EP0460422B1 - Palier à pivot, en particulier pour ailes de fenêtres, portes ou similaires - Google Patents

Palier à pivot, en particulier pour ailes de fenêtres, portes ou similaires Download PDF

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Publication number
EP0460422B1
EP0460422B1 EP91107606A EP91107606A EP0460422B1 EP 0460422 B1 EP0460422 B1 EP 0460422B1 EP 91107606 A EP91107606 A EP 91107606A EP 91107606 A EP91107606 A EP 91107606A EP 0460422 B1 EP0460422 B1 EP 0460422B1
Authority
EP
European Patent Office
Prior art keywords
support arm
wing
panel
pivot
drive member
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP91107606A
Other languages
German (de)
English (en)
Other versions
EP0460422A1 (fr
Inventor
Achim Türk
Horst Loos
Michael Zimmermann
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.)
Siegenia Aubi KG
Original Assignee
Siegenia Frank KG
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 Siegenia Frank KG filed Critical Siegenia Frank KG
Priority to AT91107606T priority Critical patent/ATE97714T1/de
Publication of EP0460422A1 publication Critical patent/EP0460422A1/fr
Application granted granted Critical
Publication of EP0460422B1 publication Critical patent/EP0460422B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00Hinges or pivots of special construction
    • E05D7/08Hinges or pivots of special construction for use in suspensions comprising two spigots placed at opposite edges of the wing, especially at the top and the bottom, e.g. trunnions
    • E05D7/081Hinges or pivots of special construction for use in suspensions comprising two spigots placed at opposite edges of the wing, especially at the top and the bottom, e.g. trunnions the pivot axis of the wing being situated near one edge of the wing, especially at the top and bottom, e.g. trunnions
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00Hinges or pivots of special construction
    • E05D7/04Hinges adjustable relative to the wing or the frame
    • E05D7/0415Hinges adjustable relative to the wing or the frame with adjusting drive means
    • E05D7/0423Screw-and-nut mechanisms
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00Hinges or pivots of special construction
    • E05D7/04Hinges adjustable relative to the wing or the frame
    • E05D2007/0469Hinges adjustable relative to the wing or the frame in an axial direction
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00Hinges or pivots of special construction
    • E05D7/04Hinges adjustable relative to the wing or the frame
    • E05D2007/0484Hinges adjustable relative to the wing or the frame in a radial direction
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING 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
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/132Doors
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING 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
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/148Windows

Definitions

  • the invention relates to a pivot bearing, in particular for the sash of windows, doors or the like, which is installed between the circumferential surfaces directed transversely to the sash and frame level, primarily the sash and frame rebate circumferential surfaces, consisting of one in a plane transverse to the axial direction of a pivot joint extending wing rail and a frame part, between which the pivot joint is provided, wherein, in the assembled state of the bearing, the wing parallel to its plane, relative to the pivot joint, by means of one hand on the wing rail and on the other hand on one Joint part attacking actuator, for example a screw, can be adjusted to a limited extent, the joint part being formed by a support arm which is arranged between the wing rail and the frame part and is adjustable in its longitudinal direction and which extends via a further actuator also transversely to its longitudinal direction in a direction transverse to the axial direction of the pivot joint Level is displaceable in connection with the wing rail.
  • a pivot bearing in particular for the sash of windows, doors
  • a pivot locator of this type is known from US-A-2 530 331.
  • the support arm here is pivotally engaged in the immediate vicinity of the pivot joint with the wing rail and engages at its end remote from the pivot joint with the actuator mounted on the wing.
  • the invention aims to create a pivot bearing of the type mentioned at the beginning , which combines at least two different adjustment options for the sash in itself with little additional effort and, in the opening position of the sash, allows simple and reliable actuation, in which the different directions of action of the actuators to influence the relative position of the sash rail and frame part relative to one another are of a sufficient magnitude lets use.
  • a pivot bearing which takes these demands and wishes into account, but nevertheless has a simple design in terms of production technology, is characterized according to the invention essentially by that the support arm arranged on the frame part, which consists of a frame rail, on the one hand, with its end remote from the pivot joint, engages in a pivotable manner on an axis which - via a slide or the like - can be moved longitudinally along the wing rail by means of the actuator, for example a screw, while it on the other hand, is supported at a point located between the pivot joint and the swivel bearing axis via the further actuator on the wing rail.
  • the actuator for example a screw
  • the frame part of the pivot bearing can be formed, for example, by a frame rail.
  • the invention provides on the one hand that the further actuator is provided between the wing rail and the support arm with direction of action transversely to the pivot bearing axis or parallel to the pivot plane of the support arm, so that it enables the position adjustment of the wing relative to the support arm normal to its plane.
  • the further actuator between the wing rail and the support arm can also be arranged with an effective direction parallel to the pivot bearing axis or transversely to the pivot plane of the support arm, which then enables position adjustment of the wing in its plane, but in a direction perpendicular to the first adjustment direction.
  • the three-dimensional adjustment possibility for a trunnion bearing according to the invention only presupposes that the above-described further actuators, which are provided individually, are used jointly or simultaneously.
  • the - the wing adjustment transverse to its plane - further actuator consist of a stiffly rotatably mounted eccentric, which sits on the wing rail or the support arm and engages in a longitudinal slot of the support arm or the wing rail, the eccentric on it the frame rail facing end face a tool engagement, z. B. has a hexagon to its rotary adjustment, which is accessible in the open position of the wing.
  • the - the vertical adjustment of the wing parallel to its plane - other actuator can attack according to the invention on a transverse to the pivot plane of the support arm on the wing rail pressure piece on the support arm, advantageously in such a way that the further actuator is formed by a pressure screw and the pressure piece consists of a slide.
  • the pressure screw is advantageously screw-displaceably accommodated in a nut arranged in a fixed manner on the wing rail and engages at the end facing it of the slide which is held and guided by a collar bolt on the wing rail.
  • a screw only rotatably in a fixed abutment on the wing rail and to have it engage in a thread on the end of the slide which is held and guided on the wing rail and faces it.
  • At least the wing rail is designed as an angle rail, on one leg of which the further actuator for displacing the support arm is arranged in its pivoting plane, while on the other leg the actuator for displacing the support arm is transverse to its swivel plane.
  • a particularly high utility value of the pivot bearing results according to the invention by their assignment to a multi-leaf window without an intermediate post in the frame, such that the bearing axis formed by two mirror-inverted pivot bearings and parallel to the spar of the wing they carry conceals along the one carrying a locking device - overlapping - the spar of the neighboring wing runs and is preferably about the same with its peripheral circumferential surface on one level.
  • a multi-wing window 1 designed as a three-wing window, which comprises the fixed frame 2 and two side wings 3 and 4 and a middle wing 5.
  • the fixed frame 2 is designed without vertical intermediate posts. When in the closed position on the fixed frame 1 sashes 3, 4 and 5 therefore their mutually adjacent, upright wing spars 6 and 7 or 8 and 9 interact directly to bring about the tight closure of the multi-sash window 1 at the relevant points.
  • the upright wing spars 6 and 7 of the left side wing 3 and the middle wing 5 are assigned to each other, while on the other hand the upright wing spars 8 and 9 of the middle wing 5 and of the right side wing 4 come into direct connection with one another.
  • the left side wing 3 and the right side wing 4 of the multi-sash window 1 are each designed as so-called sash sashes, each of which carries a so-called impact bar 22 or 23 on its upright wing spars 6 and 9, respectively, with which they engage on the upright wing spars 7 and 8 of the middle wing 5 come to the sealing pad. Consequently, the middle wing 5 is designed in relation to the two side wings 3 and 4 as a so-called underlapping wing.
  • All of the sashes 3 to 5 of the multi-sash window 1 can be attached to the fixed frame 2 as pure rotating sashes.
  • the side wings 3 and 4 of the multi-wing window 1 can also be attached to the fixed frame 2 as so-called tilt and turn sashes.
  • the middle wing 5 is only ever provided as a pure rotating wing.
  • the middle wing 5 interacts with the horizontal frame spars 20 and 21 of the fixed frame 2, each via pivot bearings 24 and 25, which in the embodiment according to FIG. 1 in the area of the upright wing spar 7 is hidden between the folded peripheral surfaces of the fixed frame 1 and the left side wing 3 and of the middle wing 5 are housed.
  • pivot bearings 24 and 25 adjacent to the upright wing spar 8 of the middle wing 5 between the folded peripheral surfaces of the fixed frame 2 and the middle wing 5 and the right side wing 4.
  • FIG. 2 The structure and mode of operation of the pivot bearing 24 are shown in FIG. 2, while the structure and mode of operation of the pivot bearing 25 are shown in FIG. 3 of the drawing.
  • the - upper - pivot bearing 24 shown in FIG. 2 is fastened, for example screwed, by means of a frame rail 26 to the fold circumferential surface 27 of the upper, horizontal frame spar 20 oriented transversely to the frame plane of the fixed frame 2.
  • a wing rail 28 strikes the middle wing 5 at least on the peripheral circumferential surface 29 of the upper, horizontal wing spar 16.
  • the wing rail 28 is preferably designed as an angle rail 28a / 28b and is also fastened to the upright wing spar 7 of the middle wing 5 with the rebate peripheral surface 30.
  • the leg 28a of the angle rail 28a / 28b bears against the circumferential surface 29 of the fold and the leg 28b bears against the circumferential surface 30 of the middle wing 5.
  • a support arm 31 is provided, which is at its one end 32 via a pin joint 33 with the frame rail 26 in a pivotally movable connection.
  • the pin joint 33 is directed transversely to the plane of the frame rail 26 and also transversely to the plane of the leg 28a of the wing rail 28, the main plane of the support arm 31 extending transversely to the axial direction of the pin joint 33.
  • the support arm 31 is connected to the wing rail 28, specifically with its horizontal leg 28a, and thereby forms the actual joint part of the pivot bearing 24.
  • the releasable connection between the leg 28a of the wing rail 28 and the support arm 31 are useful two bolts 34 and 35, which are each seated on the leg 28a of the wing rail 28 as shown in FIG. 2 and are brought into releasable engagement with openings 36 and 37 in the support arm 31, respectively can.
  • the opening 36 has - according to the additional illustration (A) of FIG. 2 - an approximately circularly limited
  • the bolt 34 has a matching head part 40 with a circularly delimited area 41 and a subsequent radial nose 42, as can be seen in the additional sketch (B) for FIG. 2.
  • the opening 37 in the support arm 31 has the shape of a longitudinal slot, while the bolt 35 that comes into engagement therewith has a circularly delimited head part 43, which adjoins its shaft 44 eccentrically.
  • the bolt 35 is rotatably mounted in the leg 28a of the wing rail 28 and has a tool engagement 45, for example a hexagon socket, on the end for its actuation.
  • a tool engagement 45 for example a hexagon socket
  • the support arm 31 can be moved with the wing rail 28 simply by a displacement movement transverse to it Engage and disengage the plane. To secure the engagement connection, it is only necessary to turn the bolt 34 to such an extent that the radial nose 42 of its head part 40 reaches the area of the radial expansion slot 39 in the opening 36 of the support arm 31.
  • the bolt 34 is located on the leg 28a of the wing rail 28, it is seated on a carriage 46 which is guided in a longitudinally sliding manner on the underside of the leg 28a of the wing rail 28.
  • the pin 34 extends through a longitudinal slot 47 in the leg 28a of the wing rail 28, which is also useful for the sliding guide of the slide 46.
  • the carriage 46 is received by a groove 48, as is usually provided on window or door sashes for receiving espagnolette fittings.
  • the carriage 46 contains in its end facing the corner region of the wing rail 28 an internal thread 49 which extends parallel to its sliding direction and with which the shaft 50 is engaged by a screw 51 which, although rotatable but non-displaceably anchored in the longitudinal direction, is anchored to the wing rail 28.
  • the screw 51 has a tool engagement 52, for example a hexagon socket, which is accessible through a hole 53 in the leg 28b of the wing rail 28.
  • a tool engagement 52 for example a hexagon socket
  • the slide 46 By turning the screw 51 by means of an actuating tool, for example a hexagon socket wrench, the slide 46 can be moved longitudinally on the underside of the leg 28a of the wing rail 28. In this way it is therefore possible to continuously adjust the central wing 5 parallel to its plane relative to the pivot joint 33 to an extent limited by the longitudinal slot 47. Depending on the extent of the adjustment, the eccentric head part 43 of the bolt 35 can move freely in the opening 37 in the form of an elongated hole in the support arm 31.
  • an actuating tool for example a hexagon socket wrench
  • the middle wing 5 can also be adjusted in the direction transverse to its plane relative to the support arm 31, namely over an area which corresponds in its extent to twice the eccentricity 54 as it is indicated in the additional sketch (C) for FIG. 2.
  • the rotation of the bolt 35 results in an angular displacement of the support arm 31 relative to the leg 28a of the wing rail 28, specifically around the bolt 34.
  • the lower pivot bearing 25 according to FIG. 1 largely corresponds in structure and mode of operation to the upper pivot bearing 24 already explained with reference to FIG. 2. Therefore, in FIG. 3, for the sake of simplicity, reference numerals have been used for the corresponding components and functional parts, each of which has tens of digits higher than the reference numerals of FIG. 2.
  • the pivot bearing 25 has a frame rail 56 which is fastened to the circumferential surface 57 of the horizontal frame spar 21.
  • wing rail 58 with the legs 58a and 58b, which is fastened to the wing rebate peripheral surfaces 59 and 60, and the support arm 61, which acts as a joint part which connects the wing rail 58 to the frame rail 56 via the pivot joint 63.
  • the support arm 61 has a higher dimensional stability or material thickness than the support arm 31 of the upper pivot bearing 24 according to FIG. 2
  • pivot bearing 25 What is different about the pivot bearing 25 is also that the pivot joint 63 between the support arm 61 and the frame rail 56 has a pivot pin 69 with which the support arm 61 is in a detachable or extractable plug connection. A correspondingly extractable or uncouplable plug connection is also provided between the bolt 64 of the slide 76 and the opening 66 in the support arm 61. The engagement or holding connection at these points is maintained by the weight of the center wing 5.
  • the longitudinal adjustment between the wing rail 58 and the support arm 61 i.e. the position adjustment of the middle wing 5 parallel to its plane, is carried out in the lower pivot bearing 25 in the same manner as in the upper pivot bearing 24, namely with the aid of the thread 79 on the slide 76 about your Screw 80 engaging screw 81, which is held and supported on the rear of the leg 58a of the wing rail 58 by the bearing eye 58c.
  • the bolt 65 with its head part 73 eccentric to the shaft 74 is also suitable for adjusting the position of the middle wing 5 transversely to its plane relative to the support arm 61.
  • the bolt 65 on the end face of its head part 73 is equipped with the tool engagement 75, for example a hexagon socket.
  • pivot bearing 25 according to FIG. 3 is equipped with a third adjustment option for the center wing 5 carried by it.
  • This third adjustment option extends parallel to the main plane of the center wing 5 and is effective in the vertical direction, that is, at a right angle to the longitudinal adjustment between the wing rail 58 and the support arm 61 that can be achieved by means of the screw 81.
  • a further actuator for exercising the third adjustment option is a thrust piece 86 which can be adjusted transversely to the pivoting plane of the support arm 61 on the vertical leg 58b of the angular wing rail 58, the lower end 87 of which simply sits on the upper side of the support arm 61.
  • a pressure screw 89 acts on the upper end of the pressure piece 86, which is designed as a slide, and is screwingly axially displaceably received in a nut 90 arranged in a fixed manner on the vertical leg 58b of the wing rail 58.
  • the pressure screw 89 In its head, the pressure screw 89 has a tool engagement 91, for example a hexagon socket, which is accessible with a socket wrench and thereby enables the pressure screw 89 to be turned.
  • the slide forming the pressure piece 86 is held and guided via a collar bolt 92 on the vertical leg 58b of the wing rail 58, which extends through a longitudinal slot 93 in the pressure piece 86.
  • the longitudinal slot 93 is designed or provided so that it allows the insertion of a socket wrench through the hole 83 of the wing rail 58 into the tool engagement 82 of the screw 81 at any time.
  • the pressure screw 89 and the pressure piece 86 are provided such that they act on the support arm 61 with the direction of action parallel to the pivot bearing axis of the Actuate the pin joint 63 or transversely to the pivoting plane of the support arm 61.
  • the bearing axis 94-94 formed jointly by the two pivot bearings 24 and 25, which are essentially mirror images of one another, extends parallel to the spar 7 of the center wing 5 carried by them, so that they are concealed along the spar-bearing spar 6 which carries a locking device left side wing 3 runs.
  • the aim is for the bearing axis 94-94 to lie approximately on a plane with the fold peripheral surface 95 on the spar 6 of the side wing 3, as can be seen in FIGS. 2 and 3 of the drawing.
  • pivot bearings 24 and 25 described above are preferably suitable for use in the middle sash of multi-leaf windows and doors or the like, in which the fixed frame is designed without intermediate posts, they can also be used in other cases. For example, it would be conceivable to use these pivot bearings 24 and 25 also in windows and doors that are equipped with sashes arranged flush in the fixed frame without a rollover.
  • Unwanted lifting of the middle wing 5 out of the pivot joint 63 of the lower pivot bearing 25 can be prevented in various ways.
  • the upper pivot bearing 24 can also have a design which corresponds completely to the lower pivot bearing 25. If both thrust pieces 86 are then set against the support arms 31 and 61 by means of the screws 89, there is a positive locking block because the support arms 31 and 61 are in turn supported on the associated frame rails 26 and 56.
  • the pivot bearings 24 and 25 can also be modified insofar as their frame rail 26 or 56 can be provided on the back in extension of the pivot joint 33 or 63 with a support bolt which can be inserted into a frame bore.
  • the frame rail 26 or 56 can then be attached symmetrically to the support bolt by a screw on the frame rebate circumferential surface 27 or 57.
  • the support arm 31 can be designed or clamped so that it can come into engagement with the bolts 35 and 34 of the wing rail 28 during the hanging process for the middle wing 5 by a snap-locking effect.
  • the bolt 35 comes into engagement at the front end of the elongated opening 37.
  • the middle wing 5 can then be displaced in the direction of its plane towards the pivot joint 33 until the bolt 34 also automatically engages in the opening 36.
  • both pivot bearings 24 and 25 are equipped with thrust piece 86 and thrust screw 89, then the height of the middle wing 5 relative to the fixed frame 2 can, if necessary, be adjusted in two opposite directions, namely upwards and downwards.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Wing Frames And Configurations (AREA)

Claims (10)

  1. Un coussinet de pivot (24; 25) qui est destiné en particulier aux vantaux (5) de fenêtres (1), portes ou pièces analogues, s'encastre de manière non apparente entre les surfaces de délimitation orientées transversalement par rapport au plan du vantail et de l'encadrement, de préférence entre les surfaces périphériques de feuillure du vantail et de l'encadrement, et se compose, d'une part, d'un rail de vantail (28; 58) s'étendant dans un plan perpendiculaire à la direction axiale d'une articulation de pivot (33; 63) et, d'autre part, d'un élément d'encadrement (26; 56), entre lesquels cette articulation de pivot (33; 63) est installé, étant entendu, d'une part, qu'au moment où le pivot est en position montée, le vantail (5) peut être ajusté de manière limitée, parallèlement à son plan et par rapport à l'articulation de pivot (33; 63), grâce à un élément de réglage (50, 51; 51, 81), par exemple une vis, engagée dans le rail de vantail (28; 58) ainsi que, par ailleurs, dans un élément d'articulation (31; 61), et, d'autre part, que ce dernier élément d'articulation (31; 61) est constitué d'un bras de support (31 ou 61) qui est disposé entre le rail de vantail (28 ou 58) et l'élément d'encadrement (26 ou 56), peut être réglé dans le sens de sa longueur et est relié au rail de vantail (28 ou 58) par l'intermédiaire d'un autre élément de réglage (35 ou 65), de manière à pouvoir être également décalé, dans une mesure limitée, perpendiculairement à son sens longitudinal, dans un plan qui s'étend transversalement à la direction axiale de l'articulation de pivot,
    ce coussinet de pivot étant caractérisé
    par le fait que, d'une part, le bras de support (31 ou 61) installé sur l'élément d'encadrement consistant en un rail d'encadrement s'articule, par son extrémité opposée à l'articulation de pivot (33 ou 63) et de manière à pouvoir opérer un mouvement de pivotement, avec un axe (34 ou 64) susceptible, grâce à un élément de réglage (50, 51 ou 80, 81) tel qu'une vis, de coulisser longitudinalement le long du rail d e vantail (28 ou 58) par le biais d'un glissoir (46 ou 76) ou autre pièce similaire, tandis que, d'autre part, ce bras de support (31 ou 61) s'appuie, par l'intermédiaire de l'élément de réglage complémentaire (35 ou 65), contre le rail de vantail (28 ou 58) en un emplacement situé entre l'articulation de pivot (33 ou 63) et l'axe du coussinet de pivotement (34 ou 64).
  2. Un coussinet de pivotement conforme à la revendication 1,
    caractérisé
    par le fait que l'élément de réglage complémentaire (35 ou 63), située entre le rail de vantail (28 ou 58) et le bras de support (31 ou 61), est prévu avec un sens de fonctionnement perpendiculaire à l'axe du coussinet de pivotement (94-94) ou, en d'autres termes, parallèle au plan de pivotement du bras de support (31 ou 61).
  3. Un coussinet de pivotement conforme à l'une des revendications 1 et 2,
    caractérisé
    par le fait que l'élément de réglage complémentaire (86, 89), situé entre le rail de vantail (58) et le bras de support (61) est disposé avec un sens de fonctionnement parallèle à l'axe de pivotement (94-94) ou, en d'autres termes, parallèle au plan de pivotement du bras de support (61).
  4. Un coussinet de pivotement conforme à la revendication 3,
    caractérisé
    par le fait que l'élément de réglage complémentaire (86, 89) est prévu en supplément comme troisième élément de réglage.
  5. Un coussinet de pivotement conforme à l'une des revendications 1 et 2,
    caractérisé
    par le fait que l'élément de réglage complémentaire (35 ou 65) consiste en un excentrique (43, 44, 54 ou 73, 74) qui est logé d e manière à pouvoir subir une torsion dure, repose sur le rail de vantail (28 ou 58) ou sur le bras de support (31 ou 61) et s'emboîte dans une rainure longitudinale (37 ou 67) du bras de support (31 ou 61) ou du rail de vantail (28 ou 58), cet excentrique (43, 44, 54 ou 73, 74) présentant sur sa surface frontale orientée vers le rail d'encadrement (26 ou 56) une prise pour outil (45 ou 75), par exemple une prise à six pans creux, qui permette de le régler par rotation.
  6. Un coussinet de pivotement conforme à l'une des revendications 1 à 4,
    caractérisé
    par le fait que l'élément de réglage complémentaire (86, 89) s'articule avec le bras de support (61) par l'intermédiaire d'un élément de pression (86) mené contre le rail de vantail (58) perpendiculairement au plan de pivotement du bras de support (61).
  7. Un coussinet de pivotement conforme à la revendication 6,
    caractérisé
    par le fait que l'élément de réglage complémentaire (86, 89) est formé par une vis de pression (89), tandis que l'élément de pression (86) consiste en un coulisseau.
  8. Un coussinet de pivotement conforme à l'une des revendications 6 et 7,
    caractérisé
    par le fait que la vis de pression (89) se loge, de manière à pouvoir être décalée par vissage, dans un écrou (90) installé de manière fixe sur le rail de vantail (58) et pénètre dans l'extrémité (88), orientée vers elle, du coulisseau qu'un boulon à collerette maintient et guide contre le rail de vantail (58).
  9. Un coussinet de pivotement conforme à l'une des revendications 1 à 8,
    caractérisé
    par le fait que le rail de vantail (28 ou 58) au moins a reçu la forme d'un rail coudé (28a/28b ou 58a/58b), dont l'une des branches (28a ou 58a) a été dotée de l'élément de réglage supplémentaire (35 ou 65) destiné à déplacer le bras de support (31 ou 61) dans son plan de pivotement, tandis que le troisième élément de réglage (86, 89), destiné à déplacer le bras de support (61) perpendiculairement à son plan de pivotement, se trouve sur l'autre branche (58b) de ce rail coudé (28a/28b ou 58a/58b).
  10. Un coussinet de pivotement conforme à l'une des revendications 1 à 9,
    caractérisé
    par le fait que dans une fenêtre possédant plusieurs vantaux (1) et dotée d'un encadrement dépourvu de jambage intermédiaire, ces coussinets de pivotement soient montés d'une manière telle que l'axe de pivotement (94-94) qui est formé par deux coussinets de pivotement (24 et 25) installés à peu près symétriquement l'un par rapport à l'autre et s'étend parallèlement au montant (7) du vantail (5) supporté par la fenêtre (1) passe de manière masquée le long du montant (6) recouvrant faisant partie du vantail voisin (3) et portant un dispositif de fermeture et soit de préférence situé sur le même plan que la surface périphérique de feuillure (95) de ce vantail voisin (3) (fig. 2 et 3).
EP91107606A 1990-06-08 1991-05-10 Palier à pivot, en particulier pour ailes de fenêtres, portes ou similaires Expired - Lifetime EP0460422B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT91107606T ATE97714T1 (de) 1990-06-08 1991-05-10 Drehzapfenlager, insbesondere fuer die fluegel von fenstern, tueren od. dgl.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4018345A DE4018345A1 (de) 1990-06-08 1990-06-08 Drehzapfenlager, insbesondere fuer die fluegel von fenstern, tueren o. dgl.
DE4018345 1990-06-08

Publications (2)

Publication Number Publication Date
EP0460422A1 EP0460422A1 (fr) 1991-12-11
EP0460422B1 true EP0460422B1 (fr) 1993-11-24

Family

ID=6408018

Family Applications (1)

Application Number Title Priority Date Filing Date
EP91107606A Expired - Lifetime EP0460422B1 (fr) 1990-06-08 1991-05-10 Palier à pivot, en particulier pour ailes de fenêtres, portes ou similaires

Country Status (3)

Country Link
EP (1) EP0460422B1 (fr)
AT (1) ATE97714T1 (fr)
DE (2) DE4018345A1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE9301655U1 (de) * 1993-02-06 1994-06-09 Siegenia-Frank Kg, 57074 Siegen Scharnierbeschlag
DE29707358U1 (de) 1997-04-23 1998-08-27 Ferco International Ferrures et Serrures de Bâtiment S.A., Reding Beschlag mit Tragarm oder Ausstellarm zur Lagerung eines Drehflügels oder Dreh-Kippflügels
DE29907934U1 (de) * 1999-05-04 2000-09-14 Ferco International Ferrures et Serrures de Bâtiment, Reding Beschlag zur Drehlagerung eines Fenster- oder Türflügels
DE20318250U1 (de) * 2003-11-24 2004-02-12 Siegenia-Aubi Kg Drehzapfenlager

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT189957B (de) * 1955-01-20 1957-05-25 Beschlag für mehrflügelige Fenster, Türen od. dgl.

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE253202C (fr) *
DE489535C (de) * 1930-01-20 August Armbrust Zapfenband, insbesondere fuer Schranktueren
GB593949A (en) * 1945-07-16 1947-10-29 Arthur Edward King Improvements in or connected with hinges
DE292183C (fr) *
US2530331A (en) * 1948-07-14 1950-11-14 Shelby Spring Hinge Co Adjustable hinge mechanism
GB1014354A (en) * 1963-06-17 1965-12-22 Tonks Birmingham Ltd Means for connecting a door to a door closer
DE8106122U1 (de) * 1981-03-04 1981-07-30 Bosch-Siemens Hausgeräte GmbH, 7000 Stuttgart Tuerlager, insbesondere spurzapfenlager fuer tueren von kuehl- und gefrierschraenken

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT189957B (de) * 1955-01-20 1957-05-25 Beschlag für mehrflügelige Fenster, Türen od. dgl.

Also Published As

Publication number Publication date
EP0460422A1 (fr) 1991-12-11
ATE97714T1 (de) 1993-12-15
DE59100630D1 (de) 1994-01-05
DE4018345A1 (de) 1991-12-19

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