EP3201413A1 - Fitting arrangement - Google Patents

Fitting arrangement

Info

Publication number
EP3201413A1
EP3201413A1 EP15762616.9A EP15762616A EP3201413A1 EP 3201413 A1 EP3201413 A1 EP 3201413A1 EP 15762616 A EP15762616 A EP 15762616A EP 3201413 A1 EP3201413 A1 EP 3201413A1
Authority
EP
European Patent Office
Prior art keywords
wing
doing
carriage
fitting arrangement
arrangement according
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.)
Granted
Application number
EP15762616.9A
Other languages
German (de)
French (fr)
Other versions
EP3201413B1 (en
Inventor
Marco MÖSL
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.)
Maco Technologie GmbH
Original Assignee
Maco Technologie 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 Maco Technologie GmbH filed Critical Maco Technologie GmbH
Publication of EP3201413A1 publication Critical patent/EP3201413A1/en
Application granted granted Critical
Publication of EP3201413B1 publication Critical patent/EP3201413B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • E05D15/56—Suspension arrangements for wings with successive different movements
    • E05D15/565—Suspension arrangements for wings with successive different movements for raising wings before sliding
    • 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
    • E05D15/06—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/0621—Details, e.g. suspension or supporting guides
    • E05D15/066—Details, e.g. suspension or supporting guides for wings supported at the bottom
    • E05D15/0665—Details, e.g. suspension or supporting guides for wings supported at the bottom on wheels with fixed axis
    • E05D15/0669—Details, e.g. suspension or supporting guides for wings supported at the bottom on wheels with fixed axis with height adjustment
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00—Constructional elements; Accessories therefor
    • E05Y2201/60—Suspension or transmission members; Accessories therefor
    • E05Y2201/622—Suspension or transmission members elements
    • E05Y2201/638—Cams; Ramps
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2600/00—Mounting or coupling arrangements for elements provided for in this subclass
    • E05Y2600/10—Adjustable
    • E05Y2600/12—Adjustable by manual operation
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2800/00—Details, accessories and auxiliary operations not otherwise provided for
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Type of wing
    • E05Y2900/148—Windows

Definitions

  • the present invention relates to a fitting arrangement for a lift-slide element such as a lift-slide door or a lift-and-slide window comprising a frame and a movable along a lower track in a direction of displacement relative to the frame wings, with at least one A carriage having a carriage frame and at least one roller mounted on the carriage frame, and a lift mechanism operable by a drive rod of the fitting assembly to lift the wing relative to the carriage frame from a lowered position to a raised position in which a lower surface of the wing is separated by an air gap of the track is spaced.
  • a lift-slide element such as a lift-slide door or a lift-and-slide window
  • Such lifting-sliding elements find, for example in the form of large patio doors or windows increasing popularity.
  • the direction of displacement is horizontal when the lift-slide element is installed.
  • several carriages are arranged in a formed on the underside of the wing receiving groove, the rollers roll directly on the lower track.
  • one or more carriages could be arranged at the top of the wing, the rollers roll on a suspension rail.
  • the lower track is in such a configuration z. B. provided only as Absetz phenomenon.
  • the underside of the wing is seated in the lowered position on the track. While in such an embodiment, the wing in a closed position with its underside immovably on the bo seated side or formed on a frame base or the like raceway can be raised by pivoting an actuating lever of the wings relative to the carriage frame, whereby the air gap is formed and the wing can be moved by means of the rollers.
  • a seating of the underside of the wing on the track in the lowered position is not mandatory. That is, the wing can be supported in principle in the lowered position by the rollers. In this case, the underside of the wing is also spaced in the lowered position by an air gap from the raceway. However, this is smaller than the air gap which exists in the raised position of the wing between the underside of the wing and the raceway.
  • the carriage frame may be any carrier for supporting the rollers. That is, the carriage frame does not necessarily have to be frame-like in the sense that it has a closed shape.
  • the carriage frame could be formed by two spaced-apart flat bars, which are interconnected by a spacer or by the axes of the rollers themselves.
  • the air gap does not necessarily have to be recognized as such from the side. For example, he could run labyrinthine.
  • the term "air gap" is intended merely to express that each section of the underside of the wing is slightly removed from the directly opposite section of the lower track.
  • the assembly of lifting-sliding elements is so far connected with difficulties, on the one hand, the Anhebeweg and thus the air gap should be as low as possible, on the other hand, a grinding of the wing bottom is to be avoided at the lower track. If the air gap is not suitable in this regard, the fitting assembly has to be solved in a complicated manner from the wing and re-attached. It is an object of the invention to simplify the assembly of lift-slide elements. The object is achieved by a fitting arrangement with the features of claim 1.
  • the lifting mechanism comprises a guide slot extending obliquely to the direction of displacement and a support element guided in the guide slot, wherein the guide slot is formed on a fixedly connected to the wing member and the support member is arranged on the carriage frame, or vice versa, and wherein for adjusting Air gap an adjusting element is provided by means of which the position of the support member in the guide slot is independent of an actuation of the drive rod changeable.
  • the associated with the wing member on which the guide slot is arranged in this case can be displaced in the horizontal direction relative to the wing.
  • the term "firmly connected" thus refers only to the vertical direction. Since the component having the guide slot is wing-resistant in the vertical direction and the carrier element is fixed to the carriage frame in the vertical direction, a relative horizontal movement between the carrier element and the guide link can be converted into a lifting or lowering movement of the wing due to the obliquely running guide link.
  • a user can thus adjust the air gap on site by means of the adjusting element after mounting the fitting arrangement or after installation of the lifting-sliding element. In this way, the distance between the lower track and the underside of the wing can be minimized in a fully assembled lift-slide element.
  • the adjustment can be done on the built-in sash, that is, it is also possible to make subsequent adjustments. Changing the mounting position NEN the fitting arrangement is not required. Thus, the adjustment can be done very quickly and easily.
  • an "oblique" course of the guide slot does not necessarily mean a straight-line oblique course. Rather, to be understood under a slanted to the direction of the guide slot such a guide slot, which is not parallel and not perpendicular to the direction of displacement.
  • the guide slot can also be curved as a whole, as long as infinitesimal sections of the guide slot each run obliquely to the displacement direction.
  • the adjusting element is arranged such that it can be actuated from a narrow side of the wing.
  • the narrow sides of the wing are normally not in the field of vision of a user, so that the corresponding lifting-sliding element is hardly impaired optically by the adjusting element.
  • the control element can be accommodated, for example, together with a carriage in a provided on the underside of the wing receiving groove and accessible from the lower edge region of the corresponding narrow side. It can be provided on the narrow side of the wing cuff rail, which has a recess for performing a tool, by means of which the actuating element can be actuated.
  • the faceplate may be provided with a hole for insertion of a screwdriver or the like at the point which is arranged in accordance with the intended installation of the lifting-sliding element in front of the adjusting element.
  • the actuator can be arranged in a cavity of the wing and covered by the faceplate.
  • the support element may comprise a sliding peg, which is slidable within the guide backdrop.
  • the support element comprises a rotatable roller, since in this case the frictional forces during lifting of the wing are particularly low.
  • the rotatable roller may be mounted on a horizontal roller axle, which is arranged directly on the carriage frame.
  • the adjusting element can be designed to move the carriage frame relative to the wing in or against the displacement direction for changing the position of the support element in the guide slot. This refinement is particularly suitable for lifting and sliding elements in which a drive movement of the drive rod or a drive rod arrangement acts on the carriage in a different manner and the carriage is therefore guided displaceably on the wing anyway.
  • the adjusting element is adapted to move the carriage frame with the carriage frame connecting coupling parts against each other for moving the carriage frame when the drive rod is held.
  • the adjusting element can be designed to change the distance between a reference point of the drive rod and a reference point of the carriage frame. The actuator thus engages neither in the sliding guide of the drive rod nor in the storage of the carriage, but only in the coupling mechanism. This is favorable in terms of design.
  • a special embodiment provides in this case that a first coupling part is a lever, whose one lever end is mounted on the carriage frame and the other end of the lever has a slot through which a bearing arranged on the second coupling part bearing axis is passed, wherein by means of the adjusting element, the bearing axis within the slot is displaceable.
  • a lever which in particular can be pivoted, is often provided in the region of a corner deflection. hen to implement a vertical espagnolette movement in a horizontal carriage displacement.
  • the adjusting element can be designed as a set screw, which is received in a threaded portion of the elongated hole having lever end and acts with its shaft end, the bearing axis. This allows a particularly simple construction. In general, it is sufficient if the actuator acts on the bearing axis only in one direction, since in the opposite direction, the weight of the wing is effective and thus no active adjustment is necessary.
  • the adjusting element can be designed to displace the guide slot having bearing element relative to the wing in or against the displacement direction for changing the position of the support element in the guide slot.
  • the bearing element can be, for example, a vertically oriented plate in which an elongate recess forming the guide slot is provided. In such an embodiment, the carriage does not necessarily have to be displaceable relative to the wing, which is desirable for certain applications.
  • the adjusting element can be designed as a screw head having an adjusting screw, which is accommodated in a threaded portion of the bearing element and is supported with the screw head on a wing-fixed stop surface. Supporting the screw head in only one direction is sufficient because, as mentioned above, in the opposite direction, the weight of the wing provides for automatic tracking.
  • the bearing element can be guided by means of a sliding guide on a holding body attached to the wing, on which the stop surface is formed or a component having the stop surface is fastened.
  • the guide of the bearing element can be accomplished by means of a T-groove or dovetail groove formed on the holding body.
  • the carriage may have two rollers spaced from one another with respect to the direction of displacement, the carrier element being mounted between the rollers on the carriage frame. It is then per carriage frame only one support element required without the risk of tilting of the carriage. In principle, a single roller could be mounted between two support elements on the carriage frame.
  • a further embodiment of the invention provides that at least two, preferably exactly two, with respect to the direction of displacement spaced-standing carriage are provided, wherein the lifting mechanism has respective carriage associated arrangements of guide slot and support member, and wherein the positions of the support members in the guide slots can be changed together by means of the adjusting element.
  • the underside of the wing is movable by means of the adjusting element while maintaining its horizontal orientation up and down, which facilitates the setting process.
  • the carriage frame of the carriage can be coupled together for a common sliding movement by means of a rigid, in particular rod-shaped, connecting member. This allows a particularly simple and inexpensive execution of a jointly displaceable carriage assembly.
  • Another embodiment of the invention provides an additional actuator configured to vary the relative positions of the support member and the guide link in one of the assemblies while maintaining the relative positions of the support member and the guide link in the other arrangement. This makes it possible not only to move the bottom of the wing in the vertical direction, but also to change their inclination. Thus, a deviation of the parallelism between the wing bottom and the lower raceway, which consists after the assembly of the lift-slide element can be compensated.
  • one of the adjusting elements is designed for displacing the carriage frame relative to the wing and the other adjusting element is designed for displacing a bearing block having the guide slot with respect to the wing.
  • an adjusting element for adjusting the thickness of the air gap and a further adjusting element for correcting the inclination of the wing underside can be used. In this way, a particularly precise adjustment of the air gap is possible.
  • FIG. 1 is a partially cutaway perspective view of a provided with a fitting assembly according to the invention lifting-sliding element in an unadjusted ground state.
  • Fig. 2 shows the lifting-pushing element according to FIG. 1 in one
  • FIG. 3 is an enlarged detail view of that shown in FIG. 1.
  • Fitting arrangement which shows a front carriage in more detail.
  • Fig. 4 shows the front carriage in a relation to FIG. 3 adjusted state.
  • FIG. 5 is an enlarged detail view of that shown in FIG.
  • FIG. 6 shows the rear carriage in a relation to FIG. 5 adjusted state.
  • Fig. 7 shows the rear carriage from a narrow side of the
  • Fig. 8 shows the rear carriage from a narrow side of the
  • Fig. 1 and 2 show the lower portion of a lift-slide door 1 1, which has a frame, not shown, and a relative to the frame in a horizontal displacement direction V movable wings 15.
  • wing 15 Of the wing 15 is shown in Fig. 1 and 2 especially the front narrow side 75, the rear narrow side 76 and the wing bottom 77 can be seen.
  • an arrangement of two carriages 17a, 17b is provided, which roll by means of rollers 27 on a guide rail 19 arranged below the wing 15.
  • the guide rail 19 may form part of the window frame or be formed as a separate component, for example as a floor sill.
  • the top of the guide rail 19 forms a raceway 21, along which the wing 15 by means of the carriage 17a, 17b is displaceable.
  • the two carriages 17a, 17b are coupled to each other by means of a horizontal connecting rod 22.
  • the carriages 17a, 17b including the connecting rod 22 are accommodated in a lower-side receptacle 23 of the wing 15.
  • Each of the carriages 17a, 17b has a carriage frame 25 on which two with respect to the direction of displacement V spaced rollers 27 are rotatably mounted. In Fig. 1 and 2, only one roller 27 per carriage 17a, 17b visible due to the partial sectional view.
  • a support element 29 in the form of a rotatable roller between the rollers 27 on the carriage frame 25 is mounted in each of the two carriages 17a, 17b.
  • the wing 15 is to be opened to the left and close to the right. Accordingly, in the following, the carriage 17a located on the right in FIG. 1 is referred to as the "front carriage” and the carriage 17b located on the left in FIG. 1 is referred to as the "rear carriage”.
  • the support members 29 are guided in respective guide slots 31 which extend obliquely to the direction of displacement V and are connected in the vertical direction fixed to the wing 15.
  • the carriage frames 25 of both carriages 17a, 17b are displaceable in the horizontal direction relative to the wing 15.
  • the mutually coupled carriage frames 25 are shifted from the base position shown in Fig. 3 relative to the wing 15 to the right, takes place due to the oblique orientation of the guide slots 31, a lifting of the wing 15 relative to the guide rail 19.
  • a user can such a common horizontal Displacement of the carriages 17a, 17b accomplish by operation of a drive rod assembly, not shown in the figures, which is coupled via a Eckum- deflection 33 with the carriage frame 25 of the front carriage 17a.
  • the guide slots 31 and the guided in the guide slots 31 support members 29 of the carriage 17a, 17b thus form a lifting mechanism 35 which allows a user, for example, by operating a provided on the wing 15 handle (not shown) the wing 15 from a lowered position, in which an underside of the wing 15 is firmly and immovably seated on the track 21, in a raised position in which the underside of the wing 15 by an air gap 37 (Fig. 2) is spaced from the raceway 21 to transfer.
  • a front adjusting screw 39 which can be seen in FIGS. 3 and 4 is provided for the front carriage 17a, which can be actuated from the front narrow side 75 of the wing 15 by means of a handpiece 43 provided in a cuff rail 40.
  • the front adjusting screw 39 it is possible to move a lever 45 and a deflection frame 47, which couple the drive rod to the carriage frame 25 of the front carriage 17a, against each other.
  • the first lever end 49 of the lever 45 is mounted on the carriage frame 25, while the second end of the lever 50 has a slot 51 through which a mounted on the deflection frame 47 bearing shaft 53 is passed.
  • the front adjusting screw 39 is received in a threaded portion of the second lever end 50 and acted with its shaft end the bearing axis 53.
  • the bearing axis 53 can be moved within the slot 51 to the left, whereby at a fixed drive rod and thus stationary deflection frame 47, the carriage frame 25 is pulled to the right, for example into the position shown in FIG.
  • the carriage frame 25 of the front running 17a pulls on the connecting rod 22 (FIG.
  • the two carriages 17a, 17b can also be adjusted independently of one another.
  • a visible in Fig. 5-8 rear adjusting screw 59 is provided, by means of which the position of the support member 29 of the rear carriage 17 b in the associated guide slot 31 can be changed without moving the front carriage 17 a.
  • the rear adjusting screw 59 does not act on the carriage frame 25, but on a bearing element 61, in which the guide slot 31 is formed.
  • the bearing element 61 is the upper side in a non-visible guide such.
  • the turning of the rear adjusting screw 59 does not affect the position of the front carriage 17a, and hence the wing 15 does not act in the region of the front carriage 17a is raised. As a result, the wing 15 is thus slightly tilted with respect to the horizontal. Similar to the front carriage 17a, the actuation of the rear adjusting screw 59 takes place by means of a hand tool 43 from a narrow side of the wing 15 - here from the rear narrow side 76. For performing the hand tool 43, in turn, a suitable recess is provided, which is not shown in Fig. 5-8.
  • a fitter can adjust the air gap 37 in a desired manner by operating the front adjusting screw 39 and the rear adjusting screw 59 after installation of the lifting-sliding door 1 1.
  • a parallel displacement of the wing 15 is brought about exclusively in the vertical direction and by means of the rear adjusting screw 59 a tilting of the wing 15 is effected. This allows a particularly fast and precise adjustment of the air gap 37.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Support Devices For Sliding Doors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Power-Operated Mechanisms For Wings (AREA)

Abstract

The invention relates to a fitting arrangement for a lifting-sliding element, which comprises a window frame and a blade that is displaceable along a track in a direction of displacement. The fitting arrangement comprises at least one carriage, which has a trolley frame and at least one roller mounted on the trolley frame, and a lifting mechanism for raising the blade in relation to the trolley frame from a lowered position to a raised position in which an underside of the blade is spaced apart from the track by an air gap. The lifting mechanism comprises a guide slot which runs obliquely with respect to the direction of displacement and a carrier element directed in the guide slot, wherein an adjusting element is provided for adjusting the air gap, by means of which the position of the carrier element in the guide slot can be changed.

Description

BESCHLAGANORDNUNG  FITTING ARRANGEMENT
Die vorliegende Erfindung betrifft eine Beschlaganordnung für ein Hebe-Schiebe- Element wie eine Hebe-Schiebe-Tür oder ein Hebe-Schiebe-Fenster, das einen Blendrahmen und einen entlang einer unteren Laufbahn in einer Verschieberichtung gegenüber dem Blendrahmen verschiebbaren Flügel umfasst, mit wenigstens einem Laufwagen, der einen Wagenrahmen und zumindest eine an dem Wagenrahmen gelagerte Laufrolle aufweist, und einen durch eine Treibstange der Beschlaganordnung betätigbaren Hebemechanismus zum Anheben des Flügels gegenüber dem Wagenrahmen von einer abgesenkten Stellung in eine angehobene Stellung, in welcher eine Unterseite des Flügels durch einen Luftspalt von der Laufbahn beabstandet ist. The present invention relates to a fitting arrangement for a lift-slide element such as a lift-slide door or a lift-and-slide window comprising a frame and a movable along a lower track in a direction of displacement relative to the frame wings, with at least one A carriage having a carriage frame and at least one roller mounted on the carriage frame, and a lift mechanism operable by a drive rod of the fitting assembly to lift the wing relative to the carriage frame from a lowered position to a raised position in which a lower surface of the wing is separated by an air gap of the track is spaced.
Derartige Hebe-Schiebe-Elemente finden beispielsweise in Form von großflächigen Terrassentüren oder -fenstern zunehmende Verbreitung. Die Verschieberichtung verläuft bei eingebautem Hebe-Schiebe-Element horizontal. Häufig sind bei solchen Hebe-Schiebe-Elementen mehrere Laufwagen in einer an der Unterseite des Flügels ausgebildeten Aufnahmenut angeordnet, wobei die Laufrollen direkt auf der unteren Laufbahn abrollen. Grundsätzlich könnten auch ein oder mehrere Laufwagen an der Oberseite des Flügels angeordnet sein, wobei die Laufrollen an einer Hängeschiene abrollen. Die untere Laufbahn ist bei einer solchen Ausgestal- tung z. B. lediglich als Absetzfläche vorgesehen. Such lifting-sliding elements find, for example in the form of large patio doors or windows increasing popularity. The direction of displacement is horizontal when the lift-slide element is installed. Frequently, in such lifting-sliding elements several carriages are arranged in a formed on the underside of the wing receiving groove, the rollers roll directly on the lower track. In principle, one or more carriages could be arranged at the top of the wing, the rollers roll on a suspension rail. The lower track is in such a configuration z. B. provided only as Absetzfläche.
Es kann vorgesehen sein, dass die Unterseite des Flügels in der abgesenkten Stellung auf der Laufbahn aufsitzt. Während bei einer solchen Ausgestaltung der Flügel in einer Schließstellung mit seiner Unterseite unverschiebbar auf der bo- denseitigen bzw. an einem Rahmenunterteil oder dergleichen gebildeten Laufbahn aufsitzt, kann durch Verschwenken eines Betätigungshebels der Flügel gegenüber dem Wagenrahmen angehoben werden, wodurch der Luftspalt gebildet wird und der Flügel mittels der Laufrollen verschoben werden kann. Ein Aufsitzen der Un- terseite des Flügels auf der Laufbahn in der abgesenkten Stellung ist jedoch nicht zwingend. Das heißt der Flügel kann im Prinzip auch in der abgesenkten Stellung durch die Laufrollen getragen sein. In diesem Fall ist die Unterseite des Flügels auch in der abgesenkten Stellung durch einen Luftspalt von der Laufbahn beabstandet. Dieser ist jedoch kleiner als derjenige Luftspalt, welcher in der angehobe- nen Stellung des Flügels zwischen der Unterseite des Flügels und der Laufbahn besteht. It can be provided that the underside of the wing is seated in the lowered position on the track. While in such an embodiment, the wing in a closed position with its underside immovably on the bo seated side or formed on a frame base or the like raceway can be raised by pivoting an actuating lever of the wings relative to the carriage frame, whereby the air gap is formed and the wing can be moved by means of the rollers. However, a seating of the underside of the wing on the track in the lowered position is not mandatory. That is, the wing can be supported in principle in the lowered position by the rollers. In this case, the underside of the wing is also spaced in the lowered position by an air gap from the raceway. However, this is smaller than the air gap which exists in the raised position of the wing between the underside of the wing and the raceway.
Bei dem Wagenrahmen kann es sich um einen beliebigen Träger zur Lagerung der Laufrollen handeln. Das heißt der Wagenrahmen muss nicht zwingend in dem Sinne rahmenartig sein, dass er eine geschlossene Form aufweist. Beispielsweise könnte der Wagenrahmen durch zwei voneinander beabstandete Flacheisen gebildet sein, die durch einen Abstandhalter oder auch durch die Achsen der Laufrollen selbst miteinander verbunden sind. Es ist auch darauf hinzuweisen, dass der Luftspalt nicht unbedingt von der Seite aus als solcher zu erkennen sein muss. Z. B. könnte er labyrinthartig verlaufen. Der Begriff "Luftspalt" soll lediglich zum Ausdruck bringen, dass jeder Abschnitt der Unterseite des Flügels um einen geringfügigen Betrag von dem direkt gegenüberliegenden Abschnitt der unteren Laufbahn entfernt ist. Die Montage von Hebe-Schiebe-Elementen ist insofern mit Schwierigkeiten verbunden, als einerseits der Anhebeweg und somit der Luftspalt möglichst gering ausfallen sollen, andererseits aber ein Schleifen der Flügelunterseite an der unteren Laufbahn zu vermeiden ist. Falls der Luftspalt in dieser Hinsicht nicht passend ist, muss die Beschlaganordnung in umständlicher Weise vom Flügel gelöst und wieder neu angebracht werden. Es ist eine Aufgabe der Erfindung, die Montage von Hebe-Schiebe-Elementen zu vereinfachen. Die Lösung der Aufgabe erfolgt durch eine Beschlaganordnung mit den Merkmalen des Anspruchs 1 . The carriage frame may be any carrier for supporting the rollers. That is, the carriage frame does not necessarily have to be frame-like in the sense that it has a closed shape. For example, the carriage frame could be formed by two spaced-apart flat bars, which are interconnected by a spacer or by the axes of the rollers themselves. It should also be noted that the air gap does not necessarily have to be recognized as such from the side. For example, he could run labyrinthine. The term "air gap" is intended merely to express that each section of the underside of the wing is slightly removed from the directly opposite section of the lower track. The assembly of lifting-sliding elements is so far connected with difficulties, on the one hand, the Anhebeweg and thus the air gap should be as low as possible, on the other hand, a grinding of the wing bottom is to be avoided at the lower track. If the air gap is not suitable in this regard, the fitting assembly has to be solved in a complicated manner from the wing and re-attached. It is an object of the invention to simplify the assembly of lift-slide elements. The object is achieved by a fitting arrangement with the features of claim 1.
Erfindungsgemäß umfasst der Hebemechanismus eine schräg zur Verschieberichtung verlaufende Führungskulisse und ein in der Führungskulisse geführtes Trag- element, wobei die Führungskulisse an einem fest mit dem Flügel verbundenen Bauteil ausgebildet ist und das Tragelement an dem Wagenrahmen angeordnet ist, oder umgekehrt, und wobei zum Einstellen des Luftspalts ein Stellelement vorgesehen ist, mittels dessen die Position des Tragelements in der Führungskulisse unabhängig von einer Betätigung der Treibstange veränderbar ist. According to the invention, the lifting mechanism comprises a guide slot extending obliquely to the direction of displacement and a support element guided in the guide slot, wherein the guide slot is formed on a fixedly connected to the wing member and the support member is arranged on the carriage frame, or vice versa, and wherein for adjusting Air gap an adjusting element is provided by means of which the position of the support member in the guide slot is independent of an actuation of the drive rod changeable.
Das mit dem Flügel verbundene Bauteil, an welchem die Führungskulisse angeordnet ist, kann hierbei in horizontaler Richtung gegenüber dem Flügel verschiebbar sein. Der Begriff "fest verbunden" bezieht sich also nur auf die vertikale Richtung. Da das die Führungskulisse aufweisende Bauteil in vertikaler Richtung flü- gelfest ist und das Tragelement in vertikaler Richtung wagenrahmenfest ist, kann aufgrund der schräg verlaufenden Führungskulisse eine relative Horizontalbewegung zwischen dem Tragelement und der Führungskulisse in eine Hebe- oder Senkbewegung des Flügels umgesetzt werden. Ein Benutzer kann somit mittels des Stellelements nach der Montage der Beschlaganordnung bzw. nach dem Einbau des Hebe-Schiebe-Elements den Luftspalt vor Ort einstellen. Auf diese Weise kann bei einem fertig montierten Hebe-Schiebe-Element der Abstand zwischen der unteren Laufbahn und der Unterseite des Flügels minimiert werden. Die Verstellung kann am eingebauten Flügel erfolgen, das heißt es ist auch möglich, nachträgliche Justierarbeiten vorzunehmen. Ein Verändern der Anschraubpositio- nen der Beschlaganordnung ist nicht erforderlich. Somit kann der Einstellvorgang besonders schnell und einfach erfolgen. The associated with the wing member on which the guide slot is arranged, in this case can be displaced in the horizontal direction relative to the wing. The term "firmly connected" thus refers only to the vertical direction. Since the component having the guide slot is wing-resistant in the vertical direction and the carrier element is fixed to the carriage frame in the vertical direction, a relative horizontal movement between the carrier element and the guide link can be converted into a lifting or lowering movement of the wing due to the obliquely running guide link. A user can thus adjust the air gap on site by means of the adjusting element after mounting the fitting arrangement or after installation of the lifting-sliding element. In this way, the distance between the lower track and the underside of the wing can be minimized in a fully assembled lift-slide element. The adjustment can be done on the built-in sash, that is, it is also possible to make subsequent adjustments. Changing the mounting position NEN the fitting arrangement is not required. Thus, the adjustment can be done very quickly and easily.
Unter einem "schrägen" Verlauf der Führungskulisse ist nicht zwingend ein gerad- linig schräger Verlauf zu verstehen. Vielmehr soll unter einer schräg zur Verschieberichtung verlaufenden Führungskulisse eine solche Führungskulisse zu verstehen sein, die nicht parallel und nicht rechtwinklig zu der Verschieberichtung verläuft. Die Führungskulisse kann also insgesamt auch gekrümmt verlaufen, solange infinitesimale Abschnitte der Führungskulisse jeweils schräg zur Verschieberich- tung verlaufen. An "oblique" course of the guide slot does not necessarily mean a straight-line oblique course. Rather, to be understood under a slanted to the direction of the guide slot such a guide slot, which is not parallel and not perpendicular to the direction of displacement. Thus, the guide slot can also be curved as a whole, as long as infinitesimal sections of the guide slot each run obliquely to the displacement direction.
Vorzugsweise ist das Stellelement derart angeordnet, dass es von einer Schmalseite des Flügels aus betätigbar ist. Die Schmalseiten des Flügels liegen nämlich im Normalfall nicht im Sichtbereich eines Benutzers, so dass das entsprechende Hebe-Schiebe-Element durch das Stellelement optisch kaum beeinträchtigt ist. Das Stellelement kann beispielsweise gemeinsam mit einem Laufwagen in einer an der Unterseite des Flügels vorgesehenen Aufnahmenut untergebracht und über den unteren Randbereich der entsprechenden Schmalseite aus zugänglich sein. Es kann eine an der Schmalseite des Flügels angeordnete Stulpschiene vorgesehen sein, welche eine Aussparung zum Durchführen eines Werkzeugs aufweist, mittels welchem das Stellelement betätigbar ist. Beispielsweise kann die Stulpschiene an derjenigen Stelle, welche bei bestimmungsgemäßer Montage des Hebe-Schiebe-Elements vor dem Stellelement angeordnet ist, mit einem Loch zum Einführen eines Schraubendrehers oder dergleichen versehen sein. Somit kann das Stellelement in einem Hohlraum des Flügels angeordnet und durch die Stulpschiene abgedeckt sein. Preferably, the adjusting element is arranged such that it can be actuated from a narrow side of the wing. Namely, the narrow sides of the wing are normally not in the field of vision of a user, so that the corresponding lifting-sliding element is hardly impaired optically by the adjusting element. The control element can be accommodated, for example, together with a carriage in a provided on the underside of the wing receiving groove and accessible from the lower edge region of the corresponding narrow side. It can be provided on the narrow side of the wing cuff rail, which has a recess for performing a tool, by means of which the actuating element can be actuated. For example, the faceplate may be provided with a hole for insertion of a screwdriver or the like at the point which is arranged in accordance with the intended installation of the lifting-sliding element in front of the adjusting element. Thus, the actuator can be arranged in a cavity of the wing and covered by the faceplate.
Das Tragelement kann einen Gleitzapfen umfassen, der innerhalb der Führungs- kulisse gleitend verschiebbar ist. Bevorzugt ist es jedoch, dass das Tragelement eine drehbare Rolle umfasst, da hierbei die Reibungskräfte beim Anheben des Flügels besonders gering sind. Die drehbare Rolle kann an einer horizontalen Rollenachse gelagert sein, welche direkt am Wagenrahmen angeordnet ist. Das Stellelement kann dazu ausgebildet sein, zum Verändern der Position des Tragelements in der Führungskulisse den Wagenrahmen gegenüber dem Flügel in oder entgegen der Verschieberichtung zu verschieben. Diese Ausgestaltung bietet sich insbesondere bei solchen Hebe-Schiebe-Elementen an, bei welchen eine Antriebsbewegung der Treibstange bzw. einer Treibstangenanordnung verschie- bend auf den Laufwagen wirkt und der Laufwagen daher ohnehin verschiebbar am Flügel geführt ist. Es kann dann ein und derselbe Hebemechanismus sowohl zum Anheben und Absenken des Flügels durch Hebelbetätigung als auch zum Einstellen des Luftspalts nach der Montage verwendet werden. Gemäß einer Ausgestaltung der Erfindung ist das Stellelement dazu ausgebildet, zum Verschieben des Wagenrahmens bei festgehaltener Treibstange zwei die Treibstange mit dem Wagenrahmen verbindende Kopplungsteile gegeneinander zu verschieben. Mit anderen Worten kann das Stellelement dazu ausgebildet sein, den Abstand zwischen einem Bezugspunkt der Treibstange und einem Bezugs- punkt des Wagenrahmens zu verändern. Das Stellelement greift somit weder in die Schiebeführung der Treibstange noch in die Lagerung des Laufwagens ein, sondern lediglich in den Kopplungsmechanismus. Dies ist in konstruktiver Hinsicht günstig. Eine spezielle Ausgestaltung sieht hierbei vor, dass ein erstes Kopplungsteil ein Hebel ist, dessen eines Hebelende am Wagenrahmen gelagert ist und dessen anderes Hebelende ein Langloch aufweist, durch das eine am zweiten Kopplungsteil angeordnete Lagerachse hindurchgeführt ist, wobei mittels des Stellelements die Lagerachse innerhalb des Langlochs verschiebbar ist. Ein derartiger, insbe- sondere schwenkbarer Hebel ist häufig im Bereich einer Eckumlenkung vorgese- hen, um eine vertikale Treibstangenbewegung in eine horizontale Laufwagenverschiebung umzusetzen. Durch Versehen eines Hebelendes des Hebels mit einem Langloch und Verschieben der Lagerachse innerhalb des Langlochs mittels des Stellelements kann ein Mechanismus zum Einstellen des Luftspalts in einfacher Weise in eine bestehende Eckumlenkung integriert werden. The support element may comprise a sliding peg, which is slidable within the guide backdrop. However, it is preferred that the support element comprises a rotatable roller, since in this case the frictional forces during lifting of the wing are particularly low. The rotatable roller may be mounted on a horizontal roller axle, which is arranged directly on the carriage frame. The adjusting element can be designed to move the carriage frame relative to the wing in or against the displacement direction for changing the position of the support element in the guide slot. This refinement is particularly suitable for lifting and sliding elements in which a drive movement of the drive rod or a drive rod arrangement acts on the carriage in a different manner and the carriage is therefore guided displaceably on the wing anyway. One and the same lifting mechanism can then be used both to lift and lower the sash by lever actuation and to adjust the air gap after assembly. According to one embodiment of the invention, the adjusting element is adapted to move the carriage frame with the carriage frame connecting coupling parts against each other for moving the carriage frame when the drive rod is held. In other words, the adjusting element can be designed to change the distance between a reference point of the drive rod and a reference point of the carriage frame. The actuator thus engages neither in the sliding guide of the drive rod nor in the storage of the carriage, but only in the coupling mechanism. This is favorable in terms of design. A special embodiment provides in this case that a first coupling part is a lever, whose one lever end is mounted on the carriage frame and the other end of the lever has a slot through which a bearing arranged on the second coupling part bearing axis is passed, wherein by means of the adjusting element, the bearing axis within the slot is displaceable. Such a lever, which in particular can be pivoted, is often provided in the region of a corner deflection. hen to implement a vertical espagnolette movement in a horizontal carriage displacement. By providing a lever end of the lever with a slot and moving the bearing axis within the slot by means of the actuator, a mechanism for adjusting the air gap can be easily integrated into an existing corner drive.
Das Stellelement kann als Stellschraube ausgeführt sein, welche in einem Gewindeabschnitt des das Langloch aufweisenden Hebelendes aufgenommen ist und mit ihrem Schaftende die Lagerachse beaufschlagt. Dies ermöglicht eine beson- ders einfache Konstruktion. Im Allgemeinen ist es ausreichend, wenn das Stellelement die Lagerachse lediglich in einer Richtung beaufschlagt, da in der Gegenrichtung das Gewicht des Flügels wirksam ist und somit keine aktive Verstellung notwendig ist. Das Stellelement kann dazu ausgebildet sein, zum Verändern der Position des Tragelements in der Führungskulisse ein die Führungskulisse aufweisendes Lagerelement gegenüber dem Flügel in oder entgegen der Verschieberichtung zu verschieben. Bei dem Lagerelement kann es sich beispielsweise um eine vertikal ausgerichtete Platte handeln, in welcher eine längliche, die Führungskulisse bil- dende Aussparung vorgesehen ist. Bei einer solchen Ausgestaltung muss der Laufwagen nicht zwingend gegenüber dem Flügel verschiebbar sein, was für bestimmte Anwendungen wünschenswert ist. The adjusting element can be designed as a set screw, which is received in a threaded portion of the elongated hole having lever end and acts with its shaft end, the bearing axis. This allows a particularly simple construction. In general, it is sufficient if the actuator acts on the bearing axis only in one direction, since in the opposite direction, the weight of the wing is effective and thus no active adjustment is necessary. The adjusting element can be designed to displace the guide slot having bearing element relative to the wing in or against the displacement direction for changing the position of the support element in the guide slot. The bearing element can be, for example, a vertically oriented plate in which an elongate recess forming the guide slot is provided. In such an embodiment, the carriage does not necessarily have to be displaceable relative to the wing, which is desirable for certain applications.
Das Stellelement kann als eine einen Schraubenkopf aufweisende Stellschraube ausgeführt sein, welche in einem Gewindeabschnitt des Lagerelements aufgenommen ist und sich mit dem Schraubenkopf an einer flügelfesten Anschlagfläche abstützt. Das Abstützen des Schraubenkopfs in lediglich einer Richtung ist ausreichend, da wie vorstehend erwähnt in der entgegengesetzten Richtung die Gewichtskraft des Flügels für eine automatische Nachführung sorgt. Das Lagerelement kann mittels einer Gleitführung an einem am Flügel befestigten Haltekörper geführt sein, an welchem die Anschlagfläche ausgebildet oder ein die Anschlagfläche aufweisendes Bauteil befestigt ist. Beispielsweise kann die Führung des Lagerelements mittels einer am Haltekörper gebildeten T-Nut oder Schwalbenschwanznut bewerkstelligt sein. The adjusting element can be designed as a screw head having an adjusting screw, which is accommodated in a threaded portion of the bearing element and is supported with the screw head on a wing-fixed stop surface. Supporting the screw head in only one direction is sufficient because, as mentioned above, in the opposite direction, the weight of the wing provides for automatic tracking. The bearing element can be guided by means of a sliding guide on a holding body attached to the wing, on which the stop surface is formed or a component having the stop surface is fastened. For example, the guide of the bearing element can be accomplished by means of a T-groove or dovetail groove formed on the holding body.
Der Laufwagen kann zwei bezüglich der Verschieberichtung voneinander beab- standete Laufrollen aufweisen, wobei das Tragelement zwischen den Laufrollen am Wagenrahmen angebracht ist. Es ist dann pro Wagenrahmen lediglich ein Tragelement erforderlich, ohne dass die Gefahr eines Verkippens des Laufwagens besteht. Prinzipiell könnte auch eine einzelne Laufrolle zwischen zwei Tragelementen am Wagenrahmen gelagert sein. The carriage may have two rollers spaced from one another with respect to the direction of displacement, the carrier element being mounted between the rollers on the carriage frame. It is then per carriage frame only one support element required without the risk of tilting of the carriage. In principle, a single roller could be mounted between two support elements on the carriage frame.
Eine weitere Ausführungsform der Erfindung sieht vor, dass wenigstens zwei, vorzugsweise genau zwei, bezüglich der Verschieberichtung voneinander beab- standete Laufwagen vorgesehen sind, wobei der Hebemechanismus jeweilige den Laufwagen zugeordnete Anordnungen aus Führungskulisse und Tragelement aufweist, und wobei die Positionen der Tragelemente in den Führungskulissen mittels des Stellelements gemeinsam veränderbar sind. Somit ist lediglich die Betätigung eines einzelnen Stellelements nötig, um die Positionen aller Laufwagen anzupassen. Die Unterseite des Flügels ist mittels des Stellelements unter Beibehaltung ihrer horizontalen Ausrichtung auf und ab bewegbar, was den Einstellvorgang erleichtert. Die Wagenrahmen der Laufwagen können für eine gemeinsame Verschiebebewegung mittels eines starren, insbesondere stangenförmigen, Verbindungsbauteils miteinander gekoppelt sein. Dies ermöglicht eine besonders einfache und kostengünstige Ausführung einer gemeinsam verschiebbaren Laufwagen-Anordnung. Eine weitere Ausführungsform der Erfindung sieht ein zusätzliches Stellelement vor, welches zum Verändern der relativen Positionen von Tragelement und Führungskulisse bei einer der Anordnungen unter Beibehaltung der relativen Positionen von Tragelement und Führungskulisse bei der anderen Anordnung ausgebil- det ist. Dadurch ist es möglich, die Unterseite des Flügels nicht nur in vertikaler Richtung zu bewegen, sondern auch deren Neigung zu verändern. Somit kann auch eine Abweichung der Parallelität zwischen der Flügelunterseite und der unteren Laufbahn, welche nach der Montage des Hebe-Schiebe-Elements besteht, kompensiert werden. A further embodiment of the invention provides that at least two, preferably exactly two, with respect to the direction of displacement spaced-standing carriage are provided, wherein the lifting mechanism has respective carriage associated arrangements of guide slot and support member, and wherein the positions of the support members in the guide slots can be changed together by means of the adjusting element. Thus, only the operation of a single actuator is necessary to adjust the positions of all carriages. The underside of the wing is movable by means of the adjusting element while maintaining its horizontal orientation up and down, which facilitates the setting process. The carriage frame of the carriage can be coupled together for a common sliding movement by means of a rigid, in particular rod-shaped, connecting member. This allows a particularly simple and inexpensive execution of a jointly displaceable carriage assembly. Another embodiment of the invention provides an additional actuator configured to vary the relative positions of the support member and the guide link in one of the assemblies while maintaining the relative positions of the support member and the guide link in the other arrangement. This makes it possible not only to move the bottom of the wing in the vertical direction, but also to change their inclination. Thus, a deviation of the parallelism between the wing bottom and the lower raceway, which consists after the assembly of the lift-slide element can be compensated.
Es kann vorgesehen sein, dass eines der Stellelemente zum Verschieben des Wagenrahmens gegenüber dem Flügel ausgebildet ist und das andere Stellelement zum Verschieben eines die Führungskulisse aufweisenden Lagerelements gegenüber dem Flügel ausgebildet ist. Somit kann ein Stellelement zum Anpassen der Dicke des Luftspalts und ein weiteres Stellelement zur Korrektur der Neigung der Flügelunterseite genutzt werden. Auf diese Weise ist eine besonders präzise Einstellung des Luftspalts möglich. It can be provided that one of the adjusting elements is designed for displacing the carriage frame relative to the wing and the other adjusting element is designed for displacing a bearing block having the guide slot with respect to the wing. Thus, an adjusting element for adjusting the thickness of the air gap and a further adjusting element for correcting the inclination of the wing underside can be used. In this way, a particularly precise adjustment of the air gap is possible.
Weiterbildungen der Erfindung sind auch in den abhängigen Ansprüchen, der Beschreibung sowie den beigefügten Zeichnungen angegeben. Further developments of the invention are set forth in the dependent claims, the description and the accompanying drawings.
Die Erfindung wird nachfolgend beispielhaft unter Bezugnahme auf die Zeichnung beschrieben. Fig. 1 ist eine teilweise aufgeschnittene Perspektivdarstellung eines mit einer erfindungsgemäßen Beschlaganordnung versehenen Hebe-Schiebe-Elements in einem unverstellten Grundzustand. Fig. 2 zeigt das Hebe-Schiebe-Element gemäß Fig. 1 in einem The invention will now be described by way of example with reference to the drawings. Fig. 1 is a partially cutaway perspective view of a provided with a fitting assembly according to the invention lifting-sliding element in an unadjusted ground state. Fig. 2 shows the lifting-pushing element according to FIG. 1 in one
verstellten Zustand.  disfigured state.
Fig. 3 ist eine vergrößerte Detaildarstellung der in Fig. 1 gezeigten FIG. 3 is an enlarged detail view of that shown in FIG. 1. FIG
Beschlaganordnung, welche einen vorderen Laufwagen genauer zeigt.  Fitting arrangement which shows a front carriage in more detail.
Fig. 4 zeigt den vorderen Laufwagen in einem gegenüber Fig. 3 verstellten Zustand. Fig. 4 shows the front carriage in a relation to FIG. 3 adjusted state.
Fig. 5 ist eine vergrößerte Detaildarstellung der in Fig. 1 gezeigten FIG. 5 is an enlarged detail view of that shown in FIG
Beschlaganordnung, welche einen hinteren Laufwagen genauer zeigt. Fig. 6 zeigt den hinteren Laufwagen in einem gegenüber Fig. 5 verstellten Zustand.  Fitting arrangement which shows a rear carriage in more detail. Fig. 6 shows the rear carriage in a relation to FIG. 5 adjusted state.
Fig. 7 zeigt den hinteren Laufwagen von einer Schmalseite des Fig. 7 shows the rear carriage from a narrow side of the
Flügels aus gesehen.  Wing seen from.
Fig. 8 zeigt den hinteren Laufwagen von einer Schmalseite des Fig. 8 shows the rear carriage from a narrow side of the
Flügels aus gesehen in einem verstellten Zustand.  Wing seen in an obstructed state.
Fig. 1 und 2 zeigen den unteren Bereich einer Hebe-Schiebe-Tür 1 1 , welche einen nicht dargestellten Blendrahmen und einen gegenüber dem Blendrahmen in einer horizontalen Verschieberichtung V verschiebbaren Flügel 15 aufweist. Von dem Flügel 15 ist in Fig. 1 und 2 speziell die vordere Schmalseite 75, die hintere Schmalseite 76 sowie die Flügelunterseite 77 zu erkennen. Zur Verschiebung des Flügels 15 ist eine Anordnung aus zwei Laufwagen 17a, 17b vorgesehen, die mittels Laufrollen 27 auf einer unterhalb des Flügels 15 angeordneten Führungsschiene 19 abrollen. Die Führungsschiene 19 kann einen Teil des Blendrahmens bilden oder als separate Komponente, beispielsweise als Bodenschwelle, ausgebildet sein. Die Oberseite der Führungsschiene 19 bildet eine Laufbahn 21 , entlang welcher der Flügel 15 mittels der Laufwagen 17a, 17b verschiebbar ist. Die beiden Laufwagen 17a, 17b sind mittels einer horizontalen Verbindungsstange 22 miteinander gekoppelt. Wie dargestellt sind die Laufwagen 17a, 17b einschließlich der Verbindungsstange 22 in einer unterseitigen Aufnahme 23 des Flügels 15 untergebracht. Jeder der Laufwagen 17a, 17b weist einen Wagenrahmen 25 auf, an welchem zwei bezüglich der Verschieberichtung V voneinander beabstandete Laufrollen 27 drehbar gelagert sind. In Fig. 1 und 2 ist aufgrund der Teilschnittdarstellung jeweils lediglich eine Laufrolle 27 pro Laufwagen 17a, 17b sichtbar. Fig. 1 and 2 show the lower portion of a lift-slide door 1 1, which has a frame, not shown, and a relative to the frame in a horizontal displacement direction V movable wings 15. Of the wing 15 is shown in Fig. 1 and 2 especially the front narrow side 75, the rear narrow side 76 and the wing bottom 77 can be seen. For displacement of the wing 15, an arrangement of two carriages 17a, 17b is provided, which roll by means of rollers 27 on a guide rail 19 arranged below the wing 15. The guide rail 19 may form part of the window frame or be formed as a separate component, for example as a floor sill. The top of the guide rail 19 forms a raceway 21, along which the wing 15 by means of the carriage 17a, 17b is displaceable. The two carriages 17a, 17b are coupled to each other by means of a horizontal connecting rod 22. As shown, the carriages 17a, 17b including the connecting rod 22 are accommodated in a lower-side receptacle 23 of the wing 15. Each of the carriages 17a, 17b has a carriage frame 25 on which two with respect to the direction of displacement V spaced rollers 27 are rotatably mounted. In Fig. 1 and 2, only one roller 27 per carriage 17a, 17b visible due to the partial sectional view.
Wie Fig. 3-6 zu entnehmen ist, ist bei jedem der beiden Laufwagen 17a, 17b ein Tragelement 29 in Form einer drehbaren Rolle zwischen den Laufrollen 27 am Wagenrahmen 25 gelagert. In den Figuren 1 -6 ist der Flügel 15 nach links zu öffnen und nach rechts zu schließen. Dementsprechend wird im Folgenden der in Fig. 1 rechts gelegene Laufwagen 17a als "vorderer Laufwagen" und der in Fig. 1 links gelegene Laufwagen 17b als "hinterer Laufwagen" bezeichnet. As can be seen in FIGS. 3-6, a support element 29 in the form of a rotatable roller between the rollers 27 on the carriage frame 25 is mounted in each of the two carriages 17a, 17b. In Figures 1 -6, the wing 15 is to be opened to the left and close to the right. Accordingly, in the following, the carriage 17a located on the right in FIG. 1 is referred to as the "front carriage" and the carriage 17b located on the left in FIG. 1 is referred to as the "rear carriage".
Die Tragelemente 29 sind in jeweiligen Führungskulissen 31 geführt, welche schräg zur Verschieberichtung V verlaufen und in vertikaler Richtung fest mit dem Flügel 15 verbunden sind. Die Wagenrahmen 25 beider Laufwagen 17a, 17b sind in horizontaler Richtung relativ zum Flügel 15 verschiebbar. Wenn die miteinander gekoppelten Wagenrahmen 25 ausgehend von der in Fig. 3 gezeigten Grundstellung relativ zum Flügel 15 nach rechts verschoben werden, erfolgt aufgrund der schrägen Ausrichtung der Führungskulissen 31 ein Anheben des Flügels 15 relativ zur Führungsschiene 19. Ein Benutzer kann eine solche gemeinsame horizontale Verschiebung der Laufwagen 17a, 17b durch Betätigung einer in den Figuren nicht dargestellten Treibstangenanordnung bewerkstelligen, welche über eine Eckum- lenkung 33 mit dem Wagenrahmen 25 des vorderen Laufwagens 17a gekoppelt ist. Die Führungskulissen 31 sowie die in den Führungskulissen 31 geführten Tragelemente 29 der Laufwagen 17a, 17b bilden somit einen Hebemechanismus 35, der es einem Benutzer ermöglicht, beispielsweise durch Bedienen einer am Flügel 15 vorgesehenen Handhabe (nicht dargestellt) den Flügel 15 von einer abgesenkten Stellung, in welcher eine Unterseite des Flügels 15 fest und unverschiebbar auf der Laufbahn 21 aufsitzt, in eine angehobene Stellung, in welcher die Unterseite des Flügels 15 durch einen Luftspalt 37 (Fig. 2) von der Laufbahn 21 beabstandet ist, zu überführen. The support members 29 are guided in respective guide slots 31 which extend obliquely to the direction of displacement V and are connected in the vertical direction fixed to the wing 15. The carriage frames 25 of both carriages 17a, 17b are displaceable in the horizontal direction relative to the wing 15. When the mutually coupled carriage frames 25 are shifted from the base position shown in Fig. 3 relative to the wing 15 to the right, takes place due to the oblique orientation of the guide slots 31, a lifting of the wing 15 relative to the guide rail 19. A user can such a common horizontal Displacement of the carriages 17a, 17b accomplish by operation of a drive rod assembly, not shown in the figures, which is coupled via a Eckum- deflection 33 with the carriage frame 25 of the front carriage 17a. The guide slots 31 and the guided in the guide slots 31 support members 29 of the carriage 17a, 17b thus form a lifting mechanism 35 which allows a user, for example, by operating a provided on the wing 15 handle (not shown) the wing 15 from a lowered position, in which an underside of the wing 15 is firmly and immovably seated on the track 21, in a raised position in which the underside of the wing 15 by an air gap 37 (Fig. 2) is spaced from the raceway 21 to transfer.
Zum Einstellen des Luftspalts 37 kann bei jedem Laufwagen 17a, 17b die relative Position des Tragelements 29 innerhalb der Führungskulisse 31 verändert wer- den. Für den vorderen Laufwagen 17a ist zu diesem Zweck eine in Fig. 3 und 4 erkennbare vordere Stellschraube 39 vorgesehen, die von der vorderen Schmalseite 75 des Flügels 15 aus durch eine in einer Stulpschiene 40 vorgesehene Durchführung 41 mittels eines Handwerkzeugs 43 betätigbar ist. Mittels der vorderen Stellschraube 39 ist es möglich, einen Hebel 45 und einen Umlenkrahmen 47, welche die Treibstange mit dem Wagenrahmen 25 des vorderen Laufwagens 17a koppeln, gegeneinander zu verschieben. Das erste Hebelende 49 des Hebels 45 ist am Wagenrahmen 25 gelagert, während das zweite Hebelende 50 ein Langloch 51 aufweist, durch das eine am Umlenkrahmen 47 angebrachte Lagerachse 53 hindurchgeführt ist. Die vordere Stellschraube 39 ist in einem Gewindeab- schnitt des zweiten Hebelendes 50 aufgenommen und beaufschlagt mit ihrem Schaftende die Lagerachse 53. Durch ein Drehen der vorderen Stellschraube 39 im Uhrzeigersinn kann die Lagerachse 53 innerhalb des Langlochs 51 nach links bewegt werden, wodurch bei festgehaltener Treibstange und somit feststehendem Umlenkrahmen 47 der Wagenrahmen 25 nach rechts gezogen wird, beispielswei- se in die in Fig. 4 gezeigte Stellung. Der Wagenrahmen 25 des vorderen Laufwa- gens 17a zieht hierbei über die Verbindungsstange 22 (Fig. 1 ) auch am Wagenrahmen 25 des hinteren Laufwagens 17b, so dass bei einem Drehen der vorderen Stellschraube 39 im Uhrzeigersinn beide Laufwagen 17a, 17b gemeinsam um den gleichen Betrag nach rechts verschoben und demgemäß der Flügel 15 unter Ver- größerung des Luftspalts 37 angehoben wird. Bei einem Drehen der vorderen Stellschraube 39 gegen den Uhrzeigersinn bewegt sich das Schaftende nach rechts aus dem Langloch 51 heraus, sodass sich der vordere Laufwagen 17a nach links bewegen kann und der Flügel 15 gewichtsbedingt absinkt. Dieses zum Einstellen des Luftspalts 37 vorgesehene Anheben und Absenken des Flügels 15 erfolgt völlig unabhängig vom Anheben und Absenken des Flügels 15 während des Normalgebrauchs der Hebe-Schiebe-Tür 1 1 mittels Betätigung einer auf die Treibstange wirkenden Handhabe. For adjusting the air gap 37, the relative position of the support element 29 within the guide slot 31 can be changed in each carriage 17a, 17b. For the purpose of this purpose, a front adjusting screw 39 which can be seen in FIGS. 3 and 4 is provided for the front carriage 17a, which can be actuated from the front narrow side 75 of the wing 15 by means of a handpiece 43 provided in a cuff rail 40. By means of the front adjusting screw 39, it is possible to move a lever 45 and a deflection frame 47, which couple the drive rod to the carriage frame 25 of the front carriage 17a, against each other. The first lever end 49 of the lever 45 is mounted on the carriage frame 25, while the second end of the lever 50 has a slot 51 through which a mounted on the deflection frame 47 bearing shaft 53 is passed. The front adjusting screw 39 is received in a threaded portion of the second lever end 50 and acted with its shaft end the bearing axis 53. By rotating the front adjusting screw 39 clockwise, the bearing axis 53 can be moved within the slot 51 to the left, whereby at a fixed drive rod and thus stationary deflection frame 47, the carriage frame 25 is pulled to the right, for example into the position shown in FIG. The carriage frame 25 of the front running 17a pulls on the connecting rod 22 (FIG. 1) also on the carriage frame 25 of the rear carriage 17b, so that when turning the front adjusting screw 39 clockwise both carriages 17a, 17b moved together by the same amount to the right and accordingly the wing 15 is increased by increasing the air gap 37. When turning the front adjusting screw 39 counterclockwise, the shaft end moves out of the slot 51 to the right, so that the front carriage 17a can move to the left and the wing 15 drops due to weight. This intended for adjusting the air gap 37 raising and lowering of the wing 15 is completely independent of the raising and lowering of the wing 15 during normal use of the lift-slide door 1 1 by means of an acting on the drive rod handle.
Um bei Bedarf eine Verkippung der Flügelunterseite 77 in Bezug auf die Horizon- tale kompensieren zu können, können die beiden Laufwagen 17a, 17b auch unabhängig voneinander verstellt werden. Hierfür ist eine in Fig. 5-8 sichtbare hintere Stellschraube 59 vorgesehen, mittels welcher die Position des Tragelements 29 des hinteren Laufwagens 17b in der zugehörigen Führungskulisse 31 verändert werden kann, ohne hierbei den vorderen Laufwagen 17a mitzubewegen. Um dies zu erreichen, wirkt die hintere Stellschraube 59 nicht auf den Wagenrahmen 25, sondern auf ein Lagerelement 61 , in dem die Führungskulisse 31 ausgebildet ist. Das Lagerelement 61 ist oberseitig in einer nicht sichtbaren Führung wie z. B. einer T-Nut geführt, welche an einer flügelfesten Halteplatte 63 gebildet ist. In Fig. 5 links von dem Lagerelement 61 befindet sich ein an der Halteplatte 63 befestig- ter Stützkörper 65, an welchem sich der Schraubenkopf 67 der hinteren Stellschraube 59 abstützt. Der nicht sichtbare Schaft der hinteren Stellschraube 59 ist in einem Gewindeabschnitt des Lagerelements 61 aufgenommen. Bei einem Drehen der hinteren Stellschraube 59 im Uhrzeigersinn kann somit das Lagerelement 61 gegenüber dem Flügel 15 in Fig. 5 nach links gezogen werden, beispielsweise bis in die in Fig. 6 dargestellte Stellung. Mit dieser Bewegung ist ein Anheben des hinteren Laufwagens 17b verbunden. Da jedoch der Wagenrahmen 25 des hinteren Laufwagens 17b in Bezug auf den Flügel 15 nicht bewegt wird, wirkt sich das Drehen der hinteren Stellschraube 59 nicht auf die Stellung des vorderen Laufwagens 17a aus, so dass dementsprechend der Flügel 15 im Bereich des vorderen Laufwagens 17a nicht angehoben wird. Im Ergebnis wird somit der Flügel 15 in Bezug auf die Horizontale geringfügig verkippt. Ähnlich wie bei dem vorderen Laufwagen 17a erfolgt das Betätigen der hinteren Stellschraube 59 mittels eines Handwerkzeugs 43 von einer Schmalseite des Flügels 15 aus - hier von der hinteren Schmalseite 76 aus. Zur Durchführung des Handwerkzeugs 43 ist wiederum eine geeignete Aussparung vorgesehen, was in Fig. 5-8 jedoch nicht dargestellt ist. Ein Drehen der hinteren Stellschraube 59 gegen den Uhrzeigersinn gibt das Lagerelement 61 frei für eine Bewegung nach rechts, sodass sich der hintere Abschnitt des Flügels 15 gewichtsbedingt absenkt. Ein Monteur kann nach dem Einbau der Hebe-Schiebe-Tür 1 1 den Luftspalt 37 in gewünschter Weise durch Betätigen der vorderen Stellschraube 39 sowie der hinteren Stellschraube 59 anpassen. Hierbei kann einerseits mittels der vorderen Stellschraube 39 eine Parallelverschiebung des Flügels 15 ausschließlich in vertikaler Richtung herbeigeführt und mittels der hinteren Stellschraube 59 eine Ver- kippung des Flügels 15 bewirkt werden. Dies erlaubt eine besonders schnelle und präzise Justierung des Luftspalts 37. In order to be able to compensate for a tilting of the wing bottom side 77 with respect to the horizontal, if necessary, the two carriages 17a, 17b can also be adjusted independently of one another. For this purpose, a visible in Fig. 5-8 rear adjusting screw 59 is provided, by means of which the position of the support member 29 of the rear carriage 17 b in the associated guide slot 31 can be changed without moving the front carriage 17 a. To achieve this, the rear adjusting screw 59 does not act on the carriage frame 25, but on a bearing element 61, in which the guide slot 31 is formed. The bearing element 61 is the upper side in a non-visible guide such. B. a T-groove, which is formed on a wing-fixed plate 63. In FIG. 5, to the left of the bearing element 61, there is a supporting body 65 fastened to the holding plate 63, on which the screw head 67 of the rear adjusting screw 59 is supported. The invisible shaft of the rear adjusting screw 59 is received in a threaded portion of the bearing member 61. When turning the rear adjusting screw 59 in a clockwise direction thus the bearing member 61 relative to the wing 15 in Fig. 5 are pulled to the left, for example, to the position shown in Fig. 6. With this movement is a lifting of the rear carriage 17b connected. However, since the carriage frame 25 of the rear carriage 17b is not moved with respect to the wing 15, the turning of the rear adjusting screw 59 does not affect the position of the front carriage 17a, and hence the wing 15 does not act in the region of the front carriage 17a is raised. As a result, the wing 15 is thus slightly tilted with respect to the horizontal. Similar to the front carriage 17a, the actuation of the rear adjusting screw 59 takes place by means of a hand tool 43 from a narrow side of the wing 15 - here from the rear narrow side 76. For performing the hand tool 43, in turn, a suitable recess is provided, which is not shown in Fig. 5-8. Turning the rear adjusting screw 59 counterclockwise releases the bearing member 61 for movement to the right so that the rear portion of the wing 15 lowers by weight. A fitter can adjust the air gap 37 in a desired manner by operating the front adjusting screw 39 and the rear adjusting screw 59 after installation of the lifting-sliding door 1 1. In this case, on the one hand, by means of the front adjusting screw 39, a parallel displacement of the wing 15 is brought about exclusively in the vertical direction and by means of the rear adjusting screw 59 a tilting of the wing 15 is effected. This allows a particularly fast and precise adjustment of the air gap 37.
Bezuqszeichenliste LIST OF REFERENCES
1 1 Hebe-Schiebe-Tür 1 1 lift-slide door
15 Flügel  15 wings
17a, 17b Laufwagen  17a, 17b carriage
19 Führungsschiene  19 guide rail
21 Laufbahn  21 career
22 Verbindungsstange  22 connecting rod
23 Aufnahme  23 recording
25 Wagenrahmen  25 car frames
27 Laufrolle  27 roller
29 Tragelement  29 supporting element
31 Führungskulisse  31 guidance course
33 Eckumlenkung  33 corner drive
35 Hebemechanismus  35 lifting mechanism
37 Luftspalt  37 air gap
39 vordere Stellschraube 39 front adjusting screw
40 Stulpschiene 40 faceplate
41 Durchführung  41 implementation
43 Handwerkzeug  43 Hand tools
45 Hebel  45 levers
47 Umlenkrahmen  47 deflection frame
49 erstes Hebelende  49 first lever end
50 zweites Hebelende  50 second lever end
51 Langloch  51 slot
53 Lagerachse  53 bearing axis
59 hintere Stellschraube  59 rear adjusting screw
61 Lagerelement  61 bearing element
63 Haltekörper  63 holding body
65 Anschlagfläche  65 stop surface
67 Schraubenkopf  67 screw head
75 vordere Schmalseite  75 front narrow side
76 hintere Schmalseite  76 rear narrow side
77 Flügelunterseite  77 wing base
V Verschieberichtung V shift direction

Claims

Patentansprüche claims
Beschlaganordnung für ein Hebe-Schiebe-Element (1 1 ) wie eine Hebe- Schiebe-Tür oder ein Hebe-Schiebe-Fenster, das einen Blendrahmen und einen entlang einer unteren Laufbahn (21 ) in einer Verschieberichtung (V) gegenüber dem Blendrahmen verschiebbaren Flügel (15) umfasst, mit wenigstens einem Laufwagen (17a, 17b), der einen Wagenrahmen (25) und zumindest eine an dem Wagenrahmen (25) gelagerte Laufrolle (27) aufweist, und einem durch eine Treibstange der Beschlaganordnung betätigbaren Hebemechanismus (35) zum Anheben des Flügels (15) gegenüber dem Wagenrahmen (25) von einer abgesenkten Stellung in eine angehobene Stellung, in welcher eine Unterseite (77) des Flügels (15) durch einen Luftspalt (37) von der Laufbahn (21 ) beabstandet ist, Fitting arrangement for a lifting-sliding element (1 1) such as a lift-slide door or a lift-and-slide window, the one frame and along a lower track (21) in a direction of displacement (V) relative to the frame movable wings (15), comprising at least one carriage (17a, 17b) having a carriage frame (25) and at least one roller (27) mounted on the carriage frame (25) and a lift mechanism (35) operable by a drive rod of the fitting assembly Lifting the wing (15) relative to the carriage frame (25) from a lowered position to a raised position, in which a lower side (77) of the wing (15) is spaced from the raceway (21) by an air gap (37),
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
der Hebemechanismus (35) eine schräg zur Verschieberichtung (V) verlaufende Führungskulisse (31 ) und ein in der Führungskulisse (31 ) geführtes Tragelement (29) umfasst, wobei die Führungskulisse (31 ) an einem fest mit dem Flügel (15) verbundenen Bauteil ausgebildet ist und das Tragelement (29) an dem Wagenrahmen (25) angeordnet ist, oder umgekehrt, und wobei zum Einstellen des Luftspalts (37) ein Stellelement (39, 59) vorgesehen ist, mittels dessen die Position des Tragelements (29) in der Führungskulisse (31 ) unabhängig von einer Betätigung der Treibstange veränderbar ist. the lifting mechanism (35) comprises a guide slot (31) running obliquely to the displacement direction (V) and a carrying element (29) guided in the guide slot (31), wherein the guide slot (31) is formed on a component integral with the blade (15) and the support element (29) is arranged on the carriage frame (25), or vice versa, and wherein an adjusting element (39, 59) is provided for adjusting the air gap (37), by means of which the position of the support element (29) in the guide link (31) is variable independently of an actuation of the drive rod.
Beschlaganordnung nach Anspruch 1, Fitting arrangement according to claim 1,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
das Stellelennent (39, 59) derart angeordnet ist, dass es von einer Schmalseite (75, 76) des Flügels (15) aus betätigbar ist. the Stellelennent (39, 59) is arranged such that it can be actuated from a narrow side (75, 76) of the wing (15).
Beschlaganordnung nach Anspruch 2, Fitting arrangement according to claim 2,
g e k e n n z e i c h n e t durch marked by
eine an der Schmalseite (75, 76) des Flügels (15) angeordnete Stulpschiene (40), welche eine Aussparung (41) zum Durchführen eines Werkzeugs (43) aufweist, mittels welchem das Stellelement (39, 59) betätigbar ist. a face-plate rail (40) arranged on the narrow side (75, 76) of the wing (15) and having a recess (41) for passing a tool (43) by means of which the adjusting element (39, 59) can be actuated.
Beschlaganordnung nach einem der vorstehenden Ansprüche, Fitting arrangement according to one of the preceding claims,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
das Tragelement (29) einen Gleitzapfen oder eine drehbare Rolle umfasst. the support element (29) comprises a sliding peg or a rotatable roller.
Beschlaganordnung nach einem der vorstehenden Ansprüche, Fitting arrangement according to one of the preceding claims,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
das Stellelement (39) dazu ausgebildet ist, zum Verändern der Position des Tragelements (29) in der Führungskulisse (31) den Wagenrahmen (25) gegenüber dem Flügel (15) in oder entgegen der Verschieberichtung (V) zu verschieben. the adjusting element (39) is designed to displace the carriage frame (25) relative to the wing (15) in or against the displacement direction (V) in order to change the position of the support element (29) in the guide slot (31).
Beschlaganordnung nach Anspruch 5, Fitting arrangement according to claim 5,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
das Stellelement (39) dazu ausgebildet ist, zum Verschieben des Wagenrahmens (25) bei festgehaltener Treibstange zwei die Treibstange mit dem Wagenrahmen (25) verbindende Kopplungsteile (45, 47) gegeneinander zu verschieben. the adjusting element (39) is designed to displace the drive rod with the carriage frame (25) connecting coupling parts (45, 47) against each other for moving the carriage frame (25) at a fixed drive rod.
Beschlaganordnung nach Anspruch 6, Fitting arrangement according to claim 6,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
ein erstes Kopplungsteil ein Hebel (45) ist, dessen eines Hebelende (49) am Wagenrahmen (25) gelagert ist und dessen anderes Hebelende (50) ein Langloch (51) aufweist, durch das eine am zweiten Kopplungsteil (47) angeordnete Lagerachse (53) hindurchgeführt ist, wobei mittels des Stellelements (39) die Lagerachse (53) innerhalb des Langlochs (51) verschiebbar ist. a first coupling part is a lever (45), one lever end (49) of which is mounted on the carriage frame (25) and the other lever end (50) has a slot (51) through which a bearing axle (53) arranged on the second coupling part (47) passes ) is guided, wherein by means of the adjusting element (39), the bearing axis (53) within the slot (51) is displaceable.
Beschlaganordnung nach Anspruch 7, Fitting arrangement according to claim 7,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
das Stellelement als Stellschraube (39) ausgeführt ist, welche in einem Gewindeabschnitt des das Langloch (51) aufweisenden Hebelendes (50) aufgenommen ist und mit ihrem Schaftende die Lagerachse (53) beaufschlagt. the adjusting element is designed as a set screw (39) which is received in a threaded portion of the elongated hole (51) having the lever end (50) and acts with its shaft end, the bearing axis (53).
Beschlaganordnung nach einem der vorstehenden Ansprüche, Fitting arrangement according to one of the preceding claims,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
das Stellelement (59) dazu ausgebildet ist, zum Verändern der Position des Tragelements (29) in der Führungskulisse (31) ein die Führungskulisse (31) aufweisendes Lagerelement (61) gegenüber dem Flügel (15) in oder entgegen der Verschieberichtung (V) zu verschieben. the adjusting element (59) is designed to change the position of the supporting element (29) in the guide slot (31) to a bearing element (61) facing the guide slot (31) in relation to the wing (15) in or against the displacement direction (V) move.
Beschlaganordnung nach Anspruch 9, Fitting arrangement according to claim 9,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
das Stellelement als eine einen Schraubenkopf (67) aufweisende Stellschraube (59) ausgeführt ist, welche in einem Gewindeabschnitt des Lagerelements (61) aufgenommen ist und sich mit dem Schraubenkopf (67) an einer flügelfesten Anschlagfläche (65) abstützt. the adjusting element is designed as an adjusting screw (59) having a screw head (67), which is accommodated in a threaded section of the bearing element (61) and is supported by the screw head (67) against a wing-fixed stop face (65).
11. Beschlaganordnung nach Anspruch 10, 11. fitting arrangement according to claim 10,
dadurch g e k e n n z e i c h n e t , dass  By doing so, that is
das Lagerelement (61) mittels einer Gleitführung an einem am Flügel (15) befestigten Haltekörper (63) geführt ist, an welchem die Anschlagfläche (65) ausgebildet oder ein die Anschlagfläche (65) aufweisendes Bauteil befestigt ist.  the bearing element (61) is guided by means of a sliding guide on a holding body (63) fastened to the wing (15), on which the stop face (65) is formed or a component having the stop face (65) is fastened.
12. Beschlaganordnung nach einem der vorstehenden Ansprüche, 12. fitting arrangement according to one of the preceding claims,
dadurch g e k e n n z e i c h n e t , dass  By doing so, that is
der Laufwagen (17a, 17b) zwei bezüglich der Verschieberichtung (V) voneinander beabstandete Laufrollen (27) aufweist, wobei das Tragelement (29) zwischen den Laufrollen (27) am Wagenrahmen (25) angebracht ist.  the carriage (17a, 17b) has two with respect to the direction of displacement (V) spaced from each other rollers (27), wherein the support member (29) between the rollers (27) on the carriage frame (25) is mounted.
13. Beschlaganordnung nach einem der vorstehenden Ansprüche, 13. Fitting arrangement according to one of the preceding claims,
dadurch g e k e n n z e i c h n e t , dass  By doing so, that is
wenigstens zwei, vorzugsweise genau zwei, bezüglich der Verschieberichtung (V) voneinander beabstandete Laufwagen (17a, 17b) vorgesehen sind, wobei der Hebemechanismus (35) jeweilige den Laufwagen (17a, 17b) zugeordnete Anordnungen aus Führungskulisse (31) und Tragelement (29) aufweist, und wobei die Positionen der Tragelemente (29) in den Führungskulissen (31) mittels des Stellelements (39) gemeinsam veränderbar sind.  at least two, preferably exactly two, with respect to the direction of displacement (V) spaced apart carriages (17a, 17b) are provided, wherein the lifting mechanism (35) respective the carriage (17a, 17b) associated arrangements of guide slot (31) and support member (29) and wherein the positions of the support elements (29) in the guide slots (31) by means of the adjusting element (39) are mutually variable.
14. Beschlaganordnung nach Anspruch 13, 14. Fitting arrangement according to claim 13,
dadurch g e k e n n z e i c h n e t , dass  By doing so, that is
die Wagenrahmen (25) der Laufwagen (17a, 17b) für eine gemeinsame Verschiebebewegung mittels eines starren, insbesondere stangenformigen, Verbindungsbauteils (22) miteinander gekoppelt sind. Beschlaganordnung nach Anspruch 13 oder 14, the carriage frames (25) of the carriages (17a, 17b) are coupled together for a common displacement movement by means of a rigid, in particular rod-shaped, connecting component (22). Fitting arrangement according to claim 13 or 14,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
ein zusätzliches Stellelement (59) vorgesehen ist, welches zum Verändern der relativen Positionen von Tragelement (29) und Führungskulisse (31) bei einer der Anordnungen unter Beibehaltung der relativen Positionen vonan additional actuator (59) is provided for changing the relative positions of the support member (29) and guide link (31) in one of the assemblies while maintaining the relative positions of
Tragelement (29) und Führungskulisse (31) bei der anderen Anordnung ausgebildet ist. Support member (29) and guide slot (31) is formed in the other arrangement.
Beschlaganordnung nach Anspruch 15, Fitting arrangement according to claim 15,
dadurch g e k e n n z e i c h n e t , dass By doing so, that is
eines der Stellelemente (39) zum Verschieben des Wagenrahmens (25) gegenüber dem Flügel (15) ausgebildet ist und das andere Stellelement (59) zum Verschieben eines die Führungskulisse (31) aufweisenden Lagerelements (61) gegenüber dem Flügel (15) ausgebildet ist. one of the adjusting elements (39) is designed to move the carriage frame (25) relative to the wing (15) and the other adjusting element (59) is designed to displace a bearing element (61) having the guide slot (31) relative to the wing (15).
EP15762616.9A 2014-10-02 2015-09-10 Fitting arrangement Active EP3201413B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102014114373.6A DE102014114373A1 (en) 2014-10-02 2014-10-02 fitting assembly
PCT/EP2015/070772 WO2016050480A1 (en) 2014-10-02 2015-09-10 Fitting arrangement

Publications (2)

Publication Number Publication Date
EP3201413A1 true EP3201413A1 (en) 2017-08-09
EP3201413B1 EP3201413B1 (en) 2018-08-22

Family

ID=54072859

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15762616.9A Active EP3201413B1 (en) 2014-10-02 2015-09-10 Fitting arrangement

Country Status (4)

Country Link
EP (1) EP3201413B1 (en)
CN (1) CN107002437B (en)
DE (1) DE102014114373A1 (en)
WO (1) WO2016050480A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016212793C5 (en) 2016-07-13 2023-01-05 Roto Frank Ag Fitting arrangement with a lifting device
DE102020113741A1 (en) * 2020-05-20 2021-11-25 Maco Technologie Gmbh FITTINGS FOR ADJUSTING THE HEIGHT OF A LIFTING DEVICE OF A LIFTING-SLIDING ELEMENT
DE102021123034A1 (en) 2021-09-06 2023-03-09 Maco Technologie Gmbh Low-wear fitting arrangement for lifting a lift and slide element

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE20115938U1 (en) * 2001-09-27 2002-01-03 Gretsch-Unitas GmbH Baubeschläge, 71254 Ditzingen Carriage arrangement of a fitting for lift-slide doors or windows and fitting with such a carriage arrangement
DE202005000547U1 (en) * 2005-01-13 2005-03-17 Siegenia Aubi Kg Fitting an at least liftable and / or tiltable, but preferably also movable wing of a window or door
IT1390715B1 (en) * 2008-07-14 2011-09-15 Gsg Int S P A TROLLEY FOR SLIDING DOORS
ITBO20120524A1 (en) * 2012-09-26 2014-03-27 Gsg Int Spa TROLLEY GROUP FOR SLIDING DOORS OR WINDOWS UP AND SLIDE.
CN203808695U (en) * 2014-03-13 2014-09-03 广东坚朗五金制品股份有限公司 Sliding assembly of sliding door and window
CN104047489B (en) * 2014-05-27 2017-02-15 许姜德 Lower upward-protruding pulley used on sliding door

Also Published As

Publication number Publication date
CN107002437B (en) 2019-03-19
CN107002437A (en) 2017-08-01
EP3201413B1 (en) 2018-08-22
DE102014114373A1 (en) 2016-04-07
WO2016050480A1 (en) 2016-04-07

Similar Documents

Publication Publication Date Title
DE20107278U1 (en) Device for producing a snap connection
DE3043925C2 (en) Device on a window for setting the casement in a gap opening position
DE69002037T2 (en) Rolling device for sliding doors, windows or the like.
EP3201413B1 (en) Fitting arrangement
EP0718456A1 (en) Closing device for window, door and the like
EP2799651A1 (en) Fitting for sliding furniture doors
DE2462141A1 (en) DRAWER SLIDE WITH ADJUSTMENT
AT524607B1 (en) Arrangement for guiding a movable piece of furniture
EP2463467A2 (en) Narrow three-position actuating device for controlling a parallel movement of a door- or window-wing
EP3825503A1 (en) Sealing device of sliding door
WO2020074314A1 (en) Fittings assembly
DE202015103771U1 (en) glazing system
EP1298271A2 (en) Carriage for a fitting for lifting and sliding doors or windows and a fitting with such a carriage
DE102012222210A1 (en) For concealed arrangement provided corner bearing
EP3371402B1 (en) Fitting device for a lifting and sliding element with frame-mounted adjusting element
DE8800862U1 (en) sliding door
DE9101597U1 (en) hinge
EP1527245A1 (en) Hinge part for door or window hinge or the like
CH715705B1 (en) Sliding leaf assembly with a movable guide rail in a bottom guide.
EP0853179B1 (en) Wing for a door or window or the like
AT526424B1 (en) Management system
DE20100745U1 (en) Tape for doors or windows
DE7709672U1 (en) ADJUSTABLE LOWER CORNER BEARING FOR TILT-TURN LEAF
DE19854739C1 (en) Support roller assembly for building movable door or window leaf has adjusting screw engaging semi-circular notch in cantilever
EP3296497A1 (en) Pivot sliding door assembly for a vehicle

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20170315

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20180219

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1032727

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180915

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502015005581

Country of ref document: DE

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 4

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180822

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181123

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181122

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181122

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181222

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502015005581

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20180930

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180910

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20190523

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180910

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180930

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180930

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180822

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20150910

Ref country code: MK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180822

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20190910

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190910

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20240918

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20240925

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: AT

Payment date: 20240919

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20240924

Year of fee payment: 10