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EP0619410B1 - Fitting for a sliding wing with non-circular guide pin - Google Patents

Fitting for a sliding wing with non-circular guide pin Download PDF

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Publication number
EP0619410B1
EP0619410B1 EP94105171A EP94105171A EP0619410B1 EP 0619410 B1 EP0619410 B1 EP 0619410B1 EP 94105171 A EP94105171 A EP 94105171A EP 94105171 A EP94105171 A EP 94105171A EP 0619410 B1 EP0619410 B1 EP 0619410B1
Authority
EP
European Patent Office
Prior art keywords
guide pin
guide
fixing recess
fitting
pin
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
EP94105171A
Other languages
German (de)
French (fr)
Other versions
EP0619410A1 (en
Inventor
Ernst Lahmann
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.)
Hautau GmbH
Original Assignee
Hautau GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hautau GmbH filed Critical Hautau GmbH
Publication of EP0619410A1 publication Critical patent/EP0619410A1/en
Application granted granted Critical
Publication of EP0619410B1 publication Critical patent/EP0619410B1/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
    • E05D15/00Suspension arrangements for wings
    • E05D15/06Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • E05D15/1005Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane the wing being supported on arms movable in horizontal planes
    • E05D15/1013Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane the wing being supported on arms movable in horizontal planes specially adapted for windows
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/06Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • E05D2015/1028Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane with only the wing moving transversely
    • E05D2015/1031Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane with only the wing moving transversely the wing supported on arms extending from the carriage
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/148Windows

Definitions

  • the invention relates to fittings for parallel adjustable, tiltable and - after parallel parking - sliding wing.
  • the invention focuses particularly on the design of a guide or functional plate which has a control or guide slot in which a guide pin is slidably held.
  • a fitting is also proposed with DE 32 34 677 C2.
  • a fitting is also explained there, which can be used to deploy a horizontally displaceable sash in parallel by means of deployment arms, which is achieved with lower deployment arms.
  • a locking member is provided on the lower extension arms, which slides in a sliding slot with slot arms.
  • the sliding slot consists of a longitudinal slot arm and a locking receptacle arm oriented at an angle of approximately 60 °, in which the locking element engages in the parallel-adjusted position of the wing.
  • the locking member is designed as a round bolt and can be moved along the entire control slot in this.
  • the fitting described has a considerable depth, so that in the closed state of the parallel-adjustable wing, the carriage protrudes noticeably from the wing plane (cf. the transverse section of FIG. 2 there).
  • the aim of the invention is to reduce this height .
  • the invention is based on the fact that in order to achieve a reduced overall height, it is necessary to leave the rotational symmetry of the symmetrical and well-functioning guide pin in the StdT. It suggests that this guide pin should no longer be rotationally symmetrical, but non-circular, for example only axisymmetric.
  • the guide pin can have two flat sides and have slightly convex outer curvature on the remaining sides (claim 2). This axisymmetric guide pin reached it is essential that the width of the guide plate can be reduced, because the control slot to be provided in this guide plate can now be made narrower in accordance with the narrower shape of the guide pin.
  • the fixing recess has a dimension that allows the guide pin to be fixed in the front end of the guide slot with its convex curvatures - those sides that are not flat sides.
  • the guide pin slides along the transfer bevel and over the nose projection into the fixing recess (claim 3).
  • the fixing recess can have a depth which allows the guide pin to introduce its entire transverse extent - from flat side to flat side - into the fixing recess. The guide pin is thus fixed or held in the wing position in the parallel position at the front end (4a) of the guide slot, so that the wing can be easily moved with the carriage in the open position.
  • a more concrete design of this more reliable fitting with its reduced overall depth results if the distance between the flat sides of the guide pin and the mutual alignment and spacing of transfer bevel and nose projection are coordinated with one another (claim 4), in such a way that the center plane of the guide pin matches the nose projection has already exceeded when the guide pin leaves or has (just) left the transfer bevel - in the direction of the fixing recess.
  • the center plane of the guide pin is the plane that is arranged in the middle between its two flat sides (fictitious). It also contains the longitudinal axis of the pin.
  • the pin transverse axis is oriented, about which the depth of the fixing recess was concerned (claim 3), specifically that the fixing recess in the transverse direction of the pin is just so deep that the entire guide pin finds space in it.
  • the guide slot has a width which corresponds to the expansion of the guide pin in the transverse direction of the pin corresponds to or is slightly larger.
  • the guide slot tapers to a width that is based on the transverse dimensions of the guide pin.
  • the invention means no round guide pins or rotationally symmetrical bolts; Rather, it is the philosophy of the invention to give these guide pins a no longer rotationally symmetrical shape, for example the selected axially symmetrical shape (symmetrical with respect to the mentioned longitudinal axis and Transverse axis). Only with this shape of the guide pin - different dimensions in the two axes of symmetry mentioned - can the success according to the invention be achieved that the fitting projects as little as possible towards the interior (reduced overall depth). This is also particularly aesthetically pleasing, since modern windows and sashes are to show only a few structural elements that are attached uncovered to the support bars of the window walls.
  • Operational safety also goes hand in hand with the reduction in overall height according to the invention, since the load-bearing capacity of the less protruding arm can be increased.
  • the trunnion which carries the parallel-adjustable sliding sash at the inside end of the extension arm, comes as close as possible to the sash frame or the center of the window sash.
  • a supplement can be provided, which consists of a compression spring which is arranged on the extension arm (claim 6). It cooperates with a rear stop of the control arm, on which the guide pin explained is arranged; this rear stop resiliently strikes the compression spring in the wing parallel position when the guide pin comes into the fixing recess (claim 6); this is the open position of the wing, in which it can be moved in parallel with the carriage.
  • the wing remains in this open position because the spring holds the control arm in the fixing or latching position.
  • the spring also supports this latching movement.
  • the non-circular guide pin 2 can then only against the resistance of the spring slide out of the fixing recess (snap-in).
  • the spring can be interchangeably mounted in the extension arm (claim 7), which makes it possible to easily replace it if it breaks.
  • Figure 1 is a plan view of a carriage, with a guide plate 5, which has a control slot 4 (right side). Roles are shown in dashed lines.
  • An extension arm 10 is shown articulated on the carriage and a control arm 6 is shown articulated on it.
  • FIG. 2 deepens a detailed aspect of FIG. 1 by showing the axially symmetrical, non-circular guide pin 2 between transfer bevel 1 and locking edge 3a (fixing lug) in its movement sequence from the elongated part of the control slot 4 into the fixing recess 3.
  • Figure 3 shows a section transverse to the wing plane, in which the carriage 101 is recognizable on the lower spar of the wing frame.
  • the closed and open sash positions are also shown, in which the guide pin 2 is fixed or locked in the fixing recess 3 (cf. FIG. 1).
  • the reduced overall height can be seen from the distance L between the vertical central axis of the wing 100 in the closed position and the central axis of the support pin 7, which rotatably connects the wing 100 to the extension arm 10.
  • FIGS. 4a and 4b explain the striking of a rear end 9 of the control arm 6 on a spring 8, which is removably mounted in the extension arm 10. This resilient end stop holds the control arm in its locked position, so that the wing remains fixed in the parallel parking end position.
  • FIG. 5 deepens this aspect by showing an angular position of control arm 6 and extension arm 10, which is present shortly before this parallel parking end position is reached.
  • FIG. 1 shows a top view of a carriage 101 with which a wing 100 which can be set down in parallel (cf. FIG. 3 or FIG. 4) can be moved in parallel.
  • a guide plate 5 is provided on the right side, which has an elongated control slot 4 with a front end 4a and a rear end 4b.
  • a guide pin 2 is slidably mounted in the guide slot 4 and has two flat sides 2a, 2b (cf. FIG. 2). The two flat sides of the guide pin 2 are connected via 2 convex, outwardly directed curvatures 2c, 2d.
  • an extension arm 10 is articulated on the carriage 101.
  • a control arm 6 is articulated on the extension arm 10, spaced apart from the aforementioned joint, which carries the mentioned guide pin 2 at its end, which is opposite the latter joint.
  • a parallel movement of the wing 100 now causes the scissors to pivot out of the extension arm 10 and control arm 6, the guide pin 2 sliding out of the rear end 4b of the control slot and being displaced in the direction of the front end 4a. Shortly before reaching the front end, it is deflected by a transfer bevel 1 and receives a movement path 21 which forces it into the fixing recess 3, which is arranged behind a locking edge 3a.
  • the control slot thus widens from its rear end 4b to the front fixing recess 3 at the front end 4a.
  • Figure 2 shows the guide pin 2 with its two flat sides 2a, 2b.
  • the curved sides 2c, 2d can have a semicircular shape. They can also have a reduced, less bulge.
  • the guide pin with the two flat sides can be formed from a bolt which has been deformed on both sides by pressing force.
  • the dimensions of the guide pin 2 are important. The most reliable solution is obtained when the central axis 2L (between the two flat sides 2a, 2b) has just exceeded the locking edge 3a - or the locking nose axis 3b - when the curved side 2c of the guide pin 2 leaves the transfer bevel 1. Then the guide pin 2 is located in the safe intake area of the fixing recess 3, into which it should pass without falling back into the elongated part of the control slot 4.
  • the path that the non-circular guide pin 2 takes is determined by the slope 1 and its slight rotary movement when the control arm 6 is raised. It is shown in dashed lines with the arrow 21. Since both the locking lug 3a and the edge surface 2d of the guide pin sliding over it are curved towards one another, this supports the latching function of the guide pin 2 in the fixing recess 3. The likewise curved surface 2c - compared to the surface 2d just mentioned - allows a smooth and smooth sliding of the non-circular guide pin 2 along the transfer bevel 1.
  • Figure 3 deepens the structural design of Figures 1 and 4 by showing a section BB, transverse to the control slot 4 in the guide plate 5.
  • the sash is shown once in the closed position - on the frame - and parallel to it in the open, parallel open position.
  • the control arm 10 is indicated.
  • the support pin 7 with which the sliding sash is pivotally arranged on the control arm 10.
  • the distance L between the center axis of the guide pin 7 and the center of gravity of the window sash is markedly shortened due to the narrow control plate 5 compared to conventional fittings of this type.
  • the reduction in the width of the plate 5 is made possible by the non-circular design of the guide pin 2.
  • FIG. 4 is also intended to clarify the engagement of the control arm when the wing 100 is parked in parallel by means of the section AA, which is shown in two open positions of the sliding wing 100 in FIGS. 4a and 4b.
  • a shaped spring 8 made of flat material is provided, which is interchangeably mounted in the extension arm 10. It acts together with a rear stop edge 9 on the control arm 6, and only in the open position of the sliding leaf 100. In all other positions between the fully open position and the closed position, the spring 8 is relieved. This is illustrated in FIG. 5, which shows a "nearly open position", namely a position of the wing 100 which can be set parallel, shortly before it reaches the final parallel setting.
  • FIG. 5 can be related to FIG. 4a, where the rear stop surface or edge 9 of the control arm 6 is just in front of the shaped spring 8. Shortly thereafter, the stop edge 9 comes to a stop at the upper protruding end of the spring 8 and supports the parallel fixing of the wing 100 placed in parallel in the final open position when the guide pin 2 slides completely into the fixing receptacle and the locking edge 3a in connection with the spring pressure prevents that the wing can now leave the open position again.
  • the guide pin 2 can only be against the resistance of the shaped spring 8 unlatched again and the wing leaves its open position.
  • the spring 8 has an elongated bearing section, a bent retaining flange 8c and a protruding stop bracket 8b, 8d.
  • the stop bracket 8b, 8d has an essentially S-shape; the lower curved end portion 8d comes to rest on the positioning arm.
  • This S-bracket protrudes from the display arm 10, while the elongated holding section 8a, which is slightly bent or curved, comes to rest in an insertion slot of the display arm 10.
  • the upper rounding of the S-bracket 8b and the length of the holding section 8a are formed so that the bent holding flange 8c can appear on the underside of the extension arm 10, so that the spring is latched into the opening arm.
  • the slot 10a can have a pressure 10b to the outside so that it assumes a T-shape.
  • the location of the spring 8 was previously said that it is arranged in the raising arm 10, its exact location there depends on the shape of the control arm 6.
  • a wishbone as Control arm 6 selected.
  • the shape of the wishbone 6 is essentially isosceles, the two legs being much longer than the hypotenuse.
  • the guide pin 2 is arranged at the corner point where the two elongated legs meet.
  • a pivot bearing 11 is provided, which connects the raising arm 10 to the control arm 6 in an articulated manner.
  • the location of the spring is then at the remaining corner of the elongated equilateral triangle, where the hypotenuse meets the leg near the window.
  • the rear stop surface 9 is also provided, which is formed by a section of the hypotenuse.
  • the guide pin 2 has a pin longitudinal axis 21 and a pin transverse axis 2q (see FIG. 2). These two axes are perpendicular to each other. It has also been shown that the guide pin can be designed as a non-circular round bolt, whereby it receives two flat sides 2a and 2b which come to lie parallel to the longitudinal axis 21 of the pin. The asymmetry in the longitudinal and transverse directions is therefore essential for the shape of the non-circular pin. If pins in the prior art regularly have a round bolt shape, the intention of the invention is precisely to avoid this rotational symmetry. It should therefore be emphasized that the invention uses a guide pin which is asymmetrical in the longitudinal and transverse directions shown, and is therefore out of round. The invention does not mean a shape other than the non-round in the longitudinal and transverse direction asymmetrical when it speaks of the non-round guide pin.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Closing And Opening Devices For Wings, And Checks For Wings (AREA)
  • Wing Frames And Configurations (AREA)

Description

Die Erfindung betrifft Beschläge für parallelabstellbare, kippbare und - nach Parallelabstellen - verschiebbare Flügel. Ihr besonderes Augenmerk richtet die Erfindung dabei auf die Gestaltung einer Führungs- oder Funktionsplatte, die einen Steuer- oder Führungsschlitz aufweist, in welchem ein Führungszapfen verschieblich gehalten ist.The invention relates to fittings for parallel adjustable, tiltable and - after parallel parking - sliding wing. The invention focuses particularly on the design of a guide or functional plate which has a control or guide slot in which a guide pin is slidably held.

Ein solcher Beschlag wird auch mit der DE 32 34 677 C2 vorgeschlagen. Auch dort ist ein Beschlag erläutert, der mittels Ausstellarmen einen horizontalverschiebbaren Flügel parallelabstellen kann, was mit unteren Ausstellarmen bewirkt wird. An den unteren Ausstellarmen ist ein Riegelglied vorgesehen, das in einem Verschiebeschlitz mit Schlitzarmen gleitet. Der Verschiebeschlitz besteht aus einem längsgerichteten Schlitzarm und einem in einem Winkel von etwa 60° demgegenüber orientierten Rastaufnahme-Arm, in den das Riegelglied in der parallelabgestellten Stellung des Flügels eingreift. Das Riegelglied ist als Rund-Bolzen ausgebildet und entlang des gesamten Steuerschlitzes in diesem verschieblich. Der beschriebene Beschlag weist eine erhebliche Bautiefe auf, so daß im geschlossenen Zustand des parallelabstellbaren Flügels der Laufwagen spürbar aus der Flügelebene hervorsteht (vgl. dort den querverlaufenden Schnitt von Fig. 2). Die Reduzierung dieser Bauhöhe hat sich die Erfindung zur Aufgabe gemacht. Such a fitting is also proposed with DE 32 34 677 C2. A fitting is also explained there, which can be used to deploy a horizontally displaceable sash in parallel by means of deployment arms, which is achieved with lower deployment arms. A locking member is provided on the lower extension arms, which slides in a sliding slot with slot arms. The sliding slot consists of a longitudinal slot arm and a locking receptacle arm oriented at an angle of approximately 60 °, in which the locking element engages in the parallel-adjusted position of the wing. The locking member is designed as a round bolt and can be moved along the entire control slot in this. The fitting described has a considerable depth, so that in the closed state of the parallel-adjustable wing, the carriage protrudes noticeably from the wing plane (cf. the transverse section of FIG. 2 there). The aim of the invention is to reduce this height .

Sie löst diese Aufgabe mit der im folgenden erläuterten technischen Lehre, deren wesentliche Merkmale der Anspruch 1 zeigt. Dabei geht die Erfindung davon aus, daß es zum Erreichen einer reduzierten Bauhöhe erforderlich ist, die Rotationssymmetrie des an sich symmetrischen und gut funktionsfähigen Führungszapfens im StdT zu verlassen. Sie schlägt dazu vor, diesen Führungszapfen nicht mehr rotationssymmetrisch auszubilden, sondern unrund, beispielsweise nur noch achsensymmetrisch. In spezieller Gestaltung kann der Führungszapfen zwei Flachseiten aufweisen und an den verbleibenden Seiten leicht konvexe Außenwölbung zeigen (Anspruch 2). Dieser achsensymmetrische Führungszapfen erreicht es maßgeblich, daß die Breite der Führungsplatte reduziert werden kann, denn der in dieser Führungsplatte vorzusehende Steuerschlitz kann nunmehr entsprechend der schmäleren Gestalt des Führungszapfens schmäler gestaltet werden. Nachdem sich der erwähnte Führungszapfen bei einer Parallelabstellung des erwähnten Flügels - bei einer Ausstellbewegung von Ausstellarm und Steuerarm des Beschlages - nicht nur im Steuerschlitz längsverschiebt, sondern sich dabei auch geringfügig dreht, ist eine besondere Gestalt des Steuerschlitzes vorgesehen. Das Ende des Steuerschlitzes, an den der Führungszapfen gelangt, wenn der Flügel parallelabgestellt ist, ist dazu abgeschrägt; er weist dort eine Überleitschräge auf, die gegenüber einer Fixierausnehmung angeordnet ist (Anspruch 1). Diese Überleitschräge ermöglicht die gewünschte Bahnführung des nicht mehr rotationssymmetrischen Führungszapfens entsprehend der Ausstellbewegung von Steuerarm und Ausstellarm. Mit dieser Schräge wird der Führungszapfen also bei seiner Längs-/Drehbewegung in dem Steuerschlitz so geführt, daß er in die Fixierausnehmung hineingleitet, und dort mit einem Nasenvorsprung fixierbar ist. Die Fixierausnehmung weist dabei eine Abmessung auf, die es dem Führungszapfen erlaubt, mit seinen konvexen Wölbungen - denjenigen Seiten, die keine Flachseiten sind - in dem vorderseitigen Ende des Führungsschlitzes fixiert zu werden. Dabei gleitet der Führungszapfen entlang der Überleitschräge und über den Nasenvorsprung in die Fixierausnehmung (Anspruch 3). Die Fixierausnehmung kann eine Tiefe aufweisen, die es dem Führungszapfen erlaubt, seine gesamte Querausdehnung - von Flachseite zu Flachseite - in die Fixierausnehmung einzubringen. Damit wird der Führungszapfen in der parallelabgestellten Flügelstellung am vorderseitigen Ende (4a) des Führungsschlitzes fixiert oder festgehalten, so daß der Flügel in der Offenstellung mit dem Laufwagen bequem verschiebbar ist. It solves this problem with the technical teaching explained below, the essential features of which claim 1 shows. The invention is based on the fact that in order to achieve a reduced overall height, it is necessary to leave the rotational symmetry of the symmetrical and well-functioning guide pin in the StdT. It suggests that this guide pin should no longer be rotationally symmetrical, but non-circular, for example only axisymmetric. In a special design, the guide pin can have two flat sides and have slightly convex outer curvature on the remaining sides (claim 2). This axisymmetric guide pin reached it is essential that the width of the guide plate can be reduced, because the control slot to be provided in this guide plate can now be made narrower in accordance with the narrower shape of the guide pin. After the above-mentioned guide pin not only shifts longitudinally in the control slot, but also rotates slightly in the event of a parallel movement of the wing mentioned - in the case of a deployment movement of the deployment arm and control arm of the fitting, a special shape of the control slot is provided. The end of the control slot, to which the guide pin reaches when the wing is placed in parallel, is chamfered to this end; there it has a transfer bevel, which is arranged opposite a fixing recess (claim 1). This transfer bevel enables the desired path guidance of the guide pin, which is no longer rotationally symmetrical, in accordance with the deployment movement of the control arm and deployment arm. With this bevel, the guide pin is guided in its longitudinal / rotary movement in the control slot so that it slides into the fixing recess and can be fixed there with a nose projection. The fixing recess has a dimension that allows the guide pin to be fixed in the front end of the guide slot with its convex curvatures - those sides that are not flat sides. The guide pin slides along the transfer bevel and over the nose projection into the fixing recess (claim 3). The fixing recess can have a depth which allows the guide pin to introduce its entire transverse extent - from flat side to flat side - into the fixing recess. The guide pin is thus fixed or held in the wing position in the parallel position at the front end (4a) of the guide slot, so that the wing can be easily moved with the carriage in the open position.

Überraschenderweise hat sich dabei ergeben, daß die Kombination aus nicht mehr rotationssymmetrischem (nicht mehr rundem) Führungszapfen und der langgestreckte Führungsschlitz mit Überleitschräge eine Erhöhung der Betriebssicherheit der erwähnten parallelabstellbaren Flügel ergibt.Surprisingly, it has been found that the combination of no longer rotationally symmetrical (no longer round) guide pin and the elongated guide slot with transfer bevel increase the operational reliability of the mentioned parallel-adjustable wing results.

Eine konkretere Gestaltung dieses betriebssichereren Beschlages mit seiner reduzierten Bautiefe ergibt sich dann, wenn der Abstand der Flachseiten des Führungszapfens und die gegenseitige Ausrichtung und Beabstandung von Überleitschräge und Nasenvorsprung aufeinander abgestimmt werden (Anspruch 4), und zwar so, daß die Mittelebene des Führungszapfens den Nasenvorsprung bereits überschritten hat, wenn der Führungszapfen die Überleitschräge - in Richtung zur Fixierausnehmung - verläßt oder (gerade) verlassen hat. Die Mittelebene des Führungszapfens ist diejenige Ebene, die mittig zwischen seinen beiden Flachseiten (fiktiv) angeordnet ist. In ihr liegt auch die Zapfen-Längsachse. Quer zu ihr - also senkrecht zu den Flachseiten - ist die Zapfen-Querachse orientiert, um die es bei der Tiefe der Fixierausnehmung ging (Anspruch 3), namentlich darum, daß in Zapfen-Querrichtung die Fixierausnehmung gerade so tief ist, daß der gesamte Führungszapfen in ihr Platz findet.A more concrete design of this more reliable fitting with its reduced overall depth results if the distance between the flat sides of the guide pin and the mutual alignment and spacing of transfer bevel and nose projection are coordinated with one another (claim 4), in such a way that the center plane of the guide pin matches the nose projection has already exceeded when the guide pin leaves or has (just) left the transfer bevel - in the direction of the fixing recess. The center plane of the guide pin is the plane that is arranged in the middle between its two flat sides (fictitious). It also contains the longitudinal axis of the pin. Transversely to it - that is perpendicular to the flat sides - the pin transverse axis is oriented, about which the depth of the fixing recess was concerned (claim 3), specifically that the fixing recess in the transverse direction of the pin is just so deep that the entire guide pin finds space in it.

Am entgegengesetzten Ende des Steuerschlitzes - dort, wo der Führungszapfen dann zu liegen kommt, wenn der Ausstellarm und Steuerarm des Beschlages eingeschwenkt sind und der Flügel sich in der geschlossenen Stellung befindet - hat der Führungsschlitz eine Breite, die der Ausdehnung des Führungszapfens in Zapfen-Querrichtung entspricht oder geringfügig größer ist. Ausgehend vom vorderseitigen Ende, an welchem die Fixierausnehmung und ihr gegenüber die Überleitschräge liegen, verjüngt sich also der Führungsschlitz bis auf eine Breite, die sich an den Quer-Abmessungen des Führungszapfens orientieren.At the opposite end of the control slot - where the guide pin comes to rest when the extension arm and control arm of the fitting are pivoted in and the sash is in the closed position - the guide slot has a width which corresponds to the expansion of the guide pin in the transverse direction of the pin corresponds to or is slightly larger. Starting from the front end, at which the fixing recess and the transfer bevel lie opposite it, the guide slot tapers to a width that is based on the transverse dimensions of the guide pin.

Wenn im Rahmen dieser Erfindung also von Führungszapfen gesprochen wird, so meint die Erfindung damit keine Rund-Führungszapfen oder rotationssymmetrische Bolzen; vielmehr ist es Philosophie der Erfindung, gerade diesen Führungszapfen eine nicht mehr rotationssymmetrische Gestalt zu geben, beispielsweise die gewählte achsensymmetrische Gestalt (symmetrisch bezüglich der erwähnten Zapfen-Längsachse und Zapfen-Querachse). Nur mit dieser Gestalt des Führungszapfens - verschiedene Abmessungen in den beiden erwähnten Symmetrieachsen - läßt sich der erfindungsgemäße Erfolg erreichen, daß der Beschlag zum Innenraum hin so wenig wie möglich vorsteht (reduzierte Bautiefe). Dies ist außerdem ästhetisch besonders ansprechend, da moderne Fenster und Flügel nur noch wenig Bauelemente zeigen sollen, die unverdeckt an den Tragholmen der Fensterwände angebracht werden. Kann man es aber nicht vermeiden, daß unverdeckt angeordnete Laufwägen zugegen sein müssen, so schafft zumindest die reduzierte Bauhöhe eine erhebliche ästhetische Verbesserung, da ein nur wenig hervorstehender Laufwagen aufgrund der schmäleren Führungsplatte optisch weniger hervorsticht als eine deutlich abstehende Laufwagen-Konstruktion, wie sie der erwähnten DE 32 34 677 C2 zu entnehmen ist.When speaking within the scope of this invention of guide pins, the invention means no round guide pins or rotationally symmetrical bolts; Rather, it is the philosophy of the invention to give these guide pins a no longer rotationally symmetrical shape, for example the selected axially symmetrical shape (symmetrical with respect to the mentioned longitudinal axis and Transverse axis). Only with this shape of the guide pin - different dimensions in the two axes of symmetry mentioned - can the success according to the invention be achieved that the fitting projects as little as possible towards the interior (reduced overall depth). This is also particularly aesthetically pleasing, since modern windows and sashes are to show only a few structural elements that are attached uncovered to the support bars of the window walls. However, if it cannot be avoided that uncovered carriages must be present, at least the reduced overall height creates a considerable aesthetic improvement, since a carriage that protrudes only slightly stands out less visually due to the narrower guide plate than a clearly protruding carriage construction, as it does DE 32 34 677 C2 mentioned can be seen.

Hand in Hand mit der erfindungsgemäßen Reduzierung der Bauhöhe geht auch die Betriebssicherheit, denn die Tragfähigkeit des weniger abstehenden Ausstellarmes kann erhöht werden. Der Tragzapfen, der am innenseitigen Ende des Ausstellarmes den parallelabstellbaren Schiebeflügel trägt, gelangt so dicht wie möglich an den Flügelrahmen bzw. den Fensterflügelschwerpunkt.Operational safety also goes hand in hand with the reduction in overall height according to the invention, since the load-bearing capacity of the less protruding arm can be increased. The trunnion, which carries the parallel-adjustable sliding sash at the inside end of the extension arm, comes as close as possible to the sash frame or the center of the window sash.

Zu der bauhöhenreduzierten, betriebssichereren und ästhetisch ansprechenderen Gestaltung des Beschlages für parallelabstellbare Flügel (Ansprüche 1 bis 5) kann eine Ergänzung vorgesehen werden, die in einer Druckfeder besteht, die am Ausstellarm angeordnet wird (Anspruch 6). Sie wirkt mit einem rückseitigen Anschlag des Steuerarmes zusammen, an dem auch der erläuterte Führungszapfen angeordnet ist; dieser rückseitige Anschlag schlägt in der Flügel-Parallelabstellung an die Druckfeder elastisch an, wenn der Führungszapfen in die Fixierausnehmung gelangt (Anspruch 6); das ist die Offenstellung des Flügels, in der er mit dem Laufwagen parallelverschiebbar ist. In dieser Offenstellung verbleibt der Flügel, da die Feder den Steuerarm in der Fixier- oder Einraststellung hält. Die Feder unterstützt auch diese Einrastbewegung. Der unrunde Führungszapfen 2 kann danach nur gegen den Widerstand der Feder aus der Fixierausnehmung (Einrastung) herausgleiten bzw. ausrasten. Die Feder kann auswechselbar in dem Ausstellarm gelagert sein (Anspruch 7), womit es möglich wird, sie bei Bruch leicht auszutauschen.For the reduced height, more reliable and more aesthetically pleasing design of the fitting for parallel-adjustable sash (claims 1 to 5), a supplement can be provided, which consists of a compression spring which is arranged on the extension arm (claim 6). It cooperates with a rear stop of the control arm, on which the guide pin explained is arranged; this rear stop resiliently strikes the compression spring in the wing parallel position when the guide pin comes into the fixing recess (claim 6); this is the open position of the wing, in which it can be moved in parallel with the carriage. The wing remains in this open position because the spring holds the control arm in the fixing or latching position. The spring also supports this latching movement. The non-circular guide pin 2 can then only against the resistance of the spring slide out of the fixing recess (snap-in). The spring can be interchangeably mounted in the extension arm (claim 7), which makes it possible to easily replace it if it breaks.

Zwar zeigt die erwähnte Patentschrift (DE 32 34 677 C2) auch schon eine Spreizfeder, die zwischen Steuerarm und Ausstellarm angeordnet ist und den Steuerarm in Richtung seiner Einrastbewegung in den rastaufnehmenden Schlitzarm vorspannt. Diese Spreizfeder steht allerdings ständig unter Spannung, so daß sie einer erhöhten Bruchgefahr ausgesetzt ist. Nicht so die erfindungsgemäße Druckfeder, die mit dem rückseitigen Anschlag des Steuerarmes zusammenwirkt, wobei sie selbst in dem Ausstellarm gelagert ist. Sie wird nur dann stärker belastet, wenn der parallelabgestellte Flügel in seine Offenstellung gelangt, in allen anderen Betriebsstellungen des Flügels ist sie entlastet bzw. in der Offenstellung selbst nur leicht belastet.Although the mentioned patent specification (DE 32 34 677 C2) also already shows a spreading spring which is arranged between the control arm and the raising arm and prestresses the control arm in the direction of its latching movement in the latching slot arm. However, this spreading spring is constantly under tension, so that it is exposed to an increased risk of breakage. Not so the compression spring according to the invention, which cooperates with the rear stop of the control arm, wherein it is itself mounted in the extension arm. It is only subjected to a greater load when the wing placed in parallel reaches its open position, in all other operating positions of the wing it is relieved or only slightly loaded in the open position itself.

Das Verständnis der Erfindung wird nachfolgend anhand eines Ausführungsbeispiels vertieft und erweitert.The understanding of the invention is deepened and expanded below using an exemplary embodiment.

Figur 1 ist eine Aufsicht auf einen Laufwagen, mit einer Führungsplatte 5, die einen Steuerschlitz 4 (rechtsseitig) aufweist. Strichliniert sind Rollen dargestellt. Gelenkig an dem Laufwagen ist ein Ausstellarm 10 und gelenkig an diesem ein Steuerarm 6 dargestellt. Figure 1 is a plan view of a carriage, with a guide plate 5, which has a control slot 4 (right side). Roles are shown in dashed lines. An extension arm 10 is shown articulated on the carriage and a control arm 6 is shown articulated on it.

Figur 2 vertieft einen Detailaspekt der Figur 1, indem der achsensymmetrische unrunde Führungszapfen 2 zwischen Überleitschräge 1 und Rastkante 3a (Fixiernase) in seinem Bewegungsablauf vom langgestreckten Teil des Steuerschlitzes 4 in die Fixierausnehmung 3 dargestellt ist. FIG. 2 deepens a detailed aspect of FIG. 1 by showing the axially symmetrical, non-circular guide pin 2 between transfer bevel 1 and locking edge 3a (fixing lug) in its movement sequence from the elongated part of the control slot 4 into the fixing recess 3.

Figur 3 zeigt einen Schnitt quer zur Flügel-Ebene, bei dem der Laufwagen 101 am unteren Holm des Flügelrahmens erkennbar ist. Dargestellt ist dabei auch die geschlossene und die offene Flügelstellung, bei welcher der Führungszapfen 2 in der Fixierausnehmung 3 (vgl. Fig. 1) fixiert oder eingerastet ist. Erkennbar ist die reduzierte Bauhöhe anhand des Abstandes L zwischen Vertikal-Mittelachse des Flügels 100 in Schließstellung und der Mittelachse des Tragzapfens 7, der den Flügel 100 mit dem Ausstellarm 10 drehbar verbindet. Figure 3 shows a section transverse to the wing plane, in which the carriage 101 is recognizable on the lower spar of the wing frame. The closed and open sash positions are also shown, in which the guide pin 2 is fixed or locked in the fixing recess 3 (cf. FIG. 1). The reduced overall height can be seen from the distance L between the vertical central axis of the wing 100 in the closed position and the central axis of the support pin 7, which rotatably connects the wing 100 to the extension arm 10.

Figur 4 erläutert vertiefend diese Ausstell-Position mit einer Aufsicht auf den abgestellten Flügel mit Laufwagen. Auch hier ist der Tragzapfen 7 zu erkennen, sowie der eingerastete Führungszapfen 2 in der Fixierausnehmung 3 der Führungsplatte 5. Figur 4a und 4b erläutern das Anschlagen eines rückwärtigen Endes 9 des Steuerarmes 6 an einer Feder 8, die im Ausstellarm 10 entnehmbar gelagert ist. Dieser federnde Endanschlag hält den Steuerarm in seiner Einraststellung, womit der Flügel in der Parallelabstell-Endlage fixiert bleibt. Figure 4 explains this opening position in more detail with a view of the parked wing with carriage. Here too, the support pin 7 can be seen, as well as the latched guide pin 2 in the fixing recess 3 of the guide plate 5. FIGS. 4a and 4b explain the striking of a rear end 9 of the control arm 6 on a spring 8, which is removably mounted in the extension arm 10. This resilient end stop holds the control arm in its locked position, so that the wing remains fixed in the parallel parking end position.

Figur 5 vertieft diesen Aspekt, indem eine Winkellage von Steuerarm 6 und Ausstellarm 10 gezeigt wird, die kurz vor Erreichen dieser Parallelabstell-Endlage vorliegt. FIG. 5 deepens this aspect by showing an angular position of control arm 6 and extension arm 10, which is present shortly before this parallel parking end position is reached.

Figur 1 zeigt eine Aufsicht auf einen Laufwagen 101, mit dem ein parallelabstellbarer Flügel 100 (vgl. Fig. 3 oder Fig. 4) parallelverfahrbar ist. Auf dem Laufwagen 101 ist rechtsseitig eine Führungsplatte 5 vorgesehen, die einen langgestreckten Steuerschlitz 4 mit vorderseitigem Ende 4a und rückseitigem Ende 4b aufweist. In dem Führungsschlitz 4 ist ein Führungszapfen 2 verschieblich gelagert, der zwei Flachseiten 2a,2b aufweist (vgl. Fig. 2). Die beiden Flachseiten des Führungszapfens 2 werden verbunden über 2 konvexe, nach außen gerichtete Wölbungen 2c,2d. Im Abstand von dem vorderseitigen Ende 4a des Steuerschlitzes 4 ist ein Ausstellarm 10 an dem Laufwagen 101 angelenkt. An dem Ausstellarm 10 - beabstandet von dem vorgenannten Gelenk - ist ein Steuerarm 6 angelenkt, der an seinem - dem letzteren Gelenk gegenüberliegenden - Ende den erwähnten Führungszapfen 2 trägt. FIG. 1 shows a top view of a carriage 101 with which a wing 100 which can be set down in parallel (cf. FIG. 3 or FIG. 4) can be moved in parallel. On the carriage 101, a guide plate 5 is provided on the right side, which has an elongated control slot 4 with a front end 4a and a rear end 4b. A guide pin 2 is slidably mounted in the guide slot 4 and has two flat sides 2a, 2b (cf. FIG. 2). The two flat sides of the guide pin 2 are connected via 2 convex, outwardly directed curvatures 2c, 2d. At a distance from the front end 4a of the control slot 4, an extension arm 10 is articulated on the carriage 101. A control arm 6 is articulated on the extension arm 10, spaced apart from the aforementioned joint, which carries the mentioned guide pin 2 at its end, which is opposite the latter joint.

Eine Parallelabstell-Bewegung des Flügels 100 führt nun zu einem Ausschwenken der Schere aus Ausstellarm 10 und Steuerarm 6, wobei der Führungszapfen 2 aus dem hinteren Ende 4b des Steuerschlitzes herausgleitet und in Richtung zum vorderseitigen Ende 4a verschoben wird. Kurz vor Erreichen des vorderseitigen Endes wird er von einer Überleitschräge 1 abgelenkt und erhält eine Bewegungsbahn 21, die ihn in die Fixierausnehmung 3 zwingt, die hinter einer Rastkante 3a angeordnet ist. Der Steuerschlitz verbreitert sich somit von seinem hinteren Ende 4b zu der vorseitigen Fixierausnehmung 3 am Vorderende 4a. In dieser Fixierausnehmung 3 - zwischen dem Vorderende 4a und der Rastkante 3a (Fixiernase) - findet der Führungszapfen 2 einen sicheren Halt; der parallelabgestellte Flügel 100 kann nun mit dem Wagen 101 - ohne Gefahr des Zurückklappens -parallelverfahren werden.A parallel movement of the wing 100 now causes the scissors to pivot out of the extension arm 10 and control arm 6, the guide pin 2 sliding out of the rear end 4b of the control slot and being displaced in the direction of the front end 4a. Shortly before reaching the front end, it is deflected by a transfer bevel 1 and receives a movement path 21 which forces it into the fixing recess 3, which is arranged behind a locking edge 3a. The control slot thus widens from its rear end 4b to the front fixing recess 3 at the front end 4a. In this fixing recess 3 - between the front end 4a and the locking edge 3a (fixing nose) - the guide pin 2 finds a secure hold; the wing 100 parked in parallel can now be moved parallel to the carriage 101 - without the risk of folding back.

Figur 2 zeigt den Führungszapfen 2 mit seinen beiden Flachseiten 2a, 2b. Die gewölbten Seiten 2c,2d können Halbrund-Form aufweisen. Sie können auch eine reduzierte schwächere Wölbung haben. Der Führungszapfen mit den beiden Flachseiten kann geformt sein aus einem Bolzen, der beidseitig durch Preßkraft verformt wurde. Für die Ausrichtung und Anordnung der Überleitschräge 1 und der Rastkante oder Rastnase 3a sind die Abmessungen des Führungszapfens 2 von Bedeutung. Die betriebssicherste Lösung ergibt sich, wenn die Mittelachse 2L (zwischen den beiden Flachseiten 2a,2b) gerade die Rastkante 3a - bzw. die Rastnasen-Achse 3b - überschritten hat, wenn die vorderseitig gewölbte Seite 2c des Führungszapfens 2 die Überleitschräge 1 verläßt. Dann befindet sich der Führungszapfen 2 im sicheren Einzugsbereich der Fixierausnehmung 3, in die er gelangen soll, ohne in den langgestreckten Teil des Steuerschlitzes 4 zurückzufallen. Figure 2 shows the guide pin 2 with its two flat sides 2a, 2b. The curved sides 2c, 2d can have a semicircular shape. They can also have a reduced, less bulge. The guide pin with the two flat sides can be formed from a bolt which has been deformed on both sides by pressing force. For the alignment and arrangement of the Transfer bevel 1 and the detent edge or detent 3a, the dimensions of the guide pin 2 are important. The most reliable solution is obtained when the central axis 2L (between the two flat sides 2a, 2b) has just exceeded the locking edge 3a - or the locking nose axis 3b - when the curved side 2c of the guide pin 2 leaves the transfer bevel 1. Then the guide pin 2 is located in the safe intake area of the fixing recess 3, into which it should pass without falling back into the elongated part of the control slot 4.

Die Bahn, die der unrunde Führungszapfen 2 nimmt, wird von der Schräge 1 sowie seiner leichten Drehbewegung beim Ausstellen des Steuerarmes 6 bestimmt. Sie ist strichliniert mit dem Pfeil 21 eingezeichnet. Da sowohl die Rastnase 3a als auch die über sie hinweggleitende Randfläche 2d des Führungszapfens zueinander gewölbt sind, unterstützt dies die Einrastfunktion des Führungszapfens 2 in der Fixierausnehmung 3. Die ebenfalls nach außen gewölbte Fläche 2c - gegenüber der soeben erwähnten Fläche 2d - erlaubt ein sanftes und leichtgängiges Gleiten des unrunden Führungszapfens 2 entlang der Überleitschräge 1.The path that the non-circular guide pin 2 takes is determined by the slope 1 and its slight rotary movement when the control arm 6 is raised. It is shown in dashed lines with the arrow 21. Since both the locking lug 3a and the edge surface 2d of the guide pin sliding over it are curved towards one another, this supports the latching function of the guide pin 2 in the fixing recess 3. The likewise curved surface 2c - compared to the surface 2d just mentioned - allows a smooth and smooth sliding of the non-circular guide pin 2 along the transfer bevel 1.

Figur 3 vertieft die bauliche Gestaltung der Figuren 1 und 4, indem sie einen Schnitt B-B zeigt, quer zum Steuerschlitz 4 in der Führungsplatte 5. Dabei ist der Flügel einmal in geschlossener Stellung - am Blendrahmen - und parallel dazu in geöffneter, parallelabgestellter Offenstellung gezeigt. Der Steuerarm 10 ist angedeutet. Auch hervorgehoben ist der Tragzapfen 7, mit welchem der Schiebeflügel auf dem Steuerarm 10 schwenkbar angeordnet ist. Der eingezeichnete Abstand L zwischen Mittelachse des Führungszapfens 7 und Schwerpunktslinie des Fensterflügels ist aufgrund der schmalen Steuerplatte 5 deutlich verkürzt gegenüber herkömmlichen Beschlägen dieser Art. Die Reduzierung der Breite der Platte 5 wird möglich durch die unrunde Gestaltung des Führungszapfens 2. Begrenzt wird die Reduktion der Breite der Führungsplatte 5 dadurch, daß der Führungszapfen 2 nicht beliebig in seiner Zapfen-Querrichtung 2a verschmälert werden kann. Er muß ein Mindestmaß an Kräften aufnehmen, was seine Abmessungen bestimmt. Damit kann die Platte - abhängig vom Gewicht des parallelabstellbaren Fensterflügels - so schmal wie möglich gehalten sein, damit der Tragzapfen 7 des Ausstellarmes 10 möglichst dicht am Flügelrahmen bzw. möglichst nahe zum Fensterflügel-Schwerpunkt hingelagert werden kann. Damit erhöht sich auf die Tragfähigkeit des Ausstellarmes 10, da er nur noch reduzierte Biegemomente aufnehmen muß. Dies ist schließlich auch in Figur 4 veranschaulicht, wo wiederum eine Aufsicht auf den Laufwagen 101 gezeigt ist - vgl. Figur 1 -, jedoch mit auf dem Ende des Ausstellarmes 10 aufsitzendem Schiebeflügel 100. Figure 3 deepens the structural design of Figures 1 and 4 by showing a section BB, transverse to the control slot 4 in the guide plate 5. The sash is shown once in the closed position - on the frame - and parallel to it in the open, parallel open position. The control arm 10 is indicated. Also highlighted is the support pin 7 with which the sliding sash is pivotally arranged on the control arm 10. The distance L between the center axis of the guide pin 7 and the center of gravity of the window sash is markedly shortened due to the narrow control plate 5 compared to conventional fittings of this type. The reduction in the width of the plate 5 is made possible by the non-circular design of the guide pin 2. The reduction in the width is limited the guide plate 5 in that the guide pin 2 cannot be narrowed arbitrarily in its pin transverse direction 2a. He must have a minimum level of strength record what determines its dimensions. Thus, the plate - depending on the weight of the window sash that can be set in parallel - be kept as narrow as possible so that the support pin 7 of the extension arm 10 can be stored as close as possible to the sash frame or as close as possible to the window sash center of gravity. This increases the load-bearing capacity of the extension arm 10, since it only has to absorb reduced bending moments. Finally, this is also illustrated in FIG. 4, which in turn shows a top view of the carriage 101 - cf. 1 - but with the sliding sash 100 seated on the end of the extension arm 10.

Figur 4 soll mittels des Schnittes A-A, der in zwei Öffnungsstellungen des Schiebeflügels 100 in den Figuren 4a und 4b gezeigt wird, auch die Einrastung des Steuerarms beim Parallelabstellen des Flügels 100 verdeutlichen. FIG. 4 is also intended to clarify the engagement of the control arm when the wing 100 is parked in parallel by means of the section AA, which is shown in two open positions of the sliding wing 100 in FIGS. 4a and 4b.

Dazu wird eine geformte Feder 8 aus Flachmaterial vorgesehen, die im Ausstellarm 10 auswechselbar gelagert ist. Sie wirkt zusammen mit einer rückwärtigen Anschlagkante 9 am Steuerarm 6, und zwar nur in Offenstellung des Schiebeflügels 100. In allen anderen Stellungen zwischen der vollständigen Offenstellung und der geschlossenen Stellung ist die Feder 8 entlastet. Dies verdeutlicht die Figur 5, die eine Nahezu-Offenstellung" zeigt, namentlich eine Stellung des parallelabstellbaren Flügels 100, kurz bevor dieser die endgültige Parallelabstellung erreicht.For this purpose, a shaped spring 8 made of flat material is provided, which is interchangeably mounted in the extension arm 10. It acts together with a rear stop edge 9 on the control arm 6, and only in the open position of the sliding leaf 100. In all other positions between the fully open position and the closed position, the spring 8 is relieved. This is illustrated in FIG. 5, which shows a "nearly open position", namely a position of the wing 100 which can be set parallel, shortly before it reaches the final parallel setting.

Figur 5 kann in Beziehung gesetzt werden mit Fig. 4a, wo die rückwärtige Anschlagfläche oder -kante 9 des Steuerarmes 6 kurz vor der geformten Feder 8 steht. Kurz danach kommt die Anschlagkante 9 an dem oberen herausstehenden Ende der Feder 8 zum Anschlag und unterstützt die Parallelfixierung des parallelabgestellten Flügels 100 in der endgültigen Offenstellung, wenn der Führungszapfen 2 vollständig in die Fixieraufnehmung hineingleitet und die Rastkante 3a in Verbindung mit dem Federdruck verhindert, daß der Flügel nunmehr die Offenstellung wieder verlassen kann. Nur gegen den Widerstand der geformten Feder 8 kann der Führungszapfen 2 wieder ausgerastet werden und der Flügel seine Offenstellung verlassen. FIG. 5 can be related to FIG. 4a, where the rear stop surface or edge 9 of the control arm 6 is just in front of the shaped spring 8. Shortly thereafter, the stop edge 9 comes to a stop at the upper protruding end of the spring 8 and supports the parallel fixing of the wing 100 placed in parallel in the final open position when the guide pin 2 slides completely into the fixing receptacle and the locking edge 3a in connection with the spring pressure prevents that the wing can now leave the open position again. The guide pin 2 can only be against the resistance of the shaped spring 8 unlatched again and the wing leaves its open position.

Die Feder 8 weist einen langgestreckten Lagerabschnitt, einen umgebogenen Halteflansch 8c und einen herausstehenden Anschlagbügel 8b,8d auf. Der Anschlagbügel 8b,8d hat im wesentlichen S-Form; wobei der untere gekrümmte Endabschnitt 8d auf dem Anstellarm zu liegen kommt. Dieser S-Bügel steht aus dem Ausstellarm 10 hervor, während der langgestreckte Halteabschnitt 8a, der leicht geknickt oder gekrümmt ist, in einem Einlegeschlitz des Ausstellungsarmes 10 zu liegen kommt. Die obere Rundung des S-Bügels 8b und die Länge des Halteabschnittes 8a sind gerade so ausgebildet, daß der umgebogene Halteflansch 8c auf der Unterseite des Ausstellarmes 10 zum Vorschein kommen kann, so daß die Feder im Ausstellarm eingerastet ist. Stößt nun die rückwärtige Anschlagkante 9 des Steuerarmes 6 gegen den herausstehenden S-Bügel, so verschiebt dieser sich in Richtung der Bewegung des Flügels 100, wodurch der leicht gekrümmte oder abgeknickte Halteabschnitt 8a der Flachfeder 8 begradigt wird und eine Federkraft entsteht. Diese Federkraft ist mithin nur dann aufzubringen, wenn der Schiebeflügel in seine Offenstellung gelangt und dabei der Führungszapfen einrastet. Sie ist verständlicherweise aber auch dann - jedoch in reduziertem Umfang - aufzubringen, während der parallelabgestellte Flügel in dieser Offenstellung verbleibt. Die Beanspruchung der Flachfeder 8 wird also geringer sein.The spring 8 has an elongated bearing section, a bent retaining flange 8c and a protruding stop bracket 8b, 8d. The stop bracket 8b, 8d has an essentially S-shape; the lower curved end portion 8d comes to rest on the positioning arm. This S-bracket protrudes from the display arm 10, while the elongated holding section 8a, which is slightly bent or curved, comes to rest in an insertion slot of the display arm 10. The upper rounding of the S-bracket 8b and the length of the holding section 8a are formed so that the bent holding flange 8c can appear on the underside of the extension arm 10, so that the spring is latched into the opening arm. If the rear stop edge 9 of the control arm 6 abuts against the protruding S-bracket, the latter moves in the direction of the movement of the wing 100, as a result of which the slightly curved or kinked holding section 8a of the flat spring 8 is straightened and a spring force arises. This spring force can therefore only be applied when the sliding sash comes into its open position and the guide pin engages. Understandably, however, it is then also to be applied, however to a reduced extent, while the wing placed in parallel remains in this open position. The stress on the flat spring 8 will therefore be lower.

Sollte die in dieser Gestaltung bereits stark - gegenüber dem Stand der Technik - gesenkte Belastung der Flachfeder 8 doch einmal dazu führen, daß diese Feder bricht, so kann diese Feder aufgrund der einfachen Anbringung in dem Schlitz 10a des Steuerarmes 10 leicht ausgewechselt werden. Der Schlitz 10a kann nach außen einen Durchdruck 10b haben, so daß er T-Form annimmt.Should the load on the flat spring 8, which is already strongly reduced in this design compared to the prior art, cause this spring to break, this spring can be easily replaced due to the simple attachment in the slot 10a of the control arm 10. The slot 10a can have a pressure 10b to the outside so that it assumes a T-shape.

Zum Anbringungsort der Feder 8 war bislang gesagt, daß sie im Ausstellarm 10 angeordnet wird, ihre genaue Lage dort hängt von der Gestalt des Steuerarmes 6 ab. Im Ausführungsbeispiel - vgl. beispielsweise die Figur 4 - ist ein Dreieckslenker als Steuerarm 6 gewählt. Die Form des Dreieckslenkers 6 ist im wesentlichen gleichschenklig, wobei die beiden Schenkel wesentlich länger sind als die Hypotenuse. Im Eckpunkt, in dem die beiden langgestreckten Schenkel zusammentreffen, ist der Führungszapfen 2 angeordnet. An dem Eckpunkt, in dem die Hypotenuse mit dem beschlagsfernen Schenkel zusammentrifft, ist ein Drehlager 11 vorgesehen, das den Ausstellarm 10 gelenkig mit dem Steuerarm 6 verbindet. Der Anbringungsort der Feder ist dann etwa an der verbleibenden Ecke des langgestreckten gleichseitigen Dreiecks, wo die Hypotenuse mit dem fensternahen Schenkel zusammentrifft. Hier ist auch die rückwärtige Anschlagfläche 9 vorgesehen, die von einem Abschnitt der Hypotenuse gebildet wird.The location of the spring 8 was previously said that it is arranged in the raising arm 10, its exact location there depends on the shape of the control arm 6. In the exemplary embodiment - cf. for example Figure 4 - is a wishbone as Control arm 6 selected. The shape of the wishbone 6 is essentially isosceles, the two legs being much longer than the hypotenuse. The guide pin 2 is arranged at the corner point where the two elongated legs meet. At the corner where the hypotenuse meets the leg remote from the fitting, a pivot bearing 11 is provided, which connects the raising arm 10 to the control arm 6 in an articulated manner. The location of the spring is then at the remaining corner of the elongated equilateral triangle, where the hypotenuse meets the leg near the window. Here, the rear stop surface 9 is also provided, which is formed by a section of the hypotenuse.

Erwähnt worden ist, daß der Führungszapfen 2 eine Zapfen-Längsachse 21 und eine Zapfen-Querachse 2q aufweist (vgl. Fig. 2). Diese beiden Achsen stehen senkrecht aufeinander. Dargestellt worden ist auch, daß der Führungszapfen als unrunder Rundbolzen ausgeführt werden kann, wobei er zwei Flachseiten 2a und 2b erhält, die parallel zur Zapfen-Längsachse 21 zu liegen kommen. Wesentlich für die Gestalt des unrunden Zapfens ist also die Unsymmetrie in Längs- und Querrichtung. Haben Zapfen im Stand der Technik regelmäßig eine runde Bolzen-Form ist es gemäß der Erfindung gerade beabsichtigt, diese Rotationssymmetrie zu vermeiden. Betont werden soll deshalb, daß mit der Erfindung ein Führungszapfen eingesetzt wird, der in gezeigter Längs- und Querrichtung unsymmetrisch ist, mithin unrund ist. Eine andere als die unrunde in Längs- und Querrichtung unsymmetrische Form meint die Erfindung nicht, wenn sie von dem unrunden Führungszapfen spricht.It has been mentioned that the guide pin 2 has a pin longitudinal axis 21 and a pin transverse axis 2q (see FIG. 2). These two axes are perpendicular to each other. It has also been shown that the guide pin can be designed as a non-circular round bolt, whereby it receives two flat sides 2a and 2b which come to lie parallel to the longitudinal axis 21 of the pin. The asymmetry in the longitudinal and transverse directions is therefore essential for the shape of the non-circular pin. If pins in the prior art regularly have a round bolt shape, the intention of the invention is precisely to avoid this rotational symmetry. It should therefore be emphasized that the invention uses a guide pin which is asymmetrical in the longitudinal and transverse directions shown, and is therefore out of round. The invention does not mean a shape other than the non-round in the longitudinal and transverse direction asymmetrical when it speaks of the non-round guide pin.

Claims (7)

  1. A fitting for a tiltable, moveable panel (100) which can be immobilised in parallel position, characterised in that
    (a) a guide plate (5) disposed on a carriage (101) has a guide slot (4) in which a rotationally asymmetrical, especially axially asymmetrical, non-round guide pin (2) is slidably held, and
    (b) the guide slot (4) is elongate and at one end (4a) has a transitional slope (1) disposed opposite a fixing recess (3).
  2. A fitting according to claim 1, wherein the guide pin (2) is flat on two sides (2a, 2b) and has a slightly convex external curvature on the remaining sides (2c, 2d).
  3. A fitting according to claim 1 or 2, wherein the fixing recess (3) is dimensioned so that
    (a) the convex curved parts of the guide pin (2) can be fixed between the front end (4a) of the guide slot (4) and a nose or projection (3a) disposed opposite the transitional slope (1) and
    (b) in its transverse direction (2q) from one flat side (2a) to the opposite flat side (2b) the guide pin (2) can be received by the fixing recess (3), that is when the fitting is in the position where the panel is moved and immobilised in parallel position.
  4. A fitting according to claim 2 or 3, wherein the distance between the flat sides (2a, 2b) of the guide pin (2) and the mutual alignment and spacing of the transitional slope (1) and the projection (3a) are adjusted to one another so that the centre plane (21) half way between the flat sides (2a, 2b) of the guide pin (2) has already passed the projection (3a) when the guide pin (2) leaves the transitional slope (1) in the direction towards the fixing recess (3).
  5. A fitting according to any of claims 2 to 4, wherein the guide slot (4; 4a, 4b) at the rear end (4b) has a width approximately equal to the distance between the flat sides (2a, 2b) of the guide pin (2) (that is the transverse axis 2q of the pin) and widens in the direction towards the front end (4a) towards the transitional slope (1).
  6. A fitting according to any of the preceding claims wherein
    (a) a pressure spring (8) is disposed on an extension arm (10) pivotably connected to the carriage (101), and
    (b) a rear abutment (9) is provided on a control arm (6) bearing the guide pin (2; 2a, 2b) and the pressure spring (8) resiliently abuts it (only) when the guide pin (2) reaches and remains in the fixing recess (3) (parallel immobilisation - open position - of the panel).
  7. A fitting according to claim 6, wherein the spring (8) is interchangeably held in the extension arm (10).
EP94105171A 1993-04-06 1994-03-31 Fitting for a sliding wing with non-circular guide pin Expired - Lifetime EP0619410B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE9305261U 1993-04-06
DE9305261U DE9305261U1 (en) 1993-04-06 1993-04-06 Sliding sash fitting with non-circular guide pin

Publications (2)

Publication Number Publication Date
EP0619410A1 EP0619410A1 (en) 1994-10-12
EP0619410B1 true EP0619410B1 (en) 1997-03-12

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Application Number Title Priority Date Filing Date
EP94105171A Expired - Lifetime EP0619410B1 (en) 1993-04-06 1994-03-31 Fitting for a sliding wing with non-circular guide pin

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EP (1) EP0619410B1 (en)
DE (2) DE9305261U1 (en)

Cited By (5)

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WO2010079461A2 (en) 2009-01-11 2010-07-15 Hautau Gmbh Compact carriage for a longitudinally movable, heavy door leaf
DE102009004013A1 (en) 2009-01-11 2010-07-22 Hautau Gmbh Carriage for longitudinally moving leaf at window or door, into parallel supported position, has dual bolts as upwardly protruding projections detached from engaged position and as downwardly protruding projections at control arm end region
EP2216472A2 (en) 2009-01-11 2010-08-11 HAUTAU GmbH Compact carriage for a leaf for longitudinal movement of the leaf in a parallel position
DE102009061095B3 (en) * 2009-01-11 2016-02-18 Hautau Gmbh Carriage for a wing for longitudinally moving the wing in a parallel parked position
DK201470766A1 (en) * 2014-12-05 2016-06-27 Vkr Holding As Sliding door or window assembly with a low bottom sill height

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EP1959080B1 (en) 2007-02-15 2017-12-27 HAUTAU GmbH Fitting for a sliding leaf of a door or window
CN103477010B (en) 2010-12-11 2016-06-29 豪塔马有限责任公司 For the handware of mobile sashes that can move in parallel on door frame and the window with door frame and sash
DE102011000164B3 (en) * 2011-01-16 2012-03-22 Hautau Gmbh Fitting for e.g. sliding wing of building, has energy storage units that absorb and store energy during pivoting movement of pivotable positioning arms from closing position after one of arms is locked in tilted out condition
DE102014212463A1 (en) * 2014-06-27 2015-12-31 Roto Frank Ag Carriage assembly with a spring recess and sliding door, sliding window or the like with such a carriage assembly
DE102014212461B3 (en) * 2014-06-27 2015-08-13 Roto Frank Ag Carriage assembly with an eccentric control pin and sliding or sliding window with such a carriage assembly
DE102015222116B3 (en) * 2015-11-10 2016-11-24 Roto Frank Ag Ausstellscherenanordnung and sliding or sliding windows with such Ausstellscherenanordnung

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Publication number Priority date Publication date Assignee Title
DE3234677C2 (en) * 1982-09-18 1986-10-23 Gretsch-Unitas GmbH Baubeschläge, 7257 Ditzingen Fitting for an at least parallel hinged wing of a window, door or the like.
ATE141991T1 (en) * 1991-09-13 1996-09-15 Hautau Gmbh W FITTING FOR INSB. FORCED TILTING AND PARALLEL STABLE WINGS
DE9112078U1 (en) * 1991-09-27 1991-12-05 Siegenia-Frank Kg, 5900 Siegen Opening device for the wings of windows, doors, etc.

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010079461A2 (en) 2009-01-11 2010-07-15 Hautau Gmbh Compact carriage for a longitudinally movable, heavy door leaf
DE102009004013A1 (en) 2009-01-11 2010-07-22 Hautau Gmbh Carriage for longitudinally moving leaf at window or door, into parallel supported position, has dual bolts as upwardly protruding projections detached from engaged position and as downwardly protruding projections at control arm end region
EP2216472A2 (en) 2009-01-11 2010-08-11 HAUTAU GmbH Compact carriage for a leaf for longitudinal movement of the leaf in a parallel position
DE102009004013B4 (en) * 2009-01-11 2012-04-19 Hautau Gmbh Compact carriage for a wing for longitudinally moving the wing in a parallel-parked position
EP2538009A2 (en) 2009-01-11 2012-12-26 HAUTAU GmbH Compact carriage for a wing and method for longitudinal movement of the wing in a parallel offset and secured position
DE102009061095B3 (en) * 2009-01-11 2016-02-18 Hautau Gmbh Carriage for a wing for longitudinally moving the wing in a parallel parked position
EP2538009A3 (en) * 2009-01-11 2016-04-20 HAUTAU GmbH Compact carriage for a wing and method for longitudinal movement of the wing in a parallel offset and secured position
DE202009019144U1 (en) 2009-01-11 2017-02-03 Hautau Gmbh Carriage for a wing for longitudinally moving the wing in a parallel parked position
EP3216959A1 (en) 2009-01-11 2017-09-13 HAUTAU GmbH Carriage for a leaf for longitudinal movement of the leaf in a parallel situation
DK201470766A1 (en) * 2014-12-05 2016-06-27 Vkr Holding As Sliding door or window assembly with a low bottom sill height
DK178574B1 (en) * 2014-12-05 2016-07-04 Vkr Holding As Sliding door or window assembly with a low bottom sill height

Also Published As

Publication number Publication date
DE9305261U1 (en) 1993-06-17
EP0619410A1 (en) 1994-10-12
DE59401993D1 (en) 1997-04-17

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