EP0875651B1 - Automatic adjusting device - Google Patents

Automatic adjusting device Download PDF

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Publication number
EP0875651B1
EP0875651B1 EP98102033A EP98102033A EP0875651B1 EP 0875651 B1 EP0875651 B1 EP 0875651B1 EP 98102033 A EP98102033 A EP 98102033A EP 98102033 A EP98102033 A EP 98102033A EP 0875651 B1 EP0875651 B1 EP 0875651B1
Authority
EP
European Patent Office
Prior art keywords
hinge
frame
wing
positive engagement
engagement elements
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
EP98102033A
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German (de)
French (fr)
Other versions
EP0875651A3 (en
EP0875651A2 (en
Inventor
Thomas Freudenberg
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 Aubi KG
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Filing date
Publication date
Application filed by Siegenia Aubi KG filed Critical Siegenia Aubi KG
Publication of EP0875651A2 publication Critical patent/EP0875651A2/en
Publication of EP0875651A3 publication Critical patent/EP0875651A3/en
Application granted granted Critical
Publication of EP0875651B1 publication Critical patent/EP0875651B1/en
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Classifications

    • 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
    • E05F7/005Aligning devices for wings
    • 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
    • E05D15/5205Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis with horizontally-extending checks
    • 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
    • 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
    • E05Y2800/00Details, accessories and auxiliary operations not otherwise provided for
    • E05Y2800/37Length, width or depth adjustment
    • 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 device for aligning the Wing of a door, a window or the like. Relative to one fixed frame, with sash and frame over a relative to the frame adjustable axis of rotation through Hinge elements are formed at least around a vertical one Axis of rotation are pivotally connected to each other and where Hinge element made of at least two movable relative to each other Hinge parts exist, with a first part stationary in the Frame and a second fixedly assigned to the wing with one at least in the surface-parallel position of sash and frame acting alignment element producing an alignment movement.
  • the frame can be turned by turning the adjusting screw be caused, which is a relative displacement of the end of the Hinge arm attached coupling piece with respect to the Hinge arm results.
  • the adjustment is done manually and may have to be repeated at regular intervals as the wing follows some time by loosening the fasteners and by Wear of the bearing components an anti-parallel position to the frame occupies.
  • Sashes and frames can also have auxiliary devices are aligned with each other, such as the DE 327 608 or also show DE 41 17 407 C2.
  • auxiliary devices are aligned with each other, such as the DE 327 608 or also show DE 41 17 407 C2.
  • the tilt function for turn-tilt sashes is also achieved by this Auxiliary devices adversely affected because the tilt axis is shifted by the auxiliary device.
  • Another device for aligning the wing opposite the framework is known from DE-OS 20 65 840.
  • a downward protruding coupling piece attached with an am Bolt linkage of the wing attached locking bolt interacts, with the dome as the mushroom head pin trained locking pin engages around a fork.
  • the coupling piece is anti-parallel to the rebate circumferential surface of the wing or the frame aligned and causes at one Displacements of the locking bolt a relative movement of the Wing opposite the frame.
  • the object of the invention is therefore a device for Align the wing of a door, a window or the like. in relation to a fixed frame that this independently by normal operation of the wing takes place with a safe storage of the sash on the frame and lock against the alignment movement.
  • the object is achieved by one or more between the hinge parts automatically acting or acting locking element or locking elements, which fix the hinge parts against each other and lock against the alignment movement, the Hinge parts against each other by the alignment element are movable.
  • Locking elements look like Form-locking elements exist, and that the positive-locking elements between each other through the alignment movement removing boundary edges of the hinge parts relocatable are arranged.
  • a simple design and manufacturing technology Design provides that the positive locking elements from with Wedge-provided actuators exist, the Wedge surfaces lie against each other and the adjusting pieces against each other are arranged displaceable.
  • Another embodiment is to prevent large wings the invention that the wedge surfaces offset from step-like lying, to an opposite to the alignment movement load direction, almost vertical aligned plan areas exist, the levels by Sections running at an obtuse angle to the plane surfaces are connected. This configuration causes the on Normal forces due to the vertical Flat surfaces are transferred while making an adjustment the wedge surfaces interacting with each other adjusting the Effect form-locking elements.
  • a particularly simple embodiment provides that one of the Wedge surfaces in one piece with a fixed to the axis of rotation connected hinge frame is formed. This reduces the necessary assembly work considerably.
  • Form-fit elements consist of plate-shaped components and the boundary edges almost perpendicular to Direction of loading.
  • the invention further provides that the positive locking elements through an energy storage device into which the hinge parts mutually blocking position are brought. This is supposed to any friction or odor acting between the positive locking elements Like. Be overcome.
  • a preferred embodiment also provides that one of the hinge parts is designed as a hinge arm, the one with a hinge pin forming the hinge axis fixed and at the other end with the wing-fixed hinge part - Angled part is at least longitudinally connected.
  • This Design relates above all to turn and tilt and turn sash commercially available fittings, which subsequently with automatic effective adjustment should be equipped.
  • one of the Hinge parts is designed as a frame-fixed bearing block, while the second moved by means of the alignment element Hinge part is formed by the bearing pin and when the Positive locking elements via a force accumulator, in particular via a spring are connected.
  • the bearing pin enclosing bearing eyes transverse to the axis of rotation - in the Frame level - are elongated and that the Interlocking elements between the narrow side walls of the Bearing eyes and the bearing pin are arranged.
  • the Narrow side walls and the positive locking elements with adjacent wedge surfaces are provided.
  • a right and such a bearing block can be used on the left, if the two bearing eyes are symmetrical on a base plate are arranged. In this case, the bearing block can be used for both can be used on the right as well as for windows that can be opened on the left.
  • a particularly simple embodiment of such Bearing block provides that the energy storage device as Tension spring is formed. This can be between the two Form-fit elements lie and be effective between them.
  • the locking device from a locking device locking against the opening device consists. This also works positively, but prevents it a sliding back of the hinge parts in the position in front of Alignment movement.
  • FIG. 1 shows a window 1 consisting of a fixed frame 2 and one in it both about a vertical axis of rotation 3 and wings 4 pivotable about a horizontal axis of rotation 5 Frame 2 and the wing 5 are via an upper hinge 6 and a lower hinge 7 connected to each other.
  • the design provides that the upper hinge 6th is designed as a so-called scissor store, while the lower hinge 7 is designed as a so-called corner bearing.
  • the Wing 5 has one for locking in the frame 2 - here not shown - locking fitting on a Hand lever 8 on the wing 5 can be operated. At a The locking fitting is made of a tilt and turn fitting via the hand lever 8 also the possibility for one Swiveling movement around the lower horizontal axis of rotation 4 adjustable.
  • On the upper horizontal wing spar 9 is in this case, an opening device with a perpendicular to Wing-level movable extension arm attached to the upper horizontal wing spar 9 connects to the upper hinge 6.
  • At the lower horizontal wing spar 10 is between the frame 2 and wing 5 a - not visible here - tilt lock effective so that the lower horizontal wing edge 11 on the frame 2 is held.
  • an alignment element 17 is provided which is in contact with the fold surface 14 of the wing 5 or one - not shown here - fixed Component interacts in such a way that the original intended distance of the folding surfaces 14, 13 at Closing of the wing 5 again.
  • the alignment element In the simplest case, 17 consists of one with an in Equipped with ascending ramp Casserole, which with the fold surface 14 of the wing interacts.
  • the wing 5 receives through the alignment element 17th its original starting position 12, in which the frame and Wing spars are parallel to each other. When opening the wing 5 however the front wing edge 18 sags again, as soon as the fold surface 14 slips off the alignment element 17.
  • the wing 5 can only by manually lifting the front wing edge 18 into the frame 2 plunge.
  • Tilt and turn fittings therefore provide that on the upper hinge 6 manual adjustment options are attached to the Restore the starting position 12 serve.
  • Fig. 2 shows an upper hinge assembly 20, which consists of a wing-fixed angle component 21, one movable transversely thereto mounted hinge arm 22, one attached to the end and in front of the frame plane projecting coupling part 23 and a fixed to the frame, fixed on the frame visible surface 24 Bearing block 25, the bearing block 25 and that Coupling part 23 pivotally connected via a bearing pin 26 are.
  • one Hinge arrangement 20 is a pure one Rotary fitting, in which only one vertical axis of rotation 3 is provided is.
  • the angle component 21 is fastened in here a fitting groove 27 introduced into the rebate surface 14 Hinge arm 22 is on the pin 28, 29 with the Angle component 21 connected, the pin 29 fixed in the Angle component 21 is anchored and the hinge arm 22 in one Passes through slot 30 and this with a mushroom head 31st guaranteed.
  • the pin 28 is rotatable in the eccentric Angle component 21 is mounted and extends through the angle component 21 in an elongated hole 32 and also has a mushroom head 33.
  • the eccentric mounting of the pin 28 is used for Achieving a greater pressure of the wing 5 on the frame 2, i.e.
  • the oblong hole 30 almost corresponds in its transverse dimension the diameter of the pin 29 so that the hinge arm 22 at Actuation of the pin 28 by an inserted therein Tool engagement 34 around the pin 29 acting as the axis of rotation is pivoted, whereby the wing plane is opposite the Frame level shifted.
  • the hinge arrangement 20 in the illustrated embodiment also has a manually operated adjusting screw 35 on, which acts in the longitudinal direction of the hinge arm 22. This is with a - not visible - thread at the end of a Actuator 36 in engagement, but on the other hand by their location on the coupling part 23 and over the bearing pin 26 with stationary connected to the frame 2.
  • Window 1 also shows - not here visible - alignment element 17, which the wing 5 in the closed position - i.e. when immersing the wing 5 in align the frame 2 - in a parallel position.
  • the angle member 21 is relative to Hinge arm 22 moves until the rebate surfaces 13, 14th stand parallel and the rebate clearance or the chamber dimension 15 in its normal size.
  • the hinge arm 22 which, because it is stationary the bearing pin 26 is connected to the frame-fixed bearing block 25, the alignment movement is not carried out.
  • Form-locking element 37 is free in the area of the adjusting element 36 movable, which on the one hand in the direction of the coupling part 23 pointing recess 38 passes through, but perpendicular to Fold surface 14 is slidably arranged, on the other hand with a wedge surface 39 on a complementary Wedge surface 40 of the actuator 36 abuts.
  • the form-locking element 37 passes through the common Recess 38 of the hinge arm 22 and the actuator 36 and a, recess 38a in the angular component 21.
  • the almost vertical back of the form-locking element 37 lies at least in the area of the recess 38a of the Angular component 21 in a form-fitting manner on this.
  • the positive locking element 37 is free to an extent that corresponds to the amount in which the front - not visible here Wing edge 18 is raised.
  • the tension spring 41 Form-locking element 37 pulled down so that - according to the wedge effect - the new, spread position of the Hinge arm 22 adjusts with respect to the angle component 21.
  • Locking element acting form-locking element 37 against the Direction R loaded, it being a form fit between the Angle component 21 and the hinge arm 22 and this to each other, against the direction R of the alignment movement, in Load direction fixed, i.e. locked. In the R direction the lock can still be released.
  • FIG. 4 shows the hinge arrangement 20 corresponding to FIG. 3, where the automatic alignment has already taken effect. How is particularly visible in connection with Fig. 3, by the immersion of the positive locking element 37, the relative position of the Hinge arm 22 changed with respect to the angle component 21, see above that the distance between two arbitrarily chosen points on each Component - here based on the fold surface 14 and the Boundary edge 42 'of the actuator 36 shown - changes.
  • the positive locking element 37 can - as shown in FIG. 5 - also by a plug 45, which is seated in the opening 43, fixed become. This is for example when assembling the Hinge arrangement 20 makes sense to the adjustment range of automatic adjustment.
  • the plug 45 protrudes through the leg 46 of the angle component 21 and touches with its lateral surface 47 the lower end 48 of the Form-locking element 37 in its initial position.
  • the stopper 45 According to this configuration, it is only after the wing 5 is installed removed on the frame 2 from the opening 43, so that the Form-locking element 37 only becomes movable.
  • Fig. 6 shows the form-locking element 37 in an enlarged Scale.
  • the form-locking element 37 has a wedge shape the stepped shoulders 50 are arranged.
  • the depth 52 of paragraphs 50 determines the minimum possible measure with which the alignment movement of the alignment element 17 can be fixed can. The smaller this depth 52 is chosen, the finer Alignment movements can be fixed and retained.
  • phase-like sections 53 running to the flat surfaces 51 get connected.
  • FIG. 7 shows an embodiment of an opening device a tilt and turn window, the as locking elements acting form-locking elements 37 made of plate-shaped components exist in an opening 55 of the actuator 36th lie next to each other in layers.
  • the positive locking elements 37 are loaded on their underside by spring elements. Is the actuator 36 slidably leading and overlapping extension arm 56 by the aligning force in Direction R - together with wing 5 - moves, so overlap the opening 57 in the extension arm 56 and the opening 55 in Actuator 36 partially. If the cover reaches a clear dimension, that is greater than the strength of one of the form-locking elements 37, so this is arranged under the influence of the one below Spring element moved up and locked the Extension arm 56 with respect to that arranged displaceably Actuator 36 against the direction R.
  • Fig. 7a the spring elements consist of spring tongues 58 which are mutually parallel and by a common transverse web 59 are connected and the molded part 60 form.
  • the molded part 60 can be stamped or the like produce a spring steel and is on the actuator 36th attached.
  • the extension arm 56 - also to avoid the Penetration of the mobility of the interlocking elements 37 impairing dirt - with a thin-walled cover 61 closed.
  • This thin-walled cover 61 can for example from a removable plastic or sheet metal part be formed.
  • FIGS. 8a and 8b show a schematic Embodiment of the invention in which the Form-locking elements 37 in a fixed position on the frame 2 Bearing block 70 are performed.
  • a tape roll 71 is in Transverse direction fixed with a - not shown - extension arm an opening device or the like connected. It sticks out a cantilever 72 of the tape roll 71 up to the - not here either shown - folding surface 13 of the frame 2.
  • the tape roll 71st engages around a bearing pin 73 which is in an elongated hole Bearing eyes 74 of the bearing block 70 parallel to the frame plane is led.
  • the bearing block 70 has bearing eyes 74, in which the positive locking elements 37 along the central axis of the Bearing pin 73 are performed.
  • the bearing eyes 74 are on one Provide the end with the wedge surfaces 40 to the central transverse axis 75 of the bearing block 70 the wall thickness of the bearing eye 74 enlarge.
  • the form-locking elements 37 are also with Wedge surfaces 39 provided in the opposite direction run so that the bearing pin 73 facing, with a Circular segment 76 provided lateral boundary edges 77 of the Form-locking elements 37 run parallel to the bearing pin 73.
  • the illustrated embodiment has compared to the embodiments described above have the advantage that the wing components are left almost unchanged can. Also 15 are attached outside of the air gap Do not adapt devices to the limited space available and can be easily od with a suitable cover cap. Adapt to the optical conditions.
  • the base plate 79 of the bracket 70 as shown in FIG Recognizing the embodiment is symmetrical with respect to Central transverse axis 75 designed so that the bearing block 70 both for wing 5 opening to the right as well as to the left opening Wing 5 can be used.
  • Wings 5 is advantageous if the positive locking element 37 for example according to Fig. 2 to 5 with the vertical back as large as possible on the vertical angle leg 46 des Angle component 21 bears against a tilting or twisting of the Prevent angular component 21.
  • angle leg 46 a has an extension projecting into the recess 38 and / or that the interlocking element 37 along the fold surface 14 of the angle leg 46 is guided. This would also do that Moving the form-locking elements 37 relative to the actuator 36 favors.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Massaging Devices (AREA)
  • Paper (AREA)
  • Fluid-Damping Devices (AREA)

Abstract

The door or window is hung in a fixed frame about an adjustable axis by a number of hinges, each with one section fixed to the frame and one section to the door or window pane. An adjusting element provides an adjustment movement, at least in the plane of the door or window pane and alters the setting of each hinge with respect to the hinge axis to align the hinged frame inside the fixed frame. The hinge sections can slide against each other by the movement of the adjusting element. One or more independently acting locking elements (37) between the hinge sections fix the hinge pieces with respect to each other and prevents the adjustment movement.

Description

Die Erfindung betrifft eine Vorrichtung zum Ausrichten des Flügels einer Tür, eines Fensters od. dgl. relativ zu einem feststehenden Rahmen, wobei Flügel und Rahmen über eine relativ zum Rahmen lagenjustierbare Drehachse die durch Scharnierelemente gebildet wird mindestens um eine vertikale Drehachse schwenkbar miteinander verbunden sind und wobei das Scharnier element aus mindestens zwei relativ zueinander beweglichen Scharnierteilen besteht, wobei ein erstes Teil ortsfest im Rahmen und ein zweites lagefest dem Flügel zugeordnet ist, mit einem zumindest in flächenparalleler Lage von Flügel und Rahmen wirkenden, eine Ausrichtbewegung erzeugendes Ausrichtelement.The invention relates to a device for aligning the Wing of a door, a window or the like. Relative to one fixed frame, with sash and frame over a relative to the frame adjustable axis of rotation through Hinge elements are formed at least around a vertical one Axis of rotation are pivotally connected to each other and where Hinge element made of at least two movable relative to each other Hinge parts exist, with a first part stationary in the Frame and a second fixedly assigned to the wing with one at least in the surface-parallel position of sash and frame acting alignment element producing an alignment movement.

Es sind Vorrichtungen bekannt, die eine Justage des Flügels bezüglich seiner Lager zum feststehenden Rahmen mittels Stellgliedern erlauben. So ist es beispielsweise aus der DE 36 37 077 C1 ebenso wie einer Reihe weiterer Veröffentlichungen bekannt, einen Scharnierarm bezüglich eines blendrahmenfesten Lagerbocks verschiebbar zu befestigen und entgegen der durch das Gewicht des Flügels wirkenden Belastungsrichtung mittels einer Stellschraube zu sichern.Devices are known for adjusting the wing regarding its bearings to the fixed frame by means of Allow actuators. For example, it is from the DE 36 37 077 C1 as well as a number of others Publications known a hinge arm regarding one frame fixed to the frame and fixed contrary to that acting through the weight of the wing Secure the load direction with an adjusting screw.

Eine Justage des Flügels gegenüber dem feststehenden Blendrahmen kann dabei durch ein Verdrehen der Stellschraube bewirkt werden, was eine Relativverschiebung des am Ende des Scharnierarms angebrachten Kupplungsstücks bezüglich des Scharnierarms zur Folge hat.An adjustment of the wing compared to the fixed The frame can be turned by turning the adjusting screw be caused, which is a relative displacement of the end of the Hinge arm attached coupling piece with respect to the Hinge arm results.

Die Justage erfolgt dabei manuell und muß unter Umständen in regelmäßigen Abständen wiederholt werden, da der Flügel nach einiger Zeit durch Lockerung der Befestigungselemente und durch Verschleiß der Lagerbauteile eine antiparallele Lage zum Rahmen einnimmt.The adjustment is done manually and may have to be repeated at regular intervals as the wing follows some time by loosening the fasteners and by Wear of the bearing components an anti-parallel position to the frame occupies.

Flügel und Rahmen können auch über Hilfseinrichtungen gegeneinander ausgerichtet werden wie sie beispielsweise die DE 327 608 oder auch die DE 41 17 407 C2 zeigen. Dabei sind Vorrichtungen zum Ausrichten des Flügels auf der der Drehachse entgegengesetzt liegenden Seite des Flügels angebracht, die beim Eintauchen des Flügels in den Rahmen mit lagefest am Rahmen angebrachten Elemente zusammenwirken und ein Ausrichten des Flügels bezüglich des Rahmens erzielen.Sashes and frames can also have auxiliary devices are aligned with each other, such as the DE 327 608 or also show DE 41 17 407 C2. Are there Devices for aligning the wing on the axis of rotation opposite side of the wing attached that when immersing the sash in the frame with fixed position on Frame-mounted elements interact and align of the wing with respect to the frame.

Von großem Nachteil ist es dabei, daß derartige Vorrichtungen nur in einem bestimmten Bereich des Schwenkwinkels des Flügels wirken und in dem Wirkbereich, beim Eintauchen des Flügels in dem Blendrahmen, einen Zwang in den Scharnieren bewirken. Weiterhin werden derartige Vorrichtungen bei sehr großen Abweichungen der Lage unwirksam oder müssen durch besondere technisch aufwendige Ausgestaltungen flexibler werden, da sie die ihnen zugeordneten Bauteile an Rahmen nicht treffen bzw. finden und so ein zusammenwirken unmöglich wird. It is a great disadvantage that such devices only in a certain range of the swing angle of the wing act and in the effective range when immersing the wing in the frame, a constraint in the hinges. Furthermore, such devices are very large Deviations in the situation ineffective or must be caused by special technically complex designs become more flexible because they the components assigned to them do not meet on the frame or find and so cooperation becomes impossible.

Auch wird die Kippfunktion bei Dreh-Kipp-Flügeln durch diese Hilfseinrichtungen nachteilig beeinflußt, da die Kipp-Achse durch die Hilfseinrichtung verlagert wird.The tilt function for turn-tilt sashes is also achieved by this Auxiliary devices adversely affected because the tilt axis is shifted by the auxiliary device.

Eine weitere Vorrichtung zum Ausrichten des Flügels gegenüber dem Rahmen ist durch die DE-OS 20 65 840 bekannt geworden. Bei der darin offenbarten Ausstellvorrichtung ist ein nach unten ragendes Kuppelstück angebracht, das mit einem am Riegelgestänge des Flügels befestigten Feststellbolzen zusammenwirkt, wobei das Kuppelstück den als Pilzkopfzapfen ausgebildeten Feststellbolzen gabelförmig umgreift. Das Kuppelstück ist antiparallel zur Falzumfangsfläche des Flügels bzw. des Rahmens ausgerichtet und bewirkt bei einer Verschiebungen des Feststellbolzens eine Relativbewegung des Flügels gegenüber dem Rahmen.Another device for aligning the wing opposite the framework is known from DE-OS 20 65 840. at the display device disclosed therein is a downward protruding coupling piece attached with an am Bolt linkage of the wing attached locking bolt interacts, with the dome as the mushroom head pin trained locking pin engages around a fork. The The coupling piece is anti-parallel to the rebate circumferential surface of the wing or the frame aligned and causes at one Displacements of the locking bolt a relative movement of the Wing opposite the frame.

Es ist dabei von großem Nachteil, daß die Ausrichtung des Flügels nicht in allen Schaltstellungen des Beschlages wirksam ist, sondern - abhängig von der Stellung des Feststellbolzens-die Ausrichtvorrichtung außer Kraft gesetzt wird.It is a major disadvantage that the orientation of the Wing is not effective in all switch positions of the fitting is, but - depending on the position of the locking bolt Alignment device is overridden.

Aufgabe der Erfindung ist es daher, eine Vorrichtung zum Ausrichten des Flügels einer Tür, eines Fensters od. dgl. relativ zu einem feststehenden Rahmen derart auszugestalten, daß diese selbständig durch normale Betätigung des Flügels erfolgt bei einer sicheren Lagerung des Flügels am Rahmen und entgegen der Ausrichtbewegung sperren.The object of the invention is therefore a device for Align the wing of a door, a window or the like. in relation to a fixed frame that this independently by normal operation of the wing takes place with a safe storage of the sash on the frame and lock against the alignment movement.

Die Aufgabe wird erfindungsgemäß gelöst durch ein oder mehrere zwischen den Scharnierteilen selbsttätig wirkendes bzw. wirkende Verriegelungselement bzw. Verriegelungselemente, welche die Scharnierteile gegeneinander lagefixieren und entgegen der Ausrichtbewegung sperren, wobei die Scharnierteile durch das Ausrichtelement gegeneinander verschiebbar sind. According to the invention, the object is achieved by one or more between the hinge parts automatically acting or acting locking element or locking elements, which fix the hinge parts against each other and lock against the alignment movement, the Hinge parts against each other by the alignment element are movable.

Vorteilhafte Ausgestaltungen der Erfindung sind begenstand der abhängigen Ansprüche.Advantageous embodiments of the invention are the subject of the study of the dependent claims.

Eine besonders sichere und einfache Ausgestaltung der Verriegelelemente sieht vor, daß die Verriegelungselemente aus Formschlußelementen bestehen, und daß die Formschlußelemente zwischen sich durch die Ausrichtbewegung voneinander entfernenden Begrenzungskanten der Scharnierteile verlagerbar angeordnet sind.A particularly safe and simple design of the Locking elements provides that the locking elements look like Form-locking elements exist, and that the positive-locking elements between each other through the alignment movement removing boundary edges of the hinge parts relocatable are arranged.

Eine konstruktiv wie herstellungstechnisch einfache Ausgestaltung sieht vor, daß die Formschlußelemente aus mit Keilflächen versehenen Stellstücken bestehen, wobei die Keilflächen aneinander liegen und die Stellstücke gegeneinander verlagerbar angeordnet sind.A simple design and manufacturing technology Design provides that the positive locking elements from with Wedge-provided actuators exist, the Wedge surfaces lie against each other and the adjusting pieces against each other are arranged displaceable.

Dadurch wird erreicht, daß die durch das Ausrichtelement gegeneinander verschobenen Scharnierteile gegeneinander lagenfixiert werden und dadurch die vertikale Drehachse des Flügels relativ zum Flügel verschoben wird. Der Flügel erhält dadurch eine neue Ausrichtung gegenüber dem feststehenden Rahmen und zwar so, daß die aufrechten und waagerechten Holme des Flügels nahezu parallel zu denen des Rahmens stehen. Eine weitere Bedienung des Flügels ist daher problemlos möglich, da die Verriegelungselemente die einmal eingestellte und durch das Ausrichtelement bestimmte Lage des Flügels bezüglich des Rahmens lagenfixieren.This ensures that the alignment element hinge parts shifted against each other be fixed in position and thereby the vertical axis of rotation of the Wing is moved relative to the wing. The wing receives thereby a new orientation compared to the fixed Frame in such a way that the upright and horizontal bars of the wing are almost parallel to those of the frame. A further operation of the wing is therefore easily possible because the locking elements once set and by the Alignment element certain position of the wing with respect to Fix the frame in place.

Um ein Rückstellen der Verriegelung durch das Flügelgewicht bei großen Flügeln zu verhindern, sieht eine weitere Ausgestaltung der Erfindung vor, daß die Keilflächen aus stufenartig versetzt liegenden, zu einer entgegengesetzt zur Ausrichtbewegung verlaufenden Belastungsrichtung, nahezu senkrecht ausgerichteten Planflächen bestehen, wobei die Stufen durch stumpfwinkelig zu den Planflächen verlaufende Abschnitte verbunden sind. Diese Ausgestaltung bewirkt, daß die auf die Keilflächen wirkenden Normalkräfte durch die senkrechten Planflächen übertragen werden, während bei einer Verstellung die Keilflächen miteinander in Wirkbeziehung ein Verstellen der Formschlußelemente bewirken.To reset the locking mechanism by the sash weight Another embodiment is to prevent large wings the invention that the wedge surfaces offset from step-like lying, to an opposite to the alignment movement load direction, almost vertical aligned plan areas exist, the levels by Sections running at an obtuse angle to the plane surfaces are connected. This configuration causes the on Normal forces due to the vertical Flat surfaces are transferred while making an adjustment the wedge surfaces interacting with each other adjusting the Effect form-locking elements.

Eine besonders einfache Ausgestaltung sieht vor, daß eine der Keilflächen einteilig mit einem fest mit der Drehachse verbundenen Scharnierrahmen ausgebildet ist. Dies reduziert den notwendigen Montageaufwand erheblich.A particularly simple embodiment provides that one of the Wedge surfaces in one piece with a fixed to the axis of rotation connected hinge frame is formed. This reduces the necessary assembly work considerably.

Alternativ kann auch vorgesehen werden, daß die Formschlußelemente aus plattenförmigen Bauteilen bestehen und die Begrenzungskanten nahezu rechtwinklig zur Belastungsrichtung verlaufen.Alternatively, it can also be provided that the Form-fit elements consist of plate-shaped components and the boundary edges almost perpendicular to Direction of loading.

Die Erfindung sieht weiterhin vor, daß die Formschlußelemente durch eine Kraftspeichervorrichtung in die die Scharnierteile gegeneinander sperrende Lage gebracht werden. Dadurch soll evtl. zwischen den Formschlußelementen wirkende Reibung od. dgl. überwunden werden.The invention further provides that the positive locking elements through an energy storage device into which the hinge parts mutually blocking position are brought. This is supposed to any friction or odor acting between the positive locking elements Like. Be overcome.

Eine bevorzugte Ausgestaltung sieht dabei weiterhin vor, daß eines der Scharnierteile als Scharnierarm ausgebildet ist, der einerends mit einem die Scharnierachse bildenden Lagerbolzen fest und anderenends mit dem flügelfesten Scharnierteil - Winkelteil -zumindest längsverschieblich verbunden ist. Diese Ausgestaltung betrifft vor allem Dreh- und Drehkippflügel mit handelsüblichen Beschlägen, die so nachträglich mit selbsttätig wirkender Verstellung ausgestattet werden sollen.A preferred embodiment also provides that one of the hinge parts is designed as a hinge arm, the one with a hinge pin forming the hinge axis fixed and at the other end with the wing-fixed hinge part - Angled part is at least longitudinally connected. This Design relates above all to turn and tilt and turn sash commercially available fittings, which subsequently with automatic effective adjustment should be equipped.

Eine andere Ausgestaltung ist möglich, wenn eines der Scharnierteile als rahmenfester Lagerbock ausgebildet ist, während das zweite mittels des Ausrichtelementes bewegte Scharnierteil durch den Lagerbolzen gebildet wird und wenn die Formschlußelemente über einen Kraftspeicher, insbesondere über eine Feder miteinander verbunden sind.Another configuration is possible if one of the Hinge parts is designed as a frame-fixed bearing block, while the second moved by means of the alignment element Hinge part is formed by the bearing pin and when the Positive locking elements via a force accumulator, in particular via a spring are connected.

In diesem Fall findet die Verriegelung bzw. der Formschluß nicht am Flügel sondern am Rahmen statt, so daß die Vorrichtung insgesamt am Rahmen befestigt ist. Bei einer derartigen Ausgestaltung ist es vorteilhaft, daß die den Lagerbolzen umschließenden Lageraugen quer zur Drehachse - in der Rahmenebene - langlochförmig ausgebildet sind und daß die Formschlußelemente zwischen den Schmalseitenwänden der Lageraugen und dem Lagerbolzen angeordnet sind. Auch hierbei sieht eine vorteilhafte Ausgestaltung vor, daß die Schmalseitenwände und die Formschlußelemente mit aneinanderliegenden Keilflächen versehen sind. Eine rechte und linke Verwendbarkeit eines derartigen Lagerbocks ist gegeben, wenn die zwei Lageraugen symmetrisch auf einer Basisplatte angeordnet sind. In diesem Fall kann der Lagerbock sowohl für rechts als auch für links zu öffnende Fenster verwendet werden.In this case, the locking or positive locking takes place not on the wing but on the frame, so that the device overall is attached to the frame. With such a Design, it is advantageous that the bearing pin enclosing bearing eyes transverse to the axis of rotation - in the Frame level - are elongated and that the Interlocking elements between the narrow side walls of the Bearing eyes and the bearing pin are arranged. Here too provides an advantageous embodiment that the Narrow side walls and the positive locking elements with adjacent wedge surfaces are provided. A right and such a bearing block can be used on the left, if the two bearing eyes are symmetrical on a base plate are arranged. In this case, the bearing block can be used for both can be used on the right as well as for windows that can be opened on the left.

Eine besonders einfache Ausgestaltung eines derartigen Lagerbocks sieht vor, daß die Kraftspeichervorrichtung als Zugfeder ausgebildet ist. Diesen kann zwischen den beiden Formschlußelementen liegen und zwischen diesen wirksam sein.A particularly simple embodiment of such Bearing block provides that the energy storage device as Tension spring is formed. This can be between the two Form-fit elements lie and be effective between them.

Alternativ zu den vorstehenden Ausführungen kann auch vorgesehen sein, daß die Verriegelungsvorrichtung aus einer entgegen der Ausstellvorrichtung sperrenden Rastvorrichtung besteht. Diese wirkt ebenfalls formschlüssig, verhindert jedoch ein Zurückgleiten der Scharnierteile in die Stellung vor der Ausrichtbewegung.As an alternative to the above, can also be provided that the locking device from a locking device locking against the opening device consists. This also works positively, but prevents it a sliding back of the hinge parts in the position in front of Alignment movement.

Alternativ zu den beschriebenen formschlüssigen - mechanisch wirksamen - Verriegelungsvorrichtungen ist es möglich, daß die Verriegelungsvorrichtung aus einem hydraulischen Zylinder besteht, dessen Einlaßventil entgegen der Ausrichtbewegung sperrt und mit der Ausrichtbewegung ein Medienzufluß zum Zylinder bewirkt.As an alternative to the described positive - mechanical effective - locking devices, it is possible that the Locking device from a hydraulic cylinder exists, the inlet valve against the alignment movement blocks and with the alignment movement a media inflow to Cylinder causes.

Die Figuren zeigen einige Ausführungsbeispiele der Vorrichtung. Es zeigt

Fig. 1
eine schematische Skizze eines Fensters, einer Tür od. dgl.,
Fig. 2
eine obere Scharieranordnung,
Fig. 3
einen Längsschnitt durch eine Scharnieranordnung nach Fig. 1 in vergrößerter Teilansicht,
Fig. 4
Fig. 3 mit einer dazu teilweise verstellten Scharnieranordnung,
Fig. 5
einen Ausschnitt der Scharnieranordnung am senkrechten Schenkel,
Fig. 6
ein Formschlußelement nach den Fig. 2 und 3 in vergrößertem Maßstab,
Fig. 7
eine Ausstellvorrichtung eines Drehkippfensters mit plattenförmigen Bauteilen in Drauf- und Seitenansicht,
Fig. 7a und 7b
eine Kraftspeichereinrichtung zur Verlagerung der plattenförmigen Bauteile nach Fig. 7,
Fig. 8a und 8b
einen rahmenfesten Lagerbock in Drauf- und Seitenansicht.
The figures show some embodiments of the device. It shows
Fig. 1
a schematic sketch of a window, a door or the like,
Fig. 2
an upper hatchling arrangement,
Fig. 3
2 shows a longitudinal section through a hinge arrangement according to FIG. 1 in an enlarged partial view,
Fig. 4
3 with a partially adjusted hinge arrangement,
Fig. 5
a section of the hinge arrangement on the vertical leg,
Fig. 6
a form-locking element according to FIGS. 2 and 3 on an enlarged scale,
Fig. 7
an opening device of a tilt and turn window with plate-shaped components in top and side views,
7a and 7b
an energy storage device for displacing the plate-shaped components according to FIG. 7,
8a and 8b
a frame-fixed bearing block in top and side view.

Fig. 1 zeigt ein Fenster 1 bestehend aus einem festen Rahmen 2 und einem darin sowohl um eine vertikale Drehachse 3 als auch um eine horizontale Drehachse 4 schwenkbaren Flügel 5. Der Rahmen 2 und der Flügel 5 sind über ein oberes Scharnier 6 und ein unteres Scharnier 7 miteinander verbunden.1 shows a window 1 consisting of a fixed frame 2 and one in it both about a vertical axis of rotation 3 and wings 4 pivotable about a horizontal axis of rotation 5 Frame 2 and the wing 5 are via an upper hinge 6 and a lower hinge 7 connected to each other.

Die Ausgestaltung sieht dabei vor, daß das obere Scharnier 6 als sogenanntes Scherenlager ausgestaltet ist, während das untere Scharnier 7 als sogenanntes Ecklager ausgeführt ist. Der Flügel 5 weist zur Verriegelung in dem Rahmen 2 einen - hier nicht dargestellten - Verriegelungsbeschlag auf, der über einen Handhebel 8 am Flügel 5 bedient werden kann. Bei einer Ausführung des Verriegelungsbeschlags aus Drehkippbeschlag ist über den Handhebel 8 auch die Möglichkeit für eine Schwenkbewegung um die untere horizontale Drehachse 4 einstellbar. An dem oberen waagerechten Flügelholm 9 ist in diesem Fall eine Ausstellvorrichtung mit einem senkrecht zur Flügelebene beweglichen Ausstellarm befestigt, der den oberen waagerechten Flügelholm 9 mit dem oberen Scharnier 6 verbindet. Am unteren waagerechten Flügelholm 10 ist dabei zwischen Rahmen 2 und Flügel 5 eine - hier nicht sichtbare - Kippverriegelung wirksam, so daß die untere waagerechte Flügelkante 11 am Rahmen 2 gehalten ist.The design provides that the upper hinge 6th is designed as a so-called scissor store, while the lower hinge 7 is designed as a so-called corner bearing. The Wing 5 has one for locking in the frame 2 - here not shown - locking fitting on a Hand lever 8 on the wing 5 can be operated. At a The locking fitting is made of a tilt and turn fitting via the hand lever 8 also the possibility for one Swiveling movement around the lower horizontal axis of rotation 4 adjustable. On the upper horizontal wing spar 9 is in this case, an opening device with a perpendicular to Wing-level movable extension arm attached to the upper horizontal wing spar 9 connects to the upper hinge 6. At the lower horizontal wing spar 10 is between the frame 2 and wing 5 a - not visible here - tilt lock effective so that the lower horizontal wing edge 11 on the frame 2 is held.

Im dargestellten Ausführungsbeispiel ist angedeutet, daß die Rahmenholme des Rahmens 2 und die Flügelholme des Flügels 5 nicht parallel verlaufen, sondern sich durch längere Benutzung, Verschleiß od. dgl. in eine antiparallele Lage verschoben haben. Dadurch ist ein zwischen dem Flügel 5 und dem Rahmen 2 in der - angedeuteten - Ausgangslage 12 bestehender Abstand der Falzflächen 13, 14 - die sogenannte Falzluft oder das Kammermaß 15 - in einzelnen Bereichen auf ein Minimum reduziert. Daher kommt es beim Schließen des Flügels 5 beispielsweise aus der Drehstellung zum Klemmen.In the illustrated embodiment, it is indicated that the Frame spars of the frame 2 and the wing spars of the wing 5 do not run in parallel, but through prolonged use, Wear or the like is shifted to an antiparallel position to have. This is a between the wing 5 and the frame 2nd in the - indicated - starting position 12 existing distance of Folded surfaces 13, 14 - the so-called folded air or the chamber dimension 15 - reduced to a minimum in individual areas. Therefore it comes when closing the wing 5, for example, from the Rotary position for clamping.

Daher wird beispielsweise am unteren waagerechten Rahmenholm 16 ein Ausrichtelement 17 vorgesehen, das mit der Falzfläche 14 des Flügels 5 oder einem - hier nicht dargestellten-lagefesten Bauteil derart zusammenwirkt, daß der ursprünglich beabsichtigte Abstand der Falzflächen 14, 13 sich beim Schließen des Flügels 5 wieder einstellt. Das Ausrichtelement 17 besteht dabei im einfachsten Fall aus einem mit einer in Bewegungsrichtung aufsteigenden Auflaufschräge ausgestatteten Auflauf, welches mit der Falzfläche 14 des Flügels zusammenwirkt. Der Flügel 5 erhält durch das Ausrichtelement 17 seine ursprüngliche Ausgangslage 12, bei der die Rahmen- und Flügelholme parallel zueinander liegen. Beim Öffnen des Flügels 5 jedoch sackt die vordere Flügelkante 18 wieder nach unten, sobald die Falzfläche 14 von dem Ausrichtelement 17 abrutscht. Therefore, for example, on the lower horizontal frame beam 16 an alignment element 17 is provided which is in contact with the fold surface 14 of the wing 5 or one - not shown here - fixed Component interacts in such a way that the original intended distance of the folding surfaces 14, 13 at Closing of the wing 5 again. The alignment element In the simplest case, 17 consists of one with an in Equipped with ascending ramp Casserole, which with the fold surface 14 of the wing interacts. The wing 5 receives through the alignment element 17th its original starting position 12, in which the frame and Wing spars are parallel to each other. When opening the wing 5 however the front wing edge 18 sags again, as soon as the fold surface 14 slips off the alignment element 17.

Ist der Flügel 5 so weit antiparallel ausgerichtet, daß die Falzfläche 14 nicht mehr die Auflaufschräge des Ausrichtelementes 17 trifft, kann der Flügel 5 nur noch durch manuelles Anheben der vorderen Flügelkante 18 in den Rahmen 2 eintauchen.Is the wing 5 aligned so far antiparallel that the Folding surface 14 no longer the run-up slope of the Alignment element 17 hits, the wing 5 can only by manually lifting the front wing edge 18 into the frame 2 plunge.

Drehkippbeschläge sehen daher vor, daß an dem oberen Scharnier 6 manuelle Verstellmöglichkeiten angebracht sind, die zum Wiederherstellen der Ausgangslage 12 dienen.Tilt and turn fittings therefore provide that on the upper hinge 6 manual adjustment options are attached to the Restore the starting position 12 serve.

Fig. 2 zeigt eine obere Scharnieranordnung 20, die aus einem flügelfesten Winkelbauteil 21, einem dazu querbeweglich gelagerten Scharnierarm 22, einem an dessen Ende befestigten und vor die Rahmenebene ragenden Kupplungsteil 23 sowie einem rahmenfesten, auf der Rahmensichtfläche 24 befestigten Lagerbock 25 besteht, wobei der Lagerbock 25 und das Kupplungsteil 23 über einen Lagerzapfen 26 schwenkbar verbunden sind.Fig. 2 shows an upper hinge assembly 20, which consists of a wing-fixed angle component 21, one movable transversely thereto mounted hinge arm 22, one attached to the end and in front of the frame plane projecting coupling part 23 and a fixed to the frame, fixed on the frame visible surface 24 Bearing block 25, the bearing block 25 and that Coupling part 23 pivotally connected via a bearing pin 26 are.

Bei dem in Fig. 2 dargestellten Ausführungsbeispiel einer Scharnieranordnung 20 handelt es sich um einen reinen Drehbeschlag, bei dem nur eine vertikale Drehachse 3 vorgesehen ist. Die Befestigung des Winkelbauteils 21 erfolgt dabei in einer in die Falzfläche 14 eingebrachten Beschlagnut 27. Der Scharnierarm 22 ist über die Zapfen 28, 29 mit dem Winkelbauteil 21 verbunden, wobei der Zapfen 29 fest in dem Winkelbauteil 21 verankert ist und den Scharnierarm 22 in einem Langloch 30 durchgreift und diesen mit einem Pilzkopf 31 sichert. Der Zapfen 28 ist exzentrisch drehbar in dem Winkelbaurteil 21 gelagert und durchgreift das Winkelbauteil 21 in einem Langloch 32 und besitzt ebenfalls einen Pilzkopf 33. Die exzentrische Lagerung des Zapfens 28 dient dabei zur Erzielung eines größeren Andrucks des Flügels 5 an den Rahmen 2, d.h., eine Verlagerung der Flügelebene zur Rahmenebene hin. Dazu entspricht das Langloch 30 in seiner Querabmessung nahezu dem Durchmesser des Zapfens 29, so daß der Scharnierarm 22 beim Betätigen des Zapfens 28 durch einen darin eingebrachten Werkzeugeingriff 34 um den als Drehachse wirksamen Zapfen 29 verschwenkt wird, wodurch sich die Flügelebene gegenüber der Rahmenebene verlagert.In the embodiment shown in Fig. 2 one Hinge arrangement 20 is a pure one Rotary fitting, in which only one vertical axis of rotation 3 is provided is. The angle component 21 is fastened in here a fitting groove 27 introduced into the rebate surface 14 Hinge arm 22 is on the pin 28, 29 with the Angle component 21 connected, the pin 29 fixed in the Angle component 21 is anchored and the hinge arm 22 in one Passes through slot 30 and this with a mushroom head 31st guaranteed. The pin 28 is rotatable in the eccentric Angle component 21 is mounted and extends through the angle component 21 in an elongated hole 32 and also has a mushroom head 33. The eccentric mounting of the pin 28 is used for Achieving a greater pressure of the wing 5 on the frame 2, i.e. a shift of the sash level towards the frame level. For this purpose, the oblong hole 30 almost corresponds in its transverse dimension the diameter of the pin 29 so that the hinge arm 22 at Actuation of the pin 28 by an inserted therein Tool engagement 34 around the pin 29 acting as the axis of rotation is pivoted, whereby the wing plane is opposite the Frame level shifted.

Die Scharnieranordnung 20 im dargestellten Ausführungsbeispiel weist ebenfalls eine manuell zu betätigende Stellschraube 35 auf, die in Längsrichtung des Scharnierarms 22 wirkt. Diese ist mit einem - nicht sichtbaren - Gewinde am Ende eines Stellstücks 36 in Eingriff, andererseits jedoch durch ihre Lage am Kupplungsteil 23 und über den Lagerzapfen 26 ortsfest mit dem Rahmen 2 verbunden.The hinge arrangement 20 in the illustrated embodiment also has a manually operated adjusting screw 35 on, which acts in the longitudinal direction of the hinge arm 22. This is with a - not visible - thread at the end of a Actuator 36 in engagement, but on the other hand by their location on the coupling part 23 and over the bearing pin 26 with stationary connected to the frame 2.

Eine Betätigung der Stellschraube 35 bewirkt dabei, daß der Scharnierarm 22 bezüglich der ortsfesten Stellschraube 35 längs verschoben wird, so daß die Falzflächen 13, 14 eine parallele Lage erhalten können. Dazu gelangt zumindest der Zapfen 29 an eine Endkante des Langlochs 30 so daß der Flügel 5 über das Winkelbauteil 21 mit dem Scharnierarm 22 verschoben wird.An actuation of the screw 35 causes the Hinge arm 22 with respect to the fixed screw 35 lengthways is moved so that the fold surfaces 13, 14 a parallel Able to maintain location. For this purpose, at least the pin 29 arrives an end edge of the slot 30 so that the wing 5 over the Angle component 21 is moved with the hinge arm 22.

Das Fenster 1 weist darüber hinaus ein - hier nicht sichtbares - Ausrichtelement 17 auf, welches den Flügel 5 in der Verschlußstellung - d.h. beim Eintauchen des Flügels 5 in den Rahmen 2 - in eine parallele Lage ausrichtet. Wird der Flügel 5 durch das Ausrichtelement 17 verschoben bzw. angehoben, dann wird das Winkelbauteil 21 relativ zum Scharnierarm 22 so lange bewegt, bis die Falzflächen 13, 14 parallel stehen und sich die Falzluft bzw. das Kammermaß 15 in seiner normalen Größe einstellt. Durch dies Ausrichtbewegung wird auch der Scharnierarm 22 entlastet, der, da ortsfest über den Lagerzapfen 26 mit dem rahmenfesten Lagerbock 25 verbunden, die Ausrichtbewegung nicht mit vollführt. Dadurch wird ein Formschlußelement 37 im Bereich des Stellstücks 36 frei beweglich, welches einerseits eine in Richtung Kupplungsteil 23 weisende Ausnehmung 38 durchgreift, jedoch senkrecht zur Falzfläche 14 verschiebbar angeordnet ist, andererseits mit einer Keilfläche 39 an einer komplementär dazu gestalteten Keilfläche 40 des Stellstücks 36 anliegt. Window 1 also shows - not here visible - alignment element 17, which the wing 5 in the closed position - i.e. when immersing the wing 5 in align the frame 2 - in a parallel position. Will the Wing 5 moved or aligned by the alignment element 17 raised, then the angle member 21 is relative to Hinge arm 22 moves until the rebate surfaces 13, 14th stand parallel and the rebate clearance or the chamber dimension 15 in its normal size. Through this alignment movement is also relieved of the hinge arm 22, which, because it is stationary the bearing pin 26 is connected to the frame-fixed bearing block 25, the alignment movement is not carried out. This will make a Form-locking element 37 is free in the area of the adjusting element 36 movable, which on the one hand in the direction of the coupling part 23 pointing recess 38 passes through, but perpendicular to Fold surface 14 is slidably arranged, on the other hand with a wedge surface 39 on a complementary Wedge surface 40 of the actuator 36 abuts.

Wie Fig. 3 in einem vergrößerten Ausschnitt der Fig. 2 deutlich macht, durchgreift das Formschlußelement 37 die gemeinsame Ausnehmung 38 des Scharnierarms 22 und des Stellstücks 36 sowie eine, Ausnehmung 38a im Winkelbauteil 21.As shown in FIG. 3 in an enlarged detail of FIG. 2 clearly makes, the form-locking element 37 passes through the common Recess 38 of the hinge arm 22 and the actuator 36 and a, recess 38a in the angular component 21.

Die nahezu lotrechte Rückseite des Formschlußelementes 37 liegt dabei zumindest im Bereich der Ausnehmung 38a des Winkelbauteils 21 formschlüssig an diesem an.The almost vertical back of the form-locking element 37 lies at least in the area of the recess 38a of the Angular component 21 in a form-fitting manner on this.

Um die Anlagefläche des Formschlußelementes 37 an dem Winkelbauteil 21 zu vergrößern ist die Ausnehmung 38a mit einem Ende fluchtend mit dem senkrechten Schenkel 46 ausgeführt.To the contact surface of the form-locking element 37 on the Angle component 21 is enlarged with a recess 38a Aligned at the end with the vertical leg 46.

Wird, wie bereits beschrieben, durch das Ausrichtelement 17 die Ausrichtbewegung des Winkelbauteils 21 in Richtung R vollzogen, wird das Formschlußelement 37 frei und zwar in einem Maße, der dem Betrag entspricht, in dem - hier nicht sichtbare - vordere Flügelkante 18 angehoben wird. Durch die Zugfeder 41 wird das Formschlußelement 37 nach unten gezogen, so daß sich - entsprechend der Keilwirkung - die neue, gespreitzte Lage des Scharnierarms 22 bezüglich des Winkelbauteils 21 einstellt. Beim nächsten Öffnen des Flügels 5 wird das als Verriegelungselement wirkende Formschlußelement 37 entgegen der Richtung R belastet, wobei es formschlüssig zwischen dem Winkelbauteil 21 und dem Scharnierarm 22 liegt und dieses zueinander, entgegen der Richtung R der Ausrichtbewegung, in Lastrichtung lagefixiert, also verriegelt. In Richtung R bleibt die Verriegelung weiterhin lösbar.As already described, is the alignment element 17 Alignment movement of the angular component 21 in the direction R, the positive locking element 37 is free to an extent that corresponds to the amount in which the front - not visible here Wing edge 18 is raised. The tension spring 41 Form-locking element 37 pulled down so that - according to the wedge effect - the new, spread position of the Hinge arm 22 adjusts with respect to the angle component 21. The next time you open wing 5, it will be called Locking element acting form-locking element 37 against the Direction R loaded, it being a form fit between the Angle component 21 and the hinge arm 22 and this to each other, against the direction R of the alignment movement, in Load direction fixed, i.e. locked. In the R direction the lock can still be released.

Fig. 4 zeigt die Scharnieranordnung 20 entsprechend der Fig. 3, bei der die selbsttätige Ausrichtung bereits wirksam wurde. Wie insbesondere in Verbindung mit Fig. 3 sichtbar ist, wird durch das Eintauchen des Formschlußelements 37 die relative Lage des Scharnierarms 22 bezüglich des Winkelbauteils 21 verändert, so daß der Abstand zwei beliebig gewählter Punkte auf jedem Bauteil - hier anhand der Falzfläche 14 und der Begrenzungskante 42' des Stellstücks 36 dargestellt - ändert. 4 shows the hinge arrangement 20 corresponding to FIG. 3, where the automatic alignment has already taken effect. How is particularly visible in connection with Fig. 3, by the immersion of the positive locking element 37, the relative position of the Hinge arm 22 changed with respect to the angle component 21, see above that the distance between two arbitrarily chosen points on each Component - here based on the fold surface 14 and the Boundary edge 42 'of the actuator 36 shown - changes.

Fig. 3 und 4 zeigen auch, daß die Zugfeder 41 an einem Ende an dem Formschlußelement 37 angreift und an dem entgegengesetzten Ende ein Widerlager an einem Zapfen 42 erhält. Soll beispielsweise die selbsttätige Justierung zurückgenommen werden, so kann durch eine Öffnung 43 ein Werkzeug 44 oder ähnliches eingeführt werden und das Formschlußelement 37 entgegen der Zugfeder 41 nach oben verschoben werden und eine gewünschte Ausrichtlage des Flügels 5 bezüglich des Rahmens 2 mit der Stellschraube 35 neu eingestellt werden. Sowohl die Stellschraube 35 als auch die Öffnung 43 sind dabei nur in geöffnetem Zustand des Flügels 5 erreichbar.3 and 4 also show that the tension spring 41 at one end the form-locking element 37 engages and on the opposite End receives an abutment on a pin 42. Should For example, the automatic adjustment is withdrawn through a hole 43, a tool 44 or Similar introduced and the positive locking element 37th against the tension spring 41 are moved up and a Desired alignment position of the wing 5 with respect to the frame 2 can be reset with the adjusting screw 35. Both the Set screw 35 and the opening 43 are only in open state of the wing 5 accessible.

Das Formschlußelement 37 kann - wie Fig. 5 zeigt - auch durch einen Stopfen 45, der in der Öffnung 43 einsitzt, fixiert werden. Dies ist beispielsweise bei der Montage der Scharnieranordnung 20 sinnvoll, um den Verstellbereich der automatischen Justierung zu wahren. Der Stopfen 45 ragt dazu durch den Schenkel 46 des Winkelbauteils 21 hindurch und berührt mit seiner Mantelfläche 47 das untere Ende 48 des Formschlußelementes 37 in dessen Ausgangslage. Der Stopfen 45 wird gemäß dieser Ausgestaltung erst nach Montage des Flügels 5 am Rahmen 2 aus der Öffnung 43 entfernt, so daß das Formschlußelement 37 erst dann beweglich wird.The positive locking element 37 can - as shown in FIG. 5 - also by a plug 45, which is seated in the opening 43, fixed become. This is for example when assembling the Hinge arrangement 20 makes sense to the adjustment range of automatic adjustment. The plug 45 protrudes through the leg 46 of the angle component 21 and touches with its lateral surface 47 the lower end 48 of the Form-locking element 37 in its initial position. The stopper 45 According to this configuration, it is only after the wing 5 is installed removed on the frame 2 from the opening 43, so that the Form-locking element 37 only becomes movable.

Fig. 6 zeigt das Formschlußelement 37 in einem vergrößerten Maßstab. Das Formschlußelement 37 weist eine Keilform auf, auf der stufenförmige Absätze 50 angeordnet sind. Durch diese Anordnung der stufenförmigen Absätze 50 wird erreicht, daß bei einer in Richtung R wirkenden Last die Planflächen 51 nahezu senkrecht belastet werden und keine das Formschlußelement 37 senkrecht zur Richtung R und entgegen der Richtung F resultierende Kraftkomponente entsteht, die bei schweren Flügeln 5 ein Entweichen des Formschlußelementes 37 nach oben - entgegengesetzt zur Richtung F - bewirken könnte. Die Tiefe 52 der Absätze 50 bestimmt das minimal mögliche Maß, mit dem die Ausrichtbewegung des Ausrichtelementes 17 fixiert werden kann. Je geringer diese Tiefe 52 gewählt wird, um so feinere Ausrichtbewegungen können fixiert und beibehalten werden. Fig. 6 shows the form-locking element 37 in an enlarged Scale. The form-locking element 37 has a wedge shape the stepped shoulders 50 are arranged. Through this Arrangement of the step-shaped paragraphs 50 is achieved in that a load acting in the R direction, the flat surfaces 51 almost are loaded vertically and none form-locking element 37 perpendicular to the R direction and counter to the F direction resulting force component arises when heavy Wings 5 an escape of the positive locking element 37 upwards - opposite to direction F - could cause. The depth 52 of paragraphs 50 determines the minimum possible measure with which the alignment movement of the alignment element 17 can be fixed can. The smaller this depth 52 is chosen, the finer Alignment movements can be fixed and retained.

Um ein Verschieben der gegeneinander liegenden Planflächen 51 zu erleichtern, können die Planflächen 51 durch stumpfwinklig zu den Planflächen 51 verlaufende, phasenartige Abschnitte 53 verbunden werden.To shift the flat surfaces 51 lying opposite one another to facilitate, the flat surfaces 51 by obtuse angles phase-like sections 53 running to the flat surfaces 51 get connected.

Fig. 7 zeigt ein Ausführungsbeispiel einer Ausstellvorrichtung eines Drehkippfensters, wobei die als Verriegelungselemente wirkenden Formschlußelemente 37 aus plattenförmigen Bauteilen bestehen, die in einer Öffnung 55 des Stellstücks 36 nebeneinander geschichtet liegen. Die Formschlußelemente 37 sind dabei an ihrer Unterseite von Federelementen beaufschlagt. Wird der das Stellstück 36 verschiebbar führende und übergreifende Ausstellarm 56 durch die Ausrichtkraft in Richtung R - zusammen mit dem Flügel 5 - bewegt, so decken sich die Öffnung 57 im Ausstellarm 56 und die Öffnung 55 im Stellstück 36 teilweise. Erreicht die Deckung ein lichtes Maß, das größer ist als die Stärke eines der Formschlußelemente 37, so wird dieses unter Einwirkung des unterhalb angeordneten Federelements nach oben verschoben und verriegelt den Ausstellarm 56 gegenüber dem dazu verschiebbar angeordneten Stellstück 36 entgegen der Richtung R.7 shows an embodiment of an opening device a tilt and turn window, the as locking elements acting form-locking elements 37 made of plate-shaped components exist in an opening 55 of the actuator 36th lie next to each other in layers. The positive locking elements 37 are loaded on their underside by spring elements. Is the actuator 36 slidably leading and overlapping extension arm 56 by the aligning force in Direction R - together with wing 5 - moves, so overlap the opening 57 in the extension arm 56 and the opening 55 in Actuator 36 partially. If the cover reaches a clear dimension, that is greater than the strength of one of the form-locking elements 37, so this is arranged under the influence of the one below Spring element moved up and locked the Extension arm 56 with respect to that arranged displaceably Actuator 36 against the direction R.

Da der Ausstellarm 56 beim Einwirken des - nicht sichtbaren-Ausrichtelements 17 kraftfrei ist, werden keine großen Federkräfte durch die Federelemente notwendig. Daher kann eine Ausgestaltung entsprechend der Fig. 7a gewählt werden, bei dem die Federelemente aus Federzungen 58 bestehen, die zueinander parallel verlaufenden und durch einen gemeinsamen querverlaufenden Steg 59 verbunden sind und das Formteil 60 bilden. Das Formteil 60 läßt sich durch Stanzen od. dgl. aus einem Federstahl herstellen und wird am Stellstück 36 befestigt.As the extension arm 56 when the - not visible - alignment element acts 17 is powerless, will not be large Spring forces required by the spring elements. Therefore one Design are selected according to Fig. 7a, in which the spring elements consist of spring tongues 58 which are mutually parallel and by a common transverse web 59 are connected and the molded part 60 form. The molded part 60 can be stamped or the like produce a spring steel and is on the actuator 36th attached.

Um die maximale Bewegung der Formschlußelemente 37 zu begrenzen, ist der Ausstellarm 56 - auch zur Vermeidung des Eindringens von die Beweglichkeit der Formschlußelemente 37 beeinträchtigenden Schmutz - mit einer dünnwandigen Abdeckung 61 verschlossen. Diese dünnwandige Abdeckung 61 kann beispielsweise aus einem abnehmbaren Kunststoff- oder Blechteil gebildet werden.To the maximum movement of the positive locking elements 37 limit, the extension arm 56 - also to avoid the Penetration of the mobility of the interlocking elements 37 impairing dirt - with a thin-walled cover 61 closed. This thin-walled cover 61 can for example from a removable plastic or sheet metal part be formed.

Fig. 8a und Fig, 8b zeigen ein schematisiertes Ausführungsbeispiel der Erfindung, bei dem die Formschlußelemente 37 in einem ortsfest am Rahmen 2 gelagerten Lagerbock 70 geführt werden. Eine Bandrolle 71 ist dabei in Querrichtung fest mit einem - nicht dargestellten - Ausstellarm einer Ausstellvorrichtung oder ähnlichem verbunden. Dazu ragt ein Ausleger 72 der Bandrolle 71 bis vor die - hier auch nicht dargestellte - Falzfläche 13 des Rahmens 2. Die Bandrolle 71 umgreift einen Lagerbolzen 73, der in einer langlochförmigen Lageraugen 74 des Lagerbocks 70 parallel zur Rahmenebene geführt ist. Dazu weist der Lagerbock 70 Lageraugen 74 auf, in denen die Formschlußelemente 37 längs der Mittelachse des Lagerbolzens 73 geführt werden. Die Lageraugen 74 sind an einem Ende mit den Keilflächen 40 versehen, die zur Mittelquerachse 75 des Lagerbocks 70 hin die Wandstärke des Lagerauges 74 vergrößern. Die Formschlußelemente 37 sind ebenfalls mit Keilflächen 39 versehen, die in entgegengesetzter Richtung verlaufen, so daß die dem Lagerbolzen 73 zugewandten, mit einem Kreissegment 76 versehenen seitlichen Begrenzungskanten 77 der Formschlußelemente 37 parallel zum Lagerbolzen 73 verlaufen.8a and 8b show a schematic Embodiment of the invention in which the Form-locking elements 37 in a fixed position on the frame 2 Bearing block 70 are performed. A tape roll 71 is in Transverse direction fixed with a - not shown - extension arm an opening device or the like connected. It sticks out a cantilever 72 of the tape roll 71 up to the - not here either shown - folding surface 13 of the frame 2. The tape roll 71st engages around a bearing pin 73 which is in an elongated hole Bearing eyes 74 of the bearing block 70 parallel to the frame plane is led. For this purpose, the bearing block 70 has bearing eyes 74, in which the positive locking elements 37 along the central axis of the Bearing pin 73 are performed. The bearing eyes 74 are on one Provide the end with the wedge surfaces 40 to the central transverse axis 75 of the bearing block 70 the wall thickness of the bearing eye 74 enlarge. The form-locking elements 37 are also with Wedge surfaces 39 provided in the opposite direction run so that the bearing pin 73 facing, with a Circular segment 76 provided lateral boundary edges 77 of the Form-locking elements 37 run parallel to the bearing pin 73.

Durch das Zusammenwirken des - hier nicht dargestellten Flügels 5 mit dem ebenfalls nicht dargestellen Ausrichtelement 17-wird die starr in der Ebene des Flügels 5 mit diesem verbundene Bandrolle 71 zusammen in dem von der Bandrolle 71 umschlossenen Lagerbolzen 73 in Richtung R verschoben. Die durch die Kraftspeichereinrichtung in Form einer Feder 78 verbundenen Formschlußelemente 37 werden frei und können sich unter Einwirkung der Feder 78 aufeinander zu bewegen bis sie sich - aufgrund der Keilflächen 39, 40 - mit den Kreissegmenten 76 wieder an den - durch die Bandrolle 71 bewegten - Lagerbolzen 73 anlegen und dessen neue, durch das Ausrichtelement 17 bewirkte Lage, fixieren bzw. verriegeln. Through the interaction of the wing - not shown here 5 with the alignment element 17, also not shown the rigidly connected in the plane of the wing 5 with this Tape roll 71 together in that enclosed by the tape roll 71 Bearing pin 73 moved in the R. The through the Energy storage device connected in the form of a spring 78 Form-locking elements 37 are free and can under Action of the spring 78 to move towards each other until they move - Due to the wedge surfaces 39, 40 - with the circular segments 76 again on the - moved by the band roller 71 - bearing pin 73 create and its new, through the alignment element 17th caused position, fix or lock.

Das dargestellte Ausführungsbeispiel weist gegenüber den vorstehend beschriebenen Ausführungsbeispielen den Vorteil auf, daß die Flügelbauteile nahezu unverändert belassen werden können. Auch sind außerhalb der Falzluft 15 angebrachte Vorrichtungen nicht den knappen Platzverhältnissen anzupassen und lassen sich leicht durch eine geeignete Abdeckkappe od. dgl. den optischen Gegebenheiten anpassen.The illustrated embodiment has compared to the embodiments described above have the advantage that the wing components are left almost unchanged can. Also 15 are attached outside of the air gap Do not adapt devices to the limited space available and can be easily od with a suitable cover cap. Adapt to the optical conditions.

Die Basisplatte 79 des Lagebocks 70, wie im dargestellten Ausführungsbeispiel zu erkennen, ist symmetrisch bezüglich der Mittelquerachse 75 ausgestaltet, so daß der Lagerbock 70 sowohl für nach rechts öffnende Flügel 5 wie auch nach links öffnende Flügel 5 verwendet werden kann.The base plate 79 of the bracket 70 as shown in FIG Recognizing the embodiment is symmetrical with respect to Central transverse axis 75 designed so that the bearing block 70 both for wing 5 opening to the right as well as to the left opening Wing 5 can be used.

Nur der Form halber sei darauf hingewiesen, daß auch in diesem Beispiel die miteinander wirkenden Keilflächen 39, 40 des Formschlußelementes 37 und des Lagerauges 74 mit entsprechend senkrecht zur Belastungsrichtung verlaufenden Planflächen 51 versehen sein kann.Just for the sake of form, it should be noted that this too Example the interacting wedge surfaces 39, 40 of the Form-locking element 37 and the bearing eye 74 with accordingly Flat surfaces 51 running perpendicular to the direction of loading can be provided.

Der Form halber sei auch darauf hingewiesen, daß auch hierbei bekannte, manuelle Justiervorrichtungen im Bereich der Ausstellschere weiterhin Verwendung, z.B. zur Grundjustage, finden können.For the sake of form, it should also be pointed out that here too known, manual adjustment devices in the field of Stay scissors still used, e.g. for basic adjustment, can find.

Es sei ergänzend darauf hingewiesen, daß es bei sehr schweren Flügeln 5 von Vorteil ist, wenn das Formschlußelement 37 beispielsweise nach Fig. 2 bis 5 mit der lotrechten Rückseite möglichst großflächig am senkrechten Winkelschenkel 46 des Winkelbauteils 21 anliegt um ein Verkanten bzw. Verwinden des Winkelbauteils 21 zu verhindern.It should also be noted that it is very severe Wings 5 is advantageous if the positive locking element 37 for example according to Fig. 2 to 5 with the vertical back as large as possible on the vertical angle leg 46 des Angle component 21 bears against a tilting or twisting of the Prevent angular component 21.

Daher kann auch vorgesehen sein, daß der Winkelschenkel 46 eine in die Ausnehmung 38 hineinragende Verlängerung aufweist und/oder daß das Formschlußelement 37 längs der Falzfläche 14 des Winkelsschenkels 46 geführt ist. Dadurch würde auch das Verschieben der Formschlußelemente 37 gegenüber dem Stellstück 36 begünstigt.Therefore, it can also be provided that the angle leg 46 a has an extension projecting into the recess 38 and / or that the interlocking element 37 along the fold surface 14 of the angle leg 46 is guided. This would also do that Moving the form-locking elements 37 relative to the actuator 36 favors.

Claims (13)

  1. A device for aligning a leaf (5) of a door, a window, or the like, relatively to a fixed frame (2), the leaf (5) and frame (2) being interconnected pivotally, at least about a vertical pivot axis (3), by way of a pivot axis, the position of which is adjustable relatively to the frame (2) and which is formed by hinge elements (6, 7), the hinge element consisting of at least two hinge parts movable relatively to one another, a first part being in a fixed location in the frame (2) and a second being associated in a fixed position with the leaf (5), with an alignment element (17) which produces an alignment movement and which acts at least in a surface-parallel position of the leaf (5) and frame (2),
    characterised by
    one or more locking elements (37) acting automatically between the hinge parts and fixing the position of the hinge parts relatively to one another and locking them against the alignment movement, the hinge parts being movable relatively to one another by means of the alignment element (17) .
  2. A device according to claim 1, characterised in that the locking elements consist of positive engagement elements (37) and in that the positive engagement elements (37) are disposed movably between boundary edges of the hinge parts, said boundary edges moving away from one another as a result of the alignment movement.
  3. A device according to claim 2, characterised in that the positive engagement elements (37) are provided with wedge surfaces (39, 40), the latter abutting one another and the positive engagement elements (37) being disposed so as to be movable relatively to one another transversely of the direction (R) of the load.
  4. A device according to any one of claims 1 to 3, characterised in that the wedge surfaces (39, 40) consist of plane surfaces (51) which are staggered after the style of steps and which are aligned substantially perpendicularly to a loading direction extending in opposition to the alignment movement, the steps being connected by sections (53) extending at an obtuse angle to the plane surfaces (51).
  5. A device according to any one of claims 1 to 4, characterised in that one of the wedge surfaces (40) is made in one piece with a hinge arm (22) rigidly connected to the pivot (3).
  6. A device according to claim 2, characterised in that the positive engagement elements (37) consist of components in the form of plates and the adjoining boundary edges extend substantially perpendicularly to the loading direction.
  7. A device according to claim 3 or 6, characterised in that the positive engagement elements (37) are brought by a force storage device into the position in which the hinge parts are locked relatively to one another.
  8. A device according to claim 1, characterised in that one of the hinge parts is constructed as a hinge arm (22) one end of which is rigidly connected to a bearing pin (26) forming the hinge axis while: the other end is connected so as to be at least longitudinally displaceable to the hinge part fixed to the leaf - angle component (21).
  9. A device according to claim 1, characterised in that one of the hinge parts is constructed as a bearing block (70) fixed to the frame, while the second hinge part moved by the alignment element (17) is formed by the bearing pin (73) and in that the positive engagement elements (37) are interconnected via a force storage means.
  10. A device according to claim 9, characterised in that the bearing bosses (74) enclosing the bearing pin (73) are formed as a slot transversely of the pivot axis - in the frame planes - and in that the positive engagement elements are disposed between the narrow side walls of the bearing bosses (74) and the bearing pin (73).
  11. A device according to claim 9 or 10, characterised in that the narrow side walls and the positive engagement elements (37) are provided with abutting wedge surfaces (39, 40).
  12. A device according to any one of claims 9 to 11, characterised in that two bearing bosses (74) are disposed symmetrically on a baseplate (79).
  13. A device according to any one of claims 9 to 12, characterised in that the force storage device is constructed in the form of a tension spring (78).
EP98102033A 1997-04-30 1998-02-06 Automatic adjusting device Expired - Lifetime EP0875651B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19718325A DE19718325C1 (en) 1997-04-30 1997-04-30 Adjuster for aligning door and window hinge
DE19718325 1997-04-30

Publications (3)

Publication Number Publication Date
EP0875651A2 EP0875651A2 (en) 1998-11-04
EP0875651A3 EP0875651A3 (en) 2000-07-19
EP0875651B1 true EP0875651B1 (en) 2004-01-28

Family

ID=7828263

Family Applications (1)

Application Number Title Priority Date Filing Date
EP98102033A Expired - Lifetime EP0875651B1 (en) 1997-04-30 1998-02-06 Automatic adjusting device

Country Status (4)

Country Link
EP (1) EP0875651B1 (en)
AT (1) ATE258642T1 (en)
DE (2) DE19718325C1 (en)
PL (1) PL326100A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015003931B3 (en) * 2015-03-25 2015-11-12 Siegenia-Aubi Kg Joint belt arrangement

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE20120613U1 (en) 2001-12-14 2002-04-04 Gretsch-Unitas GmbH Baubeschläge, 71254 Ditzingen hinge
DE102014101218A1 (en) * 2014-01-31 2015-08-06 Maco Technologie Gmbh fitting assembly
DE202016002166U1 (en) 2016-04-07 2017-07-10 Siegenia-Aubi Kg fitting assembly
DE202023100930U1 (en) 2023-02-28 2023-03-08 Siegenia-Aubi Kg fitting arrangement

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE327608C (en) * 1920-10-14 Franz Werner Automatic door or window support to avoid lowering door or window leaves
DE2065840C3 (en) * 1970-08-05 1983-12-22 Winkhaus, August, 4404 Telgte Opening device for tilting and swiveling sashes
DE3637077C1 (en) * 1986-10-31 1988-02-04 Siegenia Frank Kg Hinge joint for windows, doors or the like.
DE4117407C2 (en) * 1991-05-28 1995-01-05 Bilstein August Gmbh Co Kg Tilt & Turn hardware

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015003931B3 (en) * 2015-03-25 2015-11-12 Siegenia-Aubi Kg Joint belt arrangement
EP3073039A1 (en) 2015-03-25 2016-09-28 Siegenia-Aubi Kg Top hinge alignment

Also Published As

Publication number Publication date
DE19718325C1 (en) 1998-08-13
PL326100A1 (en) 1998-11-09
EP0875651A3 (en) 2000-07-19
EP0875651A2 (en) 1998-11-04
DE59810645D1 (en) 2004-03-04
ATE258642T1 (en) 2004-02-15

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