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EP3045638A1 - Sliding and rotating leaf system - Google Patents

Sliding and rotating leaf system Download PDF

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Publication number
EP3045638A1
EP3045638A1 EP15151501.2A EP15151501A EP3045638A1 EP 3045638 A1 EP3045638 A1 EP 3045638A1 EP 15151501 A EP15151501 A EP 15151501A EP 3045638 A1 EP3045638 A1 EP 3045638A1
Authority
EP
European Patent Office
Prior art keywords
wing
carriage
rail profile
sliding
bottom rail
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.)
Granted
Application number
EP15151501.2A
Other languages
German (de)
French (fr)
Other versions
EP3045638B1 (en
Inventor
Malte Schneider
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.)
Sunflex Aluminiumsysteme GmbH
Original Assignee
Sunflex Aluminiumsysteme 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 Sunflex Aluminiumsysteme GmbH filed Critical Sunflex Aluminiumsysteme GmbH
Priority to ES15151501.2T priority Critical patent/ES2617138T3/en
Priority to EP15151501.2A priority patent/EP3045638B1/en
Priority to PCT/EP2016/050387 priority patent/WO2016113224A1/en
Priority to US15/127,593 priority patent/US10119315B2/en
Publication of EP3045638A1 publication Critical patent/EP3045638A1/en
Priority to ZA2016/05984A priority patent/ZA201605984B/en
Priority to CL2016002687A priority patent/CL2016002687A1/en
Application granted granted Critical
Publication of EP3045638B1 publication Critical patent/EP3045638B1/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
    • E05D15/56Suspension arrangements for wings with successive different movements
    • E05D15/58Suspension arrangements for wings with successive different movements with both swinging and sliding movements
    • 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
    • E05Y2201/606Accessories therefor
    • E05Y2201/61Cooperation between suspension or transmission members
    • E05Y2201/612Cooperation between suspension or transmission members between carriers and rails
    • E05Y2201/614Anti-derailing means
    • 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
    • E05Y2201/638Cams; Ramps
    • 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
    • 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
    • E05Y2900/15Balcony glazing

Definitions

  • the invention relates to a sliding and rotary wing system according to the preamble of patent claim 1.
  • Such sliding and rotary wing systems are well known. They have a plurality of sliding window sash, which are individually pivotable, which can almost completely open a mostly very large front or space division.
  • the individual wings are slidably guided between arranged on the ceiling and the floor rail profiles. Each wing is guided via two support elements displaceable in a ceiling rail profile.
  • the ceiling rail profile has an outlet opening for notching a support element of a wing.
  • a Sp Dr Drklammer is arranged end in the ceiling rail profile, in which a arranged on the respective wing locking element is introduced.
  • the blocking element For pivoting a wing, the blocking element is retracted into the locking cam element and the bearing element located at the other end of the wing is disengaged from the outlet opening and pivoted about the axis extending through the blocking element.
  • the blocking element rotates in a guide of the locking cam element, so that the wing is securely held.
  • the invention aims to remedy this situation.
  • the invention is based on the object to provide a sliding and rotary vane system of the aforementioned type, which allows installation even in the case of limited viable ceilings. According to the invention, this object is solved by the features of the characterizing part of patent claim 1.
  • a sliding sash system of the aforementioned type is created, in which an installation is made possible even with limited load-bearing ceilings.
  • the at least two wings are each mounted on at least one carriage in the floor rail profile, such that in the pivoted state of the wing, i. in flight with floor and ceiling rail profile, a complete recording of the weight load of the wing through the floor rail profile, the ceiling rail profile is only the leadership of arranged between the floor rail profile and ceiling rail profile wings;
  • the tensile load of the ceiling rail profile is significantly reduced or even eliminated.
  • the at least one lateral outlet opening enables a swinging out and pivoting of a wing.
  • the wing with the arranged lever runner is lifted when passing the ramp element.
  • the rollers are relieved.
  • the parking position i. the swing-out position of the wing are the rollers without contact with the bottom rail and can be moved out with the wing from the outlet opening.
  • a locking cam member for receiving a arranged on each wing locking element is arranged horizontally spaced from the locking cam member in the bottom rail profile at least one outlet opening for notching a wing is arranged.
  • a locking cam element may also be provided in the bottom profile, in which case a corresponding blocking element is preferably required on the carriage.
  • the wings are provided on their side facing the ceiling rail profile top with at least one guide cylinder which projects into the gap of the C-shaped ceiling rail profile.
  • the wing is guided over the guide cylinder in the gap of the ceiling rail profile without a support load acting on the ceiling rail profile.
  • the locking element is mounted on the guide cylinder, in particular integrally formed on this or screwed onto this.
  • the lever traveler is arranged on the carriage. As a result, a compact design is achieved.
  • At least one outlet opening is framed by a guide frame on which the ramp element is formed.
  • the ramp element is designed to be moved out of the travel path of the lever traveler. As a result, a method of a wing without raising in the case is made possible that this is not to be pivoted.
  • a hold-down is arranged on at least one wing.
  • the hold-down is arranged on the carriage, in particular below an impeller of the carriage, such that the gap of the bottom rail between the impeller and hold-down runs.
  • the hold-down device interacts with the bottom rail in such a way that a linear guide of the associated wing is effected. As a result, a guided movement of the wing along the bottom rail is achieved.
  • the carriage comprises a carriage housing with a wing receptacle and a hollow cylindrical bearing receptacle integrally formed thereon, in which bearing receptacle a bearing for rotatably supporting an axle is arranged, which receives at least one impeller, wherein on the bearing receptacle of the wing receptacle opposite a hold-down is formed.
  • the lever rotor is preferably formed at a distance from the bearing receptacle on the carriage housing.
  • the sliding and rotary sash system selected as an exemplary embodiment consists essentially of a floor rail profile 1, a ceiling rail profile 2 and a number of wings 3, which are displaceably guided in the floor rail profile 1 via carriages 4, 5. On the ceiling side, the wings 3 are guided over a guide cylinder 35 in the ceiling rail profile 2.
  • the floor rail profile 1 is formed from a base profile 11 and a supporting profile 12 attached thereto, which is fixed in height adjustable in the base profile 11.
  • the support profile 12 is formed substantially in the manner of a C-profile and has a gap 13 on its upper side facing away from the base profile 11.
  • a first web 14 is integrally formed on a longitudinal side wall and a second web 15 is offset vertically on the opposite longitudinal side wall to the first web 14.
  • an outlet opening 16 is introduced in the floor rail profile 1 in a longitudinal side wall.
  • the outlet opening 16 of the floor rail profile 1 is framed by a guide frame 6, on whose the wings 3 facing top a support surface 61 is formed.
  • a ramp element 62 is formed, which is provided on both sides with a slope 63.
  • the guide frame 6 is made with integrally formed ramp element 62 as plastic.
  • the ceiling rail profile 2 is formed substantially in the manner of a C-profile and has a gap 21 on its upper side opposite the bottom rail profile 1. Laterally, an outlet opening 23 for notching a guide cylinder 35 of a wing 3 is inserted in the ceiling rail profile 2. (If only one guide cylinder 35 is arranged on the wing 3, the ceiling rail profile has no outlet opening 23.) At the end, a latching cam element 22 is arranged in the ceiling rail profile 2.
  • the locking cam member 22 is formed in the form of a pliers-shaped plastic part, in whose oppositely arranged arms strung together arcuate formations are introduced, which is approximately centrally provided with a transverse to the ceiling profile 2 groove for receiving the locking element 36 of a wing 3.
  • the inner contour of the circular arc-shaped formations substantially corresponds to the outer contour of the guide cylinder 35 of the wings 3.
  • the wings 3 are each formed from a disc element 31, which is bordered by a frame profile 32.
  • the frame profiles 32 are each provided with a C-profile-like receptacle 33 for receiving the grooved plate 42, 51 of a carriage 4, 5 or the grooved plate 351 of a guide cylinder 35.
  • each wing 3 is provided on its side facing the ceiling rail profile 2 with two guide cylinders 35 and on its bottom rail profile 1 side facing two carriages 4, 5, which in each case via their grooves plates 351, 42, 51 in the C-profile-like receptacle 33rd the frame profile 32 are attached.
  • Each of the locking cam member 22 facing guide cylinder 35 of each wing 3 is at its the frame profile 32 opposite top provided with a blocking element 36 which is formed substantially in the manner of a rectangular plate with arcuate narrow sides.
  • a blocking element 36 which is formed substantially in the manner of a rectangular plate with arcuate narrow sides.
  • At its bottom rail profile 1 facing underside of the wings 3 are further provided on both sides with brush 37.
  • the first carriage 4 comprises a carriage housing 41, on which a groove plate 42 is formed.
  • the groove plate 42 serves as a receptacle for a wing 3, in the frame profile 32, the groove plate 42 can be fastened.
  • a substantially hollow cylindrical bearing receptacle 43 is arranged in the carriage housing 41, which receives a rolling bearing 44.
  • the roller bearing 44 receives an axle 45, at both ends of which an impeller 46 is attached.
  • the bearing receptacle 43 is adjoined by a cylindrical web 47, which merges into an abutment 48 protruding on all sides.
  • a lever 49 Spaced to the bearing receptacle 43 a lever 49 is arranged on the carriage body further.
  • the lever 49 is formed like a stamp. Its free end is positioned slightly higher than the running surfaces of the wheels 46.
  • the second carriage 5 is positioned at its end opposite the first carriage 4 end of the frame profile 32 of a wing 3. It has a groove plate 41 on which a support arm 52 is formed orthogonal to this.
  • the support arm 52 is followed by a substantially rectangular plate 53, which merges into an axle 54 for receiving two rollers 55 arranged parallel to one another.
  • the wings 3 are arranged between the floor rail profile 1 and ceiling rail profile 2 that the support arm 52 of each second carriage 5 protrude through the gap 13 of the bottom rail profile 1, wherein the plate 53 respectively facing roller 55 of the respective carriage 5 on the second web 15 and the second roller 55 rest on the first web 14 of the floor rail profile 1.
  • the wheels 46 of each first carriage are on top of the support section 12 of the soil profile 1.
  • the web 47 also protrudes through the gap 13 of the floor rail profile 1, wherein the hold-48 abuts the inside of both sides of the gap 13 on the support section 12.
  • the guide cylinder 35 project through the gap 21 into the ceiling rail profile 2.
  • the wing 3 For pivoting a blade 3 of the sliding and rotary wing system, the wing 3 is first moved along the bottom rail profile 1 until the locking element 36 engages in the most distant free forming the locking cam member 22.
  • the lever 49 of the runner 4 arranged at the opposite end of the wing 3 is moved over the slope 63 of an outlet opening 16 associated ramp element 62, whereby the wheels 46 of this carriage 4 are raised relative to the support section 12 vertically.
  • the carriage 4 In this position, the carriage 4 is located at the outlet opening 16 of the profile 1; the outer guide cylinder 35 is located at the outlet opening 23 of the ceiling rail profile 2. (As already noted, with only one arranged on the wing guide cylinder 35 in the ceiling rail profile 2 no outlet opening 23 is present.)
  • the lever traveler 49 slides on the ramp element 62, which forms an elevated support surface until the locking element 36 engages in the groove of the locking cam member 22, whereby the locking element 36 has reached its breakpoint. Subsequently, the other wings can be correspondingly notched and pivoted to the first wing 3 are created.
  • holding-down device and / or lever runner can also be part of a separate fastener to the frame 32 of a wing 3 Be components as exemplified in FIG. 11 (Carriage 4a with lever traveler component 4b) and FIG. 12 (Carriage 4a with lever traveler component 4b and hold-down member 4c) shown.
  • the hold-down can be designed differently. So is in FIG. 14 a hold-down 48 'is shown, which protrudes only on one side of the web 47, with which it bears against the bottom profile 1 inside. In FIG. 15 is formed at the hold-down 48 "this one-sided projection U-shaped and the modified support section 12" of the bottom profile 1 has a guide web, which engages in the U-shaped projection.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Support Devices For Sliding Doors (AREA)
  • Conveying And Assembling Of Building Elements In Situ (AREA)
  • Wing Frames And Configurations (AREA)

Abstract

Die Erfindung betrifft ein Schiebe- und Drehflügelsystem, umfassend ein Bodenschienenprofil (1) und ein Deckenschienenprofil (2), welche jeweils C-förmig ausgebildet sind und in denen wenigstens zwei zwischen diesen angeordnete Flügel (3) verschiebbar geführt sind, die wenigstens jeweils über wenigstens einen Laufwagen (4, 5) in dem Bodenschienenprofil (1) gelagert sind, derart, dass im eingeschwenkten Zustand der Flügel (3) eine vollständige Aufnahme der Gewichtslast der Flügel (3) durch das Bodenschienenprofil (1) erfolgt. In dem Bodenschienenprofil (1) ist wenigstens eine seitliche Auslassöffnung (16) zum Ausklinken eines Flügels (3) angeordnet, wobei an wenigstens einem Flügel (3) ein Hebeläufer (49) angebracht ist, der oberhalb des Bodenschienenprofils (1) angeordnet ist, wobei auf der Bodenschiene (1) benachbart zu wenigstens einer Auslauföffnung (16) ein Rampenelement (62) angeordnet ist, das mit dem Hebeläufer (49) derart zusammenwirkt, dass der Flügel (3) beim Passieren des Rampenelements (62) angehoben wird.The invention relates to a sliding and rotary sash system comprising a floor rail profile (1) and a ceiling rail profile (2), which are each C-shaped and in which at least two arranged between these wings (3) are displaceably guided, at least in each case over at least a carriage (4, 5) in the bottom rail profile (1) are mounted, such that in the pivoted state of the wing (3) a complete absorption of the weight load of the wings (3) by the bottom rail profile (1). In the bottom rail profile (1) at least one lateral outlet opening (16) for notching a wing (3) is arranged, wherein at least one wing (3) a lever runner (49) is mounted, which is arranged above the bottom rail profile (1) a ramp element (62) is arranged on the bottom rail (1) adjacent to at least one outlet opening (16) and interacts with the lever traveler (49) such that the wing (3) is lifted when passing the ramp element (62).

Description

Die Erfindung betrifft ein Schiebe-und Drehflügelsystem nach dem Oberbegriff des Patentanspruchs 1.The invention relates to a sliding and rotary wing system according to the preamble of patent claim 1.

Derartige Schiebe- und Drehflügelsysteme sind hinlänglich bekannt. Sie weisen mehrere verschiebbare Fensterflügel auf, welche einzeln verschwenkbar sind, wodurch sich eine meist sehr große Front- oder Raumteilung fast vollständig öffnen lässt. Die einzelnen Flügel sind zwischen an der Decke und dem Boden angeordneten Schienenprofilen verschiebbar geführt. Dabei ist jeder Flügel über zwei Auflageelemente verschiebbar in einem Deckenschienenprofil geführt. Zum Verschwenken eines Flügels weist das Deckenschienenprofil eine Auslassöffnung zum Ausklinken eines Auflageelementes eines Flügels auf. In diesem Fall ist endseitig in dem Deckenschienenprofil eine Spreizklammer angeordnet, in die ein an dem jeweiligen Flügel angeordnetes Sperrelement eingebracht wird. Zum Verschwenken eines Flügels wird das Sperrelement in das Rastnockenelement eingefahren und das am anderen Ende des Flügels befindliche Auflageelement aus der Auslassöffnung ausgeklinkt und um die durch das Sperrelement verlaufende Achse verschwenkt. Das Sperrelement dreht sich dabei in eine Führung des Rastnockenelements ein, sodass der Flügel sicher gehalten ist.Such sliding and rotary wing systems are well known. They have a plurality of sliding window sash, which are individually pivotable, which can almost completely open a mostly very large front or space division. The individual wings are slidably guided between arranged on the ceiling and the floor rail profiles. Each wing is guided via two support elements displaceable in a ceiling rail profile. For pivoting a wing, the ceiling rail profile has an outlet opening for notching a support element of a wing. In this case, a Spreizklammer is arranged end in the ceiling rail profile, in which a arranged on the respective wing locking element is introduced. For pivoting a wing, the blocking element is retracted into the locking cam element and the bearing element located at the other end of the wing is disengaged from the outlet opening and pivoted about the axis extending through the blocking element. The blocking element rotates in a guide of the locking cam element, so that the wing is securely held.

Nachteilig an den vorbekannten Schiebe- und Drehflügelsystemen ist, dass das Deckenschienenprofil eine hohe Tragfähigkeit der Decke erfordert, an die dieses montiert wird. Hierdurch ist eine Installation des Systems beispielsweise bei abgehängten Decken erschwert. In der WO 99/45224 A1 ist ein Schiebeflügelsystem beschrieben, bei dem die Flügel über einen Laufwagen in der Bodenschiene verschiebbar gelagert sind, sodass die Gewichtskraft der Flügel im Wesentlichen von der Bodenschiene aufgenommen werden. Bei diesem vorbekannten System ist jedoch ein Ausklinken und Verschwenken einzelner Flügel nicht möglich.A disadvantage of the known sliding and swing systems that the ceiling rail profile requires a high load capacity of the ceiling to which this is mounted. As a result, an installation of the system is difficult, for example, suspended ceilings. In the WO 99/45224 A1 is a sliding wing system described in which the wings are slidably mounted via a carriage in the bottom rail, so that the weight of the wings are substantially absorbed by the bottom rail. In this prior art system, however, a notching and pivoting individual wings is not possible.

Hier will die Erfindung Abhilfe schaffen. Der Erfindung liegt die Aufgabe zu Grunde, ein Schiebe- und Drehflügelsystem der vorgenannten Art bereitzustellen, welches eine Installation auch im Falle von nur begrenzt tragfähigen Decken ermöglicht. Gemäß der Erfindung wird diese Aufgabe durch die Merkmale des kennzeichnenden Teils des Patentanspruchs 1 gelöst.The invention aims to remedy this situation. The invention is based on the object to provide a sliding and rotary vane system of the aforementioned type, which allows installation even in the case of limited viable ceilings. According to the invention, this object is solved by the features of the characterizing part of patent claim 1.

Mit der Erfindung ist ein Schiebeflügelsystem der vorgenannten Art geschaffen, bei dem eine Installation auch bei nur begrenzt tragfähigen Decken ermöglicht ist. Dadurch, dass die wenigstens zwei Flügel jeweils über wenigstens einen Laufwagen in dem Bodenschienenprofil gelagert sind, derart, dass im eingeschwenkten Zustand der Flügel, d.h. in Flucht mit Boden- und Deckenschienenprofil, eine vollständige Aufnahme der Gewichtslast der Flügel durch das Bodenschienenprofil erfolgt, dient das Deckenschienenprofil lediglich der Führung der zwischen Bodenschienenprofil und Deckenschienenprofil angeordneten Flügel; die Zugbelastung des Deckenschienenprofils ist so deutlich reduziert oder sogar eliminiert. Dabei ermöglicht die wenigstens eine seitliche Auslassöffnung ein Ausklingen und Verschwenken eines Flügels. Durch das Zusammenwirken von Hebeläufer und Rampenelement wird der Flügel mit dem Angeordneten Hebeläufer beim Passieren des Rampenelements angehoben. Hierdurch werden die Laufrollen entlastet. Mit Erreichen der Parkposition, d.h. der Ausschwenkposition des Flügels sind die Laufrollen ohne Kontakt mit der Bodenschiene und können so mit dem Flügel aus der Auslassöffnung herausbewegt werden.With the invention, a sliding sash system of the aforementioned type is created, in which an installation is made possible even with limited load-bearing ceilings. Characterized in that the at least two wings are each mounted on at least one carriage in the floor rail profile, such that in the pivoted state of the wing, i. in flight with floor and ceiling rail profile, a complete recording of the weight load of the wing through the floor rail profile, the ceiling rail profile is only the leadership of arranged between the floor rail profile and ceiling rail profile wings; The tensile load of the ceiling rail profile is significantly reduced or even eliminated. In this case, the at least one lateral outlet opening enables a swinging out and pivoting of a wing. Through the interaction of the lever runner and the ramp element, the wing with the arranged lever runner is lifted when passing the ramp element. As a result, the rollers are relieved. Upon reaching the parking position, i. the swing-out position of the wing are the rollers without contact with the bottom rail and can be moved out with the wing from the outlet opening.

Vorteilhaft ist zumindest in dem Deckenschienenprofil endseitig ein Rastnockenelement zur Aufnahme eines an einem jeden Flügel angeordneten Sperrelements angeordnet, wobei horizontal beabstandet zum Rastnockenelement in dem Bodenschienenprofil wenigstens eine Auslassöffnung zum Ausklinken eines Flügels angeordnet ist. Zusätzlich kann auch in dem Bodenprofil ein Rastnockenelement vorgesehen sein, wobei in diesem Fall bevorzugt an dem Laufwagen ein entsprechendes Sperrelement erforderlich ist.Advantageously, at least in the ceiling rail profile end a locking cam member for receiving a arranged on each wing locking element is arranged horizontally spaced from the locking cam member in the bottom rail profile at least one outlet opening for notching a wing is arranged. In addition, a locking cam element may also be provided in the bottom profile, in which case a corresponding blocking element is preferably required on the carriage.

Bevorzugt sind die Flügel an ihrer dem Deckenschienenprofil zugewandten Oberseite mit wenigstens einem Führungszylinder versehen, der in den Spalt des C-förmigen Deckenschienenprofils hineinragt. Hierdurch ist der Flügel über den Führungszylinder in dem Spalt des Deckenschienenprofils geführt, ohne dass eine Auflagelast auf das Deckenschienenprofil einwirkt. Vorteilhaft ist das Sperrelement auf dem Führungszylinder befestigt, insbesondere an diesem angeformt oder auf diesem aufgeschraubt.Preferably, the wings are provided on their side facing the ceiling rail profile top with at least one guide cylinder which projects into the gap of the C-shaped ceiling rail profile. As a result, the wing is guided over the guide cylinder in the gap of the ceiling rail profile without a support load acting on the ceiling rail profile. Advantageously, the locking element is mounted on the guide cylinder, in particular integrally formed on this or screwed onto this.

In Weiterbildung der Erfindung ist der Hebeläufer an dem Laufwagen angeordnet. Hierdurch ist eine kompakte Bauweise erzielt.In a further development of the invention, the lever traveler is arranged on the carriage. As a result, a compact design is achieved.

In Ausgestaltung der Erfindung ist wenigstens eine Auslassöffnung von einem Führungsrahmen eingerahmt, an welchem das Rampenelement angeformt ist. Hierdurch ist eine kombinierte Anhebung und Führung eines Flügels zum Ausschwenken ermöglicht.In an embodiment of the invention, at least one outlet opening is framed by a guide frame on which the ramp element is formed. As a result, a combined raising and guiding a wing for swinging allows.

Vorteilhaft ist das Rampenelement aus dem Fahrweg des Hebeläufers herausbewegbar ausgebildet. Hierdurch ist ein Verfahren eines Flügels ohne Anhebung in dem Fall ermöglicht, dass dieser nicht verschwenkt werden soll.Advantageously, the ramp element is designed to be moved out of the travel path of the lever traveler. As a result, a method of a wing without raising in the case is made possible that this is not to be pivoted.

In weiterer Ausgestaltung der Erfindung ist an wenigstens einem Flügel ein Niederhalter angeordnet. Vorzugsweise ist der Niederhalter an dem Laufwagen angeordnet, insbesondere unterhalb eines Laufrades des Laufwagens, derart, dass der Spalt der Bodenschiene zwischen Laufrad und Niederhalter verläuft. Hierdurch ist eine weitere kompakte Bauweise erzielt.In a further embodiment of the invention, a hold-down is arranged on at least one wing. Preferably, the hold-down is arranged on the carriage, in particular below an impeller of the carriage, such that the gap of the bottom rail between the impeller and hold-down runs. As a result, a further compact design is achieved.

In weiterer Ausgestaltung der Erfindung wirkt der Niederhalter derart mit der Bodenschiene zusammen, dass eine Linearführung des zugehörigen Flügels bewirkt ist. Hierdurch ist eine geführte Bewegung des Flügels entlang der Bodenschiene erzielt.In a further embodiment of the invention, the hold-down device interacts with the bottom rail in such a way that a linear guide of the associated wing is effected. As a result, a guided movement of the wing along the bottom rail is achieved.

In Weiterbildung der Erfindung umfasst der Laufwagen ein Wagengehäuse mit einer Flügelaufnahme und einer an dieser angeformten hohlzylindrischen Lageraufnahme, in welcher Lageraufnahme ein Lager zur rotierbaren Lagerung einer Achse angeordnet ist, die mindestens ein Laufrad aufnimmt, wobei an der Lageraufnahme der Flügelaufnahme gegenüberliegend ein Niederhalter angeformt ist. Hierdurch ist eine weitere kompakte Bauweise ermöglicht. Dabei ist der Hebeläufer bevorzugt beabstandet zu der Lageraufnahme an dem Wagengehäuse angeformt.In a further development of the invention, the carriage comprises a carriage housing with a wing receptacle and a hollow cylindrical bearing receptacle integrally formed thereon, in which bearing receptacle a bearing for rotatably supporting an axle is arranged, which receives at least one impeller, wherein on the bearing receptacle of the wing receptacle opposite a hold-down is formed. As a result, a further compact design is possible. In this case, the lever rotor is preferably formed at a distance from the bearing receptacle on the carriage housing.

Andere Weiterbildungen und Ausgestaltungen der Erfindung sind in den übrigen Unteransprüchen angegeben. Ein Ausführungsbeispiel der Erfindung ist in den Zeichnungen dargestellt und wird nachfolgend im Einzelnen beschrieben. Es zeigen:

Figur 1
die schematische Darstellung eines Schiebe- und Drehflügelsystems;
Figur 2
die Detaildarstellung Flügelführung des Bodenprofils des Schiebe- und Drehflügelsystems aus Figur 1;
Figur 3
die Darstellung der Auslassöffnung des Schiebe- und Drehflügelsystems aus Figur 1;
Figur 4
die räumliche Darstellung des Schiebe- und Drehflügelsystems aus Figur 1 mit Teilausschnitten;
Figur 5
die schematische Darstellung des Eingriffs des Führungszylinders eines Flügels in ein Deckenschienenprofil im Querschnitt;
Figur 6
die schematische Darstellung der Anordnung eines Laufwagens eines Flügels in einem Bodenschienenprofil im Querschnitt;
Figur 7
die schematische Darstellung eines Laufwagens eines Schiebe- und Drehflügelsystem in einer weiteren Ausführungsform mit horizontalen Laufrädern;
Figur 8
die räumliche Darstellung eines ersten Laufwagens des Schiebe- und Drehflügelsystems aus Figur 1;
Figur 9
den Laufwagen aus Figur 8 mit integriertem Niederhalter und Hebeläufer in Explosionsdarstellung;
Figur 10
die schematische Darstellung des Laufwagens aus Figur 8 im Eingriff mit einer Bodenschiene;
Figur 11
die Darstellung aus Figur 10 mit einem Laufwagen in einer zweiten Ausführungsform mit separatem Hebeläufer;
Figur 12
die Darstellung aus Figur 10 mit einem Laufwagen in einer dritten Ausführungsform mit separatem Hebeläufer und Niederhalter;
Figur 13
die schematische Darstellung des Niederhalters des Laufwagens aus Figur 8 im Eingriff einer Bodenschiene;
Figur 14
die schematische Darstellung eines Niederhalters in einer zweiten Ausführungsformmit einseitigem Überstand im Eingriff einer Bodenschiene und
Figur 15
die schematische Darstellung eines Niederhalters in einer dritten Ausführungsformmit einseitigem, U-förmigen Überstand im Eingriff einer modifizierten Bodenschiene mit vertikalem Führungssteg.
Other developments and refinements of the invention are specified in the remaining subclaims. An embodiment of the invention is illustrated in the drawings and will be described in detail below. Show it:
FIG. 1
the schematic representation of a sliding and rotary wing system;
FIG. 2
the detailed representation wing guide of the bottom profile of the sliding and rotary wing system FIG. 1 ;
FIG. 3
the representation of the outlet opening of the sliding and rotary wing system FIG. 1 ;
FIG. 4
the spatial representation of the sliding and rotary wing system FIG. 1 with partial cutouts;
FIG. 5
the schematic representation of the engagement of the guide cylinder of a wing in a ceiling rail profile in cross section;
FIG. 6
the schematic representation of the arrangement of a carriage of a wing in a floor rail profile in cross section;
FIG. 7
the schematic representation of a carriage of a sliding and rotary wing system in another embodiment with horizontal wheels;
FIG. 8
the spatial representation of a first carriage of the sliding and rotary wing system FIG. 1 ;
FIG. 9
the carriage out FIG. 8 with integrated hold-down and lever rotor in exploded view;
FIG. 10
the schematic representation of the carriage from FIG. 8 in engagement with a bottom rail;
FIG. 11
the presentation FIG. 10 with a carriage in a second embodiment with separate lever rotor;
FIG. 12
the presentation FIG. 10 with a carriage in a third embodiment with separate lever rotor and hold-down;
FIG. 13
the schematic representation of the hold of the carriage from FIG. 8 in engagement with a floor rail;
FIG. 14
the schematic representation of a hold-down in a second embodiment with one-sided projection in engagement with a bottom rail and
FIG. 15
the schematic representation of a hold-down in a third embodiment with one-sided, U-shaped projection in engagement of a modified bottom rail with vertical guide bar.

Das als Ausführungsbeispiel gewählte Schiebe- und Drehflügelsystem besteht im Wesentlichen aus einem Bodenschienenprofil 1, einem Deckenschienenprofil 2 sowie einer Anzahl von Flügeln 3, die über Laufwagen 4, 5 in dem Bodenschienenprofil 1 verschiebbar geführt sind. Deckenseitig sind die Flügel 3 über einen Führungszylinder 35 in dem Deckenschienenprofil 2 geführt.The sliding and rotary sash system selected as an exemplary embodiment consists essentially of a floor rail profile 1, a ceiling rail profile 2 and a number of wings 3, which are displaceably guided in the floor rail profile 1 via carriages 4, 5. On the ceiling side, the wings 3 are guided over a guide cylinder 35 in the ceiling rail profile 2.

Das Bodenschienenprofil 1 ist gebildet aus einem Grundprofil 11 und einem hieran befestigten Tragprofil 12, das in dem Grundprofil 11 höhenjustierbar befestigt ist. Das Tragprofil 12 ist im Wesentlichen in Art eines C-Profils ausgebildet und weist an seiner dem Grundprofil 11 abgewandten Oberseite einen Spalt 13 auf. Innerhalb des Tragprofils 12 ist an einer Längsseitenwand ein erster Steg 14 sowie an der gegenüberliegenden Längsseitenwand vertikal versetzt zum ersten Steg 14 ein zweiter Steg 15 angeformt. Weiterhin ist in dem Bodenschienenprofil 1 in einer Längsseitenwand eine Auslassöffnung 16 eingebracht. Die Auslassöffnung 16 des Bodenschienenprofils 1 ist von einem Führungsrahmen 6 eingerahmt, an dessen den Flügeln 3 zugewandter Oberseite eine Auflagefläche 61 ausgebildet ist. An einer Seite ist auf der Auflagefläche ein Rampenelement 62 angeformt, dass zu beiden Seiten mit einer Schräge 63 versehen ist. Im Ausführungsbeispiel ist der Führungsrahmen 6 mit angeformten Rampenelement 62 als Kunststoff hergestellt.The floor rail profile 1 is formed from a base profile 11 and a supporting profile 12 attached thereto, which is fixed in height adjustable in the base profile 11. The support profile 12 is formed substantially in the manner of a C-profile and has a gap 13 on its upper side facing away from the base profile 11. Within the supporting profile 12, a first web 14 is integrally formed on a longitudinal side wall and a second web 15 is offset vertically on the opposite longitudinal side wall to the first web 14. Furthermore, an outlet opening 16 is introduced in the floor rail profile 1 in a longitudinal side wall. The outlet opening 16 of the floor rail profile 1 is framed by a guide frame 6, on whose the wings 3 facing top a support surface 61 is formed. On one side of the support surface, a ramp element 62 is formed, which is provided on both sides with a slope 63. In the exemplary embodiment, the guide frame 6 is made with integrally formed ramp element 62 as plastic.

Das Deckenschienenprofil 2 ist im Wesentlichen in Art eines C-Profils ausgebildet und weist an seiner dem Bodenschienenprofil 1 gegenüberliegenden Oberseite einen Spalt 21 auf. Seitlich ist in dem Deckenschienenprofil 2 eine Auslassöffnung 23 zum Ausklinken eines Führungszylinders 35 eines Flügels 3 eingebracht. (Sofern an dem Flügel 3 nur ein Führungszylinder 35 angeordnet ist, weist das Deckenschienenprofil keine Auslassöffnung 23 auf.) Endseitig ist in dem Deckenschienenprofil 2 ein Rastnockenelement 22 angeordnet. Das Rastnockenelement 22 ist in Form eines zangenförmigen Kunststoffteils ausgebildet, in dessen gegenüberliegend angeordneten Armen aneinandergereiht kreisbogenförmige Ausformungen eingebracht sind, welche etwa mittig mit einer quer zum Deckenprofil 2 verlaufenden Nut zur Aufnahme des Sperrelements 36 eines Flügels 3 versehen ist. Die Innenkontur der kreisbogenförmigen Ausformungen entspricht im Wesentlichen der Außenkontur des Führungszylinders 35 der Flügel 3.The ceiling rail profile 2 is formed substantially in the manner of a C-profile and has a gap 21 on its upper side opposite the bottom rail profile 1. Laterally, an outlet opening 23 for notching a guide cylinder 35 of a wing 3 is inserted in the ceiling rail profile 2. (If only one guide cylinder 35 is arranged on the wing 3, the ceiling rail profile has no outlet opening 23.) At the end, a latching cam element 22 is arranged in the ceiling rail profile 2. The locking cam member 22 is formed in the form of a pliers-shaped plastic part, in whose oppositely arranged arms strung together arcuate formations are introduced, which is approximately centrally provided with a transverse to the ceiling profile 2 groove for receiving the locking element 36 of a wing 3. The inner contour of the circular arc-shaped formations substantially corresponds to the outer contour of the guide cylinder 35 of the wings 3.

Die Flügel 3 sind jeweils aus einem Scheibenelement 31 gebildet, welches endseitig mit einem Rahmenprofil 32 eingefasst ist. An ihrer dem Scheibenelement 31 gegenüberliegenden Seite sind die Rahmenprofile 32 jeweils mit einer C-profilartigen Aufnahme 33 zur Aufnahme der Nutenplatte 42, 51 eines Laufwagens 4, 5 bzw. der Nutenplatte 351 eines Führungszylinders 35 versehen. Im Ausführungsbeispiel ist jeder Flügel 3 an seiner dem Deckenschienenprofil 2 zugewandten Seite mit zwei Führungszylindern 35 sowie an seiner dem Bodenschienenprofil 1 zugewandten Seite mit zwei Laufwagen 4, 5 versehen, welche jeweils über ihre Nutenplatten 351, 42, 51 in der C-profilartigen Aufnahme 33 des Rahmenprofils 32 befestigt sind. Der jeweils dem Rastnockenelement 22 zugewandte Führungszylinder 35 eines jeden Flügels 3 ist an seiner dem Rahmenprofil 32 entgegengesetzten Oberseite mit einem Sperrelement 36 versehen, welches im Wesentlichen in Art einer rechteckigen Platte mit bogenförmigen schmalen Seiten ausgebildet ist. An seiner dem Bodenschienenprofil 1 zugewandten Unterseite sind die Flügel 3 weiterhin beidseitig mit Bürsten 37 versehen.The wings 3 are each formed from a disc element 31, which is bordered by a frame profile 32. On their side opposite the disc element 31 side, the frame profiles 32 are each provided with a C-profile-like receptacle 33 for receiving the grooved plate 42, 51 of a carriage 4, 5 or the grooved plate 351 of a guide cylinder 35. In the exemplary embodiment, each wing 3 is provided on its side facing the ceiling rail profile 2 with two guide cylinders 35 and on its bottom rail profile 1 side facing two carriages 4, 5, which in each case via their grooves plates 351, 42, 51 in the C-profile-like receptacle 33rd the frame profile 32 are attached. Each of the locking cam member 22 facing guide cylinder 35 of each wing 3 is at its the frame profile 32 opposite top provided with a blocking element 36 which is formed substantially in the manner of a rectangular plate with arcuate narrow sides. At its bottom rail profile 1 facing underside of the wings 3 are further provided on both sides with brush 37.

Der erste Laufwagen 4 umfasst ein Wagengehäuse 41, an dem eine Nutenplatte 42 angeformt ist. Die Nutenplatte 42 dient als Aufnahme für einen Flügel 3, in dessen Rahmenprofil 32 die Nutenplatte 42 befestigbar ist. Unterhalb der Nutenplatte 42 ist in dem Wagengehäuse 41 eine im Wesentlichen hohlzylindrische Lageraufnahme 43 angeordnet, die ein Wälzlager 44 aufnimmt. Das Wälzlager 44 nimmt eine Achse 45 auf, an deren beiden Enden jeweils ein Laufrad 46 befestigt ist. An die Lageraufnahme 43 schließt sich ein zylindrischer Steg 47 an, der endseitig in einen zu allen Seiten überstehenden Niederhalter 48 übergeht. Beabstandet zu der Lageraufnahme 43 ist an dem Wagengehäuse weiterhin ein Hebeläufer 49 angeordnet. Der Hebeläufer 49 ist stempelartig ausgebildet. Sein freies Ende ist etwas höher positioniert, als die Laufflächen der Laufräder 46.The first carriage 4 comprises a carriage housing 41, on which a groove plate 42 is formed. The groove plate 42 serves as a receptacle for a wing 3, in the frame profile 32, the groove plate 42 can be fastened. Below the groove plate 42, a substantially hollow cylindrical bearing receptacle 43 is arranged in the carriage housing 41, which receives a rolling bearing 44. The roller bearing 44 receives an axle 45, at both ends of which an impeller 46 is attached. The bearing receptacle 43 is adjoined by a cylindrical web 47, which merges into an abutment 48 protruding on all sides. Spaced to the bearing receptacle 43 a lever 49 is arranged on the carriage body further. The lever 49 is formed like a stamp. Its free end is positioned slightly higher than the running surfaces of the wheels 46.

Der zweite Laufwagen 5 ist an seinem dem ersten Laufwagen 4 gegenüberliegenden Ende des Rahmenprofils 32 eines Flügels 3 positioniert. Er weist eine Nutenplatte 41 auf, an der orthogonal zu dieser ein Tragarm 52 angeformt ist. An den Tragarm 52 schließt sich eine im Wesentlichen rechteckförmige Platte 53 an, die in eine Achse 54 zur Aufnahme von zwei parallel zueinander angeordneten Laufrollen 55 übergeht.The second carriage 5 is positioned at its end opposite the first carriage 4 end of the frame profile 32 of a wing 3. It has a groove plate 41 on which a support arm 52 is formed orthogonal to this. The support arm 52 is followed by a substantially rectangular plate 53, which merges into an axle 54 for receiving two rollers 55 arranged parallel to one another.

Die Flügel 3 sind derart zwischen Bodenschienenprofil 1 und Deckenschienenprofil 2 angeordnet, dass der Tragarm 52 des jeweils zweiten Laufwagens 5 durch den Spalt 13 des Bodenschienenprofils 1 hindurchragen, wobei die der Platte 53 jeweils zugewandte Laufrolle 55 des jeweiligen Laufwagens 5 auf dem zweiten Steg 15 und die zweite Laufrolle 55 auf dem ersten Steg 14 des Bodenschienenprofils 1 aufliegen. Hierdurch rotieren die Laufräder bei Verschieben eines Flügels in entgegengesetzten Richtungen. Die Laufräder 46 des jeweils ersten Laufwagens liegen oben auf dem Tragprofil 12 des Bodenprofils 1 auf. Dabei ragt der Steg 47 ebenfalls durch den Spalt 13 des Bodenschienenprofils 1 hindurch, wobei der Niederhalter 48 innen beidseitig des Spaltes 13 an dem Tragprofil 12 anliegt. Auf der dem Laufwagen gegenüberliegenden Seite ragen die Führungszylinder 35 durch den Spalt 21 in das Deckenschienenprofil 2 hinein.The wings 3 are arranged between the floor rail profile 1 and ceiling rail profile 2 that the support arm 52 of each second carriage 5 protrude through the gap 13 of the bottom rail profile 1, wherein the plate 53 respectively facing roller 55 of the respective carriage 5 on the second web 15 and the second roller 55 rest on the first web 14 of the floor rail profile 1. As a result, the wheels rotate when moving a wing in opposite directions. The wheels 46 of each first carriage are on top of the support section 12 of the soil profile 1. In this case, the web 47 also protrudes through the gap 13 of the floor rail profile 1, wherein the hold-48 abuts the inside of both sides of the gap 13 on the support section 12. On the side opposite the carriage, the guide cylinder 35 project through the gap 21 into the ceiling rail profile 2.

Zum Verschwenken eines Flügels 3 des Schiebe- und Drehflügelsystems wird der Flügel 3 zunächst entlang des Bodenschienenprofils 1 verschoben, bis das Sperrelement 36 in die entferntest liegende freie Ausformung des Rastnockenelements 22 eingreift. Dabei wird der Hebeläufer 49 des am entgegengesetzten Ende des Flügels 3 angeordneten Laufwagens 4 über die Schräge 63 des einer Auslassöffnung 16 zugeordneten Rampenelements 62 bewegt, wodurch die Laufräder 46 dieses Laufwagens 4 relativ zu dem Tragprofil 12 vertikal angehoben werden. In dieser Position befindet sich der Laufwagen 4 an der Auslassöffnung 16 des Profils 1; der äußere Führungszylinder 35 befindet sich an der Auslassöffnung 23 des Deckenschienenprofils 2. (Wie bereits angemerkt, ist bei lediglich einem an dem Flügel angeordneten Führungszylinder 35 in dem Deckenschienenprofil 2 keine Auslassöffnung 23 vorhanden.)For pivoting a blade 3 of the sliding and rotary wing system, the wing 3 is first moved along the bottom rail profile 1 until the locking element 36 engages in the most distant free forming the locking cam member 22. In this case, the lever 49 of the runner 4 arranged at the opposite end of the wing 3 is moved over the slope 63 of an outlet opening 16 associated ramp element 62, whereby the wheels 46 of this carriage 4 are raised relative to the support section 12 vertically. In this position, the carriage 4 is located at the outlet opening 16 of the profile 1; the outer guide cylinder 35 is located at the outlet opening 23 of the ceiling rail profile 2. (As already noted, with only one arranged on the wing guide cylinder 35 in the ceiling rail profile 2 no outlet opening 23 is present.)

Wird nachfolgend der Flügel 3 um die durch das Sperrelement 36 verlaufende Drehachse verschwenkt, so wird der an der Auslassöffnung 16 befindliche Laufwagen 4, dessen Laufräder 46 nicht mehr in Kontakt mit dem Tragprofil 12 sind, aus dieser ausgeklinkt. Der Hebeläufer 49 gleitet dabei auf dem Rampenelement 62, das eine erhöhte Auflagefläche ausbildet, bis das Sperrelement 36 in die Nut des Rastnockenelements 22 eingreift, wodurch das Sperrelement 36 seinen Haltepunkt erreicht hat. Nachfolgend können die weiteren Flügel entsprechend ausgeklinkt und verschwenkt an dem ersten Flügel 3 angelegt werden.If the wing 3 is subsequently pivoted about the axis of rotation passing through the blocking element 36, then the carriage 4 located at the outlet opening 16, whose running wheels 46 are no longer in contact with the supporting profile 12, is unlatched therefrom. The lever traveler 49 slides on the ramp element 62, which forms an elevated support surface until the locking element 36 engages in the groove of the locking cam member 22, whereby the locking element 36 has reached its breakpoint. Subsequently, the other wings can be correspondingly notched and pivoted to the first wing 3 are created.

Im Ausführungsbeispiel ist der Laufwagen 4 mit integriertem Niederhalter 48 und Hebeläufer 49 ausgeführt. Selbstverständlich können Niederhalter und/oder Hebelläufer auch Bestandteil separater an dem Rahmen 32 eines Flügels 3 befestigbarer Bauteile sein, wie beispielhaft in Figur 11 (Laufwagen 4a mit Hebeläuferbauteil 4b) und Figur 12 (Laufwagen 4a mit Hebeläuferbauteil 4b und Niederhalterbauteil 4c) dargestellt. Auch der Niederhalter kann unterschiedlich ausgebildet sein. So ist in Figur 14 ein Niederhalter 48' gezeigt, der lediglich an einer Seite des Steges 47 übersteht, mit der er innen an dem Bodenprofil 1 anliegt. In Figur 15 ist bei dem Niederhalter 48" dieser einseitige Überstand U-förmig ausgebildet und das modifizierte Tragprofil 12" des Bodenprofils 1 weist einen Führungssteg auf, der in den U-förmigen Überstand eingreift.In the exemplary embodiment of the carriage 4 with integrated hold-48 and lever 49 is executed. Of course, holding-down device and / or lever runner can also be part of a separate fastener to the frame 32 of a wing 3 Be components as exemplified in FIG. 11 (Carriage 4a with lever traveler component 4b) and FIG. 12 (Carriage 4a with lever traveler component 4b and hold-down member 4c) shown. Also, the hold-down can be designed differently. So is in FIG. 14 a hold-down 48 'is shown, which protrudes only on one side of the web 47, with which it bears against the bottom profile 1 inside. In FIG. 15 is formed at the hold-down 48 "this one-sided projection U-shaped and the modified support section 12" of the bottom profile 1 has a guide web, which engages in the U-shaped projection.

Claims (10)

Schiebe- und Drehflügelsystem, umfassend ein Bodenschienenprofil (1) und ein Deckenschienenprofil (2), welche jeweils C-förmig ausgebildet sind und in denen wenigstens zwei zwischen diesen angeordnete Flügel (3) verschiebbar geführt sind, die wenigstens jeweils über wenigstens einen Laufwagen (4, 5) in dem Bodenschienenprofil (1) gelagert sind, derart, dass im eingeschwenkten Zustand der Flügel (3) eine vollständige Aufnahme der Gewichtslast der Flügel (3) durch das Bodenschienenprofil (1) erfolgt, dadurch gekennzeichnet, dass in dem Bodenschienenprofil (1) wenigstens eine seitliche Auslassöffnung (16) zum Ausklinken eines Flügels (3) angeordnet ist, wobei an wenigstens einem Flügel (3) ein Hebeläufer (49) angebracht ist, der oberhalb des Bodenschienenprofils (1) angeordnet ist, wobei auf der Bodenschiene (1) benachbart zu wenigstens einer Auslauföffnung (16) ein Rampenelement (62) angeordnet ist, das mit dem Hebeläufer (49) derart zusammenwirkt, dass der Flügel (3) beim Passieren des Rampenelements (62) angehoben wird.Sliding and rotary wing system, comprising a floor rail profile (1) and a ceiling rail profile (2), which are each C-shaped and in which at least two arranged between these wings (3) are displaceably guided, at least in each case at least one carriage (4 , 5) in the bottom rail profile (1) are mounted, such that in the pivoted state of the wing (3) a complete recording of the weight load of the wing (3) by the bottom rail profile (1), characterized in that in the bottom rail profile (1 ) at least one lateral outlet opening (16) for notching a wing (3) is arranged, wherein at least one wing (3) a lever runner (49) is mounted, which is arranged above the floor rail profile (1), wherein on the bottom rail (1 ) is arranged adjacent to at least one outlet opening (16), a ramp element (62) which cooperates with the lever rotor (49) such that the wing (3) during Passing the ramp element (62) is raised. Schiebeflügelsystem nach Anspruch 1, dadurch gekennzeichnet, dass der Hebeläufer (49) an einem Laufwagen (4) angeordnet ist.Sliding wing system according to claim 1, characterized in that the lever runner (49) is arranged on a carriage (4). Schiebeflügelsystem nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass an wenigstens einem Flügel (3) ein Niederhalter (48) angeordnet ist.Sliding wing system according to claim 1 or 2, characterized in that on at least one wing (3) has a hold-down (48) is arranged. Schiebeflügelsystem nach Anspruch 3, dadurch gekennzeichnet, dass der Niederhalter (48) an einem Laufwagen (4) angeordnet ist.Sliding wing system according to claim 3, characterized in that the hold-down device (48) is arranged on a carriage (4). Schiebeflügelsystem nach Anspruch 4, dadurch gekennzeichnet, dass der Niederhalter (48) unterhalb eines Laufrades (46) des Laufwagens (4) angeordnet ist, derart, dass der Spalt (13) der Bodenschiene (1) zwischen Laufrad (46) und Niederhalter (48) verläuft.Sliding wing system according to claim 4, characterized in that the hold-down (48) below an impeller (46) of the carriage (4) is arranged such that the gap (13) of the bottom rail (1) between the impeller (46) and hold-down (48 ) runs. Schiebeflügelelement nach einem der Ansprüche 3 bis 5, dadurch gekennzeichnet, dass der Niederhalter (48) derart mit der Bodenschiene (1) zusammenwirkt, dass eine Linearführung des zugehörigen Flügels(3) bewirkt ist.Sliding wing element according to one of claims 3 to 5, characterized in that the holding-down device (48) cooperates with the bottom rail (1) in such a way that a linear guidance of the associated leaf (3) is effected. Schiebeflügelsystem nach einem der vorgenannten Ansprüche, dadurch gekennzeichnet, dass wenigstens eine Auslassöffnung (16) von einem Führungsrahmen 9 eingerahmt ist, an welchem das Rampenelement (62) angeformt ist.Sliding wing system according to one of the preceding claims, characterized in that at least one outlet opening (16) is framed by a guide frame 9, on which the ramp element (62) is integrally formed. Schiebeflügelsystem nach einem der vorgenannten Ansprüche, dadurch gekennzeichnet, dass das Rampenelement (62) aus dem Verfahrweg des Hebeläufers (49) herausbewegbar ausgebildet ist.Sliding wing system according to one of the preceding claims, characterized in that the ramp element (62) can be moved out of the travel path of the lever traveler (49). Schiebeflügelsystem nach einem der vorgenannten Ansprüche, dadurch gekennzeichnet, dass wenigstens ein Laufwagen (4) ein Wagengehäuse (41) mit einer Flügelaufnahme und einer an dieser angeformten hohlzylindrischen Lageraufnahme (43) umfasst, in welcher Lageraufnahme (43) ein Lager zur rotierbaren Lagerung einer Achse (45) angeordnet ist, die mindestens ein Laufrad (46) aufnimmt, wobei an der Lageraufnahme (43) der Flügelaufnahme gegenüberliegend ein Niederhalter (48) angeformt ist.Sliding wing system according to one of the preceding claims, characterized in that at least one carriage (4) comprises a carriage housing (41) with a wing receptacle and a molded on this hollow cylindrical bearing receptacle (43), in which bearing receptacle (43) a bearing for rotatably supporting an axis (45) is arranged, which receives at least one impeller (46), wherein on the bearing receptacle (43) of the wing receptacle opposite a hold-down (48) is integrally formed. Schiebeflügelsystem nach Anspruch 9, dadurch gekennzeichnet, dass der Hebeläufer (49) beabstandet zu der Lageraufnahme (43) an dem Wagengehäuse (41) angeformt ist.Sliding wing system according to claim 9, characterized in that the lever traveler (49) spaced from the bearing receptacle (43) on the carriage housing (41) is integrally formed.
EP15151501.2A 2015-01-16 2015-01-16 Sliding and rotating leaf system Active EP3045638B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
ES15151501.2T ES2617138T3 (en) 2015-01-16 2015-01-16 Sliding and rotating blade system
EP15151501.2A EP3045638B1 (en) 2015-01-16 2015-01-16 Sliding and rotating leaf system
PCT/EP2016/050387 WO2016113224A1 (en) 2015-01-16 2016-01-11 Slide and swing leaf/sash system
US15/127,593 US10119315B2 (en) 2015-01-16 2016-01-11 Slide and swing leaf/sash system
ZA2016/05984A ZA201605984B (en) 2015-01-16 2016-08-29 Slide and swing leaf/sash system
CL2016002687A CL2016002687A1 (en) 2015-01-16 2016-10-21 System of sliding and tilting window panels.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP15151501.2A EP3045638B1 (en) 2015-01-16 2015-01-16 Sliding and rotating leaf system

Publications (2)

Publication Number Publication Date
EP3045638A1 true EP3045638A1 (en) 2016-07-20
EP3045638B1 EP3045638B1 (en) 2016-12-07

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EP15151501.2A Active EP3045638B1 (en) 2015-01-16 2015-01-16 Sliding and rotating leaf system

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US (1) US10119315B2 (en)
EP (1) EP3045638B1 (en)
CL (1) CL2016002687A1 (en)
ES (1) ES2617138T3 (en)
WO (1) WO2016113224A1 (en)
ZA (1) ZA201605984B (en)

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EP3486416A1 (en) * 2017-11-20 2019-05-22 Riikku Group Oy Fitting

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GB2533368A (en) * 2014-12-18 2016-06-22 Invisifold Ltd A window
FI127852B (en) * 2015-11-10 2019-04-15 Lumon Invest Oy Panel and panel system
CN110199072A (en) * 2016-12-09 2019-09-03 斯坦利布莱克和戴克公司 With the door system for swinging interlock system
US10851569B2 (en) * 2018-07-06 2020-12-01 Overhead Door Corporation Telescoping door with swing clear breakout hinge

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WO1999045224A1 (en) 1998-03-04 1999-09-10 Loennberg Benth Arrangement for pivotable and slidable suspension of sheets
US20110094161A1 (en) * 2009-10-26 2011-04-28 Alan Rees Sliding door structure having sliding doors and pivoting doors
EP2546441A1 (en) * 2011-07-14 2013-01-16 Sunflex Aluminiumsysteme GmbH Sliding and rotating leaf system

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SE523675C2 (en) * 2002-09-06 2004-05-11 Global Financial Advisors Ltd Device for forming a sliding wall structure
SE524005C2 (en) * 2002-10-23 2004-06-15 Nordiska Balco Ab Sliding window assembly
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Publication number Priority date Publication date Assignee Title
DE29723889U1 (en) * 1996-07-05 1999-05-20 Weikert, Dagmar, 31008 Elze Running element
WO1999045224A1 (en) 1998-03-04 1999-09-10 Loennberg Benth Arrangement for pivotable and slidable suspension of sheets
US20110094161A1 (en) * 2009-10-26 2011-04-28 Alan Rees Sliding door structure having sliding doors and pivoting doors
EP2546441A1 (en) * 2011-07-14 2013-01-16 Sunflex Aluminiumsysteme GmbH Sliding and rotating leaf system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3486416A1 (en) * 2017-11-20 2019-05-22 Riikku Group Oy Fitting

Also Published As

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ZA201605984B (en) 2017-09-27
CL2016002687A1 (en) 2017-02-03
US20170130499A1 (en) 2017-05-11
US10119315B2 (en) 2018-11-06
EP3045638B1 (en) 2016-12-07
ES2617138T3 (en) 2017-06-15
WO2016113224A1 (en) 2016-07-21

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