EP0570945A1 - Concealed hinge - Google Patents

Abstract

What is provided is a hinge joint (4, 5), installed in a concealed manner, for tilting and pivoting wings (2) of windows and doors having a wing overlap (6, 22), in which hinge joint the pivot pin (12, 43) is arranged concealed in the region of the wing overlap, specifically in an interruption (8) of the seal (7) in the case of a metal frame (2) or in a recess (23) on the inside of the wing overlap (22) in the case of wooden or plastic windows (21), the interruption or recess terminating in both cases at a distance from the top edge or bottom edge of the wing overlap (6, 22), the said distance corresponding approximately to the width of the wing overlap itself. <IMAGE>

Description

The invention relates to a concealed hinge joint for tilting and pivoting sashes of windows and doors with sash flaps, in which the swivel axis lies in the area of the sash flap between the respective outer surfaces of the frame and the sash flap.

Concealed hinge joints are generally known. The installation takes place in a recess in the area of the wing, which rests on the fixed frame or bend frame in the closed position of the wing (cf. DE-OS'n 29 51 236 or 33 07 777). Such concealed hinge joints are also known for tilt and pivot sashes of windows and doors, in which the wing outside lies in the same plane as the outside of the frame, so that the wing rebate ends in a so-called shadow groove (see. DE-PS 23 30 874).

According to a proposal that has not been published beforehand, attempts have also been made to install such a hinge cover concealed in tilting and swiveling sashes with wing overlap, by working the wing overlap in the area of the wing corner on the inside to a small thickness, and in this way to both corners adjacent edges open recess a cap-shaped body eg made of plastic, in which the parts of the hinge joint which determine the pivot axis are accommodated.

It is an object of the invention to develop a concealed hinge joint for the purposes specified at the outset and with the features of the preamble so that this installation option consists not only of wooden windows, but also of metal windows or windows made of plastic profiles, caps or the like. Covering or reinforcing parts are not necessary and the sash weight can also be reliably transferred to the pivot frame in the area of the lower corner bearing via the swivel axis or the tilt axis.

This object is achieved by the teaching of claim 1.

The recess on the inside of the wing flap or the interruption of the seal arranged in the area of the wing flap ends in both cases for the upper bearing and for the lower bearing at a sufficient distance from the upper and the lower edge of the wing, this distance in essentially corresponds to the normal rollover width. The interruption or recess is thus only open in the area of the vertical wing rebate towards the wing edge, but not only closed to the upper and lower wing edge but arranged in such a way that the wing flap is stable and resilient even in this form without a cap or the like .

This design also allows such an arrangement of the tilt axis that the sash weight can be reliably transmitted regardless of the material of the frame or sash. The lower hinge joint is expediently designed according to the teaching according to claim 3 or according to the teaching according to claim 7. In the former case, the pivot axis between the frame-side hinge screw plate and the intermediate plate is effective, while the tilt axis between the intermediate plate and the wing-side hinge screw plate is effective. In this case, the lower hinge joint is thus formed in three parts, the parts being connected to one another in pairs by the two axes of movement of the wing.

The embodiment according to claim 7 offers the advantage of a large-area support of the wing for the tilting movements, namely in the region of the lower spar of the frame. This training offers the further advantage of an adjustment possibility of the wing in the direction of the tilt axis.

Regardless of the hinge joints according to claim 1 in conjunction with claim 2 or claim 7, claim 9 materializes the idea of the displacement of the orthogonal pivot / rotation axis against the tilt axis of the wing. The shift ensures that there is no longer a common point of intersection, as is the case with ball joints, for example. If the tilt axis is arranged in or on the frame, a recess for its concealed arrangement in the sash is unnecessary (claim 10). Specifically, claim 11 summarizes the arrangement strategy, the tilt axis is displaced or displaced inwards (perpendicular to the window frame plane) so far (in / on the window frame) that it no longer protrudes from the inner edge of the window frame. It is therefore provided in the inner edge area.

But not only is the tilting axis shifted so far inwards that it no longer protrudes, the pivoting / swiveling axis ("inside of the frame") is concealed and no longer protrudes. On the inside of the frame, both the pivot / pivot axis of the wing and the tilt axis are arranged, which means that no more bearings or hinges protrude from the wing or frame; the entire fitting is covered - following the arrangement principle of claims 9, 10, 11; which justifies its excellent optical effect - turn / tilt sash "without" (visible) fittings.

Technical outflow from this "basic principle" of the two mutually perpendicular axes of rotation, which are mutually displaced and concealed on the sash and bland frame, is a large number of specific fitting designs which are explained using exemplary embodiments.

Figur 1

in Vorderansicht ein Fenster mit Kipp- und Schwenkflügel und mit verdeckt eingebauten Scharniergelenken gemäß der Erfindung;

Figur 2

einen zur Schwenkachse parallelen Schnitt durch das Fenster nach Figur 1;

Figur 3

einen horizontalen Schnitt durch das Fenster nach Figur 1 im Bereich des unteren, verdeckt eingebauten Scharniergelenkes;

Figur 4

in entsprechender Darstellung nach Figur 3 das untere Scharniergelenk, das bei Holzrahmen verdeckt eingebaut ist;

Figur 5

einen der Figur 2 entsprechenden senkrechten Schnitt durch das Fenster nach Figur 4;

Figur 6

die Anordnung nach Figur 4 bei einem Fenster aus Kunststoffrahmen in gleicher Darstellung wie Figur 4;

Figur 7

einen zur Flügelebene parallelen Schnitt durch den Flügel im Bereich des unteren Ecklagers des Flügels nach Figur 4;

Figur 8

das untere Ecklager in der Kippstellung in perspektivischer Darstellung;

Figur 9

das Lager nach Figur 8 in auseinandergezogener perspektivischer Darstellung;

Fig. 10

das zugehörige obere Scharniergelenk des Flügels in perspektivisch auseinandergezogener Darstellung;

Fig. 11

in ähnlicher Darstellung wie Figur 7 eine abgewandelte Ausführungsform des verdeckt eingebauten Scharniergelenkes für das untere Ecklager;

Fig. 12

das Ecklager nach Figur 11 in perspektivischer Ansicht;

Fig. 13

das Ecklager nach Figur 11 in perspektivisch auseinandergezogener Darstellung;

Fig.14a und 14b

Querschnitte durch den Kipplagerbereich des Scharniergelenkes nach Figur 11 und

Fig.14c

einen Schnitt in einer zur Flügelebene orthogonalen Ebene, zur Darstellung eines eingebauten Scharniergelenkes nach Fig. 14a,b,

Fig.14d

einen horizontalen Schnitt im Bereich des unteren verdeckt eingebauten Scharniergelenkes und

Fig. 15

im Ausschnitt eine abgewandelte Ausführungsform des Lagers nach Figur 11.

The invention is explained in more detail below with the aid of schematic drawings using several exemplary embodiments.
Show it:

Figure 1

in front view a window with tilt and swivel wing and with concealed hinge joints according to the invention;

Figure 2

a section parallel to the pivot axis through the window of Figure 1;

Figure 3

a horizontal section through the window of Figure 1 in the area of the lower, concealed hinge joint;

Figure 4

in a corresponding representation according to Figure 3, the lower hinge joint, which is concealed in wooden frames;

Figure 5

a vertical section corresponding to Figure 2 through the window of Figure 4;

Figure 6

the arrangement of Figure 4 in a window made of plastic frame in the same representation as Figure 4;

Figure 7

a section parallel to the wing plane through the wing in the region of the lower corner bearing of the wing according to Figure 4;

Figure 8

the lower corner bearing in the tilted position in a perspective view;

Figure 9

the bearing of Figure 8 in an exploded perspective view;

Fig. 10

the associated upper hinge joint of the wing in a perspective exploded view;

Fig. 11

in a representation similar to FIG. 7, a modified embodiment of the concealed hinge joint for the lower corner bearing;

Fig. 12

the corner bearing of Figure 11 in perspective view;

Fig. 13

the corner bearing of Figure 11 in a perspective exploded view;

14a and 14b

Cross sections through the tilt bearing area of the hinge joint according to Figure 11 and

Fig. 14c

FIG. 14a, b shows a section in a plane orthogonal to the wing plane, to show a built-in hinge joint; FIG.

Fig. 14d

a horizontal section in the area of the lower concealed hinge joint and

Fig. 15

the cutout shows a modified embodiment of the bearing according to FIG. 11.

In the figures 1 to 3, a window formed from metal profiles is shown with tilting and swiveling sashes and sash flaps. The wing overlap 6 engages in a known manner in the closed position of the wing 2, the frame 1 on the outer surface lying on the room side. An actuating linkage is arranged in the casement in the usual way and can be actuated between the closed position, the tilted position and the pivoted position via the actuating handle 3 which can be moved into three positions. The sash is connected to the frame via an upper (4) and a lower (5) concealed hinge joint. FIG. 3 shows the concealed hinge joint serving as the lower corner joint. The hinge joint 5 is installed in such a way that the pivot axis 12 comes to rest between the wing overlap 6 and the outer surface of the frame 1 facing the interior of the room. The hinge joint has a hinge joint which can be screwed onto the hollow profile of the metal frame, for example, or a screw-on plate 13 which is pivotably connected to an intermediate plate 15 via the pivot axis 12. The intermediate plate 15 lies in the sash rebate 10 between the screw-on plate 13 of the frame and a screw-on plate 14 of the metal profile frame of the sash 2. The arrangement is such that the areas receiving the pivot axis 12 are in an interruption 8 of the seal lying in a profile groove 6a of the sash flap 6 7 is provided. It can be seen from FIG. 2 that the seal interruption 8 ends at a predetermined distance from the lower or upper rollover edge, which distance corresponds to the width of the rollover itself.

Figures 4 and 5 show the relationships previously described with a metal profile in wooden profiles. The frame is designated 20, the casement 21 and the rollover 22. Otherwise, the same reference numerals are used as in Figures 1 to 3. In this case, however, the hinge joints 4 and 5 are provided in recesses 23 on the inside of the flap flap 22. Here, too, the recesses 23 end at a distance 24 from the upper and lower rollover edges, which corresponds to the width 24 of the rollover.

FIG. 6 shows the same conditions in a representation according to FIG. 4 for frames made of plastic. The same reference numerals are used here as in FIG. 4, however, insofar as the parts differ from one another, with the addition of the letter "a".

FIGS. 9 and 10 show the concealed hinge joints used in the exemplary embodiments described above. According to FIG. 10, the upper hinge joint 4 has a screw-on plate 42 on the frame side, which is connected via the hinge pin 43 which forms the pivot axis 12 to a screw-on plate 40 on the sash frame side, which is connected to a stay arm 41 or stay scissors or the like arranged in the area of the upper wing side.

The lower concealed hinge joint 5 forms the lower corner bearing and has already been described essentially. Further details emerge from FIGS. 7, 8 and 9. It can be seen that the lower screw-on plate 16 on the frame side corresponds to the screw-on plate 42 of the upper hinge joint 4. The same also applies to the (lower) hinge pin 43 arranged in the pivot axis 12. In the lower hinge joint 5, the intermediate plate 15 is articulated via this hinge pin 43. In the area of its upper edge, this has an edge recess 30 which merges into an angular slot 31. The slightly curved slot section 31 corresponds to the relative movement of a guide pin 34 arranged on the wing-side screw-on plate 14 and provided with a head. In the example shown, a keyhole-like recess 32 is provided in the lower region of the intermediate plate 15, into which the pin 33 forming the tilt axis and provided with a head engages on the screw-on plate 14. Figure 8 shows the lower corner bearing in its tilted position. It can be seen that in this position the wing 2 is reliably secured against unhooking, the guide pin 34 and the slot section 31 forming the anti-lifting device. In the closed position, however, the parts can be unhooked by the pin 34 can be separated from the intermediate plate 15 via the edge recess 32 and the headed pin 33 via the extension of the recess 32.

The wing-side screw-on plate 14 engages with a reinforcing section 14a in the rebate profile groove of the wing frame 21, while an angled section 14b extends over the lower wing corner.

In the embodiment according to FIGS. 11 to 14, which show the lower corner joint, the intermediate plate is omitted. The cover plate-side screw-on plate 51 is pivotally connected directly to the wing-side screw-on plate 53 via the hinge pin 52. However, the screw-on plate 51 on the frame side is not fastened to the vertical spar of the window frame, but instead has an angled lower section 55. This extends over a significant length of the lower frame spar and is freely movable over its entire length on a screw-on plate 54 fixed to the lower frame spar. Its front edge is rounded and, together with section 55, forms the tilt axis 54a of the lower corner bearing 5. For this purpose, section 55 engages over slot-like recesses with sufficient play over conical or spherical pins 56, 57, which allow sufficient play for the tilting movement of the wing. One or both pins 56, 57 can have an anti-lift device. An adjusting eccentric 60 is arranged on the screw-on plate 54 and engages with its eccentric portion in a transverse recess in portion 55, so that an adjustment in the direction of the double arrow 61 is possible.

The wing-side screw-on plate 53 is designed as an angle piece and engages with a corresponding reinforcement 59 in the rebate groove of the wing, as illustrated in FIG. 11. Figure 14a shows the closed position, while Figure 14b shows the parts in the wing tilt position.

In all embodiments, the recesses or interruptions can be made and the hinge joints arranged so that a gap 65 remains between the hinge joint and the space-side outer surface of the frame 1, in which the remaining thickness of the sash rebate can engage when the sash is opened, so that the sash over the swivel axis can be opened up to almost 180 °; this is illustrated in FIG. 15.

The relationships of FIGS. 3, 8, 11 and 14a and 14b are illustrated in FIGS. 14c and 14d, with particular reference to the axes determining the movement of the wing 2 - the axis of rotation and the tilting axis. The axes form an orthogonal pair of axes, which allows the pivoting (rotation) of the wing 2 about the pivoting or rotating axis 12, 52 and the tilting of the wing 2 about the tilting axis 33, 54a. Both respective axes are orthogonal, but they are mutually crazy and do not have a common intersection. This applies to all regular movements and positions of the wing 2 with respect to the window frame 1. The displacement allows that the recesses 23 or 8 (see FIG. 2, FIG. 5) also in the lower rotary / tilting element 5 at a corresponding distance can end from the lower edge of the wing. For the tilt axis, there is therefore no need for a recess, which basically weakens the wing.

The extent of the displacement described above is designed such that the tilt axis 52 is displaced so far inward with respect to the axis of rotation 54a that it (the tilt axis) does not protrude from the inner edge of the frame. The latter applies when viewed in a plane perpendicular to the frame level.

With a suitable design of the screw-on plates 54 and 55, or of the section 55 of the screw-on plate 51, the tilt axis is displaced parallel to the frame level - when the wing 2 is tilted. The shift is slight and corresponds to the width of the lower rollover.

If a recess is not required for the tilt axis, which does not protrude from the inner edge of the frame, the recesses 8, 23 can end at a good distance from the lower edge of the wing, thus increasing the stability of the wing.

Claims (11)

Concealed hinge joint for tilting and swiveling sashes of windows and doors with sash flaps, in which the swivel axis in the area of the sash flap lies between the outer surfaces of the frame and the sash flap on the inside, characterized in that the hinge joint sections (4, 4) that determine the swivel axis (12) 5) project in the area of the flap (22) into a recess (23) on the inside of the flap (22) or into an interruption (8) of the seal (7) arranged on the inside of the flap (6), which recess ( 23) or interruption (8) each end at a distance corresponding to the rollover width (24) from the edge of the rollover (22) on the upper side and lower side of the wing. Concealed hinge joint according to claim 1, characterized in that the hinge joint sections (4, 5) determining the pivot axis (12) in the wing closing or wing pivot position are at a distance (65) from the outer side surface of the frame (1) which is at least corresponds to the thickness or the remaining thickness of the rollover (6) in the region of the recess (23) or in the region of the seal interruption (8). Concealed hinge joint according to claim 1 or 2, characterized in that for the lower corner joint (5) the hinge screw plate (13) on the frame side is articulated via the pivot axis (12) to an intermediate plate (15) which is also connected via the tilt axis (33) a wing-side hinge screw plate (14) is connected. Concealed hinge joint according to claim 3, characterized in that the tilt axis is determined by the bearing recess (32) and a bearing pin (33) engaging therein in the intermediate plate (15) and the wing-side screw plate (14). Concealed hinge joint according to claim 4, characterized in that the connection between the wing-side screw-on plate (14) and intermediate plate (15) is designed as a release connection for the wing (2) and at the same time as a release lock in the tilted position of the wing. Concealed hinge joint according to claim 5, characterized in that the bearing recess is an edge recess of the intermediate plate (15) or is designed in the form of a keyhole (32) and the intermediate plate (15) has a guide slot (30, 31) open to the edge of the intermediate plate has a guide pin (34) on the wing-side screw-on plate (14), the course of the guide slot being adapted to the movement of the guide pin (34) during the tilting movement. Concealed hinge joint according to claim 1 or 2, characterized in that for the lower corner joint (5) the hinge portion (51) of the hinge on the frame, which determines the pivot axis (52), extends along the horizontal bar of the frame (1) Section (55) is freely supported on an abutment (54) screwed to this spar to form the tilt axis (54a) and is held and guided on the abutment (54) in order to carry out limited tilting movements. Concealed hinge joint according to claim 7, characterized in that the abutment (54) has an adjusting device (60) for the adjusting displacement of the section (55) supported on the abutment. Method for tilting and pivoting bearings or the same operation - in particular with a concealed hinge joint according to one or more of the preceding claims - of wings (2) with a rollover (22) on / in the frame (1), in which
the tilt axis (54a, 33) of the wing (2) is aligned orthogonally to the swivel or rotation axis (12, 52),
characterized,
that at no point in time of the operational movements and positions of the wing (2) do the two axes (54a, 33; 12, 52) have an intersection. Method according to claim 9,
characterized,
that the axis of rotation (12, 52) on the inside of the frame is moved away from the tilt axis (54a, 33) orthogonal thereto, the tilt axis (54a, 33) being arranged in / on the frame (1). A method according to claim 9 or claim 10,
characterized,
that the tilt axis (54a, 33) - viewed perpendicular to the frame level - is placed in the inner edge region of the frame (1) and / or is slightly shifted when the wing (2) tilts, but does not move beyond the inner frame edge.

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