dem Scherenlager und der Schere erfolgt vorteilhaft über einen Rastmechanismus.In a further preferred embodiment of the fitting, the scissors is designed as a separate structural unit of the scissor bearing. This has an advantageous effect on the storage, since then only in each case mirror-symmetrical trained scissor bearings for a right or left stop and three variants of scissors, which differ in terms of their length, must be kept. For the six conceivable variations of two shear bearings and three shears, only five components are needed. In the known one-piece scissors and Scherenlagern, however, six different components are needed. The required connection between the scissors bearing and the scissors is advantageously carried out via a latching mechanism.
Eine vorteilhafte Vereinfachung beim Zusammenbau des Beschlags wird in weiterer Ausgestaltung der Erfindung dadurch erreicht, dass Nietbolzen, die die Steuerungslaschen miteinander und mit den Winkelstücken verbindende Lagerbolzen bilden, sämtlich von einer Richtung her vernietet werden. Ein Umspannen des Beschlags in der Nietmaschine ist damit nicht erforderlich.An advantageous simplification in the assembly of the fitting is achieved in a further embodiment of the invention in that rivet bolts, which form the control plates together and with the elbows connecting bearing bolts, are all riveted from one direction. A repositioning of the fitting in the riveting machine is not required.
In weiterer vorteilhafter Ausgestaltung der Erfindung weist der Beschlag einen Stellkeil auf, der eine Horizontaljustierung des Flügels des Fensters oder der Tür ermöglicht und der reversibel zwischen einem Vertikalschenkel des flügelseitigen Winkelstücks und einem an den Flügel angeordneten Kernstück angeordnet ist. Eine erste Position der Horizontaljustierung wird durch gänzliches Weglassen des Stellkeils erreicht, zwei weitere Positionen der Horizontaljustierung die sich beispielsweise von der ersten Position um jeweils 1 mm unterscheiden, werden durch Einsetzen des Stellkeils in den zwei möglichen unterschiedlichen Orientierungen erreicht.In a further advantageous embodiment of the invention, the fitting on an actuating wedge, which allows a horizontal adjustment of the wing of the window or the door and which is arranged reversibly between a vertical leg of the wing-side elbow and a wing arranged on the core piece. A first position of the horizontal adjustment is achieved by completely omitting the adjusting wedge, two further positions of the horizontal adjustment, for example, differ from the first position by 1 mm, are achieved by inserting the wedge in the two possible different orientations.
Im Folgenden wird die Erfindung anhand eines in der Zeichnung in schematischer Weise dargestellten Ausführungsbeispiels näher erläutert. Es zeigen
- Fig. 1
- ein Scherenlager und ein Ecklager eines verdeckt angeordneten Beschlags als Explosionsdarstellung;
- Fig. 2a
- und b das Ecklager im Schnitt und in Seitenansicht im geschlossenen Zustand;
- Fig. 3a
- bis c die Horizontaleinstellung des Flügels mittels eines Verstellungskeils;
- Fig. 4
- die Horizontaleinstellung des Flügels gemäß
Fig. 3 als Explosionsdarstellung; - Fig. 5a
- und b ein Scherenlager und eine Schere des Beschlags.
- Fig. 1
- a scissor bearing and a corner bearing of a concealed hardware as an exploded view;
- Fig. 2a
- and b the corner bearing in section and in side view in the closed state;
- Fig. 3a
- to c the horizontal adjustment of the wing by means of a displacement wedge;
- Fig. 4
- the horizontal adjustment of the wing according to
Fig. 3 as an exploded view; - Fig. 5a
- and b a scissors bearing and scissors of the fitting.
Der in der Zeichnung dargestellte Beschlag umfasst ein in
Das Ecklager 10 besteht im Wesentlichen aus einem ersten, rahmenseitigen Winkelstück 14 und einem zweiten, flügelseitigen Winkelstück 16, die über einen Gelenkmechanismus miteinander verbunden sind. Die Winkelstücke 14 und 16 dienen zur Befestigung des Ecklagers 10 in den Profilen des Flügels und des Rahmens. Das Winkelstück 14 ist als Blechbiegeteil aus Stahl gefertigt, während das Winkelstück 16 ein Gussteil aus Zink oder einem anderen Metall ist. Der Gelenkmechanismus umfasst ein erstes Laschenelement 18, dessen eines Ende mittels eines als Drehgelenk fungierenden Niets 20 mit dem Winkelstück 14 verbunden. Das andere Ende des Laschenelements 18 ist mittels eines Kopfniets 22 in einem Langloch 24 in einem Horizontalschenkel 26 des Winkelstücks 16 verschieblich geführt. Ein zweites Laschenelement 28 ist an einer Lagerstelle 30 mittels eines als Drehgelenk fungierenden Niets 32 mit dem ersten Laschenelement 18 drehbar verbunden. Die Lagerstelle 30 ist zwischen den Nieten 20 und 22 angeordnet. Das zweite Laschenelement 28 ist an einem Endbereich mittels eines Niets 34 drehbar und verschieblich in einem Langloch 40 in einem horizontal ausgerichteten Schenkel 36 des Winkelstücks 14 geführt, während der andere Endbereich des Laschenelements 28 einen im Wesentlichen senkrecht nach oben über das Laschenelement 28 überstehenden Ecklagerbolzen 38 trägt. Der Ecklagerbolzen 38 greift in eine nach unten weisende, ein Gleitlager bildende Öffnung 42 (
Da das Ecklager 10 für besonders schwere Flügelvarianten ausgelegt ist, sind weitere Maßnahmen für die Kraftübertragung getroffen, die den Kern der vorliegenden Erfindung darstellen. So ist in eine Ausnehmung 44 (
Eine weitere Maßnahme zur Verbesserung der Kraftübertragung zwischen dem Flügel und dem Rahmen wird durch einen Gleitkörper 52 erreicht, der mittels einer Mehrzahl von Vorsprüngen in komplementären Vertiefungen an der Oberseite des Laschenelements 18 verdrehsicher angeordnet ist. Die glatte Oberfläche des Gleitkörpers 52 steht geringfügig, weniger als etwa 1 mm, über die Oberfläche des Laschenelements 18 über und bildet eine Auflagerfläche für die Unterseite des zweiten Laschenelements 28, so dass dieses spaltfrei mit dem Gleitkörper 52 in Gleitkontakt steht und darüber mit dem ersten Laschenelement 18 einem Kraftübertragungspfad bildet. Der Gleitkörper 52 besteht wie die Lagerbüchse 48 aus einem Kunststoff oder einem metallischen Gleitlagerwerkstoff. Sowohl die Lagerbüchse 48 als auch der Gleitkörper 52 ermöglichen damit eine langandauernde, schmiermittelfreie oder -arme Verwendung des Ecklagers 10.Another measure for improving the transmission of force between the wing and the frame is achieved by a sliding
Als dritte Maßnahme zur Verbesserung der Kraftübertragung zwischen dem Flügel und dem Rahmen im Schwenkbetrieb des Flügels ist zwischen der Unterseite des ersten Laschenelements 18 und der Oberseite des horizontal ausgerichteten Schenkels 36 des Winkelstücks 14 eine Scheibe 54 angeordnet, die als Lochscheibe ausgebildet ist und den als Drehgelenk fungierenden Niet 20 ringartig umschließt. Die Scheibe 54 besteht wie die Lagerbüchse 48 und der Gleitkörper 52 aus einem Kunststoff oder einem metallischen Gleitlagerwerkstoff. Die Scheibe 54 ermöglicht ein reibungsarmes, an dieser Stelle spaltfreies Verschwenken der zwei Laschenelemente 18, 28 gegeneinander und bildet damit einen weiteren Kraftübertragungspfad zwischen dem Flügel und dem Rahmen.As a third measure for improving the power transmission between the wing and the frame in the swing operation of the wing, a
Die Anordnung und Befestigung der Winkelstücke 14, 16 an bzw. in den zugeordneten Profilen des Flügels und des Rahmens erfolgt mit den allseits bekannten Mitteln und Bauteilen und braucht daher hier nicht näher erläutert werden. Neu ist jedoch, dass sämtliche Nietverbindungen werkzeugmäßig in einer Ecklagerlage ausgeführt werden, so dass das Ecklager 10 während des Nietvorgangs nicht bezüglich des Werkzeugs in seiner Orientierung verändert werden muss, wodurch dieser Herstellungsvorgang effizienter und präziser als bisher ausgeführt wird.The arrangement and attachment of the
Das im oberen Teil der
Da eine toleranzfreie Herstellung und Montage des Flügels nicht wirtschaftlich möglich ist, ist in den
Zusammenfassend ist folgendes festzuhalten: Die Erfindung betrifft einen Beschlag, insbesondere einen verdeckt liegenden Beschlag, für einen Rahmen 76 und mindestens einen Flügel 74 aufweisende Fenster und Türen, umfassend einen aus mindestens einem Ecklager 10 und mindestens einem Scherenlager 12 bestehenden Bandbeschlag, mindestens eine in einem oberen, horizontalen Holm des mindestens einen Flügels 74 angeordnete, mit dem mindestens einen Scherenlager 12 gekoppelte Schere 80, mindestens einen die Ent- und Verriegelung des Flügels 74 ermöglichenden Verriegelungsbeschlag und mindestens eine Betätigungsvorrichtung zur Betätigung des Verriegelungsbeschlags, wobei das Ecklager 10 ein rahmenseitiges Winkelstück 14 und ein flügelseitiges Winkelstück 16 aufweist und wobei das flügelseitige Winkelstück 16 eine Lagerstelle für einen Ecklagerbolzen 38 aufweist. Um die Belastbarkeit des Ecklagers 10 durch besonders schwere Flügel 74 zu erhöhen, wird gemäß der Erfindung vorgeschlagen, dass das flügelseitige Winkelstück 16 in einem seitlichen Abstand zur Lagerstelle für den Ecklagerbolzen 38 ein weiteres Lager 50 aufweist.In summary, the following is to be noted: The invention relates to a fitting, in particular a concealed fitting, for a frame 76 and at least one
Claims (12)
- Fitting, in particular concealed fitting, for windows and doors having a frame (76) and at least one wing (74), comprising a band fitting consisting of at least one corner bearing (10) and at least one scissor hinge (12), at least one scissor (80) which isd connected to the scissor hinge (12) and disposed in an upper, horizontal spar of the wing (74), at least one lock fitting allowing the locking and unlocking of the wing (74), and at least one actuator for actuating the lock fitting, wherein the corner bearing (10) comprises a frame-side angle piece (14) and a wing-side angle piece (16), wherein said wing-side angle piece (16) has a bearing point for a corner bearing journal (38), and wherein the wing-side angle piece (16) comprises a further bearing point (50) at a lateral distance from the bearing point for the corner bearing journal (38), characterized in that the bearing point for the corner bearing journal (38) is formed by a bearing bush (48) disposed in the wing-side angle piece (16) and the further bearing (50) is formed integrally with the bearing bush (48), that the corner bearing (10) comprises two wing-side and frame-side control links (18, 28) which are hinged to each other and disposed between the wing-side angle piece (16) and the frame-side angle piece (14), which together form a scissor-like opening mechanism, and that the further bearing (50) is supported in a sliding manner on a surface of the wing-side control link (28) facing the wing-side angle piece (16).
- Fitting according to claim 1, characterized in that the bearing bush (48) consists of a plastic or a metallic plain bearing material.
- Fitting according to one of claims 1 or 2, characterized in that the wing-side angle piece (16) has a height adjustment mechanism for the bearing bush (48).
- Fitting according to claim 3, characterized in that the height adjustment mechanism comprises an adjustment screw acting on the side of the bearing bush (48) facing away from frame-side angle piece (14).
- Fitting according to one of claims 1 to 4, characterized in that a sliding body (52) made of plastic or a metallic bearing material is disposed between the two control links (18, 28).
- Fitting according to one of claims 1 to 5, characterized in that the frame-side control link (18) is disposed with a first hinge on the frame-side angle piece (14) and that between the frame-side control link (18) and the frame-side angle piece (14) there is a disc (54) made of plastic or a metallic bearing material.
- Fitting according to claim 6, characterized in that the control links (18, 28) are interconnected via a second hinge arranged at a distance from the first hinge.
- Fitting according to one of claims 1 to 7, characterized in that the control links (18, 28) comprise bearing bolts (22, 34) at end portions located opposed to the first hinge and the bearing bolts (22, 34) are slidably disposed in slot-like openings (24, 40) in the wing-side angle piece (16) and the frame-side angle piece (14).
- Fitting according to one of claims 1 to 8, characterized in that the scissor (80) is designed as a separate assembly from the scissor hinge (12).
- Fitting according to claim 13, characterized in that the scissor (80) is detachably connected to the scissor hinge (12) via a detent mechanism (82, 82'; 86, 86'; 88).
- Fitting according to one of claims 1 to 10, characterized in that bearing bolts connecting the control links (18, 28) of the corner bearing (10) with each other and with the angle pieces (14, 16) are formed as rivets (20, 22, 32, 34) and that all rivetings during the assembly of the corner bearing (10) have been carried out from one direction.
- Fitting according to one of claims 1 to 11, characterized in that and adjustment wedge (78) is provided for the horizontal adjustment of the at least one wing (74) of the window or door, which is reversibly disposed between a vertical limb (46) of the wing-side angle piece (16) and a clamping piece disposed on the wing (74), thereby effecting different clearances.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RS20171016A RS56430B1 (en) | 2014-12-19 | 2015-12-15 | Fitting for windows and doors |
HRP20171618TT HRP20171618T1 (en) | 2014-12-19 | 2017-10-24 | Fitting for windows and doors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102014226590.8A DE102014226590A1 (en) | 2014-12-19 | 2014-12-19 | Hardware for windows and doors |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3034731A1 EP3034731A1 (en) | 2016-06-22 |
EP3034731B1 true EP3034731B1 (en) | 2017-07-26 |
Family
ID=54849880
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15200012.1A Active EP3034731B1 (en) | 2014-12-19 | 2015-12-15 | Fitting for windows and doors |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP3034731B1 (en) |
DE (1) | DE102014226590A1 (en) |
HR (1) | HRP20171618T1 (en) |
RS (1) | RS56430B1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2839516T3 (en) * | 2016-05-31 | 2021-07-05 | Vkr Holding As | A hinge for a window, a window that includes a set of said hinges, and a method of installing said window |
DK3619387T3 (en) * | 2017-05-05 | 2021-10-04 | Vkr Holding As | A hinge for a window, a window including a set of such hinges and a method of mounting such a window |
DE102017207707B3 (en) | 2017-05-08 | 2018-06-28 | Roto Frank Ag | Fitting arrangement and window or door with such a fitting arrangement |
DE102022205247A1 (en) | 2022-05-25 | 2023-11-30 | Roto Frank Fenster- und Türtechnologie GmbH | Hinge fitting for horizontally adjusting the sash of a window or door |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2404267A1 (en) * | 1974-01-30 | 1975-07-31 | Siegenia Frank Kg | Support member for rotary swing windows OR DOORS - has angular bracket with connection slot for support member |
DE3336573A1 (en) * | 1983-03-29 | 1985-04-25 | Fa. Aug. Winkhaus, 4404 Telgte | Window or door having a turn-and-tilt fitting |
DE8516560U1 (en) * | 1985-06-07 | 1985-07-18 | Siegenia-Frank Kg, 5900 Siegen | Opening device for the sash of windows, doors or the like. |
DE9000594U1 (en) * | 1990-01-20 | 1990-03-01 | Gretsch-Unitas GmbH Baubeschläge, 71254 Ditzingen | Fitting for at least one rotating wing of a window, door or similar. |
DE29511756U1 (en) * | 1995-07-20 | 1995-09-28 | Ferco International Usine de Ferrures de Bâtiment S.A.R.L., Sarrebourg | Wing-side corner bearing fitting for tilt and turn windows |
FR2808045B1 (en) * | 2000-04-20 | 2002-07-12 | Ferco Int Usine Ferrures | CORNER SUPPORT FOR DOOR, WINDOW OR THE LIKE |
DE102004060716A1 (en) * | 2004-12-17 | 2006-07-06 | Aug. Winkhaus Gmbh & Co. Kg | Window, has wing-sided fitting part with horizontal support at one steering arm, where connection of wing-sided and frame-sided fitting parts is movably kept over other arm for movement of wing-sided fitting part into tilting position |
EP1936086B1 (en) * | 2006-12-23 | 2010-02-10 | ROTO FRANK Aktiengesellschaft | Corner fitting for windows, doors or similar |
DE102008000048A1 (en) * | 2008-01-14 | 2009-07-16 | Aug. Winkhaus Gmbh & Co. Kg | Corner hinge of a corner bearing |
DE202008005218U1 (en) * | 2008-04-15 | 2008-07-03 | Siegenia-Aubi Kg | Beschlagsatz |
DE102010003186A1 (en) * | 2010-03-24 | 2011-09-29 | Aug. Winkhaus Gmbh & Co. Kg | For concealed arrangement provided corner bearing |
-
2014
- 2014-12-19 DE DE102014226590.8A patent/DE102014226590A1/en not_active Withdrawn
-
2015
- 2015-12-15 RS RS20171016A patent/RS56430B1/en unknown
- 2015-12-15 EP EP15200012.1A patent/EP3034731B1/en active Active
-
2017
- 2017-10-24 HR HRP20171618TT patent/HRP20171618T1/en unknown
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
HRP20171618T1 (en) | 2017-12-01 |
EP3034731A1 (en) | 2016-06-22 |
RS56430B1 (en) | 2018-01-31 |
DE102014226590A1 (en) | 2016-06-23 |
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