EP1302616B1 - Système de ferrure oscillo-battant - Google Patents

Système de ferrure oscillo-battant Download PDF

Info

Publication number
EP1302616B1
EP1302616B1 EP02016147A EP02016147A EP1302616B1 EP 1302616 B1 EP1302616 B1 EP 1302616B1 EP 02016147 A EP02016147 A EP 02016147A EP 02016147 A EP02016147 A EP 02016147A EP 1302616 B1 EP1302616 B1 EP 1302616B1
Authority
EP
European Patent Office
Prior art keywords
corner
arm
wing
deflection element
turn
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.)
Expired - Lifetime
Application number
EP02016147A
Other languages
German (de)
English (en)
Other versions
EP1302616A1 (fr
Inventor
Jens Peter Kochheim
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.)
Siegenia Aubi KG
Original Assignee
Siegenia Aubi KG
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 Siegenia Aubi KG filed Critical Siegenia Aubi KG
Publication of EP1302616A1 publication Critical patent/EP1302616A1/fr
Application granted granted Critical
Publication of EP1302616B1 publication Critical patent/EP1302616B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/48Suspension arrangements for wings allowing alternative movements
    • E05D15/52Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
    • E05D15/5205Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis with horizontally-extending checks
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
    • E05Y2900/148Windows

Definitions

  • the object of the invention is a turn-tilt fitting system according to the preamble of claim 1.
  • the fitting system consists of an espagnolette fitting with an espagnolette drive element in the form of an espagnolette gear, an opening device and a corner deflection element attached to the upper wing corner on the axis of rotation.
  • the drive rod drive element can be used to adjust the position of a drive rod, depending on the switching position of the sash of the window or of the door on the window frame, which can be pivoted about a vertically extending axis of rotation or tilted about a horizontally running lower axis of rotation.
  • the opening device is provided on the upper horizontal wing leg.
  • An extension arm that is loose when the Tilt & Turn hardware system is installed can be coupled to this, in which it can be assigned at one end with a guide pin in a sliding-pivot bearing of the faceplate of the opening device and at the other end is pivotally connected to a bearing block fixed on the frame side.
  • An auxiliary arm is also provided on the opening device, which serves in addition to the pivoting bearing of the opening arm for fastening the opening arm to the faceplate of the opening device.
  • extension arm is only assembled, for example, only after the entire connecting rod fitting has been fully assembled, or possibly only is coupled to the opening device when the sash is mounted on the frame.
  • the corner deflection element is provided with a corner angle and carries a locking member which is suitable for fixing the extension arm in a parallel position with respect to the opening device or the corner angle of the corner deflection is, so that the extension arm is fixed in the rotationally open position of the connecting rod fitting relative to the faceplate of the opening device or the corner deflection.
  • the tilt and turn fitting system according to EP 0 683 296 B1 is assembled on the fully assembled sash and frame consisting of individual sash and frame spars.
  • the final position of the opening device on the assembled sash frame can only be determined, if this was put together, because the position relative to the wing corner can change due to the manufacturing process.
  • the miter-cut ends of which are subsequently machined e.g. can be welded together by milling the caterpillar. Due to the welding process, the caterpillar can be more or less strong depending on the joining pressure and thus the usable length of the wing spar can vary slightly.
  • the position of the opening device relative to the upper wing corner on the rotational axis side normally varies and must be adjusted by adjusting the opening device accordingly or by mounting the Display arm can be adjusted or the display device is attached to the finished frame.
  • the invention is therefore based on the object of specifying a turn-tilt fitting system for windows or doors which is suitable for using the method known from DE 196 16 271 A1 without having to carry out expensive reworking or observing compliance with closely tolerated production facilities.
  • the installation of the opening device can already take place on the loose rod and the processing tolerances in the manufacture of the sash frame from the wing spars are generous. There are no tolerances which are disadvantageous due to the use of the method and which must be compensated for by appropriate adjustment of the raising device or the raising arm on the frame-side bearing block. Since the pivot bearing of the auxiliary arm requires comparatively little installation space, the size of the corner deflection element can also be kept small and the overall length of the opening device is reduced. It is also possible that the Positioning also takes place on an already assembled sash of a window or a door.
  • the invention basically assumes that the connecting rod drive element can be coupled directly to the opening device, for example by the connecting rod driving element being mounted directly next to the opening device on the upper horizontal wing spar.
  • This arrangement is useful, for example, in the case of pure bottom-hung wings, in which the operation is carried out on the upper wing leg.
  • the connecting rod drive element is to be attached to the upright wing spar remote from the axis of rotation, the connecting rod element is to be connected to the opening device via a further corner deflection element.
  • the corner deflection element has a locking member that interacts with the opening arm in a rotationally open position of the wing. This eliminates the need for such locking devices on the display device, so that the space required for the display device is further reduced.
  • the corner deflection element may also be expedient for the exact positional positioning of the wing-side pivot bearing of the auxiliary arm if the corner deflection element is provided with a corner angle. This is supported on the upright wing rebate edge of the wing leg near the axis of rotation, so that the positioning of the pivot bearing on the corner deflection element relative to this wing rebate surface is ensured.
  • corner deflection element may also have an incorrect operation lock which interacts with the auxiliary arm.
  • misuse protection can be seen, for example, from DE 35 44 778 C1, to which reference is made in full in this regard.
  • the connecting rod fitting of the turn-tilt fitting system is designated by 1.
  • the necessary frame parts of the turn-tilt fitting system are not shown here.
  • the connecting rod fitting 1 essentially consists of the connecting rod drive element 2, the opening device 3 and the corner deflection element 4.
  • the connecting rod drive element 2 and the opening device 3 are connected to one another in the exemplary embodiment shown via a corner deflecting element 5.
  • the espagnolette fitting 1 is usually received in a groove in the rebate surface of the wing 10, which is covered by a faceplate of the espagnolette fitting 1.
  • the drive rod drive element 2 is also attached to the upper horizontal wing leg 6, which is indicated here, so that with the elimination of the corner deflection element 5, a direct coupling is possible.
  • a band 11 and an extension arm 12 are provided on the wing 10 formed from the wing legs 6, 7, 8 and 9.
  • the extension arm 12 can either be attached to the fully assembled wing 10 or also to the frame (not shown here).
  • the wing 10 can be pivoted relative to the frame about a lateral vertical axis 13 or a lower horizontal axis 14 via the connecting rod fitting 1.
  • the extension arm 12 can be coupled with a band 15 and the band 11 is seated in a corner bearing attached to the frame.
  • the band 15 is also assigned a - not shown - bearing block on the frame, so that the band 15 and the bearing block, not shown here, can be pivotally coupled to one another via an axle journal.
  • locking members 16, 17 are provided, which can be moved longitudinally via the connecting rods of the connecting rod fitting 1.
  • the locking members 16 are moved behind locking webs by locking engagements which are fixed in the frame, so that the wing 10 is fixed relative to the frame.
  • the locking members 16 are moved out of the locking engagements and the locking member 17 engages behind a locking engagement 18 attached to the deployment arm 12 such that the deployment arm 12 is fixed in parallel relative to the deployment device 3 or to the corner deflection element 4.
  • the wing 10 can be pivoted about the vertical axis 13.
  • the locking member 17 is moved out of the locking engagement 18 and a locking member 19 on the drive rod drive element 2 interacts with a bolt engagement attached to the frame, so that the wing 10 is fixed at its lower end - along the wing leg 8.
  • the wing 10 can be pivoted about the lower horizontal axis 14. This pivoting movement is limited by the extension arm 12 on the upper horizontal wing leg 6.
  • the extension arm 12 is provided at its end with a guide pin 25 which can be coupled in an elongated hole 26 in the opening device 3.
  • the elongated hole 26 is provided with a keyhole-like extension, which is matched to the enlarged head of the mushroom-shaped guide pin 25, so that it can be inserted into the elongated hole 26 in a sliding end position, which is from the wing corner lying at the junction of the wing legs 6 and 9 24 is located.
  • auxiliary arm 27 which is pivotably attached to it via a pin bore connection 43 and which in turn can be assigned with its free end 28 to a coupling member 29 of the corner deflection element 4.
  • the auxiliary arm 27 is provided with a bore 30 in which a pin 31 of the coupling member 29 can be received. Together, the bore 30 and the pin 31 form the wing-side pivot bearing of the auxiliary arm 27.
  • the opening device 3 and the corner deflection element 4 consist of face plates 32 and 33 and, underneath, longitudinally displaceable drive rods 34, 35. These can be connected to one another via coupling elements 36, 37.
  • the faceplate 33 of the corner deflection element 4 is designed as a corner bracket 38, to which a guide channel 39 for receiving deflection members 40 is fastened.
  • the faceplate 32, 33 or the corner bracket 38 also serve to cover the groove receiving the connecting rod fitting 1 in the fold of the wing 10 and partially form the fold surfaces.
  • the latch engagement 18 is provided, which cooperates with the latch member 17 in the rotationally open position of the wing 10.
  • the locking member 17 is provided on the corner deflection element 4, as is a misuse protection 41, which is designed in accordance with DE 35 44 778 C1, to which reference is made in full in this regard.
  • extension arm 12 is only partially assigned to the opening device 3. At least via the auxiliary arm 27, the extension arm 12 is also assigned to the corner deflection element 4 and releasably connected to it.
  • the extension arm 12 is provided with a coupling section 42 which serves to couple the band 15.
  • the deployment arm 12 is connected to the guide pin 25 with the deployment device 3 and via the auxiliary arm 27 to the corner deflection element 4.
  • the deployment device 3 can already be attached to the wing leg 6, which is not yet connected to the wing legs 7 and 9.
  • the rebated surfaces of the wing 10 and the frame run antiparallel and the functional elements of the wing 10 or the connecting rod fitting 1 cannot interact with the functional members assigned to them on the frame.
  • the extension arm 12 In the rotationally open position of the leaf 10 or the connecting rod fitting 1, the extension arm 12 is supported on the leaf 10 by the auxiliary arm 27, the parallel position of the opening arm 12 relative to the faceplate rails 32, 33 being ensured by the engagement of the locking element 17 and the locking engagement 18 is.
  • the position of the deployment device 3 can also be achieved by the engagement of the guide pin 25 in the slot 26, for example by coupling of the coupling elements 36, 37 vary.
  • the arrangement allows tolerances of the connection of the opening device 3 with the corner deflection element 4 to be compensated for, as well as manufacturing tolerances in the connection of the horizontal wing arm 6 with the vertical wing arms 9. It is only necessary to ensure that the guide pin 25 does not extend into the keyhole-like extension of the elongated hole 26 arrives so that it is always held over the mushroom-like projection in the narrower part of the key-shaped elongated hole 26. This reduces an adjustment of the extension arm 12 or the band 15 attached to it, which may be otherwise necessary, relative to the finished wing 10, which is nevertheless possible via an adjusting screw attached in the area of the coupling section 42, in order to set the time after a period of time Compensate for wing 10.
  • a possible existing dimension 46 of the faceplate 32 of the opening device 3 from the rebate surface 44 is irrelevant.
  • the wing 10 sits completely in the frame and is fixed relative to it via the locking members 16.
  • a parallel alignment position of the extension arm 12 relative to the face plates 32, 33 of the opening device 3 and corner deflection element 4 is also ensured, and the auxiliary arm 27 effects a necessary alignment as in the rotationally open position of the wing 10 or drive rod fitting 1.
  • the wing is in the tilt-open position 10 at its front, lower wing corner distant from the axis of rotation about the Bolt member 19 and the associated bolt engagement supported on the frame, so that the wing 10 can not be moved down along the front vertical wing leg 7 over the usual game.
  • special support devices are usually provided between the sash 10 and the frame, which become effective when the sash 10 runs into the frame. At least when closing the wing 10 pivoted about the lower horizontal axis 14, an elevation of the entire wing 10 is ensured via the auxiliary arm 27, since the extension arm 12 is connected to the frame via the band 15 fastened to it.
  • the exemplary embodiment shown relates to an assembly sequence in which the opening device 3 takes place before the wing 10 is assembled from the wing limbs 6, 7, 8 and 9, the use of the tilt and turn fitting system is also expedient in an assembly sequence, as shown, for example, in FIG EP 0 683 296 B1 is proposed.
  • a coupling point consisting of the coupling elements 36, 37 is located between the opening device 3 and the corner deflection element 4, these can include a relative shift with respect to one another.

Claims (5)

  1. Système d'armature oscillo-battante pour fenêtre ou porte, comprenant au moins une tringlerie d'entraînement (1) avec un élément de commande (2) de la tringlerie d'entraînement, un élément de renvoi angulaire (4) et un dispositif d'orientation (3), ledit élément de renvoi angulaire (4) et le dispositif d'orientation (3) présentant des têtières (32, 33),
    l'élément de commande (2) de la tringlerie d'entraînement, l'élément de renvoi angulaire (4) monté à l'angle supérieur (24) du battant, côté axe de pivotement, et le dispositif d'orientation (3) prévu à l'aile supérieure, horizontale (5) du battant étant couplés ensemble,
    et le système d'armature oscillo-battante présentant un bras d'orientation (12) amovible, qui peut être couplé au battant (10), dans un support de coulissement pivotement, et au dormant, dans un palier de support,
    le bras d'orientation (12) étant équipé d'un bras auxiliaire (27) qui peut être couplé de manière amovible avec le bras d'orientation (12) et / ou la têtière (32, 33), dans des supports de pivotement (43 ; 30, 31),
    caractérisé en ce que
    le supports de pivotement (30, 31) du bras auxiliaire (27), côté battant, est monté de manière amovible sur l'élément de renvoi angulaire (4).
  2. Système d'armature oscilla-battante selon la revendication 1, caractérisé en ce que l'élément de commande (2) de la tringlerie d'entraînement est relié au dispositif d'orientation (3) par l'intermédiaire d'un autre élément de renvoi angulaire (5).
  3. Système d'armature oscillo-battante selon la revendication 1 ou 2, caractérisé en ce que l'élément de renvoi angulaire (4) présente un organe de verrouillage (17) qui, dans une position d'ouverture en pivotement du battant (10), coopère avec le bras d'orientation (12), en verrouillant celui-ci.
  4. Système d'armature oscillo-battante selon l'une des revendications 1 à 3, caractérisé en ce que l'élément de renvoi angulaire (4) est équipé d'une cornière (38)
  5. Système d'armature oscilla-battante selon l'une des revendications 1 à 4, caractérisé en ce que l'élément de renvoi angulaire (4) présente un dispositif anti-fausse manoeuvre, qui coopère avec le bras auxiliaire (27).
EP02016147A 2001-10-10 2002-07-20 Système de ferrure oscillo-battant Expired - Lifetime EP1302616B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10149865 2001-10-10
DE10149865A DE10149865A1 (de) 2001-10-10 2001-10-10 Drehkipp-Beschlagsystem

Publications (2)

Publication Number Publication Date
EP1302616A1 EP1302616A1 (fr) 2003-04-16
EP1302616B1 true EP1302616B1 (fr) 2004-12-29

Family

ID=7701972

Family Applications (1)

Application Number Title Priority Date Filing Date
EP02016147A Expired - Lifetime EP1302616B1 (fr) 2001-10-10 2002-07-20 Système de ferrure oscillo-battant

Country Status (3)

Country Link
EP (1) EP1302616B1 (fr)
AT (1) ATE286194T1 (fr)
DE (2) DE10149865A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007017452A1 (de) * 2007-04-02 2008-10-16 Roto Frank Ag Beschlag für ein Fenster, eine Tür oder dergleichen

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
YU35648B (en) * 1970-12-02 1981-04-30 Frank Gmbh Wilh Main frame holder for the turning and tilting wing of a window or door and the like
DE3544778C1 (de) 1985-12-18 1986-08-21 Siegenia-Frank Kg, 5900 Siegen Fehlbedienungssperre fuer Treibstangenbeschlaege
DE4417842A1 (de) * 1994-05-20 1995-11-23 Winkhaus Fa August Teilautomatisch anschlagbares Beschlagssystem für Fenster, Türen oder dergleichen
DK0740039T3 (da) 1995-04-28 2000-01-17 Siegenia Frank Kg Fremgangsmåde til at udruste en vindues- eller dørfløj med et stangbeslag

Also Published As

Publication number Publication date
EP1302616A1 (fr) 2003-04-16
ATE286194T1 (de) 2005-01-15
DE10149865A1 (de) 2003-04-24
DE50201877D1 (de) 2005-02-03

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