EP0851085B1 - Ferrure oscillo-battante avec support d'angle non-coulissant - Google Patents

Ferrure oscillo-battante avec support d'angle non-coulissant Download PDF

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Publication number
EP0851085B1
EP0851085B1 EP97123028A EP97123028A EP0851085B1 EP 0851085 B1 EP0851085 B1 EP 0851085B1 EP 97123028 A EP97123028 A EP 97123028A EP 97123028 A EP97123028 A EP 97123028A EP 0851085 B1 EP0851085 B1 EP 0851085B1
Authority
EP
European Patent Office
Prior art keywords
mounting
bearing
casement
comer
movement
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
EP97123028A
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German (de)
English (en)
Other versions
EP0851085A1 (fr
Inventor
Ernst Lahmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hautau GmbH
Original Assignee
Hautau GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hautau GmbH filed Critical Hautau GmbH
Priority to DE1998128670 priority Critical patent/DE19828670A1/de
Publication of EP0851085A1 publication Critical patent/EP0851085A1/fr
Application granted granted Critical
Publication of EP0851085B1 publication Critical patent/EP0851085B1/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
    • E05D15/00Suspension arrangements for wings
    • E05D15/48Suspension arrangements for wings allowing alternative movements
    • E05D15/52Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
    • E05D15/5211Concealed suspension fittings
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05FDEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F7/00Accessories for wings not provided for in other groups of this subclass
    • E05F7/06Devices for taking the weight of the wing, arranged away from the hinge axis
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/28Suspension arrangements for wings supported on arms movable in horizontal plane
    • E05D15/30Suspension arrangements for wings supported on arms movable in horizontal plane with pivoted arms and sliding guides
    • 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
    • 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 proposed corner bearing design consists of a support rod, a long and short scissor links and a support rod link together.
  • a partially comparable scissor construction is known from DE-A 32 23 451 (W.Hautau) (there Figure 5,6), the pivot point of the wing being shifted via a parallelogram on a guide rail in the frame (there 21).
  • DE-A 38 29 053 a tilt and turn axis that is displaceable in a slot of the support plate near the corner is provided in the lower frame (there 98, 100).
  • a second support point (support tab 180) for the support rod (there 162) is provided on the vertical leg of the corner bracket.
  • the task of the invention is to simplify the assembly of tilt-and-turn sashes in that a fitting is designed in such a way that it is easier to assemble and still allows larger sash weights to be safely absorbed and introduced into the frame during the operational movements (turning, tilting) ,
  • the proposed solution for the solution has only one support point for all functions of the fitting (claim 1, claim 4).
  • "Near and far" of the frame corner refers with regard to the handlebars to the open condition of the fitting and the linkage of the handlebars to the frame. The handlebars control the opening movement of the sash when turning.
  • the rotary and tilting bearing "D" remains immovable in one Support trough on a support plate (holding and control rail) in the frame corner and also forms the support point of the support rod for the tilting movement.
  • This new support device is not an independent device, as described in DE-A 38 29 053 (A. Winkhaus), with regard to the support rod (there 162), which here defines the bearing for the corner handlebar through its penetration by this control link.
  • the scissor bearings for the rotary and Tilting movement and the support of the support rod (continuously) in the lower one Frame corner are connected to a protruding from the same base in the fold of the fitting extending support rod 40 of great length, which is greater than the longer of the several control arms that control the movement of the wing take over the rotary motion.
  • the other end of the support rod, which is used to absorb the forces on the vertical bar attacking the wing can also be used for settings (claim 8).
  • Such an adjustment by an appropriate control device can either a height adjustment that does not change with operational changes in location changed, i.e. a basic setting or basic setting enabled, or one changes in operational position as part of the rotary movement of the wing be constantly changing height adjustment (claim 9 or claim 10), which The latter allows a slight lowering movement of the wing when the bar is supported Compensate rotary movement so that the wing is not or only insignificantly decreases with this rotation.
  • Both setting devices, the basic setting and the operationally changing "length change" of the support rod can also be combined (claim 9 and claim 10).
  • the "change in length" of the support rod is physically not an actual one Length change, but takes place due to a shift in the contact point the upper end of the support rod on an inclined support strip, in particular support surface, it appears to the outside as if the support rod at the rotational movement would lengthen, but in fact only its contact point would increase continuously is changed with the pivoting movement (rotary movement), in such a way that at one Rotary movement to open the wing moved the contact point downwards to "lengthen” the support rod and the sinking movement of the wing counteract and with a closing movement of the wing the corresponding opposite movement of the contact point on the inclined system (surface) takes place (Claim 10).
  • a second abutment is formed on the support rod so that the Support rod around this abutment when the wing rotates swiveled and sliding, but constantly touching on the inclined surface of the Frame fixedly attached counterpart is moved.
  • a crowned Forming which runs in the form of a drop, forms an advantageous design of the upper end of the support rod, while an advantageous design of the lower End of the support rod is an approximately cylindrical bearing section through a rotary opening of one of the control links is able to reach through and one cannot close-fitting, but rather "loose" corner storage allows which is only functional when the cylindrical end of the rod through the also cylindrical but slightly larger in diameter of the mentioned control arm reaches through and thereby forms a pin-eye bearing, to enable the full function of the fitting.
  • the system outlined above designed at least as a system strip, in particular but as a wider investment area, is preferred over a wide area in one oriented between 40 ° and 60 ° so that the inclined surface or Diagonal stripes from the upward oriented leg of the casement side Fitting part is oriented pioneering and downward towards immovable turn-tilt bearing shows.
  • the angle is based on the Front of the wing or the vertically oriented leg of the fitting.
  • the track can also be stronger in certain sections be curved, depending on the parallelogram motion control by the several handlebars, so that the compensation in the result is exactly that apparent Length change caused by pushing out in the direction "I" of the rod, which the Sash with the currently existing swivel movement (rotary movement) Moving out extended as a distance.
  • This can change the shape of the path the only preferably straight inclined surface or the diagonal stripe be adjusted so that exactly that change in distance is compensated for by moving the sash out as an extension of the distance from the fixed tilting point to the original contact point in the closed position.
  • parabolic function f1 begins with a short, clearly curved, after outward first half-branch and then runs over an elongated, largely parallel to the ideal gap distance and the second parabolic load has a turning point between these two branches, at which the initially easy Moving away from the frame corner and creating the gap in the elongated parallel movement that runs in the opposite direction and describes the opening movement of the wing.
  • FIGS. 1, 2 and 3 describe a first embodiment in a side view in the closed state (FIG. 1), in a rotationally open (pivotally open) position in supervision (FIG. 2) and in a likewise rotationally open (pivotally open) position in a side view (FIG. 3)
  • Figures 1a, 2a and 3a indicate the same operational positions of a second exemplary embodiment, which is identical to the first exemplary embodiment, but supplemented by a control device 50 at the upper end of the support rod 40 and by an eccentric device 70 on the horizontal section of the fitting for changing the lateral position of the tilt and turn bearing D on the fitting after installation.
  • These two devices 50, 70 are explained separately, otherwise, in the explanation of FIGS. 1, 2 and 3, which are explained together, the figures 1a, 2a and 3a, which are identical in this respect, are also explained accordingly.
  • the first exemplary embodiment has, as a lower corner bearing for the wing F, which, in the case of a tilt and turn fitting, allows a pivot opening (pivot opening) about a vertical axis and a tilt opening about a horizontal axis, a support rod 40 which is aligned vertically and in the rebate space between the wing F and frame B finds space.
  • the control of the rotary opening is carried out by a plurality of links which are connected to one another via a plurality of articulation points A i , "i" running from 1 to 4 in the exemplary embodiment, so that movement control of the wing occurs when opening, which in FIG characteristic positions of the wing corners F1 and F2 can be seen, which wing corners run along the curved paths f1, f2 during the opening movement, which are parabolic-like and in which the inner wing corner F1 describes a very small parabola, relative to the outer wing corner F2.
  • the small parabola f1 is closely approximated to a rectangular function, which first runs away from the frame, but then largely closely adjacent to it.
  • the parabola has two different steep branches and an intermediate reversal point.
  • FIG. 4 is self-explanatory, in which the said first parabola f1 runs from the closed point F1 to the opening point F1 ', while the second parabola f2 runs from the closed point F2 to the opening point F2'.
  • the connection F1 'and F2' defines a line which runs approximately parallel to the frame level, while the connection of the points F1 and F2 also defines a line which, however, runs approximately perpendicular to the plane of the frame.
  • the plane of the frame is represented by the area RE, which represents the surface of the frame B.
  • the parallelogram movement control according to FIG. 4 which takes place via the plurality of links, is in the first exemplary embodiment of a support rod link 10 as the link closest to the corner of the frame (in the open state), by a long scissor link 20 than the link remote from the frame corner (in the opened state) and one causes short scissor link 11, which connects the support rod link 10 with the frame corner of the wing side of the fitting.
  • the length relations are readily apparent from FIG. 2 .
  • the support rod arm is slightly larger than half (up to 3/4) the length of the long scissor arm 20 and the short scissor arm 11 is about a third to a quarter as long as the support rod arm.
  • bearing point D (the tilt and turn bearing) is a fixed articulation point provided, in which both the rotary movement and the tilting movement of the fitting and - with the sash attached - also the sash is initiated.
  • the right end of the support rod handlebar is right there 10 rotatably arranged, but positioned immovable. That is against it End of the long scissor link 20 on the frame side in a bearing point 32 approximately slidable along the frame level, in a slot guide 31a, which in a slightly raised portion 31, which is separated by two spaced, opposite directions Cranks of the frame plate 30 comes about, stored.
  • the slit 31a is far from the corner of the tilt & turn bearing D.
  • a support rod 40 which permits the tilting movement of the wing F is supported in a trough 35 which is provided in the frame corner on the frame plate 30 directly or indirectly via a separate short plate piece 75.
  • FIGS. 1a and 3a show this corner bearing D, consisting of a trough 35, the lower nose-shaped end 40a with a section which is somewhat reduced in diameter compared to the rest of the support rod 40 and the support rod link 10 penetrated by the reduced-diameter cylindrical bearing section 40a with an opening 10a provided there, the diameter of which is recognizably larger than the diameter of the bearing section 40a.
  • the bearing section 40a is shaped in accordance with the curvature of the trough 35 in order to allow the tilting movement.
  • the diameter of the opening 10a of the support rod link 10 is dimensioned such that the tilting movement of the rod 40 is made possible and the offset at the point of penetration when the rod is inclined does not become greater than the intended widened opening 10a of the support rod link 10 at the pivot / tilt bearing point D.
  • the wing-side section of the fitting is clearly visible in FIG . It consists of an angle with two legs, of which the vertical leg 42 carries a support with height adjustment 41 of the upper end of the support rod (support rod) 40.
  • the height adjustment 41 can be effected by a screw or a threaded section, it is adjustable, but cannot be changed during the operational movement of the wing and consequently the fitting. It offers the possibility of a basic or basic setting of the fitting.
  • the other leg 43 is oriented horizontally and carries the wing on the horizontal spar, on which the several links already explained in detail according to FIG .
  • the articulation points 32 and D are provided, of which only the former is displaceable, whereas the latter remains immovable in the corner of the frame. Between these hinged frame side and sash frame side articulation points, intermediate articulation points A1, A3 are provided which enable the parallelogram-like control according to FIG. 4 between the control links.
  • the tilting movement of the wing is not explicitly shown in the figures, but it follows, analogously to FIGS. 1 and 1a, with respect to the inclination of the support rod 40 out of the frame frame plane corresponding to the paper plane (to the front).
  • the inclination of the support rod 40 is essential and desirable during the tilting movement, at the same time the force (weight) of the wing F is derived into the immovable corner bearing point D, so that the control arms 10, 11, 20 and the wing corner are practically unaffected by the weight of the wing , Nevertheless, the function of the fitting is dependent on the support rod 40, since its nose section 40a first creates a pivot bearing of the support rod handlebar 10, without which pivot bearing the function of the fitting as a pivoting and tilting fitting would not be possible.
  • the support rod 40 is therefore a dependent device, without which the fitting does not work. With its nose-shaped bearing section 40a, it has a function for the pivoting bearing and with its inclination out of the frame level during the tilting movement, a force-dissipating function for the tilting movement.
  • the force is precisely introduced into the pivot bearing and the force introduction point is not next to the pivot bearing or above the pivot bearing, in order to make assembly easier if only a single point has to be mounted to create the pivot bearing and tilting bearing at the same time.
  • pivot / tilt bearing D is immovable and itself moved from its place neither during the rotating movement nor during the tilting movement.
  • control device 50 which works at the upper end 40b of the support rod 40 mentioned, is to be explained in more detail.
  • the control device 50 is most clearly visible in a side view (partially in section) in FIG. 1a and FIG. 3a . Once in the closed position with the support rod 40 standing vertically and once in the rotationally open position of FIG. 3a. It can clearly be seen that the corner bearing D on the frame side remains immovable.
  • the control device 50 changes the point of application or contact point of the support rod 40 with its upper end 40b, which in the example shown is similar to the approximately cylindrical bearing section 40a with reduced diameter, but is slightly drop-shaped in the uppermost section and is slightly thickened again, so that a larger one curved surface for changing plant is available.
  • the contact point is provided in a housing block or box 53 with an upper end 52, in which a wedge-shaped counterpart 51 is provided at its inner, upper end region.
  • the counterpart 51 can be changed by an additional adjustment device 41, as was explained with the height adjustment 41, which is independent of the operation, with reference to FIG. 1 .
  • This basic setting changes only the starting point and the end point, but in between, between the movements of the closed position of FIG. 1a and the open position of FIG. 3a when the rotary opening is opened, the point of contact of the drop-shaped end 40b of the support rod 40 on the inclined surface 51a of the counterpart 51 shifts The displacement is caused by the passage of the upper end of the support rod 40 through the lower wall of the box-shaped housing 53.
  • the rod 40 appears to be pushed out of the housing in the direction "I" from the function to be extended and is able to the wing at his Not to let the rotary motion sink, rather to remain largely stable in height hold.
  • the control device 50 is approximately the same as the length of the rod 40 Distance firmly on the vertical leg 42 of the casement side Mounting bracket 42/43 arranged. It has when the wing tilts no function, since there is no displacement of the contact point 40b parallel to the Wing frame remaining support rod 40 is carried out. This does not result in any Apparent physical extension of the support rod 40 reached at the Tilting movement of the wing is also not required.
  • an eccentric adjustment device 70 can be provided on the frame plate 30 of the fitting, very close to the non-displaceable corner bearing D, as shown in FIGS. 1a and 2a, especially in the enlarged detail.
  • a short attachment piece 75 can be used in the area near the corner bearing on the frame plate.
  • the Attachment piece 75 is flat, then carries the aforementioned cross-oriented oval Recess 72, while the eccentric 71a with axis 71 on the Frame plate 30 is arranged; the top piece 75 has on the in Figure 2a on the left side, the peg-shaped engagement 74 in an elongated hole recess the frame plate 30 and carries on the other side of the oval recess 72nd the essentially immovable corner bearing D, which is only part of a Adjustment movement by a small amount, which is given by the eccentric 71a / 72 is adjustable. This remains unaffected in the normal operational process completely non-displaceable pivot / tilt bearing point D at which the lower end 40a of the Support rod 40 and the one used for pivoting (turning) Support rod link 10 are stored.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Wing Frames And Configurations (AREA)
  • Soil Working Implements (AREA)
  • Walking Sticks, Umbrellas, And Fans (AREA)
  • Toys (AREA)

Claims (12)

  1. Ferrure pour un vantail (F), laquelle est appliquée de façon pivotante sur un dormant (B) comportant un coin de dormant de telle manière qu'il peut tourner et basculer, un coin de vantail (F1) s'écartant du plan du dormant (B) et continuant à se déplacer le long d'une voie (f1) courbe pendant un mouvement de rotation, laquelle ferrure
    a) dispose de plusieurs bras (10, 20, 11) qui sont reliés par plusieurs articulations (Ai ; i = 1, ..., 4) afin que la commande du mouvement du vantail (F) soit possible, caractérisée en ce que
    b) le bras (10) à proximité du coin de dormant de la ferrure y est articulé sans pouvoir coulisser (D) et le bras (20) éloigné du même coin est plus long et est monté (32) coulissant approximativement le long du plan de dormant et que
    c) sur le point d'articulation (D) non coulissant une barre de soutien (40) qui permet que le vantail ait un mouvement de basculement est soutenue de façon à basculer vers l'extérieur (35) pour que le poids du vantail soit appliqué directement au point d'articulation (D) non coulissant.
  2. Ferrure selon la revendication 1, pour laquelle la barre (40) basculante est nettement plus longue que le bras (10, 11, 20) et est maintenue dans une cavité (35).
  3. Ferrure selon la revendication 2, pour laquelle à proximité de la cavité (35) la barre (40) a un segment de palier (40a) à peu près cylindrique, notamment réduit en diamètre, autour duquel le bras (10) proche du coin peut pivoter pour servir de point d'articulation qui dépend de la barre de soutien (40).
  4. Ferrure selon l'une des revendications 1 à 3, pour laquelle le bras proche et le bras éloigné (10, 20) sont respectivement articulés d'un côté sur un rail (30) de façon coulissante (D) ou non coulissante (31a, 32).
  5. Ferrure oscillobattante comportant plusieurs bras de commande pour un vantail (F), pour laquelle un palier croisé (D, 35, 40a) horizontal pour ce qui est d'un des bras de commande (10, 11, 20) se trouve et reste dans un coin de dormant de la ferrure dans chaque position fonctionnelle de la ferrure et forme en même temps un point de soutien (35) d'une barre d'appui (40, 40a) dirigée verticalement qui soutient le vantail lors d'un mouvement de basculement sur un de ses longerons orientés à la verticale.
  6. Ferrure pour un vantail (F) oscillobattant, pour laquelle on prévoit un palier de rotation ou un palier de pivotement sur le côté du dormant (30) de la ferrure et un palier basculant du même côté de ferrure sur un seul et même point (D, 35), lequel point n'est coulissant pour aucune des positions de ferrure possibles et une barre de soutien (40) s'applique avec un effet de soutien sur le côté de vantail de la ferrure en faisant saillie devant ce point sur un montant (42) vertical.
  7. Ferrure selon la revendication 1, pour laquelle le " bras éloigné " (20) en étant disposé (32) du côté du dormant est guidé de façon coulissante dans une fente (31a) éloignée du palier d'angle sur un segment (31) - légèrement soulevé sur des coudes - d'un rail de maintien et de guidage (30).
  8. Ferrure selon l'une des revendications précédentes, pour laquelle on prévoit sur le côté du châssis du battant une installation de commande (41, 50) pour effectuer le réglage de la barre d'appui (40) à l'extrémité (40b) qui se trouve en face de l'extrémité de palier (40a) non coulissante.
  9. Ferrure selon la revendication 8, pour laquelle le réglage est un ajustement réglable en hauteur (41, 51) qui ne se modifie pas lors de modifications fonctionnelles de la position de la barre d'appui (40).
  10. Ferrure selon la revendication 8, pour laquelle le réglage est un ajustement réglable en longueur (50 ; 51a, 40b) selon lequel l'extrémité (40b), éloignée du palier de coin, de la barre d'appui (40) s'applique sur une bande d'application (51a) d'une pièce opposée (51), laquelle bande d'application s'étend en étant inclinée à plat dans une application de contact durable pour provoquer une " modification en longueur " permanente de la barre d'appui (40) en cas de mouvement de rotation fonctionnel grâce à un déplacement permanent du point d'application sur la surface d'application (51a).
  11. Ferrure selon la revendication 1, la revendication 5 ou la revendication 6, pour laquelle la barre (40) basculante - du bras (10) qui est proche du coin de dormant et qui est monté de façon à tourner près du point d'articulation (D) non coulissante - est maintenue dans une cavité (35) à son extrémité inférieure (40a) de façon à pouvoir basculer vers l'extérieur.
  12. Ferrure selon la revendication 11, pour laquelle grâce au support, qu'on peut faire basculer vers l'extérieur, du bras (10) rotatif proche une commande de l'écartement du coin (F1) - proche de la surface de dormant (RE) - du vantail ou du recouvrement de vantail (F) est effectuée le long d'une voie (f1) qui se rapproche dans une grande mesure d'une forme angulaire, de sorte que, dans la zone initiale du mouvement d'ouverture, elle produit une distance - qu'on obtient rapidement mais qui est petit entre le coin (F1) et la surface (RE) pour ensuite s'étendre à peu près parallèlement à la surface (RE) jusqu'à la position d'ouverture de la ferrure selon pratiquement la même distance petite.
EP97123028A 1996-12-31 1997-12-31 Ferrure oscillo-battante avec support d'angle non-coulissant Expired - Lifetime EP0851085B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE1998128670 DE19828670A1 (de) 1996-12-31 1998-06-26 Steuereinrichtung für einen ecklagerpunktfesten Drehkippbeschlag

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19654682A DE19654682A1 (de) 1996-12-31 1996-12-31 Drehkippbeschlag mit unverschieblichem Ecklagerpunkt
DE19654682 1996-12-31

Publications (2)

Publication Number Publication Date
EP0851085A1 EP0851085A1 (fr) 1998-07-01
EP0851085B1 true EP0851085B1 (fr) 2004-05-12

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EP (1) EP0851085B1 (fr)
AT (1) ATE266791T1 (fr)
DE (2) DE19654682A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1837472A1 (fr) 2006-03-25 2007-09-26 Roto Frank Ag Fenêtre, porte ou similaire avec un dispositif de délestage
DE102007024742A1 (de) 2007-05-26 2008-11-27 Roto Frank Ag Fenster, Tür oder dergleichen mit einer Entlastungseinrichtung

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE20010653U1 (de) * 2000-06-21 2001-10-31 Siegenia Frank Kg Drehkippbeschlag
DE20012351U1 (de) * 2000-07-14 2001-11-15 Siegenia Frank Kg Fenster oder Tür mit Entlastungseinrichtung
WO2006125934A1 (fr) * 2005-05-25 2006-11-30 Trojan Hardware & Designs, Ltd. Installation de charnieres de porte
DE102010000675A1 (de) * 2010-01-05 2011-07-07 Aug. Winkhaus GmbH & Co. KG, 48291 Ecklager eines gegen einen Rahmen schwenkbaren Flügels eines Fensters und Fenster mit einem solchen Ecklager
DE202010012004U1 (de) * 2010-08-31 2011-12-28 Maco Technologie Gmbh Lastabtragung für Fenster, Türen oder dergleichen
DE102015003931B3 (de) * 2015-03-25 2015-11-12 Siegenia-Aubi Kg Gelenkbandanordnung

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3829053C2 (de) * 1988-08-26 1994-02-17 Winkhaus Fa August Dreh-Beschlag oder Dreh-Kipp-Beschlag von Fenstern, Türen oder dergleichen
DE3834388C1 (fr) * 1988-10-10 1990-03-22 Siegenia-Frank Kg, 5900 Siegen, De
DE3843680C2 (de) * 1988-12-23 1996-05-15 Bayerwald Fensterfabrik Altenb Verdeckt angeordneter Beschlag für Schwenklager von Türen, Fenstern oder dergleichen
DE9000152U1 (fr) * 1990-01-09 1990-03-15 August Bilstein Gmbh & Co Kg, 5828 Ennepetal, De

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1837472A1 (fr) 2006-03-25 2007-09-26 Roto Frank Ag Fenêtre, porte ou similaire avec un dispositif de délestage
DE102007024742A1 (de) 2007-05-26 2008-11-27 Roto Frank Ag Fenster, Tür oder dergleichen mit einer Entlastungseinrichtung
DE102007024742B4 (de) * 2007-05-26 2016-07-28 Roto Frank Ag Fenster oder Tür mit einer Entlastungseinrichtung

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DE59711616D1 (de) 2004-06-17
ATE266791T1 (de) 2004-05-15
EP0851085A1 (fr) 1998-07-01
DE19654682A1 (de) 1998-07-02

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