EP1245771A1 - Hinge for doors or windows - Google Patents

Abstract

The hinge (10.3) has a horizontal position adjustment device comprising an adjustment screw in contact with the engagement section of the hinge flap (15) extending into the gap between the frame and wing. The screw is supported at right angles by a frame member extending at right angles to this gap. The adjustment position of the screw is held in place by the pressing of the hinge flap against this frame member. The hinge comprises a part (11.3) for securing to the frame, a part for securing to the wing pivotally connected to the frame part via a pivot bearing axle (13), and a hinge flap with a bearing hole (14) for receiving the pivot bearing axle. The hinge has a horizontal position adjustment device for altering the distance between the bearing hole and a frame member extending at right angles to the gap between the wing and frame.

Description

The invention relates to a door or window hinge with the features of the preamble of claim 1.

A hinge with the features mentioned above is well known. The horizontal adjustment device is one Elongated plate resting on the frame spar, which is in contact with relocate an eccentric on the frame spar to the side leaves. The plate has sloping surfaces on which the band tab is supported with appropriate inclined surfaces and in different distances to the frame rail can, why fastening screws of the hinge flap through the Plate is screwed into the frame spar. Around an undesirable slippage of the band tab on the plate To prevent both are in the area of their inclined surfaces a groove preventing this slipping. The Structure of this known horizontal adjustment device complex and the adjustment is tedious, because when adjusting Levels must be observed, which are caused by the slipping preventing grooves are formed. The operation of the horizontal adjustment device is accordingly tedious and you Setup is complicated.

In contrast, the invention is based on the object to improve a tape with the characteristics mentioned at the beginning, that with simple means a reliable horizontal adjustment of the tape is possible.

The above task is characterized by the characteristics of the Characteristic part of claim 1 solved. It is particularly advantageous the use of an adjusting screw that in conventional Reliably operated with simple tools can be. The adjustment screw allows a stepless To adjust. It can be short, because its length in is essentially determined by the thickness of the band tab, in which it intervenes, plus the maximum adjustment path which for horizontal adjustment devices is only a few millimeters. The relative position of the adjustment screw is simple Secure means because it is supported on the frame spar. For this, it is sufficient to strike the hinge tab on the frame rail, through which the adjusting screw is loaded so that it can no longer twist. This results at the same time a simple structure of the horizontal adjustment device.

In the sense of a simplification of the construction the band can be provided that the adjusting screw is screwed into the center of the hinge. The length of the Adjusting screw is minimized and the load is applied within the wall thickness of the band tab. The regarding the hinge tab results in the central arrangement of the adjusting screw an advantageous symmetrization, that of an even distribution of burdens is useful.

It is particularly preferred that between the band tab and the frame spar to be attached to the latter There is a screw-on plate with a hinge edge is articulated. The screw-on plate is for one Base provided that the attachment of the Band tab on the frame spar ensures. The articulated connection between the screw-on plate and the band flap edge for a proper holding of the band tab in the sense of a Keep the bearing eye straight at different distances of the tape tab from the frame spar.

It can be advantageous if the ligament flap and / or the mounting plate continuously from a common joint have decreasing wall thickness. In the area of the joint can then take loads into account, sufficient thick wall thicknesses are provided and yet the Band lobe or its bearing eye comparatively close to the Frame spar can be pivoted.

The hinge can be equipped so that a common Hinge of the hinge plate and the screw-on plate with one joint hinge pin or with an offset of the Hinge is formed, in which the screw plate is articulated is attached. The pin is a stable and proven joint component, that the cohesion of the ligament flap and its Top plate always guaranteed after it is factory made was produced. An assembly of the band tab and its Screw-on plate made possible by cranking the hinge flap an inexpensive manufacture of the tape, as well a simple and inexpensive assembly, the Cohesion of the band parts and the load on the screw-on plate about the cranking of the hinge after assembly are guaranteed.

The screw-on plate can be of different designs Be used to further constraints the construction and the application of the horizontal adjustment device to suffice. It is advantageous if one Bolt-on plate is an arm of a handlebar parallelogram that an adjustment of the hinge flap parallel to the screw-on plate allows. With such a tape, relocations are possible of the wing perpendicular to the frame plane avoided because of Band tabs exactly parallel to the end face of the frame spar can be held to which the screw-on plate is attached becomes.

A further advantageous embodiment of the tape can be in it exist that a top plate is an arm of a two-armed Scissors is the one adjustment parallel to the screw-on plate of the band flap. They also apply here the advantages mentioned above. The Components of the two-armed scissors are, however, compared to Handlebar parallelogram less numerous and can be more robust be trained so that this tape for larger loads suitable is.

An expedient embodiment of the band is thereby characterized in that a screw plate parallel to the bearing axis protrudes above the hinge and with a protruding plate section is firmly screwed to the frame spar. Thereby is the screw-on area of the screw-on plate from the movement area of the hinge tab so that the operation the horizontal adjustment device completely independent of the fastening the mounting plate on the frame spar.

Furthermore, it can be provided that a screw-on plate band flap encompassing and / or engaging in the band flap Has holding ribs. The holding ribs serve the Stabilization of the ligament flap. The stabilization takes place either at the enclosed edges of the band flap or through positive engagement a retaining groove in the band tab. Tilting of the band flap is prevented in all cases, so that its bearing eye even with large loads are held precisely in the predetermined axis position can.

A particularly simple embodiment of the band results itself when the adjusting screw is in a screwless plate Band flap is screwed in the area of his Lifting means a tilting movement of the belt tab on the frame rail permissible tilting bead. Because the one carried by the hinge Bearing eye is at a distance from the tilting bead Tilting movements of the hinge flap in such a way that the bearing eye arranged more or less from the frame spar is, so that a corresponding horizontal adjustment takes place.

To the adjustment position of the adjusting screw with simple to secure constructive means, the tape is designed so that the hinge against a support effect of Adjusting screw on the frame rail and / or on a screw-on plate is attached.

A special design of the door or window hinge, which in particular has the features of claim 1, is characterized in that a threaded part of the wing hinge is supported on the frame hinge, and is in threaded engagement with the bearing eye and with the Swivel bearing axis having rotary adjustment means with a positive rotation is coupled. With this configuration of the A vertical adjustment is made possible with which the Horizontal adjustment device via the bearing eye in different vertical positions of the wing hinge positioned can be. This is a combined adjustment of the Wing not only horizontally in the plane of the wing or in the plane of the frame possible, but also vertically in the plane of the frame. This embodiment of the door or Window tape leads to a very slim design, at that from the pivot bearing axis in the radial direction in the area the thread engagement requires only two components are, namely by absorbing the weight of the Wing-bearing eye and consequently wing-loaded bearing eye Threaded part on which the bearing eye over the Thread engagement is supported. For the rest, the slenderness of the Band only by the dimensions of the pivot bearing axis certainly.

It serves the simplicity of building the band, though the threaded part with a threaded end directly on the frame hinge is supported. As a result, the bearing eye of the wing hinge the frame band closely adjacent, so that also a height adjustment of the bearing eye is only an optically immaterial Gap between the bearing eye of the wing hinge and that of the frame band is available. That applies equally for two-part belts as for three-part belts.

If a belt is made in three parts, it can be an advantage be that the threaded part of the wing hinge with a gap bearing bush engaging the bearing eye of the wing hinge is in positive engagement, which is a gapless upper bearing eye of the frame hinge connects. The gap closure bush avoids an open or deep gap between the upper end of the bearing eye of the wing hinge and the lower end of the bearing eye of the upper part of the frame hinge up to the swivel bearing axis. In addition, the gap closure bushing for additional radial support of the Swivel bearing axis in the upper area of the bearing eye of the sash hinge to care.

In the sense of an improved support of the pivot bearing axis in the radial direction it is advantageous if the band the bearing eye of the wing hinge in its two-part design averted from the frame hinge with a radially fixed cap is in which the threaded part engages radially supported. This will result in a more even distribution of loads of the wing hinge or the pivot bearing axis in their allows upper area.

In addition, the tape can be designed so that the threaded part with the gap closure bushing or with the radial one Cap is in threaded or locking engagement, or is relatively displaceable in it. A vertically fixed connection between the threaded part and the gap closure bush or the cap is particularly advantageous if one such connection with the bearing eye is missing. The positioning this secures the socket or cap. if the Vertical position of these components secured in another way is, the threaded part can be relatively displaceable in them his.

Fig.1

einen Querschnitt durch ein dreiteiliges Drehband im Bereich der Schwenklagerachse,

Fig.1a

eine von Fig.1 abweichende Detailausbildung,

Fig.2

eine perspektivische Darstellung des Flügelbandes der Fig.1,

Fig.3

eine perspektivische Darstellung des Rahmenbandes der Fig.1,

Fig.4

eine perspektivische Darstellung eines Rahmenbandes eines zweiteiligen Drehbandes,

Fig.5

einen der Fig.1 entsprechenden Schnitt durch ein zweiteiliges Band,

Fig.5a

eine bezüglich der Fig.5 abweichende Detailausbildung,

Fig.6a

bis 6f Stirnseitenansichten unterschiedlicher Ausbildungsformen von ähnlich Fig.2 ausgebildeten Flügelbändern,

Fig.7

eine weitere Stirnseitenansicht eines Flügelbandes in spezieller Ausgestaltung, und

Fig.8

einen schematischen Querschnitt durch zwei Rahmenholme mit zwischen beide eingreifenden Bandlappen eines Drehbandes.

The invention is explained with reference to exemplary embodiments shown in the drawing. It shows:

Fig.1

a cross section through a three-part hinge in the area of the pivot bearing axis,

1a

a detailed training deviating from FIG. 1,

Fig.2

2 shows a perspective illustration of the wing hinge of FIG. 1,

Figure 3

2 shows a perspective illustration of the frame hinge of FIG. 1,

Figure 4

1 shows a perspective illustration of a frame hinge of a two-part hinge,

Figure 5

1 corresponding section through a two-part band,

5a

a detailed training which deviates from FIG. 5,

6a

to 6f end views of different forms of formation of wing hinges similarly designed in FIG. 2,

Figure 7

another end view of a wing hinge in a special embodiment, and

Figure 8

a schematic cross section through two frame spars with between two engaging band tabs of a rotating belt.

The Fig.1.5 show hinges 10.2,10.3 for doors that each from a frame volume 11.2, 11.3 and from a Assemble sash hinge 12. One frame strap each 11.2 or 11.3 is with a wing hinge 12 via a pivot bearing axis 13 articulated. A bearing of the pivot bearing axis 13 serve the bearing eyes 14,34,36 and 37. They are each worn by band rags. The wing hinge 12 has one of a hinge 15 worn bearing eye. The frame straps 11.2, 11.3 are designed differently. The frame band 11.2 is part of a two-part hinge with 10.2 a single bearing eye 37 of its frame hinge 11.2. The Frame band 11.3 has two spaced apart Bearing eyes 34, 36 carried by band tabs 38 and with a Connecting web 39 with one another via the band tabs 38 are connected. These bearing eyes 34, 36 take between them the bearing eye 14 of the wing hinge 12. They make one special resilient bearing for the pivot bearing axis 13, wherein in particular tipping loads transversely to the axis 13 absorbed be as they are particularly heavy wing occur when opening.

The installation of the window strips 10.2, 10.3 is carried out in accordance with Figure 8. Two frame bars 18, 19 form one between them Folding space 20, in which the band tabs 15, 38 engage, so that on the facing end walls of the frame bars 18,19 can be attached in the manner shown. there is a bearing roller formed by the bearing eyes 14,34,36 and 37 40 in a constant position with respect to the frame spar 18 of a fixed frame spar. An engagement section 16 of the band tab 15 can be relative to the frame spar 19 of a wing are attached so that this frame spar 19 and thus the wing more or less distance from Frame spar 18 has, that is, horizontally in the plane of representation the Fig.8 or horizontally in a plane that of the Frame spar 18 formed closed frame becomes. It is assumed that the role 40 and thus the axis of rotation of the wing is arranged vertically.

Attach adjustable to the sash hinge 12 on the frame spar 19 to so that the distance of the frame spar 19 from Frame spar 18 can be adjusted by a few millimeters in the desired manner FIGS. 2,6a to 6f and 7 show in particular special training. The formation of the wing bands 12 2 and 6a to 6f have in common that the band tab 15th or its engagement section 16 with a screw-on plate 21 is assembled.

The screw plate 21 is located directly on the rebate 20 mainly forming end wall of the frame spar 19, as Fig. 7 indicates, but for an engagement section 16 without screw-on plate 21. The screw-on plate is attached to the frame spar. For this it has plate sections 28, the top and bottom over the elongated top plate 21 project parallel to the bearing axles. In the plate sections 28 are screw holes 41 through which Fixing screws, not shown, in the frame rail 19 be screwed and the screw plate 21 immovable establish. Accordingly, the band tab 15 is also fixed, the articulated with the screw plate 28 is.

The formation of the articulated connection of the two is different. Fig.2 shows a hinge pin 24 which is used for formation of a joint 23 is used by being in joint eyes 28 'of the plate sections 28 and an intermediate one Eyelet of the band flap edge 22 engages. Corresponding joints 23 are also in the embodiments of Figures 6a to 6c given.

Similar joints 23 'with hinge pins 24 are also at the embodiments of Figures 6d, 6e available. Here is the Screw-on plate 21, similar to FIG. However, it is not or not exclusively with the engagement section 16 connected. In Fig.6d are the screw-on plate 21 and the engaging portion 16 are not directly with each other connected. Rather, the engagement section 16 is by means of of a joint 23 'via a link 42 on the screw-on plate 21 articulated, which also with a joint 23 ' has a further link 43 which is connected to the engagement section 16 is articulated. This kinematics ensures that the Engagement section 16 and thus the bearing eye 14 always exactly parallel to the mounting surface of the screw-on plate 21 to be led.

A corresponding parallel guidance results from the Embodiment of Figure 6e, in which a pair of scissors 27 is used is, in which the screw plate 21 forms a scissor arm and has a joint 23 'on the screw plate side. Of this joint 23 'extends at least one further Arm 43 to a joint 23 ', on which the engagement portion 16th attacks. In this case, the engaging portion 16 can be moved so that it is in Fig.6e, except in the vertical the display level, also moved to the right. Compared for this purpose, the bearing eyes 14 or those carrying them move Engagement sections 16 with a component in the representation plane to the left. In all cases this component is practically negligible small.

Fig. 6f shows a special training in that the mechanical cohesion of the screw plate 21 with the Engagement section 16 by means of an offset 25 of the band tab 15 is formed. The crank 25 clasps you Articulated bead 44, which is designed so that the screw-on plate 21 and the engagement section 16 in a starting position can lie flat against each other.

6c shows an embodiment in which the engaging section 16 and the screw plate 21 from the joint 23 to the bearing eye 14 continuously decreasing wall thicknesses exhibit. The facing outer surfaces of the mounting plate 21 and the engaging portion 16 form mutually parallel arrangement an angle α. This can be too be made zero when the engaging portion 16 is complete is folded against the screw plate 21. In this In this case, the bearing eye 14 can be adjusted further in the minus direction are, so towards the sash 19.

Fig. 6b shows with a bearing rib parallel to the bearing eye 29 a special feature for positive assembly with the Engagement section 16, on the one hand in coordination thereon has a groove 16 'and on the other hand a rib 16' ', so that vertical wing loads are better absorbed in Fig. 6b can by holding the rib 29 on the components 16 ', 16' 'supports and thus relieves the joint 23.

This can further relieve the band flap 15 achieved that retaining ribs 29 on the screw plate 21st are formed, namely on the over the band tab 15th protruding plate sections 28. The shown in Fig.2 Retaining ribs 29 encompass the end edges of the engagement section 16, which wing loads occurring here on the top plate 21 and thus transferred to the frame spar 19.

All the above-described embodiments of wing hinges 12 is an adjusting screw 17 common, which in Fig.6a is shown by way of example. The adjusting screw 17 has On the rebate side, an adjustment engagement 17 'and on the frame spar side an annular collar 17 '' which is inserted into the screw-on plate 21 is. The collar 17 '' prevents the engaging portion 16 is folded away from the screw-on plate 21, if there are corresponding loads on the bearing eye 14, since the adjusting screw 17 is screwed into the engagement section 16 is. The screwing depth can be adjusted by adjusting the Adjustment screw 17 can be changed. Depending on the direction of rotation the engagement section 16 moves away from the screw-on plate 21, the adjusting screw 17 being supported on the frame rail 19, or the engagement section 16 becomes the screw-on plate 21 pulled out and is in an end position on this on. The engagement conditions described above are at given all embodiments of Figures 6a to 6f. It is to point to Fig.2, where it is shown that the adjusting screw 17 in the center with respect to the band tab 15 or in relation is arranged on the screw plate 21. So that results there is a symmetrical distribution of load forces the other symmetrically formed components of the wing hinge 12th

An exemplary embodiment is shown in FIG which in turn has an adjusting screw 17 in the band tab 15 or is screwed into its engagement section 16. It However, a screw-on plate 21 is missing of slings, which are designed as a screw hole 45 are present, a tilting bead 30. The tilting bead 30 is a projection which is on the end wall of the frame spar 19th abuts, as well as the adjusting screw 17. If the latter screwed out of the engagement section 16, so tilted this and thus the bearing eye 14 in a counterclockwise direction the point of contact of the tilting bead 30 on the frame spar 19, so that the bearing eye 14 reaches the dotted position 14 '. Also in this way a horizontal adjustment of the wing can be achieved, bearing in mind that the wing for Frame is relatively movable, so that in reality does not result in a different position 14 ', but the sash frame spar 19 according to the deviation shown in FIG. 7 is adjusted and thus adjusted.

1 and 5 is the assembly of the wing hinge 12 with the frame hinge 11.2 or 11.3. The bearing eye 14 of the wing hinge 12 is coaxial with the bearing eyes 34,36 of the frame band 10.3 arranged. In the bearing eye 14, a threaded part 31 is used, namely a sleeve a cross section which is non-circular at least over a length section, into which a correspondingly non-round length section 13 ' the pivot bearing axis 13 is installed. As a result a rotational adjustment movement of the pivot bearing axis 13, for example via a front hexagon recess 46 is initiated with a suitable key to which Threaded part 31 are transmitted.

A rotary movement of the threaded part 31 can be used for this be, the bearing eye 14 and thus the entire wing hinge 12 higher or lower to adjust. This is the threaded part 31 provided with a threaded end 32 with which it itself on the lower bearing eye 36 of the frame hinge 11.3 or is supported on its bearing sleeve 36 '. The bearing sleeve 36 'takes a lower end of the pivot bearing axis 13 during which upper end in a bearing sleeve 34 'of the upper bearing eye 34 is supported radially. A vertical support for the swivel bearing axis 13 is not shown, but can for example can be reached by a locking screw in the area of the bearing eye 14 clamped transversely on the pivot bearing axis 13 and preferably engages in a circumferential groove, which creates a vertical form fit.

The threaded part 14 or its threaded end 32 has one External thread, which are screwed into the bearing eye 14 can. For this purpose, the bearing eye 14 is at its lower end a thread 47 is formed. At the top of the bearing eye 14 there is a recess 48, that of the lower end corresponds to the bearing eye 14. However, the illustration shows no thread on. In the recess 48 is one Gap closure bushing 33 used without in the - not shown - engage thread. The bearing eye 14 could also provided with an internal thread over the entire length his. The aforementioned gap closure bush is with an internal thread 49 provided, in which an upper thread end 50 of Threaded part 31 is screwed. The order is made that the total distance between the bearing eyes 34, 36 with the threaded part 31 and the gap closure bushing 33 is bridged. As a result, 14 are above the bearing eye to the bearing eye 34 and below the bearing eye 14 to the bearing eye 36 only very narrow, in the extent of the adjustment stroke the vertical adjustment device of a few millimeters Column can be seen which is the respectability of the whole Do not significantly affect the tape. An assembly the bearing of Fig.1 must be done so that the threaded end 32 is completely unscrewed from the bearing eye 14 and the Gap closure bushing 33 fully inserted into the bearing eye 14 and screwed to the upper threaded part end 50 have to be. Then the threaded part 32 can be screwed into the thread 47 be, the gap closure bushing 33rd unscrewed upwards on the upper threaded part 50. The bearing eye 14 comes into the middle position shown.

1a shows a locking engagement between an upper one Thread part end 50 'and a gap closure bushing 33. Instead the upper end of the threaded part 50 'carries a thread Annular collar 51, which is form-fitting in an annular groove of the socket 33 engages so that this is always in the position shown is held and the upper end of the bearing eye 14 on the outer circumference the bushing 33 slides when the threaded part 31 is rotated is and the bearing eye 14 a correspondingly upwards or slides down.

The gap closure sleeve 33 does not only do one extensive gap between the bearing eye 34th and the bearing eye 14, but also a radial support the upper part of the bearing eye 14 and the pivot bearing axis 13 against each other, so that a corresponding even distribution of radial forces over the length of the bearing eye 14 he follows. A correspondingly even distribution of support or load forces should also be achieved if the band 10.2 is formed only in two parts. In this Case is the bearing eye 14 of Figure 5 above with a cap 35 closed, which has an annular collar 35 ', the axially parallel is formed with the pivot bearing axis 13 and in a Recess 48 of the upper end of the bearing eye 14 engages. The upper threaded part end 50 'is threadless and engages appropriately in the collar 35, so that here radial support between the bearing eye 14 and the threaded part 31 takes place in the radial direction via the collar 35 '.

Fig.5a shows one of Fig.5 with respect to the conclusion with a cap 35 similar training, but with the threaded part end 50 'with the cap 35 or with its ring collar 35 'is in locking engagement. For this purpose, the threaded part end has 50 ' Similar to Fig.1a an annular collar 51, which in an annular groove Ring cuffs 35 'engages. Vertical adjustments of the bearing eye 14 'then lead to slight relative changes in position with respect to the cap 35. If this is to be avoided, the locking engagement described can be abandoned and the cap 35 in a thread not shown in Fig.5a in the area the recess 48 of the upper end of the bearing is screwed in, so that relative adjustments are not visible to the outside Way between the cap 35 and the upper end of the threaded part 50 '.

Claims (16)

Door or window hinge (10.2, 10.3) with a frame hinge (11.2, 11.3) and with a wing hinge (12) articulated to it by means of a swivel bearing axis (13), with a hinge (14) containing the swivel bearing axis (13) 15) of the frame (11.2, 11.3) or sash hinge (12) which, with an engagement section (16), is able to engage in a rebate space (20) formed between two frame spars (18, 19) and there is attached to one of the frame spars (19 ) and a horizontal adjustment device which allows the distance of the bearing eye (14) from a frame spar (19) to be set transversely to the rebate space (20), characterized in that the horizontal adjustment device engages in the rebate space (20) on the engagement section (16) of the hinge flap (15) acting adjusting screw (17), which is supported transversely on the frame spar and whose setting position is to be secured by striking the hinge flap (15) on the frame spar (19). Band according to claim 1, characterized in that the adjusting screw (17) is screwed into the center of the band tab (15). Hinge according to claim 1 or 2, characterized in that between the hinge flap (15) and the frame spar (19) there is a screw-on plate (21) to be fastened to the latter, which is articulated to a hinge flap edge (22). Band according to one of claims 1 to 3, characterized in that the band tab (15) and / or the screw-on plate (21) have a continuously decreasing wall thickness from a common joint (23). Hinge according to one of claims 1 to 4, characterized in that a common hinge (23) of the hinge flap (15) and the screw-on plate (21) is formed with a common hinge pin (24) or with an offset (25) of the hinge flap (15) in which the screw-on plate (21) is hinged. Band according to one of claims 1 to 5, characterized in that a screw-on plate (21) is an arm of a parallelogram of the handlebars (26) which enables the band tab (15) to be adjusted parallel to the screw-on plate (21). Hinge according to one of claims 1 to 5, characterized in that a screw-on plate (21) is an arm of a two-armed scissors (27) which enables the belt flap (15) to be adjusted parallel to the screw-on plate (21). Hinge according to one of claims 1 to 7, characterized in that a screw-on plate (21) protrudes parallel to the bearing axis over the hinge flap (15) and is firmly screwed to the frame spar (19) with a protruding plate section (28). Hinge according to one of claims 1 to 8, characterized in that a screw-on plate (21) has retaining ribs (29) encompassing the hinge and / or engaging in the hinge (15). Hinge according to one of claims 1 to 9, characterized in that the adjusting screw (17) is screwed into a hinge-free hinge (15) which, in the region of its attachment means, allows the hinge (15) on the frame spar (19) to tilt the swivel bead (30). Has. Hinge according to one of claims 1 to 10, characterized in that the hinge flap (15) is fastened to the frame spar (19) and / or to a screw-on plate (21) against a supporting action of the adjusting screw (17). Hinge according to one of claims 1 to 11, characterized in that a threaded part (31) of the sash hinge (12) is supported on the frame hinge (11.2, 11.3) in such a way as to absorb the wing load and is in threaded engagement with the bearing eye (14) of the sash hinge (12) and is coupled in a rotationally positive manner to the pivot bearing axis (13) having rotary adjustment means. Hinge according to claim 12, characterized in that the threaded part (31) is supported directly on the frame hinge (11.2, 11.3) with a threaded end (32). Hinge according to claim 12 or 13, characterized in that the threaded part (31) of the wing hinge (12) is in positive engagement with a gap closure bushing (33) which engages in the bearing eye (14) and which fits without gap to an upper bearing eye (34) of the frame hinge (11.3) follows. Hinge according to claim 12 or 13, characterized in that the bearing eye (14) in a two-part design of the sash hinge (12) facing away from the hinge is provided with a radially fixed cap (35) into which the threaded part (14) engages in a radially supported manner. Band according to claim 14 or 15, characterized in that the threaded part (14) with the gap closure bush (33) or with the radially fixed cap (35) is in threaded or locking engagement, or is relatively displaceable therein.

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