EP2589734B1 - Agencement de ferrure - Google Patents

Agencement de ferrure Download PDF

Info

Publication number
EP2589734B1
EP2589734B1 EP12190635.8A EP12190635A EP2589734B1 EP 2589734 B1 EP2589734 B1 EP 2589734B1 EP 12190635 A EP12190635 A EP 12190635A EP 2589734 B1 EP2589734 B1 EP 2589734B1
Authority
EP
European Patent Office
Prior art keywords
adjustment
fitting arrangement
frame
leaf
wing
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
EP12190635.8A
Other languages
German (de)
English (en)
Other versions
EP2589734A3 (fr
EP2589734A2 (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
Priority to PL12190635T priority Critical patent/PL2589734T3/pl
Publication of EP2589734A2 publication Critical patent/EP2589734A2/fr
Publication of EP2589734A3 publication Critical patent/EP2589734A3/fr
Application granted granted Critical
Publication of EP2589734B1 publication Critical patent/EP2589734B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • 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
    • 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
    • E05Y2600/50—Mounting methods; Positioning
    • E05Y2600/56—Positioning, e.g. re-positioning, or pre-mounting
    • 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
    • E05Y2900/132—Doors

Definitions

  • the present invention relates to a fitting arrangement for a wing of a window, a door or the like having a wing portion adapted to be mounted on the wing and having a frame part adapted for attachment to a fixed frame.
  • the wing part and the frame part are pivotally coupled together.
  • the fitting arrangement may comprise an adjusting unit, by which the relative position of the wing part and the frame part can be changed and / or by the position of a pivot axis to pivot about the wing part and the frame part are to be influenced.
  • an adjusting unit can also be designed so that with its help a position of the frame part and / or the wing part on the frame or on the wing can be corrected. In other words, small inaccuracies of the frame and / or the wing as well as errors in attaching the fitting arrangement can be compensated by the adjusting unit.
  • the US 2006/0179610 A1 discloses a fitting assembly having a longitudinal adjustment mechanism with a rotatable spindle held axially fixed in a housing of the assembly.
  • the WO 2005/075776 A1 describes a fitting arrangement with the features of the preamble of claim 1.
  • the fitting arrangement of the aforementioned type comprises a wing part and a frame part, which are pivotably coupled to one another about a pivot axis.
  • the frame part and the wing portion are movable relative to each other for adjustment purposes by means of a longitudinal adjustment mechanism of an adjusting unit in a direction parallel to the pivot axis.
  • the frame part or the wing part comprises a fixedly connectable to the frame or with the wing base member. Between in loaded condition of the fitting assembly cooperating components of the base member and the longitudinal adjustment mechanism is provided in an unloaded state of the fitting assembly in a direction parallel to the pivot axis a mounting clearance.
  • the mounting clearance determines a maximum relative offset between the frame part and the wing part.
  • the fitting arrangements according to the invention In contrast to the complex iterative adjustment procedure of conventional type described above, it is possible when using the fitting arrangements according to the invention with mounting clearance to first attach a plurality of fitting arrangements on the wing and the frame and then position the wing by means of one of the fitting arrangements.
  • the other fitting arrangements do not hinder this adjustment process, since their frame parts and wing parts are freely movable relative to each other due to the mounting clearance.
  • the longitudinal adjustment mechanisms of the other fitting assemblies can be adjusted to load them as well. That is, their assembly game is passed through until the corresponding components of the respective base member and the associated longitudinal adjustment mechanism cooperate and thus this fitting arrangements thus develop a supporting effect, so that the first adjusted fitting arrangement is relieved.
  • the mounting clearance can be dimensioned such that the maximum relative offset between the frame part and the wing part between about 1 mm and about 10 mm, in particular between about 1 mm and about 5 mm, preferably between about 3 mm and about 10 mm, advantageously between about 3 mm and about 8 mm.
  • the longitudinal adjustment mechanism comprises a rotatably mounted adjustment shaft, which is drivable by an adjusting element or directly to a rotational movement, to effect a relative movement between the frame part and the wing part.
  • An axis of rotation of the adjusting shaft is arranged parallel to the pivot axis.
  • the adjusting shaft has a shoulder which cooperates in a loaded state of the fitting arrangement with a provided on the base element lug element.
  • the neck element is supported in a loaded state of the fitting arrangement on the shoulder of the Justierwelle, or vice versa.
  • the loading of the fitting arrangement is thus transmitted through the shoulder and the correspondingly formed attachment element from the wing part to the frame part, or vice versa.
  • the adjusting shaft is movable in an unloaded state of the fitting arrangement relative to the base element in a direction parallel to the pivot axis.
  • the longitudinal adjustment mechanism cooperates with a carriage, wherein the frame part and / or the wing part are movable relative to the carriage.
  • the adjusting shaft acts via a thread, in particular an external thread female thread mating, with the carriage together.
  • the longitudinal adjustment mechanism comprises a screw thread, which preferably has self-locking properties.
  • the worm thread can be provided, for example, between an adjusting element which can be directly actuated by an operator and the adjusting shaft.
  • the worm thread comprises a worm which is arranged on the adjustment element which can be actuated for adjustment purposes and in which a toothed wheel, which is arranged on the adjusting shaft, engages.
  • the base member is a component of a housing which receives the adjusting unit and in particular substantially completely covers.
  • the housing may further comprise a component attachable to the base member and having a component cooperating with the component of the longitudinal adjustment mechanism in a loaded condition of the fitting assembly.
  • said component of the cover component is formed complementary to the corresponding component of the base element.
  • Fig. 1 shows a fitting assembly 10, which serves for example for fixing a wing of a window, a door or the like to a corresponding frame.
  • the fitting assembly 10 includes a wing portion 14 which is secured to the wing and a frame portion 12 which is secured to the frame.
  • the wing part 14 and the frame part 12 are pivotally coupled together by an axle 16.
  • the axle pin 16 thus forms a pivot axis of the fitting arrangement 10.
  • the problem often arises that the wing is not correctly positioned in the frame. Although the positioning errors are usually quite small, they can hinder a correct closing of the window or the door. Apart from that, a bad centering of the wing in the frame disturbs the visual impression to a considerable extent.
  • the fitting arrangement 10 comprises an adjustment unit with which the relative spatial arrangement of the wing part 14 and the frame part 12 can be adjusted.
  • the adjusting unit is arranged substantially in the interior of the wing part 14, so that their mechanical components or the mechanisms for generating the various adjustment movements in Fig. 1 not to be seen. In Fig. 1 only adjustment screws 18, 18 'and a position indicator 20 can be seen.
  • the axle 16 is received by pivot bearings 24 of the frame part 12.
  • the flap 22 projects into a body 14a of the wing portion 14.
  • the wing associated with the wing portion 14 ultimately bears on the flap 22.
  • the adjusting screw 18 By rotation the adjusting screw 18, the wing member 14 relative to the tab 22 in a direction parallel to the pivot axis of the fitting assembly 10 forming axis pin 16 are moved. If the fitting arrangement 10 is used, for example, in the case of a door, an adjustment of the height of the wing of the door in the frame can be adjusted by actuating the adjustment screw 18.
  • the position indicator 20 indicates in which position - relative to a direction parallel to the axle pin 16 - the tab 22 is relative to the body 14a of the wing portion 14 so that an operator can better observe the progress of the adjustment process.
  • the position indicator 20 directly indicates 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 allows an adjustment of the angle between a plane spanned by the tab 22 and a plane through the Wing part 14 spanned plane, according to below with reference to Fig. 8 is explained in more detail.
  • the adjustment screws 18, 18 'and the position indicator 20 are associated with markings to facilitate the operation of the adjustment of the fitting assembly 10. Further, the body 14a mounting holes 32, can be guided by the fastening elements - for example screws - for attachment of the wing portion 14 to the wing. Mounting openings 32 are also provided on a mounting plate 33 of the frame part 12.
  • Fig. 2 shows a further perspective view of the fitting assembly 10, whereby it can be seen that the body 14a of the wing portion 14 of a base portion 28 and a cover member 30 composed.
  • the base part 28 and the cover part 30 form a housing and protect the mechanical components of the adjusting unit and therefore contribute to the robust design of the fitting arrangement 10.
  • the view of Fig. 2 allow the view of a mounting opening 34 of the housing, which is arranged on the side facing away from the frame part 12 of the body 14a.
  • the transverse adjustment mechanism serves to displace the tab 22 in a direction perpendicular to the pivot axis of the fitting assembly 10.
  • Fig. 3 illustrates the basically very simple construction of the frame part 12.
  • the pivot bearings 24 includes the frame part 12th only the mounting holes 33 having the mounting plate 33.
  • the frame part 12 includes no components of the adjusting unit.
  • Fig. 4 shows a view of the wing portion 14 with the cover part 30. It can be seen that the tab 22 protrudes into a carriage 36 which is movable in a direction parallel to the pivot axis of the fitting assembly 10 in the interior of the body 14 a of the wing member 14.
  • the carriage 36 and portions of the base portion 28 and the lid portion 30 which are in direct contact with it are provided with complementary surface structures which allow said movement and reliably prevent the carriage 36 from moving in other directions.
  • a flat groove 38 is provided on the base part 28, which runs parallel to the axle pin 16.
  • the carriage 36 is at its - in Fig. 4 not to be seen - underside provided with a complementarily shaped rib.
  • a corresponding guide means comprising a rib 40 on the upper side of the carriage 36 is provided between the lid member 30 and the carriage 36.
  • the ribs 40 and the grooves 38 form - as based on Fig. 8 will be explained in detail below - also a bearing by which the tab 22 is pivotally mounted relative to the wing member 14.
  • a longitudinal adjustment mechanism 42 which comprises the adjustment screw 18 already mentioned above.
  • the adjusting screw 18 is radially outwardly provided 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 carriage 36.
  • the in the Carriage 36 projecting end of the adjusting shaft 48 is provided with an external thread which engages in a corresponding internal thread of the opening of the carriage 36.
  • the adjusting screw 18 is thus coupled via a worm thread and the above-described male / female combination with the carriage 36.
  • a rotation of the adjusting screw 18 causes via the worm gear consisting of the worm 44 and the gear 46, a rotation of the adjusting shaft 48, via the above-mentioned external / internal thread combination with fixed frame part 12 in a movement of the wing member 14 in a direction parallel to the pivot axis of the fitting assembly 10 is implemented.
  • the longitudinal adjustment mechanism 42 has the advantage that it does not move even when using the fitting assembly 10.
  • the screw thread consisting of the worm 44 and the gear wheel 46 has self-locking properties.
  • a pivotal movement of the fitting assembly 10 acts on the carriage 36.
  • the axis of rotation of the adjusting screw 18 is aligned perpendicular to the axis of rotation of the adjusting shaft 48 and a worm gear coupling the two said components 18, 48, also continuous loads of the carriage 36 does not lead to a Movement of the adjusting screw 18.
  • a spatial displacement of the parts 12, 14 relative to each other 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 the Fig. 4 , However, parts of the carriage 36 have been removed to make the gear 46 remote and projecting into the carriage end of the adjusting shaft 48 recognizable.
  • an external thread 49 a is provided, which cooperates with a complementarily formed internal thread 49 b of the carriage 36.
  • the threads 49a, 49b are used to implement a rotational movement of the adjusting shaft 48 in a lifting movement B1 of the wing member 14 parallel to the pivot axis of the fitting assembly 10th
  • the Fig. 5 also provides insights into the operation of a lateral adjustment mechanism 50, the purpose of which has already been mentioned above.
  • a screw 52 is provided which cooperates with the tab 22.
  • a head of the screw 52 can be reached through the adjusting hole 53.
  • a rotation of the screw 52 causes the tab 22 is pulled into the carriage 36, which in Fig. 5 corresponds to a movement B2 in the image plane to the right, or is pushed away from the carriage 36, which in Fig. 5 corresponds to a movement B2 in the image plane to the left.
  • the mounting hole 34 is provided.
  • the transverse adjustment mechanism can also be designed to be self-locking, differing from the design shown. Since the problem with respect to a loss of adjustment when using the fitting assembly - ie by pivoting the frame or wing part - Occurs in particular in connection with the longitudinal adjustment mechanism, it is sufficient in many cases, to provide only the latter with self-locking properties.
  • Fig. 6 shows a part of the longitudinal adjustment mechanism 42 in a detailed view.
  • the adjusting screw 18 with the worm 44 in which engages the arranged on the adjusting shaft 48 gear 46.
  • the wing part 14 In a loaded state of the fitting arrangement 10, the wing part 14 ultimately hangs on the tab 22 on the frame part 12 fixedly arranged on the frame.
  • the adjusting shaft 48 plays a decisive role here.
  • a shoulder 54 is formed on which in a loaded state of the fitting assembly 10, a projection 56 rests, which is integrally formed with the base part 28.
  • the cover part 30 has a complementary projection 56, so that they together in an assembled state of the parts 28, 30 ultimately form a support ring which rests on the shoulder 54.
  • Fig. 6 the longitudinal adjustment mechanism 42 is shown in an unloaded state of the fitting assembly 10.
  • the projection 56 does not rest on the shoulder 54.
  • a game X1 which simplifies the assembly and adjustment of the fitting assembly 10 in an unloaded condition of the fitting assembly 10.
  • a maximum available assembly game X is made from the above called game X1 and a second game X2 together, which is present in the illustrated state between the projection 56 and a shoulder 54 'of the adjusting shaft 48.
  • the clearance X is determined by the distance of the shoulders 54, 54 'and the width of the projection 56.
  • the mounting clearance X is in practice between 1 and 10 mm, preferably less than 5 mm, z. B. about 3 mm.
  • the adjusting shaft 48 is movable relative to the base part 28 and thus ultimately to the adjusting screw 18.
  • the components 44, 46 of the worm thread must be displaceable relative to each other.
  • the frame members 12 are fixed to the frame and the wing members 14 are fixed to the wing in the approximately correct positions. Then, with the aid of one of the fitting arrangements 10, an adjustment of the position of the wing in the frame is made. Due to the play X, the respective frame parts 12 and wing parts 14 can move freely relative to each other, so that the other fitting arrangement not loaded in this state 10 does not hinder the adjustment.
  • the fitting assembly 10 used in the adjustment carries in this state, the wing alone. Once the wing is properly positioned in the frame, the longitudinal adjustment mechanism 42 of the previously unstressed fitting assembly 10 is actuated until its shoulder 54 abuts the protrusions 56 of the members 28, 30. From then also this fitting assembly 10 provides a supporting effect, without the adjustment itself - ie in the position correction of the wing - to have been used.
  • Fig. 7 illustrates the geometry of the tab 22, since the carriage 36 is not shown.
  • the carriage 36 ultimately serves as an intermediate element for implementing a rotational movement of the adjusting shaft 48 in a translational movement, which is transmitted to the movable perpendicular thereto by the Querjust istsmechanismus 50 tab 22.
  • Fig. 8 shows a section through the fitting assembly 10 in a plane perpendicular to the pivot axis.
  • the fitting assembly 10 is shown in a closed condition of the wing.
  • the fitting assembly 10 is a concealed fitting.

Landscapes

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

Claims (5)

  1. Ensemble de ferrure pour un battant d'une fenêtre, d'une porte ou similaires, comportant une partie de battant (14) réalisée pour le montage sur le battant et une partie de cadre (12) réalisée pour le montage 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, et la partie de cadre (12) et la partie de battant (14) étant mobiles l'une par rapport à l'autre dans une direction 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
    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,
    le mécanisme d'ajustement longitudinal (42) coopère avec un chariot (36), la partie de cadre (12) et/ou la partie de battant (14) sont mobiles par rapport au chariot (36), 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),
    le mécanisme d'ajustement longitudinal (42) comprend un engrenage à vis sans fin (44, 46) en particulier autobloquant pourvu d'une vis sans fin (44) qui est agencée sur un élément d'ajustement (18) actionnable à des fins d'ajustement et dans laquelle vient s'engager une roue dentée (46) qui est agencée sur un arbre d'ajustement (48) monté mobile en rotation,
    l'arbre d'ajustement (48) est susceptible d'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),
    un axe de rotation de l'arbre d'ajustement (48) est agencé parallèlement à l'axe de basculement,
    l'arbre d'ajustement (48) coopère avec le chariot (36) par un pas de vis (49a, 49b),
    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 formant talon (56) prévu sur l'élément de base (28), et
    dans un état non chargé de l'ensemble de ferrure, l'arbre d'ajustement (48) est déplaçable par rapport à l'élément de base (28) dans une direction parallèle à l'axe de basculement.
  2. Ensemble de ferrure selon la revendication 1,
    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.
  3. Ensemble de ferrure selon l'une au moins des revendications précédentes,
    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.
  4. Ensemble de ferrure selon la revendication 3,
    caractérisé 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).
  5. Ensemble de ferrure selon l'une au moins des revendications précédentes,
    caractérisé en ce que
    l'unité d'ajustement est agencée sur la partie de battant (14).
EP12190635.8A 2011-11-03 2012-10-30 Agencement de ferrure Active EP2589734B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL12190635T PL2589734T3 (pl) 2011-11-03 2012-10-30 Zestaw montażowy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE202011107504U DE202011107504U1 (de) 2011-11-03 2011-11-03 Beschlaganordnung

Publications (3)

Publication Number Publication Date
EP2589734A2 EP2589734A2 (fr) 2013-05-08
EP2589734A3 EP2589734A3 (fr) 2016-05-11
EP2589734B1 true EP2589734B1 (fr) 2019-07-17

Family

ID=47143623

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12190635.8A Active EP2589734B1 (fr) 2011-11-03 2012-10-30 Agencement de ferrure

Country Status (3)

Country Link
EP (1) EP2589734B1 (fr)
DE (1) DE202011107504U1 (fr)
PL (1) PL2589734T3 (fr)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5694665A (en) * 1996-03-15 1997-12-09 The Stanley Works Adjustable hinge
SE529138C2 (sv) * 2004-02-09 2007-05-08 Assa Ab Gångled
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

Non-Patent Citations (1)

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

Also Published As

Publication number Publication date
DE202011107504U1 (de) 2013-02-04
EP2589734A3 (fr) 2016-05-11
PL2589734T3 (pl) 2020-03-31
EP2589734A2 (fr) 2013-05-08

Similar Documents

Publication Publication Date Title
EP2430273B1 (fr) Entraînement de volet de meuble, pouvant pivoter
EP3613931B1 (fr) Module de bande destiné au raccordement mobile par charnière autour d'un axe de charnière d'un battant sur un cadre
DE102007054476B4 (de) Kulissenanordnung
EP3277899B1 (fr) Système de poignée de porte d'un véhicule automobile
DE60315128T2 (de) Verstellbares Scharnier für Fenster oder Türen
EP2503084A1 (fr) Charnière réglable
DE19642637C2 (de) Türscharnier zur schwenkbaren Lagerung eines Türflügels an einem Türrahmen
EP2589734B1 (fr) Agencement de ferrure
DE102019200066A1 (de) Lukenanordnung für ein Freizeitfahrzeug
EP2589735B1 (fr) Agencement de ferrure
EP1793067B1 (fr) Ferrure pour portes, fenêtres ou similaires
WO2007014604A1 (fr) Systeme a profile et a bande
EP3755858B1 (fr) Charnière et procédé pour le réglage d'une charnière
DE202020002389U1 (de) Kammschanier für Fenster und Türen mit drehbarem Blatt
EP0467122A1 (fr) Douille pour broches de ferrures ou charnières
EP3278693B1 (fr) Ferrure de porte coulissante
EP1422371B1 (fr) Charnière pour portes, fenêtres ou similaires
EP2304146B1 (fr) Dispositif d'orientation pour une fenetre, une porte ou similaire
EP2374973B1 (fr) Bande pour portes, fenêtres ou analogues
EP3461666B1 (fr) Dispositif de palier doté d'une roue de commande et aérateur comportant un tel dispositif de palier
EP1747338B1 (fr) Ferrure de charniere pour une porte de vehicule a moteur
WO2007028490A1 (fr) Charniere pour portes, fenetres ou elements similaires
DE102019134407A1 (de) Beschlaganordnung
DE102006062620A1 (de) Stellmechanismus für einen Sonnenschirm
DE202004012085U1 (de) Scharnierbeschlag für eine Kfz-Tür

Legal Events

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

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

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

AX Request for extension of the european patent

Extension state: BA ME

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

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

AX Request for extension of the european patent

Extension state: BA ME

RIC1 Information provided on ipc code assigned before grant

Ipc: E05D 7/04 20060101AFI20160404BHEP

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20161111

RBV Designated contracting states (corrected)

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

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

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20180504

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20190125

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

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

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502012015032

Country of ref document: DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1155976

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190815

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20190717

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

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

Ref country code: LT

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

Effective date: 20190717

Ref country code: FI

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

Effective date: 20190717

Ref country code: PT

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

Effective date: 20191118

Ref country code: NL

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

Effective date: 20190717

Ref country code: BG

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

Effective date: 20191017

Ref country code: NO

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

Effective date: 20191017

Ref country code: SE

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

Effective date: 20190717

Ref country code: HR

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

Effective date: 20190717

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

Ref country code: IS

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

Effective date: 20191117

Ref country code: RS

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

Effective date: 20190717

Ref country code: GR

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

Effective date: 20191018

Ref country code: AL

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

Effective date: 20190717

Ref country code: LV

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

Effective date: 20190717

Ref country code: ES

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

Effective date: 20190717

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

Ref country code: TR

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

Effective date: 20190717

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

Ref country code: DK

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

Effective date: 20190717

Ref country code: EE

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

Effective date: 20190717

Ref country code: RO

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

Effective date: 20190717

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

Ref country code: IS

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

Effective date: 20200224

Ref country code: SM

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

Effective date: 20190717

Ref country code: SK

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

Effective date: 20190717

Ref country code: MC

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

Effective date: 20190717

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502012015032

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

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

PG2D Information on lapse in contracting state deleted

Ref country code: IS

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

Ref country code: LI

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

Effective date: 20191031

Ref country code: CH

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

Effective date: 20191031

Ref country code: LU

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

Effective date: 20191030

26N No opposition filed

Effective date: 20200603

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20191031

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

Ref country code: SI

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

Effective date: 20190717

Ref country code: BE

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

Effective date: 20191031

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

Ref country code: IE

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

Effective date: 20191030

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

Ref country code: CY

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

Effective date: 20190717

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

Ref country code: HU

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

Effective date: 20121030

Ref country code: MT

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

Effective date: 20190717

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

Ref country code: MK

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

Effective date: 20190717

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

Ref country code: GB

Payment date: 20231020

Year of fee payment: 12

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

Ref country code: IT

Payment date: 20231026

Year of fee payment: 12

Ref country code: FR

Payment date: 20231025

Year of fee payment: 12

Ref country code: DE

Payment date: 20231020

Year of fee payment: 12

Ref country code: CZ

Payment date: 20231023

Year of fee payment: 12

Ref country code: AT

Payment date: 20231020

Year of fee payment: 12

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

Ref country code: PL

Payment date: 20231019

Year of fee payment: 12