EP2663710B1 - Élément de renforcement vertical réglable pour un vantail coulissant - Google Patents

Élément de renforcement vertical réglable pour un vantail coulissant Download PDF

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Publication number
EP2663710B1
EP2663710B1 EP12703156.5A EP12703156A EP2663710B1 EP 2663710 B1 EP2663710 B1 EP 2663710B1 EP 12703156 A EP12703156 A EP 12703156A EP 2663710 B1 EP2663710 B1 EP 2663710B1
Authority
EP
European Patent Office
Prior art keywords
bolt
vertical
support profile
sash
spar
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.)
Active
Application number
EP12703156.5A
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German (de)
English (en)
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EP2663710A1 (fr
Inventor
Dirk Muegge
Stefan Kording
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hautau GmbH
Original Assignee
Hautau GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
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Application filed by Hautau GmbH filed Critical Hautau GmbH
Priority to PL12703156T priority Critical patent/PL2663710T3/pl
Publication of EP2663710A1 publication Critical patent/EP2663710A1/fr
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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
    • 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
    • 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
    • E05Y2201/696—Screw mechanisms
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2600/00—Mounting or coupling arrangements for elements provided for in this subclass
    • E05Y2600/10—Adjustable
    • E05Y2600/20—Adjustable with specific transmission movement
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2600/00—Mounting or coupling arrangements for elements provided for in this subclass
    • E05Y2600/10—Adjustable
    • E05Y2600/30—Adjustment motion
    • E05Y2600/31—Linear motion
    • E05Y2600/312—Horizontal motion
    • 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
    • E05Y2800/00—Details, accessories and auxiliary operations not otherwise provided for
    • E05Y2800/15—Applicability
    • E05Y2800/17—Universally applicable
    • E05Y2800/176—Universally applicable on different wing types, weights or sizes
    • 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
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Type of wing
    • E05Y2900/148—Windows

Definitions

  • the invention relates to a vertical stiffening for the wing of a sliding door or a sliding window (as a method and as a device).
  • a vertical reinforcement requires a corner reinforcement in the drive area of the wing, which counteracts the torsion of the lower wing spar.
  • the torsion which significantly increases the effort required to close the sash, is thereby counteracted.
  • Corner reinforcements of this type are already known, for example EP-A 1 132 562 (HAUTAU) and EP-A 1 391 576 (HAUTAU). These known stiffeners have a fixed, consistent relationship to the wing when assembled. This means that the resulting torsion in various wing materials, such as plastic, wood and metal, or different sash weights, z. B. due to the weight of the disc, not even and comparable can be collected.
  • the DE 20 2008 007 829 discloses a fitting for a sliding wing, in which a display device comprises a bearing and guide plate as a stationary base, on which a control for stopping and moving the wing is provided, which is coupled to an actuating and locking linkage.
  • the object of the invention is to provide a vertical stiffening, which is adjustable so that it can be used on various spars with adaptive effect, regardless of how the spars of the sash constructed and what material they are made.
  • the adjusting means (as adjusting device) at the upper end of the vertical stiffener (its bolt) acts on this upper end and causes, thanks to a distance from the vertical wing spar, a change in the angle between the pin of Vertical stiffening and the vertical wing spar. If, for example, the angle is set to a negative value, the lower horizontal wing spar, together with the carriages assigned to it, rises.
  • the parallel position is only relative to the wing. It can vary in a small angular range (claim 11) when the insertion region (the insertion opening) is inclined for the bolt, with respect to the plane of the contact surface of the support profile for the horizontal wing spar. This can be done in a range of + - 5 °, preferably + -2 °. The "parallel position" should also rewrite this.
  • An alternative way of describing the change in pressure at the upper end of the vertical stiffener is to change the distance of the upper end of the bolt from the surface of the vertical wing spar so as to provide a path controlled torque build-up in the insertion area on the support profile which compensates.
  • This compensation can also be called “distance-controlled bagging compensation", based on the extension arm of the carriage.
  • the term of the bolt which may have different cross-sectional shapes (claim 3), is to be understood functionally. He is elongated and stuck in the bottom of the support profile. He brings a torque in the profile. Also an elongated, thick Plate fulfills this task. More generally, “the bolt” means an elongated torque lever that is clamped down and up (in its angular position or distance from the vertical beam). At the clamping point he exerts its torque (claim 8), which can achieve the compensation of the "sagging" of the wing, and this adjustable.
  • connection of the bolt with the support profile, at one or both corners is at least form-fitting according to claim 1.
  • the connection can also be created cohesively or non-positively, which means that it is also form-fitting for a cohesive connection.
  • An integral connection so the immediate attachment of the bolt on the support section (as a component) is to be understood as "at least form-fitting". This is not exclusive, but a consecutive kind of connection.
  • a one-piece is also achieved by welding or gluing.
  • a riveting process may not produce a one-piece, but is non-positive. All these types of connection are possible, but the insertion into a vertical or slightly inclined insertion in the support section allows the subsequent removal of the bolt. For the stiffening such removal is not mandatory, but also meets the one-piece component in the corner of its task of variable vertical stiffening.
  • the insertion may be able to apply a higher torque on a larger height portion of the support profile. It is also conceivable, however, an initially positive connection by plugging with a subsequent additional connection process, for example, welding. This combines the stability and resilience of the compound. Instead of welding, gluing in combination with play-free insertion can fulfill both functions.
  • FIG. 1 the sliding leaf 1 is shown in its lower area, where its horizontal spar 1a is connected to the two vertical bars 1b.
  • a running rail 3 with track 3a is fixedly mounted, on which the carriages 4 sit, which via Ausstellarme 5 with the sliding wing via one on the horizontal spar 1a of the casement fixed (non-displaceable) arranged supporting profile 6 pivotally connected (pivot axis 50) are.
  • Ausstellarme 5 with the sliding wing via one on the horizontal spar 1a of the casement fixed (non-displaceable) arranged supporting profile 6 pivotally connected (pivot axis 50) are.
  • 7 and 8 are tools for vertical bracing and their adjustment in FIG. 1 indicated.
  • FIGS. 2 to 4 show the adjustable stiffener in the vertical section, with the window frame 2 turned off wing 1, each in the same representation, but with different angles ⁇ of the bolt 7 relative to the vertical beam 1b. This corresponds to different torques in the insertion region 6a of each support profile.
  • FIG. 2 is the carriage 4 with swung-out arm 5 and its connection to the wing shown on the support section 6.
  • the lower portion 7b of the elongated torque lever 7, which can be used for stiffening, can be inserted without clearance into an insertion opening 6a.
  • This lever is a longer, stronger bolt 7 with a circular or polygonal cross-section.
  • Each of the two support profiles 6 has, on the side facing the lower spar 1a, a plate-shaped web 6 engaging under the lower spar and a profile which fixes the lever 7 in a predetermined distance "e" parallel to the contact surface E of the carrying profile.
  • the parallel situation of FIG. 2 refers to the insertion region 6a, in which the bolt 7 is inserted.
  • the insertion region has a constant distance e when it runs parallel to the surface E of the support profile 6.
  • the insertion region 6a also slightly inclined relative to the surface E extend, for example. In an angular range of -5 ° to + 5 °, preferably ⁇ 2 °, which refers to the orientation and axis of the insertion region 6a, based on the contact surface E. of the supporting profile. e does not change according to the angle ⁇ .
  • the axis of the insertion portion 6 a is a portion of the axis 700 of the bolt 7.
  • the bolt 7 has a (flattened) web-shaped portion 7a, substantially parallel to the outer surface of the spar.
  • a hole 7c or the like for the passage of an actuator, such as an engaging in the wing spar 1b screw 8, is provided.
  • the head 8 'of the screw 8 abuts against the outer surface of the web-shaped portion 7a.
  • the web-shaped section 7a is not completely parallel to the surface of the vertical spar 1b. Due to its short extension in the vertical direction, it can be assumed that this web section 7a extends substantially parallel to the surface even at an inclined angle of the insertion region 6a.
  • a partial compensation of the sash weight in FIG. 2 is shown results from the abutment of the head 8 'on the web-shaped portion 7a.
  • a pressure on the web-shaped portion is applied, which is effected by screwing the screw 8 in the vertical wing spar 1b, whereby the lower end of the wing lifts (torque directed to the right, mathematically negative).
  • This leads to a closing of the wing from its parked position requires a much greater effort. However, this is avoided by an adjustment of the vertical stiffening.
  • FIG. 4 The advantage of the adjustable stiffening clearly shows the FIG. 4 that are similar to FIG. 2 and 3 is shown.
  • the adjusting screw 8 is tightened more and with the help of the appropriately placed under transverse pressure upper portion 7a of the bolt 7, the lower spar 1a of the wing of the frame 2 is rotated away, which greatly facilitates the closing operation of the wing.
  • the bolt 7 was named as a torque lever and is elongated in geometric form, may be formed as a polygon bolt or round bolt or as an elongated plate. In the partially compensated position, the in FIG. 2 is shown, it is substantially parallel to the surface of the wing. Due to the inclination of the wing to lower due to its weight, the screw head 8 'by itself on the flattening 7a holds and is so far under pressure (contact pressure). Tightening the screw 8 causes the angle ⁇ is negative, so the bolt 7 is moved closer to the surface. The distance of the web 7a from the spar 16 is only a 2 , compared to a 1 of Fig. 3 ,
  • FIG. 5 shows a more developed form of vertical stiffening. This is shown in a front view with a bolt 7 'and its axis 701.
  • the mounting plate 9 which at its lower end two spaced-apart lugs 13, 13 ', which engage during assembly in corresponding receptacles in the support section 6, which is mounted in abutment with the lower wing spar (see FIG. 1 and 4 ).
  • the mounting plate 9 openings or holes 10 for the passage of screws for securing the upper portion of the vertical wing spar, which are provided in pairs in the "mutual" distance. In the example shown, there are two pairs, which are arranged once in the horizontal and the other in the vertical distance.
  • the upper end of the mounting plate 9 has at its rear a recess 8a "for receiving the head 8a 'of a strong bolt 8a, to which area on the opposite side of the plate 9 there is provided a raised area 9d of the plate, which is in one in the format and in the thickness fits or correspondingly formed flattening 12b at the upper end 7 * of the bolt 7 '.
  • This bolt has at the location of the flattening a threaded bore 8b corresponding to the thread of the bolt 8a.
  • the plate 9 On the bolt 7 'opposite side, the plate 9 has a down-expiring recess 12a, whose outline in FIG. 5 is indicated by a dashed line, and in the upper region in the plate 9, an elongated opening 11 is provided. This is also in the - the vertical section AA in FIG. 5 corresponding - both representations in the FIGS. 5a and 5b to see, as well as in FIG. 5d which one compared to FIG. 5 opposite view of the vertical stiffening with associated adjustment shows.
  • FIG. 5c shows the arrangement according to FIG. 5 in a vertical direction from above with lateral (bent out) projections 9a, 9b.
  • the bolt 7 ' is chamfered at the top 7 "and the opposite flattening 12b is visible.
  • FIG. 5a shows the device in a neutral (parallel) functional position in which the mounting plate 9 with the pin 7 'forms an angle zero (parallel position).
  • FIG. 5b shows the device in a biased position in which the bolt 8 a completely in the threaded bore 8b of the bolt 7 'is screwed in and this inclines to the mounting plate 9. In the inclination, an upper portion immersed in the recess 12 a and the opening 11 of the plate 9 a. The distance 'b' becomes smaller.
  • a push-through 9c which is designed as a contact surface for the pin 7 '.
  • the bolt 7 ' is loosely so that it can pivot, as with the FIG. 5b was clarified.
  • the resting of the bolt on the fürdrückung causes the bolt to pivot even though it does not have a bearing. As such, it is held up by the screw bolt 8a and, at least in a form-fitting manner, is inserted in the support profile 6 of the wing.
  • a lateral guidance of the bolt results from the two projections 9a, 9b of the FIG. 5c (View from above). These two bent tabs, which are bent out of the plate 9, have a distance from each other and are on both sides of the pin 7 'at. This approximately in the middle of the total height of the base plate 9. Thus, the bolt receives the lateral guidance, which also allows pivoting movements. A lateral shearing of the bolt is blocked by these holding elements 9a, 9b. It can thus also transverse forces from the pin 7 'are transmitted to the plate 9.
  • the distance "b" of the torque lever to the plate 9 changes in the upper region and results in a changed torque in the lower portion of the torque lever as a bolt 7 ', where this in the support section 6 (its insertion portion 6a ) sits.
  • the device ensures an appropriate corner reinforcement and thus a compensation of the higher force required when closing the parked wing with each application.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Door And Window Frames Mounted To Openings (AREA)
  • Hinges (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Window Of Vehicle (AREA)

Claims (12)

  1. Elément de rigidification vertical réglable pour un vantail (1) d'une porte coulissante écartable ou d'une fenêtre coulissante écartable, cet élément de rigidification vertical comprenant un goujon (7, 7'), un profil support (6) et un dispositif de réglage (8, 8'), le goujon (7, 7') étant relié au moins par une liaison par la forme au profil support (6) du longeron horizontal (1a) du vantail de sorte que le goujon (7, 7') maintienne ou permette d'obtenir une distance (X, b, a1, a2) au moins du longeron vertical (1b) du vantail (1), et le goujon (7, 7') comportant, à son extrémité supérieure (7a, 7*), au moins un perçage (7c, 8b) permettant le passage du dispositif de réglage (8, 8', 8a) par lequel une pression réglable peut être exercée sur l'extrémité supérieure (7a, 7*) du goujon de l'élément de rigidification vertical (6, 7, 7'), et le profil support (6) présentant, pour permettre une mise en place non coulissante dans la zone de coin inférieur du longeron horizontal (1a) et du longeron vertical (1b) du vantail une ouverture (6a) permettant l'enfichage sans jeu d'un segment d'extrémité inférieur (7b, 7b') du goujon (7, 7'), élément de rigidification dans lequel, entre l'ouverture d'enfichage (6a) et une surface (E) parallèle à celle-ci du profil support (6) qui est adaptée et susceptible de prendre appui sur la zone angulaire inférieure des longerons (1a, 1b) du vantail, il est prévu une distance (e) et un segment situé au-dessus du goujon peut être réglé par l'intermédiaire du dispositif de réglage (8, 8a) dans une direction perpendiculaire au longeron vertical du vantail ou à la surface parallèle (E) du profil support (6) vers l'extérieur ou vers l'intérieur pour modifier l'angle (α) défini entre un segment supérieur du goujon (7, 7') et une surface du longeron du vantail ou la surface (E) du profil support (6).
  2. Elément de rigidification vertical conforme à la revendication 1, dans lequel une ouverture verticale (6a) est prévue pour permettre un enfichage sans jeu d'un segment d'extrémité inférieur du goujon (7, 7') et la distance (e) de ce segment d'extrémité inférieur (7b, 7b') du longeron horizontal reste égale le long de la hauteur du profil support (6).
  3. Elément de rigidification vertical conforme à la revendication 1 ou 2, dans lequel la section du goujon (7, 7') est circulaire ou polygonale.
  4. Elément de rigidification vertical conforme à la revendication 1, dans lequel il est prévu une plaque de montage (9) stable qui comporte dans une zone d'extrémité supérieure des ouvertures (10) de pénétration d'éléments de fixation pour permettre la mise en appui de la plaque de montage (9) sur le longeron vertical (1b) du vantail, et, à son extrémité inférieure, des segments de mise en prise aplatis (13) pour permettre d'ancrer la plaque de montage dans le profil support (6).
  5. Elément de rigidification vertical conforme à la revendication 4, dans lequel il est prévu un goujon (7') ayant une section circulaire ou polygonale qui comporte dans sa zone d'extrémité supérieure, essentiellement à mi-distance entre deux ouvertures (10) pour les éléments de fixation un perçage fileté (8b) auquel est associée dans la plaque de montage (9) une ouverture permettant le passage d'un boulon fileté (8a), ce boulon (8a) venant en prise par une partie de tête (8a') dans une cavité (8a") de la plaque de montage adaptée à celle-ci.
  6. Elément de rigidification vertical conforme à la revendication 4 ou 5, dans lequel, sur la face plane de la plaque de montage (9) - opposée à la cavité - il est prévu une zone d'appui renforcée (9b) qui vient constamment en prise avec une zone aplatie (12b) ayant une forme et une épaisseur adaptées dans la zone d'extrémité supérieure du goujon (7'), en particulier l'axe du perçage fileté (8b) ou du boulon (8a) passe essentiellement à mi-distance au travers de ces zones.
  7. Elément de rigidification vertical conforme à l'une des revendications 4 à 6, dans lequel la plaque de montage (9) comporte, sur sa face tournée vers le goujon (7') un perçage longitudinal (11) situé à l'opposé du goujon et/ou une cavité (12a) ayant une profondeur diminuant vers le bas dans lequel ou laquelle le boulon pénètre par zones lorsque la position angulaire varie ou que la pénétration du boulon (8a) dans le perçage fileté (8b) augmente.
  8. Elément de rigidification vertical conforme à la revendication 4, caractérisé en ce qu'
    il est prévu, sur la face avant, essentiellement dans la zone médiane de la plaque de montage (9) au moins une paire faisant saillie d'éléments de retenue latéraux (9a, 9b) pour le goujon (7') s'enfichant par sa zone inférieure (7b') dans le profil support (6).
  9. Procédé permettant d'agir sur un élément de rigidification vertical conforme à l'une des revendications 1 à 8, selon lequel le goujon (7, 7') est relié au profil support (6) sur le longeron horizontal (1a) du vantail de sorte que ce goujon (7, 7') soit à une distance (X, b) du longeron vertical (1b) du vantail, et le goujon comporte à son extrémité supérieure (7a, 7*) au moins un perçage (7c, 8b), avec un dispositif de réglage (8, 8a), et, l'élément de rigidification vertical (7, 7') exerce sur l'extrémité supérieure du goujon par le dispositif de réglage une pression réglable qui permet de modifier la rigidification verticale.
  10. Procédé conforme à la revendication 9, selon lequel le goujon (7, 7') est enfiché par le haut dans le profil support (6) sur le longeron horizontal (1a) du vantail dans la zone d'enfichage (6a) de sorte que le goujon (7, 7') soit équipé à son extrémité supérieure (7a, 7*) du perçage (7c, 8b) avec le dispositif de réglage (8, 8a) introduit dans celui-ci, et qui règle ou modifie la distance (X, b, a) du segment d'extrémité supérieur du goujon de l'élément de rigidification verticale (6 ; 7, 7'), et entraine ainsi une modification du couple de rotation résultant dans la zone d'enfichage (6a) du profil support.
  11. Procédé conforme à la revendication 10, selon lequel la zone d'enfichage (6a) est inclinée dans une plage angulaire de ± 5° par rapport au plan vertical du profil support (6), en particulier, une plage angulaire de ± 2 % est prévue.
  12. Procédé conforme à la revendication 9 ou 10, selon lequel la liaison du goujon (7, 7') avec le profil support est réalisée en une seule pièce.
EP12703156.5A 2011-01-14 2012-01-11 Élément de renforcement vertical réglable pour un vantail coulissant Active EP2663710B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL12703156T PL2663710T3 (pl) 2011-01-14 2012-01-11 Regulowane usztywnienie pionowe dla odstawnego skrzydła przesuwnego

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102011000158 2011-01-14
PCT/IB2012/050147 WO2012095806A1 (fr) 2011-01-14 2012-01-11 Élément de renforcement vertical réglable pour un vantail coulissant

Publications (2)

Publication Number Publication Date
EP2663710A1 EP2663710A1 (fr) 2013-11-20
EP2663710B1 true EP2663710B1 (fr) 2014-12-17

Family

ID=45569705

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EP12703156.5A Active EP2663710B1 (fr) 2011-01-14 2012-01-11 Élément de renforcement vertical réglable pour un vantail coulissant

Country Status (5)

Country Link
EP (1) EP2663710B1 (fr)
KR (1) KR101954384B1 (fr)
CN (1) CN103328749B (fr)
PL (1) PL2663710T3 (fr)
WO (1) WO2012095806A1 (fr)

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DE102013226720B4 (de) 2013-12-19 2016-03-03 Roto Frank Ag Einstellbare Vertikalaussteifung mit Gleiter für einen abstellbaren Flügel eines Fensters einer Tür oder dergleichen
DE102013226716B4 (de) 2013-12-19 2016-02-18 Roto Frank Ag Einstellbare Vertikalaussteifung mit Exzenter für einen abstellbaren Flügel eines Fensters, einer Tür oder dergleichen
DE102014209915B3 (de) * 2014-05-23 2015-07-02 Roto Frank Ag Einstellbare Vertikalaussteifung mit Kulisse für einen abstellbaren Flügel eines Fensters oder einer Tür
DE102014014658A1 (de) 2014-10-08 2016-04-14 Lohmann Gmbh & Co. Kg Verstärkungsprofil mit Glasverklebung
DE202018001610U1 (de) * 2018-03-27 2018-04-13 Siegenia-Aubi Kg Antriebsvorrichtung mit einem Zahnstangenelement für einen verschiebbaren Flügel als Schiebeflügel oder verschiebbaren Hebe-Schiebeflügel eines Fensters oder einer Tür

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JPH09111936A (ja) * 1995-10-20 1997-04-28 T I S & Partners:Kk 板材の固定装置
JPH09279928A (ja) * 1996-04-16 1997-10-28 Shinkansai Bearing Kk 窓用ヒンジ
EP2267258B1 (fr) 2000-03-11 2017-05-10 HAUTAU GmbH Unité comportant un panneau coulissant et une ferrure
EP1391576B1 (fr) 2002-06-28 2008-05-28 HAUTAU GmbH Compensation de la torsion de battants pouvant être déplacés d'un plan vers un autre plan parallèle
KR200310949Y1 (ko) 2002-12-30 2003-04-26 (주)명진 창호용 슬라이더 어셈블리의 연결축
KR100721455B1 (ko) * 2005-12-21 2007-05-23 주식회사 엘지화학 시스템창호 개폐장치
CN201027447Y (zh) * 2007-03-27 2008-02-27 白宝鲲 门窗启闭动作的辅助装置
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DE202008007829U1 (de) * 2008-06-12 2008-08-21 Siegenia-Aubi Kg Beschlag für einen verschiebbaren Flügel von Fenstern oder Türen

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CN103328749B (zh) 2016-04-20
KR20140010376A (ko) 2014-01-24
WO2012095806A1 (fr) 2012-07-19
EP2663710A1 (fr) 2013-11-20
KR101954384B1 (ko) 2019-03-05
CN103328749A (zh) 2013-09-25

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