EP1132562B2 - Corner reinforcements or struts for sliding wings - Google Patents

Corner reinforcements or struts for sliding wings Download PDF

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Publication number
EP1132562B2
EP1132562B2 EP01105614.0A EP01105614A EP1132562B2 EP 1132562 B2 EP1132562 B2 EP 1132562B2 EP 01105614 A EP01105614 A EP 01105614A EP 1132562 B2 EP1132562 B2 EP 1132562B2
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EP
European Patent Office
Prior art keywords
carriage
plate
sliding sash
bolt
fitting 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.)
Expired - Lifetime
Application number
EP01105614.0A
Other languages
German (de)
French (fr)
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EP1132562B1 (en
EP1132562A3 (en
EP1132562A2 (en
Inventor
Dirk Mügge
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Hautau GmbH
Original Assignee
Hautau GmbH
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Application filed by Hautau GmbH filed Critical Hautau GmbH
Priority to EP10184738.2A priority Critical patent/EP2267258B1/en
Publication of EP1132562A2 publication Critical patent/EP1132562A2/en
Publication of EP1132562A3 publication Critical patent/EP1132562A3/en
Publication of EP1132562B1 publication Critical patent/EP1132562B1/en
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Publication of EP1132562B2 publication Critical patent/EP1132562B2/en
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Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00—Suspension arrangements for wings
    • E05D15/06—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • E05D15/1005—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane the wing being supported on arms movable in horizontal planes
    • E05D15/1013—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane the wing being supported on arms movable in horizontal planes specially adapted for windows
    • E05D15/1015—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane the wing being supported on arms movable in horizontal planes specially adapted for windows with an intermediate tilt position
    • 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
    • E05Y2201/64—Carriers
    • 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
    • E05Y2600/60—Mounting or coupling members; Accessories therefor
    • E05Y2600/62—Bolts
    • 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
    • E05Y2600/60—Mounting or coupling members; Accessories therefor
    • E05Y2600/628—Profiles; Strips
    • 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
    • E05Y2800/67—Materials; Strength alteration thereof
    • E05Y2800/682—Strength alteration by reinforcing, e.g. by applying ribs

Definitions

  • the invention relates to a carriage fitting for a sliding sash, which should allow improved grip of the sliding sash on trolley.
  • connection is made via an existing reinforcement, which is plugged into a horizontal support surface on the drive and bolted to the sliding sash, in particular to the vertical spar of this sash.
  • This known reinforcement counteracts the described deformation (torsion) of the sliding sash. If the plastic profiles are used, a screw connection of the mentioned reinforcement in a spar region, which has a metal reinforcement, ensures a solid assembly. But if the sash weights are getting higher, due to larger glass weights or surfaces of the horizontally displaceable wings, so the known assembly can no longer limit deformation sufficient.
  • the DE-U 87 09 299 which document discloses the features of the preamble of claim 1, shows a reinforcing member for a box-like support member which carries a pivot pin of a stay arm, and thereby a plate, there 14, is provided, which via a bend piece as a nearly horizontal transition piece has, in which a stud piece is inserted covered from below.
  • the bolt is not attached directly to the plate, but indirectly via the transition piece, which acts as a joint at high sash weights in the angular range to the plate.
  • the plate is screwed through several mounting points, there via screws 26, with the wing and the downwardly projecting bolt inserted into two receiving openings of the carriage, there 12 to there FIG. 3 , and can be taken from it.
  • a panel, there 16 provides for a cover of the plugged into the openings and from it again removable bolt, see. there page 10, middle paragraph.
  • the object of the invention is to propose a carriage fitting, with which an increased sash weight of a sliding leaf can be added, with which this wing can be stiffened in particular in the corner.
  • the assembly time should be shortened or simplified.
  • the solution is the invention according to claim 1.
  • the proposed carriage fitting makes it possible, in particular in the case of plastic profiles, for the mounting plate extending in the vertical direction to fit snugly against the wing surface on the interior side of the wing and not to raise the wing in spite of the high sash weights.
  • the panel is connected to the wing via pairs of horizontally and vertically spaced mounting locations such that four or more mounting locations form an assembly assembly that allows the panel to abut the surface of the wing to receive and transfer high forces to the drive (the carriage).
  • connection of the wing on the said plate is effected by means of a coupling piece as a bolt, which is inserted into a substantially horizontal receiving or support surface of the drive and so firmly but permanently connected to the drive.
  • a self-stiffening of the plate can be done by ahenkonturtechnik, in the form of vertical strips (claim 8).
  • vertical strips Of the vertical strips is advantageous at least one embossed strip, which causes an additional stiffening of the plate.
  • the stiffening can take the said Verbiridungsbolzen at least a little way. Two raised stripes may occur adjacent the one embossing strip to provide lateral support of the bolt (claims 8, 9 and 10).
  • the raised stripes can arise from the fact that the one embossed strip is introduced. But it can also or alone embossing strips on the other side of the plate be provided so that the raised strips on the visible side without the impression of a median strip arise. Also several spaced embossing strips can be provided.
  • An elongate support plate may be opposite to the mounting plate formed in particular with an embossed structure, specifically on the side of the rebate space (folding air). Here it is arranged so that it is located on the inside of the wing flap (facing the fixed frame). Preferably, it is not so elongated, as the described, preferably embossed mounting plate, but can also be made longer.
  • a connection is made between the support plate located in the rebate and the mounting plate arranged on the surface (visible side) of the sash, in particular a screw connection which permits stiffening of the vertical strut starting from the lower corner region.
  • the edge region of the wing serves to stiffen with a layer structure which is clamped together by screws, bolts or other clamping members to form a composite.
  • Such stiffeners can also be found in other sash frames, such as metal or wood, application.
  • FIG. 1 is explained in an upper (two-part), a middle and a lower illustration of the right lower corner region of the sash FR.
  • two drives 10,20 are provided, which are mounted in the respective corner E at the lower spar. They have rollers and run on a fixed rail BR arranged rail 65 (as in FIG. 4 shown), for parallel displacement of the entire wing, which has been previously led out of the opening of the fixed frame, for example by tilting and Parallelabstellen.
  • the corner area which will be explained below, is denoted by E.
  • the drive 20 is provided, which has a vertical pin 22 and a plate 23 has a connection to the sliding leaf FR.
  • the (right) drive 20 has in the end view a horizontally extending support or receiving surface 21 into which the said pin 22 engages.
  • a similar surface 11 is also provided in the (left) drive 10, but without opening and without a receptacle for a bolt.
  • a single row of screws 9 (in the carriage 10) and 19 (in the carriage 20) is provided to receive in a corner region over the length of the carriage substantially regularly distributed forces and to initiate the support piece of the carriage. From this single row of screws 19 in the carriage 20 two representative attachment points are shown by Phillips screws in the middle view, which engage through the vertical web 21 b of the support or receiving surface 21 (above this) and are anchored in the profile of the horizontal spar. A screw 19 of this row of screws can be seen in the large illustration AV next to the bolt 22.
  • This row of screws as a single row of screws serves to reduce the height of the carriage in order to use the fitting even with narrow profiles. She is also at the FIG. 4 explained not claimed embodiment in the same way usable.
  • the enlargement of the area E from the upper illustration is shown with the plate 23 in the middle illustration.
  • This plate is provided with four attachment openings 24 a, 24 b, 25 a, 25 b, which are provided in the upper portion of the mounting plate 23.
  • the bolt 22 is fixedly attached to the plate 23, e.g. by welding 26 or otherwise mounting.
  • the bolt is inserted in an opening 21a of the horizontal surface 21 and is received by the drive frame, which is formed from the two surfaces 21 and a vertically extending surface 21 '.
  • the bolt can be held here by positive engagement or fit.
  • the engaging piece 23 ' is an extension of the bolt plate 23 and extends in the same direction as the lower portion of the bolts 22.
  • the extension piece may be double-winged.
  • a wing is on
  • the enlarged portion AV shows the lower portion of the bolt at the engagement in the opening 21a and above the engagement of the two flanges 23 'in the vertical portion of the receiving and supporting surface 21, which with 21b is designated.
  • the intervention takes place only a little way, namely as far as the sectional view of the middle figure in the left half shows.
  • a gap is provided into which a thickness-tapered front end of the pin plate 23, shown as 23 ', engages or engages behind. This results in a multi-point provided support and holding, the bases are laterally spaced from each other.
  • the tapered piece 23 ' is made by embossing or pinching the entire one- or two-piece front portion of the plate 23, which is thereby able to engage behind the web 21 b.
  • a provided as welding point 26 on both sides of the bolt 22 connecting point is shown, which connects the lower portion of the bolt with the pin plate 23, while still above at least one, preferably two more spaced welds on both sides of the pin 22, the connection with the Make bolt plate 23.
  • mounting sites 24,25 (each a and b) will be used in the following ambiguous. They either form an opening with respect to the plate 23 to be screwed on, or the mounting points are already described in the installed state so that holding or fastening means such as screws, bolts, clamping means or other mounting parts are inserted into the openings to the plate 23 at to attach the sliding leaf FR.
  • the technical term of the mounting point should therefore be used ambiguously.
  • FIG. 2 The sectional view of the corner area E in a horizontal plane is in FIG. 2 illustrated.
  • Fixed frame BR and movable sash (also called sliding sash) FR are visible, as well as the seaming air F and the standard groove N for receiving locking rods.
  • the sash FR consists in a schematic representation of a wooden profile or - shown in phantom - of a plastic profile with interiors, which are at least partially reinforced by a metal reinforcement 31.
  • the rollover area Ü of the wing is represented by a mounting point 24b (or 25b, depending on the vertical position of the section). The rollover covers the rebate F and protrudes over to the fixed frame BR.
  • the horizontal support and receiving surface 21 in which - seen from above - the bolt 22 engages and on the drive 20 - as described - is mounted.
  • FIG. 1 There are two spaced mounting points 24a, 24b, which in FIG. 1 (in the middle illustration) have also been shown. They are arranged at the upper end portion of the plate 23 and spaced in the horizontal direction by the dimension c, which is made FIG. 3 can be seen. Spaced apart in the vertical direction, two further mounting points 25a, 25b are provided, the distance to the first mounting points is d, which is also made FIG. 3 is apparent.
  • a mounting point is realized so that a screw bolt or a screw is passed through the plate 23 and is fixed to the wing FR.
  • the attachment takes place once in the profile area (off the edge), preferably in the metal reinforcement 31, and again in the rollover area by the rollover and on an additional support plate 30 in the rebate F in FIG. 2 is recognizable.
  • This plate can be made longer than the elongated plate 23, it can also consist of individual elements, depending on which task and function is assigned to it. Should it only serve for assembly, it can consist of individual pieces.
  • the support and support plate 30 in the wing area also has support function, and all properties together can cause a greatly increased stiffening of the lower corner, with recorded without visual change high sash weights and can be transferred to the fixed frame BR without significant torsion of the entire sliding sash over the carriage 20.
  • the described multiple mounting locations 24,25 are in FIG. 3 recognizable as a surface mounting.
  • the mounting points are preferably arranged in the upper region of the bolt plate 23, wherein the plate is additionally latched below in the support and receiving surface 21 by positive engagement, as described above (21b, 23 ').
  • the geometry of the distances c and d forms a rectangle, in particular one with substantially the same edge length.
  • the plate 23 additionally has a surface profiling to allow greater stiffening of the force transmitting plate.
  • This surface profiling 23a, 23b is already in FIG. 2 can be seen, by an approximately centrally disposed extending in the vertical direction embossing whose width substantially corresponds to the diameter of the bolt 22.
  • the embossment leaves two vertical edges, which are the transitions to two protuberances 23a remaining after the stiffening embossing of the strip 23b, for receiving the mounting sites.
  • FIG. 3 In the supervision (with partial cut in section) is in FIG. 3 a respective elongated strip with rounded ends to see, which is provided as a raised strip to the left and right of the bolt 22 on the mounting plate 23.
  • These raised stripes can either be due to the normal surface of the plate 23 remaining when the vertical embossing strip 23b is inserted.
  • the plate 23 may also comprise two further spaced embossing strips, which are arranged on the rear side on the side which rests on the wing. Then the raised stripes 23a also arise, with an additional stiffening.
  • edge unembossed strip portions remain with which the plate 23 rests flat on the wing, fed, for transmitting the forces of the plurality of horizontally and vertically spaced mounting points 24 and 24.
  • Three pairs of welds 26 hold the bolt 22 fixed to the pin plate 23rd ,
  • the entire wing weight can be transferred without lifting the wing plate 23 of the surface of the sliding sash.
  • the bolt 22 does not need to be additionally stiffened. It can also be formed integrally with the plate 23.
  • the plate can be inserted as a piece in the support and support surface 21b in a gap formed there. Such an extended mounting plate 23 can be mounted in the drive 20 or fixed by positive engagement in the gap.
  • the plate 23 is substantially longer than its width, and the counterpart 30 in the folding area is substantially narrower than the width of the plate 23rd
  • FIG. 4 For aluminum profiles offers an unclaimed design according to FIG. 4 in the lower corner E on.
  • the carriage 10 is of common design with housing surfaces 11,11 'of a housing on a support profile 62,61, as well as the profiles and the catch F shown in the folding air F on a drive rod 54, which controls the Ausstellterrorism and return movement of the sash FR with the Rol over Ü serves and is guided in a fitting groove 55.
  • the support profile 62 is held on a stay arm 63, which lies over a roller 64 on a running rail 65 which is fixedly mounted on the frame BR.
  • FIG. 4 In the transition area between the drive and the sliding sash is in FIG. 4 a corner encircling angle 50 is provided, the horizontal and vertical legs 50h and 50v of FIG. 5 can be seen.
  • the angle runs not only on one side or only on the other side of the corner, but around the corner, to stiffen the whole corner and to absorb higher forces.
  • FIG. 4 shows, or something like FIG. 3 illustrates that only here is to simplify a corner each with a different kind of profile system for the spars are described.
  • corner areas take in FIG. 4 the entire load without additional reinforcement parts on metal profiles.
  • said angle 50 is provided in the folding area F and is connected to the vertical and to the horizontal bar of the sliding leaf FR, in particular by means of connectors 56, 57.
  • the corner bracket is connected to the drive 10, in particular via a vertically extending connecting surface 61 provided there, for which purpose the screw shown here serves as a third connector 60.
  • the threaded connection as connector 60 engages a thread on the vertical leg 50v. It starts from the support surface 61 on the carriage and transfers the weight of the vertical leg directly into the Carriage.
  • the threaded hole 60a see. to FIG. 5 , is provided near the corner portion 51 of the bracket 50. Distinctly spaced from it, in the outer third of both a vertical screw 57 is provided, which engages in the opening 57 a, to set the vertical leg on the vertical spar. In approximately the same distance, the opening 56a is provided, in which engages the second screw 56, which defines the horizontal leg 50h on the horizontal bar.
  • the main connector 60 When assembled, the main connector 60, above the 45 ° line, but still at the level of the horizontal beam, but goes from the vertical leg 50 v, which from the system sketch of the FIG. 4a is apparent. In it only a few components and their functional context are shown. Starting from the sash FR, in the corner region of the stiffening angle 50 with legs 50v and 50h on the inside of the sash FR, seen from the rebate F, arranged. Two lying in the same plane, parallel to the sash extending screw connector 56,57 are also visible, as the one perpendicular to vertical connector 60, which is located at the height of the connecting surface 61 of the support profile 62. The rollover Ü is in FIG. 4a not marked, but off FIG. 4 seen. The power transmission is carried out by the vertical leg 50v, respectively, the lower portion lying at the corner portion 51 on the carriage.
  • Two of the screw connectors of FIG. 4a lie in the vertically oriented leg of the stiffening angle. These two are oriented substantially perpendicular to each other.
  • the connecting screw 56 arranged in the other, horizontal leg 50h could also be dispensed with, so that the wing is supported here only by a system.
  • the corner angle piece 50 is in FIG. 5 explains and has several profiles (cross sections) along the respective legs. In the vertical and horizontal legs, the connection point 57a, 57 or 56a, 56 is initially provided, for mounting on the sliding leaf in the seaming air F.
  • the formation of the corner angle 50 is, for example, at this point an H-profile, wherein the screw is arranged in a counterbore on a connecting leg 69 of the two remaining support legs 69a, 69b.
  • the two support legs are chamfered 70b front side corresponding to the inner surface of the sliding sash to give a linear or even strip-shaped contact with the boundary surfaces of the rebate F. They also fit well into the inner corner of the inner surfaces facing the fold.
  • the force of the mounting screw 56 is transmitted via two spaced profile legs on the wing.
  • Each left and right or top and bottom of the corner angle 50 has a different profile shape or cross section, as can be seen from the section A-A.
  • This mounting point 60 is not installed in the vertical beam but only as high as the height of the horizontal beam, so that an assembly without any visible screw from the inside of the room is possible.
  • the section AA of the angle 50 consists of two mutually facing U-shaped profiles to form an H-section, wherein the in FIG. 5 right continuous leg portion stronger and more viable is now formed to serve as a plant leg on the facing to the fold inside of the end face of the sash FR.
  • the shape also referred to as H-profile (or cross-section) with the central web 70 occupies the essential portion of the respective leg 50h, 50v in order to save weight.
  • the cross-sectional shape can be obtained by elongate lateral recesses 80.
  • the angle is 50 of FIG. 5 between the fitting groove 55 for the drive rod 54 (shown here with a snap) and the inner surface of the rollover Ü arranged. This results in no penetration of the screw 56.57 by a control part or a corner drive. Therefore standard corner deflections can be used.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Joining Of Corner Units Of Frames Or Wings (AREA)
  • Hinges (AREA)
  • Body Structure For Vehicles (AREA)
  • Wing Frames And Configurations (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Sewing Machines And Sewing (AREA)

Description

Die Erfindung befasst sich mit einem Laufwagenbeschlag für einen Schiebeflügel, der einen verbesserten Halt der Schiebeflügel am laufwagen ermöglichen sollen.The invention relates to a carriage fitting for a sliding sash, which should allow improved grip of the sliding sash on trolley.

Bei großen Flügelgewichten der Schiebeflügel entsteht im Flügel eine Torsion auf den unteren horizontalen Flügelholm. Die Verwindung wirkt sich auch auf die nicht verstärkten (nicht mit Metalleinlagen armierten) Überschläge insbesondere der senkrechten Holme des Schiebeflügels aus, so dass ein Verformen nach innen -in Richtung des Festrahmens (Blendrahmens) erfolgt. Diese Torsion hat ihre Ursache in einem nicht unterhalb des Schwerpunktes des Flügels am Blendrahmen horizontal beweglichen Laufwerks, meist auch Laufwagen genannt, der zur betrieblichen Bewegung des Schiebeflügels eingesetzt wird. Dieses Laufwerk ist bei einem unten abgestützten Schiebeflügel an dem unteren horizontalen Holm verfahrbar und wird zumeist im Eckbereich des Flügels mit dem Flügel fest verbunden. Die Verbindung geschieht über eine vorhandene Verstärkung, die in eine horizontale Stützfläche am Laufwerk gesteckt wird und am Schiebeflügel verschraubt ist, insbesondere an dem vertikalen Holm dieses Schiebeflügels. Diese bekannte Verstärkung wirkt der beschriebenen Verformung (Torsion) des Schiebeflügels entgegen. Werden die Kunststoffprofile verwendet, so sorgt eine Verschraubung der erwähnten Verstärkung in einem Holmbereich, der eine Metallarmierung besitzt, für eine solide Montage. Werden die Flügelgewichte aber immer höher, aufgrund größerer Glasgewichte oder Flächen der horizontal verschiebbaren Flügel, so kann die bekannte Montage eine Verformung nicht mehr ausreichend begrenzen.For large sash weights of the sliding sash creates a torsion on the lower horizontal wing spar in the wing. The distortion also affects the unreinforced (not reinforced with metal inserts) flashovers in particular the vertical bars of the sliding sash, so that a deformation inward -in the direction of the fixed frame (window frame) takes place. This torsion has its cause in a non-below the center of gravity of the wing on the frame horizontally movable drive, usually also called carriage, which is used for operational movement of the sliding sash. This drive is movable at a bottom supported sliding sash on the lower horizontal rail and is usually firmly connected to the wing in the corner of the wing. The connection is made via an existing reinforcement, which is plugged into a horizontal support surface on the drive and bolted to the sliding sash, in particular to the vertical spar of this sash. This known reinforcement counteracts the described deformation (torsion) of the sliding sash. If the plastic profiles are used, a screw connection of the mentioned reinforcement in a spar region, which has a metal reinforcement, ensures a solid assembly. But if the sash weights are getting higher, due to larger glass weights or surfaces of the horizontally displaceable wings, so the known assembly can no longer limit deformation sufficient.

Aus der EP-A 312 738 (von GU) ist eine flache oder winkelförmige Eckversteifung bekannt, welche der dortigen Figur 3 zu entnehmen ist. Sie liegt hinter dem Flügelüberschlag und wird durch zwei vertikal beabstandete Verbindungsschrauben, dort 10 und eine jeweilige Mutter, dort 12,13, mit dem Flügel verbunden. Diese Verbindungsstellen bleiben auf der Höhe des Laufwagens und sind abgedeckt. Eine über diesen Laufwagen hinaus nach oben sich erstreckende Montage findet in der dortigen Darstellung nicht statt, insbesondere auch nicht bei einer winkelförmig ausgestalteten Versteifung nach dortiger Spalte 5, Zeilen 48 bis 52.From the EP-A 312 738 (from GU) is a flat or angular Eckversteifung known which of the local FIG. 3 can be seen. It lies behind the wing flap and is connected by two vertically spaced connecting screws, there 10 and a respective nut, there 12,13, with the wing. These joints remain at the height of the carriage and are covered. An assembly extending beyond this carriage upward assembly does not take place in the local representation, in particular not at an angle-shaped stiffening according to local column 5, lines 48 to 52.

Die DE-U 87 09 299 (von HAUTAU), welches Dokument die Merkmale des Oberbegriffs des Anspruches 1 offenbart, zeigt ein Verstärkungsteil für einen gehäuseartigen Tragteil, welcher einen Schwenkzapfen eines Ausstellarms trägt, und dabei wird eine Platte, dort 14, vorgesehen, die über ein Abwinkelungsstück als nahezu horizontales Übergangsstück verfügt, in welches ein Bolzenstück von unten abgedeckt eingesetzt ist. Der Bolzen ist nicht unmittelbar an der Platte befestigt, sondern mittelbar über das Übergangsstück, das bei hohen Flügelgewichten im Winkelbereich zur Platte als Gelenk wirkt. Die Platte ist durch mehrere Montagestellen, dort über Schrauben 26, mit dem Flügel verschraubt und der nach unten ragende Bolzen steckt in zwei Aufnahmeöffnungen des Laufwagens, dort 12 nach dortiger Figur 3, und kann daraus auch entnommen werden. In jedem Falle sorgt eine Verkleidung, dort 16 für eine Abdeckung des in die Öffnungen eingesteckten und daraus wieder herausnehmbaren Bolzens, vgl. dort Seite 10, mittlerer Absatz.The DE-U 87 09 299 (HAUTAU), which document discloses the features of the preamble of claim 1, shows a reinforcing member for a box-like support member which carries a pivot pin of a stay arm, and thereby a plate, there 14, is provided, which via a bend piece as a nearly horizontal transition piece has, in which a stud piece is inserted covered from below. The bolt is not attached directly to the plate, but indirectly via the transition piece, which acts as a joint at high sash weights in the angular range to the plate. The plate is screwed through several mounting points, there via screws 26, with the wing and the downwardly projecting bolt inserted into two receiving openings of the carriage, there 12 to there FIG. 3 , and can be taken from it. In any case, a panel, there 16 provides for a cover of the plugged into the openings and from it again removable bolt, see. there page 10, middle paragraph.

Aufgabe der Erfindung ist es, einen Laufwagenbeschlag vorzuschlagen, mit der ein erhöhtes Flügelgewicht eines Schiebeflügels aufgenommen werden kann, mit welcher dieser Flügel insbesondere im Eckbereich versteift werden kann. Auch die Montagezeit soll verkürzt bzw. vereinfacht werden. Diese Aufgaben sind als technische Problemstellung auch jeweils individuell zu lösen. The object of the invention is to propose a carriage fitting, with which an increased sash weight of a sliding leaf can be added, with which this wing can be stiffened in particular in the corner. The assembly time should be shortened or simplified. These tasks can be individually solved as a technical problem.

Die Lösung ist die Erfindung nach Anspruch 1.The solution is the invention according to claim 1.

Der vorgeschlagene Laufwagenbeschlag ermöglicht es, dass insbesondere bei Kunststoffprofilen die in Vertikalrichtung sich erstreckende Montageplatte auf der Rauminnenseite des Flügels satt auf der Flügeloberfläche anliegt und trotz hoher Flügelgewichte keine Abhebeneigung zeigt. Die Platte ist über Paare von horizontal und vertical beabstandeten Montagestellen mit dem Flügel verbunden, so dass vier oder mehr Montagestellen einen Montageverbund bilden, der eine flächige Anlage der Plate an der Oberfläche des Flügels ermöglicht, zur Aufnahme und Übertragung hoher Kräfte auf das Laufwerk (den Laufwagen).The proposed carriage fitting makes it possible, in particular in the case of plastic profiles, for the mounting plate extending in the vertical direction to fit snugly against the wing surface on the interior side of the wing and not to raise the wing in spite of the high sash weights. The panel is connected to the wing via pairs of horizontally and vertically spaced mounting locations such that four or more mounting locations form an assembly assembly that allows the panel to abut the surface of the wing to receive and transfer high forces to the drive (the carriage).

Die Verbindung des Flügels über die besagte Platte erfolgt mittels eines Kupplungsstücks als Bolzen, der in eine im Wesentlichen horizontal liegende Aufnahme- oder Stützfläche des Laufwerks eingeführt wird und so mit dem Laufwerk fest aber unlösbar verbunden wird.The connection of the wing on the said plate is effected by means of a coupling piece as a bolt, which is inserted into a substantially horizontal receiving or support surface of the drive and so firmly but permanently connected to the drive.

Eine Eigenversteifung der Platte kann durch eine Oberflächenkonturierung, in Form von vertikalen Streifen (Anspruch 8) erfolgen. Von den vertikalen Streifen ist vorteilhaft zumindest einer ein geprägter Streifen, der eine zusätzliche Versteifung der Platte verursacht. Die Versteifung kann dabei den besagten verbiridungsbolzen zumindest ein Stück weit aufnehmen. Zwei erhabene Streifen können benachbart des einen Prägestreifens auftreten, um eine seitliche Stützung des Bolzens zu übernehmen (Anspruch 8,9 und 10).A self-stiffening of the plate can be done by a Oberflächenkonturierung, in the form of vertical strips (claim 8). Of the vertical strips is advantageous at least one embossed strip, which causes an additional stiffening of the plate. The stiffening can take the said Verbiridungsbolzen at least a little way. Two raised stripes may occur adjacent the one embossing strip to provide lateral support of the bolt (claims 8, 9 and 10).

Die erhabenen Streifen können dadurch entstehen, dass der eine Prägestreifen eingebracht ist. Es können aber auch oder alleine Prägestreifen auf der anderen Seite der Platte so vorgesehen sein, dass die erhabenen Streifen auf der Sichtseite ohne das Einprägen des einen Mittelstreifens entstehen. Auch mehrere beabstandete Prägestreifen können vorgesehen sein.The raised stripes can arise from the fact that the one embossed strip is introduced. But it can also or alone embossing strips on the other side of the plate be provided so that the raised strips on the visible side without the impression of a median strip arise. Also several spaced embossing strips can be provided.

Eine langgestreckte Stützplatte kann der insbesondere mit Prägestruktur ausgebildeten Montageplatte gegenüber liegen, und zwar auf der Seite des Falzraums (Falzluft). Hier ist sie so angeordnet, dass sie auf der Innenseite des Flügelüberschlags (zum festrahmen zeigend) angeordnet ist. Bevorzugt ist sie nicht so langgestreckt, wie die Beschriebene, bevorzugt geprägte Montageplatte, kann aber auch länger ausgebildet sein. Im montierten Zustand wird dabei zwischen der im Falz befindlichen Stützplatte und der auf der Oberfläche (Sichtseite) des Flügels angeordneten Montageplatte eine Verbindung hergestellt, insbesondere eine Schraubverbindung, die eine Versteifung des vertikalen Holms ausgehend vom unteren Eckbereich ermöglicht.An elongate support plate may be opposite to the mounting plate formed in particular with an embossed structure, specifically on the side of the rebate space (folding air). Here it is arranged so that it is located on the inside of the wing flap (facing the fixed frame). Preferably, it is not so elongated, as the described, preferably embossed mounting plate, but can also be made longer. In the assembled state, a connection is made between the support plate located in the rebate and the mounting plate arranged on the surface (visible side) of the sash, in particular a screw connection which permits stiffening of the vertical strut starting from the lower corner region.

Der Randbereich des Flügels, insbesondere der Überschlag, dient dabei der Versteifung mit einer Schichtstruktur, die durch Schrauben, Bolzen oder andere Spannorgane zu einem Verbund zusammengespannt ist. Solche Versteifungen können auch bei anderen Flügelrahmen, wie Metall oder Holz, Anwendung finden.The edge region of the wing, in particular the rollover, serves to stiffen with a layer structure which is clamped together by screws, bolts or other clamping members to form a composite. Such stiffeners can also be found in other sash frames, such as metal or wood, application.

Die Erfindung wird anhand folgendes Ausführungsbeispiels erläutert und ergänzt.

Figur 1
ist eine schrittweise Vergrößerung des rechten unteren Eckbereichs E eines Schiebeflügels FR in fünf Darstellungen, wobei die Achse 100 den Positionsbezug zwischen den oberen Bildern, dem mittleren Bild und der unteren Ausschnittsvergrößerung herstellt. Das linke Bild zeigt einen Ausschnitt in einem vertikalen Schnitt durch 100.
Figur 2
ist eine weitere schematische Schnittzeichnung durch den Randbereich des Schiebeflügels FR mit dem schematisch dargestellten Festrahmen BR und dem dazwischen befindlichen Falzraum F. Anhand des Überschlages Ü ist ersichtlich, in welchem Bereich der Schnitt gelegen ist.
Figur 3
ist eine starke Vergrößerung des mittleren Bildes der Figur 1, wobei Details der Platte 23 in einer Aufsicht und einer Schnittansicht gezeigt werden.
Figur 4
ist eine nicht beanspruchte Gestaltung eines für Metallrahmen vorgesehenen unteren Eckbereiches, hier der Laufwagen 10 von Figur 1.
Figur 4a
ist eine schematische Darstellung wichtiger Funktionselemente aus Figur 4.
Figur 5
sind zwei Darstellungen mit zwei Schnittdarstellungen eines Eckwinkels 50, wie er in Figur 4 im Eckbereich in der Falzluft F am Flügelrahmen FR angeschraubt ist.
The invention will be explained and supplemented by the following embodiment.
FIG. 1
is a stepwise enlargement of the right lower corner area E of a sash FR in five representations, wherein the axis 100 establishes the positional relationship between the upper images, the middle image and the lower detail magnification. The left picture shows a section in a vertical section through 100.
FIG. 2
is a further schematic sectional view through the edge region of the sash FR with the fixed frame BR schematically illustrated and the rebate space therebetween F. On the basis of the rollover Ü can be seen in which area the cut is located.
FIG. 3
is a strong enlargement of the middle picture of the FIG. 1 showing details of the plate 23 in a plan view and a sectional view.
FIG. 4
is an unclaimed design of a metal frame provided for lower corner area, here the carriage 10 of Figure 1.
FIG. 4a
is a schematic representation of important functional elements FIG. 4 ,
FIG. 5
are two representations with two sectional views of a corner angle 50, as it is screwed in Figure 4 in the corner area in the seaming air F on the sash FR.

In Figur 1 ist in einer oberen (zweigliedrigen), einer mittleren und einer unteren Darstellung der rechte untere Eckbereich des Schiebeflügels FR erläutert. Am unteren Holm des nur im unteren Bereich in einer seitlichen Aufsicht und in einer Aufsicht von der Stirnseite her gezeigten Schiebeflügels sind zwei Laufwerke 10,20 vorgesehen, die im jeweiligen Eckbereich E am unteren Holm montiert sind. Sie haben Laufrollen und laufen auf einer am Festrahmen BR angeordneten Laufschiene 65 (wie in Figur 4 gezeigt), zum Parallelverschieben des gesamten Flügels, der zuvor aus der Öffnung des Festrahmens herausgeführt worden ist, z.B. durch Kippen und Parallelabstellen. Der Eckbereich, der im weiteren erläutert werden soll, ist mit E bezeichnet. Hier ist das Laufwerk 20 vorgesehen, das über einen vertikalen Bolzen 22 und eine Platte 23 eine Verbindung zu dem Schiebeflügel FR besitzt. Das (rechte) Laufwerk 20 hat in der Stirnansicht eine horizontal verlaufende Stütz- oder Aufnahmefläche 21, in die der besagte Bolzen 22 eingreift. Eine gleiche Fläche 11 ist auch beim (linken) Laufwerk 10 vorgesehen, jedoch ohne Öffnung und ohne eine Aufnahme für einen Bolzen.In FIG. 1 is explained in an upper (two-part), a middle and a lower illustration of the right lower corner region of the sash FR. At the lower spar of only shown in the lower area in a lateral view and in a plan view from the front side sliding leaf two drives 10,20 are provided, which are mounted in the respective corner E at the lower spar. They have rollers and run on a fixed rail BR arranged rail 65 (as in FIG. 4 shown), for parallel displacement of the entire wing, which has been previously led out of the opening of the fixed frame, for example by tilting and Parallelabstellen. The corner area, which will be explained below, is denoted by E. Here, the drive 20 is provided, which has a vertical pin 22 and a plate 23 has a connection to the sliding leaf FR. The (right) drive 20 has in the end view a horizontally extending support or receiving surface 21 into which the said pin 22 engages. A similar surface 11 is also provided in the (left) drive 10, but without opening and without a receptacle for a bolt.

Eine einzelne Schraubenreihe 9 (beim Laufwagen 10) bzw. 19 (beim Laufwagen 20) ist vorgesehen, um in einem Eckbereich über die Länge des Laufwagens im wesentlichen regelmäßig verteilte Kräfte aufzunehmen und in das Tragstück des Laufwagens einzuleiten. Von dieser einzelnen Schraubreihe 19 im Laufwagen 20 sind in der mittleren Darstellung zwei repräsentative Befestigungsstellen durch Kreuzschlitzschrauben gezeigt, die durch den vertikalen Steg 21 b der Stütz- oder Aufnahmefläche 21 (oberhalb dieser) greifen und im Profil des horizontalen Holmes verankert sind. Eine Schraube 19 dieser Schraubenreihe ist in der großen Darstellung AV neben dem Bolzen 22 ersichtlich. Diese Schraubenreihe als einzelne Schraubenreihe dient der Reduzierung der Höhe des Laufwagens, um den Beschlag auch bei schmalen Profilen einsetzen zu können. Sie ist auch bei der zu Figur 4 erläuterten nicht beanspruchten Ausführung in gleicher Weise verwendbar.A single row of screws 9 (in the carriage 10) and 19 (in the carriage 20) is provided to receive in a corner region over the length of the carriage substantially regularly distributed forces and to initiate the support piece of the carriage. From this single row of screws 19 in the carriage 20 two representative attachment points are shown by Phillips screws in the middle view, which engage through the vertical web 21 b of the support or receiving surface 21 (above this) and are anchored in the profile of the horizontal spar. A screw 19 of this row of screws can be seen in the large illustration AV next to the bolt 22. This row of screws as a single row of screws serves to reduce the height of the carriage in order to use the fitting even with narrow profiles. She is also at the FIG. 4 explained not claimed embodiment in the same way usable.

Die Vergrößerung des Bereiches E aus der oberen Darstellung ist mit der Platte 23 in der mittleren Darstellung gezeigt. Diese Platte ist mit vier Befestigungsöffnungen 24a, 24b,25a,25b versehen, die im oberen Abschnitt der Befestigungsplatte 23 vorgesehen sind. In der Mitte, entlang der Achse 100, ist der Bolzen 22 fest an der Platte 23 angeordnet, z.B. durch Schweißstellen 26 oder anderweitiges Montieren. Der Bolzen steckt in einer Öffnung 21a der Horizontalfläche 21 und wird von dem Laufwerksrahmen, das aus den zwei Flächen 21 und einer vertikal verlaufenden Fläche 21' gebildet wird, aufgenommen. Der Bolzen kann hier durch Formschluss oder Passung gehalten werden.The enlargement of the area E from the upper illustration is shown with the plate 23 in the middle illustration. This plate is provided with four attachment openings 24 a, 24 b, 25 a, 25 b, which are provided in the upper portion of the mounting plate 23. In the middle, along the axis 100, the bolt 22 is fixedly attached to the plate 23, e.g. by welding 26 or otherwise mounting. The bolt is inserted in an opening 21a of the horizontal surface 21 and is received by the drive frame, which is formed from the two surfaces 21 and a vertically extending surface 21 '. The bolt can be held here by positive engagement or fit.

Als Ausschnittsvergrößerung AV nochmals vergrößert ist der Eingriff des Bolzens 22 in das Laufwerk in der rechten unteren Darstellung, mit einem Abschnitt 23' der Platte 23, die hier ein Stück weit in den vertikalen Flansch 21 b der Trag- und Stützfläche 21 des Laufwerks 20 eingreifend dargestellt ist.As a detail enlargement AV enlarged again is the engagement of the bolt 22 in the drive in the lower right illustration, with a portion 23 'of the plate 23, here a bit far into the vertical flange 21 b of the support and support surface 21 of the drive 20 engaging is shown.

Das Eingreifstück 23' ist eine Verlängerung der Bolzenplatte 23 und erstreckt sich in dieselbe Richtung, wie der untere Abschnitt der Bolzen 22. Das Verlängerungsstück kann zweiflügelig sein. Ein Flügel liegt auf der linken Seite und einer auf der rechten Seite des Bolzen 22. Die Ausschnittsvergrößerung AV zeigt den unteren Abschnitt des Bolzens am Eingriff in die Öffnung 21a und darüber das Eingreifen der beiden Flansche 23' in den vertikalen Abschnitt der Aufnahme- und Stützfläche 21, die mit 21b bezeichnet ist. Der Eingriff erfolgt nur ein Stück weit, namentlich so weit, wie die Schnittdarstellung der mittleren Abbildung in der linken Hälfte zeigt. Hier ist ein Spalt vorgesehen, in den ein in der Dicke verjüngtes vorderes Ende der Bolzenplatte 23, dargestellt als 23', eingreift bzw. hintergreift. Es entsteht dadurch ein an mehreren Stellen vorgesehenes Stützen und Halten, wobei die Stützpunkte lateral voneinander beabstandet sind.The engaging piece 23 'is an extension of the bolt plate 23 and extends in the same direction as the lower portion of the bolts 22. The extension piece may be double-winged. A wing is on The enlarged portion AV shows the lower portion of the bolt at the engagement in the opening 21a and above the engagement of the two flanges 23 'in the vertical portion of the receiving and supporting surface 21, which with 21b is designated. The intervention takes place only a little way, namely as far as the sectional view of the middle figure in the left half shows. Here, a gap is provided into which a thickness-tapered front end of the pin plate 23, shown as 23 ', engages or engages behind. This results in a multi-point provided support and holding, the bases are laterally spaced from each other.

Das verjüngte Stück 23' wird durch eine Prägung oder Quetschung des gesamten ein- oder zweiteiligen vorderen Abschnitts der Platte 23 hergestellt, die dadurch hinter den Steg 21 b einzugreifen vermag. Kurz über dem beschriebenen Eingriff ist eine als Anschweißstelle 26 beiderseits des Bolzens 22 vorgesehene Verbindungsstelle gezeigt, die den unteren Abschnitt des Bolzens mit der Bolzenplatte 23 verbindet, während weiter oben noch zumindest eine, bevorzugt zwei weitere beabstandete Schweißstellen beiderseits des Bolzen 22 die Verbindung mit der Bolzenplatte 23 vornehmen.The tapered piece 23 'is made by embossing or pinching the entire one- or two-piece front portion of the plate 23, which is thereby able to engage behind the web 21 b. Shortly above the procedure described a provided as welding point 26 on both sides of the bolt 22 connecting point is shown, which connects the lower portion of the bolt with the pin plate 23, while still above at least one, preferably two more spaced welds on both sides of the pin 22, the connection with the Make bolt plate 23.

Die beschriebenen "Montagestellen" 24,25 (jeweils a und b) sollen im folgenden mehrdeutig verwendet werden. Sie bilden entweder eine Öffnung, mit Bezug auf die anzuschraubende Platte 23, oder die Montagestellen sind bereits im montierten Zustand so beschrieben, dass Halte- oder Befestigungsmittel wie Schrauben, Bolzen, Spannmittel oder sonstige Montageteile in die Öffnungen eingesetzt sind, um die Platte 23 an dem Schiebeflügel FR zu befestigen. Der technische Begriff der Montagestelle soll deshalb mehrdeutig verwendet werden.The described "mounting sites" 24,25 (each a and b) will be used in the following ambiguous. They either form an opening with respect to the plate 23 to be screwed on, or the mounting points are already described in the installed state so that holding or fastening means such as screws, bolts, clamping means or other mounting parts are inserted into the openings to the plate 23 at to attach the sliding leaf FR. The technical term of the mounting point should therefore be used ambiguously.

Die Schnittdarstellung des Eckbereiches E in einer horizontalen Ebene ist in Figur 2 veranschaulicht. Festrahmen BR und beweglicher Flügelrahmen (auch Schiebeflügel genannt) FR sind ersichtlich, ebenso die Falzluft F und die Standardnut N zur Aufnahme von Verschlussstangen. Der Flügelrahmen FR besteht in schematischer Darstellung aus einem Holzprofil oder - gestrichelt dargestellt - aus einem Kunststoffprofil mit Innenräumen, die durch eine Metallarmierung 31 zumindest abschnittsweise verstärkt sind. Der Überschlagsbereich Ü des Flügels ist von einer Montagestelle 24b (oder 25b, je nach Höhenlage des Schnitts) durchgriffen dargestellt. Der Überschlag überdeckt den Falzraum F und ragt herüber bis zum Festrahmen BR. Ebenfalls ersichtlich ist die horizontale Stütz- und Aufnahmefläche 21, in die - von oben gesehen - der Bolzen 22 eingreift und am Laufwerk 20 - wie beschrieben - montiert wird.The sectional view of the corner area E in a horizontal plane is in FIG. 2 illustrated. Fixed frame BR and movable sash (also called sliding sash) FR are visible, as well as the seaming air F and the standard groove N for receiving locking rods. The sash FR consists in a schematic representation of a wooden profile or - shown in phantom - of a plastic profile with interiors, which are at least partially reinforced by a metal reinforcement 31. The rollover area Ü of the wing is represented by a mounting point 24b (or 25b, depending on the vertical position of the section). The rollover covers the rebate F and protrudes over to the fixed frame BR. Also visible is the horizontal support and receiving surface 21, in which - seen from above - the bolt 22 engages and on the drive 20 - as described - is mounted.

Nachdem die beschriebene Anordnung für alle Arten von Flügelprofilen geeignet ist, spezifisch aber für Kunststoffprofile, soll die Beschreibung anhand eines Kunststoffprofils erfolgen.After the arrangement described is suitable for all types of wing profiles, but specifically for plastic profiles, the description should be made on the basis of a plastic profile.

Es sind zwei beabstandete Montagestellen 24a,24b ersichtlich, die in Figur 1 (in der mittleren Darstellung) ebenfalls gezeigt worden sind. Sie sind am oberen Endabschnitt der Platte 23 angeordnet und in Horizontalrichtung um das Maß c beabstandet, was aus Figur 3 ersehen werden kann. In Vertikalrichtung beabstandet sind zwei weitere Montagestellen 25a,25b vorgesehen, deren Abstand zu den ersten Montagestellen beträgt d, was ebenfalls aus Figur 3 ersichtlich ist. Es bilden sich somit zwei Reihen a,b von mehreren (zumindest zwei) Montagestellen diesseits und jenseits des Bolzens 22 an der Platte 23, von denen in Figur 2 zwei ersichtlich sind, welche beiden sowohl die oberen beiden Montagestellen 24a,24b wie auch die unteren beiden Montagestellen 25a,25b sein können. Eine Montagestelle wird so verwirklicht, dass durch die Platte 23 jeweils ein Schraubbolzen oder eine Schraube hindurchgeführt wird und am Flügel FR befestigt wird. Die Befestigung geschieht dabei einmal im Profilbereich (abseits des Randes), bevorzugt in der Metallarmierung 31, und ein weiteres Mal im Überschlagsbereich durch den Überschlag hindurch und an einer zusätzlichen Stützplatte 30, die im Falzraum F in Figur 2 erkennbar ist. Diese Platte kann länger ausgebildet sein als die langgestreckte Platte 23, sie kann auch aus einzelnen Elementen bestehen, je nachdem, welche Aufgabe und Funktion ihr zugewiesen wird. Soll sie nur zur Montage dienen, kann sie aus einzelnen Stücken bestehen. Soll sie langgestreckt sein, um Tragkräfte des Flügels zusätzlich aufnehmen zu können, zur Ausbildung einer aus zumindest drei Lagen bestehenden Sandwich-Struktur im Überschlagsbereich Ü, kann sie ebenfalls langgestreckt sein, bevorzugt länger als die Montageplatte 23. In der Falzluft F erstreckt sie sich dabei unsichtbar für den Benutzer des Schiebeflügels, der von außen nicht erkennt, dass weitere Versteifungsmaßnahmen im unteren Eckbereich E, insbesondere bei Kunststoffprofilen vorgesehen sind, um höhere Flügelgewichte aufnehmen zu können.There are two spaced mounting points 24a, 24b, which in FIG. 1 (in the middle illustration) have also been shown. They are arranged at the upper end portion of the plate 23 and spaced in the horizontal direction by the dimension c, which is made FIG. 3 can be seen. Spaced apart in the vertical direction, two further mounting points 25a, 25b are provided, the distance to the first mounting points is d, which is also made FIG. 3 is apparent. Thus, two rows a, b of several (at least two) mounting points on this side and on the other side of the bolt 22 on the plate 23, of which in FIG FIG. 2 two can be seen, which both can be both the upper two mounting locations 24a, 24b as well as the lower two mounting locations 25a, 25b. A mounting point is realized so that a screw bolt or a screw is passed through the plate 23 and is fixed to the wing FR. The attachment takes place once in the profile area (off the edge), preferably in the metal reinforcement 31, and again in the rollover area by the rollover and on an additional support plate 30 in the rebate F in FIG. 2 is recognizable. This plate can be made longer than the elongated plate 23, it can also consist of individual elements, depending on which task and function is assigned to it. Should it only serve for assembly, it can consist of individual pieces. If it is to be elongated in order to be able to additionally absorb bearing forces of the wing, to form a sandwich structure consisting of at least three layers in the rollover area Ü, it can likewise be elongated, preferably longer than the mounting plate 23. In the seaming air F, it extends invisible to the user of the sash, which does not recognize from the outside, that further stiffening measures in the lower corner E, especially for plastic profiles are provided to accommodate higher sash weights can.

Die zwei Schraubreihen haben damit einmal die Montagefunktion im Bereich des Profils und ein anderes Mal die Montagefunktion im Bereich des Überschlages, die Trag- und Stützplatte 30 im Flügelbereich hat ebenfalls Stützfunktion, und alle Eigenschaften gemeinsam können eine stark erhöhte Versteifung des unteren Eckbereiches hervorrufen, mit der ohne optische Veränderung hohe Flügelgewichte aufgenommen und ohne wesentliche Torsion des gesamten Schiebeflügels über den Laufwagen 20 auf den Festrahmen BR übertragen werden können.The two rows of screws thus once have the assembly function in the profile and at another time the mounting function in the area of the rollover, the support and support plate 30 in the wing area also has support function, and all properties together can cause a greatly increased stiffening of the lower corner, with recorded without visual change high sash weights and can be transferred to the fixed frame BR without significant torsion of the entire sliding sash over the carriage 20.

Die beschriebenen mehreren Montagestellen 24,25 sind in Figur 3 als eine flächige Montage erkennbar. Je mehr Montagestellen entlang der beiden - im wesentlichen Reihen bildenden - Linien a,b vorgesehen sind, desto höher sind die Kräfte, die über die Montageplatte 23 von der inneren Trag- und Versteifungsplatte 30 aufgenommen und auf den Laufwagen 20 mit seinen beiden den Tragrahmen bildenden Ebenen 21,21' übertragen werden. Für die Übertragung dieser Kräfte sorgt der auch in Figur 3 erkennbare Bolzen 22, der so zwischen die Montagestellen 24,25 gelegt ist, dass er symmetrisch dazu fest an der Platte 23 angeordnet ist.The described multiple mounting locations 24,25 are in FIG. 3 recognizable as a surface mounting. The more mounting points along the two - essentially rows forming lines a, b are provided, the higher are the forces received on the mounting plate 23 of the inner support and stiffening plate 30 and on the carriage 20 with its two forming the support frame Levels 21,21 'are transmitted. Ensures the transfer of these forces which also in FIG. 3 recognizable bolt 22, which is placed between the mounting points 24,25, that it is symmetrically arranged fixed to the plate 23.

Die Montagestellen sind bevorzugt im oberen Bereich der Bolzenplatte 23 angeordnet, wobei die Platte zusätzlich unten in der Stütz- und Aufnahmefläche 21 durch Formschluss eingeklinkt ist, wie oben beschrieben (21b,23'). Die Geometrie aus den Abständen c und d bildet ein Rechteck, insbesondere ein solches mit im wesentlichen gleicher Kantenlänge.The mounting points are preferably arranged in the upper region of the bolt plate 23, wherein the plate is additionally latched below in the support and receiving surface 21 by positive engagement, as described above (21b, 23 '). The geometry of the distances c and d forms a rectangle, in particular one with substantially the same edge length.

Die Platte 23 hat zusätzlich eine Oberflächenprofilierung, um eine größere Versteifung der die Kräfte übertragenden Platte zu ermöglichen. Diese Oberflächenprofilierung 23a,23b ist bereits in Figur 2 ersichtlich, durch eine etwa mittig angeordnete, in Vertikalrichtung verlaufende Prägung, deren Breite im wesentlichen dem Durchmesser des Bolzens 22 entspricht. Die Prägung hinterlässt zwei vertikal verlaufende Kanten, die die Übergänge zu zwei Erhebungen 23a sind, die nach dem versteifenden Prägen des Streifens 23b verbleiben, zur Aufnahme der Montagestellen.The plate 23 additionally has a surface profiling to allow greater stiffening of the force transmitting plate. This surface profiling 23a, 23b is already in FIG. 2 can be seen, by an approximately centrally disposed extending in the vertical direction embossing whose width substantially corresponds to the diameter of the bolt 22. The embossment leaves two vertical edges, which are the transitions to two protuberances 23a remaining after the stiffening embossing of the strip 23b, for receiving the mounting sites.

In der Aufsicht (mit Teilausschnitt im Schnitt) ist in Figur 3 ein jeweils langgestreckter Streifen mit abgerundeten Enden zu ersehen, der als erhabener Streifen links und rechts des Bolzens 22 an der Montageplatte 23 vorgesehen ist. Diese erhabenen Streifen können entweder durch Verbleiben der normalen Oberfläche der Platte 23 entstehen, wenn der vertikale Prägestreifen 23b eingebracht wird. Ohne einen solchen vertikalen Prägestreifen oder zusätzlich zu ihm kann die Platte 23 auch zwei weitere beabstandete Prägestreifen aufweisen, die rückseitig auf derjenigen Seite angeordnet sind, die auf dem Flügel aufliegt. Dann entstehen die erhabenen Streifen 23a ebenso, bei einer zusätzlichen Versteifung. Jeweils randseitig sind ungeprägte Streifenabschnitte verblieben, mit denen die Platte 23 am Flügel flächig, satt aufliegt, zur Übertragung der Kräfte von den mehreren horizontal und vertikal beabstandeten Montagestellen 24 bzw. 24. Drei Paare von Anschweißstellen 26 halten den Bolzen 22 fest an der Bolzenplatte 23.In the supervision (with partial cut in section) is in FIG. 3 a respective elongated strip with rounded ends to see, which is provided as a raised strip to the left and right of the bolt 22 on the mounting plate 23. These raised stripes can either be due to the normal surface of the plate 23 remaining when the vertical embossing strip 23b is inserted. Without such a vertical embossing strip or in addition to it, the plate 23 may also comprise two further spaced embossing strips, which are arranged on the rear side on the side which rests on the wing. Then the raised stripes 23a also arise, with an additional stiffening. In each case the edge unembossed strip portions remain with which the plate 23 rests flat on the wing, fed, for transmitting the forces of the plurality of horizontally and vertically spaced mounting points 24 and 24. Three pairs of welds 26 hold the bolt 22 fixed to the pin plate 23rd ,

Durch die flächige Anschraubung oder Anpressung, einerseits im Profilbereich und andererseits im Überschlagsbereich mit dem aus Stahl bestehenden Streifen 30 kann das gesamte Flügelgewicht ohne Abheben der Flügelplatte 23 von der Oberfläche des Schiebeflügels übertragen werden. Der Bolzen 22 braucht dabei nicht zusätzlich versteift zu sein. Er kann auch integral mit der Platte 23 ausgebildet werden. Die Platte kann als Stück in die Trag- und Stützfläche 21b in einen dort gebildeten Spalt eingeschoben werden. Eine so verlängerte Montageplatte 23 kann im Laufwerk 20 montiert bzw. auch durch Formschluss im Spalt befestigt werden.Due to the surface screwing or contact pressure, on the one hand in the profile area and on the other hand in the rollover area with the steel strip 30, the entire wing weight can be transferred without lifting the wing plate 23 of the surface of the sliding sash. The bolt 22 does not need to be additionally stiffened. It can also be formed integrally with the plate 23. The plate can be inserted as a piece in the support and support surface 21b in a gap formed there. Such an extended mounting plate 23 can be mounted in the drive 20 or fixed by positive engagement in the gap.

Die Platte 23 ist dabei wesentlich länger als ihre Breite, und das Gegenstück 30 im Falzbereich ist wesentlich schmäler als die Breite der Platte 23.The plate 23 is substantially longer than its width, and the counterpart 30 in the folding area is substantially narrower than the width of the plate 23rd

Für Aluminiumprofile bietet sich eine nicht beanspruchte Gestaltung gemäß Figur 4 im unteren Eckbereich E an. Hier wird der linke Laufwagen 10 der Figur 1 erläutert, der schematisch mit einer anderen Profilgestaltung des Holmes belegt werden soll, wie aus Figur 4 ersichtlich. Der Laufwagen 10 ist gängiger Bauart mit Gehäuseflächen 11,11' eines Gehäuses über einem Tragprofil 62,61, wie auch die Profile und der in der Falzluft F gezeigte Schnäpper an einer Treibstange 54, der zur Steuerung der Ausstellbewegung und Rückstellbewegung des Schiebeflügels FR mit dem Überschlag Ü dient und dazu in einer Beschlagnut 55 geführt ist. Das Tragprofil 62 ist auf einem Ausstellarm 63 gehalten, der über eine Laufrolle 64 auf einer Laufschiene 65 liegt, die am Blendrahmen BR fest angeordnet ist. Das Gehäuse 11,11' deckt das Tragprofil 62 ab. Im Übergangsbereich zwischen dem Laufwerk und dem Schiebeflügel ist ein Ausschnitt in Aufsicht dargestellt, während der übrige Teil in einer Schnittdarstellung gezeigt ist.For aluminum profiles offers an unclaimed design according to FIG. 4 in the lower corner E on. Here is the left carriage 10 of FIG. 1 explained, which is to be occupied schematically with a different profile design of the spar, as from FIG. 4 seen. The carriage 10 is of common design with housing surfaces 11,11 'of a housing on a support profile 62,61, as well as the profiles and the catch F shown in the folding air F on a drive rod 54, which controls the Ausstellbewegung and return movement of the sash FR with the Rol over Ü serves and is guided in a fitting groove 55. The support profile 62 is held on a stay arm 63, which lies over a roller 64 on a running rail 65 which is fixedly mounted on the frame BR. The housing 11,11 'covers the support profile 62. In the transition area between the drive and the sliding sash a section is shown in plan view, while the remaining part is shown in a sectional view.

Im Übergangsbereich zwischen dem Laufwerk und dem Schiebeflügel ist in Figur 4 ein eckumlaufender Winkel 50 vorgesehen, dessen horizontaler und vertikaler Schenkel 50h und 50v aus Figur 5 ersichtlich sind. Der Winkel verläuft nicht nur auf der einen oder nur auf der anderen Seite der Ecke, sondern eckumlaufend, zur Versteifung der ganzen Ecke und zur Aufnahme höherer Kräfte.In the transition area between the drive and the sliding sash is in FIG. 4 a corner encircling angle 50 is provided, the horizontal and vertical legs 50h and 50v of FIG. 5 can be seen. The angle runs not only on one side or only on the other side of the corner, but around the corner, to stiffen the whole corner and to absorb higher forces.

Es versteht sich, dass für einen regulären Schiebeflügel die linke und rechte Ecke in der Regel gleich abgestützt sind, also so wie Figur 4 zeigt, oder so wie Figur 3 veranschaulicht, nur hier soll zur Vereinfachung jeweils eine Ecke mit einem jeweils anders gearteten Profilsystem für die Holme beschrieben werden.It is understood that for a regular sliding sash, the left and right corners are usually supported the same, so as well FIG. 4 shows, or something like FIG. 3 illustrates that only here is to simplify a corner each with a different kind of profile system for the spars are described.

Die Eckbereiche nehmen in Figur 4 die gesamte Last ohne zusätzliche Verstärkungsteile bei Metallprofilen auf. Innen ist im Falzbereich F der genannte Winkel 50 vorgesehen und steht mit dem senkrechten und mit dem waagerechten Holm des Schiebeflügels FR in Verbindung, insbesondere über Verbinder 56,57 verschraubt. Zusätzlich ist der Eckwinkel mit dem Laufwerk 10 verbunden, insbesondere über eine dort vorgesehene vertikal verlaufende Verbindungsfläche 61, wozu die hier dargestellte Schraube als dritter Verbinder 60 dient. Die Verbindung des Eckwinkels mit dem vertikalen Holm erfolgt über eine Schraubverbindung 57.The corner areas take in FIG. 4 the entire load without additional reinforcement parts on metal profiles. Internally, said angle 50 is provided in the folding area F and is connected to the vertical and to the horizontal bar of the sliding leaf FR, in particular by means of connectors 56, 57. In addition, the corner bracket is connected to the drive 10, in particular via a vertically extending connecting surface 61 provided there, for which purpose the screw shown here serves as a third connector 60. The connection of the corner angle with the vertical bar via a screw 57th

Die Verbindung des horizontalen Schenkels 50h erfolgt über die Schraubverbindung 56. Im vertikalen Schenkel 50v ist die eine weitere Schraubverbindung 60 vorgesehen, mit der die Gewichtskraft der Ecke auf den Laufwagen übertragen wird. Die Schraubverbindung 60 ist die äußerste Schraubstelle für den Fall, dass eine Schraubenreihe gemäß der Figur 1 auch bei diesem Ausführungsbeispiel verwendet wird. Andere Schrauben, als die äußerste Schraube der Schraubenreihen (diejenige, die der Ecke des Flügels am nächsten ist), greifen vom Laufwagen bzw. dessen Verbindungsfläche 61 nicht in den Eckversteifungswinkel 50 ein.The connection of the horizontal leg 50h via the screw 56. In the vertical leg 50v, a further screw 60 is provided with which the weight of the corner is transmitted to the carriage. The screw 60 is the outermost Schraubstelle in the event that a row of screws according to FIG. 1 is also used in this embodiment. Screws other than the outermost screw of the screw rows (the one closest to the corner of the wing) do not engage the corner stiffening angle 50 from the carriage or its connecting surface 61.

Die Schraubverbindung als Verbinder 60 greift in ein Gewinde am vertikalen Schenkel 50v ein. Sie geht von der Stützfläche 61 am Laufwagen aus und überträgt die Gewichtskraft vom vertikalen Schenkel direkt in den Laufwagen. Die Gewindebohrung 60a, vgl. dazu Figur 5, ist nahe des Eckbereiches 51 des Winkels 50 vorgesehen. Deutlich beabstandet davon, im äußeren Drittel ist sowohl die eine dazu senkrechte Schraube 57 vorgesehen, die in die Öffnung 57a greift, um den vertikalen Schenkel am vertikalen Holm festzulegen. In etwa in einem gleichen Abstand ist die Öffnung 56a vorgesehen, in die die zweite Schraube 56 eingreift, die den horizontalen Schenkel 50h am horizontalen Holm festlegt. Die Kraftübertragung der Gewichtskraft im Eckbereich erfolgt über den horizontalen Schenkel 50h, die Ecke 51 des Winkels 50 und den vertikalen Schenkel in zumindest einem Abschnitt bis zur Verbindungsstelle 60, während auch der vertikale Schenkel 50v Kraft des Flügels aufnimmt und über dieselbe Verbindungsstelle 60 auf den Laufwagen überträgt.The threaded connection as connector 60 engages a thread on the vertical leg 50v. It starts from the support surface 61 on the carriage and transfers the weight of the vertical leg directly into the Carriage. The threaded hole 60a, see. to FIG. 5 , is provided near the corner portion 51 of the bracket 50. Distinctly spaced from it, in the outer third of both a vertical screw 57 is provided, which engages in the opening 57 a, to set the vertical leg on the vertical spar. In approximately the same distance, the opening 56a is provided, in which engages the second screw 56, which defines the horizontal leg 50h on the horizontal bar. The force transmission of the weight force in the corner region via the horizontal leg 50h, the corner 51 of the angle 50 and the vertical leg in at least a portion to the junction 60, while the vertical leg 50v receives power of the wing and the same connection point 60 on the carriage transfers.

Zur sicheren Verbindung und Übertragung im Eckbereich sind keine weiteren Schraubverbindungen nötig, so dass Montagezeit eingespart werden kann. Die Montage des Versteifungswinkels 50 erfolgt in der Innenecke, wo die beiden Innenflächen zusammenstoßen, die den Falzraum nach oben und rechts in Figur 4 begrenzen.For secure connection and transmission in the corner no further screw connections are needed, so that assembly time can be saved. The mounting of the stiffening angle 50 takes place in the inner corner, where the two inner surfaces collide, the Falzraum up and right in FIG. 4 limit.

Im montierten Zustand liegt der Hauptverbinder 60, oberhalb der 45°-Linie, jedoch noch auf der Höhe des horizontalen Holms, geht aber vom vertikalen Schenkel 50v aus, was aus der Systemskizze der Figur 4a ersichtlich ist. In ihr sind nur einige Komponenten und ihr Funktionszusammenhang gezeigt. Ausgehend vom Flügelrahmen FR ist in dessen Eckbereich der Versteifungswinkel 50 mit Schenkeln 50v und 50h an der Innenseite des Flügelrahmens FR, gesehen vom Falzraum F, angeordnet. Zwei in derselben Ebene liegende, parallel zum Flügelrahmen verlaufende Schraubverbinder 56,57 sind ebenso ersichtlich, wie der eine dazu senkrechte Hauptverbinder 60, der auf der Höhe der Verbindungsfläche 61 des Tragprofiles 62 gelegen ist. Der Überschlag Ü ist in Figur 4a nicht eingezeichnet, aber aus Figur 4 ersichtlich. Die Kraftübertragung erfolgt vom vertikalen Schenkel 50v ausgehend, respektive dessen unterem am Eckbereich 51 liegenden Abschnitt auf den Laufwagen.When assembled, the main connector 60, above the 45 ° line, but still at the level of the horizontal beam, but goes from the vertical leg 50 v, which from the system sketch of the FIG. 4a is apparent. In it only a few components and their functional context are shown. Starting from the sash FR, in the corner region of the stiffening angle 50 with legs 50v and 50h on the inside of the sash FR, seen from the rebate F, arranged. Two lying in the same plane, parallel to the sash extending screw connector 56,57 are also visible, as the one perpendicular to vertical connector 60, which is located at the height of the connecting surface 61 of the support profile 62. The rollover Ü is in FIG. 4a not marked, but off FIG. 4 seen. The power transmission is carried out by the vertical leg 50v, respectively, the lower portion lying at the corner portion 51 on the carriage.

Zwei der Schraubverbinder von Figur 4a liegen im vertikal orientierten Schenkel des Versteifungswinkels. Diese beiden sind im wesentlichen senkrecht zueinander orientiert. Die im anderen, horizontalen Schenkel 50h angeordnete Verbindungsschraube 56 könnte auch entfallen, so dass der Flügel hier nur durch eine Anlage gestützt ist.Two of the screw connectors of FIG. 4a lie in the vertically oriented leg of the stiffening angle. These two are oriented substantially perpendicular to each other. The connecting screw 56 arranged in the other, horizontal leg 50h could also be dispensed with, so that the wing is supported here only by a system.

Auch mit dieser Verstärkungsvariante kann eine Flügelgewichtserhöhung bzw. -versteifung erreicht werden, ohne dass vom Rauminneren her diese Versteifungsmaßnahmen für den Benutzer zu erkennen sind. Die vorhandene Optik bleibt erhalten. Das Eckwinkelstück 50 ist in Figur 5 erläutert und weist mehrere Profile (Querschnitte) entlang der jeweiligen Schenkel auf. Im vertikalen und horizontalen Schenkel ist dabei zunächst die Verbindungsstelle 57a,57 bzw. 56a,56 vorgesehen, zur Montage am Schiebeflügel in der Falzluft F.Even with this reinforcement variant, a wing weight increase or stiffening can be achieved without these stiffening measures for the user to be recognized from the interior of the room. The existing look is retained. The corner angle piece 50 is in FIG. 5 explains and has several profiles (cross sections) along the respective legs. In the vertical and horizontal legs, the connection point 57a, 57 or 56a, 56 is initially provided, for mounting on the sliding leaf in the seaming air F.

Die Ausbildung des Eckwinkels 50 ist beispielsweise an dieser Stelle ein H-Profil, wobei die Schraube in einer Senkbohrung auf einem Verbindungsschenkel 69 der beiden verbleibenden Stützschenkel 69a,69b angeordnet ist. Die beiden Stützschenkel sind vorderseitig entsprechend der Innenfläche am Schiebeflügel abgeschrägt 70b, um eine linienförmige oder sogar streifenförmige Anlage an den Begrenzungsflächen des Falzraumes F zu ergeben. Sie fügen sich dabei auch gut in die Innenecke der zum Falz weisenden Innenflächen ein. Die Kraft der Montageschraube 56 wird über zwei beabstandete Profilschenkel auf den Flügel übertragen.The formation of the corner angle 50 is, for example, at this point an H-profile, wherein the screw is arranged in a counterbore on a connecting leg 69 of the two remaining support legs 69a, 69b. The two support legs are chamfered 70b front side corresponding to the inner surface of the sliding sash to give a linear or even strip-shaped contact with the boundary surfaces of the rebate F. They also fit well into the inner corner of the inner surfaces facing the fold. The force of the mounting screw 56 is transmitted via two spaced profile legs on the wing.

Gleiches gilt für die vertikale Montageschraube 57. Jeweils links und rechts bzw. oben und unten davon hat der Eckwinkel 50 eine andere Profilgestalt bzw. Querschnitt, wie er aus dem Schnitt A-A ersichtlich ist.The same applies to the vertical mounting screw 57. Each left and right or top and bottom of the corner angle 50 has a different profile shape or cross section, as can be seen from the section A-A.

Nahe dem Verbindungsbereich 51 des Winkels 50, an dem die beiden Schenkel 50v und 50h zusammenlaufen, ist in einem massiven Stück einer Profilgestaltung gemäß Schnitt B-B oder einem Querschnitt gemäß Schnitt A-A eine zu den beiden Bohrungen 56a,57a senkrecht verlaufende Bohrung 60a (mit Gewinde) vorgesehen, die zur Montage an der Verbindungsfläche 61 des Laufwerks 10 mit einer weiteren Schraube 60 dient.Near the connecting portion 51 of the angle 50, at which the two legs 50v and 50h converge, is in a solid piece of a profile design according to section BB or a cross section AA according to section one to the two holes 56a, 57a perpendicular bore 60a (with thread) provided, which serves for mounting on the connecting surface 61 of the drive 10 with a further screw 60.

Es kann eine weitere solche Bohrung auch in dem horizontalen Schenkel 50h vorgesehen sein.There may be another such hole also provided in the horizontal leg 50h.

Die Höhe dieser Montagestelle 60 ist nicht in den vertikalen Holm verlegt sondern nur so hoch, wie die Höhe des horizontalen Holms, so dass eine Montage ohne jede sichtbare Schraubverbindung von der Rauminnenseite möglich ist.The height of this mounting point 60 is not installed in the vertical beam but only as high as the height of the horizontal beam, so that an assembly without any visible screw from the inside of the room is possible.

Der Schnitt A-A des Winkels 50 besteht aus zwei voneinander weg weisenden U-förmigen Profilierungen zur Bildung eines H-Querschnitts, wobei der in Figur 5 rechte durchgehenden Schenkelabschnitt stärker und tragfähiger jetzt ausgebildet ist, um als Anlageschenkel an der zum Falz weisenden Innenseite der Stirnfläche des Schiebeflügels FR zu dienen. Die auch als H-Profil (oder Querschnitt) zu bezeichnende Gestalt mit dem Mittelsteg 70 nimmt den wesentlichen Abschnitt des jeweiligen Schenkel 50h,50v ein, um Gewicht zu sparen. Bei einem Druckgussstück kann die Querschnittsform durch langgestreckte seitliche Aussparungen 80 erhalten werden.The section AA of the angle 50 consists of two mutually facing U-shaped profiles to form an H-section, wherein the in FIG. 5 right continuous leg portion stronger and more viable is now formed to serve as a plant leg on the facing to the fold inside of the end face of the sash FR. The shape also referred to as H-profile (or cross-section) with the central web 70 occupies the essential portion of the respective leg 50h, 50v in order to save weight. In a die casting, the cross-sectional shape can be obtained by elongate lateral recesses 80.

Trotz senkrecht zueinander orientierten Montagestellen 56,57 einerseits bzw. 60 andererseits kann jeweiliger Schenkel gemäß Figur 5a Kräfte in beiden genannten Richtungen aufnehmen und auf die zum Falz F weisenden Innenflächen des Aluminiumprofils übertragen. In der jeweiligen Montagestelle ist es dabei vorteilhaft, dass beidseits der Zugverbindung durch die Schraubstelle jeweils ein verbleibender Steg 69a,69b bzw. 70a,70b zu dieser Innenfläche zeigt, so dass ein Verkippen, Verkanten und Verwinden des Eckwinkels vermieden werden können.Despite perpendicular to each other oriented mounting points 56,57 on the one hand and 60 on the other hand, respective leg according to FIG. 5a Pick up forces in both directions and transferred to the facing to the seam F inside surfaces of the aluminum profile. In each assembly point, it is advantageous that both sides of the train connection through the screw point in each case a remaining web 69a, 69b and 70a, 70b points to this inner surface, so that tilting, tilting and twisting of the corner angle can be avoided.

Wie aus Figur 4 ersichtlich, ist der Winkel 50 von Figur 5 zwischen der Beschlagnut 55 für die Treibstange 54 (hier mit einen Schnäpper dargestellt) und der Innenfläche des Überschlages Ü angeordnet. Dadurch ergibt sich kein Durchgriff der Schraubverbinder 56,57 durch ein Steuerteil oder eine Eckumlenkung. Es können deshalb Standard-Eckumlenkungen verwendet werden.How out FIG. 4 can be seen, the angle is 50 of FIG. 5 between the fitting groove 55 for the drive rod 54 (shown here with a snap) and the inner surface of the rollover Ü arranged. This results in no penetration of the screw 56.57 by a control part or a corner drive. Therefore standard corner deflections can be used.

Claims (15)

  1. A carriage fitting for a sliding sash having tilt capability, which sliding sash (FR) has horizontal and vertical spars and is installable via at least one thereof on at least one carriage (10, 20), which is movable in parallel to a fixed frame (BR), of the carriage fitting, which carriage is fixedly connectable to the sliding sash in a corner region of the sliding sash (FR); wherein
    - the carriage (20) has a horizontal receptacle or support surface (21), which extends essentially perpendicularly to the plane of the sliding sash in the installed state;
    - a bolt (22) engages in an opening (21a) of the receptacle or support surface (21) to form a fixed but detachable connection and is connectable via an elongated plate (23; 23a, 23b) of the carriage fitting to the sliding sash, so that the connection is achieved in the region above the horizontal spar of the sliding sash (FR);
    - at least two installation points (24a, 24b; 25a, 25b), which are spaced apart (c) in the horizontal direction, are provided on the elongated plate (23); wherein the installation points are provided to enable screw connections to the sliding sash and pairs of installation points (24a, 24b; 25a, 25b) are provided to install the elongated plate (23) at points, which are horizontally and vertically spaced apart (c, d), on the sliding sash (FR);
    characterized in that the installation points are arranged on both sides of the bolt (22) and the bolt (22) is fixedly arranged in a center position on the elongated plate (23), for example, by welding points or another type of installation, wherein a section (23') of the elongated plate (23) engages into a vertical web (21b) to some extent, whereby the section (23') is provided as a piece which is which is tapered in thickness which is produced by embossing or squeezing the entire one-part or two-part front section of the plate (23), said plate engaging behind the web (21b).
  2. The carriage fitting according to Claim 1, wherein a region of the sash rebate (Ü) of the sliding sash can be engaged using the installation points.
  3. The carriage fitting according to Claim 1, wherein the installation points are located on the elongated plate (23) so that two vertically spaced-apart points (24b, 25b) in the edge region of the sliding sash (FR) are engaged or can be engaged.
  4. The carriage fitting according to Claim 1, wherein the plate (23) has at least two spaced-apart rows of installation openings (24a, 24b; 25a, 25b), of which one is connectable to a metallic counterpart (30) so that an edge-side region (Ü) of the sash can be clamped between the counterpart and the plate (23, 30) to reinforce it vertically in the corner or end region (E).
  5. The carriage fitting according to Claim 4, wherein the metallic counterpart (30) is arranged in the rebate (F).
  6. The carriage fitting according to Claim 1 or 5, wherein the installation points are located so that at least one, preferably two vertically spaced-apart (d) installation points are arranged in the profile space region of the vertical spar of the sliding sash (FR) to enable, in the case of a plastic profile as the vertical spar, a connection to its inner reinforcement (31) made of metal.
  7. The carriage fitting according to Claim 1, wherein openings, boreholes, or breakthroughs are provided as the installation points in the elongated plate (23) for receiving screws or bolts for the friction-locked, fixed but detachable connection to the sash.
  8. The carriage fitting according to Claim 1, wherein the elongated plate (23) is designed so that it has multiple strips (23a, 23b), which extend in the vertical direction, to form a surface contour which reinforces the plate (23).
  9. The carriage fitting according to Claim 8, wherein two spaced-apart raised strips (23a) are provided and each of these strips receives at least one of at least two installation points (24a, 24b), which are spaced apart (c) in the horizontal direction.
  10. The carriage fitting according to Claim 8 or 9, wherein the plate (23) has an embossed strip (23b), which is arranged in particular essentially in the middle between at least two raised strips (23a), for receiving the bolt (22).
  11. The carriage fitting according to Claim 1 or 8, wherein the bolt (22) is arranged as a coupling part so that - in the vertical installed state - it is placed between two vertically extending, raised strips (23a) or in a vertically extending, depressed embossed strip (23b) and is fixedly connected to the elongated plate (23), in particular is welded onto spaced-apart welding points (26).
  12. The carriage fitting according to Claim 1, wherein the bolt (22) is inserted into the support surface (21, 21a) on or in the carriage (20).
  13. The carriage fitting for the sliding sash according to Claim 1, having tilt capability, in particular having wooden spars or plastic profiles as the frame profiles, which sliding sash (FR) has horizontal and vertical spars and is installable via at least one thereof on at least one carriage (10, 20), which is movable in parallel to a fixed frame (BR), which carriage is fixedly connectable to the sliding sash in a corner region (E) of the sliding sash (FR), wherein the plate (23) is designed so that it has at least one embossing strip (23b) formed in its longitudinal direction, for reinforcing the plate and for receiving the bolt as the installation bolt (22).
  14. The carriage fitting according to any one of the preceding claims, characterized in that the bolt (22) is integrally formed with the plate (23).
  15. The carriage fitting according to any one of Claims 1 to 13, characterized in that the bolt (22) is fixedly arranged on the plate (23) by welding points (26).
EP01105614.0A 2000-03-11 2001-03-06 Corner reinforcements or struts for sliding wings Expired - Lifetime EP1132562B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP10184738.2A EP2267258B1 (en) 2000-03-11 2001-03-06 Arrangement with a sliding door and a fitting

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE10011353 2000-03-11
DE10011353 2000-03-11
DE10101544 2001-01-15
DE10101544 2001-01-15

Related Child Applications (2)

Application Number Title Priority Date Filing Date
EP10184738.2A Division-Into EP2267258B1 (en) 2000-03-11 2001-03-06 Arrangement with a sliding door and a fitting
EP10184738.2A Division EP2267258B1 (en) 2000-03-11 2001-03-06 Arrangement with a sliding door and a fitting

Publications (4)

Publication Number Publication Date
EP1132562A2 EP1132562A2 (en) 2001-09-12
EP1132562A3 EP1132562A3 (en) 2003-08-06
EP1132562B1 EP1132562B1 (en) 2016-06-29
EP1132562B2 true EP1132562B2 (en) 2019-09-04

Family

ID=26004747

Family Applications (2)

Application Number Title Priority Date Filing Date
EP01105614.0A Expired - Lifetime EP1132562B2 (en) 2000-03-11 2001-03-06 Corner reinforcements or struts for sliding wings
EP10184738.2A Expired - Lifetime EP2267258B1 (en) 2000-03-11 2001-03-06 Arrangement with a sliding door and a fitting

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP10184738.2A Expired - Lifetime EP2267258B1 (en) 2000-03-11 2001-03-06 Arrangement with a sliding door and a fitting

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EP (2) EP1132562B2 (en)
DE (1) DE10110722B4 (en)
ES (2) ES2594152T3 (en)
PT (1) PT2267258T (en)

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PT2267258T (en) * 2000-03-11 2017-08-10 Hautau Gmbh Arrangement with a sliding door and a fitting
WO2010079461A2 (en) 2009-01-11 2010-07-15 Hautau Gmbh Compact carriage for a longitudinally movable, heavy door leaf
CN101597994B (en) * 2009-07-09 2012-07-25 三一重工股份有限公司 Diplane integrated guide rail type slip door and vehicle with slip door
PL2663710T3 (en) 2011-01-14 2015-05-29 Hautau Gmbh Adjustable vertical reinforcement element for a sliding sash that is movable from one plane to a plane parallel to the frame
DE102013226716B4 (en) 2013-12-19 2016-02-18 Roto Frank Ag Adjustable vertical stiffener with eccentric for a removable wing of a window, a door or the like
DE102013226720B4 (en) 2013-12-19 2016-03-03 Roto Frank Ag Adjustable vertical stiffener with slider for a removable wing of a window of a door or the like
DE102014209915B3 (en) * 2014-05-23 2015-07-02 Roto Frank Ag Adjustable vertical stiffener with backdrop for a removable wing of a window or door
FR3113082B1 (en) * 2020-07-30 2022-11-25 M C France Joinery of the window or door type with an opening frame fitted with at least one reinforcing bracket

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Also Published As

Publication number Publication date
EP1132562B1 (en) 2016-06-29
EP2267258A3 (en) 2014-04-30
DE10110722B4 (en) 2015-09-24
DE10110722A1 (en) 2002-01-24
EP2267258A2 (en) 2010-12-29
EP1132562A3 (en) 2003-08-06
EP2267258B1 (en) 2017-05-10
ES2594152T3 (en) 2016-12-16
ES2636913T3 (en) 2017-10-10
EP1132562A2 (en) 2001-09-12
PT2267258T (en) 2017-08-10

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