EP2589735A2 - Agencement de ferrure - Google Patents

Agencement de ferrure Download PDF

Info

Publication number
EP2589735A2
EP2589735A2 EP12190894.1A EP12190894A EP2589735A2 EP 2589735 A2 EP2589735 A2 EP 2589735A2 EP 12190894 A EP12190894 A EP 12190894A EP 2589735 A2 EP2589735 A2 EP 2589735A2
Authority
EP
European Patent Office
Prior art keywords
fitting arrangement
wing
arrangement according
adjustment mechanism
carriage
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.)
Granted
Application number
EP12190894.1A
Other languages
German (de)
English (en)
Other versions
EP2589735A3 (fr
EP2589735B1 (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 EP16201126.6A priority Critical patent/EP3156573B1/fr
Publication of EP2589735A2 publication Critical patent/EP2589735A2/fr
Publication of EP2589735A3 publication Critical patent/EP2589735A3/fr
Application granted granted Critical
Publication of EP2589735B1 publication Critical patent/EP2589735B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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 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 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 member and the wing member 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 longitudinal adjustment mechanism has self-locking properties.
  • the longitudinal adjustment mechanism is designed such that the components involved only permit a change in the adjustment if this is carried out deliberately.
  • the forces occurring in the context of a conventional use thus cause no adjustment of the adjustment, so that a once performed adjustment is reliably maintained.
  • the adjustment unit has a transverse adjustment mechanism that is configured such that the frame part and the wing part are movable relative to each other for adjustment purposes in a direction perpendicular to the pivot axis, wherein the transverse adjustment mechanism in particular has self-locking properties.
  • the longitudinal adjustment mechanism can thus be provided a Querjustleitersmechanismus to adjust the fitting assembly not only parallel to the pivot axis but also perpendicular thereto.
  • Self-locking may be created by the use of suitable gears in the longitudinal adjustment mechanism and / or the lateral 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 - by a rotational movement of an adjusting element is effected.
  • An axis of rotation of the adjusting element can be arranged perpendicular to an adjustment movement effected by a rotation of the adjusting element.
  • the adjusting element may be non-rotatably connected to a worm, in which engages a rotatably connected to an adjusting shaft of the longitudinal adjustment mechanism or the Querjust istsmechanismus gear.
  • the adjusting unit is arranged on the frame part or the wing part and cooperates with a movable carriage for adjustment purposes, wherein the frame part and / or the wing part are movable relative to the carriage.
  • the carriage may be assigned to the frame part or the wing part, wherein the other part is associated with a tab which engages in the carriage.
  • the carriage cooperates with the Justierwelle, which in turn is rotatable with the aid of the adjusting element.
  • a thread can be provided to implement a rotational movement of the adjusting shaft in a translational movement of the carriage.
  • longitudinal adjustment mechanism and the transverse adjustment mechanism may be basically similar.
  • the carriage is movable in a direction parallel to the pivot axis.
  • the tab is arranged in a direction perpendicular to the pivot axis displaceable in a tab receptacle of the carriage.
  • the Querjust istsmechanismus can interact directly, in particular via a thread with the tab.
  • the slide can be arranged in a housing which has guide elements for guiding the slide. If that Housing the adjustment completely substantially covers, this is also protected against accidental or unauthorized manipulation and pollution.
  • the guide elements are in particular designed such 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 firmly connected to the frame or to the wing.
  • an assembly clearance is provided between an under loaded condition of the fitting assembly cooperating components of the base member and the longitudinal adjustment mechanism in an unloaded condition of the fitting assembly in a direction parallel to the pivot axis.
  • the mounting clearance determines a maximum relative offset between the frame part and the wing part.
  • This embodiment is particularly advantageous when multiple fitting arrangements are used for mounting a grand piano in a frame.
  • the problem arises that the individual fitting arrangements of conventional design must be adjusted in a complex iterative process, since an actuation of the directly interacting components of the respective adjustment mechanisms quickly lead to mechanical tension.
  • it is possible in a fitting arrangement of the type described above with mounting game first to attach a plurality of fitting assemblies on the wing and the frame and then position the wing accurately by means of 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 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 may comprise a rotatably mounted adjustment shaft which is drivable by an adjusting element or directly to a rotational movement in order to effect 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 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 load on the fitting arrangement is thus transmitted through the shoulder and the correspondingly formed attachment element from the wing part to the frame part.
  • 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, which receives the adjustment unit and, in particular, covers it substantially completely.
  • 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.
  • the adjusting unit is arranged on the wing part.
  • 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 of 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 plane and a plane spanned by the wing portion 14, according to below 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. Furthermore, the body 14a mounting holes 32, are guided by the fastening elements - for example screws - for fastening the wing part 14 on the wing can. 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 frame part 12 comprises only the mounting holes 32 having 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 provided with it in direct contact portions of the base portion 28 and the lid portion 30 with complementary surface structures that allow the said movement and reliably prevent the movements of the carriage 36 in other spatial 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 protrudes into an opening of the carriage 36.
  • the projecting into the carriage 36 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 existing of the worm 44 and the gear 46 worm gear a rotation of the adjusting shaft 48, which is converted via the aforementioned male / female 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.
  • 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 pivoting 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 part 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 the adjustment during use of the fitting arrangement - that is, by pivoting the frame or wing part - especially in connection with the longitudinal adjustment mechanism, it is sufficient in many cases, only to equip the latter with self-locking properties.
  • Fig. 6 shows a part of the longitudinal adjustment mechanism 42 in a detailed view.
  • 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 composed of the above-mentioned game X1 and a second game X2, which exists 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 one another, so that the other fitting arrangement 10 which is not loaded in this state 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 provides this fitting arrangement 10 a supporting 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 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)
  • Hinges (AREA)
  • Pinball Game Machines (AREA)
  • Door And Window Frames Mounted To Openings (AREA)
EP12190894.1A 2011-11-03 2012-10-31 Agencement de ferrure Active EP2589735B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP16201126.6A EP3156573B1 (fr) 2011-11-03 2012-10-31 Système d'armatures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE202011107495U DE202011107495U1 (de) 2011-11-03 2011-11-03 Beschlaganordnung

Related Child Applications (2)

Application Number Title Priority Date Filing Date
EP16201126.6A Division EP3156573B1 (fr) 2011-11-03 2012-10-31 Système d'armatures
EP16201126.6A Division-Into EP3156573B1 (fr) 2011-11-03 2012-10-31 Système d'armatures

Publications (3)

Publication Number Publication Date
EP2589735A2 true EP2589735A2 (fr) 2013-05-08
EP2589735A3 EP2589735A3 (fr) 2016-05-11
EP2589735B1 EP2589735B1 (fr) 2021-09-01

Family

ID=47143654

Family Applications (2)

Application Number Title Priority Date Filing Date
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

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP16201126.6A Active EP3156573B1 (fr) 2011-11-03 2012-10-31 Système d'armatures

Country Status (2)

Country Link
EP (2) EP3156573B1 (fr)
DE (1) DE202011107495U1 (fr)

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
CA2697693C (fr) * 2009-03-25 2018-01-02 Amesbury Group, Inc. Charniere de porte reglable

Non-Patent Citations (1)

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

Also Published As

Publication number Publication date
EP2589735A3 (fr) 2016-05-11
EP3156573A1 (fr) 2017-04-19
EP2589735B1 (fr) 2021-09-01
EP3156573B1 (fr) 2020-04-01
DE202011107495U1 (de) 2013-02-04

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