DE102019128247B3 - Band for the pivoting connection of a sash with a frame - Google Patents

Abstract

Band (100) for the pivotable connection of a sash to a frame, with a frame fastening arrangement (1), with a sash fastening arrangement (2), with a swivel bracket (3) which connects the sash fastening arrangement (2) to the frame fastening arrangement (1) and which is at least one the frame fastening arrangement (1) and the sash fastening arrangement (2) is mounted pivotably about a pivot axis (S), and which comprises a frame part (4) connected to the frame fastening arrangement (1) and a sash part (5) connected to the sash fastening arrangement (2), and with an adjusting device (6) by means of which the sash part (5) can be displaced relative to the frame part (4) in an adjustment direction (R1) running perpendicular to the pivot axis (S), and which has a first adjusting element (12) for displacing the sash part ( 5) relative to the frame part (4) in the adjustment direction (R1). The first adjusting element (12) comprises a threaded spindle (13) which has a first Has a threaded area (14) and a second threaded area (15), the threads (16, 17) of which are designed in opposite directions.

Description

The invention relates to a hinge for the pivotable connection of a sash to a frame, with a frame fastening arrangement, with a sash fastening arrangement, with a swivel bracket connecting the sash fastening arrangement to the frame fastening arrangement, which is pivotably mounted on at least one of the frame fastening arrangement and the sash fastening arrangement about a pivot axis, and the comprises a frame part connected to the frame fastening arrangement and a sash part connected to the sash fastening arrangement, and with an adjustment device by means of which the sash part can be displaced relative to the frame part in an adjustment direction perpendicular to the pivot axis, and which has a first adjustment element for displacing the sash part relative to the frame part in the adjustment direction includes.

Such a tape is for example from DE 201 00 622 U1 known.

To adjust the sash relative to the frame, the sash part can be displaced relative to the frame part using and adjusting the adjusting element. For this purpose, the adjusting element can, for example, have a wrench surface on which a tool can be attached, with which the adjusting element can be adjusted for displacing the wing part relative to the frame part. For example, the adjusting element can be designed as a screw. From the aforementioned DE 201 00 622 U1 the arrangement of an eccentric screw is known, which is arranged, for example, with a concentric section in a bore formed on the frame part and with an eccentric section in an opening formed as an elongated hole in the wing part. As a result, when the eccentric screw is turned, a displacement of the sash part relative to the frame part in an adjustment direction can generally be effected.

The assembly and adjustment of such bands is not easy, especially with heavy sashes, because the blades have to be held in position by hand while the band parts are being attached. In this case, the eccentric screw is not infrequently already rotated with a slight displacement of the sash part relative to the frame part, so that an exact positioning of the sash relative to the frame often fails. Therefore, the eccentric screw has to be fixed in addition to the frame part during the fixing of the sash part, whereby the assembly and adjustment is relatively expensive and complicated. In addition, the assembly of the eccentric screw as such is relatively complicated, since it must be positioned particularly precisely in relation to the sash part and the frame part in order to be arranged with their longitudinal sections with different functional properties in each case in an area provided for this purpose.

The object of the present invention is therefore to provide a tape in which the adjustment and assembly of the adjustment elements is simplified.

The invention solves the problem posed by a tape with the features of the main claim. Advantageous configurations and developments of the invention are disclosed in the subclaims, the description and the figures.

The band according to the invention is characterized in that the adjusting element comprises a threaded spindle which has a first threaded area and a second threaded area, the threads of which are designed in opposite directions. This enables a particularly simple, quick and exact adjustment of the sash with respect to the frame, in particular of the sash part with respect to the frame part, in the adjustment direction. For this purpose, the threaded spindle can, for example, have a key surface on at least one of its axial end sides, on which a turning tool can be attached, with which the threaded spindle can be rotated to move the wing part relative to the frame part. For this purpose, the threaded spindle can, for example, be in engagement in the first threaded area with a mating thread on one of the wing part and the frame part and with the second thread part in engagement with a mating thread formed on another component to move the wing part relative to the frame part. For this purpose, the threaded spindle preferably has a key surface for attaching a turning tool on one or both of its axial end side surfaces.

In one embodiment, the adjusting device can also be referred to as a horizontal adjustment, since it can influence the horizontal position of the sash on the frame when the hinge and the sash are mounted on the frame.

Preferably, the frame part comprises a first threaded bore formed complementary to the first threaded area and the wing part comprises a second threaded bore formed complementary to the second threaded area. This enables a particularly simple, quick and exact adjustment of the sash with respect to the frame, in particular of the sash part with respect to the frame part in the adjustment direction. For this purpose, the first threaded area of the adjusting element is preferably connected to the first threaded hole of the frame part and the second threaded area of the Adjusting element preferably in engagement with the second threaded hole of the wing part. As a result, when the threaded spindle is rotated, the wing part and the frame part can be moved towards or away from each other simultaneously in the adjustment direction, so that a wing connected to the wing part can be adjusted particularly quickly in the adjustment direction compared to a frame connected to the frame part.

The adjustment device preferably comprises at least one guide rod with a longitudinal axis extending parallel to the adjustment direction, which is anchored in one of the wing part and the frame part, and which engages in a guide, which also extends parallel to the adjustment direction and is provided in the other of the wing part and the frame part. As a result, a particularly exact alignment, guidance and positioning of the wing part with respect to the frame part can be ensured both during assembly and when adjusting the hinge. In particular, tilting of the two aforementioned components can be effectively avoided. The at least one guide rod can have a length that corresponds to at least twice the maximum possible adjustment path in the adjustment direction. In an assembled state, the guide rod is preferably at least one third of its length in the wing part and at least one third of its length in the frame part. The anchoring of the guide rod in one of the wing part and the frame part can for example be realized by means of a press fit. For example, the guide rod is laterally fixed or held on at least one longitudinal section, that is to say essentially perpendicular to its longitudinal axis, in a recess in one of the wing part and the frame part. For this purpose, it can be provided that the aforementioned longitudinal section for anchoring the guide rod in one of the wing part and the frame part has a dimension that is slightly larger than the rest of the length of the guide rod, in particular an enlarged diameter. Furthermore, a surface texture suitable for anchoring, such as corrugation, can be formed on an outer surface of this anchoring longitudinal section. The guide can be designed, for example, as a recess which can be designed to correspond to a cross section of the guide rod and can have a slightly larger dimension than the guide rod, in particular a larger diameter. Two guide rods are preferably provided on the belt, which are particularly preferably arranged at a distance from one another in a plane parallel to the pivot axis. As a result, inclination and / or tilting of the wing part relative to the frame part can be avoided particularly effectively.

The guide rod preferably comprises a round rod with a circular cross-section and the guide has a bore with an inner cross-section adapted to the cross-section of the round rod in such a way that the round rod engages the bore at least almost free of play and displaceable in the adjustment direction. This enables a particularly high level of accuracy in guiding the wing part with respect to the frame part.

The wing part preferably has a first contact surface and the frame part a second contact surface, the first contact surface and the second contact surface extending parallel to the adjustment direction and more preferably perpendicular to the pivot axis and lying directly or indirectly against one another. As a result, the forces acting on the wing part due to the wing connected to it, in particular the weight of a wing, can be particularly advantageously transferred to the frame part and ultimately the frame connected to it, in particular over a relatively large surface area. In addition, this enables a simplified adjustment of the sash with respect to the frame part, in particular due to an increased ease of movement of the displacement of the sash part with respect to the frame part during an adjustment in the adjustment direction.

At least one clamping screw is preferably provided which passes through one of the frame part and the wing part in an elongated opening, the longitudinal direction of which extends parallel to the adjustment direction, and which is screwed into an internal thread provided on the other of the frame part and the wing part. As a result, the wing part can be fixed or held in a desired position in a particularly simple and effective manner with respect to the frame part. For this purpose, the head of the clamping screw, in particular in a side area of the opening, can rest against the frame part and its thread can engage the internal thread of the wing part. Particularly preferably, an area offset from the outer surface is provided on an outer surface of the frame part in the side area of the opening, in which the head of the clamping screw is arranged and along which it is displaceable when the sash part is displaced relative to the frame part. This in particular enables a compact design and a visually appealing appearance.

Preferably, at least one of the frame fastening arrangement and the sash fastening arrangement has a fastening adapter which has a profile section with a C-groove which extends in the longitudinal direction parallel to the pivot axis and which has a 180 degree axis of symmetry perpendicular to the longitudinal direction. Has rotational symmetry. The profile section preferably has longitudinal ends, preferably two, which are referred to in the context of this publication as profile section longitudinal ends. This profile section preferably has two open profile section longitudinal ends.

The 180-degree rotational symmetry is preferably designed in such a way that the C-groove is mapped onto itself when rotated about the axis of symmetry by 180 °.

In this way, a prerequisite is created for achieving a tape that is easy to manufacture and resilient. In addition, a prerequisite is created that the same mounting adapter can be used for hinges for both right and left hinged leaves and no two different parts have to be kept available. A prerequisite for simple adjustability is also created.

The tape can preferably be referred to as a "concealed tape". It is preferably not visible from the outside when the sash is closed and is at least partially housed inside the frame profile and / or sash profile. For this purpose, the belt preferably has means which enable the pivot axis to be arranged in the interior of the frame profile or wing profile when the belt is installed. These means preferably comprise a carrier plate. The support plate can be in one piece or have two parts arranged opposite the swivel bracket. The carrier plate or each part of the carrier plate preferably has two legs which are preferably arranged at an angle of approximately 90 ° to one another. The legs can be formed in one piece or in two pieces. The two-part design makes it possible to adapt the band to profiles of the frame or sash of different depths by exchanging only part of a leg. The carrier plate shaped in this way preferably enables the pivot axis to be arranged in the interior of the frame or wing profile. In addition, these means preferably include the swivel bracket. This preferably has two areas arranged approximately at an angle to one another. This angle is preferably between 85 ° and 110 ° and can be approximately 90 ° or 105 °. The length of a region of the swivel bracket preferably corresponds at least approximately to the length of a leg. The swivel bracket formed in this way preferably enables swiveling about the swivel axis despite the swivel axis arranged in the interior of the frame or wing profile.

The fastening adapter preferably has fastening means for fastening to the frame or wing. The fastening adapter is preferably screwed to the frame profile or the wing profile. The fastening adapter preferably has an extension in the longitudinal direction of the C-groove that is smaller than ¼ of the frame height or the sash height. The fastening adapter preferably has an extension in the longitudinal direction of the C-groove that is smaller than 50 cm.

The belt preferably has at least one adjustment device, by means of which parts of the belt can be displaced relative to one another in the adjustment direction. The adjustment direction preferably runs perpendicular to the pivot axis and more preferably perpendicular to the adjustment direction. In one embodiment, the adjustment device can also be referred to as a sealing pressure adjustment, since it can influence the sealing pressure of the sash on the frame when the band and the sash are mounted on the frame. The adjusting device preferably comprises the fastening adapter.

The profile section preferably has two side walls laterally delimiting the C-groove. At least one elongated hole is preferably provided in at least one of these walls. Particularly preferably, these walls have elongated holes arranged opposite one another. In this way, a prerequisite for a simple and resilient adjustment device is created.

Preferably, at least one of the frame fastening arrangement and the sash fastening arrangement comprises a connecting element which engages in the C-groove with lateral play between the side walls. This also creates a prerequisite for a simple and resilient adjustment device.

If the connecting element comprises at least one transverse threaded bore extending transversely to the longitudinal direction of the C-groove between the two side walls, which comprises an adjusting thread element with two adjusting thread element longitudinal ends, then a prerequisite for a simple and resilient adjusting device is again created.

The longitudinal ends of the adjusting thread element are preferably in each case directly or indirectly against one of the side walls. The adjusting threaded element is preferably fixed in its longitudinal direction in the C-groove in this way. Rotating the adjusting thread element to operate the adjusting device therefore preferably leads to a displacement of the connecting element, preferably along the adjusting thread element and more preferably in the adjustment direction.

The adjustment device can be conveniently operated if the adjustment thread elements each have a longitudinal end at least at one of their adjustment thread element Have a wrench surface for attaching a turning tool - preferably through one of the elongated holes in the side walls. With wrench surfaces arranged on the two longitudinal ends of the adjusting thread element of an adjusting thread element and mutually opposite elongated holes in the side walls of the C-groove, particularly convenient operability results from both sides of the adjusting thread element or elements.

The belt preferably has an adjusting device by means of which parts of the belt can be displaced relative to one another in the adjustment direction. The adjustment direction preferably runs parallel to the pivot axis. In one embodiment, the adjusting device can also be referred to as a vertical adjustment, since it can influence the vertical position of the sash on the frame with the hinge and the sash mounted on the frame. The adjustment device preferably comprises the fastening adapter.

The adjustment direction, the adjustment direction and the setting direction preferably run perpendicular to one another.

A prerequisite for a resilient adjustment device is created when the fastening adapter comprises a rear wall in the area of the profile section, which - preferably in the area of the profile section longitudinal ends of the profile section - has a fastening adapter opening.

In turn, a resilient setting device benefits if an insert with an insert threaded hole preferably extending in the longitudinal direction of the C-groove is provided in each of the fastening adapter openings.

An adjusting threaded element is then preferably provided in each of the threaded insert bores. Each adjusting thread element preferably has at least one adjusting thread element end.

The connecting element preferably has at least one connecting element contact surface. This preferably runs at least approximately perpendicular to the longitudinal direction of the C-groove. Two mutually opposite connecting element contact surfaces are preferably provided.

The adjusting thread element can preferably be screwed with an adjusting thread element end against a connecting element contact surface of the connecting element. In this way, the connecting element is preferably clamped in the setting direction between two setting thread elements and can be set by these - preferably in the setting direction.

If the connecting element has no play in the C-groove perpendicular to the lateral play and perpendicular to the longitudinal direction of the C-groove, the play that is necessary for the displaceability of the connecting element in the fastening adapter in the longitudinal direction of the C-groove during assembly or the adjustment device is required, then a particularly resilient arrangement is created.

Resilient, easy-to-use and easy-to-manufacture fastening means for fastening the fastening adapter to the frame or sash can be created if the rear wall of the fastening adapter comprises two tabs extending in the longitudinal direction from the longitudinal ends of the profile section, and one in each of the tabs - preferably similar - Bracket threaded hole is provided.

A fastening element is preferably provided with a key contact surface extending parallel to the longitudinal direction. In this way, the wing can initially be suspended in the frame, preferably with the production of a form-fitting connection, in which the key contact surface can be brought into direct or indirect contact with the frame or the wing. The definition can then take place afterwards. The fastening member is preferably made mushroom-shaped.

Preferably, the fastening member can optionally be screwed into one of the two threaded bracket holes. This again creates a prerequisite that the same fastening adapter can be used for hinges for both right and left hinged wings and no two different parts have to be kept available. Depending on whether it is a band for right or left hinged sashes, the fastening element can be screwed into one or the other threaded lug hole.

If a fastening screw is provided which has a threaded shaft whose outer cross-section is smaller than the inside diameter of the tab threaded hole, then a prerequisite for easy usability of the same mounting adapter for right and left hinged wings is created, since the fastening screw then that tab threaded hole in which the fastening member is not arranged, can reach through.

Preferably, one of the frame attachment arrangements and the wing attachment arrangement has a reinforcement plate. This can preferably be screwed to the frame or sash. It preferably has an approximately keyhole-shaped Hole on, with a larger area through which the fastening member can be passed, and a smaller area which can be reached from behind by the key contact surface of the fastening member. In addition to the keyhole-shaped hole, the reinforcement plate preferably has a threaded hole for the fastening screw.

Preferably, the swivel bracket is pivotably mounted on at least one of the frame attachment arrangement and the sash attachment arrangement about a pivot axis defined by a hinge bolt which engages in one of the frame attachment arrangement and the sash attachment arrangement and in the swivel bracket.

It can be provided that the hinge bolt is either rotatably provided in one of the frame attachment arrangement and the sash attachment arrangement and the swivel bracket is provided rotatably about the hinge pin about the pivot axis, or the hinge bolt is provided rotatably about the pivot axis in one of the frame attachment arrangement and the sash attachment arrangement and is non-rotatably provided in the swivel bracket. Blocking means can be provided for optionally blocking this rotatability.

These blocking means simplify the assembly of the band, since it is prevented that parts of the band pivot about the pivot axis with respect to one another, for example during the attachment of the sash to the frame.

The blocking means preferably allow the rotatability to be blocked continuously. This makes assembly even easier, since the fitter can choose the position in which he would like the swivel bracket to be blocked for assembly of the frame, depending on the prevailing installation conditions.

The blocking means preferably provide an adjustable blocking torque.

It is preferred that the blocking torque can be exceeded without being destroyed. If, despite blocked rotation of the hinge bolt in one of the frame fastening arrangement and the sash fastening arrangement or in the swivel bracket by the blocking means, such a rotation occurs because the blocking torque of the blocking means has been exceeded, this does not result in any destruction. This again simplifies assembly, since the fitter, for example if he inadvertently exceeds the blocking torque while assembling the sash, can also use the blocking means that have not been destroyed during another installation attempt.

The blocking means preferably comprise a blocking screw element which is screwed either into a blocking thread receptacle of one of the frame fastening arrangement or the sash fastening arrangement or into a blocking thread receptacle of the swivel bracket and, when fully screwed in, causes a clamping effect with the hinge bolt. The locking screw element preferably acts directly on the hinge bolt, that is to say it can be brought into contact with it. In the context of this publication, the term “completely screwed in state” preferably means the state screwed in up to contact with the hinge pin. Several advantages are achieved in this way: By acting on the hinge pin, a locking screw element, the rotatability can be locked in a load-bearing capacity. In addition, in this case, the blocking means can also be arranged on the belt in a captive manner in their deactivated state, ie if they do not block the rotatability. This is because the locking screw element can also be arranged in a captive manner when it is screwed in, but not completely screwed in. The blocking means are also preferably arranged on the hinge so that they cannot be lost while the blocking effect is being established or released, because for this purpose only the complete screwing in of the already screwed-in locking screw element or the loosening of the completely screwed-in locking screw element is preferred until it is no longer in contact with the hinge bolt , required. Finally, in this way, an adjustable blocking torque can be made available very easily and effectively, the - possibly accidental - exceeding of which is possible without destruction.

A simple and reliable non-rotatable arrangement of the hinge bolt is achieved if this is achieved by knurling the hinge bolt and an interference fit between the hinge bolt and one of the frame fastening arrangement and the sash fastening arrangement or the swivel bracket.

In the embodiment in which the hinge bolt is non-rotatably provided in one of the frame fastening arrangement and the sash fastening arrangement and the swivel bracket is provided to be rotatable about the hinge bolt about the pivot axis and the blocking means comprise a blocking screw element which is screwed into a blocking thread receptacle of the swivel bracket Swivel bracket preferably an access opening for actuating the locking screw element is provided. As a result, assembly can again be facilitated, since the actuation of the blocking screw element is simplified.

If the hinge pin has a constriction with which the completely screwed-in locking screw element is in contact, then a prerequisite for a particularly effective provision of a locking torque is created.

The constriction and the front end of the locking screw element in the screwing-in direction are preferably designed to be complementary to one another. As a result, the provision of the locking torque can be further improved.

If the constriction and the front end of the locking screw element in the screwing-in direction are designed so that they are complementary to each other that at least two linear contact points between the locking screw element and the hinge bolt at an angle of less than 180 degrees result, then at a given tightening torque of the locking screw element a be provided particularly large locking torque.

The front end of the locking screw element in the screwing-in direction is preferably designed to be conical or frustoconical.

The constriction is preferably designed as a circumferential groove, the cross section of which has two sides that are not parallel to one another. The opening angle of the cone or truncated cone of the locking screw element preferably corresponds at least approximately to the inclination of the sides of the groove cross-section to one another.

The locking screw element and / or the locking thread receptacle can have an anti-rotation device, for example in the form of a plastic coating, in order to prevent the locking screw element from accidentally coming into contact with the hinge pin, for example due to vibrations.

• 1 - ein erfindungsgemäßes Band in einer Explosionsdarstellung in einer ersten perspektivischen Ansicht;
• 2 - Teile des Bandes aus 1 in einer Explosionsdarstellung in einer zweiten perspektivischen Ansicht;
• 3 - die in 2 gezeigten Teile des Bandes in einer Explosionsdarstellung in einer dritten perspektivischen Ansicht;
• 4 - das Band in einer durch die Gewindespindel geschnittenen Explosionsdarstellung; und
• 5 - das Band gemäß 4 in zusammengesetzten Zustand in einer durch die Gewindespindel geschnittenen Darstellung.

An exemplary embodiment of the invention is explained in more detail below with reference to the figures. The same reference numbers denote the same components. They show schematically:

• 1 - A tape according to the invention in an exploded view in a first perspective view;
• 2 - Parts of the tape 1 in an exploded view in a second perspective view;
• 3 - in the 2 Parts of the band shown in an exploded view in a third perspective view;
• 4th - The tape in an exploded view cut through the threaded spindle; and
• 5 - the tape according to 4th in the assembled state in a representation cut through the threaded spindle.

The hinge, indicated as a whole by 100 in the figures, serves for the pivotable connection of a sash, not shown in the figures, to a frame not shown in the figures.

The ribbon 100 includes a frame mounting assembly 1 , a wing mounting arrangement 2 and one the wing mounting assembly 2 with the frame mounting arrangement 1 connecting swivel bracket 3 . It should be clear that the frame mounting arrangement 1 basically optionally on a frame of a door or window opening or a wing forming the door or window, and the wing fastening arrangement 2 can be arranged on the corresponding other component, namely on the frame or on the wing. In the embodiment shown is the frame mounting arrangement 1 for the frame-side arrangement and the sash fastening arrangement 2 intended for wing-side arrangement.

The swivel bracket 3 is on at least one of the frame mounting arrangements 1 and the wing mounting assembly 2 around a pivot axis S. pivoted. The swivel bracket 3 includes one with the frame mounting assembly 1 connected frame part 4th and one with the wing mounting assembly 2 connected wing part 5 .

The ribbon 100 is in the present case designed as a "concealed tape". It is therefore not visible from the outside when the sash is closed, but is mainly housed inside the frame profile, which is not shown in the figures. The pivot axis S. is arranged in the embodiment shown with the tape mounted inside the frame profile. To this end, the frame mounting arrangement includes 1 a carrier plate 54 , 54 ' , the two legs arranged at an angle of approximately 90 ° to one another 55 , 55 ' , 56 , 56 ' having. One of the thighs 56 , 56 ' is designed in two parts. The swivel bracket 3 has two areas arranged at an angle of approximately 90 ° to one another 57 , 58 on. The length of an area 58 of the swivel bracket 3 agrees at least roughly with the length of the leg 56 , 56 ' the carrier plate 54 , 54 ' match.

The ribbon 100 also has an adjusting device 6th on, by means of which the wing part 5 relative to the frame part 4th in a perpendicular to the pivot axis S. running adjustment direction R1 is relocatable. To this end, the adjusting device includes 6th in this case an adjustment element 12th to relocate the Wing part 5 relative to the frame part 4th in the direction of adjustment R1 .

The adjustment element 12th includes a threaded spindle 13 having a first thread area 14th and a second threaded area 15th having, the threads of the first thread portion 14th and the second threaded area 15th are formed in opposite directions. For easy, quick and exact adjustment of the wing part 5 opposite the frame part 4th in the direction of adjustment R1 the threaded spindle is stationary 13 both with the frame part 4th as well as with the wing part 5 in an operative connection. In particular, the threaded spindle is stationary 13 with one in the first thread area 14th formed first thread 16 with the frame part 4th and with one in the second threaded area 15th formed second thread 17th with the wing part 5 engaged. The frame part 4th one complementary to the first thread area 14th trained first threaded hole 18th , in particular a first internal thread 62 , and the wing part 5 one complementary to the second thread area 15th formed second threaded hole 19th , in particular a second internal thread 63 , on. The first threaded hole 18th extends in the present case in the adjustment direction R1 . For turning the threaded spindle 13 at least indicate this to her 60 marked axial end side a key area easily accessible from the outside 61 to which a turning tool, not shown here, can be attached. With this configuration, the threaded spindle is rotated 13 the frame part 4th and the wing part 5 simultaneously driven towards or away from each other.

The adjustment device 6th In the present case it comprises two guide rods 7th , 7 ' , which in the present embodiment in a to the pivot axis S. parallel plane are arranged spaced from each other, and each one parallel to the adjustment direction R1 extending longitudinal axis A. 'A'. The management staff 7th , 7 ' are in an assembled state both in the wing part 5 as well as in the frame part 4th in adjustment direction R1 inserted. In particular, the leadership bars 7th , 7 ' each in one of the wing part 5 and the frame part 4th anchored, and each engage in a parallel to the adjustment direction R1 extending, in the other of the wing part 5 and the frame part 4th planned tour 9 , 9 ' one. Every senior staff 7th , 7 ' can have a length that is at least twice the maximum possible adjustment path in the adjustment direction R1 corresponds. The guide rod is in an assembled state 7th , 7 ' preferably with at least a third of its length in the wing part 5 and at least one third of its length in the frame part 4th . The anchoring of the management staff 7th , 7 ' in one of the wing part 5 and the frame part 4th takes place here by means of a press fit. To this end, the management staff 7th , 7 ' a longitudinal section 64 , 64 ' on, one across from the rest of the length of the stylet 7th , 7 ' has slightly enlarged diameter. In this longitudinal section 64 , 64 ' can the management team 7th , 7 ' in the assembled state laterally, that is to say essentially perpendicular to its longitudinal axis, in a recess in one of the wing part 5 and the frame part 4th be fixed or held. For this purpose, on an outer surface of this longitudinal section 64 , 64 ' a surface quality suitable for anchoring, such as corrugation, can be formed.

Here are the management staff 7th , 7 ' each as a round bar 11 , 11 ' formed with a circular cross-section. The anchoring takes place accordingly by means of an anchoring bore 8th , 8th' , which has an inner cross-section adapted in such a way that the round bar 11 , 11 ' at least with its longitudinal section 64 , 64 ' is fixed in it. The leadership 9 , 9 ' is called a pilot hole 10 , 10 ' formed, which one to the cross section of the round rod 11 , 11 ' has such adapted inner cross-section, in particular one opposite the guide rod 7th , 7 ' slightly larger diameter so that the round rod 11 , 11 ' at least almost free of play and in the direction of adjustment R1 can be moved into the respective guide hole 10 , 10 ' intervenes.

The wing part 5 in the present case comprises four first contact surfaces 20th , 20 ' , 20 '' , 20 ''' and the frame part 4th four second contact surfaces 21st , 21 ' , 21 '' , 21 ''' , the first contact surfaces 20th , 20 ' , 20 '' , 20 ''' and the second contact surfaces 21st , 21 ' , 21 '' , 21 ''' each parallel to the adjustment direction R1 , and preferably perpendicular to the pivot axis S. , extend and lie directly or indirectly next to one another in pairs. In the embodiment shown, the first contact surface lies in the assembled state 20th directly or indirectly on the second contact surface 21st , the first contact surface 20 ' directly or indirectly on the second contact surface 21 ' , the first contact surface 20 " directly or indirectly on the second contact surface 21 '' and the first contact surface 20 ''' directly or indirectly on the second contact surface 21 ''' . This allows on the one hand the on the wing part 5 Acting forces particularly advantageously over a relatively large surface area in the frame part 4th and ultimately transferred to the frame, not shown here, connected to it, for example, and on the other hand particularly easy movement when moving the sash part 5 opposite the frame part 4th are made possible.

For fixing or holding the sash part 5 opposite the frame part 4th In the present case, there are two clamping screws in a desired, in particular adjusted, position 22nd , 22 ' intended. Every clamping screw 22nd , 22 ' penetrates here one of the frame part 4th and the wing part 5 in one slot-shaped breakthrough 23 , 23 ' whose longitudinal direction is parallel to the adjustment direction R1 extends, and is in one on the other of the frame part 4th and the wing part 5 provided internal thread 24 , 24 ' screwed in. The clamping screws 22nd , 22 ' are in particular each with their screw head 65 , 65 ' in a side area of the opening 23 , 23 ' on the frame part 4th on, and stand with their thread 66 , 66 ' with the internal thread 24 , 24 ' of the wing part 5 engaged. In the present example, in particular to achieve a particularly compact design, there is an outer surface 67 of the frame part 4th , in the side area of each opening 23 , 23 ' , one opposite the outer surface 67 remote area 68 , 68 ' provided in each of the screw head 65 , 65 ' the clamping screw 22nd , 22 ' arranged and when relocating the wing part 5 opposite the frame part 4th is movable.

Approximately 2 shows that in the embodiment shown, the wing mounting arrangement 2 a mounting adapter 25th having a profile section 26th with a C-groove 27 having. The C-groove 27 extends in the longitudinal direction L. parallel to the swivel axis S. .

A synopsis of the 2 and 3 shows that the C-slot 27 a 180 degree rotational symmetry to one to the longitudinal direction L. vertical axis of symmetry B. having. It can also be seen that this is the C-groove 27 having profile section 26th two open profile section longitudinal ends 28 , 28 ' having. The 180 degree rotational symmetry is designed in such a way that the C-groove is mapped onto itself when it is rotated about the axis of symmetry by 180 °.

In the embodiment shown, the wing mounting arrangement comprises 2 a reinforcement plate 70 .

The mounting adapter 25th comprises adapter fastening means in the exemplary embodiment shown 59 for attachment to the wing, not shown, in particular to a wing profile. More precisely, is the mounting adapter 25th with the wing profile, more precisely with the reinforcement plate screwed to the wing profile, not shown 70 , screwed.

The mounting adapter 25th has an extension in its longitudinal direction L. that is smaller than 50 cm.

The ribbon 100 has an adjusting device, which can be referred to as a sealing pressure adjustment, and in the area of the fastening adapter 25th is realized. The adjustment device is used in particular to adjust the fastening adapter 25th opposite the wing part 5 in one as well as the direction of adjustment R1 as well as the swivel axis S. vertical adjustment direction V .

How about from 2 shows the profile section 26th with the C-groove 27 two the C-groove 27 laterally limiting side walls 29 , 29 ' with elongated holes arranged opposite one another 30th , 30 ' , 30 '' , 30 '' ' on.

In the embodiment shown, the wing mounting arrangement comprises 2 a fastener 31 which is in the C-slot 27 with side play 32 , 32 ' between the side walls 29 , 29 ' intervenes (see for example 5 ).

The connecting element 31 includes two themselves between the two side walls 29 , 29 ' transverse to the longitudinal direction L. extending transverse threaded holes 33 , 33 ' each one moving in the direction of adjustment V extending adjusting thread element 34 , 34 ' include. Any adjusting thread element 34 , 34 ' includes two adjusting thread element longitudinal ends 35 , 35 ' , 35 '' , 35 ''' . All adjusting thread element longitudinal ends 35 , 35 ' , 35 '' , 35 ''' each lie directly on one of the side walls 29 , 29 ' at (see about 4th ) and have a wrench flat 36 , 36 ' for attaching a turning tool, not shown in the figures, through one of the elongated holes 30th , 30 ' , 30 '' , 30 '' 'on (see about 1 ).

The mounting adapter 25th includes in the area of the profile section 26th a back wall 37 . The back wall 37 points in the area of the profile section longitudinal ends 28 , 28 ' of the profile section each have a fastening adapter opening 38 , 38 ' on (see 1 and 2 ). In each of the fastening adapter openings 38 , 38 ' is a mission 39 , 39 ' with a lengthways L. the C-slot 27 extending insert threaded hole 40 , 40 ' provided (see 1 ).

In each of the insert tapped holes 40 , 40 ' is an adjusting thread element 41 , 41 ' an adjustment device is provided with an adjustment thread element end 42 , 42 ' against a fastener contact surface 43 , 43 ' of the connecting element 31 can be screwed (see for example 2 ). The adjusting device is used in particular to adjust the connecting element 31 compared to the mounting adapter 25th in one to the pivot axis S. parallel or with this identical direction of adjustment E. .

Like a synopsis of the 1 and 2 shows includes the rear wall 37 of the mounting adapter 25th two lengthways L. from the profile section longitudinal ends 28 , 28 ' of the profile section 26th extending tabs 44 , 44 ' , and in each of the tabs 44 , 44 ' is a similar bracket tapped hole 45 , 45 ' intended.

The adapter fasteners 59 include an attachment member 46 with one extending parallel to the longitudinal direction L. extensive key contact area 47 . As a result, in the exemplary embodiment shown, a form-fitting connection between the fastening element can - at least in a first fastening step 46 and the reinforcement plate 70 be made possible. In particular, the wing, not shown in the figures, can initially be suspended in the frame in which the key contact surface 47 with the wing or the reinforcement plate, not shown 70 can be brought into contact directly or indirectly. The definition can then take place afterwards. The fastener 46 is mushroom-shaped and optionally in one of the two threaded bracket holes 45 , 45 ' screwable.

The adapter fasteners 59 include in addition to the fastening member 46 a fastening screw 48 . This has a threaded shaft 49 whose outer cross-section is smaller than the inner diameter of the tab threaded holes 45 , 45 ' is. The fastening screw 48 goes through that tab threaded hole 45 ' in which the fastening member 46 is not arranged.

The reinforcement plate 70 has a keyhole-shaped hole 71 on, with a larger area 72 through which the fastening member 46 can be passed through and a smaller area 73 that from the key pad 47 of the fastener 46 is behindable. The reinforcement plate 70 is in the embodiment shown by means of reinforcement plate screws 74 Can be screwed to the wing or wing profile. In addition to the keyhole-shaped hole 71 has the reinforcement plate 70 a threaded hole 75 for the fastening screw 48 on.

The swivel bracket 3 is in the embodiment shown on the frame mounting arrangement 1 around one by a hinge bolt 50 that goes into the frame mounting assembly 1 and in the swivel bracket 3 engages, defined pivot axis S. pivoted.

In the embodiment shown, the hinge pin is 50 non-rotatably in the frame mounting arrangement 1 provided, and the swivel bracket 3 is around the hinge pin 50 around the pivot axis S. rotatably provided.

They are blocking agents 51 intended to optionally block this rotation. These are provided in such a way that they enable the rotation to be locked continuously. They also provide an adjustable blocking torque and this blocking torque can be exceeded without being destroyed.

Like in the 1 , 4th and 5 shown include the blocking means 51 a locking screw element 52 that is in a locking thread mount 53 of the swivel bracket 3 is screwed in and in the screwed-in state a clamping effect with the hinge pin 50 causes.

The non-rotatable arrangement of the hinge pin 50 in the frame mounting arrangement 1 is through a knurl 81 of the hinge bolt 50 and an interference fit between the hinge pin 50 and the frame mounting arrangement 1 achieved.

Like that 2 and 4th show is in the swivel bracket 3 an access opening 80 , to operate the locking screw element 52 intended.

The hinge bolt 50 points in the contact area with the locking screw element 52 a constriction 82 on (see 1 ).

As not shown in detail in the figures, the constrictions are 82 and a front end in the screw-in direction 83 of the locking screw element 52 designed to be complementary to one another in such a way that two linear contact points which are inclined to one another at an angle of less than 180 degrees result.

In the exemplary embodiment shown, this is achieved in that the front end in the screwing-in direction 83 of the locking screw element 52 is designed frustoconically and the constriction 82 is designed as a groove whose cross section has two mutually non-parallel sides. The opening angle of the truncated cone of the locking screw element 52 corresponds at least approximately to the inclination of the sides of the groove cross-section to one another.

List of reference symbols

1

Frame mounting arrangement

2

Wing mounting arrangement

3

Swivel bracket

4th

Frame part

5

Wing part

6th

Adjustment device

7, 7 '

Management staff

8, 8 '

Anchor hole

9, 9 '

guide

10, 10 '

Guide hole

11, 11 '

Round bar

12

Adjustment element

13

Threaded spindle

14th

first thread area

15th

second thread area

16

first thread

17th

second thread

18th

first threaded hole

19th

second threaded hole

20, 20 ', 20' ', 20' ''

first contact surface

21, 21 ', 21' ', 21' ''

second contact surface

22, 22 '

Clamping screw

23, 23 '

breakthrough

24, 24 '

inner thread

25th

Mounting adapter

26th

Profile section

27

C-groove

28, 28 '

Profile section longitudinal end

29, 29 '

Side wall

30, 30 ', 30' ', 30' ''

Long hole

31

Connecting element

32, 32 '

game

33, 33 '

Transverse threaded hole

34, 34 '

Adjusting thread element

35, 35 ', 35' ', 35' ''

Adjusting thread element longitudinal end

36, 36 '

Wrench flat

37

Back wall

38, 38 '

Fastening adapter opening

39, 39 '

commitment

40, 40 '

Insert tapped hole

41, 41 '

Adjustment thread element

42, 42 '

Adjustment thread element end

43, 43 '

Fastener contact surface

44, 44 '

Tab

45, 45 '

Tab threaded hole

46

Fastener

47

Key contact area

48

Fastening screw

49

Threaded shaft

50

Hinge pin

51

medium

52

Locking screw element

53

Thread mount

54, 54 '

Carrier plate

55, 55 '

Leg of the carrier plate

56, 56 '

Leg of the carrier plate

57

Area of the swivel bracket

58

Area of the swivel bracket

59

Adapter fasteners

60

axial end side

61

Wrench flat

62

first internal thread

63

second internal thread

64, 64 '

Longitudinal section

65, 65 '

Screw head

66, 66 '

thread

67

Exterior surface

68, 68 '

remote area

70

Reinforcement plate

71

keyhole-shaped hole

72

larger area

73

smaller area

74

Reinforcement plate screws

75

Threaded hole

80

Access opening

81

Knurling

82

Constriction

83

front end of the locking screw element

100

tape

A, A '

Longitudinal axis

B.

Axis of symmetry

E.

Adjustment direction

L.

Longitudinal direction

R1

Adjustment direction

S.

Swivel axis

V

Adjustment direction

Claims (6)

Band (100) for the pivotable connection of a sash to a frame, with a frame fastening arrangement (1), with a sash fastening arrangement (2), with a swivel bracket (3) which connects the sash fastening arrangement (2) to the frame fastening arrangement (1) and which is at least one the frame fastening arrangement (1) and the sash fastening arrangement (2) are pivotably mounted about a pivot axis (S) and which comprises a frame part (4) connected to the frame fastening arrangement (1) and a sash part (5) connected to the sash fastening arrangement (2), and with an adjusting device (6) by means of which the sash part (5) can be displaced relative to the frame part (4) in an adjustment direction (R1) running perpendicular to the pivot axis (S), and which has a first adjusting element (12) for displacing the sash part ( 5) relative to the frame part (4) in the adjustment direction (R1), characterized in that the first adjustment element (12) has a threaded spindle (13) comprises, which has a first threaded area (14) and a second threaded area (15), the threads (16, 17) of which are formed in opposite directions. Tape after Claim 1 , characterized in that the frame part (4) comprises a first threaded hole (18) formed complementary to the first threaded area (14) and the wing part (5) comprises a second threaded hole (19) formed complementary to the second threaded area (15). Tape after one of the Claims 1 or 2 , characterized in that the adjustment device (6) comprises at least one guide rod (7, 7 ') with a longitudinal axis (A, A') extending parallel to the adjustment direction (R1), which is located in one of the wing part (5) and the frame part ( 4) is anchored, and engages in a guide (9, 9 ') also extending parallel to the adjustment direction (R1) and provided in the other of the wing part (5) and the frame part (4). Tape after Claim 3 , characterized in that the guide rod (7, 7 ') is a round rod (11, 11') with a circular cross-section and the guide (9, 9 ') has a bore (10, 10') with a cross-section of the round rod ( 11, 11 ') comprises an interior cross-section adapted in such a way that the round rod (11, 11') engages in the bore (10, 10 ') at least almost free of play and displaceable in the adjustment direction (R1). Tape after one of the Claims 1 to 4th , characterized in that the wing part (5) has a first contact surface (20, 20 ', 20 ", 20"') and the frame part (4) has a second contact surface (21, 21 ', 21 ", 21"'), the first contact surface (20, 20', 20 ", 20"') and second contact surface (21, 21', 21 ", 21"') extending parallel to the adjustment direction (R1) and lie directly or indirectly against one another. Tape after one of the Claims 1 to 5 , characterized in that at least one clamping screw (22, 22 ') is provided, which one of the frame part (4) and the wing part (5) in an elongated opening (23, 23'), the longitudinal direction of which is parallel to the adjustment direction (R1) extends, penetrates, and which is screwed into an internal thread (24, 24 ') provided on the other of the frame part (4) and the wing part (5).

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