EP2725174B1 - Assembly of a hinge - Google Patents

Description

The invention relates to an assembly of a band for hinged about a hinge axis connection of a wing to a frame.

Bands for hingedly hinged connection of a wing to a frame are known in a variety of embodiments for a variety of different uses. By way of example, simple hinge bands are mentioned which do not allow any adjustment possibilities for adjusting the wing in the surrounding frame, and mechanically and kinematic complicated bands, which include adjustment possibilities in at least one spatial direction for adjusting the wing in the frame, as well as the use in so-called " Aufdecksituationen "allow in which wings and frame partially overlap parallel to the wing plane with the wing closed, so as to effect, for example, a particularly effective seal between the wing and frame.

From the US 2008/0307606 For example, a tape is known with an assembly having a receiving chamber for attachment to a wing. It serves for the detachable attachment of a hinge strap, which extends through an elongated opening in the interior of the receiving chamber. The hinge flap is on one Attached receiving part, which is arranged in the receiving chamber. The receiving part comprises two mutually continuing pins, which are mounted in bearing seats of the receiving chamber. To form the bearing seats, the receiving chamber is divided parallel to the longitudinal direction of the pins, so that each bearing seat is formed by two parts of the receiving chamber. For pivoting the receiving part about the axis defined by the pin is a screw, which cooperates with the receiving chamber and the receiving part. For displacing the receiving part in the direction of the axis defined by the pin, one of the pins is provided with an external thread onto which a screw element rotatably mounted in a bearing recess of the receiving chamber is screwed. The screw is drehbetätigbar via lateral openings of the receiving chamber by means of a tool. A band with such an assembly is structurally complex.

Another, constructionally simple band is from the US 1,893,252 known. It has an assembly with a mounting part, which comprises a slot which opens in regions to the outside. Inwardly, the slot opens into a bore extending from about two-thirds of the overall height of the assembly. The assembly further includes a hinge tab having a thickening that is approximately complementary to the bore. The hinge flap extends over the area of the mounting part over which the slot opens outwards. In this area, a screw element oriented transversely to the bore is rotatable and fixed in its longitudinal direction. It engages in a thread provided in the hinge flap, so that a rotary actuation of the screw element leads to a pivoting of the hinge flap about the axis defined by the bore. An adjustment in a direction perpendicular to this pivoting direction is not possible.

The invention has for its object to provide an assembly of a band that allows adjustment of the wing in the frame in at least one spatial direction and yet is characterized by a structurally simple structure and a simple and quick mountability.

This object is achieved by the reproduced in claim 1 assembly.

The assembly according to the invention comprises a mounting part which can be mounted on a mounting side of the wing or the frame. As a mounting side is particularly the side of the frame or the wing into consideration, which in the closed state of the wing the other part, i. facing the frame or the wing. In this case, the mounting part is not visible with the wing closed and then protected against manipulation. In principle, however, it is also conceivable to provide a visible side as the mounting side of the wing or the frame, as is the case with so-called "screw-on bands".

The mounting part comprises an approximately parallel to the hinge axis extending bore with a central longitudinal axis. The bore has at least one lateral opening. Further, the assembly comprises a banding flap comprising a fastening part, the fastening part of which extends through the opening with clearance into the bore and comprises at least one thickening arranged in the bore. The hinge flap can thus be joined together with the mounting part by being introduced from one end of the bore with its thickening in the direction of the central longitudinal axis in the bore or clipped by insertion through the slot. In the assembled state, the fastening part and thus the entire hinge flap is pivotable about the central longitudinal axis by an angle which is limited by the clearance between the fastening part and the opening. Since the central longitudinal axis is substantially parallel to the hinge axis, a pivoting of the hinge axis is approximately perpendicular to its direction and thus - if the hinge axis in the assembled state of this assembly comprising band perpendicular - in the horizontal direction possible. To effect the adjustment, the assembly according to the invention comprises at least one horizontal adjustment means, by means of which the pivoting movement of the fastening part about the central longitudinal axis is effected.

The assembly according to the invention is thus characterized by a minimum number of components. As the mounting part as of the hinge tab and the Horizontalverstellmittel Separate component is formed, only the mounting part must be adapted to the formation of the respective wing or the respective frame to which the assembly is to be mounted. For different installation situations, therefore, always the same hinge flap and the same Horizontalverstellmittel be used, which reduces production costs.

A further advantage of a band comprising an assembly according to the invention is that for horizontal adjustment, the entire hinge flap is displaced with the hinge part regularly formed thereon, and not, as in a plurality of other embodiments of bands, a hinge pin defining the hinge axis within the hinge part, as a result, the relative displacement of the hinge parts of wing and frame hinge tabs, which is indispensable in the last-mentioned embodiment, is avoided.

The assembly according to the invention comprises at least one vertical adjustment means, by means of which the hinge flap is displaceable parallel to the hinge axis relative to the mounting member. By this measure, an adjustment of a wing in a frame in two spatial directions is possible with the assembly of the invention.

The at least one vertical adjustment means comprises a vertical adjustment screw, which is screwed into an internal thread in the bore and cooperates with the thickening of the hinge strap. Such Vertikalverstellmittel is thus very simple and inexpensive to produce or the Vertikalverstellmittel have at least one vertical adjustment, which is mounted in the direction of the central longitudinal axis A fixed to the mounting member and cooperates with a provided on the thickening thread. This embodiment of the vertical adjustment means has the advantage that, in the case of a rotary actuation of the vertical adjustment screw, its position does not change relative to the mounting part, as a result of which a constant visual impression, irrespective of the respective adjustment position, can be achieved.

Particularly preferably, the bore has internal threads on both longitudinal ends, and a vertical adjustment screw is provided on both longitudinal ends. For vertical adjustment then only at least one of the two Vertikalverstellschrauben then has to be rotationally actuated so that the thickening of the hinge strap is with play between the two Vertikalverstellschrauben and by rotational actuation at least one of the vertical adjustment vertically into the desired position, together with the hinge tab, displaced.

In a preferred embodiment, the Horizontalverstellmittel only comprises a first horizontal adjustment, which is either fixedly mounted on the hinge plate in its longitudinal direction and cooperates with a thread provided on the mounting part, or is mounted fixedly to the mounting member in its longitudinal direction and provided with a on the hinge strap Thread cooperates. For horizontal adjustment, only the first horizontal adjustment screw then has to be rotationally actuated, wherein the respective achieved position is maintained by the at least one horizontal adjustment screw, provided that a further rotation of the horizontal adjustment screw is prevented.

In another embodiment, the horizontal displacement means comprises a first and a second horizontal adjustment screw. The first horizontal adjustment screw can be arranged such that it engages behind the fastening part on the outside so that it displaces the fastening part to the mounting part during screwing. The second horizontal adjustment screw can then be arranged so that it moves the fastening part when unscrewing from its thread from the mounting part away.

Particularly preferred is furthermore an embodiment of an assembly according to the invention, in which the mounting part has at least one projection for engagement in a groove in a first lateral edge region. The mounting member is then particularly suitable for attachment to profiles that include an undercut groove, such as a "C-groove". In this way, plastic profiles are often designed that can be used on both frames, as well as on wings use. However, such configured metal, such as aluminum profiles are known for this purpose in different configurations, but with C-groove.

To assemble the assembly, this is initially set so that the projection is engaged with the groove. For complete attachment, at least one first through-bore with a first bore longitudinal axis is then preferably provided on the mounting part at a second edge region opposite the first edge region. Through this hole then a fastening screw, for example, a self-drilling screw can be screwed.

In order to increase the forces that can be introduced via the assembly in a frame or in a wing without the at least one first fastening screw is torn out, at least at the second edge region at least one second through hole may be provided with a second bore longitudinal axis preferably runs obliquely to the first bore longitudinal axis. A screwed through the second hole longitudinal axis, second fastening screw is due to this measure at loads that attack, for example, in the direction of the first mounting screw, not in its longitudinal direction, but obliquely charged to this in a direction in which it causes a significantly higher resistance to tearing , But even the first edge region can be additionally or exclusively fastened or secured by at least one such fastening screw.

Fig. 1

ein erstes Ausführungsbeispiel einer erfindungsgemäßen Baugruppe in an einem Rahmen- oder Flügelprofil montierten Zustand in einer Ansicht der Scharnierachse in einer mittleren Horizontalen Verstellposition, im Bereich eines Horizontalverstellelements teilgeschnitten;

Fig. 2

dasselbe Ausführungsbeispiel in derselben Ansicht wie in Fig. 1, jedoch nicht geschnitten, in einer gemäß der Zeichnung nach rechts verlagerten horizontalen Verstellposition;

Fig. 3

dasselbe Ausführungsbeispiel in einer Fig. 2 entsprechenden Ansicht, jedoch in einer gemäß der Zeichnung nach links verlagerten, horizontalen Verstellposition;

Fig. 4

dasselbe Ausführungsbeispiel der Baugruppe in einer ersten perspektivischen Einzeldarstellung, mit noch nicht montierten Vertikalverstellmitteln;

Fig. 5

dasselbe Ausführungsbeispiel in einer zweiten perspektivischen Einzeldarstellung, nun mit montierten Vertikalverstellmitteln;

Fig. 6 bis 8

ein zweites Ausführungsbeispiel einer erfindungsgemäßen Baugruppe in Fig. 1 bis 3 entsprechenden Darstellungen;

Fig. 9

das zweite Ausführungsbeispiel in einer ersten perspektivischen Ansicht mit noch nicht montierten Vertikalverstellmitteln;

Fig. 10

eine zweite perspektivische Ansicht des zweiten Ausführungsbeispiels, nun mit montierten Vertikalverstellmitteln;

Fig. 11 bis 13

ein drittes Ausführungsbeispiel einer erfindungsgemäßen Baugruppe in Fig. 1 bis 3 entsprechenden Darstellungen;

Fig. 14

eine perspektivische Explosionsdarstellung dieses dritten Ausführungsbeispiels;

Fig. 15

eine Fig. 1 entsprechende Ansicht eines vierten, als "Aufschraubband" ausgebildeten Ausführungsbeispiels;

Fig. 16

eine perspektivische Explosionsdarstellung eines fünften Ausführungsbeispiels sowie

Fig. 17

eine Fig. 1 entsprechende Ansicht eines sechsten Ausführungsbeispiels.

In the drawing, several embodiments of the invention are shown. Show it:

Fig. 1

a first embodiment of an assembly according to the invention in mounted on a frame or wing profile state in a view of the hinge axis in a middle horizontal adjustment position, partially cut in the region of a Horizontalverstellelements;

Fig. 2

the same embodiment in the same view as in Fig. 1 but not cut, in a according to the drawing to the right shifted horizontal adjustment position;

Fig. 3

the same embodiment in one Fig. 2 corresponding view, but in a according to the drawing to the left shifted, horizontal adjustment position;

Fig. 4

the same embodiment of the assembly in a first perspective detail view, with not yet mounted Vertikalverstellmitteln;

Fig. 5

the same embodiment in a second perspective individual representation, now with mounted Vertikalverstellmitteln;

Fig. 6 to 8

a second embodiment of an assembly according to the invention in Fig. 1 to 3 corresponding representations;

Fig. 9

the second embodiment in a first perspective view with not yet mounted Vertikalverstellmitteln;

Fig. 10

a second perspective view of the second embodiment, now with mounted Vertikalverstellmitteln;

Fig. 11 to 13

a third embodiment of an assembly according to the invention in Fig. 1 to 3 corresponding representations;

Fig. 14

an exploded perspective view of this third embodiment;

Fig. 15

a Fig. 1 corresponding view of a fourth, designed as a "Aufschraubband"embodiment;

Fig. 16

an exploded perspective view of a fifth embodiment and

Fig. 17

a Fig. 1 corresponding view of a sixth embodiment.

That in the Fig. 1 to 5 As a whole with 100 designated embodiment of an assembly according to the invention comprises a mounting part 1, which is mounted on a mounting side 2 of a wing or a frame. In the Fig. 1 to 3 the mounting part 2 is attached to a multi-chamber profile 3. This can be a multi-chamber profile forming part of a frame or a wing. The mounting part can be made of any material with required properties. In particular, it may be a zinc die-cast part or an aluminum extruded part.

The multi-chamber profile 3 shown by way of example in the drawing comprises two hollow chambers 4, 5 which are spaced apart from one another and are connected via insulating webs 6.

The multi-chamber profile 3 comprises a groove 7. The mounting part 1 has at a first lateral edge region 8, which in the Fig. 1 to 3 is shown above, a projection 9 which engages in the groove 7.

Furthermore, the mounting part 1 at a second edge region 10 opposite the first edge region (see FIG. 4 and 5 ) on two first through holes 11. These first through holes 11 serve to receive first fastening screws 12, which can be screwed in for fastening in the frame or the wing. Furthermore, the mounting part 1 comprises two second through holes 13, which serve to receive second fastening screws 14.

The first through holes 11 have first bore longitudinal axes B1, the second through holes 13 second bore longitudinal axes B2 (s. Fig. 2 ). The first and second bore longitudinal axes B1, B2 extend as in FIG Fig. 2 made clear, at an angle to each other. The first and second fastening screws 12, 14, which are formed in the illustrated embodiment as self-drilling screws, thus penetrate obliquely to each other in the example shown multi-chamber profile 3, whereby the attachment of the mounting part 1 is suitable to the multi-chamber profile for introducing higher forces in the multi-chamber profile.

The mounting part 1 further comprises a bore 15 whose central longitudinal axis A extends parallel to a hinge axis S, which is defined by a hinge part of a hinge strap, as will be described in more detail below.

The bore 15 includes a lateral opening 16 which is slit-shaped in the illustrated embodiment and extends over the entire length of the mounting member and in the Fig. 1 to 3 oriented downwards (see also 4 and 5 ).

The assembly 100 further comprises a hinge flap 17, with a fastening part 18 and a hinge part 19. The hinge part 19 serves to receive a hinge pin, not shown in the drawing, of a hinge pin receptacle 20. It has a substantially circular cross-section, the center of which is the hinge axis S. Are defined.

At the edge opposite the hinge part 19, the fastening part 18 comprises a thickening 21 (see also FIG Fig. 6 ), whose outer circumference is adapted to the inner periphery of the bore 15 so that it is received with only a slight lateral play of the bore.

The attachment part 18 of the hinge strap 17 extends through the lateral opening 16 with lateral play, so that the hinge tab 17 about the central longitudinal axis A of the bore 15 by a certain angle whose size is determined by the size of the game is pivotable. By this pivotability, the hinge axis S on a circular path of the radius R, which is determined by the distance between the central longitudinal axis A and the hinge axis S, be displaced (s. Fig. 3 ). As by comparison of Fig. 1, 2 and 3 can be seen, thus, the hinge axis of a in Fig. 1 exemplified middle position, to which the hinge axis S has a distance a to a lateral edge 22 of the multi-chamber profile 3 by pivoting in the counterclockwise direction in accordance with Fig. 1 to 3 right extreme position in which the hinge axis S to the lateral edge 22 has a minimum distance b (s. Fig. 2 ), as well as by pivoting in a clockwise direction in a position in which the hinge axis S to the edge 22 has a maximum distance c, be displaced.

This displacement, since a hinge flap is installed in most cases so that the hinge axis S is vertical, also referred to as "horizontal adjustment".

To effect the previously described pivoting movement of the hinge 17 about the central longitudinal axis A of the bore 15 and to be able to fix the hinge flap 17 in a desired position, horizontal displacement means 23 are provided. These include at the first, in Fig. 1 to 5 illustrated embodiment, in each case a first horizontal adjustment screw 24 with a flat head 25 which is mounted in a T-slot 26 in the hinge flap 17. The horizontal adjustment screw 24 is thus stationary in its longitudinal direction relative to the hinge 17, but rotatably mounted. Your threaded shaft 27 engages in a provided in the mounting part 1 thread 28 a. A rotational actuation of the first horizontal adjustment screw 24 thus leads - depending on the direction of rotation - to a pivoting of the hinge 17 in the clockwise or counterclockwise direction.

At least in the end regions, the bore 15 has internal threads 28. They form a part of Vertikalverstellmitteln 29, which include Vertikalverstellschrauben 30, 31, which are screwed into the internal thread 28.

In particular 4 and 5 9 and 10 (the latter show a second embodiment of an assembly according to the invention) can be displaced by rotational actuation of the vertical adjustment screws 30, 31 of the hinge lugs 17 in the direction of the central longitudinal axis A and thus also in the direction of the hinge axis S. Since - as already stated above - the module usually so is arranged that the hinge axis S extends vertically, this adjustment is also called vertical adjustment.

With reference to Fig. 6 to 10 Now, a second embodiment 200 of the assembly according to the invention will be explained. The mode of operation and construction essentially correspond to those of the first exemplary embodiment 100, so that only the differences are to be explained below in order to avoid repetition.

As in particular from Fig. 6 It can be seen which, for example, the representation according to Fig. 1 corresponds, but without screwed vertical screw 31 so that the contour of the thickening 21 is visible, the head 25 of the horizontal adjustment screw 24 is not stored in a T-slot. In contrast, it rests against the outer surface of the fastening part 18. The first horizontal adjustment screw 24 passes through the fastening part in a bore 32, which is slot-shaped in the vertical adjustment direction (see Fig. 14 ). It engages with its threaded shaft 27 in an internal thread 33, which is provided in the mounting part 1. A rotational actuation of the first horizontal adjustment screw 24 in the sense of screwing in turn leads to a pivoting of the hinge 17 about the central longitudinal axis A and thus to a displacement of the hinge axis S on a circular path defined by the radius R (s. Fig. 8 ), counterclockwise.

A rotational actuation of the first horizontal screw 24 in the sense of unscrewing first causes the head 25 is lifted off the outer surface of the fastening part, so that the fastening part 18 can be pivoted about the axis A in the scope of the resulting game.

In order to forcibly relocate the fastening part 18 in a clockwise direction about the axis A, until the fastening part 18 rests again with its outer surface on the head 25, this embodiment comprises a second horizontal adjustment screw 34. It is screwed into a threaded bore 35 in the mounting part 1. Its head is located on the inside of the fastening part 18 and is accessible through a bore 36 in the fastening part 18. By applying a rotary tool, not shown in the drawing through the bore 36 therethrough to the head 37 of the second Horizontalverstellschraube 34 can be so displaced that the fixing member 18 is received between the heads 25, 37 of the two second Horizontalverstellschrauben 34 backlash and positioned in the adjustment.

In contrast to the first embodiment, the horizontal adjustment in this second embodiment, first and second Horizontalverstellschrauben must be rotationally actuated. As a result, the horizontal adjustment is indeed slightly more expensive than in the first embodiment. However, the two horizontal adjustment screws 24, 34 can be tightened against the fastening part 18, so that they are regularly protected by the clamping forces effectively against an automatic adjustment.

With reference to Fig. 11 to 14 Now, a third embodiment 300 of the assembly according to the invention will be explained. The mode of operation and construction essentially correspond to those of the second exemplary embodiment 200, so that only the differences from the second exemplary embodiment 200 are to be explained below in order to avoid repetition.

In the third embodiment 300, the second horizontal adjustment screw 34 is missing. Instead, a plurality of thin spacer elements 38 are provided, which are inserted in a necessary for the respective horizontal adjustment number and thickness between the facing sides of the mounting member 1 and the fastening part 18. The first horizontal adjustment screw 24 is then tightened after insertion of the spacers 38, so that the spacers 38 are firmly clamped between the mounting member 1 and the mounting member 18 when the desired horizontal adjustment has been achieved. An exploded view of this third embodiment 300 according to Fig. 14 shows a set of four planar spacers 38. They have recesses 39 through which the first Horizontalverstellschrauben 24 extend.

This in Fig. 15 illustrated, fourth embodiment 400 of the assembly according to the invention corresponds in its construction and operation substantially the first embodiment 100, so that reference should again be made to the description thereof. However, this assembly is designed as a so-called "Aufschraubband", which is intended for mounting on a front surface 40 of a wing or frame. The mounting member 1 therefore has no projection for engagement in a groove, but it is flat and includes in its first edge region 8 first mounting screws 12 which are screwed into the frame or wing or a frame or wing profile.

An actuation of the Horizontalverstellmittel 23 now causes no longer - as in the embodiments 100 to 300 - a change in the lateral gap widths between the wing and frame, but a relative displacement of the front surfaces of the wing and frame relative to each other. In the case of a Aufdeckanordnung with seal so the sealing pressure can be influenced by the Horizontalverstellmittel.

In the Fig. 15 However, "Aufschraubvariante" shown is in no way limited to be able to be screwed only from the outside. As a mounting side is also - as in the embodiments discussed above - the side of the frame or the wing into consideration, which is opposite to the other part in the closed state of the wing, if it is suitable for mounting a mounting part with a substantially flat contact side.

With reference to Fig. 16 Now, another embodiment 500 of the assembly according to the invention will be explained. The mode of operation and construction essentially correspond to those of the second exemplary embodiment 200, so that only the differences are to be explained below in order to avoid repetition.

In the embodiment 500, the second horizontal adjustment screw 34 is formed as a stud. It is screwed into a threaded hole 35 provided in the fastening part 18 of the hinge 17, until the front end of the threaded stud in the screwing direction is supported on the mounting part 1. By further screwing in - if previously the first horizontal adjustment screw had been released, the hinge plate 17 is moved away from the mounting part 1. By corresponding actuations of both the first and the second horizontal adjustment screw, the horizontal adjustment can be made approximately in the manner corresponding to the second embodiment 200.

Another difference between the fifth and the second embodiment is that the attachment of the first lateral edge portion 8 not only by engagement of the projection 9 in the groove 7 (in Fig. 16 not shown) takes place, but additional holes 42 are provided, through which the mounting part 1 in addition with the aid of, for example, self-drilling screws (also not shown) can be bolted to a profile wall or an insulating bar of a profile.

This in Fig. 17 illustrated sixth embodiment 600 substantially corresponds to the fifth embodiment 500. Again, only the differences will be discussed.

In the sixth embodiment 600, no protrusion for engaging a groove is provided on the first edge region 8. Rather, the attachment of this edge region is carried out only by means of fastening screws 41, which are self-drilling screwed into an insulating bar. In addition, mutually offset transversely to the hinge axis, paired first fixing screws 12 are provided which are parallel to each other and are screwed into a wall of the hollow chamber 5.

In all embodiments, the mounting part is shown in one piece. Is it made of a thermally conductive material, so it can form an unfavorable cold bridge, which reduces the effect of Isolierstege 6. To avoid this, For example, the mounting part 1 itself may be made of a poorly heat-conductive material. It may alternatively or additionally comprise a coating of a poorly heat-conducting material at least in those areas which rest against the wing or the frame. In addition, it may, for example, additionally or alternatively be designed in several parts in such a way that the voltage applied to the frame or the wing at different locations areas are thermally decoupled from each other.

LIST OF REFERENCE NUMBERS

100, 200, 300, 400, 500, 600

module

1

mounting part

2

mounting side

3

More chamber profile

4

hollow

5

hollow

6

insulating bars

7

groove

8th

first edge area

9

head Start

10

second border area

11

first through holes

12

first fixing screws

13

second through-hole

14

second fixing screws

15

drilling

16

lateral opening

17

hinge flap

18

attachment portion

19

hinge part

20

Belt bolt receptacle

21

thickening

22

lateral edge

23

Horizontalverstellmittel

24

first horizontal adjustment screw

25

head

26

T-slot

27

threaded shaft

28

inner thread

29

Vertikalverstellmittel

30

vertical adjusting

31

vertical adjusting

32

drilling

33

inner thread

34

second horizontal adjustment screw

35

threaded hole

36

drilling

37

head

38

spacers

39

recesses

40

front surface

41

fixing screw

42

drilling

A

central longitudinal axis

B1

first bore longitudinal axis

B2

second bore longitudinal axis

R

radius

S

hinge axis

a, b, c

distances

Claims (11)

1. Assembly (100, 200, 300, 400, 500, 600) of a hinge for connecting a leaf to a frame such that said connection can pivot about an articulation axis (S) in an articulated manner, comprising a mounting part (1) which can be mounted on a mounting face (2) of the leaf or of the frame, wherein the mounting part (1) has a bore (15) which extends approximately parallel to the articulation axis (S), has a central longitudinal axis (A) and comprises at least one lateral opening (16), comprising a hinge flap (17) which comprises a fastening part (18), the fastening part (18) of which hinge flap extends with clearance through the opening (16) into the bore (15) and comprises at least one thickened portion (21) arranged in the bore (15), comprising at least one horizontal adjustment means (23) by means of which the fastening part (18) is pivotable about the central longitudinal axis (A), and comprising at least one vertical adjustment means (29) by means of which the hinge flap (17) can be moved parallel to the hinge axis (S) relative to the mounting part (1), the one vertical adjustment means (29) comprises a vertical adjustment screw (30, 31) which is screwed into an internal thread (28) in the bore (15) and interacts with the thickened portion (21) of the hinge flap (17) or which is fixedly fitted on the mounting part (1) in the direction of the central longitudinal axis (A) and interacts with a thread that is provided on the thickening.
2. Assembly according to claim 1, characterized in that the bore (15) has an internal thread (28) at the two longitudinal ends, and a vertical adjustment screw (30, 31) is provided in each of the two longitudinal ends.
3. Assembly according to either claim 1 or claim 2, characterized in that the at least one horizontal adjustment means (23) comprises a first horizontal adjustment screw (24).
4. Assembly according to claim 3, characterized in that the first horizontal adjustment screw (24) interacts with a thread (28) provided on the mounting part (1).
5. Assembly according to claim 4, characterized in that the first horizontal adjustment screw (24) is fixedly fitted on the hinge flap (17) in the longitudinal direction thereof, or a second horizontal adjustment screw (34) is provided which preferably interacts with a thread (35) provided on the hinge flap (17) or on the mounting part (1) and acts on the fastening part (18) in the opposite direction to the first horizontal adjustment screw (24).
6. Assembly according to claim 3, characterized in that the first horizontal adjustment screw (24) interacts with a thread (32) provided on the hinge flap (17).
7. Assembly according to claim 6, characterized in that the first horizontal adjustment screw (24) is fixedly fitted on the mounting part (1) in the longitudinal direction thereof, or a second horizontal adjustment screw (34) is provided which preferably interacts with a thread (35) provided on the hinge flap (17) or on the mounting part (1) and acts on the fastening part (18) in the opposite direction to the first horizontal adjustment screw (24).
8. Assembly according to any of claims 1 to 7, characterized in that, in a first lateral edge region (8), the mounting part (1) has at least one projection (9) for engaging in a groove (7).
9. Assembly according to claim 8, characterized in that, at a second edge region (10) which is opposite the first edge region (8), the mounting part (1) has at least one first through bore (11) which has a first longitudinal bore axis (B1).
10. Assembly according to claim 9, characterized in that, at the first and/or the second edge region (8, 10), the mounting part (1) has at least one second through bore (13) which has a second longitudinal bore axis (B2).
11. Assembly according to claim 10, characterized in that the second longitudinal bore axis (32) extends obliquely to the first longitudinal bore axis (B1).

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