DE202012102978U1 - Band arrangement for doors, windows or the like - Google Patents

Abstract

Band arrangement for doors, windows or the like, comprising a first band part (1, 101) and a second band part (24, 124) pivotally connected to the first band part, the first band part (1, 101) being a hinge part (3) and a fastening part (2, 102, 302) and the fastening part (2, 102, 202, 302) can be mounted on a frame or wing parallel to a fastening plane (E), with at least one guide member (14, 114, 214, 314) leading into a guide recess (12, 212) in the fastening part (2, 102, 202, 302), so that the fastening part (2, 102, 202, 302) is displaceable perpendicularly to the fastening plane (E) in that at least one adjusting member, preferably two adjusting members (18, 18 ', 118, 118', 218, 218 ', 318, 318') are provided which have a thread extension (19, 19 ', 319, 319') and a Radial projection (20, 20 ', 320, 320'), wherein - the threaded extension (319, 319 ') with ei a complementary thread (345) on the frame or wing or on a mounting plate or clamping plate attached to the frame or wing and the radial projection (320, 320 ') with a receptacle (341) on the fastening part (302) is engageable - or the threaded extension (19, 19 ') with a complementary thread (22, 22', 222, 222 ') on the attachment part (2, 102, 202) and the radial projection (20, 20') with a receptacle on the frame or wing , in particular between a fastening plate (10) and a clamping plate (9), is engageable and at least one adjusting member (18, 18 ', 118, 118', 218, 218 ', 318, 318') offset to a desired tilting axis ( A) is arranged.

Description

The invention relates to a hinge assembly for doors, windows or the like, comprising a first hinge part and a second hinge part, which is pivotally connected to the first hinge part, wherein the first hinge part comprises a hinge part and a fastening part, and the fastening part parallel to a mounting plane on a Can be mounted frame or a wing, with at least one guide member, which engages leading into a guide recess in the fastening part, so that the fastening part is displaceable perpendicular to the mounting plane.

Such a band arrangement is for example from the DE 20 2005 012 152 U1 known. The mounting plane is defined there by a mounting surface. In this particularly inexpensive to produce band assembly is an adjustment perpendicular to the mounting plane, or the mounting surface - in the case of doors also called "horizontal adjustment" - in a particularly simple manner possible by only the adjusting member is rotationally actuated, whereby the fastening part and all connected to this Band parts are displaced in the longitudinal direction of the at least one guide member.

Although in this band arrangement a practically desirable, particularly simple and inexpensive horizontal adjustment possibility is provided, it is disadvantageous, however, that a certain play with respect to the attachment surface or attachment plane can occur in this band arrangement due to manufacturing tolerances. Moreover, it is disadvantageous in this arrangement that a further, desirable adjustability is not given.

The invention is therefore an object of the invention to provide a band assembly, which is at least improved in one of the above disadvantages and in which the correction of the tilt of the wing is possible even with very high sash weights.

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

The band arrangement according to the invention for doors, windows or the like has a first band part and a second band part. The first band part is pivotally connected to the second band part. The first hinge part comprises a hinge part and a fastening part. The fastening part is parallel to a mounting plane to a frame or a wing mountable. At least one guide member is provided, which engages in a guiding recess in the fastening part leading, so that the fastening part is displaceable perpendicular to the mounting plane. Preferably, the guide member comprises the active surface pairing cylinder and bore. Preferably, the guide member provides a linear bearing, more preferably a linear sliding bearing.

The band assembly according to the invention also comprises at least one adjusting member, preferably two adjusting members, which have a threaded extension and a radial projection. In particular, it is also conceivable that three adjusting members are provided.

The threaded extension is engageable with a complementary thread on the frame or wing, or on a mounting plate or clamping plate secured to the frame or wing, and the radial projection is engageable with a receptacle on the mounting portion.

Or the threaded extension is engageable with a complementary thread on the attachment member and the radial projection is engageable with a receptacle on the frame or wing, in particular between a mounting plate and clamping plate disposed on the frame or wing.

At least one adjusting member is arranged offset to a desired tilting axis.

By the radial projection in an alternative between a mounting plate and a clamping plate is engageable, the adjusting member is preferably axially fixed thereby, but rotatably arranged.

The adjusting members are preferably rotationally symmetrical about their longitudinal axis.

In a particularly preferred embodiment, the fastening part is fastened to an undercut of a frame or wing, preferably a frame or wing profile, more preferably by means of a fastening plate and a clamping plate cooperating therewith. The mounting plate and the clamping plate are preferably against each other, the undercut between them clamping, braced. The fastening part can preferably be fastened to the clamping plate and / or the fastening plate by means of a guide member and guide recess and adjusting members.

With undercut is referred to in the context of this document in particular a construction element which protrudes freely.

In a further embodiment, the fastening part is on a mounting surface of a Mountable frame or sash. The attachment surface then defines the attachment plane.

The guide member is preferably attached perpendicular to the mounting plane. In the embodiment with mounting plate and clamping plate, the guide member is preferably attachable to the mounting plate and / or clamping plate. In the embodiment in which the fastening part can be attached to an attachment surface of a frame or wing, the guide member is preferably attachable to this attachment surface.

Preferably, exactly two adjusting members are provided.

If the fastening part is attached to the wing, then the fastening plane is in particular the plane in which the narrow side of the wing lies, which lies opposite the narrow side of the frame when the wing is closed. For example, in a screwed from the outside on a door belt is also conceivable that the mounting plane is a perpendicular thereto, vertical plane.

When the fastening part is fastened to the frame, the fastening plane is referred to in particular as the plane in which the narrow side of the frame lies, which faces the narrow side of the wing when the wing is closed or, for example, in a band screwed onto the door from the outside this vertical, vertical plane.

Preferably, a translational horizontal adjustment of the fastening part and more preferably also a horizontal tilting of the fastening part about a desired tilting axis can be effected by means of the adjusting members. At least two adjusting members preferably participate in the translational horizontal adjustment. Therefore, this can also be done against high forces, such as heavy wings.

The desired tilt axis preferably extends in the mounting position of the band assembly vertically and more preferably approximately centrally through the attachment part.

In an important embodiment, the play between the guide members and the guide recesses can be eliminated by tilting about the desired axis.

Preferably, a tilting of the adjustment can be achieved by tilting.

The inventive arrangement, several advantages can be achieved: Firstly, a translational horizontal adjustment is achieved in a structurally simple manner. In order to enable this translational horizontal adjustment, a game is usually present between the guide members and the guide recesses. This required during the adjustment game interferes with fully assembled and adjusted band. If, as preferred, by the tilting about the desired axis, the game between the guide members and the guide recesses is eliminated, then a play-free seat is achieved without further components. Although in principle also conceivable that the guide members and the guide recesses form a substantially backlash-free sliding fit, this assumes, however, that both the guide members, and the guide recesses are made in very tight tolerances, which leads to an increased cost.

In one embodiment, the guide members and the guide recesses are made with a rather rough tolerance.

The fastening part can be powdered. On a reworking of the guide recess is then preferably omitted.

Disadvantage of DE 20 2005 012 152 U1 is that with the aid of the displacement element adjustment is possible only in a single direction perpendicular to the hinge axis, namely in the direction that is perpendicular to the mounting plane or mounting surface. Is this in the rebate area between the wing and frame, ie on a surface of the wing or the frame, which is parallel to a wall of the other part of the wing or the frame in the closed state of the wing, so by the operation of the displacement element is a horizontal Adjustment of the wing in the frame in the sense of adjusting the gap size possible.

By tilting is in a preferred embodiment of the invention, an adjustment, for example, the wing in the direction of this horizontal adjustment and the hinge axis perpendicular direction possible. As a result, for example, the sealing pressure, with which the wing abuts in the closed state on a possibly provided between it and the frame seal arrangement, at least to a small extent adjustable.

Further, if necessary, by the tilting of the fastening part, the band arrangement can be optimized to the extent that the hinge axes defined by all the hinge parts of the band arrangement coincide as exactly as possible so as to avoid jamming between the band parts and a hinge bolt passing through them and to reduce the wear caused by Flügelverschwenkung.

By means of the adjusting a horizontal tilting P of the fastening part about a tilting axis can be effected, so that is achieved that an extremely desirable, further adjustment possibility is present.

The radial projection of the adjusting members is preferably arranged at the end and can therefore also be referred to as a head.

Preferably, the adjusting members have at least one support surface, which can be pressed against a mating surface providing an abutment.

Preferably, a support surface of the adjusting members is formed by the end face of a radial projection of the adjusting members.

The adjusting members particularly preferably have two support surfaces, which are further preferably formed from opposite sides of the radial projection. In this way, an axial fixation of the adjusting element is achieved.

Preferably, a first support surface of the adjusting members is formed by the end face of the radial projection of the adjusting members. This support surface is preferably circular surface. As a result, the support surface is increased, so that a lower compressive stress occurs. Preferably, the cooperating with this surface mating surface is formed by the cooperating with a clamping plate mounting plate.

Particularly preferably, the surface of the radial projection opposite this surface of the radial projection forms a second support surface which can likewise be pressed against an abutment-forming surface. This second support surface faces the threaded extension of the adjusting member and preferably annular surface.

In the embodiment with clamping plate, this preferably has a bore which is penetrated by the adjusting member. In the counter surface, against which the second support surface of the adjusting member can be pressed, it is then preferably arranged around this bore surface of the clamping plate.

In another conceivable embodiment, in which the thread extension of the adjusting members with a complementary thread on the frame or wing or on a mounting plate or clamping plate fastened to the frame or wing and the radial projection can be engaged with a receptacle on the fastening part, it is conceivable that an undercut is provided on the fastening part, which engages behind the radial projection of the adjusting member. The undercut can be formed in this embodiment of the edge lips of a cross-sectionally C-shaped groove, which can also be referred to as a T-slot.

Advantageously, the guide recesses in mounting position are arranged vertically one above the other and the tilting axis passes through them.

Preferably, the guide members engage in recesses in the closed state of the wing, which are arranged in the second band part or at least on the side of the second band part. This embodiment has independent inventive significance. As a result, a band page backup is effected in a simple manner.

An expedient, also independent inventive meaning having embodiment provides that the guide members have a radial projection (or head) and this radial projection engages in the closed state of the wing in recesses which are arranged in the second band part or at least on the side of the second band part ,

Advantageously, the second band part on a mounting plate in which the recesses into which engage the guide members are arranged. This embodiment also has independent inventive significance.

Preferably, measures for attacking a turning tool are provided on the adjusting elements. These are preferably arranged on the radial projection opposite end of the adjusting members.

The measures preferably include a hexagon socket.

The guide member is preferably rotationally symmetrical about its longitudinal axis and has a threaded extension and a guide region.

The thread extension preferably has a smaller diameter than the guide region.

Preferably, a radial projection is provided at the opposite end of the threaded portion of the guide portion.

The radial projection of the guide member can serve as a stop for the fastening part of the hinge part and thus limit the adjustment.

The thread of the thread extension of the guide member may be self-tapping.

The thread of the thread extension of the guide member may also be a machine thread.

In the conceivable embodiment, in which the threaded extension of the adjusting members with a complementary thread on the frame and wings and the radial projection with a receptacle on the fastening part is engageable, it is conceivable that a first threaded member is provided with an external thread, which in at least two parallel walls of the profile can be screwed and which has a thread extension of the adjusting complementary internal thread. It can then be provided with an external thread, a second threaded element, which is also screwed into at least two parallel walls of the profile and which has a thread extension of the guide member complementary internal thread. The first and second threaded elements may be identically formed components.

The sash profile and the frame profile can be made of metal, in particular aluminum, with the exception of any existing thermal insulating webs. The insulating webs may be made of a thermal insulator, such as a suitable plastic.

The invention will now be explained in more detail with reference to five embodiments shown in the drawings. Show it:

1 an exploded perspective view of a first embodiment of a band assembly according to the invention;

2 a perspective view of in 1 shown band assembly in the assembled state and smaller scale;

3 a perspective view of in 1 shown band assembly mounted on a frame and a wing state;

4 a sectional view of the band assembly along the section line IV-IV in 3 ;

5 a view like in 3 but a second embodiment;

6 a schematic partially sectioned top view of a third embodiment, wherein only the wing side is shown;

7 a schematic perspective view of a lining plate of the third embodiment;

8th a sectional view of the lining plate of 7 along the section line VIII-VIII;

9 a perspective view, inter alia, of the fastening part of the third embodiment;

10 a schematic partially sectioned top view of a fourth embodiment, wherein only the wing side is shown;

11 a sectional view of an adjusting member of the fourth embodiment;

12 a sectional view of a guide member of the fourth embodiment;

13 a schematic perspective view of a lining plate of a fifth embodiment;

14 a schematic sectional top view of a fifth embodiment, wherein only the wing side is shown.

All embodiments shown in the drawings are three-part bands. The first two embodiments shown are clamping bands.

In all embodiments shown, the first band part 1 . 101 the wing hinge part and the second hinge part 24 . 124 the frame band part.

In the in the 1 to 4 shown first embodiment is a first band part 1 provided, which is a fastening part 2 includes. With this first band part 1 is a second band part 24 by means of a hinge pin 26 pivotally connected. The second band part 24 for its part consists of two parts. It is also conceivable that the second band part does not consist of two parts, but for example (C-shape) is connected, as taken for example by the roller belt 4 the Dr. Hahn GmbH & Co. KG is known. They are bearing bushes 27 intended. The hinge pin 26 is with two setscrews 28 fixed in the longitudinal direction.

The fastening part 2 , is therefore attached to a wing, more precisely on a wing profile 6 ,

The fastening part 2 However, it is not attached to a mounting surface of the wing, but the attachment by means of a clamping device 8th , The clamping device 8th includes a mounting plate 10 that with a clamping plate 9 is tense. The mounting plate and the clamping plate clamp two undercuts 11 of the sash profile 6 between themselves ( 3 ). In this way, the clamping device 9 firmly on the wing profile 6 fixed. The bracing is done by screwing using the four screws 34 ,

The second band part 24 is by means of eight countersunk screws 29 and a mounting plate 25 jammed with two undercuts of the frame profile. In the in the 1 to 4 shown embodiment, this frame-side mounting plate 25 two parts.

The first hinge part also has a hinge part 3 on. The fastening part 2 and the hinge part 3 are over an angled connection area 4 integrally connected to each other, the dimensions of the connection area 4 to a sealing projection 5 are adjusted, as in 4 is recognizable.

The fastening part 2 is approximately plate-shaped and has a substantially flat bottom 7 on, the clamping plate 9 is facing. As 4 shows is the attachment part 2 arranged parallel to a mounting plane E, passing through the narrow side 33 of the wing is defined. (The narrow side 33 corresponds to a mounting surface of a wing whose profile has no undercuts.)

In the fastening part 2 are two guiding recesses 12 incorporated, which are formed as through holes. The diameter of each guide recess 12 is at the outside diameter of a guide area 13 a guide member 14 , which is designed as a lens shank screw, adapted so that the guide area 13 with the associated guide recess 12 forms a clearance, which is a sliding of the guide recesses 12 on the leadership area 13 , So a relative movement between the fastening part 2 and the leaders 14 allowed in the direction of the longitudinal extent of the guide members. From a frontal end 15 of the management area 13 extends a threaded extension 16 having an external thread formed as a machine thread. At the opposite end face is on the guide member 14 a radial projection 17 intended. This forms a stop for the fastening part 2 , The guide members 14 are with their threaded extension 16 with advantage as far as in guide bores 31 the clamping plate and threaded holes 32 the mounting plate 10 screwed in that the front side 15 the guide area on the clamping plate 9 is applied. The management area 13 the guide members is longer in the axial direction than the thickness of the fastening part 2 ,

The band assembly comprises two adjusting members 18 . 18 ' which a threaded extension 19 . 19 ' with a machine external thread and a radial projection 20 . 20 ' include. The adjusting members 18 . 18 ' act between the fastening part 2 and the clamping device 8th , Both adjusting members 18 . 18' are arranged in the same plane perpendicular to the hinge axis B aligned plane. In the case of a vertical hinge axis B, they are therefore arranged at the same height. They are spaced from the hinge axis B. The adjusting members 18 . 18' each with play a hole 30 in the clamping plate 9 , Each actuator 18 . 18 ' is in the direction of the translational horizontal adjustment Y positive fit to the clamping device 8th stored. Each actuator 18 . 18 ' in other words is axially on the clamping device 8th fixed. This axial fixation is effected by the fact that the radial projection 20 . 20 ' each adjuster 18 . 18 ' a front-side circular surface-shaped first support surface 21 . 21 ' trains against the mounting plate 10 is depressible. In the other axial direction, the fixation is effected by the threaded extension 19 . 19 ' facing surface of the radial projection 20 . 20 ' a second annular surface support surface 35 . 35' forms at the edge of a hole 30 , 30 'of the clamping plate rests, which is penetrated by the adjusting member. The thickness of the radial projection 20 . 20 ' of the adjusting member 18 . 18 ' is so to the clamping device 8th adjusted that with fixed mounted clamping device an axial fixation with little play is given, which is a rotation of the adjusting 18 . 18 ' allows. The thread extension 19 . 19 ' of the adjusting member 18 . 18 ' is with a complementary thread 22 . 22 ' of the fastening part 2 engageable. At the of the radial projection 20 . 20 ' Away turned end of threaded extension 19 . 19 ' of the adjusting member 18 . 18' a hexagon socket is provided for the attack of a turning tool. Both adjusting members 18 . 18' have the same shape and size. With a rotation of an adjusting member 18 . 18' clockwise becomes the first support surface 21 against the mounting plate 10 pressed. When counterclockwise, the second support surface becomes 35 against the clamping plate 9 pressed. When the adjusting member 18 . 18' has a left-hand thread, then the reverse applies.

The two adjusting members 18 . 18 ' are arranged offset to a desired tilt axis A. The desired tilting axis A runs parallel to the hinge axis B defined by the hinge pin and, when the hinge arrangement is mounted vertically. The two adjusting members are arranged on opposite sides of this axis A.

Amongst other things 4 It can be seen that in a same direction rotation of the two adjusting members 18 . 18 ' , about each by means of a rotary tool, a translational horizontal adjustment of the fixing part 2 , and with it all the parts of the band associated with it, is effectible. This horizontal adjustment is symbolized by the arrow marked Y and aligned perpendicular to the mounting plane E. By the translational horizontal adjustment is a horizontal adjustment of the wing in the frame in the sense of adjusting the gap size possible. Also, the tendency in particular particularly heavy wings to tilt with their side facing away from the bands downwards, can be counteracted. Since the forces occurring in a band are distributed to the two adjusting members, for example, the skew of heavy wings can be eliminated.

4 can also be seen that in an opposite direction actuation of the two adjusting members 18 . 18 ' a Horizontalverkippung, which is symbolized by the P designated curved arrow, the attachment part 2 about the axis A is effected. Due to the horizontal tilting P, the sealing pressure, with which the wing rests in the closed state on a sealing arrangement which may be provided between it and the frame, can be at least slightly adjustable, inter alia. The size of the achievable Horizontalverkippung P is among other things by the size of the game between the leadership 13 the guide member and the guide recess 12 affected. In the embodiment shown, the fastening part 2 , For example, after performed translational horizontal adjustment Y, are tilted so far that this game completely disappears. As a result, a very desirable backlash-free, without other components, achieved, although the guide members 14 and the guiding recesses 12 are not manufactured with very tight tolerances and therefore the play occurring between them in the non-tilted state can be considerable.

This in 5 embodiment shown differs from that in the 1 to 4 shown embodiment only in that the mounting plate 125 of the second band part 124 is one-piece and continuous, and is not divided into two parts. The mounting plate 125 has two recesses 123 on, in which the radial projections 17 . 117 the leaders 14 . 114 engage with the sash closed. In this way, a tape side protection is achieved. The radial projections 117 can in this embodiment in the longitudinal direction of the guide members 114 be greater than provided in the first embodiment, so that they advantageously with the wing closed far into the recesses 123 protrude. The horizontal tilt and translational horizontal adjustment is integrated into the clamp attachment.

The 6 to 9 show a third embodiment. This band is not a band. It is therefore not a clamping device 8th . 108 intended. The fastening part 202 is by means of a lining plate 236 on the sash profile 206 attached. The lining plate 236 is with the sash profile 206 screwed. As 6 shows is the lining plate 236 at the height of an insulating bar 239 arranged. This serves for thermal insulation of areas of the airfoil 206 , It can be made of plastic. The screwing of the lining plate 236 does not take place directly with the insulating bar, but with a counter plate 240 , The lining plate 236 and the counter-plate 240 span the insulating bar 239 and direct the forces directly into the rest of the sash profile 206 one that can be made of aluminum. The screwing of lining plate 236 and counter plate 240 can by means of two screws 240a respectively. In the lining plate 236 is for each of the two adjusting members 218 . 218' a pot hole 237 . 237' intended. The well bore is a bore penetrating the feed plate, having a larger diameter portion and a smaller diameter portion (see, in particular, FIG 8th ). The area of larger diameter is in mounting position the sash profile 206 facing. The area of larger diameter takes the radial projection of the adjusting member 218 . 218' on. The transition between the areas of different diameters forms the counter surface for the second support surface 235 . 235' of the adjusting member 218 . 218' , The sash profile 206 forms the counter surface for the first support surface 221 . 221 ' of the adjusting member. As a result, a simple axial fixation of the adjustment 218 . 218' reached. The threaded extension of the adjusting members 218 . 218' engages in complementary threads 222 . 222' of the fastening part 202 one. This complementary thread 222 . 222' are through tapped holes 238 . 238' educated.

At the radial projection of the opposite end of the adjusting member, a hexagon socket is arranged in the first three embodiments shown, for attacking a rotary tool.

Im in the 6 to 9 embodiment shown spans the lining plate 236 the insulating bridge 239 so far and the pot bores 237 . 237' are so far out on the lining plate 236 attached that the counter surfaces for the first support surface of 221 . 221 ' the adjusting members 218 . 218' at least partially of the adjacent to the insulating web aluminum region of the airfoil 206 are formed and not or only partially from the Isoliersteg. They are two leaders 214 provided, with their threaded extension in the lining plate 236 are bolted. The shown positions of the adjusting members 218 . 218' and leaders 214 are only examples.

The 10 to 12 show a fourth embodiment. On the narrow side 333 the wing is a mounting surface 342 provided, which defines the mounting plane E. The fastening part 302 is at the attachment surface 342 attached. The thread extension 319 . 319' the adjusting members 318 . 318' is with a complementary thread 322 on the wing, more precisely on a wing profile 306 , engaged. And the radial projection 320 . 320 ' is with a receptacle on the attachment part 302 engaged. The adjusting members 318 . 318' are thus turned over compared to the previous embodiments. In order to be reachable from the outside about medium of a turning tool, the measures for the attack of a turning tool on the side of the radial projection of the adjusting member are provided. The rotary tool can through a hole in the mounting part 302 be plugged. The receptacle for the radial projection is through a T-slot 341 formed as they are already taken out of the DE 20 2005 012 152 U1 is known and for an adjuster 318 in 11 is shown in more detail. As 11 shows, an in 10 not shown first threaded element 343 be provided with an external thread 344 which can be screwed into at least two parallel walls of the profile and which one to the threaded extension 319 of the adjusting member 318 . 318' complementary internal thread 322 . 345 having. 12 shows that even a second threaded element 346 may be provided with an external thread, which is also screwed into at least two parallel walls of the profile and which one to the threaded extension 316 the guide member complementary internal thread 347 having. The first and second threaded elements may be identically formed components.

The 13 and 14 show a fifth embodiment. This is different from the one in the 6 to 9 shown third embodiment only in that the lining plate 436 not bolted to a counter plate, but is attached directly to the sash profile. As a result, the thermal insulation effect of the insulating bars is less affected. The attachment of the lining plate 436 on the wing profile can by means of Futterplattenbefestigungsschrauben, in particular oblique screws 448 respectively. These oblique screws are as in 14 shown with its axis of rotation not perpendicular to the mounting plane E arranged. This can increase the load capacity of the screw connection, in particular in the direction perpendicular to the fastening plane E. 14 shows a schematic sectional view of the wing side of a band assembly according to the invention, wherein the section is horizontal and at the level of the two lower oblique screws 448 runs, looking down. The also available pot bores 437 . 437' are for that reason in 14 not to watch, as well as about the also existing adjusting members. It can, as shown, each a reduction 449 for a screw head of the oblique screws 448 be present so that these do not have the lining plate 436 (in 14 to the left) and limit the translational horizontal adjustment Y of the attachment part. The oblique screws 448 do not engage in the Isolierstege in the illustrated embodiment, but in the metallic region of the airfoil. This can benefit the resilience of the screw. However, it is also conceivable that they at least partially engage in the Isolierstege. In the illustrated embodiment, four oblique screws 448 intended. It may also be less, about two or more oblique screws may be provided. In 13 are the subsidence 449 symbolized only by circles to a possible position of four oblique screws 448 display. The oblique screws 448 can be tapping screws as shown. Their core diameter may be larger relative to the head diameter than shown. So it can be provided relatively thick screws to reduce the risk of thread breakage in the profile. They can have a self-tapping thread.

The lining plate 436 can continue beyond the insulating bars (in 14 up and down) as in 14 shown. The screws 448 can also be non-oblique, so aligned perpendicular to the mounting plane E. It can be inclined and / or non-oblique threaded elements, as in the 11 and 12 are shown provided with to the threads of the Futterplattenbefestigungsschrauben 448 complementary internal threads and the screws 448 can be bolted in the threaded elements. This, in the 13 and 14 Not shown threaded elements may be screwed with its external thread at least partially in the insulating bars, or only in the metallic region of the airfoil.

The adjusting members of all embodiments may have the same shape and size as shown in the first embodiment. The same applies to the leaders.

In all the embodiments shown, a translatory horizontal adjustment Y and a horizontal tilting P, as described above with reference to the first embodiment, can be effected by turning the adjusting members with the rotary tool. The Horizontalverkippung P and translational horizontal adjustment Y takes place in all embodiments shown time-saving on the same elements, namely the adjustment 18 . 18' . 118 . 118' . 218 . 218' . 318 . 318' , and require no hanging of the wing or loosening screws.

In addition to their adjustment function, the adjusting members 18 . 18' . 118 . 118' . 218 . 218' , 318, 318' also attachment function. In all embodiments shown, they act on the attachment of the fastening part 2 . 102 . 202 . 302 with the wing. In the first two embodiments shown by means of the clamping device 8th . 108 ,

In the complementary threads of the fastening parts and correspondingly in the threads of the thread extensions of the adjusting members, the first three and the fifth embodiments shown may be left-hand threads. This also causes in these embodiments, the assembly facilitating effect that, upon rotation of the adjusting members in a clockwise direction, by means of the externally applied turning tools, the corresponding area of the fastening part moves towards the wing and vice versa.

In the first three and fifth embodiments shown, the adjusting members engage 18 . 18 ' . 118 . 118' . 218 . 218' not in a specially made groove of a band part.

The embodiment described above on the wing hinge part is in no way limited to use in connection with a wing hinge part. In a corresponding manner, alternatively or additionally, the frame hinge part can be formed. Accordingly, the embodiment described above in connection with the frame band can be realized in connection with a leaf hinge part.

Moreover, the invention is not limited to a three-part band. In particular, it can also be found in connection with two-part or multi-part bands realization.

LIST OF REFERENCE NUMBERS

1, 101

 first band part

2, 102, 202, 302

 attachment portion

3

 hinge part

4

 connecting area

5

 sealing projection

6, 106, 206

 airfoil

7

 Bottom of the mounting part

8, 108

 clamper

9

 clamp

10

 mounting plate

11

 Undercut of the sash profile

12, 212

 guide recesses

13

 Guiding area of the guide member

14, 114, 214, 314

 guide member

15

 front end of the guide area

16, 316

 Thread extension of the guide member

17, 117, 217

 radial projection

18, 18 ', 118, 118', 218, 218 ', 318, 318'

 adjusting members

19, 19 ', 319, 319'

 Thread extension of the adjusting members

20, 20 ', 320, 320'

 radial projection

21, 21 ', 221, 221'

 first support surface

22, 22 ', 222, 222'

 complementary thread of the fastening part

123

 recesses

24, 124

 second band part

25, 125

 mounting plate

26

 hinge bolts

27

 bearing bush

28

 Set screw

29

 Senkschraube

30, 30 '

 Drilling the clamping plate

31

 Guide bore of the clamping plate

32

 Threaded hole of the mounting plate

33, 233, 333

 Narrow side of the wing

34

 screw

35, 35 ', 235, 235'

 second support surface

236, 436

 food plate

237, 237', 437, 437'

 pot hole

238, 238'

 Links threaded hole

239

 Insulating web

240

 counterplate

240a

 screw

341

 T-slot

342

 mounting surface

343

 first threaded element

344

 external thread

345

 inner thread

346

 second threaded element

347

 inner thread

448

 oblique screws

449

 reduction

Y

 translatory horizontal adjustment

P

 Horizontalverkippung

e

 mounting level

A

 tilt axis

B

 hinge axis

QUOTES INCLUDE IN THE DESCRIPTION

This list of the documents listed by the applicant has been generated automatically and is included solely for the better information of the reader. The list is not part of the German patent or utility model application. The DPMA assumes no liability for any errors or omissions.

Cited patent literature

• DE 202005012152 U1 [0002, 0027, 0085]

Claims (10)

Band arrangement for doors, windows or the like, with a first band part ( 1 . 101 ) and a second band part ( 24 . 124 ), which is pivotally connected to the first band part, wherein the first band part ( 1 . 101 ) a hinge part ( 3 ) and a fastening part ( 2 . 102 . 302 ) and the fastening part ( 2 . 102 . 202 . 302 ) is mountable parallel to a mounting plane (E) on a frame or a wing, with at least one guide member ( 14 . 114 . 214 . 314 ), which in a Führungsausnehmung ( 12 . 212 ) in the fastening part ( 2 . 102 . 202 . 302 ) leader, so that the fastening part ( 2 . 102 . 202 . 302 ) perpendicular to the mounting plane (E) is displaceable, characterized in that at least one adjusting member, preferably two adjusting members ( 18 . 18 ' 118 . 118' . 218 . 218' . 318 . 318' ) are provided which a threaded extension ( 19 . 19 ' . 319 . 319' ) and a radial projection ( 20 . 20 ' . 320 . 320' ), wherein - the threaded extension ( 319 . 319' ) with a complementary thread ( 345 ) on the frame or wing or on a mounting plate or clamping plate attached to the frame or wing and the radial projection ( 320 . 320' ) with a recording ( 341 ) on the fastening part ( 302 ) is engageable - or the threaded extension ( 19 . 19 ' ) with a complementary thread ( 22 . 22 ' . 222 . 222' ) on the fastening part ( 2 . 102 . 202 ) and the radial projection ( 20 . 20 ' ) with a receptacle on the frame or wing, in particular between a mounting plate ( 10 ) and a clamping plate ( 9 ), is engageable and at least one adjusting member ( 18 . 18 ' . 118 . 118' . 218 . 218' . 318 . 318' ) is arranged offset to a desired tilting axis (A). Band arrangement according to claim 1, characterized in that by means of the adjusting members ( 18 . 18 ' . 118 . 118' . 218 . 218' . 318 . 318' ) a translational horizontal adjustment (Y) of the fastening part ( 2 . 102 . 202 . 302 ) and a horizontal tilting (P) of the fastening part ( 2 . 102 . 202 . 302 ) about the tilting axis (A) is effected. Band assembly according to claim 1 or 2, characterized in that by tilting about the desired axis (A) the play between the guide members ( 14 . 114 . 214 . 314 ) and the guiding recesses ( 12 ) is eliminable. Band assembly according to one of claims 1 to 3, characterized in that a support surface ( 21 . 21 ' . 221 . 221 ' ) of the adjusting members ( 18 . 18 ' . 118 . 118' . 218 . 218' . 318 . 318' ) from the end face of a radial projection ( 20 . 20 ' . 320 . 320' ) of the adjusting members ( 18 . 18 ' . 118 . 118' . 218 . 218' . 318 . 318' ) is formed. Band arrangement according to one of claims 1 to 4, characterized in that the adjusting members ( 18 . 18 ' . 118 . 118' . 218 . 218' . 318 . 318' ) each have two support surfaces ( 21 . 21 ' . 221 . 221 ' . 35 . 35' . 235 . 235' ) projecting from opposite sides of the radial projection ( 20 . 20' . 320 . 320' ) are formed. Band arrangement according to one of claims 1 to 5, characterized in that the guide recesses ( 12 . 112 ) are arranged one above the other in the mounting position and the tilting axis (A) passes through them. Band arrangement for doors, windows or the like, with a first band part ( 1 . 101 ) and a second band part ( 24 . 124 ), which is pivotally connected to the first band part, wherein the first band part ( 1 . 101 ) a hinge part ( 3 ) and a fastening part ( 2 . 102 . 202 . 302 ) and the fastening part ( 2 . 102 . 202 . 302 ) is mountable parallel to a mounting plane (E) on a frame or a wing, with at least one guide member ( 14 . 114 . 214 . 314 ), which in a Führungsausnehmung ( 12 . 212 ) in the fastening part ( 2 . 102 . 202 . 302 ) leader, so that the fastening part ( 2 . 102 . 202 . 302 ) perpendicular to the mounting plane (E) is displaceable, preferably according to one of claims 1 to 6, characterized in that the guide members ( 114 ) in the closed state of the wing in recesses ( 123 ) in the second band part ( 124 ) or at least on the side of the second band part ( 124 ) engage and thereby a band side fuse is effected. Band assembly according to claim 7, characterized in that the guide members ( 114 ) a radial projection ( 117 ) and this radial projection ( 117 ) in the closed state of the wing in recesses ( 123 ) in the second band part ( 124 ) or at least on the side of the second band part ( 124 ) intervene. Band assembly according to claim 7 or 8, characterized in that the second band part ( 124 ) a single mounting plate ( 125 ) and the recesses ( 123 ) in this mounting plate ( 125 ) are arranged. Band arrangement according to one of claims 1 to 9, characterized in that on the said radial projection ( 20 . 20' ) opposite end of the adjusting members ( 18 . 18' . 118 . 118' . 218 . 218' ) Measures are provided for attacking a turning tool.

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