EP2267258B1 - Arrangement with a sliding door and a fitting - Google Patents
Arrangement with a sliding door and a fitting Download PDFInfo
- Publication number
- EP2267258B1 EP2267258B1 EP10184738.2A EP10184738A EP2267258B1 EP 2267258 B1 EP2267258 B1 EP 2267258B1 EP 10184738 A EP10184738 A EP 10184738A EP 2267258 B1 EP2267258 B1 EP 2267258B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- wing
- carriage
- connector
- unit according
- reinforcing bracket
- 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
Links
- 230000003014 reinforcing effect Effects 0.000 claims description 19
- 229910052751 metal Inorganic materials 0.000 claims description 12
- 239000002184 metal Substances 0.000 claims description 12
- 230000002787 reinforcement Effects 0.000 description 13
- 230000005540 biological transmission Effects 0.000 description 6
- 238000004049 embossing Methods 0.000 description 6
- 238000004826 seaming Methods 0.000 description 4
- 230000007704 transition Effects 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000003351 stiffener Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D15/00—Suspension arrangements for wings
- E05D15/06—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 unit with a sliding leaf and a fitting for the sliding leaf according to the preamble of claim 1.
- weights of the sliding sash creates a torsion on the lower horizontal wing spar in the wing.
- the distortion also has an effect on the non-reinforced flashovers (not reinforced with metal inserts), in particular of the vertical uprights of the sliding leaf, so that deformation takes place inwards, ie in the direction of the fixed frame (frame).
- 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 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 EP 312 738 B1 discloses a unit according to the preamble of claim 1 with a fitting for a deployable wing of a window or a door, in which a block-shaped stiffening member is provided on which a threaded bolt on the outside of a mounting plate is fixed.
- the mounting plate is supported on a Ausstellarm of the fitting part.
- the object of the invention is therefore to propose reinforcing variants with which an increased sash weight of a sliding sash can be accommodated, and with which this wing, especially in the corner, can be stiffened, especially without the (additional) reinforcement visible directly from the outside. It is intended to be able to accommodate a larger sash weight without disturbing the optics, providing less torsion of the horizontal or vertical frame members.
- the assembly time should be shortened or simplified.
- a reinforcing insert screwed into the inner surface of the rollover inside the rebate air area serves for sufficient stiffening and transmission of forces, wherein the reinforcing part is designed as an angle and runs around the corner of the wing.
- the stiffening angle in the corner area can thereby be configured in itself as a profile (variable in cross-section), whereby different profile geometries are preferably provided along both legs (the horizontal and the vertical leg) in the assembled state (claim 4), e.g. depending on whether in a section a screw connection with the wing should come about, or whether a screw connection with the drive (by the wing flap) should come about.
- the profiling lowers the weight (claim 3).
- a connector (usually arranged as a screw and a screw device) is able to tension the one leg in the direction of the receiving or support surface of the drive in order to transmit the weight forces of the wing in the corner region on the carriage.
- the stiffening angle can have two substantially vertically oriented limbs (claim 2), which can be mounted in each case on the sliding leaf at its insides facing the rebate space. They are thus next to a fitting groove in the wing. They are located closer to the rollover and lie in the corner of the wing and in the inner corner between the horizontal inside and the vertical inside, both of which point to the rebate and one of which is the front of the wing and the other is formed by the rollover.
- a chamfer can be provided continuously along the angle.
- the bevel is provided as a chamfer at least on the inner edge of the angle, which rests in the inner corner.
- connection point is provided, for mounting on the sliding leaf in the rebate air (the rebate space), cf. Claim 8.
- All the proposed reinforcement variants make it possible, in particular in the case of plastic profiles, for the mounting plate extending in the vertical direction to rest flush on the interior surface of the wing and, despite the high sash weights, not to show a lifting tendency.
- the panel is connected to the wing via at least two horizontally spaced mounting locations. There may also be more than two mounting locations, and also vertically spaced mounting locations may be added such that three, four or more mounting locations form a mounting assembly that permits planar engagement of the panel with the surface of the wing for receiving and transmitting high forces the drive.
- 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.
- a substantial part of the weight is taken up on the one hand by the vertical leg and the other by the horizontal leg, which in turn transmits it to the vertical leg, where the main connector is provided for transmitting a substantial part of the weight of the wing on the carriage (claim 12).
- the main connector In the assembled state, the main connector is in the height of the horizontal spar (claim 10,11). Nevertheless, he intervenes in the vertical leg of the stiffening angle. In this way, more horizontal rows of connectors can be saved, as they still at EP 312 738 B1 (GU) are provided. Also, the mounting on a faceplate (the rail that covers a profile groove) is not required, so that the scope of the corner bracket can be extended to those wings that have no cuff rails. In particular, metal profiles are addressed in which the leadership of the drive rods in the profile groove for controlling the wing is made in other ways. The weight of the wing is made in the corner, however, without further connectors (with the exception of the main connector) (claim 12). It is located in the height area of the recording or support surface of the drive.
- a number of identically shaped connecting screws can be provided, which engage the drive in the wing.
- a series of connecting bolts are provided which extend from the receiving or supporting surface of the drive and are substantially at the same height as the main connector.
- the fitting can also be used with narrow profile systems.
- the entire support profile of the carriage can be covered with a cover so that no additional stiffeners are visible from the outside, in particular not that, the force in the corner transmitting stiffening angle in the rebate.
- the invention does not require a transfer of weight forces directly from the horizontal leg in the drive, but the recorded weight on the horizontal leg weight is redirected to the vertical leg and from there, so indirectly, transferred to the carriage.
- the intended for the transmission of the weight of the corner main connector is - relative to the length of the legs of the stiffening angle - the corner arranged obvious, while the other mounting points (consisting of a mounting hole and a mounting screw) in the vertical and horizontal legs of the stiffening angle clearly from the Outward corner are preferably provided outside substantially the middle of the leg length.
- the arrangement with a row of screws can also be used for a Eckversteifung, in which the bolt from the pin plate, starting in the support profile in the corner intervenes.
- the other screws of the helix, as a continuation of the main connector no longer engage in the corner angle, but only in the possibly stiffened by metal side rail profile.
- the 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 deformation (torsion) of the sliding sash.
- the corners absorb the entire load without additional reinforcing parts on metal profiles.
- Inside an angle is screwed in the rebate and connected to the vertical and the horizontal spar of the sash, in particular screwed.
- the corner bracket is connected to the drive via a vertical connecting surface via a mounting location with a connecting screw as a "connector".
- 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 height of this mounting point (s) is not laid in the vertical rail, but only as high as the height of the horizontal rail runs, so that an installation without any visible screw from the inside of the room is possible.
- 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, in which the said bolt 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 take 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 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 21 a of the horizontal surface 21 and is of the drive frame, which is formed from the two surfaces 21 and a vertically extending surface 21 'added.
- 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. One wing lies on the left side and one on the right side of the bolt 22.
- the enlarged section AV shows the lower portion of the bolt at the engagement in the opening 21 a and above the engagement of the two flanges 23 'in the vertical portion of the receiving and Support surface 21, which is designated 21 b.
- the procedure takes place only a little bit, especially 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 21b.
- 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. 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. If two horizontally spaced mounting locations are provided, an additional vertically spaced mounting location may also exist only as a single mounting location, just as several pairs of mounting locations are possible, along rows a, b.
- 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 optical change high sash weights and can be transmitted to the fixed frame BR via the carriage 20 without substantial torsion of the entire sliding wing.
- the described multiple mounting locations 24,25 are in FIG. 3 recognizable as a surface mounting.
- the transfer of these forces is also ensured 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.
- 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 (21 b, 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.
- These 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.
- Each edge unembossed strip portions remain with which the plate 23 rests flat on the wing, fed to transfer the forces of the plurality of horizontally and vertically spaced Mounting points 24 and 24, respectively.
- Three pairs of welding points 26 hold the bolt 22 firmly to the bolt plate 23.
- 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 21 b 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, a design according to the invention offers 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.
- 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 fit well into the inner corner of the fold pointing inside surfaces.
- 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 laid 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 catch) 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)
- Sewing Machines And Sewing (AREA)
- Wing Frames And Configurations (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Description
Die Erfindung befasst sich mit einer Einheit mit einem Schiebeflügel und einem Beschlag für den Schiebeflügel nach dem Oberbegriff des Anspruches 1.
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, d.h. 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 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.The invention relates to a unit with a sliding leaf and a fitting for the sliding leaf according to the preamble of
For large sash weights of the sliding sash creates a torsion on the lower horizontal wing spar in the wing. The distortion also has an effect on the non-reinforced flashovers (not reinforced with metal inserts), in particular of the vertical uprights of the sliding leaf, so that deformation takes place inwards, ie in the direction of the fixed frame (frame). 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 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.
Die
Aufgabe der Erfindung ist es deshalb, Verstärkungsvarianten vorzuschlagen, mit denen ein erhöhtes Flügelgewicht eines Schiebeflügels aufgenommen werden kann, und mit welchen dieser Flügel, insbesondere im Eckbereich, versteift werden kann, besonders ohne die (zusätzliche) Verstärkung unmittelbar von außen sichtbar zu machen. Es soll ohne die Optik zu stören ein größeres Flügelgewicht aufgenommen werden können, bei Bereitstellung einer geringeren Torsion der horizontalen oder vertikalen Rahmenteile. 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 therefore to propose reinforcing variants with which an increased sash weight of a sliding sash can be accommodated, and with which this wing, especially in the corner, can be stiffened, especially without the (additional) reinforcement visible directly from the outside. It is intended to be able to accommodate a larger sash weight without disturbing the optics, providing less torsion of the horizontal or vertical frame members. The assembly time should be shortened or simplified. These tasks can be individually solved as a technical problem.
Die Lösung findet sich im Anspruch 1.The solution can be found in
Bei Metallprofilen dient ein innen im Falzluftbereich an die Innenfläche des Überschlags angeschraubter Verstärkungseinsatz zur ausreichenden Versteifung und Übertragung von Kräften, wobei der Versteifungsteil als Winkel ausgebildet ist und um die Ecke des Flügels verläuft.In the case of metal profiles, a reinforcing insert screwed into the inner surface of the rollover inside the rebate air area serves for sufficient stiffening and transmission of forces, wherein the reinforcing part is designed as an angle and runs around the corner of the wing.
Er kann mit dem senkrechten Holm, dem horizontalen Holm und der Stützfläche des Laufwagens verbunden sein, um die Flügelecke zu versteifen und höhere Flügelgewichte möglich zu machen, ohne die Torsion des Flügels zu erhöhen.It can be connected to the vertical spar, the horizontal spar and the support surface of the carriage to stiffen the wing corner and make higher sash weights possible without increasing the torsion of the wing.
Der Versteifungswinkel im Eckbereich kann dabei in sich selbst als Profil (querschnittsveränderlich) ausgestaltet sein, wobei bevorzugt entlang beider Schenkel (der horizontale und der vertikale Schenkel) im montierten Zustand unterschiedliche Profilgeometrien vorgesehen sind (Anspruch 4), z.B. je nachdem, ob in einem Abschnitt eine Schraubverbindung mit dem Flügel zustande kommen soll, oder ob eine Schraubverbindung mit dem Laufwerk (durch den Flügelüberschlag) zustande kommen soll. Die Profilierung senkt das Gewicht (Anspruch 3).The stiffening angle in the corner area can thereby be configured in itself as a profile (variable in cross-section), whereby different profile geometries are preferably provided along both legs (the horizontal and the vertical leg) in the assembled state (claim 4), e.g. depending on whether in a section a screw connection with the wing should come about, or whether a screw connection with the drive (by the wing flap) should come about. The profiling lowers the weight (claim 3).
Die gesamte Last des Flügels im Eckbereich wird dabei über den im Falz angeordneten Tragwinkel mit einem in dem vertikalen Falzraum liegenden ersten Schenkel und einem in dem horizontalen Falzraum liegenden zweiten Schenkel übertragen, ohne dass zusätzliche Verstärkungsteile, die eingangs beschrieben worden sind, nötig sind. Damit ist der gesamte - von der Innenseite eines Raumes sichtbare - Eckbereich des Schiebeflügels frei von Versteifungsteilen oberhalb des Laufwagens, und es können dennoch hohe Flügelgewichte ohne Gefahr einer Torsion oder mit stark herabgesetzter Torsionsneigung realisiert werden.The entire load of the wing in the corner region is transmitted via the arranged in the fold support bracket with a lying in the vertical rebate first leg and lying in the horizontal rebate second leg, without additional reinforcing members, which have been described above, are necessary. Thus, the entire - visible from the inside of a room - corner of the sliding sash free of stiffening parts above the carriage, and it can still high sash weights without risk of torsion or with greatly reduced Torsionsneigung can be realized.
Ein Verbinder (zumeist als eine Schraube und eine Schraubeinrichtung angeordnet) ist in der Lage, den einen Schenkel in Richtung der Aufnahme- oder Stützfläche des Laufwerks zu spannen, um die Gewichtskräfte des Flügels im Eckbereich auf den Laufwagen zu übertragen. Der Versteifungswinkel kann zwei im Wesentlichen senkrecht orientierten Schenkel (Anspruch 2) haben, die jeweils am Schiebeflügel an dessen zum Falzraum weisenden Innenseiten montierbar ist. Sie liegen damit neben einer Beschlagsnut im Flügel. Sie sind näher am Überschlag angeordnet und liegen im Eckbereich des Flügels und in der Innenecke zwischen der horizontalen Innenseite und der vertikalen Innenseite, die beide zum Falzraum zeigen und von denen einer die Stirnseite des Flügels und der andere vom Überschlag gebildet wird.A connector (usually arranged as a screw and a screw device) is able to tension the one leg in the direction of the receiving or support surface of the drive in order to transmit the weight forces of the wing in the corner region on the carriage. The stiffening angle can have two substantially vertically oriented limbs (claim 2), which can be mounted in each case on the sliding leaf at its insides facing the rebate space. They are thus next to a fitting groove in the wing. They are located closer to the rollover and lie in the corner of the wing and in the inner corner between the horizontal inside and the vertical inside, both of which point to the rebate and one of which is the front of the wing and the other is formed by the rollover.
Um sich hier besser einzupassen, kann eine Abschrägung durchgängig entlang des Winkels vorgesehen sein. Die Abschrägung wird als Fase zumindest an der Innenkante des Winkels vorgesehen, die in dem Inneneck anliegt.In order to fit better here, a chamfer can be provided continuously along the angle. The bevel is provided as a chamfer at least on the inner edge of the angle, which rests in the inner corner.
Im vertikalen und im horizontalen Schenkel ist eine Verbindungsstelle vorgesehen, zur Montage am Schiebeflügel in der Falzluft (dem Falzraum), vgl. Anspruch 8.In the vertical and in the horizontal leg, a connection point is provided, for mounting on the sliding leaf in the rebate air (the rebate space), cf. Claim 8.
Alle vorgeschlagenen Verstärkungsvarianten ermöglichen 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 zumindest zwei in Horizontalrichtung beabstandeten Montagestellen mit dem Flügel verbunden. Es können auch mehr als zwei Montagestellen vorhanden sein, und ebenfalls können vertikal beabstandete Montagestellen hinzutreten, so dass drei, vier oder mehr Montagestellen einen Montageverbund bilden, der eine flächige Anlage der Platte an der Oberfläche des Flügels ermöglicht, zur Aufnahme und Übertragung hoher Kräfte auf das Laufwerk.All the proposed reinforcement variants make it possible, in particular in the case of plastic profiles, for the mounting plate extending in the vertical direction to rest flush on the interior surface of the wing and, despite the high sash weights, not to show a lifting tendency. The panel is connected to the wing via at least two horizontally spaced mounting locations. There may also be more than two mounting locations, and also vertically spaced mounting locations may be added such that three, four or more mounting locations form a mounting assembly that permits planar engagement of the panel with the surface of the wing for receiving and transmitting high forces the drive.
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.
Senkrecht zu zwei Verbindern zwischen Versteifungswinkel und Flügelrahmen ist nur ein weiterer Verbinder vorgesehen (Anspruch 8), der die Gewichtskraft im Eckbereich von dem vertikalen Schenkel des Versteifungswinkels in das Laufwerk überträgt, das an horizontal beweglichen Rollen den Flügelrahmen auf einer Laufschiene bewegt. Diese Hauptverbindung bestehend aus Schraubverbindung und Gewindebohrung ist alleinig in der Lage, das Gewicht der Ecke zu übertragen. Weitere Schraubverbindungen dieser Art sind im Winkel deshalb nicht erforderlich (Anspruch 6,10).Perpendicular to two connectors between stiffening angle and sash, only another connector is provided (claim 8), which transfers the weight force in the corner of the vertical leg of the stiffening angle in the drive, which moves on horizontally movable rollers the sash on a running rail. This main connection consisting of screw and tapped hole is only able to transfer the weight of the corner. Further screw connections of this type are therefore not required in angle (claim 6,10).
Ein wesentlicher Teil der Gewichtskraft wird zum einen vom vertikalen Schenkel und zum anderen vom horizontalen Schenkel aufgenommen, der sie aber wiederum auf den vertikalen Schenkel überträgt, wo der Hauptverbinder zur Übertragung eines wesentlichen Teils der Gewichtskraft des Flügels auf dem Laufwagen vorgesehen ist (Anspruch 12).A substantial part of the weight is taken up on the one hand by the vertical leg and the other by the horizontal leg, which in turn transmits it to the vertical leg, where the main connector is provided for transmitting a substantial part of the weight of the wing on the carriage (claim 12). ,
Die Verwendung weniger solcher Verbinder erhöht die Effektivität der Montage und reduziert Montagekosten, ebenso wie Montagezeiten.The use of fewer such connectors increases the effectiveness of the assembly and reduces assembly costs, as well as assembly times.
Im montierten Zustand liegt der Hauptverbinder in der Höhe des horizontalen Holms (Anspruch 10,11). Dennoch greift er in den vertikalen Schenkel des Versteifungswinkels ein. Auf diese Weise können weitere horizontale Reihen von Verbindern eingespart werden, wie sie noch bei
Als Fortsetzung des einen Hauptverbinders kann eine Reihe von gleich ausgebildeten Verbindungsschrauben vorgesehen sein, die vom Laufwerk in den Flügel eingreifen. Hier ist nur eine Reihe von Verbindungsschrauben vorgesehen, die von der Aufnahme- oder Stützfläche des Laufwerkes ausgehen und im Wesentlichen auf derselben Höhe liegen, wie der Hauptverbinder. Entlang dieser langgestreckten Linie besteht eine zusätzliche Verbindungsmöglichkeit, die aber den Eckbereich und die Kraftübertragung im Eckbereich nicht zu entlasten vermag. Aufgrund der Ausführung mit nur einer Schraubenlinie (aufgereihte Schrauben entlang einer horizontal verlaufenden Linie) ist der Beschlag auch bei schmalen Profilsystemen einsetzbar. Das gesamte Tragprofil des Laufwagens kann mit einer Abdeckung abgedeckt werden, so dass von außen keine zusätzlichen Versteifungen erkennbar sind, insbesondere nicht derjenige, die Kraft in der Ecke übertragende Versteifungswinkel im Falzraum.As a continuation of the one main connector, a number of identically shaped connecting screws can be provided, which engage the drive in the wing. Here, only a series of connecting bolts are provided which extend from the receiving or supporting surface of the drive and are substantially at the same height as the main connector. Along this elongated line there is an additional possibility of connection, but which is not able to relieve the corner area and the power transmission in the corner area. Due to the design with only one helix (stringed screws along a horizontal line), the fitting can also be used with narrow profile systems. The entire support profile of the carriage can be covered with a cover so that no additional stiffeners are visible from the outside, in particular not that, the force in the corner transmitting stiffening angle in the rebate.
Die Erfindung kommt ohne eine Übertragung von Gewichtskräften direkt aus dem horizontalen Schenkel in das Laufwerk aus, vielmehr wird die am horizontalen Schenkel aufgenommene Gewichtskraft in den vertikalen Schenkel umgeleitet und von dort, also mittelbar, in den Laufwagen übertragen. Der für die Übertragung der Gewichtskraft der Ecke vorgesehen Hauptverbinder ist dabei - bezogen auf die Länge der Schenkel des Versteifungswinkels - dessen Eckbereich naheliegend angeordnet, während die anderen Montagestellen (bestehend aus einer Montageöffnung und einer Montageschraube) im vertikalen und horizontalen Schenkel des Versteifungswinkels deutlich aus der Ecke herausverlagert sind, bevorzugt außerhalb im Wesentlichen der Mitte der Schenkellänge vorgesehen sind.The invention does not require a transfer of weight forces directly from the horizontal leg in the drive, but the recorded weight on the horizontal leg weight is redirected to the vertical leg and from there, so indirectly, transferred to the carriage. The intended for the transmission of the weight of the corner main connector is - relative to the length of the legs of the stiffening angle - the corner arranged obvious, while the other mounting points (consisting of a mounting hole and a mounting screw) in the vertical and horizontal legs of the stiffening angle clearly from the Outward corner are preferably provided outside substantially the middle of the leg length.
Die Anordnung mit einer Schraubenreihe ist auch für eine Eckversteifung einsetzbar, bei der der Bolzen von der Bolzenplatte ausgehend in das Tragprofil im Eckbereich eingreift. Die weiteren Schrauben der Schraubenlinie, als Fortsetzung des Hauptverbinders greifen nicht mehr in den Eckwinkel ein, sondern nur noch in das ggf. innenseitig durch Metall versteifte Holmenprofil.The arrangement with a row of screws can also be used for a Eckversteifung, in which the bolt from the pin plate, starting in the support profile in the corner intervenes. The other screws of the helix, as a continuation of the main connector no longer engage in the corner angle, but only in the possibly stiffened by metal side rail profile.
Das 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 einer Verformung (Torsion) des Schiebeflügels entgegen.The 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 deformation (torsion) of the sliding sash.
Die Ecken nehmen dabei die gesamte Last ohne zusätzliche Verstärkungsteile bei Metallprofilen auf. Innen ist im Falzbereich ein Winkel eingeschraubt und mit dem senkrechten und mit dem waagerechten Holm des Schiebeflügels verbunden, insbesondere verschraubt. Der Eckwinkel ist mit dem Laufwerk über eine vertikal verlaufende Verbindungsfläche über eine Montagestelle mit Verbindungsschraube als "Verbinder" verbunden. 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. Die Höhe dieser Montagestelle(n) ist nicht in den vertikalen Holm verlegt, sondern nur so hoch, wie die Höhe des horizontalen Holms verläuft, so dass eine Montage ohne jede sichtbare Schraubverbindung von der Rauminnenseite möglich ist.The corners absorb the entire load without additional reinforcing parts on metal profiles. Inside an angle is screwed in the rebate and connected to the vertical and the horizontal spar of the sash, in particular screwed. The corner bracket is connected to the drive via a vertical connecting surface via a mounting location with a connecting screw as a "connector". 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 height of this mounting point (s) is not laid in the vertical rail, but only as high as the height of the horizontal rail runs, so that an installation without any visible screw from the inside of the room is possible.
Die Erfindung wird anhand von Ausführungsbeispielen 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 vertikalenSchnitt 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
, wobei Details derFigur 1Platte 23 in einer Aufsicht und einer Schnittansicht gezeigt werden. - Figur 4
- ist eine erfindungsgemäße 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.
- 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 theplate 23 in a plan view and a sectional view. - FIG. 4
- is an inventive design of a metal frame provided for lower corner area, here the
carriage 10 ofFIG. 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 inFIG. 4 is screwed in the corner area in the seaming air F on the sash FR.
In
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
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 21 a 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
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
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 21 a und darüber das Eingreifen der beiden Flansche 23' in den vertikalen Abschnitt der Aufnahme- und Stützfläche 21, die mit 21 b 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
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 21b 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
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
Die Schnittdarstellung des Eckbereiches E in einer horizontalen Ebene ist in
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
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
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
Die beschriebenen mehreren Montagestellen 24,25 sind in
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 (21 b,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
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
In der Aufsicht (mit Teilausschnitt im Schnitt) ist in
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 21 b 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
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
Für Aluminiumprofile bietet sich eine erfindungsgemäße Gestaltung gemäß
Im Übergangsbereich zwischen dem Laufwerk und dem Schiebeflügel ist in
Es versteht sich, dass für einen regulären Schiebeflügel die linke und rechte Ecke in der Regel gleich abgestützt sind, also so wie
Die Eckbereiche nehmen in
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
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
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
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
Zwei der Schraubverbinder von
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.Even with this reinforcement variant, a sash 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.
Das Eckwinkelstück 50 ist in
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
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
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
Es kann eine weitere solche Bohrung auch in dem horizontalen Schenkel 50h vorgesehen sein.There may be another such hole also provided in the
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
Der Schnitt A-A des Winkels 50 besteht aus zwei voneinander weg weisenden U-förmigen Profilierungen zur Bildung eines H-Querschnitts, wobei der in
Trotz senkrecht zueinander orientierten Montagestellen 56,57 einerseits bzw. 60 andererseits kann jeweiliger Schenkel gemäß
Wie aus
Claims (15)
- A unit with a sliding wing and a fitting for the sliding wing with a tilting possibility, especially with plastic or metal spars as frame profiles of the sliding wing, wherein the sliding wing (FR) comprises horizontal and vertical spars and can be mounted via at least one thereof on at least one carriage (10, 20) which is movable parallel to a fixed frame (BR), wherein the fitting comprises the carriage, which carriage is formed to be tightly connected to the sliding wing (FR) in a corner region thereof, and- the carriage (10) comprises a receiving or support surface (61) which extends in the mounted state substantially parallel to the plane of the sliding wing;- and with a connector (60) which engages through or in an opening of the surface (61);- and with a reinforcing bracket (50; 50h, 50v) whose one limb (50v) m can be tensioned with the connector (60) in the direction of the surface (61), such that the reinforcing bracket (50) comes to lie in the rabbet space (F) between the fixed frame (BR) and the sliding wing (FR), and extends around the corner (E) of the sliding wing (FR), characterized in that the reinforcing bracket (50) is attached to the wing adjacent to a fitting groove (55) of the wing between the fitting groove (55) and a cover (U) on the wing, wherein the cover defines a first of the inner surfaces facing the rabbet space, and that the face end of the casement defines the further inner surface extending substantially perpendicularly to the first inner surface, and the reinforcing bracket (50) is formed in such a way that it rests on both inner surfaces.
- A unit according to claim 1, wherein the reinforcing bracket (50) comprises two substantially vertically oriented limbs (50h, 50v), which are adjusted and formed to be respectively mountable on the sliding wing (FR) on its inner side or inner areas facing the rabbet clearance (F).
- A unit according to claim 1, wherein the reinforcing bracket (50) comprises recesses (80) which are profiled or elongated in the cross-section, for the purpose of reducing its weight.
- A unit according to claim 3, wherein at least two different cross-sectional or profile geometries or profile designs are provided (70, 70a, 70b; 69a, 69b) in each of the limbs.
- A unit according to claim 1, wherein the connector (60) is arranged in the region of the carriage (10) in such a way that the surface in the corner region of the sliding wing (FR) above the carriage (10) does not comprise any mounting points or surface breakthroughs that can be detected from the visible side, especially with a carriage that only extends horizontally without vertical mounting zones.
- A unit according to claim 1, wherein only one connector (60) is provided on the reinforcing bracket, for transmitting the weight in the corner region of the wing onto the carriage (20), especially the support surface (61) on the carriage.
- A unit according to claim 1 or 6, wherein the connector (60) engages in a vertical limb (50v) of the reinforcing bracket (50).
- A unit according to claim 2, wherein mounting points are formed in the two limbs (50v, 50h) as openings (56a, 57a), for the engaging through of two further connectors (56, 57) which extend substantially perpendicularly to the first connector (60), for mounting the reinforcing bracket (50) to the spars in the corner region (E).
- A unit according to claim 2, wherein other connectors for receiving and transmitting the weight of the wing (FR) are not required or provided on the reinforcing bracket (50), or the three connectors (60; 56, 57) for receiving and transmitting the weight of the wing frame (FR) on the carriage (10) in the corner region (E) are formed adequately.
- A unit according to claim 7, wherein the connector originates as the main connector (60) from the vertically oriented limb in the region above the corner (51) of the reinforcing bracket (50).
- A unit according to claim 1, wherein the connection between the reinforcing bracket (50) and the carriage occurs on the horizontal spar via the connector (60) which transmits the weight and which(a) is disposed at the height of the horizontal spar;(b) engages in the vertical limb (50v) of the bracket.
- A unit according to claim 11, wherein no further connectors (60) are provided for transmitting the weight above or beneath the (one) connector (60) in the height region of the receiving or support surface (61), especially only a number of retaining elements (19) are arranged along the support surface, of which (only) the one connector (60) engages in the reinforcing bracket.
- A unit according to claim 2, wherein the horizontal limb can be mounted on the inner side of the wing frame which is oriented horizontally and faces the rabbet space, for receiving the weight of the wing and for its introduction into the vertical limb, where it is transmitted via the connector (60) to the carriage (10).
- A unit according to claim 2 or 13, wherein no relevant proportions of the weight of the wing frame are transmitted by the horizontal limb (50h) to the carriage directly.
- A unit according to one of the preceding claims, wherein the connectors (60, 56, 57) are screw elements and/or a main connection occurs with a main connector (60) via a thread in the reinforcing bracket (50).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10011353 | 2000-03-11 | ||
DE10101544 | 2001-01-15 | ||
EP01105614.0A EP1132562B2 (en) | 2000-03-11 | 2001-03-06 | Corner reinforcements or struts for sliding wings |
Related Parent Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01105614.0A Division-Into EP1132562B2 (en) | 2000-03-11 | 2001-03-06 | Corner reinforcements or struts for sliding wings |
EP01105614.0A Division EP1132562B2 (en) | 2000-03-11 | 2001-03-06 | Corner reinforcements or struts for sliding wings |
EP01105614.0 Division | 2001-03-06 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2267258A2 EP2267258A2 (en) | 2010-12-29 |
EP2267258A3 EP2267258A3 (en) | 2014-04-30 |
EP2267258B1 true EP2267258B1 (en) | 2017-05-10 |
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 Before (1)
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 |
Country Status (4)
Country | Link |
---|---|
EP (2) | EP1132562B2 (en) |
DE (1) | DE10110722B4 (en) |
ES (2) | ES2636913T3 (en) |
PT (1) | PT2267258T (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1132562B2 (en) * | 2000-03-11 | 2019-09-04 | HAUTAU GmbH | Corner reinforcements or struts for sliding wings |
CN102348862B (en) | 2009-01-11 | 2015-03-11 | 豪塔马有限责任公司 | 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 |
CN103328749B (en) * | 2011-01-14 | 2016-04-20 | 豪塔马有限责任公司 | For slip fan page, the adjustable vertical reinforcing that can put down out |
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 |
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 |
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 |
Family Cites Families (28)
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---|---|---|---|---|
DE740745C (en) | 1940-05-19 | 1943-10-27 | Hautau Baubeschlag | Drive for sliding doors |
DE1584014B2 (en) | 1964-07-31 | 1973-05-30 | Fa August Winkhaus, 4404 Telgte | DETACHABLE PIVOT FITTING FOR Tilt & Turn Windows |
DE1559910A1 (en) | 1965-03-26 | 1969-10-30 | Jaeger Kg Frank | Fitting for liftable tilt and swivel wings of windows, doors or the like. |
DE1784748A1 (en) | 1968-09-14 | 1971-09-09 | Hettich F Kg | Rotary sliding fitting for retractable and pivoting door leaves |
FR2330836A1 (en) | 1975-11-07 | 1977-06-03 | Ferco Int Usine Ferrures | Flap window locking and seating assembly - has operating element allowing closing pressure of leaf against frame to be adjusted |
DE2625270C2 (en) | 1976-06-04 | 1982-11-11 | Josef Gartner & Co, 8883 Gundelfingen | Door leaf for a fire-retardant folding door |
DE8135509U1 (en) | 1981-12-05 | 1982-03-25 | Huwil-Werke GmbH Möbelschloß- und Beschlagfabriken, 5207 Ruppichteroth | FITTING FOR SLIDING DOORS OD. THE LIKE, IN PARTICULAR FOR FURNITURE SLIDING DOORS |
FR2527256A2 (en) | 1982-03-01 | 1983-11-25 | Heuliez Dea | DISCOVERABLE SURFACE OPENING DEVICE, IN PARTICULAR SUNROOF FOR MOTOR VEHICLE |
DE8228393U1 (en) | 1982-10-09 | 1983-01-20 | Paul Hettich & Co, 4983 Kirchlengern | BEARING RACK FOR THE ROLE OF A SLIDING DOOR HANGING IN A RAIL |
DE8308201U1 (en) | 1983-03-19 | 1983-07-21 | Gretsch-Unitas GmbH Baubeschläge, 7257 Ditzingen | AT LEAST AT THE LOWER END EXTENDABLE WING OF A WINDOW, DOOR OR. DGL. |
DE3317264A1 (en) | 1983-03-29 | 1984-10-04 | Fa. Aug. Winkhaus, 4404 Telgte | WINDOW OR DOOR FOR OPTIONAL RIGHT OR LEFT STOP |
DE3639998A1 (en) | 1986-11-22 | 1988-06-01 | Siegenia Frank Kg | Fitting for a parallel-sidetrackable horizontal sliding wing of windows, doors or the like |
DE3711170C1 (en) | 1987-04-02 | 1988-06-30 | Siegenia Frank Kg | Display device for the wing of a window, a door or the like. |
DE8709299U1 (en) * | 1987-07-06 | 1987-08-27 | W. Hautau GmbH, 3068 Helpsen | Reinforcing part for the housing-like supporting part of the lower fitting of a .... which supports the pivot pin of a projection arm. |
DE8714151U1 (en) * | 1987-10-23 | 1987-12-03 | Gretsch-Unitas GmbH Baubeschläge, 7257 Ditzingen | Fitting for a sash of a window, door or similar that can be opened at least downwards and window or door with this fitting |
GB8802496D0 (en) | 1988-02-04 | 1988-03-02 | Hardware & Systems Patents Ltd | Safety catch for tilt/turn window systems |
ES2023743A6 (en) | 1990-03-01 | 1992-02-01 | Klein Iberica | Mechanism for the hanging of sliding doors. |
DE4134828C2 (en) | 1991-10-22 | 2001-11-15 | Lautenschlaeger Mepla Werke | Mounting plate for furniture hinges |
DE9308669U1 (en) | 1993-06-10 | 1994-10-27 | Gretsch-Unitas GmbH Baubeschläge, 71254 Ditzingen | Fitting part for the at least rotatable mounting of a wing, a window, a door or the like. |
DE9308668U1 (en) | 1993-06-10 | 1994-10-27 | Gretsch-Unitas GmbH Baubeschläge, 71254 Ditzingen | Bearing part of a bearing for the at least rotatable mounting of a wing, a window, a door or the like. |
DE9308673U1 (en) | 1993-06-10 | 1994-10-27 | Gretsch-Unitas GmbH Baubeschläge, 71254 Ditzingen | Corner bracket for a tilt and turn sash of a window, a door or the like. |
DE9402162U1 (en) | 1994-02-09 | 1995-06-08 | Gretsch-Unitas GmbH Baubeschläge, 71254 Ditzingen | Additional locking device for a window, a door or the like. |
DE4433635C2 (en) | 1994-09-21 | 1996-08-08 | Schroeders Theo | Track for a sliding door |
DE19526550A1 (en) | 1994-09-21 | 1996-03-28 | Riexinger Tuerenwerke Gmbh | Sliding door with rail and carriages |
GB2321661B (en) | 1997-01-30 | 1998-11-11 | Stanley Works | Sliding Door Assembly |
DE29819076U1 (en) | 1997-10-17 | 1999-02-25 | Lunke & Sohn AG, 58455 Witten | Sliding door for vehicles |
DE29819083U1 (en) | 1997-10-17 | 1999-02-18 | Lunke & Sohn AG, 58455 Witten | Sliding door fitting with trolley |
EP1132562B2 (en) * | 2000-03-11 | 2019-09-04 | HAUTAU GmbH | Corner reinforcements or struts for sliding wings |
-
2001
- 2001-03-06 EP EP01105614.0A patent/EP1132562B2/en not_active Expired - Lifetime
- 2001-03-06 PT PT101847382T patent/PT2267258T/en unknown
- 2001-03-06 ES ES10184738.2T patent/ES2636913T3/en not_active Expired - Lifetime
- 2001-03-06 DE DE10110722.6A patent/DE10110722B4/en not_active Expired - Fee Related
- 2001-03-06 ES ES01105614.0T patent/ES2594152T3/en not_active Expired - Lifetime
- 2001-03-06 EP EP10184738.2A patent/EP2267258B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1132562B1 (en) | 2016-06-29 |
EP1132562A3 (en) | 2003-08-06 |
PT2267258T (en) | 2017-08-10 |
ES2636913T3 (en) | 2017-10-10 |
DE10110722B4 (en) | 2015-09-24 |
DE10110722A1 (en) | 2002-01-24 |
EP2267258A3 (en) | 2014-04-30 |
EP2267258A2 (en) | 2010-12-29 |
EP1132562B2 (en) | 2019-09-04 |
EP1132562A2 (en) | 2001-09-12 |
ES2594152T3 (en) | 2016-12-16 |
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