EP3156573B1 - Système d'armatures - Google Patents

Système d'armatures Download PDF

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Publication number
EP3156573B1
EP3156573B1 EP16201126.6A EP16201126A EP3156573B1 EP 3156573 B1 EP3156573 B1 EP 3156573B1 EP 16201126 A EP16201126 A EP 16201126A EP 3156573 B1 EP3156573 B1 EP 3156573B1
Authority
EP
European Patent Office
Prior art keywords
adjustment
fitting arrangement
adjustment mechanism
slide
accordance
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
EP16201126.6A
Other languages
German (de)
English (en)
Other versions
EP3156573A1 (fr
Inventor
Mathias Habersatter
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Maco Technologie GmbH
Original Assignee
Maco Technologie GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Maco Technologie GmbH filed Critical Maco Technologie GmbH
Publication of EP3156573A1 publication Critical patent/EP3156573A1/fr
Application granted granted Critical
Publication of EP3156573B1 publication Critical patent/EP3156573B1/fr
Active legal-status Critical Current
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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
    • E05D7/00—Hinges or pivots of special construction
    • E05D7/04—Hinges adjustable relative to the wing or the frame
    • E05D7/0415—Hinges adjustable relative to the wing or the frame with adjusting drive means
    • E05D7/0423—Screw-and-nut mechanisms
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00—Hinges or pivots of special construction
    • E05D7/04—Hinges adjustable relative to the wing or the frame
    • E05D2007/0461—Hinges adjustable relative to the wing or the frame in angular arrangement to the wing or the frame
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00—Hinges or pivots of special construction
    • E05D7/04—Hinges adjustable relative to the wing or the frame
    • E05D2007/0469—Hinges adjustable relative to the wing or the frame in an axial direction
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00—Hinges or pivots of special construction
    • E05D7/04—Hinges adjustable relative to the wing or the frame
    • E05D2007/0476—Pocket hinges
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00—Hinges or pivots of special construction
    • E05D7/04—Hinges adjustable relative to the wing or the frame
    • E05D2007/0484—Hinges adjustable relative to the wing or the frame in a radial direction
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00—Hinges or pivots of special construction
    • E05D7/04—Hinges adjustable relative to the wing or the frame
    • E05D2007/0492—Hinges adjustable relative to the wing or the frame in three directions
    • 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
    • E05Y2201/702—Spindles; Worms
    • 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
    • E05Y2201/704—Worm wheels

Definitions

  • the present invention relates to a fitting arrangement for a wing of a window, a door or the like with a wing part designed for attachment to the wing and with a frame part designed for attachment to a fixed frame.
  • the wing part and the frame part are pivotally coupled to one another.
  • the fitting arrangement can comprise an adjustment unit by means of which the relative position of the wing part and the frame part can be changed and / or by which the position of a pivot axis about which the wing part and the frame part can be pivoted are influenced.
  • Such an adjustment unit can also be designed such that a position of the frame part and / or the wing part on the frame or on the wing can be corrected with its help.
  • the adjustment unit can compensate for small inaccuracies in the frame and / or the sash and errors in attaching the fitting arrangement.
  • the problem with such adjustment units is often that the corresponding mechanisms for generating adjustment movements the frame part and / or the wing part are unreliable.
  • longitudinal adjustment mechanisms with the aid of which the frame part and the wing part can be moved relative to one another in a direction parallel to the pivot axis for adjustment purposes, the problem arises that the mechanism is displaced over time, so that the adjustment must be repeated.
  • the document US 2010/242227 A1 discloses a fitting arrangement according to the preamble of claim 1.
  • Other fitting arrangements with an adjusting unit are also from the documents EP 1 617 025 A2 , US 2008/022491 A1 , US 2006/179610 A1 and WO 02/086263 A1 known.
  • the fitting arrangement of the type mentioned at the beginning comprises a wing part and a frame part which are coupled to one another so as to be pivotable about a pivot axis.
  • the frame part and the wing part can be moved relative to one another in a direction parallel to the pivot axis by means of a longitudinal adjustment mechanism of an adjustment unit.
  • the longitudinal adjustment mechanism has self-locking properties.
  • the longitudinal adjustment mechanism is designed in such a way that the components involved only allow the adjustment to be changed if it is carried out consciously.
  • the forces occurring in the context of a normal use therefore do not cause any adjustment of the adjustment, so that an adjustment once carried out is reliably retained.
  • the adjustment unit has a transverse adjustment mechanism which is designed such that the frame part and the wing part can be moved relative to one another in a direction perpendicular to the pivot axis for adjustment purposes, the transverse adjustment mechanism in particular having self-locking properties.
  • a transverse adjustment mechanism can thus be provided so that the fitting arrangement can be adjusted not only parallel to the pivot axis but also perpendicular to it. An unwanted and often gradual loss of the adjustment can be reliably prevented by a self-locking design of the transverse adjustment mechanism.
  • Self-locking can be created by using suitable gears in the longitudinal adjustment mechanism and / or the transverse adjustment mechanism.
  • the longitudinal adjustment mechanism and / or the transverse adjustment mechanism comprise at least one worm gear.
  • the longitudinal adjustment mechanism and / or the transverse adjustment mechanism can be designed such that a relative movement of the frame part and the wing part - ie a movement of the frame part or the wing part or a movement of both parts - can be effected by a rotary movement of an adjusting element.
  • An axis of rotation of the adjusting element can be arranged perpendicular to an adjusting movement caused by a rotation of the adjusting element.
  • the adjusting element can be connected in a rotationally fixed manner to a worm in which a gearwheel engages in a rotationally fixed manner with an adjusting shaft of the longitudinal adjustment mechanism or the transverse adjustment mechanism.
  • the adjustment unit is arranged on the frame part or the wing part and interacts with a slide that can be moved for adjustment purposes, the frame part and / or the wing part being movable relative to the slide.
  • the slide is assigned to the frame part or the wing part, the other part being assigned a tab which engages in the slide.
  • the slide interacts with the adjustment shaft, which in turn can be rotated with the aid of the adjustment element.
  • a thread can be provided to convert a rotary movement of the adjusting shaft into a translational movement of the slide.
  • the carriage can be moved in a direction parallel to the pivot axis.
  • the tab is preferably arranged to be displaceable in a tab receptacle of the carriage in a direction perpendicular to the pivot axis.
  • the transverse adjustment mechanism can interact directly with the tab, in particular via a thread.
  • the slide is arranged in a housing which has guide elements for guiding the slide. If the housing covers the adjustment unit essentially completely, it is also protected against unintentional or unauthorized manipulation and against contamination.
  • the guide elements are designed in such a way that they form a bearing for pivoting the carriage about an axis parallel to the pivot axis.
  • the frame part or the wing part can comprise a base element which can be fixedly connected to the frame or to the wing.
  • an assembly play is provided between the components of the base element and the longitudinal adjustment mechanism interacting in the loaded state of the fitting arrangement in an unloaded state of the fitting arrangement in a direction parallel to the pivot axis.
  • the assembly play defines a maximum relative offset between the frame part and the wing part.
  • This embodiment is particularly advantageous when several fitting arrangements are used to mount a sash in a frame.
  • the problem arises that the individual fitting arrangements of conventional design have to be adjusted in a complex iterative process, since actuation of the directly interacting components of the respective adjustment mechanisms quickly leads to mechanical tension.
  • a fitting arrangement of the type described above with assembly play to first fasten a plurality of fitting arrangements to the sash and the frame and then to position the sash in an exact position using one of the fitting arrangements.
  • the other fitting arrangements do not hinder this adjustment process because whose frame parts and wing parts are movable relative to each other due to the assembly play.
  • the longitudinal adjustment mechanisms of the other fitting arrangements can be adjusted so that they are also loaded. In other words, their assembly play is run through until the corresponding components of the respective base element and the associated longitudinal adjustment mechanism interact and these fitting arrangements thus also develop a load-bearing action, so that the first adjusted fitting arrangement is relieved.
  • the assembly play can be dimensioned such that the maximum relative offset between the frame part and the wing part is between approximately 1 mm and approximately 10 mm, in particular between approximately 1 mm and approximately 5 mm, preferably between approximately 3 mm and approximately 10 mm, advantageously between about 3 mm and about 8 mm.
  • the longitudinal adjustment mechanism can comprise a rotatably mounted adjustment shaft which can be driven by an adjustment element or directly for a rotary movement in order to bring about a relative movement between the frame part and the wing part.
  • An axis of rotation of the adjusting shaft can be arranged parallel to the pivot axis.
  • the adjusting shaft has a shoulder which interacts with a shoulder element provided on the base element in a loaded state of the fitting arrangement.
  • the attachment element is supported on the shoulder of the adjusting shaft in a loaded state of the fitting arrangement, or vice versa.
  • the load on the fitting arrangement is thus transmitted from the wing part to the frame part by the shoulder and the appropriately designed attachment element.
  • the adjusting shaft can - in an unloaded or loaded state of the fitting arrangement - be movable relative to the base element in a direction parallel to the pivot axis.
  • the base element can be a component of a housing that accommodates the adjustment unit and in particular essentially completely covers it.
  • the housing can also have a component that can be fastened to the base element and that has a component that interacts with the component of the longitudinal adjustment mechanism in a loaded state of the fitting arrangement.
  • the named component of the cover component is complementary to the corresponding component of the base element.
  • the adjustment unit is preferably arranged on the wing part.
  • Fig. 1 shows a fitting arrangement 10, which is used, for example, for fastening a wing of a window, a door or the like to a corresponding frame.
  • the fitting arrangement 10 comprises a wing part 14 which is fastened to the wing and a frame part 12 which is fastened to the frame.
  • the wing part 14 and the frame part 12 are pivotally coupled to one another by an axle pin 16.
  • the axis pin 16 thus forms a pivot axis of the fitting arrangement 10.
  • the wing part 14 and the frame part 12 are fastened to the component of a window or door assigned to them, the problem often arises that the wing is not correctly positioned in the frame.
  • the positioning errors are usually quite small, but they can hinder the correct closing of the window or door. Apart from this, poor centering of the sash in the frame disturbs the visual impression to a not inconsiderable degree.
  • the fitting arrangement 10 comprises an adjustment unit with which the relative spatial arrangement of the sash part 14 and the frame part 12 can be adjusted.
  • the adjustment unit is arranged essentially in the interior of the wing part 14, so that its mechanical components or the mechanisms for generating the various adjustment movements in FIG Fig. 1 cannot be seen. In Fig. 1 only adjusting screws 18, 18 'and a position indicator 20 can be seen.
  • the axle pin 16 is received by pivot bearings 24 of the frame part 12. It couples a bracket 22 to the pivot bearings 24.
  • the bracket 22 protrudes into a body 14a of the wing part 14.
  • the wing connected to the wing member 14 ultimately bears on the bracket 22.
  • the adjusting screw 18 By rotation the adjusting screw 18, the wing part 14 can be moved relative to the bracket 22 in a direction parallel to the axis pin 16 forming the pivot axis of the fitting arrangement 10. If the fitting arrangement 10 is used, for example, in a door, an adjustment of the height of the wing of the door in the frame can be adjusted by actuating the adjusting screw 18.
  • the position indicator 20 shows the position — relative to a direction parallel to the axis pin 16 —of the tab 22 relative to the body 14a of the wing part 14, so that an operator can better observe the progress of the adjustment process.
  • the position indicator 20 shows directly in which direction and by what amount the body 14a is moved relative to the tab 22 and thus the frame part 12.
  • the adjusting screw 18 ' enables an adjustment of the angle between a plane spanned by the tab 22 and a plane spanned by the wing part 14, according to FIG Fig. 8 is explained in more detail.
  • the adjustment screws 18, 18 'and the position indicator 20 are assigned markings in order to facilitate the operation of the adjustment unit of the fitting arrangement 10. Furthermore, the body 14a has fastening openings 32 through which fastening elements - for example screws - are guided for fastening the wing part 14 to the wing can. Fastening openings 32 are also provided on a fastening plate 33 of the frame part 12.
  • Fig. 2 shows a further perspective view of the fitting arrangement 10, whereby it can be seen that the body 14a of the wing part 14 is composed of a base part 28 and a cover part 30.
  • the base part 28 and the cover part 30 form a housing and protect the mechanical components of the adjustment unit and therefore contribute to the robust design of the fitting arrangement 10.
  • the view of the Fig. 2 allow a view of a mounting opening 34 of the housing, which is arranged on the side of the body 14a facing away from the frame part 12.
  • a component of a transverse adjustment mechanism of the adjustment unit can be reached through the mounting opening 34 in order to be able to secure it in the course of a factory assembly of the fitting arrangement 10, as can be seen in FIG Fig. 5 is explained in more detail.
  • the transverse adjustment mechanism serves to move the tab 22 in a direction perpendicular to the pivot axis of the fitting arrangement 10.
  • Fig. 3 illustrates the fundamentally very simple construction of the frame part 12.
  • the frame part 12 In addition to the pivot bearings 24, the frame part 12 only includes the fastening plate 33 having the fastening openings 32.
  • the frame part 12 does not comprise any components of the adjustment unit.
  • Fig. 4 shows a view of the wing part 14 with the cover part 30 removed. It can be seen that the tab 22 projects into a carriage 36 which can be moved in a direction parallel to the pivot axis of the fitting arrangement 10 inside the body 14a of the wing part 14.
  • the carriage 36 and sections of the base part 28 and the cover part 30 which are in direct contact with it are provided with complementary surface structures which allow the movement mentioned and reliably prevent the movement of the slide 36 in other spatial directions.
  • a flat groove 38 is provided on the base part 28 and runs parallel to the axis pin 16.
  • the carriage 36 is on its - in Fig. 4 not to be seen - provide a complementary rib on the underside.
  • a corresponding guide device, comprising a rib 40 on the upper side of the slide 36, is provided between the cover part 30 and the slide 36.
  • the ribs 40 and the grooves 38 form - as by means of Fig. 8 will be explained in detail below - also a bearing through which the tab 22 is pivotally mounted relative to the wing part 14.
  • a longitudinal adjustment mechanism 42 which comprises the adjustment screw 18 already mentioned above.
  • the adjusting screw 18 is provided radially on the outside with a worm 44, in which a gear 46 engages, which in turn is non-rotatably connected to an adjusting shaft 48.
  • the adjusting shaft 48 projects into an opening of the slide 36.
  • the end of the adjusting shaft 48 protruding into the slide 36 is provided with an external thread which engages in a corresponding internal thread of the opening of the slide 36.
  • the adjusting screw 18 is thus coupled to the slide 36 via a worm thread and the above-described external / internal thread combination.
  • a rotation of the adjusting screw 18 causes the worm gear consisting of the worm 44 and the gear 46 a rotation of the adjustment shaft 48, which is converted into a movement of the wing part 14 in a direction parallel to the pivot axis of the fitting arrangement 10 via the aforementioned external / internal thread combination with the frame part 12 fixed.
  • the longitudinal adjustment mechanism 42 has the advantage that it does not move even when the fitting arrangement 10 is used.
  • the worm thread consisting of the worm 44 and the gear 46 has self-locking properties.
  • a pivoting movement of the fitting arrangement 10 acts on the slide 36.
  • the axis of rotation of the adjusting screw 18 is oriented perpendicular to the axis of rotation of the adjusting shaft 48 and a worm gear couples the two components 18, 48 mentioned, even continuous loads on the slide 36 do not lead to one Movement of the adjusting screw 18.
  • a spatial adjustment of the parts 12, 14 relative to one another in a direction parallel to the pivot axis can only be brought about when the adjusting screw 18 is actively actuated.
  • Fig. 5 shows a similar view of the frame part 14 as that Fig. 4 .
  • parts of the slide 36 have been removed in order to make the end of the adjusting shaft 48 facing away from the gear 46 and projecting into the slide recognizable.
  • an external thread 49a is provided, which interacts with a complementary internal thread 49b of the slide 36.
  • the threads 49a, 49b serve to convert a rotary movement of the adjusting shaft 48 into one Stroke movement B1 of the wing part 14 parallel to the pivot axis of the fitting arrangement 10.
  • the Fig. 5 also provides insight into the operation of a transverse adjustment mechanism 50, the purpose of which has already been mentioned above.
  • a screw 52 is provided which interacts with the tab 22.
  • a head of the screw 52 can be reached through the adjustment opening 53.
  • Rotation of the screw 52 causes the tab 22 to be pulled into the carriage 36, which is shown in FIG Fig. 5 corresponds to a movement B2 in the image plane to the right, or is pushed away from the slide 36, which in Fig. 5 corresponds to a movement B2 in the image plane to the left.
  • the screw 52 In order to prevent the screw 52 from being inadvertently completely unscrewed after a factory assembly of the fitting arrangement 10, it is widened at its end facing away from the frame part 12. In order to be able to reach this end of the screw 52 for this purpose, the mounting opening 34 is provided.
  • the transverse adjustment mechanism can also be designed to be self-locking, in contrast to the design shown. Since the problem of loss of adjustment when using the fitting arrangement - that is to say by pivoting the frame or wing part - arises in particular in connection with the longitudinal adjustment mechanism, in many cases it is sufficient to provide the latter with self-locking properties only.
  • Fig. 6 shows a part of the longitudinal adjustment mechanism 42 in a detailed view.
  • the adjusting screw 18 with the worm 44 can be seen, into which the gear 46 arranged on the adjusting shaft 48 intervenes.
  • the wing part 14 In a loaded condition of the fitting arrangement 10, the wing part 14 ultimately hangs on the bracket 22 on the frame part 12 fixedly arranged on the frame.
  • the adjusting shaft 48 plays a crucial role. This is because a shoulder 54 is formed on which, in a loaded state of the fitting arrangement 10, a projection 56 rests, which is formed in one piece with the base part 28.
  • the cover part 30 has a complementarily designed projection 56, so that when the parts 28, 30 are in the assembled state, these ultimately form a support ring which bears on the shoulder 54.
  • FIG. 6 The longitudinal adjustment mechanism 42 is shown in an unloaded state of the fitting arrangement 10.
  • the projection 56 does not rest on the shoulder 54.
  • a maximum available assembly play X is composed of the aforementioned game X1 and a second game X2, which in the state shown is present between the projection 56 and a shoulder 54 'of the adjusting shaft 48.
  • the game X is determined by the distance between the shoulders 54, 54 'and the width of the projection 56.
  • the assembly play X is in practice between 1 and 10 mm, preferably less than 5 mm, e.g. B. about 3 mm.
  • the adjusting shaft 48 can be moved relative to the base part 28 and thus ultimately also to the adjusting screw 18.
  • the components 44, 46 of the worm thread must also be displaceable relative to one another.
  • the frame parts 12 are fixed to the frame and the wing parts 14 to the wing in the approximately correct positions.
  • one of the fitting arrangements 10 is used to adjust the position of the sash in the frame. Because of the play X, the respective frame parts 12 and wing parts 14 can move freely relative to one another, so that the other fitting arrangement 10 which is not loaded in this state does not hinder the adjustment.
  • the fitting arrangement 10 used in the adjustment carries the sash alone in this state.
  • the longitudinal adjustment mechanism 42 of the previously unloaded fitting arrangement 10 is actuated until its shoulder 54 strikes the projections 56 of the parts 28, 30. From then on, this fitting arrangement also provides 10 a load-bearing effect without having been used in the adjustment itself - ie in the position correction of the wing.
  • Fig. 7 illustrates the geometry of the tab 22, since the carriage 36 is not shown.
  • the slide 36 ultimately serves as an intermediate element for converting a rotary movement of the adjusting shaft 48 into a translational movement which is transmitted to the bracket 22 which can be moved perpendicularly thereto by the transverse adjustment mechanism 50.
  • Fig. 8 shows a section through the fitting arrangement 10 in a plane perpendicular to the pivot axis.
  • the fitting arrangement 10 is shown in a closed state of the wing.
  • the fitting arrangement 10 is a concealed fitting.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Pinball Game Machines (AREA)
  • Door And Window Frames Mounted To Openings (AREA)

Claims (13)

  1. Ensemble de ferrure pour un battant d'une fenêtre, d'une porte ou similaire, comportant une partie de battant (14) réalisée pour être montée sur le battant et une partie de cadre (12) réalisée être montée sur un cadre stationnaire, la partie de battant (14) et la partie de cadre (12) étant couplées l'une à l'autre de façon mobile en basculement autour d'un axe de basculement, et la partie de cadre (12) et la partie de battant (14) étant mobiles l'une par rapport à l'autre dans une direction (B1) parallèle à l'axe de basculement, à des fins d'ajustement au moyen d'un mécanisme d'ajustement longitudinal (42) d'une unité d'ajustement,
    dans lequel
    le mécanisme d'ajustement longitudinal (42) présente des propriétés d'auto-blocage,
    l'unité d'ajustement est disposée sur la partie de cadre (12) ou sur la partie de battant (14) et coopère avec un chariot (36) mobile à des fins d'ajustement,
    la partie de cadre (12) et/ou la partie de battant (14) sont mobiles par rapport au chariot (36), et
    le chariot (36) est disposé dans un boîtier (28, 30),
    des éléments de guidage (38, 40) destinés à guider le chariot (36) sont prévus sur le chariot (36) et sur le boîtier (28, 30), et
    en particulier, le boîtier (28, 20) recouvre sensiblement complètement l'unité d'ajustement,
    caractérisé en ce que
    le chariot (36) est associé à la partie de cadre (12) ou à la partie de battant (14), et en ce que
    une patte (22) est associée à l'autre partie (14 ou 12), qui s'engage dans le chariot (36), et en ce que
    les éléments de guidage (38, 40) comprennent des nervures (40) et des rainures (38) complémentaires qui constituent un palier pour un basculement du chariot (36) autour d'un axe parallèle à l'axe de basculement.
  2. Ensemble de ferrure selon la revendication 1,
    caractérisé en ce que
    l'unité d'ajustement comprend un mécanisme d'ajustement transversal (50) qui est réalisé de telle sorte que la partie de cadre (12) et la partie de battant (14) sont mobiles l'une par rapport à l'autre dans une direction (B2) perpendiculaire à l'axe de basculement, à des fins d'ajustement, et en particulier le mécanisme d'ajustement transversal (50) présente des propriétés d'auto-blocage.
  3. Ensemble de ferrure selon l'une au moins des revendications précédentes,
    caractérisé en ce que
    le mécanisme d'ajustement longitudinal (42) et/ou le mécanisme d'ajustement transversal (50) comporte(nt) au moins un engrenage à vis sans fin (44, 46).
  4. Ensemble de ferrure selon la revendication 1 ou 2,
    caractérisé en ce que
    le mécanisme d'ajustement longitudinal (42) et/ou le mécanisme d'ajustement transversal (50) est/sont réalisé(s) de manière à pouvoir provoquer un mouvement d'ajustement (B1 ou B2) de la partie de cadre (12) et de la partie de battant (14) l'une par rapport à l'autre par un mouvement de rotation d'un élément d'ajustement (18 ou 18'), et en particulier un axe de rotation de l'élément d'ajustement (18, 18') est disposé perpendiculairement à un mouvement d'ajustement (B1 ou B2) provoqué par une rotation de l'élément d'ajustement (18, 18').
  5. Ensemble de ferrure selon la revendication 4,
    caractérisé en ce que
    l'élément d'ajustement (18) est relié solidairement en rotation à une vis sans fin (44) dans laquelle s'engage une roue dentée (46) reliée solidairement en rotation à un arbre d'ajustement (48) du mécanisme d'ajustement longitudinal (42) ou du mécanisme d'ajustement transversal.
  6. Ensemble de ferrure selon la revendication 1,
    caractérisé en ce que
    le chariot (36) coopère avec un arbre d'ajustement (48) du mécanisme d'ajustement longitudinal (42) par l'intermédiaire d'un pas de vis (49a, 49b).
  7. Ensemble de ferrure selon la revendication 1,
    caractérisé en ce que
    la patte (22) est disposée dans un logement à patte du chariot (36) de façon mobile en translation dans une direction (B2) perpendiculaire à l'axe de basculement.
  8. Ensemble de ferrure selon la revendication 2,
    caractérisé en ce que
    le mécanisme d'ajustement transversal (50) coopère avec la patte (22) directement, en particulier par l'intermédiaire d'un pas de vis.
  9. Ensemble de ferrure selon l'une au moins des revendications précédentes,
    caractérisé en ce que
    la partie de cadre (12) ou la partie de battant (14) comprend un élément de base (28) susceptible d'être fermement relié au cadre ou au battant, et dans un état non chargé de l'ensemble de ferrure, dans une direction parallèle à l'axe de basculement, il est prévu un jeu de montage (X) entre des portions (56 ou 54) de l'élément de base (28) et du mécanisme d'ajustement longitudinal (42) qui coopèrent l'une avec l'autre dans un état chargé de l'ensemble de ferrure, ledit jeu de montage définissant un décalage relatif maximal entre la partie de cadre (12) et la partie de battant (14).
  10. Ensemble de ferrure selon la revendication 9,
    caractérisé en ce que
    le jeu de montage (X) est dimensionné de telle sorte que le décalage relatif maximal entre la partie de cadre (12) et la partie de battant (14) est compris entre environ 1 mm et environ 10 mm, en particulier entre environ 1 mm et environ 5 mm, de préférence entre environ 3 mm et environ 10 mm, avantageusement entre environ 3 mm et environ 8 mm.
  11. Ensemble de ferrure selon la revendication 9 ou 10,
    caractérisé en ce que
    le mécanisme d'ajustement longitudinal (42) comprend un arbre d'ajustement (48) monté mobile en rotation qui peut être entraîné en un mouvement de rotation soit directement soit par l'élément d'ajustement (18), afin de provoquer un mouvement relatif entre la partie de cadre (12) et la partie de battant (14), et en particulier
    un axe de rotation de l'arbre d'ajustement (48) est agencé parallèlement à l'axe de basculement.
  12. Ensemble de ferrure selon la revendication 11,
    caractérisé en ce que
    l'arbre d'ajustement (48) comprend un épaulement (54) qui, dans un état chargé de l'ensemble de ferrure, coopère avec un élément rapporté (56) prévu sur l'élément de base (28), et/ou
    l'arbre d'ajustement (48) est déplaçable par rapport à l'élément de base (28) dans une direction parallèle à l'axe de basculement.
  13. Ensemble de ferrure selon l'une des revendications 9 à 12,
    caractérisé en ce que
    l'élément de base (28) est un composant d'un boîtier qui reçoit l'unité d'ajustement et qui la recouvre en particulier sensiblement complètement, et/ou en ce que
    le boîtier comprend un composant de couvercle (30) qui peut être fixé à l'élément de base (28) et qui comprend une portion qui, dans un état chargé de l'ensemble de ferrure, coopère avec la portion (54) du mécanisme d'ajustement longitudinal (42).
EP16201126.6A 2011-11-03 2012-10-31 Système d'armatures Active EP3156573B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE202011107495U DE202011107495U1 (de) 2011-11-03 2011-11-03 Beschlaganordnung
EP12190894.1A EP2589735B1 (fr) 2011-11-03 2012-10-31 Agencement de ferrure

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EP12190894.1A Division-Into EP2589735B1 (fr) 2011-11-03 2012-10-31 Agencement de ferrure
EP12190894.1A Division EP2589735B1 (fr) 2011-11-03 2012-10-31 Agencement de ferrure

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EP3156573A1 EP3156573A1 (fr) 2017-04-19
EP3156573B1 true EP3156573B1 (fr) 2020-04-01

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EP16201126.6A Active EP3156573B1 (fr) 2011-11-03 2012-10-31 Système d'armatures
EP12190894.1A Active EP2589735B1 (fr) 2011-11-03 2012-10-31 Agencement de ferrure

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EP12190894.1A Active EP2589735B1 (fr) 2011-11-03 2012-10-31 Agencement de ferrure

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Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2924211B1 (fr) * 2014-03-26 2019-10-23 Alban Giacomo S.p.A. Charnière ajustable pour portes ou fenêtres

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10120260C1 (de) * 2001-04-25 2002-06-06 Sfs Ind Holding Ag Heerbrugg Tür- oder Fensterscharnier
DE102004033883B3 (de) * 2004-07-13 2006-01-05 Sfs Intec Holding Ag Scharnier für stumpf einschlagende Türen
US7334293B2 (en) * 2005-02-16 2008-02-26 Newell Operating Company Vertically adjustable hinge
US7552511B2 (en) * 2006-07-28 2009-06-30 Creative Research & Development, Inc. Adjustable hinge
US8429794B2 (en) * 2009-03-25 2013-04-30 Amesbury Group, Inc. Adjustable door hinge

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
EP2589735B1 (fr) 2021-09-01
DE202011107495U1 (de) 2013-02-04
EP2589735A3 (fr) 2016-05-11
EP3156573A1 (fr) 2017-04-19
EP2589735A2 (fr) 2013-05-08

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