EP3555397B1 - Displacement arrangement having a rolling bearing guide - Google Patents

Displacement arrangement having a rolling bearing guide Download PDF

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Publication number
EP3555397B1
EP3555397B1 EP17811288.4A EP17811288A EP3555397B1 EP 3555397 B1 EP3555397 B1 EP 3555397B1 EP 17811288 A EP17811288 A EP 17811288A EP 3555397 B1 EP3555397 B1 EP 3555397B1
Authority
EP
European Patent Office
Prior art keywords
control
sash
displacement arrangement
projection
displacement
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP17811288.4A
Other languages
German (de)
French (fr)
Other versions
EP3555397A1 (en
Inventor
Winfried Reich
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Roto Frank Fenster und Tuertechnologie GmbH
Original Assignee
Roto Frank Fenster und Tuertechnologie GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Roto Frank Fenster und Tuertechnologie GmbH filed Critical Roto Frank Fenster und Tuertechnologie GmbH
Priority to PL17811288T priority Critical patent/PL3555397T3/en
Publication of EP3555397A1 publication Critical patent/EP3555397A1/en
Application granted granted Critical
Publication of EP3555397B1 publication Critical patent/EP3555397B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/06Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/06Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • E05D2015/1028Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane with only the wing moving transversely
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/06Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • E05D2015/1028Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane with only the wing moving transversely
    • E05D2015/1039Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane with only the wing moving transversely the wing sliding transversely on the carriage
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00Constructional elements; Accessories therefor
    • E05Y2201/60Suspension or transmission members; Accessories therefor
    • E05Y2201/622Suspension or transmission members elements
    • E05Y2201/684Rails; Tracks
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00Constructional elements; Accessories therefor
    • E05Y2201/60Suspension or transmission members; Accessories therefor
    • E05Y2201/622Suspension or transmission members elements
    • E05Y2201/688Rollers
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00Constructional elements; Accessories therefor
    • E05Y2201/60Suspension or transmission members; Accessories therefor
    • E05Y2201/622Suspension or transmission members elements
    • E05Y2201/688Rollers
    • E05Y2201/692Rollers having vertical axes
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/132Doors
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/148Windows

Definitions

  • the invention relates to a displacement arrangement for displacing a sash of a window or a door transversely to the main plane of a fixed frame of the window or the door according to the preamble of patent claim 1.
  • the invention further relates to a window or a door with such a displacement arrangement.
  • a displacement arrangement mentioned at the outset which has a guide part which can be fixedly arranged on a wing and a first control part guided on the guide part.
  • the first control part has a curved first control link in which a first control projection is guided, the first control projection being firmly connected to an actuating mechanism in the form of a drive rod.
  • the WO 2007/139354 A1 discloses an actuating mechanism in the form of a drive rod on which a roller arrangement is mounted, the drive rod being received in a guide profile with a U-shaped cross section.
  • the guide profile has curved control slotted links in which control projections are guided, the control projections being firmly mounted on connecting rods.
  • the control projections can have roller bearings in order to reduce the friction between the control projections and the control link.
  • a displacement arrangement which has a control projection, the control projection being guided in a control link.
  • a roller bearing is arranged on the control projection.
  • the DE 10 2014 220 837 B3 discloses a displacement assembly having a roller assembly.
  • the roller arrangement comprises a guide part which can be arranged on a wing and a first control part with a roller which can be displaced relative to the guide part.
  • Several roller bearings are provided between the first control part and the guide part.
  • the object of the present invention is therefore to provide a displacement arrangement which enables a user to make wing movements easier. It is a further object of the present invention to provide a window or a door with such a displacement arrangement.
  • the object according to the invention is thus achieved by a displacement arrangement for a sash of a window or a door, the sash being able to be parked in a positively controlled manner from the fixed frame by operating an actuating mechanism of the displacement arrangement.
  • the relocation order has a first control projection and a first control link, the first control projection engaging the first control link.
  • the first control link runs at least in sections at an angle to the main plane of the wing, the main plane of the wing in particular coinciding with the plane spanned by the actuating mechanism.
  • a displacement of the first control projection by means of the actuating mechanism causes a movement of a control part of the displacement arrangement, so that the sash can be set down from the fixed frame.
  • the displacement arrangement also has a guide part which can be fixedly arranged on the wing.
  • the first control projection is partially guided in a first guide slot which is formed in the guide part.
  • the first guide link preferably runs in the main plane of the wing or parallel to the main plane of the wing.
  • the first control projection has a first roller bearing in the area of the first guide slot, which can be supported on the first guide slot when the actuating mechanism is actuated.
  • the control part is preferably displaceable transversely to the main plane of the wing.
  • the invention is based on the knowledge that the operation of the actuating mechanism is significantly facilitated if the sliding friction of the first control projection on the guide part is eliminated. This sliding friction has so far been neglected, since it was assumed that significant friction losses only occur between the first control projection and the first control link.
  • the friction between the first control projection and the first guide slot accounts for a large part of the resistance of the actuating mechanism User.
  • the arrangement of the first roller bearing between the first control projection and the first guide slot therefore significantly facilitates the operation of the displacement arrangement.
  • the first roller bearing can be designed in the form of a ball bearing or needle bearing.
  • the first roller bearing can have an outer ring made of metal.
  • the first roller bearing can have an additional body, in particular in the form of an additional outer ring, made of plastic.
  • the outer ring of the first roller bearing can be coated with plastic.
  • the first roller bearing preferably has a play of less than 2 mm, in particular less than 1 mm, preferably less than 0.5 mm, more preferably less than 0.2 mm, particularly preferably less than 0, 1 mm.
  • the first control projection is arranged or formed on the actuating mechanism and the first control link is arranged or formed on the first control part. This enables a particularly simple construction of the displacement arrangement.
  • the first control part can be guided on the guide part in such a way that it can only be moved in one direction relative to the guide part.
  • the control part is preferably movable relative to the guide part exclusively perpendicular to the main plane of the wing.
  • the first control part can be rotatably mounted on the guide part.
  • the axis of rotation is preferably arranged parallel to the main plane of the wing or in the main plane of the wing.
  • the displacement arrangement can have a roller arrangement connected to the control part on the lower side of the displacement arrangement and / or a support arrangement on the upper side of the displacement arrangement.
  • the support arrangement can have a roller with an axis of rotation, the axis of rotation being aligned in particular in the main plane of the wing.
  • the first control projection can have a second roller bearing in the area of the first control link in order to minimize the friction losses between the first control projection and the first control link.
  • the second roller bearing can be designed in the form of a ball bearing or needle bearing.
  • the first roller bearing and the second roller bearing are preferably of identical design.
  • the displacement arrangement has a roller support bearing which is arranged or formed between the guide part and the control part.
  • the support roller bearing can be designed in the form of a ball bearing or - preferably - in the form of a roller bearing with several needle rollers.
  • the displacement arrangement can have a second control projection which engages in a second control link and is guided in a second guide link of the guide part.
  • the second control link is formed at least in sections at an angle to the main plane of the wing.
  • the second guide link preferably runs in the main plane of the wing or parallel to the main plane of the wing.
  • the first roller bearing of the second control projection preferably has a play of less than 2 mm, in particular less than 1 mm, preferably less than 0.5 mm, more preferably less than 0.2 mm, particularly preferably less, in the second guide slot than 0.1 mm.
  • the second control projection preferably has a first roller bearing for supporting the second control projection on the second guide slot.
  • the second control projection can have a second roller bearing to support the second control projection on the second control link.
  • the first roller bearing of the first control projection can be designed in the same way as the first roller bearing of the second control projection.
  • the second roller bearing of the first control projection can be designed like the second roller bearing of the second control projection.
  • the first control projection is preferably designed in the same way as the second control projection.
  • the object according to the invention is also achieved by a window or a door with a fixed frame, a sash and a displacement arrangement as described above.
  • the guide part can be permanently mounted on the wing.
  • the wing is preferably designed in the form of a sliding wing, which can be set down, in particular parallel, from the fixed frame and is displaceable parallel to the fixed frame.
  • Fig. 1 shows a displacement arrangement 10 with an actuating mechanism 12 designed as a circumferential drive rod fitting which can be operated via an actuating handle 14.
  • the actuation mechanism 12 is on a / a in the Figs. 4 and 5 window or door shown and extends along the fold circumferential direction 16.
  • the fold circumferential direction 16 extends in the main plane 18 (in Fig. 1 only indicated) of the window or door.
  • the displacement arrangement 10 has two points a, b with a roller arrangement 20a, 20b and two points c, d with a support arrangement 22a, 22b, the Roller arrangements 20a, 20b and the support arrangements 22a, 22b can each be displaced transversely to the circumferential direction 16 of the fold.
  • Fig. 2 shows part of the components of section II according to FIG Fig. 1 .
  • the actuation mechanism 12 has a bolt-shaped first control projection 24a which engages in a first control link 26a which is designed in the form of a first control slot.
  • the first control link 26a is formed at least in sections at an angle to the circumferential direction 16 of the fold.
  • the roller arrangement 20a is displaced perpendicular to the fold circumferential direction 16.
  • the first control link 26a is formed in a control part 28.
  • the roller arrangement 20a has at least one roller 30a, 30b.
  • the roller arrangement 20a has a support roller 32 in the present case.
  • the support roller 32 has an outer diameter which is greater than the width of the rest of the roller arrangement 20a. In this way, by supporting the support roller 32, transverse forces on the roller arrangement 20a can be avoided.
  • Fig. 3 shows a representation of the detail III according to Fig. 1 .
  • the support arrangement 22a also has a support roller 32 which is arranged around a vertical axis of rotation.
  • Analogous to the structure according to Fig. 2 If the displacement arrangement 10 has a control part 28 with a first control link (not visible) in the area of detail III, into which a first control projection 24a engages.
  • the displacement arrangement 10 has a guide part 34, which in the displacement arrangement 10 according to FIG Fig. 2 is not shown.
  • the guide part 34 is immovable on the wing 40 (see Figs. 4, 5 ) assembled.
  • the first control projection 24a is mounted in the circumferential direction 16 of the fold on a first guide slot (not shown) in the guide part 28.
  • the first Control projection 24a passes through guide part 34 and engages control part 28.
  • FIG. 11 shows a view from the locking side of a window or door 36 with a fixed frame 38 and a leaf 40.
  • the actuating mechanism 12 is mounted on the leaf 40. This is supported on a running rail 42 via the roller arrangement 20a. There is a gap 44 between the wing 40 and the fixed frame 38. The wing 40 accordingly does not lie against a circumferential seal 46 of the fixed frame 38.
  • the support roller 32 rests on a guide 48 of the fixed frame 38, which guide is designed as a vertical web. In the position shown, the wing 40 can be displaced with respect to the fixed frame 38, the support roller 32 being supported on the guide 48 or being able to roll on it.
  • the fixed frame 38 also has a guide 48, which here is designed like a groove.
  • the guide 48 is the support roller 32 (see also Fig. 3 ) guided.
  • Fig. 5 12 shows the window or door 36 after the actuation mechanism 12 has been operated.
  • the roller assemblies in Fig. 5 the roller assembly 20a is visible
  • the support assemblies in Fig. 5 the support arrangement 22a is visible
  • Fig. 6 shows a further detailed view of the displacement arrangement 10 according to detail II of FIG Fig. 1 .
  • the first control projection 24a has a cylindrical shape and is arranged on the actuating mechanism 12.
  • the first control projection 24a has a first roller bearing 50 and a second roller bearing 52.
  • the first roller bearing 50 serves to guide the first control projection 24a with little friction in a first guide slot 54a of the guide part 34.
  • the second roller bearing 52 serves to guide the first control projection 24a with little friction in the first control slot 26a of the control part 28.
  • the first guide slot 54a is formed in the direction of the circumferential fold direction 16 or parallel to the circumferential fold direction 16, whereas the first control slot 26a is formed at least partially transversely to the circumferential fold direction 16.
  • the roller arrangement 20a is arranged on the control part 28.
  • the displacement arrangement 10 is in the area of detail III (see Fig. 3 ) designed analogously to this, the control part 28 instead of the roller arrangement 20a the support arrangement 22a (see Fig. 3 ) having.
  • the guide part 34 is fixed, ie rigid and immobile, on the wing 40 (see Figs. 4, 5 ) can be arranged, screwed on here. How out Fig. 6 As can be seen, a guide 56 is provided between the guide part 34 and the control part 28, which only allows a limited movement of the control part 28 relative to the guide part 34 transversely to the fold circumferential direction 16.
  • the guide 56 is designed in the form of a dovetail guide.
  • Fig. 7 shows a further example of a displacement arrangement 10.
  • the displacement arrangement 10 has a first control projection 24a and a second control projection 24b.
  • the control projections 24a, 24b are identical.
  • both control projections 24a, 24b are identical to the first control projection 24a according to FIG Fig. 6 educated.
  • Both control projections 24a, 24b are arranged on the actuation mechanism 12.
  • the first control projection 24a is guided in a first guide slot 54a, here open on one side.
  • the second control projection 24b is in one, here also open, second guide slot 54b out.
  • the first control projection 24a engages in a first control link 26a and the second control projection 24b in a second control link 26b.
  • the displacement arrangement 10 is actuated, the first control projection 24a emerges from the connecting links 26a, 54a assigned to it.
  • the second control projection 24b enters into the connecting links 26b, 54b assigned to it, so that continuous guidance of the control part 28 (see FIG Figs. 8, 9 ) given is.
  • the embodiment described here is analogous to FIG DE 10 2014 220 837 B3 , the content of which is fully referred to.
  • Fig. 8 shows a cross section of the displacement arrangement 10 in area VIII (see Fig. 7 ).
  • the guidance of the first roller bearing 50 on the first guide part 34 and the guidance of the second roller bearing 52 on the control part 28 can be seen.
  • the horizontal play of the first control projection 24a in the guide part 34 and in the control part 28, which is made up of the distances A and B (in Fig. 8 indicated enlarged for clarity) is less than 0.5 mm. Ideally, the game tends towards zero.
  • the inner rings of the roller bearings 50, 52 are spaced apart by a spacer ring 58.
  • Fig. 9 shows a cross section of the displacement arrangement 10 in the area IX (see Fig. 7 ).
  • a support roller bearing 60 is arranged between the control part 28 and the guide part 34. This means that very heavy wings 40 (see Figs. 4, 5 ) be supported with low friction.
  • the invention relates in summary to a displacement arrangement 10 for moving a sash 40 of a window or a door 36 transversely to the fixed frame 38 of the window or door 36.
  • the displacement arrangement 10 has a means of indirectly supporting the transverse movement Control part 28, which by means of a Actuating device 12 is moved relative to a guide part 34 which can be fixedly mounted on the wing 40.
  • a first control projection 24a is provided, which engages in a first control link 26a of the control part 28 and at the same time in a first guide link 54a of the guide part 34.
  • the first control projection 24a has a first roller bearing 50 for bearing on the first guide slot 54a.
  • first control projection 24a can have a second roller bearing 52 for support on the first control link 26a.
  • a roller support bearing 60 can be provided between the guide part 34 and the control part 28.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Wing Frames And Configurations (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Window Of Vehicle (AREA)

Description

Die Erfindung betrifft eine Verlagerungsanordnung zur Verlagerung eines Flügels eines Fensters oder einer Tür quer zur Hauptebene eines festen Rahmens des Fensters oder der Tür gemäß dem Oberbegriff des Patentanspruchs 1. Die Erfindung betrifft weiterhin ein Fenster oder eine Tür mit einer solchen Verlagerungsanordnung.The invention relates to a displacement arrangement for displacing a sash of a window or a door transversely to the main plane of a fixed frame of the window or the door according to the preamble of patent claim 1. The invention further relates to a window or a door with such a displacement arrangement.

Aus der EP 2 829 679 A1 ist eine eingangs genannte Verlagerungsanordnung bekannt geworden, die ein fest an einem Flügel anordenbares Führungsteil und ein am Führungsteil geführtes erstes Steuerteil aufweist. Das erste Steuerteil weist eine geschwungen verlaufende erste Steuerkulisse auf, in der ein erster Steuervorsprung geführt ist, wobei der erste Steuervorsprung fest mit einem Betätigungsmechanismus in Form einer Treibstange verbunden ist.From the EP 2 829 679 A1 a displacement arrangement mentioned at the outset has become known which has a guide part which can be fixedly arranged on a wing and a first control part guided on the guide part. The first control part has a curved first control link in which a first control projection is guided, the first control projection being firmly connected to an actuating mechanism in the form of a drive rod.

Die WO 2007/139354 A1 offenbart einen Betätigungsmechanismus in Form einer Treibstange, an der eine Rollenanordnung montiert ist, wobei die Treibstange in einem Führungsprofil mit U-förmigen Querschnitt aufgenommen ist. Das Führungsprofil weist geschwungen verlaufende Steuerkulissen auf, in denen Steuervorsprünge geführt sind, wobei die Steuervorsprünge fest an Treibstangen montiert sind. Die Steuervorsprünge können Wälzlager aufweisen, um die Reibung zwischen den Steuervorsprüngen und den Steuerkulissen zu verringern.The WO 2007/139354 A1 discloses an actuating mechanism in the form of a drive rod on which a roller arrangement is mounted, the drive rod being received in a guide profile with a U-shaped cross section. The guide profile has curved control slotted links in which control projections are guided, the control projections being firmly mounted on connecting rods. The control projections can have roller bearings in order to reduce the friction between the control projections and the control link.

Aus der WO 2012/093382 A1 ist weiterhin eine Verlagerungsanordnung bekannt geworden, die einen Steuervorsprung aufweist, wobei der Steuervorsprung in einer Steuerkulisse geführt ist. Zur Verringerung der Reibung zwischen Steuervorsprung und Steuerkulisse ist ein Wälzlager am Steuervorsprung angeordnet.From the WO 2012/093382 A1 a displacement arrangement has also become known which has a control projection, the control projection being guided in a control link. To reduce the friction between the control projection and the control link, a roller bearing is arranged on the control projection.

Die DE 10 2014 220 837 B3 offenbart eine Verlagerungsanordnung mit einer Rollenanordnung. Die Rollenanordnung umfasst ein an einem Flügel anordenbares Führungsteil und ein relativ zum Führungsteil verschiebbares erstes Steuerteil mit einer Laufrolle. Zwischen dem ersten Steuerteil und dem Führungsteil sind mehrere Wälzlager vorgesehen.The DE 10 2014 220 837 B3 discloses a displacement assembly having a roller assembly. The roller arrangement comprises a guide part which can be arranged on a wing and a first control part with a roller which can be displaced relative to the guide part. Several roller bearings are provided between the first control part and the guide part.

Aus der CN 105 909 155 A ist eine gattungsgemäße Verlagerungsanordnung zur Verlagerung eines Flügels eines Fensters oder einer Tür quer zur Hauptebene eines festen Rahmens des Fensters oder der Tür bekannt geworden.From the CN 105 909 155 A a generic displacement arrangement for displacing a sash of a window or a door transversely to the main plane of a fixed frame of the window or the door has become known.

Es ist somit bekannt, durch die Anordnung eines Wälzlagers zwischen Steuervorsprung und Steuerkulisse die Reibung bei der Betätigung der Verlagerungsanordnung zu vermindern. Dennoch hat sich gezeigt, dass insbesondere sehr schwere Flügel mit Mehrfachverglasung nur schwer zwangsgesteuert vom festen Rahmen abstellbar sind. Weiterhin lässt sich mit den bekannten Lösungen nur ein begrenzter Anpressdruck bei benutzerfreundlichen Bedienkräften erzeugen.It is thus known to reduce the friction during the actuation of the displacement arrangement by arranging a roller bearing between the control projection and the control link. Nevertheless, it has been shown that, in particular, very heavy sashes with multiple glazing can only be disconnected from the fixed frame with forced control with difficulty. Furthermore, with the known solutions, only a limited contact pressure can be generated with user-friendly operators.

Aufgabe der vorliegenden Erfindung ist es daher, eine Verlagerungsanordnung bereit zu stellen, die eine erleichterte Flügelbewegung durch einen Nutzer ermöglicht. Aufgabe der vorliegenden Erfindung ist es weiterhin, ein Fenster oder eine Tür mit einer solchen Verlagerungsanordnung bereit zu stellen.The object of the present invention is therefore to provide a displacement arrangement which enables a user to make wing movements easier. It is a further object of the present invention to provide a window or a door with such a displacement arrangement.

Diese Aufgabe wird durch eine Verlagerungsanordnung gemäß Patentanspruch 1 bzw. ein Fenster oder eine Tür gemäß Patentanspruch 9 gelöst. Die Unteransprüche geben bevorzugte Weiterbildungen wieder.This object is achieved by a displacement arrangement according to claim 1 or a window or door according to claim 9. The sub-claims reproduce preferred developments.

Die erfindungsgemäße Aufgabe wird somit durch eine Verlagerungsanordnung für einen Flügel eines Fensters oder einer Tür gelöst, wobei der Flügel durch die Bedienung eines Betätigungsmechanismus der Verlagerungsanordnung zwangsgesteuert vom festen Rahmen abstellbar ist. Die Verlagerungsanordnung weist einen ersten Steuervorsprung und eine erste Steuerkulisse auf, wobei der erste Steuervorsprung in die erste Steuerkulisse eingreift. Die erste Steuerkulisse verläuft zumindest abschnittsweise schräg zur Hauptebene des Flügels, wobei sich die Hauptebene des Flügels insbesondere mit der durch den Betätigungsmechanismus aufgespannten Ebene deckt. Eine Verschiebung des ersten Steuervorsprungs mittels des Betätigungsmechanismus bewirkt dabei eine Bewegung eines Steuerteils der Verlagerungsanordnung, sodass ein Abstellen des Flügels vom festen Rahmen erfolgen kann. Die Verlagerungsanordnung weist weiterhin ein Führungsteil auf, das fest am Flügel anordenbar ist. Der erste Steuervorsprung ist teilweise in einer ersten Führungskulisse geführt, die in dem Führungsteil ausgebildet ist. Die erste Führungskulisse verläuft bevorzugt in der Hauptebene des Flügels oder parallel zur Hauptebene des Flügels. Der erste Steuervorsprung weist im Bereich der ersten Führungskulisse ein erstes Wälzlager auf, das sich bei einer Betätigung des Betätigungsmechanismus an der ersten Führungskulisse abstützen kann. Das Steuerteil ist vorzugsweise quer zur Hauptebene des Flügels verlagerbar.The object according to the invention is thus achieved by a displacement arrangement for a sash of a window or a door, the sash being able to be parked in a positively controlled manner from the fixed frame by operating an actuating mechanism of the displacement arrangement. The relocation order has a first control projection and a first control link, the first control projection engaging the first control link. The first control link runs at least in sections at an angle to the main plane of the wing, the main plane of the wing in particular coinciding with the plane spanned by the actuating mechanism. A displacement of the first control projection by means of the actuating mechanism causes a movement of a control part of the displacement arrangement, so that the sash can be set down from the fixed frame. The displacement arrangement also has a guide part which can be fixedly arranged on the wing. The first control projection is partially guided in a first guide slot which is formed in the guide part. The first guide link preferably runs in the main plane of the wing or parallel to the main plane of the wing. The first control projection has a first roller bearing in the area of the first guide slot, which can be supported on the first guide slot when the actuating mechanism is actuated. The control part is preferably displaceable transversely to the main plane of the wing.

Der Erfindung liegt die Erkenntnis zu Grunde, dass die Bedienung des Betätigungsmechanismus maßgeblich erleichtert wird, wenn die Gleitreibung des ersten Steuervorsprungs am Führungsteil eliminiert wird. Diese Gleitreibung wurde bislang vernachlässigt, da davon ausgegangen wurde, dass signifikante Reibungsverluste nur zwischen dem ersten Steuervorsprung und der ersten Steuerkulisse entstehen. Es hat sich jedoch gezeigt, dass insbesondere bei hohen Anpresskräften des Flügels an den festen Rahmen (und dem dadurch erfolgenden Komprimieren einer Dichtung zwischen Flügel und festem Rahmen) die Reibung zwischen dem ersten Steuervorsprung und der ersten Führungskulisse einen großen Teil des Widerstands des Betätigungsmechanismus für einen Nutzer ausmacht. Die Anordnung des ersten Wälzlagers zwischen erstem Steuervorsprung und erster Führungskulisse erleichtert daher die Bedienung der Verlagerungsanordnung signifikant.The invention is based on the knowledge that the operation of the actuating mechanism is significantly facilitated if the sliding friction of the first control projection on the guide part is eliminated. This sliding friction has so far been neglected, since it was assumed that significant friction losses only occur between the first control projection and the first control link. However, it has been shown that, especially with high contact pressure of the sash on the fixed frame (and the resulting compression of a seal between the sash and the fixed frame), the friction between the first control projection and the first guide slot accounts for a large part of the resistance of the actuating mechanism User. The arrangement of the first roller bearing between the first control projection and the first guide slot therefore significantly facilitates the operation of the displacement arrangement.

Das erste Wälzlager kann in Form eines Kugellagers oder Nadellagers ausgebildet sein. Das erste Wälzlager kann einen Außenring aus Metall aufweisen. Alternativ oder zusätzlich dazu kann das erste Wälzlager einen Zusatzkörper, insbesondere in Form eines Zusatzaußenrings, aus Kunststoff aufweisen. In diesem Fall kann der Außenring des ersten Wälzlagers mit Kunststoff umspritzt sein.The first roller bearing can be designed in the form of a ball bearing or needle bearing. The first roller bearing can have an outer ring made of metal. As an alternative or in addition to this, the first roller bearing can have an additional body, in particular in the form of an additional outer ring, made of plastic. In this case, the outer ring of the first roller bearing can be coated with plastic.

Das erste Wälzlager weist in der ersten Führungskulisse vorzugsweise ein Spiel von weniger als 2 mm, insbesondere von weniger als 1 mm, vorzugsweise von weniger als 0,5 mm, weiter bevorzugt von weniger als 0,2 mm, besonders bevorzugt von weniger als 0,1 mm auf.In the first guide slot, the first roller bearing preferably has a play of less than 2 mm, in particular less than 1 mm, preferably less than 0.5 mm, more preferably less than 0.2 mm, particularly preferably less than 0, 1 mm.

Erfindungsgemäß ist der erste Steuervorsprung am Betätigungsmechanismus angeordnet oder ausgebildet und die erste Steuerkulisse am ersten Steuerteil angeordnet oder ausgebildet. Hierdurch wird ein konstruktiv besonders einfacher Aufbau der Verlagerungsanordnung ermöglicht.According to the invention, the first control projection is arranged or formed on the actuating mechanism and the first control link is arranged or formed on the first control part. This enables a particularly simple construction of the displacement arrangement.

Das erste Steuerteil kann am Führungsteil derart geführt sein, dass es nur in eine Richtung relativ zum Führungsteil bewegbar ist. Vorzugsweise ist das Steuerteil ausschließlich senkrecht zur Hauptebene des Flügels relativ zum Führungsteil bewegbar.The first control part can be guided on the guide part in such a way that it can only be moved in one direction relative to the guide part. The control part is preferably movable relative to the guide part exclusively perpendicular to the main plane of the wing.

Das erste Steuerteil kann am Führungsteil drehbar gelagert sein. Vorzugsweise ist dabei die Drehachse parallel zur Hauptebene des Flügels oder in der Hauptebene des Flügels angeordnet.The first control part can be rotatably mounted on the guide part. The axis of rotation is preferably arranged parallel to the main plane of the wing or in the main plane of the wing.

Die Verlagerungsanordnung kann eine mit dem Steuerteil verbundene Rollenanordnung an der unteren Seite der Verlagerungsanordnung und/oder eine Stützanordnung an der oberen Seite der Verlagerungsanordnung aufweisen. Die Stützanordnung kann eine Rolle mit einer Drehachse aufweisen, wobei die Drehachse insbesondere in der Hauptebene des Flügels ausgerichtet ist.The displacement arrangement can have a roller arrangement connected to the control part on the lower side of the displacement arrangement and / or a support arrangement on the upper side of the displacement arrangement. The support arrangement can have a roller with an axis of rotation, the axis of rotation being aligned in particular in the main plane of the wing.

Zusätzlich zu dem ersten Wälzlager kann der erste Steuervorsprung ein zweites Wälzlager im Bereich der ersten Steuerkulisse aufweisen, um die Reibungsverluste zwischen dem ersten Steuervorsprung und der ersten Steuerkulisse zu minimieren. Das zweite Wälzlager kann in Form eines Kugellagers oder Nadellagers ausgebildet sein. Vorzugsweise sind das erste Wälzlager und das zweite Wälzlager gleich ausgebildet.In addition to the first roller bearing, the first control projection can have a second roller bearing in the area of the first control link in order to minimize the friction losses between the first control projection and the first control link. The second roller bearing can be designed in the form of a ball bearing or needle bearing. The first roller bearing and the second roller bearing are preferably of identical design.

Weiter bevorzugt weist die Verlagerungsanordnung ein Stützwälzlager auf, das zwischen dem Führungsteil und dem Steuerteil angeordnet oder ausgebildet ist. Das Stützwälzlager kann in Form eines Kugellagers oder - bevorzugt - in Form eines Rollenlagers mit mehreren Nadelrollen ausgebildet sein.More preferably, the displacement arrangement has a roller support bearing which is arranged or formed between the guide part and the control part. The support roller bearing can be designed in the form of a ball bearing or - preferably - in the form of a roller bearing with several needle rollers.

Die Verlagerungsanordnung kann einen zweiten Steuervorsprung aufweisen, der in eine zweite Steuerkulisse eingreift und in einer zweiten Führungskulisse des Führungsteils geführt ist. Die zweite Steuerkulisse ist zumindest abschnittsweise schräg zur Hauptebene des Flügels ausgebildet. Die zweite Führungskulisse verläuft bevorzugt in der Hauptebene des Flügels oder parallel zur Hauptebene des Flügels.The displacement arrangement can have a second control projection which engages in a second control link and is guided in a second guide link of the guide part. The second control link is formed at least in sections at an angle to the main plane of the wing. The second guide link preferably runs in the main plane of the wing or parallel to the main plane of the wing.

Das erste Wälzlager des zweiten Steuervorsprungs weist in der zweiten Führungskulisse vorzugsweise ein Spiel von weniger als 2 mm, insbesondere von weniger als 1 mm, vorzugsweise von weniger als 0,5 mm, weiter bevorzugt von weniger als 0,2 mm, besonders bevorzugt von weniger als 0,1 mm auf.The first roller bearing of the second control projection preferably has a play of less than 2 mm, in particular less than 1 mm, preferably less than 0.5 mm, more preferably less than 0.2 mm, particularly preferably less, in the second guide slot than 0.1 mm.

Vorzugsweise weist der zweite Steuervorsprung ein erstes Wälzlager zur Abstützung des zweiten Steuervorsprungs an der zweiten Führungskulisse auf. Alternativ oder zusätzlich dazu kann der zweite Steuervorsprung ein zweites Wälzlager zur Abstützung des zweiten Steuervorsprungs an der zweiten Steuerkulisse aufweisen.The second control projection preferably has a first roller bearing for supporting the second control projection on the second guide slot. As an alternative or in addition to this, the second control projection can have a second roller bearing to support the second control projection on the second control link.

Das erste Wälzlager des ersten Steuervorsprungs kann gleich dem ersten Wälzlager des zweiten Steuervorsprungs ausgebildet sein. Das zweite Wälzlager des ersten Steuervorsprungs kann gleich dem zweiten Wälzlager des zweiten Steuervorsprungs ausgebildet sein. Vorzugsweise ist der erste Steuervorsprung gleich dem zweiten Steuervorsprung ausgebildet.The first roller bearing of the first control projection can be designed in the same way as the first roller bearing of the second control projection. The second roller bearing of the first control projection can be designed like the second roller bearing of the second control projection. The first control projection is preferably designed in the same way as the second control projection.

Die erfindungsgemäße Aufgabe wird weiterhin gelöst durch ein Fenster oder eine Tür mit einem festen Rahmen, einem Flügel und einer zuvor beschriebenen Verlagerungsanordnung. Das Führungsteil kann dabei fest am Flügel montiert sein.The object according to the invention is also achieved by a window or a door with a fixed frame, a sash and a displacement arrangement as described above. The guide part can be permanently mounted on the wing.

Der Flügel ist vorzugsweise in Form eines Schiebeflügels ausgebildet, der, insbesondere parallel, vom festen Rahmen abstellbar und parallel zum festen Rahmen verschiebbar ist.The wing is preferably designed in the form of a sliding wing, which can be set down, in particular parallel, from the fixed frame and is displaceable parallel to the fixed frame.

Weitere Merkmale und Vorteile der Erfindung sind in der nachfolgenden detaillierten Beschreibung durch mehrehre Ausführungsbeispiele der Erfindung dargestellt. Die verschiedene Merkmale können in beliebigen Kombination bei Varianten der Erfindung verwirklicht sein, ohne von dem in den beigefügten Ansprüchen definierten Umfang abzuweichen. Die in der Zeichnung gezeigten Merkmale sind derart dargestellt, dass die erfindungsgemäßen Besonderheiten deutlich sichtbar gemacht werden können.Further features and advantages of the invention are illustrated in the following detailed description by way of several exemplary embodiments of the invention. The various features can be realized in any combination in variants of the invention without departing from the scope defined in the appended claims. The features shown in the drawing are shown in such a way that the special features according to the invention can be made clearly visible.

Es zeigen:

Fig. 1
eine isometrische Darstellung einer Verlagerungsanordnung;
Fig. 2
eine teilweise Explosionsansicht des Details II aus Fig. 1;
Fig. 3
eine teilweise Explosionsansicht des Details III aus Fig. 1;
Fig. 4
eine Ansicht von der Verschlussseite auf einen Flügel mit einer Verschlussanordnung, wobei der Flügel beabstandet zu einem festen Rahmen angeordnet ist;
Fig. 5
eine der Fig. 4 entsprechende Darstellung, wobei der Flügel gegenüber der Darstellung der Fig. 4 quer zur Hauptebene des festen Rahmens verlagert wurde;
Fig. 6
eine weitere teilweise Explosionsdarstellung des Details II aus Fig. 1;
Fig. 7
eine isometrische Ansicht einer weiteren Ausführungsform einer Verlagerungsanordnung;
Fig. 8
eine Schnittansicht im Bereich VIII gemäß Fig. 7 bei montierter Verlagerungsanordnung; und
Fig. 9
eine Schnittansicht im Bereich IX gemäß Fig. 7 bei montierter Verlagerungsanordnung.
Show it:
Fig. 1
an isometric view of a displacement assembly;
Fig. 2
a partially exploded view of the detail II Fig. 1 ;
Fig. 3
a partially exploded view of the detail III Fig. 1 ;
Fig. 4
a view from the closure side of a wing with a closure arrangement, wherein the wing is spaced apart from a fixed frame;
Fig. 5
one of the Fig. 4 corresponding representation, the wing compared to the representation of the Fig. 4 was relocated transversely to the main plane of the fixed frame;
Fig. 6
another partially exploded view of detail II Fig. 1 ;
Fig. 7
an isometric view of another embodiment of a displacement assembly;
Fig. 8
a sectional view in area VIII according to Fig. 7 with assembled displacement arrangement; and
Fig. 9
a sectional view in the area IX according to Fig. 7 with mounted displacement arrangement.

Fig. 1 zeigt eine Verlagerungsanordnung 10 mit einem als umlaufender Treibstangenbeschlag ausgebildeten Betätigungsmechanismus 12, der über einen Betätigungsgriff 14 bedient werden kann. Der Betätigungsmechanismus 12 wird an einem/einer in den Fign. 4 und 5 dargestellten Fenster oder Tür montiert und erstreckt sich entlang der Falzumfangsrichtung 16. Die Falzumfangsrichtung 16 erstreckt sich in der Hauptebene 18 (in Fig. 1 lediglich angedeutet) des Fensters oder der Tür. Im gezeigten Ausführungsbeispiel weist die Verlagerungsanordnung 10 zwei Stellen a, b mit einer Rollenanordnung 20a, 20b und zwei Stellen c, d mit einer Stützanordnung 22a, 22b auf, wobei die Rollenanordnungen 20a, 20b und die Stützanordnungen 22a, 22b jeweils quer zur Falzumfangsrichtung 16 verlagerbar sind. Fig. 1 shows a displacement arrangement 10 with an actuating mechanism 12 designed as a circumferential drive rod fitting which can be operated via an actuating handle 14. The actuation mechanism 12 is on a / a in the Figs. 4 and 5 window or door shown and extends along the fold circumferential direction 16. The fold circumferential direction 16 extends in the main plane 18 (in Fig. 1 only indicated) of the window or door. In the exemplary embodiment shown, the displacement arrangement 10 has two points a, b with a roller arrangement 20a, 20b and two points c, d with a support arrangement 22a, 22b, the Roller arrangements 20a, 20b and the support arrangements 22a, 22b can each be displaced transversely to the circumferential direction 16 of the fold.

Fig. 2 zeigt einen Teil der Bauteile des Ausschnitts II gemäß Fig. 1. Zu erkennen ist, dass der Betätigungsmechanismus 12 einen bolzenförmigen ersten Steuervorsprung 24a aufweist, welcher in eine erste Steuerkulisse 26a eingreift, die in Form eines ersten Steuerschlitzes ausgebildet ist. Die erste Steuerkulisse 26a ist dabei zumindest abschnittsweise schräg zur Falzumfangsrichtung 16 ausgebildet. Bei einer Verlagerung des Betätigungsmechanismus 12 in Falzumfangsrichtung 16 wird dadurch die Rollenanordnung 20a senkrecht zur Falzumfangsrichtung 16 verlagert. Die erste Steuerkulisse 26a ist in einem Steuerteil 28 ausgebildet. Fig. 2 shows part of the components of section II according to FIG Fig. 1 . It can be seen that the actuation mechanism 12 has a bolt-shaped first control projection 24a which engages in a first control link 26a which is designed in the form of a first control slot. The first control link 26a is formed at least in sections at an angle to the circumferential direction 16 of the fold. When the actuating mechanism 12 is displaced in the fold circumferential direction 16, the roller arrangement 20a is displaced perpendicular to the fold circumferential direction 16. The first control link 26a is formed in a control part 28.

Die Rollenanordnung 20a weist zumindest eine Laufrolle 30a, 30b auf. Zusätzlich dazu weist die Rollenanordnung 20a im vorliegenden Fall eine Stützrolle 32 auf. Die Stützrolle 32 weist einen Außendurchmesser auf, der größer ist als die Breite der übrigen Rollenanordnung 20a. Hierdurch können durch die Abstützung der Stützrolle 32 Querkräfte auf die Rollenanordnung 20a vermieden werden.The roller arrangement 20a has at least one roller 30a, 30b. In addition, the roller arrangement 20a has a support roller 32 in the present case. The support roller 32 has an outer diameter which is greater than the width of the rest of the roller arrangement 20a. In this way, by supporting the support roller 32, transverse forces on the roller arrangement 20a can be avoided.

Fig. 3 zeigt eine Darstellung des Details III gemäß Fig. 1. Die Stützanordnung 22a weist ebenfalls eine Stützrolle 32 auf, die um eine vertikale Drehachse angeordnet ist. Analog zu dem Aufbau gemäß Fig. 2 weist die Verlagerungsanordnung 10 im Bereich des Details III ein Steuerteil 28 mit einer ersten Steuerkulisse (nicht sichtbar) auf, in die ein erster Steuervorsprung 24a eingreift. Weiterhin weist die Verlagerungsanordnung 10 ein Führungsteil 34 auf, das in der Verlagerungsanordnung 10 gemäß Fig. 2 nicht dargestellt ist. Das Führungsteil 34 ist unbeweglich am Flügel 40 (siehe Fign. 4, 5) montiert. Der erste Steuervorsprung 24a ist zur Verringerung der Reibung bei der Bedienung des Betätigungsmechanismus 12 in Falzumfangsrichtung 16 an einer nicht gezeigten ersten Führungskulisse im Führungsteil 28 gelagert. Der erste Steuervorsprung 24a durchgreift das Führungsteil 34 und greift in das Steuerteil 28 ein. Fig. 3 shows a representation of the detail III according to Fig. 1 . The support arrangement 22a also has a support roller 32 which is arranged around a vertical axis of rotation. Analogous to the structure according to Fig. 2 If the displacement arrangement 10 has a control part 28 with a first control link (not visible) in the area of detail III, into which a first control projection 24a engages. Furthermore, the displacement arrangement 10 has a guide part 34, which in the displacement arrangement 10 according to FIG Fig. 2 is not shown. The guide part 34 is immovable on the wing 40 (see Figs. 4, 5 ) assembled. To reduce the friction when operating the actuating mechanism 12, the first control projection 24a is mounted in the circumferential direction 16 of the fold on a first guide slot (not shown) in the guide part 28. The first Control projection 24a passes through guide part 34 and engages control part 28.

Fig. 4 zeigt eine Ansicht von der Verschlussseite auf ein Fenster oder eine Tür 36 mit einem festen Rahmen 38 und einem Flügel 40. Der Betätigungsmechanismus 12 ist an den Flügel 40 montiert. Dieser stützt sich über die Rollenanordnung 20a an einer Laufschiene 42 ab. Zwischen dem Flügel 40 und dem festen Rahmen 38 ist ein Spalt 44. Der Flügel 40 liegt demnach nicht an einer umlaufenden Dichtung 46 des festen Rahmens 38 an. Fig. 4 FIG. 11 shows a view from the locking side of a window or door 36 with a fixed frame 38 and a leaf 40. The actuating mechanism 12 is mounted on the leaf 40. This is supported on a running rail 42 via the roller arrangement 20a. There is a gap 44 between the wing 40 and the fixed frame 38. The wing 40 accordingly does not lie against a circumferential seal 46 of the fixed frame 38.

Die Stützrolle 32 liegt an einer als vertikaler Steg ausgebildeten Führung 48 des festen Rahmens 38 an. In der gezeigten Stellung kann der Flügel 40 bezüglich des festen Rahmens 38 verschoben werden, wobei sich die Stützrolle 32 an der Führung 48 abstützen bzw. sich an dieser abrollen kann.The support roller 32 rests on a guide 48 of the fixed frame 38, which guide is designed as a vertical web. In the position shown, the wing 40 can be displaced with respect to the fixed frame 38, the support roller 32 being supported on the guide 48 or being able to roll on it.

Im oberen Bereich des Fensters oder der Tür 36 weist der feste Rahmen 38 ebenfalls eine Führung 48 auf, die hier nutartig ausgebildet ist. In der Führung 48 ist die Stützrolle 32 (siehe auch Fig. 3) geführt.In the upper area of the window or door 36, the fixed frame 38 also has a guide 48, which here is designed like a groove. In the guide 48 is the support roller 32 (see also Fig. 3 ) guided.

Fig. 5 zeigt das Fenster oder die Tür 36 nach dem Bedienen des Betätigungsmechanismus 12. Durch die Betätigung des Betätigungsmechanismus 12 werden die Rollenanordnungen (in Fig. 5 ist die Rollenanordnung 20a sichtbar) und die Stützanordnungen (in Fig. 5 ist die Stützanordnung 22a sichtbar) verlagert. Dies bedeutet, dass sich der Flügel 40 dem festen Rahmen 38 annähert, sodass die Dichtung 46 zwischen dem Flügel 40 und dem festen Rahmen 38 eingeklemmt und komprimiert wird. Fig. 5 12 shows the window or door 36 after the actuation mechanism 12 has been operated. By actuating the actuation mechanism 12, the roller assemblies (in Fig. 5 the roller assembly 20a is visible) and the support assemblies (in Fig. 5 the support arrangement 22a is visible) displaced. This means that the wing 40 approaches the fixed frame 38 so that the seal 46 is pinched and compressed between the wing 40 and the fixed frame 38.

Fig. 6 zeigt eine weitere Detailansicht der Verlagerungsanordnung 10 gemäß Detail II der Fig. 1. Aus Fig. 6 ist ersichtlich, dass der erste Steuervorsprung 24a eine zylindrische Form aufweist und an dem Betätigungsmechanismus 12 angeordnet ist. Der erste Steuervorsprung 24a weist ein erstes Wälzlager 50 und ein zweites Wälzlager 52 auf. Das erste Wälzlager 50 dient der reibungsarmen Führung des ersten Steuervorsprungs 24a in einer ersten Führungskulisse 54a des Führungsteils 34. Das zweite Wälzlager 52 dient der reibungsarmen Führung des ersten Steuervorsprungs 24a in der ersten Steuerkulisse 26a des Steuerteils 28. Fig. 6 shows a further detailed view of the displacement arrangement 10 according to detail II of FIG Fig. 1 . Out Fig. 6 it can be seen that the first control projection 24a has a cylindrical shape and is arranged on the actuating mechanism 12. The first control projection 24a has a first roller bearing 50 and a second roller bearing 52. The first roller bearing 50 serves to guide the first control projection 24a with little friction in a first guide slot 54a of the guide part 34. The second roller bearing 52 serves to guide the first control projection 24a with little friction in the first control slot 26a of the control part 28.

Die erste Führungskulisse 54a ist in Richtung der Falzumfangsrichtung 16 oder parallel zur Falzumfangsrichtung 16 ausgebildet, wohingegen die erste Steuerkulisse 26a zumindest teilweise quer zur Falzumfangsrichtung 16 ausgebildet ist. Am Steuerteil 28 ist die Rollenanordnung 20a angeordnet. Die Verlagerungsanordnung 10 ist im Bereich des Details III (siehe Fig. 3) hierzu analog ausgebildet, wobei das Steuerteil 28 statt der Rollenanordnung 20a die Stützanordnung 22a (siehe Fig. 3) aufweist.The first guide slot 54a is formed in the direction of the circumferential fold direction 16 or parallel to the circumferential fold direction 16, whereas the first control slot 26a is formed at least partially transversely to the circumferential fold direction 16. The roller arrangement 20a is arranged on the control part 28. The displacement arrangement 10 is in the area of detail III (see Fig. 3 ) designed analogously to this, the control part 28 instead of the roller arrangement 20a the support arrangement 22a (see Fig. 3 ) having.

Das Führungsteil 34 ist fest, d.h. starr und unbeweglich, am Flügel 40 (siehe Fign. 4, 5) anordenbar, hier anschraubbar. Wie aus Fig. 6 ersichtlich ist, ist zwischen dem Führungsteil 34 und dem Steuerteil 28 eine Führung 56 vorgesehen, die ausschließlich eine begrenzte Bewegung des Steuerteils 28 relativ zum Führungsteil 34 quer zur Falzumfangsrichtung 16 erlaubt. Im vorliegenden Ausführungsbeispiel ist die Führung 56 in Form einer Schwalbenschwanzführung ausgebildet.The guide part 34 is fixed, ie rigid and immobile, on the wing 40 (see Figs. 4, 5 ) can be arranged, screwed on here. How out Fig. 6 As can be seen, a guide 56 is provided between the guide part 34 and the control part 28, which only allows a limited movement of the control part 28 relative to the guide part 34 transversely to the fold circumferential direction 16. In the present exemplary embodiment, the guide 56 is designed in the form of a dovetail guide.

Fig. 7 zeigt ein weiteres Beispiel einer Verlagerungsanordnung 10. Die Verlagerungsanordnung 10 weist einen ersten Steuervorsprung 24a und einen zweiten Steuervorsprung 24b auf. Die Steuervorsprünge 24a, 24b sind gleich ausgebildet. Weiterhin sind beide Steuervorsprünge 24a, 24b gleich dem ersten Steuervorsprung 24a gemäß Fig. 6 ausgebildet. Beide Steuervorsprünge 24a, 24b sind an dem Betätigungsmechanismus 12 angeordnet. Fig. 7 shows a further example of a displacement arrangement 10. The displacement arrangement 10 has a first control projection 24a and a second control projection 24b. The control projections 24a, 24b are identical. Furthermore, both control projections 24a, 24b are identical to the first control projection 24a according to FIG Fig. 6 educated. Both control projections 24a, 24b are arranged on the actuation mechanism 12.

Der erste Steuervorsprung 24a ist in einer, hier einseitig offenen, ersten Führungskulisse 54a geführt. Der zweite Steuervorsprung 24b ist in einer, hier ebenfalls offenen, zweiten Führungskulisse 54b geführt. Weiterhin greift der erste Steuervorsprung 24a in eine erste Steuerkulisse 26a und der zweite Steuervorsprung 24b in eine zweite Steuerkulisse 26b ein. Beim Betätigen der Verlagerungsanordnung 10 tritt der erste Steuervorsprung 24a aus den ihm zugeordneten Kulissen 26a, 54a aus. Kurz vor diesem Austreten tritt der zweite Steuervorsprung 24b in die ihm zugeordneten Kulissen 26b, 54b ein, sodass eine kontinuierliche Führung des Steuerteils 28 (siehe Fign. 8, 9) gegeben ist. Die hier beschriebene Ausführungsform ist analog in DE 10 2014 220 837 B3 beschrieben, auf deren Inhalt vollumfänglich Bezug genommen wird.The first control projection 24a is guided in a first guide slot 54a, here open on one side. The second control projection 24b is in one, here also open, second guide slot 54b out. Furthermore, the first control projection 24a engages in a first control link 26a and the second control projection 24b in a second control link 26b. When the displacement arrangement 10 is actuated, the first control projection 24a emerges from the connecting links 26a, 54a assigned to it. Shortly before this exit, the second control projection 24b enters into the connecting links 26b, 54b assigned to it, so that continuous guidance of the control part 28 (see FIG Figs. 8, 9 ) given is. The embodiment described here is analogous to FIG DE 10 2014 220 837 B3 , the content of which is fully referred to.

Fig. 8 zeigt einen Querschnitt der Verlagerungsanordnung 10 im Bereich VIII (siehe Fig. 7). Aus Fig. 8 ist die Führung des ersten Wälzlagers 50 am ersten Führungsteil 34 sowie die Führung des zweiten Wälzlagers 52 am Steuerteil 28 ersichtlich. Das horizontale Spiel des ersten Steuervorsprungs 24a im Führungsteil 34 und im Steuerteil 28, das sich aus den Abständen A und B (in Fig. 8 zur Verdeutlichung vergrößert angedeutet) zusammensetzt, beträgt weniger als 0,5 mm. Idealerweise tendiert das Spiel gegen null. Die Innenringe der Wälzlager 50, 52 sind durch einen Distanzring 58 beabstandet. Fig. 8 shows a cross section of the displacement arrangement 10 in area VIII (see Fig. 7 ). Out Fig. 8 the guidance of the first roller bearing 50 on the first guide part 34 and the guidance of the second roller bearing 52 on the control part 28 can be seen. The horizontal play of the first control projection 24a in the guide part 34 and in the control part 28, which is made up of the distances A and B (in Fig. 8 indicated enlarged for clarity) is less than 0.5 mm. Ideally, the game tends towards zero. The inner rings of the roller bearings 50, 52 are spaced apart by a spacer ring 58.

Fig. 9 zeigt einen Querschnitt der Verlagerungsanordnung 10 im Bereich IX (siehe Fig. 7). Aus Fig. 9 ist ersichtlich, dass zwischen dem Steuerteil 28 und dem Führungsteil 34 ein Stützwälzlager 60 angeordnet ist. Hierdurch können auch sehr schwere Flügel 40 (siehe Fign. 4, 5) reibungsarm verschiebbar abgestützt werden. Fig. 9 shows a cross section of the displacement arrangement 10 in the area IX (see Fig. 7 ). Out Fig. 9 it can be seen that a support roller bearing 60 is arranged between the control part 28 and the guide part 34. This means that very heavy wings 40 (see Figs. 4, 5 ) be supported with low friction.

Unter Vornahme einer Zusammenschau aller Figuren der Zeichnung betrifft die Erfindung zusammenfassend eine Verlagerungsanordnung 10 zum Bewegen eines Flügels 40 eines Fensters bzw. einer Tür 36 quer zum festen Rahmen 38 des Fensters bzw. der Tür 36. Die Verlagerungsanordnung 10 weist zum mittelbaren Abstützen der Querbewegung ein Steuerteil 28 auf, das mittels einer Betätigungseinrichtung 12 relativ zu einem fest am Flügel 40 montierbaren Führungsteil 34 verschoben wird. Zwischen Steuerteil 28 und Betätigungseinrichtung 12 ist hierbei ein erster Steuervorsprung 24a vorgesehen, der in eine erste Steuerkulisse 26a des Steuerteils 28 und gleichzeitig in eine erste Führungskulisse 54a des Führungsteils 34 eingreift. Der erste Steuervorsprung 24a weist ein erstes Wälzlager 50 zur Anlage an der ersten Führungskulisse 54a auf. Zusätzlich dazu kann der erste Steuervorsprung 24a ein zweites Wälzlager 52 zur Abstützung an der ersten Steuerkulisse 26a aufweisen. Alternativ oder zusätzlich dazu kann ein Stützwälzlager 60 zwischen dem Führungsteil 34 und dem Steuerteil 28 vorgesehen sein. Die Verlagerungsanordnung 10 ermöglicht das Erzeugen eines hohen Anpressdrucks des Flügels 40 an den festen Rahmen 38 bei moderaten Bedienkräften und damit eine gute Abdichtung des Fensters bzw. der Tür 36. Weiterhin ist ein sehr reibungsarmes Abstellen selbst schwerer Flügel 40 mittels der Bedienung der Betätigungseinrichtung 12 durch einen Nutzer des Fensters bzw. der Tür 36 möglich.Taking all the figures of the drawing together, the invention relates in summary to a displacement arrangement 10 for moving a sash 40 of a window or a door 36 transversely to the fixed frame 38 of the window or door 36. The displacement arrangement 10 has a means of indirectly supporting the transverse movement Control part 28, which by means of a Actuating device 12 is moved relative to a guide part 34 which can be fixedly mounted on the wing 40. Between the control part 28 and the actuating device 12, a first control projection 24a is provided, which engages in a first control link 26a of the control part 28 and at the same time in a first guide link 54a of the guide part 34. The first control projection 24a has a first roller bearing 50 for bearing on the first guide slot 54a. In addition to this, the first control projection 24a can have a second roller bearing 52 for support on the first control link 26a. Alternatively or in addition to this, a roller support bearing 60 can be provided between the guide part 34 and the control part 28. The displacement arrangement 10 enables a high contact pressure of the sash 40 to be generated against the fixed frame 38 with moderate operating forces and thus a good sealing of the window or door 36. Furthermore, even heavy sashes 40 can be put down with very little friction by operating the actuating device 12 a user of the window or the door 36 is possible.

Claims (10)

  1. Displacement arrangement (10) for displacing a sash/leaf (40) of a window or a door (36) transversely to the main plane of a fixed frame (38) of the window or door (36), the displacement arrangement (10) comprising the following:
    a) an actuating mechanism (12) which can be arranged on the sash/leaf (40) and can be moved in the fold circumferential direction (16) at least in portions;
    b) a first control projection (24a);
    c) a control part (28);
    d) a first control slot (26a), the first control projection (24a) being received in the first control slot (26a) in portions and the first control slot (26a) being inclined with respect to the main plane (18) of the sash/leaf (40) at least in portions, so that a displacement of the first control projection (24a) by the actuating mechanism (12) causes a displacement of the first control part (28);
    e) a guide part (34) which can be mounted immovably on the sash/leaf (40) and has a first guide slot (54a) in which the first control projection (24a) is received in portions;
    the control part (28) being movable relative to the guide part (34) in order to cause the displacement of the sash/leaf (40) relative to the fixed frame (38);
    the first control projection (24a) being arranged or formed on the actuating mechanism (12) and the first control slot (26a) being arranged or formed on the first control part (28);
    characterized in that the first control projection (24a) has a first roller bearing (50) for low-friction guidance of the first control projection (24a) in the first guide slot (54a).
  2. Displacement arrangement according to claim 1, wherein the first control part (28) is guided on the guide part (34), the first control part (28) being guided transversely with respect to the main plane (18) of the sash/leaf (40), in particular perpendicularly with respect to the main plane (18) of the sash/leaf (40).
  3. Displacement arrangement according to claim 1, wherein the first control part (28) is rotatably mounted on the guide part (34), the axis of rotation being arranged parallel to the main plane (18) of the sash/leaf (40).
  4. Displacement arrangement according to any of the preceding claims, wherein the displacement arrangement (10) has a roller arrangement (20a, 20b) arranged or formed on the control part (28) and/or a support arrangement (22a, 22b) for supporting on the fixed frame (38).
  5. Displacement arrangement according to any of the preceding claims, wherein the first control projection (24a) has a second roller bearing (52) for low-friction guidance of the first control projection (24a) in the first control slot (26a).
  6. Displacement arrangement according to any of the preceding claims, wherein the displacement arrangement (10) has a supporting roller bearing (60) between the guide part (34) and the first control part (28).
  7. Displacement arrangement according to any of the preceding claims, wherein the displacement arrangement for actuating the control part (28) comprises a second control projection (24b) and a second control slot (26b), the second control projection (24b) being received in the second control slot (26b) in portions and the guide part (34) having a second guide slot (54b) in which the second control projection (24b) is received in portions.
  8. Displacement arrangement according to claim 7, wherein the second control projection (24b) is designed alike the first control projection (24a).
  9. Window or door (36) comprising a fixed frame (38), a sash/leaf (40) and a displacement arrangement (10) according to any of the preceding claims for guiding the sash/leaf (40) relative to the fixed frame (38).
  10. Window or door according to claim 9, wherein the sash/leaf (40) is designed in the form of a sliding sash/leaf which can be set aside of the fixed frame (38) and displaced parallel to the fixed frame (38).
EP17811288.4A 2016-12-19 2017-12-06 Displacement arrangement having a rolling bearing guide Active EP3555397B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL17811288T PL3555397T3 (en) 2016-12-19 2017-12-06 Displacement arrangement having a rolling bearing guide

Applications Claiming Priority (2)

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DE102016225385.9A DE102016225385A1 (en) 2016-12-19 2016-12-19 Displacement arrangement with roller bearing guide
PCT/EP2017/081694 WO2018114337A1 (en) 2016-12-19 2017-12-06 Displacement arrangement having a rolling bearing guide

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EP3555397A1 EP3555397A1 (en) 2019-10-23
EP3555397B1 true EP3555397B1 (en) 2020-11-04

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US (1) US11085216B2 (en)
EP (1) EP3555397B1 (en)
KR (1) KR102373281B1 (en)
CN (1) CN110088420B (en)
CA (1) CA3063624C (en)
DE (1) DE102016225385A1 (en)
PL (1) PL3555397T3 (en)
WO (1) WO2018114337A1 (en)

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WO2022179815A1 (en) 2021-02-26 2022-09-01 Roto Frank Fenster- und Türtechnologie GmbH Simple control pin fastening

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WO2022179815A1 (en) 2021-02-26 2022-09-01 Roto Frank Fenster- und Türtechnologie GmbH Simple control pin fastening
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Publication number Publication date
KR20190098182A (en) 2019-08-21
CN110088420B (en) 2021-07-20
KR102373281B1 (en) 2022-03-10
PL3555397T3 (en) 2021-05-17
US11085216B2 (en) 2021-08-10
EP3555397A1 (en) 2019-10-23
US20190345749A1 (en) 2019-11-14
CA3063624C (en) 2023-11-21
DE102016225385A1 (en) 2018-06-21
CA3063624A1 (en) 2019-12-06
CN110088420A (en) 2019-08-02
WO2018114337A1 (en) 2018-06-28

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