EP1533457B1 - Window or door with at least a concealed scissor-type fitting between a fixed frame and a wing - Google Patents

Window or door with at least a concealed scissor-type fitting between a fixed frame and a wing Download PDF

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Publication number
EP1533457B1
EP1533457B1 EP03026856A EP03026856A EP1533457B1 EP 1533457 B1 EP1533457 B1 EP 1533457B1 EP 03026856 A EP03026856 A EP 03026856A EP 03026856 A EP03026856 A EP 03026856A EP 1533457 B1 EP1533457 B1 EP 1533457B1
Authority
EP
European Patent Office
Prior art keywords
sash
axis
scissor
tilt
guide means
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
EP03026856A
Other languages
German (de)
French (fr)
Other versions
EP1533457A1 (en
Inventor
Stefan Schmock
Martin Siegler
Dirk Hanel
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 AG
Original Assignee
Roto Frank AG
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 AG filed Critical Roto Frank AG
Priority to AT03026856T priority Critical patent/ATE335114T1/en
Priority to EP03026856A priority patent/EP1533457B1/en
Priority to DE50304498T priority patent/DE50304498D1/en
Publication of EP1533457A1 publication Critical patent/EP1533457A1/en
Application granted granted Critical
Publication of EP1533457B1 publication Critical patent/EP1533457B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00—Suspension arrangements for wings
    • E05D15/48—Suspension arrangements for wings allowing alternative movements
    • E05D15/52—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
    • E05D15/5211—Concealed suspension fittings
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING 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
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Type of wing
    • E05Y2900/148—Windows

Definitions

  • the invention relates to a window or a door with a fixed frame, a rotatably mounted on the fixed frame at least about a wing rotation axis wings and with at least one shearing between the fixed frame and the wing, which includes scissor arms and with these in the closed position of the wing in a Fold between folding surfaces of the fixed frame and the wing is arranged, wherein the scissor arms articulated joint joints on each other and hinged to the fixed frame and on the wing and wherein the wing is movable in parallel with the pivot axis of the scissor arms about the hinge axes with the wing pivot axis transversely to the main plane of the fixed frame.
  • Such windows or doors with concealed hardware shears are widely known.
  • the prior art discloses in printed form, for example, in EP 0 360 024 B1 and in DE 34 42 364 C2.
  • the concealed fittings shears are configured such that the wing, when opened and closed simultaneously with its rotational movement on the hinge side, makes a movement transverse to the main plane of the fixed frame. Due to the transverse component of the wing movement an arrangement of the shearing shears in the fold between the fixed frame and the wing and a cover of the folding gap by a wing flap are possible without the wing flap would collide with the fixed frame when opening and closing the wing.
  • the articulation axes of the articulated joints between the scissor arms of the fitting shears with one another and between the scissor arms and the fixed frame or the wing are accordingly aligned parallel to the wing axis of rotation. Due to the chosen arrangement and orientation the fittings shears extend to previously known windows or doors fitting parts or fittings fitting relatively far in the released at lubge Communicationem wing area. If the wing axis of rotation runs vertically, then the removal of the wing load into the fixed frame can be difficult during rotary movement of the wing. Especially in the case of large wings, the shearing scissors alone are not sufficient for the transmission of the wing weight. There are then additional measures to support the wing to the fixed frame required.
  • the present invention has set itself the goal.
  • this object is achieved by the combination of features of claim 1.
  • the shears are housed in the closed position of the wing in the mosachs practicallyen fold between mosachsparallelen folding surfaces of the fixed frame and the wing.
  • the joint axes of the articulated joints of the scissor arms with each other and between the scissor arms and the fixed frame or the wing run in the transverse direction of the closing side fold.
  • the fitting shears are therefore arranged in the case of the invention at the outermost lateral edge of the opening of the fixed frame released at the revolving door.
  • a vertical wing rotation axis With a vertical wing rotation axis, it acts in the fixed wing At least to a large extent frame to be removed wing weight in the longitudinal direction of the scissor arms and thus in a direction in which the scissor arms have a sufficient load-bearing capacity.
  • the Erfindungsbauart according to claim 2 is characterized by a simple structural design.
  • the described hardware shears comprises two scissor arms, which can be articulated to one another both in the manner of an X and in the manner of a Y-scissors.
  • the scissor handlebar connected to the fixed frame and the wing is provided as a guide link, the at least on the wing hinged scissor arms as a control link.
  • the claimed drive is used to open and close the fitting shears and thus to move the wing rotation axis in the transverse direction of the fixed frame. To generate a relative movement of the wing-side articulated joints of the scissor arms, it is conceivable to displace either only one or both joint connections in the direction of the wing axis of rotation.
  • the drive for the relative movement of the wing-side joints of the scissor arms can be designed in many ways. Possibilities according to the invention are indicated in claims 3 to 12.
  • drive elements are used, of which at least one has at least one control track rising in the direction of the wing rotation axis and at least one other has at least one control counterpart resting against the control track. If control track and control counterpart are moved along one another by actuation of the drive, the result is a relative movement of the wing-side articulated connections of the scissor arms in the direction of the wing rotation axis.
  • the actuator When the actuator is actuated by the rotary vane movement, the number of required drive components can be minimized. If the drive for the relative movement of the wing-side articulated joints of the scissor arms is effected by means of a push rod arrangement, the wing can be turned off with respect to the fixed frame, irrespective of the rotary wing movement, in particular when assuming its closed position.
  • the gear described in the claims 5 and 9, in particular the wedge gear according to the claims 6 and 10 are characterized.
  • the types of invention according to claims 7 and 11 are advantageous in that parts of the vane pivot bearings are used simultaneously for actuating the drive for the relative movement of the wing-side articulated joints of the scissor arms in the direction of the vane rotation axis.
  • Claim 12 describes an expedient because structurally simple and space-saving possibility for motion coupling of the wing-side push rod assembly with the on the wing in the transverse direction of the wing axis movably guided slide.
  • the wing is rotatable about both a wing pivot axis and about a copekippachse tiltably mounted on the fixed frame.
  • a tilting-axis-proximate and / or tilt-remote fitting arrangement in this case have a fitting shears of the type described above.
  • the scissor arms When pivoting open and close the wing, the scissor arms are pivoted relative to each other transverse to the mosachsparallelen folding surface of the fixed frame extending hinge axes, the shearing (n) thus opened in a plane transverse to the main plane of the fixed frame and in the transverse direction of copegelkippachse level closed.
  • the tipping near the fitting assembly can at least partially, possibly pivot with the relevant hardware shears to the copekippachse.
  • the wing is released on the tilting axis remote fitting arrangement or fitting shears for tilting movement about the copekippachse.
  • the tilting-near and / or the tilting-axial fitting scissors in development of the invention in each case two mutually hinged scissor arms whose wing-side joints in DrehfunktionsSullivan the fitting arrangements can be moved by means of a drive of the type described above in the direction of the wing axis of rotation relative to each other.
  • the wing-side articulated joints of the scissor arms of the tipping arm near the tilting arm for tilting the wing are optionally locked against a relative movement in the transverse direction of the diegelkippachse (claim 15).
  • the claims 16 to 20 relate to inventions types, which have at least one tilting shear remote scissors.
  • wing-side articulated joints of the scissor arms for a relative movement in the transverse direction of the wing tilt axis are provided on the tilting-axis fitting shears, then one provides controllable locking device that the said wing-side joints are locked when turning the wing around the wing rotation axis relative to movement in the transverse direction of copekippachse and regardless of the tilting of the wing at least one of the joints for movement in the transverse direction of copekippachse can be released (claim 18).
  • a structurally simple and yet functionally reliable locking device for the wing-side joints of the scissor arms of the tilting arm remote scissors is described in claim 20.
  • a window 1 comprises a fixed frame 2 and a wing 3.
  • the wing 3 is rotatable relative to the fixed frame 2 about a vertical wing pivot axis 4 in FIG. 1 and about a wing tilt axis 5 perpendicular to the plane of the drawing in FIG tiltable.
  • a conventional push rod assembly which is guided on the wing 3 in Falz donorsscardi and actuated by a handle.
  • a not shown rempligelkipplager be activated on the rotary-opening side of the wing 3 for tilting the wing 3.
  • the wing 3 is mounted on the fixed frame 2 via a fitting arrangement 6 with a fitting shears 7 designed as a Y-scissors.
  • a long scissor arm 8 and a short scissor arm 9 of the fitting scissors 7 are hinged to each other via a hinge connection 10.
  • the long scissors arm 8 is also pivotally mounted on the hinge side via a hinge connection 11 and a hinge connection 12 fixed frame side.
  • the articulated connection 12 between the long scissors link 8 and the fixed frame 2 is made on a bearing block 13 bolted to the fixed frame 2.
  • the short scissors arm 9 has, in addition to the articulated connection 10, a hinge connection 14 for mounting on the wing 3.
  • the joint axes of all articulated joints 10, 11, 12, 14 are perpendicular to a vertical in Fig. 1 folding surface 15 of the fixed frame second
  • the connection of the long scissors arm 8 with the wing 3 is made on the hinge 11 via an upper rotary bearing sleeve 16.
  • the upper rotary bearing sleeve 16 is seated on a wing-fixed pivot bearing pin 17.
  • a lower rotary bearing sleeve 18 seated on the pivot bearing pin 17 serves for producing a rotary connection between the short scissors link 9 and the wing-side pivot bearing pin 17.
  • the upper pivot bushing 16 and the lower pivot bushing 18 form a handlebar pivot bearing part.
  • a mounting sleeve 19 This takes the pivot pin 17 against rotation and is bolted to mounting tabs 20, 21 with the wing 3. Together with the pivot bearing pin 17, the mounting sleeve 19 forms a wing-side wing-pivot bearing part.
  • the hinged to the short scissors arm 9 lower rotary bearing sleeve 18 rotatably but immovably in the direction of the wing pivot axis 4 on the pivot pin 17.
  • the mounted on the long scissor arm 8 upper rotary bearing sleeve 16 is different from the lower pivot sleeve 18 relative to the pivot pin 17 not only rotatable about the wing axis 4 but also in the direction of the wing axis 4 slidably.
  • the translational mobility of the upper rotary bearing sleeve 16 is indicated in FIG. 3 by a double arrow 24. During its movement in the direction of the double arrow 24, the upper rotary bearing sleeve 16 takes the articulated connection 11 and via this the wing-side end of the long scissor arm 8 With.
  • the upper rotary bearing sleeve 16 is a the wing-side articulated joints 11, 14 of the scissor arm 8, 9 associated drive element of a drive for moving the hinge joint 11 in the direction of the wing axis 4.
  • Such movements performs the hinge joint 11 relative to the hinge connection 14, on which the short Scissor arm 9 is mounted on the wing 3.
  • To implement the wing rotation in a rectilinear motion of the hinge 11 in the direction of the wing axis 4 serve a drive control track 25 on the mounting sleeve 19th and a control counterpart in the form of a drive control track 26 on the upper rotary bearing sleeve 16.
  • the relevant fitting detail is shown in Fig. 4 on an enlarged scale.
  • the mounting sleeve 19 forms a movement-coupled with the wing 3 drive element.
  • Figures 1 to 4 show the window 1 at maximum wovenge carefullyem wing 3. At smaller wing opening angles results in a rotational opening movement of the wing 3 in a translational downward movement of the hinge 11 against the hinge connection 14 and thus in a closing of the hardware shears 7. The closing of the shears 7 in turn causes a parallel Abstellterrorism the wing rotation axis 4 relative to the fixed frame. 2
  • the wing 3 rotated about the wing rotation axis 4 performs all movements transversely to the main plane of the fixed frame 2, without raising or lowering relative to the fixed frame 2 in the direction of the wing rotation axis 4.
  • the articulated connection 14 between the short scissors link 9 and the wing 3 thus shifts during the rotational movement of the wing 3 along a plane perpendicular to the main plane of the fixed frame 2 trajectory.
  • the radial pin slides 27 along a positive control path 28, which traces the course of the drive control tracks 25,26 on the upper rotary bearing sleeve 16 and on the mounting sleeve 19.
  • the positive control track 28 causes the radial pin 27 during the rotational movement of the blade 3, that the drive control tracks 25, 26 abut closely against each other during their entire relative movement.
  • the maximum rotational opening angle of the blade 3 is 110 ° in the example shown. It is marked by two stop surfaces 29, 30 which come to rest on reaching the maximum rotational open position of the wing 3.
  • the stop surfaces 29, 30 are provided on the one hand on the mounting sleeve 19 and on the other hand on the upper rotary bearing sleeve 16.
  • the Fign. Figs. 5 to 7 show the window 1 at a sash rotation angle of 45 °.
  • the window 1 is shown at a vane rotational opening angle of 0 °, that is, when the vane 3 is in the closed position.
  • a distance a 1 between the vane rotation axis 4 and the closing side of the visible surface of the fixed frame 2 at maximum lubge sulfurem wing 3 is a distance a 2 at a rotational opening angle of the blade 3 of 45 ° opposite.
  • the distance dimension is selected such that a collision of a wing override 31 is avoided on the rotary wing 3 with the fixed frame 2.
  • Fig. 8 shows the concealed arrangement of the fitting shears 7 in the closed position of the wing 3.
  • the wing flap 31 covers the remaining between the vertical folding surface 15 of the fixed frame 2 and a vertical folding surface 32 of the wing 3 and, the shearing 7 receiving rebate.
  • the wing 3 is used to connect the wing 3 with the fixed frame 2 in addition to the the fitting arrangement 6 provided opposite the lower closing-side corner region of the window 1 uses a fitting arrangement 56 which is structurally modified with respect to this, as shown in FIGS. 11 to 20 is shown in its rotary function state.
  • the fitting arrangement 56 is mounted in the direction of the wing rotation axis 4 above the fitting arrangement 6 in the upper corner region of the window 1.
  • a conventional opening device with an opening arm is conceivable, which is set for rotating the wing 3 at this and is released for tilting the wing 3 for a pivoting movement about a vertical axis.
  • On the extension arm a fitting shears for parallel parking of the rotary wing 3 would be provided.
  • the fitting arrangement 56 comprises, as shown in FIG. 11, a Y-fitting scissors 57 with a long scissors link 58 and a short scissors link 59.
  • the fitting scissors 57 of the fitting arrangement 56 form a tilting-axis remote, the fitting scissors 7 of the additionally provided fitting arrangement 6 a fitting scissors-near scissors.
  • the long scissors link 58 and the short scissors link 59 of the fitting scissors 7 are articulated to each other via a hinge connection 60.
  • the long scissors arm 58 is pivotally mounted on the wing side via a hinge connection 61 and via an articulated connection 62 on the fixed frame side.
  • the hinge connection 62 is provided on a bolted to the upper horizontal spar of the fixed frame 2 bearing block 63.
  • the wing-side mounting of the short scissors arm 59 is effected by means of a hinge connection 64.
  • a rotary bearing sleeve 66 Between the long scissors link 58 and the wing 3, a rotary bearing sleeve 66, between the short scissors arm 59 and the wing 3, a rotary bearing sleeve 68 is provided.
  • the two pivot bearing sleeves 66, 68 form a handlebar-side wing-pivot bearing part and sit on a wing-fixed pivot bearing pin 67. This is rotatably received in a two-part mounting sleeve 69.
  • the parts of the fastening sleeve 69 are in turn screwed to the wing 3 via fastening straps 70, 71.
  • the rotary bearing sleeve 66 is used when turning the blade 3 as the articulated connections 61, 64 associated drive element for generating a movement of the hinge 61 relative to the hinge connection 64 in the direction of the wing axis 4.
  • the rotary bearing sleeve 66 is for this purpose provided with a drive control track 76.
  • On the drive control track 76 is located as a control counterpart to a drive control pin 75, which in turn protrudes from the pivot pin 67 in the radial direction.
  • the pivot bearing pin 67 forms a movement-coupled with the wing 3 drive element.
  • the drive control track 76 opposite a positive control track 78 is provided which defines a slot-like pin receiving means 74 for the drive control pin 75 together with the drive control track 76.
  • the pin receptacle 74 has a passage opening 77 running in the vertical direction.
  • a slot-like pin receptacle 79 with a horizontal portion and a vertical passage opening 80 is provided at the top in Fig. 11 .
  • a locking pin 81 is guided, the as well as the drive control pin 75 protrudes in the radial direction of the pivot pin 67.
  • Fig. 15 shows the area of the rotary bearing sleeve 68 in an enlarged scale.
  • the drive control pin 75 is located between the drive control track 76 and the positive control track 78.
  • the locking pin 81 is disposed in the horizontal part of the pin receiving 79.
  • the wing 3 takes over the wing-fixed pivot bearing pin 67, the drive control pin 75 and the locking pin 81 in the direction of rotation.
  • the drive control pin 75 accordingly shifts in the direction of the: through opening 77 of the pin receptacle 74, the locking pin 81 in the direction of the passage opening 80 of the pin receiving 79.
  • the drive control pin 75 slides in the described movement of the drive control track 76 of the rotary bearing sleeve 66 along. That the drive control pin 75 of the drive control track 76 actually follows closely fitting, is ensured by means of the positive control path 78.
  • FIGS. 21 to 24 The sequences at the fitting arrangement 6 mounted in the lower closing-side corner region of the window 1 when the wing 3 is tilted about the wing tilting axis 5 are shown in FIGS. 21 to 24 shown.
  • the long scissors link 8 and the short scissors link 9 of the fitting arrangement 6 are essentially parallel to the wing rotation axis 4 and thus with the wing 3 closed vertically aligned.
  • the fitting shears 7 is open at most.
  • the shearing scissors 7 is pivoted overall about the copekippachse 5 in the position shown in FIG. Both in the tilt-ready state shown in FIG. 21 and in the tilting position shown in FIG. 23 and during the tilting movement of the wing 3, the fitting shears 7 by means of the relevant components of the fitting assembly 6 against accidental closing and thus the wing 3 against an undesirable Abstellterrorism relative to the fixed frame 2 secured.
  • a relative rotational movement of the handlebar-side rotary bearing sleeve 16 relative to the wing-side fastening sleeve 19 required for closing the fitting shears 7 is blocked (FIGS. 22, 24).
  • FIGS. 25 to 30 The resulting when tilting of the wing 3 to the copegelkippachse 5 on the fitting assembly 56 in the upper closing side corner portion of the window 1 ratios are shown in FIGS. 25 to 30 shown.
  • FIGS. 19 and 20 show Figs. 25 to 27 the conditions in the closed position of the wing 3.
  • the drive control pin 75 is located on the pivot bearing pin 67.
  • the locking pin 81 on the pivot bearing pin 67 is located at the level of the passage opening 80 of the pin receptacle 79.
  • FIG. 31 shows the fitting arrangement 106 in the view from the closing-side vertical folding surface 15 of the fixed frame 2 to the closing-side vertical folding surface 32 of the wing 3.
  • FIG. 31 shows a tilting shear clip 107 with a long scissor arm 108 and a short scissor arm 109.
  • the scissor arms 108, 109 are hinged to each other via a hinge connection 110.
  • the long scissor arm 108 is also pivotally mounted by means of a hinge 111 to a pivot bearing sleeve 116 and by means of a hinge connection 112 to a bearing block 113 bolted to the fixed frame 2.
  • the short scissors link 109 is coupled on the wing side via a hinge connection 114 with a rotary bearing sleeve 118.
  • Both pivot bearing sleeves 116, 118 sit on a wing-fixed pivot bearing pin 117 and form a handlebar-side pivot bearing part.
  • the pivot bearing pin 117 is rotatably received in the interior of a mounting sleeve 119, which in turn is bolted to a mounting bracket 120 with the wing 3.
  • Pivot bearing pin 117 and mounting sleeve 119 jointly form a wing-side pivot bearing part.
  • the rotary bearing sleeve 116 is movably mounted with a sleeve portion 180 on the pivot pin 117 in the direction mentioned.
  • FIG. 32 shows in detail a slider 182, which is displaceably guided as a drive element on the wing 3 in the direction of a double arrow 183.
  • a drive control track 184 on the side remote from the viewer of FIG. 32 the slider 182 engages in a control groove 185 on the sleeve portion 180 of the rotary bearing sleeve 116.
  • the control track 184 on the slider 182 in this case bears against a drive control track 186 formed by a longitudinal wall of the control groove 185.
  • a slide control 187 To implement the movement of the wing-side push rod assembly to be effected, for example, by means of a hand-operated handle in a movement of the push rod assembly movement-coupled slide 182 is a slide control 187.
  • the link slot 188 has two rectilinear in the direction of the wing rotation axis 4 extending end portions 190, 191 and an angle between them 192 lying.
  • the fitting assembly 106 is to actuate the displacement of the wing pivot axis 4 transversely to the main plane of the fixed frame 2 in the closed position of the wing 3. If this operation takes place approximately by means of a conventional manual transmission with a manual operating handle and the usual gripping positions, then the horizontal gripping position of FIG. 31 and 32 illustrated state of the fitting shears 107 assigned. In this handle position, the wing pivot axis 4 is turned off at the maximum relative to the fixed frame 2. The wing 3 can consequently be rotationally opened without the risk of collisions between the wing flap 31 and the fixed frame 2.
  • the Fign. 33, 34 show the fitting arrangement 106 in the case of the locked-in wing 3.
  • the control pin 189 of the link control 187 was moved by the handle-controlled push rod assembly in the link slot 188 down.
  • the control pin 189 has run into the lower end portion 191 of the guide slot 188. This was associated with a transverse displacement of the slider 182 with respect to FIG. 32 to the right. With this transverse displacement of the slider 182 was accompanied by a lifting movement of the rotary bearing sleeve 116.
  • FIGS. 35 and 36 show the tilt standby state of the wing 3.
  • the handle of the push bar assembly has been rotated to a vertically upwardly facing position.
  • the control pin 189 moved in the cam slot 188 of the link control 187 in the upper end portion 190 of the cam slot 188.
  • a transverse displacement of the slider 182 was connected to the right.
  • the rotary bearing sleeve 116 has been moved upwards, the fitting shears 107 are opened to the maximum.
  • 34 is in the case of the ratios according to FIGS. 35, 36 of the wing 3 unlocked to tilt open. A not shown in detail tilt bearing between the wing 3 and the fixed frame 2 is effective.
  • the fitting assembly 106 with tilted wing 3 show the Fign. 37, 38. Also in the case of the fitting arrangement 106 it is ensured that the tilted wing 3 on the tipping side can not be turned off accidentally with respect to the fixed frame 2.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Wing Frames And Configurations (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
  • Securing Of Glass Panes Or The Like (AREA)

Abstract

The window (1) or door has a fixed frame (2) and at least one swing panel (3) rotating around an axis (4). The panel is mounted to the frame by a pantograph structure (7), with linked arms (8,9) in the closed position between the rabbet surfaces (15,32) of the frame and the panel, For an opening swing movement, the linked arms move on their joints (10-12,14) in a parallel movement with the rotary axis, across the main plane of the fixed frame.

Description

Die Erfindung betrifft ein Fenster oder eine Tür mit einem festen Rahmen, einem an dem festen Rahmen zumindest um eine Flügeldrehachse drehbar gelagerten Flügel sowie mit wenigstens einer Beschlagschere zwischen dem festen Rahmen und dem Flügel, die Scherenlenker umfasst und mit diesen bei Schließlage des Flügels in einem Falz zwischen Falzflächen des festen Rahmens und des Flügels angeordnet ist, wobei die Scherenlenker über Gelenkachsen ausbildende Gelenkverbindungen aneinander sowie an dem festen Rahmen und an dem Flügel angelenkt sind und wobei der Flügel unter gegenseitiger Schwenkbewegung der Scherenlenker um die Gelenkachsen mit der Flügeldrehachse quer zu der Hauptebene des festen Rahmens parallelbeweglich ist.The invention relates to a window or a door with a fixed frame, a rotatably mounted on the fixed frame at least about a wing rotation axis wings and with at least one shearing between the fixed frame and the wing, which includes scissor arms and with these in the closed position of the wing in a Fold between folding surfaces of the fixed frame and the wing is arranged, wherein the scissor arms articulated joint joints on each other and hinged to the fixed frame and on the wing and wherein the wing is movable in parallel with the pivot axis of the scissor arms about the hinge axes with the wing pivot axis transversely to the main plane of the fixed frame.

Derartige Fenster oder Türen mit verdeckt angeordneten Beschlagscheren sind vielfach bekannt. Druckschriftlich offenbart ist gattungsgemäßer Stand der Technik beispielsweise in EP 0 360 024 B1 und in DE 34 42 364 C2. Im Falle der vorbekannten Vorrichtungen sind die verdeckt liegenden Beschlagscheren derart konfiguriert, dass der Flügel beim Öffnen und Schließen gleichzeitig mit seiner Drehbewegung an der Bandseite eine Bewegung quer zu der Hauptebene des festen Rahmens ausführt. Aufgrund der Querkomponente der Flügelbewegung sind eine Anordnung der Beschlagscheren im Falz zwischen festem Rahmen und Flügel sowie eine Abdeckung des Falzspaltes durch einen Flügelüberschlag möglich, ohne dass beim Öffnen und Schließen des Flügels der Flügelüberschlag mit dem festen Rahmen kollidieren würde. Zur Unterbringung der Beschlagscheren dient im Falle des Standes der Technik der Falzraum zwischen den quer zu der Flügeldrehachse verlaufenden Falzflächen des festen Rahmens und des Flügels. Die Gelenkachsen der Gelenkverbindungen zwischen den Scherenlenkern der Beschlagscheren untereinander sowie zwischen den Scherenlenkern und dem festen Rahmen bzw. dem Flügel sind dementsprechend parallel zu der Flügeldrehachse ausgerichtet. Aufgrund der gewählten Anordnung und Ausrichtung der Beschlagscheren erstrecken sich an vorbekannten Fenstern oder Türen Beschlagteile bzw. Beschlageinbauten verhältnismäßig weit in den bei drehgeöffnetem Flügel freigegebenen Bereich. Verläuft die Flügeldrehachse vertikal, so kann sich der Abtrag der Flügellast in den festen Rahmen bei Drehbewegung des Flügels schwierig gestalten. Insbesondere im Falle großer Flügel reichen die Beschlagscheren allein zur Übertragung der Flügel-Gewichtskraft nicht aus. Es sind dann zusätzliche Maßnahmen zur Abstützung des Flügels an dem festen Rahmen erforderlich.Such windows or doors with concealed hardware shears are widely known. The prior art discloses in printed form, for example, in EP 0 360 024 B1 and in DE 34 42 364 C2. In the case of the prior art devices, the concealed fittings shears are configured such that the wing, when opened and closed simultaneously with its rotational movement on the hinge side, makes a movement transverse to the main plane of the fixed frame. Due to the transverse component of the wing movement an arrangement of the shearing shears in the fold between the fixed frame and the wing and a cover of the folding gap by a wing flap are possible without the wing flap would collide with the fixed frame when opening and closing the wing. To accommodate the shearing scissors is in the case of the prior art, the seam between the transverse to the wing axis extending folding surfaces of the fixed frame and the wing. The articulation axes of the articulated joints between the scissor arms of the fitting shears with one another and between the scissor arms and the fixed frame or the wing are accordingly aligned parallel to the wing axis of rotation. Due to the chosen arrangement and orientation the fittings shears extend to previously known windows or doors fitting parts or fittings fitting relatively far in the released at drehgeöffnetem wing area. If the wing axis of rotation runs vertically, then the removal of the wing load into the fixed frame can be difficult during rotary movement of the wing. Especially in the case of large wings, the shearing scissors alone are not sufficient for the transmission of the wing weight. There are then additional measures to support the wing to the fixed frame required.

Den vorstehenden Nachteilen des Standes der Technik abzuhelfen, hat sich die vorliegende Erfindung zum Ziel gesetzt.To remedy the above disadvantages of the prior art, the present invention has set itself the goal.

Erfindungsgemäß gelöst wird diese Aufgabe durch die Merkmalskombination von Patentanspruch 1. An den beanspruchten Fenstern oder Türen sind die Beschlagscheren bei Schließlage des Flügels in dem drehachsseitigen Falz zwischen drehachsparallelen Falzflächen des festen Rahmens und des Flügels untergebracht. Die Gelenkachsen der Gelenkverbindungen der Scherenlenker untereinander sowie zwischen den Scherenlenkern und dem festen Rahmen bzw. dem Flügel verlaufen in Querrichtung des schließseitigen Falzes. Die Beschlagscheren sind im Falle der Erfindung folglich an dem äußersten seitlichen Rand der bei drehgeöffnetem Flügel freigegebenen Öffnung des festen Rahmens angeordnet. Bei vertikaler Flügeldrehachse wirkt die in den festen Rahmen abzutragende Flügel-Gewichtskraft jedenfalls zu einem großen Teil in Längsrichtung der Scherenlenker und somit in einer Richtung, in welcher die Scherenlenker eine hinreichende Lastaufnahmefähigkeit besitzen.According to the invention this object is achieved by the combination of features of claim 1. At the claimed windows or doors the shears are housed in the closed position of the wing in the drehachsseitigen fold between drehachsparallelen folding surfaces of the fixed frame and the wing. The joint axes of the articulated joints of the scissor arms with each other and between the scissor arms and the fixed frame or the wing run in the transverse direction of the closing side fold. The fitting shears are therefore arranged in the case of the invention at the outermost lateral edge of the opening of the fixed frame released at the revolving door. With a vertical wing rotation axis, it acts in the fixed wing At least to a large extent frame to be removed wing weight in the longitudinal direction of the scissor arms and thus in a direction in which the scissor arms have a sufficient load-bearing capacity.

Besondere Ausführungsarten der Erfindung nach Patentanspruch 1 ergeben sich aus den abhängigen Patentansprüchen 2 bis 20.Particular embodiments of the invention according to claim 1 emerge from the dependent claims 2 to 20.

Die Erfindungsbauart nach Patentanspruch 2 zeichnet sich durch einen einfachen konstruktiven Aufbau aus. Die beschriebene Beschlagschere umfasst zwei Scherenlenker, die sowohl nach Art einer X- als auch nach Art einer Y-Schere aneinander angelenkt sein können. Der mit dem festen Rahmen und dem Flügel verbundene Scherenlenker ist als Führungslenker, der zumindest an dem Flügel angelenkte Scherenlenker als Steuerlenker vorgesehen. Der anspruchsgemäße Antrieb dient zum Öffnen und Schließen der Beschlagschere und somit zur Bewegung der Flügeldrehachse in Querrichtung des festen Rahmens. Zur Erzeugung einer Relativbewegung der flügelseitigen Gelenkverbindungen der Scherenlenker ist es denkbar, entweder nur eine oder aber beide Gelenkverbindungen in Richtung der Flügeldrehachse zu verlagern.The Erfindungsbauart according to claim 2 is characterized by a simple structural design. The described hardware shears comprises two scissor arms, which can be articulated to one another both in the manner of an X and in the manner of a Y-scissors. The scissor handlebar connected to the fixed frame and the wing is provided as a guide link, the at least on the wing hinged scissor arms as a control link. The claimed drive is used to open and close the fitting shears and thus to move the wing rotation axis in the transverse direction of the fixed frame. To generate a relative movement of the wing-side articulated joints of the scissor arms, it is conceivable to displace either only one or both joint connections in the direction of the wing axis of rotation.

Der Antrieb für die Relativbewegung der flügelseitigen Gelenkverbindungen der Scherenlenker kann auf vielfältige Art und Weise gestaltet sein. Erfindungsgemäß bevorzugte Möglichkeiten sind in den Patentansprüchen 3 bis 12 angegeben.The drive for the relative movement of the wing-side joints of the scissor arms can be designed in many ways. Possibilities according to the invention are indicated in claims 3 to 12.

In Patentanspruch 3 ist ein konstruktiv einfach aufgebauter und einen lediglich kleinen Einbauraum benötigender Antrieb beschrieben. Es werden dabei Antriebselemente verwendet, von denen wenigstens eines zumindest eine in Richtung der Flügeldrehachse ansteigende Steuerbahn und wenigstens ein anderes zumindest ein an der Steuerbahn anliegendes Steuer-Gegenstück aufweist. Werden Steuerbahn und Steuer-Gegenstück durch Betätigen des Antriebes aneinander entlang bewegt, so resultiert daraus eine Relativbewegung der flügelseitigen Gelenkverbindungen der Scherenlenker in Richtung der Flügeldrehachse.In claim 3, a structurally simple structure and a small installation space requiring drive is described. In this case, drive elements are used, of which at least one has at least one control track rising in the direction of the wing rotation axis and at least one other has at least one control counterpart resting against the control track. If control track and control counterpart are moved along one another by actuation of the drive, the result is a relative movement of the wing-side articulated connections of the scissor arms in the direction of the wing rotation axis.

Zur Betätigung des Antriebes für die Relativbewegung der flügelseitigen Gelenkverbindungen der Scherenlenker wird im Falle der Erfindung die Drehbewegung des Flügels um die Flügeldrehachse (Patentanspruch 4) und/oder eine an dem Flügel in Falzumfangsrichtung bewegbar geführte Schubstangenanordnung (Patentanspruch 8) genutzt.To actuate the drive for the relative movement of the wing-side joints of the scissor arms in the invention, the rotational movement of the wing about the wing axis (claim 4) and / or on the wing in Falzumfangsrichtung movably guided push rod assembly (claim 8) is used.

Bei Antriebsbetätigung durch die Flügel-Drehbewegung lässt sich die Anzahl der benötigten Antriebs-Bauteile minimieren. Wird der Antrieb für die Relativbewegung der flügelseitigen Gelenkverbindungen der Scherenlenker mittels einer Schubstangenanordnung bewirkt, so kann der Flügel unabhängig von der Flügel-Drehbewegung, insbesondere bei Einnahme seiner Schließlage bandseitig mit der Flügeldrehachse gegenüber dem festen Rahmen abgestellt werden.When the actuator is actuated by the rotary vane movement, the number of required drive components can be minimized. If the drive for the relative movement of the wing-side articulated joints of the scissor arms is effected by means of a push rod arrangement, the wing can be turned off with respect to the fixed frame, irrespective of the rotary wing movement, in particular when assuming its closed position.

Erfindungsgemäß bevorzugte Maßnahmen zur Antriebsbetätigung durch die Flügel-Drehbewegung ergeben sich aus den Patentansprüchen 5 bis 7. Entsprechende Maßnahmen zur Antriebsbetätigung mittels einer an dem Flügel in Falzumfangsrichtung bewegbar geführten Schubstangenanordhung sind in den Patentansprüchen 9 bis 12 beschrieben. Die angegebenen Vorkehrungen zur Steuerung der Beschlagscheren durch die Flügel-Drehbewegung einerseits sowie durch eine flügelseitige Schubstangenanordnung andererseits können alternativ oder einander ergänzend vorgesehen sein.According to the invention, preferred measures for actuating actuation by the rotary wing movement result from the claims 5 to 7. Corresponding measures for actuating actuation by means of a movable in the Falzumfangsrichtung Schubstangenanordhung are described in the claims 9 to 12. The arrangements provided for the control of the fittings shears by the wing rotation on the one hand and by a wing-side push rod arrangement on the other hand can be provided alternatively or in addition to each other.

Durch eine hohe Funktionssicherheit bei geringem konstruktivem Aufwand und kleinem Einbaumaß zeichnen sich die in den Patentansprüchen 5 und 9 beschriebenen Getriebe, insbesondere die Keilgetriebe nach den Patentansprüchen 6 und 10 aus. Die Erfindungsbauarten gemäß den Patentansprüchen 7 und 11 sind insofern vorteilhaft, als Teile der Flügel-Drehlager gleichzeitig zur Betätigung des Antriebes für die Relativbewegung der flügelseitigen Gelenkverbindungen der Scherenlenker in Richtung der Flügeldrehachse genutzt werden. Patentanspruch 12 beschreibt eine zweckmäßige weil konstruktiv einfache und platzsparende Möglichkeit zur Bewegungskopplung der flügelseitigen Schubstangenanordnung mit dem an dem Flügel in Querrichtung der Flügeldrehachse bewegbar geführten Schieber.By a high level of reliability with low design effort and small installation dimensions, the gear described in the claims 5 and 9, in particular the wedge gear according to the claims 6 and 10 are characterized. The types of invention according to claims 7 and 11 are advantageous in that parts of the vane pivot bearings are used simultaneously for actuating the drive for the relative movement of the wing-side articulated joints of the scissor arms in the direction of the vane rotation axis. Claim 12 describes an expedient because structurally simple and space-saving possibility for motion coupling of the wing-side push rod assembly with the on the wing in the transverse direction of the wing axis movably guided slide.

Im Falle der in Patentanspruch 13 beschriebenen Variante der Erfindung ist der Flügel sowohl um eine Flügeldrehachse drehbar als auch um eine Flügelkippachse kippbar an dem festen Rahmen gelagert. Eine kippachsnahe und/oder eine kippachsferne Beschlaganordnung weisen dabei eine Beschlagschere der vorstehend beschriebenen Art auf. Bei Schließlage des Flügels ist die kippachsnahe Beschlagschere und/oder die kippachsferne Beschlagschere mit den jeweiligen Scherenlenkern im schließseitigen Falz zwischen festem Rahmen und Flügel untergebracht. Beim Drehöffnen und -schließen des Flügels werden die Scherenlenker um quer zu der drehachsparallelen Falzfläche des festen Rahmens verlaufende Gelenkachsen relativ zueinander geschwenkt, die Beschlagschere(n) mithin in einer quer zu der Hauptebene des festen Rahmens und in Querrichtung der Flügelkippachse verlaufenden Ebene geöffnet bzw. geschlossen. Zum Kippen des Flügels um die Flügelkippachse lässt sich die kippachsnahe Beschlaganordnung wenigstens teilweise, gegebenenfalls mit der betreffenden Beschlagschere, um die Flügelkippachse schwenken. Gleichzeitig ist der Flügel an der kippachsfernen Beschlaganordnung bzw. Beschlagschere zur Kippbewegung um die Flügelkippachse freigegeben.In the case of the variant of the invention described in claim 13, the wing is rotatable about both a wing pivot axis and about a Flügelkippachse tiltably mounted on the fixed frame. A tilting-axis-proximate and / or tilt-remote fitting arrangement in this case have a fitting shears of the type described above. When the wing is in the closed position, the tipping shears near the tipping lever and / or the tipping shears with the respective scissor arms are accommodated in the closing fold between the fixed frame and the wing. When pivoting open and close the wing, the scissor arms are pivoted relative to each other transverse to the drehachsparallelen folding surface of the fixed frame extending hinge axes, the shearing (n) thus opened in a plane transverse to the main plane of the fixed frame and in the transverse direction of Flügelkippachse level closed. To tilt the wing about the Flügelkippachse the tipping near the fitting assembly can at least partially, possibly pivot with the relevant hardware shears to the Flügelkippachse. At the same time, the wing is released on the tilting axis remote fitting arrangement or fitting shears for tilting movement about the Flügelkippachse.

Ausweislich Patentanspruch 14 umfasst die kippachsnahe und/oder die kippachsferne Beschlagschere in Weiterbildung der Erfindung jeweils zwei aneinander angelenkte Scherenlenker, deren flügelseitige Gelenkverbindungen bei Drehfunktionszustand der Beschlaganordnungen mittels eines Antriebes der vorstehend beschriebenen Art in Richtung der Flügeldrehachse relativ zueinander bewegbar sind.As shown in claim 14, the tilting-near and / or the tilting-axial fitting scissors in development of the invention in each case two mutually hinged scissor arms whose wing-side joints in Drehfunktionszustand the fitting arrangements can be moved by means of a drive of the type described above in the direction of the wing axis of rotation relative to each other.

Zur Vermeidung von Fehlfunktionen sind gegebenenfalls die flügelseitigen Gelenkverbindungen der Scherenlenker der kippachsnahen Beschlagschere zum Kippen des Flügels gegen eine Relativbewegung in Querrichtung der Flügelkippachse gesperrt (Patentanspruch 15).To avoid malfunctions, the wing-side articulated joints of the scissor arms of the tipping arm near the tilting arm for tilting the wing are optionally locked against a relative movement in the transverse direction of the Flügelkippachse (claim 15).

Die Patentansprüche 16 bis 20 betreffen Erfindungsbauarten, die zumindest eine kippachsferne Beschlagschere aufweisen.The claims 16 to 20 relate to inventions types, which have at least one tilting shear remote scissors.

Zur Freigabe des Flügels an der kippachsfernen Beschlagschere bieten sich mehrere konstruktive Möglichkeiten. Erfindungsgemäß können zu diesem Zweck die flügelseitigen Gelenkverbindungen der Scherenlenker der kippachsfernen Beschlagschere für eine Relativbewegung in Querrichtung der Flügelkippachse freigegeben sein (Patentanspruch 16). Außerdem ist es erfindungsgemäß aber auch denkbar, die kippachsferne Beschlagschere insgesamt für eine Schwenkbewegung um die Flügelkippachse freizugeben (Patentanspruch 17).There are several design options for releasing the sash on the tilting shear remover. According to the invention, the wing-side articulated joints of the scissor arms of the tilting-axis fitting shears for a relative movement in the transverse direction of the Flügelkippachse be released for this purpose (claim 16). Moreover, it is according to the invention but also conceivable to release the kippachsferne hardware shears in total for a pivoting movement about the Flügelkippachse (claim 17).

Sind an der kippachsfernen Beschlagschere die flügelseitigen Gelenkverbindungen der Scherenlenker für eine Relativbewegung in Querrichtung der Flügelkippachse vorgesehen, so sorgt eine steuerbare Sperrvorrichtung dafür, dass die genannten flügelseitigen Gelenkverbindungen beim Drehen des Flügels um die Flügeldrehachse gegen Relativbewegung in Querrichtung der Flügelkippachse gesperrt sind und dessen ungeachtet zum Kippen des Flügels wenigstens eine der Gelenkverbindungen für eine Bewegung in Querrichtung der Flügelkippachse freigegeben werden kann (Patentanspruch 18).If the wing-side articulated joints of the scissor arms for a relative movement in the transverse direction of the wing tilt axis are provided on the tilting-axis fitting shears, then one provides controllable locking device that the said wing-side joints are locked when turning the wing around the wing rotation axis relative to movement in the transverse direction of Flügelkippachse and regardless of the tilting of the wing at least one of the joints for movement in the transverse direction of Flügelkippachse can be released (claim 18).

Der Einfachheit halber wird im Falle der Erfindungsbauart gemäß Patentanspruch 19 die Drehbewegung des Flügel um die Flügeldrehachse zur Steuerung der Sperrvorrichtung für die flügelseitigen Gelenkverbindungen der Scherenlenker der kippachsfernen Beschlagschere genutzt.For simplicity, in the case of Erfindungsbauart according to claim 19, the rotational movement of the wing to the wing axis used to control the locking device for the wing-side joints of the scissor arms of the tilting arm remote scissors.

Eine konstruktiv einfach ausgebildete und gleichwohl funktionssichere Sperrvorrichtung für die flügelseitigen Gelenkverbindungen der Scherenlenker der kippachsfernen Beschlagschere ist in Patentanspruch 20 beschrieben.A structurally simple and yet functionally reliable locking device for the wing-side joints of the scissor arms of the tilting arm remote scissors is described in claim 20.

Nachstehend wird die Erfindung anhand schematischer Darstellungen zu Ausführungsbeispielen näher erläutert. Es zeigen:

Fig. 1
den schließseitigen unteren Eckbereich eines Fensters mit einem festen Rahmen, einem um 110° drehgeöffneten Flügel und einer zwischen dem festen Rahmen und dem Flügel angeordneten ersten Bauart einer unteren Beschlaganordnung mit Beschlagschere in der Ansicht in Richtung auf die vertikale Falzfläche des festen Rahmens,
Fig. 2
die Verhältnisse nach Fig. 1 in der Ansicht in Richtung des Pfeils II in Fig. 1,
Fig. 3
die Beschlaganordnung nach den Fign. 1 und 2 in Einzeldarstellung,
Fig. 4
das Detail IV in Fig. 3 in vergrößerter Darstellung,
Fign. 5 bis 7
Darstellungen entsprechend den Fign. 2 bis 4 bei um 45° drehgeöffnetem Flügel,
Fign. 8 bis 10
Darstellungen entsprechend den Fign. 2 bis 4 bei geschlossenem Flügel,
Fig. 11
den schließseitigen oberen Eckbereich des Fensters nach Fig. 1 mit einer oberen Beschlaganordnung mit Beschlagschere in der Ansicht in Richtung auf die vertikale Falzfläche des festen Rahmens,
Fig. 12
die Verhältnisse nach Fig. 11 in der Ansicht in Richtung des Pfeils XII in Fig. 11,
Fig. 13
die Beschlaganordnung nach den Fign. 11 und 12 in Einzeldarstellung,
Fig. 14
die Beschlaganordnung nach Fig. 13 in der Ansicht in Richtung des Pfeils XIV in Fig. 13,
Fign. 15, 16
die Details XV, XVI in Fig. 14 in vergrößerter Darstellung,
Fign. 17, 18
Darstellungen entsprechend den Fign. 12 und 13 bei um 45° drehgeöffnetem Flügel,
Fign. 19, 20
Darstellungen entsprechend den Fign. 12 und 13 bei geschlossenem Flügel,
Fig. 21
den schließseitigen unteren Eckbereich des Fensters nach den vorhergehenden Figuren bei geschlossenem Flügel und bei im Kippbereitschaftszustand befindlicher unterer Beschlaganordnung in der Ansicht von der vertikalen Falzfläche des festen Rahmens her,
Fig. 22
das Detail XXII in Fig. 21 in vergrößerter Darstellung,
Fign. 23, 24
Darstellungen entsprechend den Fign. 21, 22 bei kippgeöffnetem Flügel,
Fig. 25
den schließseitigen oberen Eckbereich des Fensters nach den vorhergehenden Figuren bei geschlossenem Flügel und bei im Kippbereitschaftszustand befindlicher oberer Beschlaganordnung in der Ansicht von der vertikalen Falzfläche des Flügels her,
Fign. 26, 27
die Details XXVI, XXVII in Fig. 25 in vergrößerter Darstellung,
Fign. 28 bis 30
Darstellungen entsprechend den Fign. 25 bis 27 bei kippgeöffnetem Flügel,
Fign. 31, 32
eine zweite Bauart einer unteren Beschlaganordnung mit Beschlagschere im Drehbereitschaftszustand,
Fign. 33, 34
die Beschlaganordnung nach den Fign. 31 und 32 bei geschlossenem und verriegeltem Flügel,
Fign. 35, 36
die Beschlaganordnung nach den Fign. 31 und 32 im Kippbereitschaftszustand,
Fig. 37
die Beschlaganordnung nach den Fign. 31 bis 36 bei kippgeöffnetem Flügel in der Ansicht von der vertikalen Falzfläche des festen Rahmens her und
Fig. 38
die Beschlaganordnung nach Fig. 37 in der Ansicht von der vertikalen Falzfläche des Flügels her.
The invention will be explained in more detail with reference to schematic representations of exemplary embodiments. Show it:
Fig. 1
the closing-side lower corner region of a window with a fixed frame, a wing which is opened by 110 ° and a first design of a lower one arranged between the fixed frame and the wing Fitting arrangement with fitting shears in the view in the direction of the vertical folding surface of the fixed frame,
Fig. 2
1 in the direction in the direction of the arrow II in Fig. 1,
Fig. 3
the fitting arrangement according to FIGS. 1 and 2 in detail,
Fig. 4
the detail IV in Fig. 3 in an enlarged view,
FIGS. 5 to 7
Representations according to FIGS. 2 to 4 with the door open at 45 °,
FIGS. 8 to 10
Representations according to FIGS. 2 to 4 with the wing closed,
Fig. 11
the closing-side upper corner region of the window according to FIG. 1 with an upper fitting arrangement with fitting shears in the view in the direction of the vertical folding surface of the fixed frame,
Fig. 12
11 in the direction in the direction of the arrow XII in Fig. 11,
Fig. 13
the fitting arrangement according to FIGS. 11 and 12 in detail,
Fig. 14
the fitting arrangement according to FIG. 13 in the direction in the direction of the arrow XIV in FIG. 13,
FIGS. 15, 16
the details XV, XVI in Fig. 14 in an enlarged view,
FIGS. 17, 18
Representations according to FIGS. 12 and 13 with the door open at 45 °,
FIGS. 19, 20
Representations according to FIGS. 12 and 13 with the wing closed,
Fig. 21
the closing-side lower corner region of the window according to the preceding figures with the wing closed and with the lower fitting arrangement in the tilt-ready state in the view from the vertical folding surface of the fixed frame,
Fig. 22
the detail XXII in Fig. 21 in an enlarged view,
FIGS. 23, 24
Representations according to FIGS. 21, 22 at tilt-open wing,
Fig. 25
the closing-side upper corner region of the window according to the preceding figures with the wing closed and with the upper fitting arrangement in the tilt-ready state in the view from the vertical folding surface of the wing,
FIGS. 26, 27
the details XXVI, XXVII in Fig. 25 in an enlarged view,
FIGS. 28 to 30
Representations according to FIGS. 25 to 27 with tilt-open wing,
FIGS. 31, 32
a second type of lower fitting arrangement with fitting shears in the rotary standby state,
FIGS. 33, 34
the fitting arrangement according to FIGS. 31 and 32 with closed and locked wing,
FIGS. 35, 36
the fitting arrangement according to FIGS. 31 and 32 in the tipping-ready state,
Fig. 37
the fitting arrangement according to FIGS. 31 to 36 with tilt-open wing in the view from the vertical folding surface of the fixed frame forth and
Fig. 38
the fitting arrangement according to Fig. 37 in the view from the vertical folding surface of the wing ago.

Gemäß Fig. 1 umfasst ein Fenster 1 einen festen Rahmen 2 sowie einen Flügel 3. Der Flügel 3 ist gegenüber dem festen Rahmen 2 um eine in Fig. 1 vertikale Flügeldrehachse 4 drehbar sowie um eine in Fig. 1 senkrecht zu der Zeichenebene verlaufende Flügelkippachse 5 kippbar. Zur Verriegelung des Flügels 3 an dem festen Rahmen 2 dient eine herkömmliche Schubstangenanordnung, die an dem Flügel 3 in Falzumfangsrichtung geführt und mittels eines Handgriffs betätigbar ist. Insbesondere kann mittels der Schubstangenanordnung ein nicht gezeigtes Flügelkipplager an der Dreh-Öffnungsseite des Flügels 3 zum Kippen des Flügels 3 aktiviert werden.According to FIG. 1, a window 1 comprises a fixed frame 2 and a wing 3. The wing 3 is rotatable relative to the fixed frame 2 about a vertical wing pivot axis 4 in FIG. 1 and about a wing tilt axis 5 perpendicular to the plane of the drawing in FIG tiltable. To lock the wing 3 to the fixed frame 2 is a conventional push rod assembly which is guided on the wing 3 in Falzumfangsrichtung and actuated by a handle. In particular, by means of the push rod arrangement, a not shown Flügelkipplager be activated on the rotary-opening side of the wing 3 for tilting the wing 3.

In dem unteren schließseitigen Eckbereich des Fensters 1 ist der Flügel 3 über eine Beschlaganordnung 6 mit einer als Y-Schere ausgebildeten Beschlagschere 7 an dem festen Rahmen 2 gelagert. Ein langer Scherenlenker 8 sowie ein kurzer Scherenlenker 9 der Beschlagschere 7 sind über eine Gelenkverbindung 10 aneinander angelenkt. Der lange Scherenlenker 8 ist außerdem über eine Gelenkverbindung 11 flügelseitig und über eine Gelenkverbindung 12 festrahmenseitig schwenkgelagert. Die Gelenkverbindung 12 zwischen dem langen Scherenlenker 8 und dem festen Rahmen 2 wird an einem mit dem festen Rahmen 2 verschraubten Lagerbock 13 hergestellt. Der kurze Scherenlenker 9 weist zusätzlich zu der Gelenkverbindung 10 eine Gelenkverbindung 14 zur Lagerung an dem Flügel 3 auf. Die Gelenkachsen sämtlicher Gelenkverbindungen 10, 11, 12, 14 verlaufen senkrecht zu einer in Fig. 1 vertikalen Falzfläche 15 des festen Rahmens 2.In the lower closing-side corner region of the window 1, the wing 3 is mounted on the fixed frame 2 via a fitting arrangement 6 with a fitting shears 7 designed as a Y-scissors. A long scissor arm 8 and a short scissor arm 9 of the fitting scissors 7 are hinged to each other via a hinge connection 10. The long scissors arm 8 is also pivotally mounted on the hinge side via a hinge connection 11 and a hinge connection 12 fixed frame side. The articulated connection 12 between the long scissors link 8 and the fixed frame 2 is made on a bearing block 13 bolted to the fixed frame 2. The short scissors arm 9 has, in addition to the articulated connection 10, a hinge connection 14 for mounting on the wing 3. The joint axes of all articulated joints 10, 11, 12, 14 are perpendicular to a vertical in Fig. 1 folding surface 15 of the fixed frame second

Die Verbindung des langen Scherenlenkers 8 mit dem Flügel 3 ist an der Gelenkverbindung 11 über eine obere Drehlagerhülse 16 hergestellt. Die obere Drehlagerhülse 16 sitzt auf einem flügelfesten Drehlagerbolzen 17 auf. Entsprechend dient an der Gelenkverbindung 14 eine auf dem Drehlagerbolzen 17 aufsitzende untere Drehlagerhülse 18 zur Herstellung einer Drehverbindung zwischen dem kurzen Scherenlenker 9 und dem flügelseitigen Drehlagerbolzen 17. Die obere Drehlagerhülse 16 und die untere Drehlagerhülse 18 bilden einen lenkerseitigen Flügel-Drehlagerteil.The connection of the long scissors arm 8 with the wing 3 is made on the hinge 11 via an upper rotary bearing sleeve 16. The upper rotary bearing sleeve 16 is seated on a wing-fixed pivot bearing pin 17. Correspondingly, at the articulated connection 14, a lower rotary bearing sleeve 18 seated on the pivot bearing pin 17 serves for producing a rotary connection between the short scissors link 9 and the wing-side pivot bearing pin 17. The upper pivot bushing 16 and the lower pivot bushing 18 form a handlebar pivot bearing part.

Zwischen den Drehlagerhülsen 16, 18 durchsetzt der Drehlagerbolzen 17 eine Befestigungshülse 19. Diese nimmt den Drehlagerbolzen 17 drehfest auf und ist an Befestigungslaschen 20, 21 mit dem Flügel 3 verschraubt. Gemeinsam mit dem Drehlagerbolzen 17 bildet die Befestigungshülse 19 einen flügelseitigen Flügel-Drehlagerteil.Between the rotary bearing sleeves 16, 18 passes through the pivot bearing pin 17 a mounting sleeve 19. This takes the pivot pin 17 against rotation and is bolted to mounting tabs 20, 21 with the wing 3. Together with the pivot bearing pin 17, the mounting sleeve 19 forms a wing-side wing-pivot bearing part.

Wie im Einzelnen Fig. 3 entnommen werden kann, sitzt die an den kurzen Scherenlenker 9 angelenkte untere Drehlagerhülse 18 drehbar aber in Richtung der Flügeldrehachse 4 unverschiebbar auf dem Drehlagerbolzen 17 auf. Die zu diesem Zweck zwischen der unteren Drehlagerhülse 18 und dem Drehlagerbolzen 17 vorgesehene Formschlussverbindung wird mittels eines Axialsicherungsstiftes 22 hergestellt, von dem die untere Drehlagerhülse 18 durchsetzt wird und der tangential in eine Umfangsnut 23 an dem Drehlagerbolzen 17 eingreift.As can be seen in detail in Fig. 3, the hinged to the short scissors arm 9 lower rotary bearing sleeve 18 rotatably but immovably in the direction of the wing pivot axis 4 on the pivot pin 17. The provided for this purpose between the lower rotary bearing sleeve 18 and the pivot pin 17 positive connection is made by means of an axial securing pin 22, of which the lower rotary bearing sleeve 18 is penetrated and engages tangentially in a circumferential groove 23 on the pivot pin 17.

Die an dem langen Scherenlenker 8 angebrachte obere Drehlagerhülse 16 ist anders als die untere Drehlagerhülse 18 relativ zu dem Drehlagerbolzen 17 nicht nur um die Flügeldrehachse 4 drehbar sondern darüber hinaus auch in Richtung der Flügeldrehachse 4 verschiebbar. Die translatorische Beweglichkeit der oberen Drehlagerhülse 16 ist in Fig. 3 durch einen Doppelpfeil 24 angedeutet. Bei ihrer Bewegung in Richtung des Doppelpfeils 24 nimmt die obere Drehlagerhülse 16 die Gelenkverbindung 11 und über diese das flügelseitige Ende des langen Scherenlenkers 8 mit. Dementsprechend ist die obere Drehlagerhülse 16 ein den flügelseitigen Gelenkverbindungen 11, 14 des Scherenlenkers 8, 9 zugeordnetes Antriebselement eines Antriebes zur Bewegung der Gelenkverbindung 11 in Richtung der Flügeldrehachse 4. Derartige Bewegungen führt die Gelenkverbindung 11 relativ zu der Gelenkverbindung 14 aus, über welche der kurze Scherenlenker 9 an dem Flügel 3 gelagert ist.The mounted on the long scissor arm 8 upper rotary bearing sleeve 16 is different from the lower pivot sleeve 18 relative to the pivot pin 17 not only rotatable about the wing axis 4 but also in the direction of the wing axis 4 slidably. The translational mobility of the upper rotary bearing sleeve 16 is indicated in FIG. 3 by a double arrow 24. During its movement in the direction of the double arrow 24, the upper rotary bearing sleeve 16 takes the articulated connection 11 and via this the wing-side end of the long scissor arm 8 With. Accordingly, the upper rotary bearing sleeve 16 is a the wing-side articulated joints 11, 14 of the scissor arm 8, 9 associated drive element of a drive for moving the hinge joint 11 in the direction of the wing axis 4. Such movements performs the hinge joint 11 relative to the hinge connection 14, on which the short Scissor arm 9 is mounted on the wing 3.

Betätigt wird der Antrieb für die Relativbewegung der flügelseitigen Gelenkverbindungen 11, 14 der Scherenlenker 8, 9 durch Drehbewegung des Flügels 3. Zur Umsetzung der Flügeldrehbewegung in eine geradlinige Bewegung der Gelenkverbindung 11 in Richtung der Flügeldrehachse 4 dienen eine Antriebs-Steuerbahn 25 an der Befestigungshülse 19 sowie ein Steuer-Gegenstück in Form einer Antriebs-Steuerbahn 26 an der oberen Drehlagerhülse 16. Das betreffende Beschlagdetail ist in Fig. 4 in vergrößertem Maßstab dargestellt. Die Befestigungshülse 19 bildet ein mit dem Flügel 3 bewegungsgekoppeltes Antriebselement.The drive for the relative movement of the wing-side articulated joints 11, 14 of the scissor arms 8, 9 by rotational movement of the wing 3. To implement the wing rotation in a rectilinear motion of the hinge 11 in the direction of the wing axis 4 serve a drive control track 25 on the mounting sleeve 19th and a control counterpart in the form of a drive control track 26 on the upper rotary bearing sleeve 16. The relevant fitting detail is shown in Fig. 4 on an enlarged scale. The mounting sleeve 19 forms a movement-coupled with the wing 3 drive element.

Bei einer Drehbewegung des Flügels 3 um die Flügeldrehachse 4 gleiten die Antriebs-Steuerbahnen 25, 26 aneinander entlang. Eine Schließ-Drehbewegung des Flügels 3 bewirkt eine Verlagerung der Gelenkverbindung 11 in Fig. 4 nach oben. Nachdem die untere Drehlagerhülse 18 und mit dieser die Gelenkverbindung 14 in Richtung der Flügeldrehachse 4 ortsunveränderlich ist, geht die Aufwärtsbewegung der Gelenkverbindung 11 einher mit einem Öffnen der Beschlagschere 7, Dadurch wiederum wird eine Verlagerung der Flügeldrehachse 4 zu dem festen Rahmen 2 hin bewirkt.Upon a rotational movement of the wing 3 about the wing axis 4, the drive control tracks 25, 26 slide along each other. A closing rotational movement of the wing 3 causes a displacement of the hinge 11 in Fig. 4 upwards. After the lower rotary bearing sleeve 18 and with this the articulated connection 14 in the direction of the wing pivot axis 4 is ortsunveränderlich, the upward movement of the articulated joint 11 is accompanied by a Opening the fitting shears 7, This in turn causes a displacement of the wing pivot axis 4 to the fixed frame 2 out.

Die Figuren 1 bis 4 zeigen das Fenster 1 bei maximal drehgeöffnetem Flügel 3. Bei kleineren Flügelöffnungswinkeln resultiert eine Dreh-Öffnungsbewegung des Flügels 3 in einer translatorischen Abwärtsbewegung der Gelenkverbindung 11 gegenüber der Gelenkverbindung 14 und somit in einem Schließen der Beschlagschere 7. Das Schließen der Beschlagschere 7 wiederum bewirkt eine Parallel-Abstellbewegung der Flügeldrehachse 4 gegenüber dem festen Rahmen 2.Figures 1 to 4 show the window 1 at maximum drehgeöffnetem wing 3. At smaller wing opening angles results in a rotational opening movement of the wing 3 in a translational downward movement of the hinge 11 against the hinge connection 14 and thus in a closing of the hardware shears 7. The closing of the shears 7 in turn causes a parallel Abstellbewegung the wing rotation axis 4 relative to the fixed frame. 2

Aufgrund der gewählten Konfiguration der Beschlagschere 7 führt der um die Flügeldrehachse 4 gedrehte Flügel 3 sämtliche Bewegungen quer zu der Hauptebene des festen Rahmens 2 aus, ohne sich gegenüber dem festen Rahmen 2 in Richtung der Flügeldrehachse 4 anzuheben oder abzusenken. Die Gelenkverbindung 14 zwischen dem kurzen Scherenlenker 9 und dem Flügel 3 verlagert sich demnach bei der Drehbewegung des Flügels 3 entlang einer senkrecht zu der Hauptebene des festen Rahmens 2 verlaufenden Bewegungsbahn.Due to the chosen configuration of the fitting shears 7, the wing 3 rotated about the wing rotation axis 4 performs all movements transversely to the main plane of the fixed frame 2, without raising or lowering relative to the fixed frame 2 in the direction of the wing rotation axis 4. The articulated connection 14 between the short scissors link 9 and the wing 3 thus shifts during the rotational movement of the wing 3 along a plane perpendicular to the main plane of the fixed frame 2 trajectory.

Ein in den Abbildungen ebenfalls dargestellter Radialstift 27 durchsetzt den Drehlagerbolzen 17 oberhalb der oberen Drehlagerhülse 16. Bei der Drehbewegung des Flügels 3 gleitet der Radialstift 27 an einer Zwangssteuerbahn 28 entlang, welche den Verlauf der Antriebs-Steuerbahnen 25,26 an der oberen Drehlagerhülse 16 und an der Befestigungshülse 19 nachvollzieht. Im Zusammenspiel mit der Zwangssteuerbahn 28 bewirkt der Radialstift 27 bei der Drehbewegung des Flügels 3, dass die Antriebs-Steuerbahnen 25, 26 während ihrer gesamten Relativbewegung eng aneinander anliegen. Eine funktionssichere, fügelgesteuerte Bewegung der oberen Drehlagerhülse 16 und somit der Gelenkverbindung 11 in Richtung der Flügeldrehachse 4 ist die Folge. Dass eine derartige Bewegung der oberen Drehlagerhülse 16 relativ zu dem Drehlagerbolzen 17 auch tatsächlich zu einem Öffnen bzw. Schließen der Beschlagschere 7 führt, wird durch die in Richtung der Flügeldrehachse 4 ortsfeste Lagerung der unteren Drehlagerhülse 18 an dem Drehlagerbolzen 17 gewährleistet.A radial pin 27, also shown in the figures, passes through the pivot bearing pin 17 above the upper pivot bearing sleeve 16. During the rotational movement of the wing 3, the radial pin slides 27 along a positive control path 28, which traces the course of the drive control tracks 25,26 on the upper rotary bearing sleeve 16 and on the mounting sleeve 19. In conjunction with the positive control track 28 causes the radial pin 27 during the rotational movement of the blade 3, that the drive control tracks 25, 26 abut closely against each other during their entire relative movement. A functionally reliable, pad-controlled movement of the upper rotary bearing sleeve 16 and thus the articulated connection 11 in the direction of the wing pivot axis 4 is the result. That such a movement of the upper rotary bearing sleeve 16 relative to the pivot pin 17 actually leads to an opening or closing of the fitting shears 7, is ensured by the fixed in the direction of the wing rotation axis 4 stationary mounting of the lower pivot sleeve 18 to the pivot pin 17.

Der maximale Drehöffnungswinkel des Flügels 3 beträgt in dem gezeigten Beispielsfall 110°. Er wird markiert durch zwei Anschlagflächen 29, 30, die bei Erreichen der maximalen Dreh-Offenstellung des Flügels 3 aneinander zur Anlage kommen. Die Anschlagflächen 29, 30 sind einerseits an der Befestigungshülse 19 und andererseits an der oberen Drehlagerhülse 16 vorgesehen.The maximum rotational opening angle of the blade 3 is 110 ° in the example shown. It is marked by two stop surfaces 29, 30 which come to rest on reaching the maximum rotational open position of the wing 3. The stop surfaces 29, 30 are provided on the one hand on the mounting sleeve 19 and on the other hand on the upper rotary bearing sleeve 16.

Die Fign. 5 bis 7 zeigen das Fenster 1 bei einem Flügel-Drehöffnungswinkel von 45°. In den Fign. 8 bis 10 ist das Fenster 1 bei einem Flügel-Drehöffnungswinkel von 0°, d.h. bei in der Schließlage befindlichem Flügel 3 gezeigt.The Fign. Figs. 5 to 7 show the window 1 at a sash rotation angle of 45 °. In the Fign. 8 to 10, the window 1 is shown at a vane rotational opening angle of 0 °, that is, when the vane 3 is in the closed position.

Bei Vergleich der Fign. 2 und 5 ist erkennbar, in welchem Maß sich die Flügeldrehachse 4 bei Drehbewegung des Flügels 3 in Querrichtung des festen Rahmens 2 von diesem entfernt bzw. an diesen annähert. Einem Abstand a1 zwischen der Flügeldrehachse 4 und der schließseitigen Sichtfläche des festen Rahmens 2 bei maximal drehgeöffnetem Flügel 3 steht ein Abstand a2 bei einem Drehöffnungswinkel des Flügels 3 von 45° gegenüber. Über den genannten Drehwinkel des Flügels 3 ist das Abstandsmaß derart gewählt, dass eine Kollision eines Flügelüberschlages 31 an dem drehbewegten Flügel 3 mit dem festen Rahmen 2 vermieden wird.When comparing the Fign. 2 and 5 it can be seen to what extent the wing rotational axis 4 moves away from or approaches the rotational direction of the wing 3 in the transverse direction of the fixed frame 2. A distance a 1 between the vane rotation axis 4 and the closing side of the visible surface of the fixed frame 2 at maximum drehgeöffnetem wing 3 is a distance a 2 at a rotational opening angle of the blade 3 of 45 ° opposite. About the above angle of rotation of the blade 3, the distance dimension is selected such that a collision of a wing override 31 is avoided on the rotary wing 3 with the fixed frame 2.

Fig. 8 zeigt die verdeckte Anordnung der Beschlagschere 7 bei Schließlage des Flügels 3. Der Flügelüberschlag 31 überdeckt dabei den zwischen der vertikalen Falzfläche 15 des festen Rahmens 2 und einer vertikalen Falzfläche 32 des Flügels 3 verbleibenden und,die Beschlagschere 7 aufnehmenden Falzraum.Fig. 8 shows the concealed arrangement of the fitting shears 7 in the closed position of the wing 3. The wing flap 31 covers the remaining between the vertical folding surface 15 of the fixed frame 2 and a vertical folding surface 32 of the wing 3 and, the shearing 7 receiving rebate.

Zur Lagerung des Flügels 3 an dem festen Rahmen 2 bedarf es neben der vorstehend beschriebenen, in dem schließseitigen unteren Eckbereich des Fensters 1 angebrachten Beschlaganordnung 6 einer weiteren Beschlaganordnung. Wäre der Flügel 3 ausschließlich um die Flügeldrehachse 4 drehbar an dem festen Rahmen 2 anzubringen, so könnte diese weitere Beschlaganordnung baugleich mit der Beschlaganordnung 6 ausgeführt sein. Die zweite Beschlaganordnung 6 wäre in Richtung der Flügeldrehachse 4 oberhalb des schließseitigen unteren Eckbereichs des Fensters 1, vorzugsweise in dem oberen schließseitigen Eckbereich des Fensters 1 zu montieren. Bei Anordnung in dem oberen schließseitigen.Eckbereich des Fensters 1 wäre der Lagerbock 13 für den langen Scherenlenker 8 an dem oberen horizontalen Querholm des festen Rahmens 2 mit diesem zu verschrauben. Insgesamt ergäbe sich eine bezüglich der horizontalen Mittelebene des festen Rahmens 2 spiegelsymmetrische Anordnung von oberer und unterer Beschlaganordnung 6.To mount the wing 3 on the fixed frame 2, in addition to the above-described, in the closing side lower corner portion of the window 1 attached fitting assembly 6 requires a further fitting arrangement. If the wing 3 were to be mounted rotatably on the fixed frame 2 exclusively around the wing pivot 4, then this additional fitting arrangement could be of identical design to the fitting arrangement 6. The second fitting arrangement 6 would be in the direction of the wing rotation axis 4 above the closing-side lower corner region of the window 1, preferably to be mounted in the upper closing-side corner region of the window 1. If arranged in the upper closing-side corner region of the window 1, the bearing block 13 for the long scissors link 8 would be screwed to the upper horizontal transverse spar of the fixed frame 2. Overall, a mirror-symmetrical arrangement of the upper and lower fitting arrangement 6 would result with respect to the horizontal center plane of the fixed frame 2.

Da in dem vorliegend dargestellten Beispielsfall der Flügel 3 aber nicht nur um die Flügeldrehachse 4 drehbar sondern darüber hinaus auch um die Flügelkippachse 5 kippbar an dem festen Rahmen 2 zu lagern ist, wird zur Verbindung des Flügels 3 mit dem festen Rahmen 2 zusätzlich zu der in dem unteren schließseitigen Eckbereich des Fensters 1 vorgesehenen Beschlaganordnung 6 eine gegenüber dieser baulich abgewandelte Beschlaganordnung 56 verwendet, wie sie in den Fign. 11 bis 20 in ihrem Drehfunktionszustand gezeigt ist. Die Beschlaganordnung 56 ist in Richtung der Flügeldrehachse 4 oberhalb der Beschlaganordnung 6 in dem oberen Eckbereich des Fensters 1 montiert. Anstelle der Beschlaganordnung 56 ist auch eine herkömmliche Ausstellvorrichtung mit einem Ausstellarm denkbar, der zum Drehen des Flügels 3 an diesem festgelegt und zum Kippen des Flügels 3 für eine Schwenkbewegung um eine vertikale Achse freigegeben wird. An dem Ausstellarm wäre eine Beschlagschere zum Parallelabstellen des drehbewegten Flügels 3 vorzusehen.Since in the present case illustrated the wing 3 but not only about the wing axis 4 rotatable but also about the Flügelkippachse 5 tiltable to be stored on the fixed frame 2, is used to connect the wing 3 with the fixed frame 2 in addition to the the fitting arrangement 6 provided opposite the lower closing-side corner region of the window 1 uses a fitting arrangement 56 which is structurally modified with respect to this, as shown in FIGS. 11 to 20 is shown in its rotary function state. The fitting arrangement 56 is mounted in the direction of the wing rotation axis 4 above the fitting arrangement 6 in the upper corner region of the window 1. Instead of the fitting arrangement 56, a conventional opening device with an opening arm is conceivable, which is set for rotating the wing 3 at this and is released for tilting the wing 3 for a pivoting movement about a vertical axis. On the extension arm a fitting shears for parallel parking of the rotary wing 3 would be provided.

Die Beschlaganordnung 56 umfasst ausweislich Fig. 11 eine Y-Beschlagschere 57 mit einem langen Scherenlenker 58 sowie einem kurzen Scherenlenker 59. Die Beschlagschere 57 der Beschlaganordnung 56 bildet eine kippachsferne, die Beschlagschere 7 der außerdem vorgesehenen Beschlaganordnung 6 eine kippachsnahe Beschlagschere.The fitting arrangement 56 comprises, as shown in FIG. 11, a Y-fitting scissors 57 with a long scissors link 58 and a short scissors link 59. The fitting scissors 57 of the fitting arrangement 56 form a tilting-axis remote, the fitting scissors 7 of the additionally provided fitting arrangement 6 a fitting scissors-near scissors.

Der lange Scherenlenker 58 und der kurze Scherenlenker 59 der Beschlagschere 7 sind über eine Gelenkverbindung 60 aneinander angelenkt. Zusätzlich ist der lange Scherenlenker 58 über eine Gelenkverbindung 61 flügelseitig und über eine Gelenkverbindung 62 festrahmenseitig schwenkgelagert. Die Gelenkverbindung 62 ist dabei an einem mit dem oberen Horizontalholm des festen Rahmens 2 verschraubten Lagerbock 63 vorgesehen. Die flügelseitige Lagerung des kurzen Scherenlenkers 59 erfolgt mittels einer Gelenkverbindung 64.The long scissors link 58 and the short scissors link 59 of the fitting scissors 7 are articulated to each other via a hinge connection 60. In addition, the long scissors arm 58 is pivotally mounted on the wing side via a hinge connection 61 and via an articulated connection 62 on the fixed frame side. The hinge connection 62 is provided on a bolted to the upper horizontal spar of the fixed frame 2 bearing block 63. The wing-side mounting of the short scissors arm 59 is effected by means of a hinge connection 64.

Zwischen dem langen Scherenlenker 58 und dem Flügel 3 ist eine Drehlagerhülse 66, zwischen dem kurzen Scherenlenker 59 und dem Flügel 3 ein Drehlagerhülse 68 vorgesehen. Die beiden Drehlagerhülsen 66, 68 bilden einen lenkerseitigen Flügel-Drehlagerteil und sitzen auf einem flügelfesten Drehlagerbolzen 67 auf. Dieser ist in einer zweiteiligen Befestigungshülse 69 drehfest aufgenommen. Die Teile der Befestigungshülse 69 wiederum sind über Befestigungslaschen 70, 71 mit dem Flügel 3 verschraubt.Between the long scissors link 58 and the wing 3, a rotary bearing sleeve 66, between the short scissors arm 59 and the wing 3, a rotary bearing sleeve 68 is provided. The two pivot bearing sleeves 66, 68 form a handlebar-side wing-pivot bearing part and sit on a wing-fixed pivot bearing pin 67. This is rotatably received in a two-part mounting sleeve 69. The parts of the fastening sleeve 69 are in turn screwed to the wing 3 via fastening straps 70, 71.

Befestigungshülse 69 und Drehlagerbolzen 67 bilden einen flügelseitigen Drehlagerteil.Mounting sleeve 69 and pivot pin 67 form a wing-side pivot bearing part.

Die Drehlagerhülse 66 dient bei Drehen des Flügels 3 als den Gelenkverbindungen 61, 64 zugeordnetes Antriebselement zur Erzeugung einer Bewegung der Gelenkverbindung 61 gegenüber der Gelenkverbindung 64 in Richtung der Flügeldrehachse 4. Wie Fig. 16 in vergrößertem Maßstab zeigt, ist die Drehlagerhülse 66 zu diesem Zweck mit einer Antriebs-Steuerbahn 76 versehen. An der Antriebs-Steuerbahn 76 liegt als Steuer-Gegenstück ein Antriebs-Steuerzapfen 75 an, der seinerseits von dem Drehlagerbolzen 67 in radialer Richtung vorsteht. Der Drehlagerbolzen 67 bildet ein mit dem Flügel 3 bewegungsgekoppeltes Antriebselement.The rotary bearing sleeve 66 is used when turning the blade 3 as the articulated connections 61, 64 associated drive element for generating a movement of the hinge 61 relative to the hinge connection 64 in the direction of the wing axis 4. As shown in Fig. 16 on an enlarged scale, the rotary bearing sleeve 66 is for this purpose provided with a drive control track 76. On the drive control track 76 is located as a control counterpart to a drive control pin 75, which in turn protrudes from the pivot pin 67 in the radial direction. The pivot bearing pin 67 forms a movement-coupled with the wing 3 drive element.

Der Antriebs-Steuerbahn 76 gegenüberliegend ist eine Zwangssteuerbahn 78 vorgesehen, die gemeinsam mit der Antriebs-Steuerbahn 76 eine schlitzartige Zapfenaufnahme 74 für den Antriebs-Steuerzapfen 75 begrenzt. An ihrem in Fig. 11 sichtbaren Ende weist die Zapfenaufnahme 74 eine in vertikaler Richtung verlaufende Durchtrittsöffnung 77 auf.The drive control track 76 opposite a positive control track 78 is provided which defines a slot-like pin receiving means 74 for the drive control pin 75 together with the drive control track 76. At its end visible in FIG. 11, the pin receptacle 74 has a passage opening 77 running in the vertical direction.

An der in Fig. 11 obenliegenden Drehlagerhülse 18 ist eine schlitzartige Zapfenaufnahme 79 mit einem horizontalen Abschnitt und einer vertikalen Durchtrittsöffnung 80 vorgesehen. In der Zapfenaufnahme 79 ist ein Sperrzapfen 81 geführt, der ebenso wie der Antriebs-Steuerzapfen 75 in radialer Richtung von dem Drehlagerbolzen 67 vorsteht. Fig. 15 zeigt den Bereich der Drehlagerhülse 68 in vergrößertem Maßstab.At the top in Fig. 11 rotary bearing sleeve 18, a slot-like pin receptacle 79 with a horizontal portion and a vertical passage opening 80 is provided. In the pin receiving 79 a locking pin 81 is guided, the as well as the drive control pin 75 protrudes in the radial direction of the pivot pin 67. Fig. 15 shows the area of the rotary bearing sleeve 68 in an enlarged scale.

In den Fign. 11 bis 16 sind die Verhältnisse an der oberen schließseitigen Ecke des Fensters 1 bei einem Drehöffnungswinkel des Flügels 3 von 110°, d.h. bei maximaler Drehöffnungsweite des Flügels 3 dargestellt. Der Antriebs-Steuerzapfen 75 liegt zwischen der Antriebs-Steuerbahn 76 und der Zwangssteuerbahn 78. Der Sperrzapfen 81 ist in dem horizontalen Teil der Zapfenaufnahme 79 angeordnet.In the Fign. 11 to 16 are the ratios at the upper closing side corner of the window 1 at a rotational opening angle of the blade 3 of 110 °, i. shown at maximum rotational opening width of the wing 3. The drive control pin 75 is located between the drive control track 76 and the positive control track 78. The locking pin 81 is disposed in the horizontal part of the pin receiving 79.

Wird nun ausgehend von dem Zustand gemäß den Fign. 11 bis 16 der Flügel 3 um die Flügeldrehachse 4 in Schließrichtung bewegt, so nimmt der Flügel 3 über den flügelfesten Drehlagerbolzen 67 den Antriebs-Steuerzapfen 75 sowie den Sperrzapfen 81 in Drehrichtung mit. Der Antriebs-Steuerzapfen 75 verlagert sich dementsprechend in Richtung auf die:Durchtrittsöffnung 77 der Zapfenaufnahme 74, der Sperrzapfen 81 in Richtung auf die Durchtrittsöffnung 80 der Zapfenaufnahme 79. Der Antriebs-Steuerzapfen 75 gleitet bei der beschriebenen Bewegung an der Antriebs-Steuerbahn 76 der Drehlagerhülse 66 entlang. Dass der Antriebs-Steuerzapfen 75 der Antriebs-Steuerbahn 76 dabei auch tatsächlich eng anliegend folgt, wird mittels der Zwangssteuerbahn 78 gewährleistet. Infolge des Anstieges der Antriebs-Steuerbahn 76 in Richtung der Flügeldrehachse 4 verlagert sich bei der Bewegung des Antriebs-Steuerzapfens 75 entlang der Antriebs-Steuerbahn 76 die Drehlagerhülse 66 an dem Drehlagerbolzen 67 entlang nach unten. Die Drehlagerhülse 68 wird mittels des Sperrzapfens 81 in Richtung der Flügeldrehachse 4 ortsfest gehalten. Im Ergebnis bewegt sich die Drehlagerhülse 66 von der Drehlagerhülse 68 weg. Eine entsprechende Relativbewegung führen die von den Drehlagerhülsen 66, 68 mitgenommenen Gelenkverbindungen 61, 64 des langen Scherenlenkers 58 und des kurzen Scherenlenkers 59 aus. Die Beschlagschere 57 öffnet sich.Now, starting from the state shown in FIGS. 11 to 16 of the wing 3 is moved about the wing axis 4 in the closing direction, the wing 3 takes over the wing-fixed pivot bearing pin 67, the drive control pin 75 and the locking pin 81 in the direction of rotation. The drive control pin 75 accordingly shifts in the direction of the: through opening 77 of the pin receptacle 74, the locking pin 81 in the direction of the passage opening 80 of the pin receiving 79. The drive control pin 75 slides in the described movement of the drive control track 76 of the rotary bearing sleeve 66 along. That the drive control pin 75 of the drive control track 76 actually follows closely fitting, is ensured by means of the positive control path 78. As a result of the increase of the drive control track 76 in the direction of the wing rotation axis 4 shifts at the movement of the drive control pin 75 along the drive control track 76, the rotary bearing sleeve 66 on the pivot pin 67 down along. The rotary bearing sleeve 68 is held stationary by means of the locking pin 81 in the direction of the wing rotation axis 4. As a result, the rotary bearing sleeve 66 moves away from the rotary bearing sleeve 68. A corresponding relative movement lead from the pivot bearing sleeves 66, 68 entrained joint connections 61, 64 of the long scissor arm 58 and the short scissor arm 59 from. The fitting scissors 57 opens.

Bei einem Drehöffnungswinkel des Flügels.3 von 45° ist die Gesamtanordnung in den Fign. 17 und 18 gezeigt. Bei Vergleich der Fign. 12 und 17 ist erkennbar, dass sich die Flügeldrehachse 4 infolge der Schließdrehbewegung des Flügels 3 an den festen Rahmen 2 angenähert hat. Der bei einem Drehöffnungswinkel des Flügels 3 von 110° bestehende Abstand a1 hat sich zu einem Abstand a2 verringert.At a Drehöffnungswinkel the Flügel.3 of 45 °, the overall arrangement in Figs. 17 and 18 are shown. When comparing the Fign. 12 and 17 it can be seen that the vane rotation axis 4 has approached the fixed frame 2 as a result of the closing rotational movement of the vane 3. The existing at a rotary opening angle of the blade 3 of 110 ° distance a 1 has decreased to a distance a 2 .

Wird der Flügel 3 weiter um die Flügeldrehachse 4 in Schließrichtung gedreht, so kommt er letzten Endes an dem festen Rahmen 2 zur Anlage. Die sich bei Schließlage des Flügels 3 ergebenden Verhältnisse sind in den Fign. 19 und 20 gezeigt. Die Beschlagschere 57 ist nun vollständig in dem Falzraum zwischen der vertikalen Falzfläche 15 des festen Rahmens 2 und der vertikalen Falzfläche 32 des Flügels 3 aufgenommen. Die gesamte Beschlaganordnung 56 wird durch den Flügelüberschlag 31 verdeckt.If the wing 3 is further rotated about the wing axis 4 in the closing direction, it finally comes to the fixed frame 2 to the plant. The resulting in the closed position of the wing 3 conditions are shown in FIGS. 19 and 20 are shown. The fitting scissors 57 is now completely received in the rebate space between the vertical folding surface 15 of the fixed frame 2 and the vertical folding surface 32 of the wing 3. The whole Fitting assembly 56 is hidden by the wing flap 31.

Ausweislich Fig. 20 liegt bei geschlossenem Flügel 3 an der Drehlagerhülse 66 der an dem Drehlagerbolzen 67 angebrachte Antriebs-Steuerzapfen 75 der Durchtrittsöffnung 77 gegenüber. An der Drehlagerhülse 68 befindet sich der Sperrzapfen 81 auf Höhe der Durchtrittsöffnung 80. Aufgrund dieser Anordnung geben der zuvor auch als Sperrzapfen wirksame Antriebs-Steuerzapfen 75 und der Sperrzapfen 81 an sich den Flügel 3 für eine in Richtung der Flügeldrehachse 4 nach oben gerichtete Bewegung frei. Ein derartiges Ausheben des Flügels 3 wird aber mittels einer nicht im Einzelnen gezeigten Aushebesicherung verhindert.As shown in FIG. 20, when the vane 3 is closed, the drive control pin 75 of the passage opening 77, which is attached to the pivot bearing pin 67, adjoins the rotary bearing sleeve 66. As a result of this arrangement, the drive pin 75 and the locking pin 81, which were previously effective as locking pins, release the wing 3 for upward movement in the direction of the wing rotation axis 4 , However, such lifting of the wing 3 is prevented by means of a not shown in detail Aushebsicherung.

Ausgehend von der Schließlage des Flügels 3 möglich ist eine Kippbewegung des Flügels 3 um die Flügelkippachse 5.Starting from the closed position of the wing 3 is possible a tilting movement of the wing 3 to the Flügelkippachse. 5

Die Abläufe an der in dem unteren schließseitigen Eckbereich des Fensters 1 montierten Beschlaganordnung 6 beim Kippen des Flügels 3.um die Flügelkippachse 5 sind in den Fign. 21 bis 24 dargestellt.The sequences at the fitting arrangement 6 mounted in the lower closing-side corner region of the window 1 when the wing 3 is tilted about the wing tilting axis 5 are shown in FIGS. 21 to 24 shown.

Gemäß Fig. 21 sind der lange Scherenlenker 8 und der kurze Scherenlenker 9 der Beschlaganordnung 6 bei geschlossenem Flügel 3 im Wesentlichen parallel zu der Flügeldrehachse 4 und damit vertikal ausgerichtet. Die Beschlagschere 7 ist maximal geöffnet.According to FIG. 21, the long scissors link 8 and the short scissors link 9 of the fitting arrangement 6 are essentially parallel to the wing rotation axis 4 and thus with the wing 3 closed vertically aligned. The fitting shears 7 is open at most.

Zum Kippen des Flügels 3 wird die Beschlagschere 7 insgesamt um die Flügelkippachse 5 in die Position gemäß Fig. 23 geschwenkt. Sowohl im Kippbereitschaftszustand gemäß Fig. 21 als auch in der Kipplage gemäß Fig. 23 sowie während der Kippbewegung des Flügels 3 ist die Beschlagschere 7 mittels der betreffenden Bauteile der Beschlaganordnung 6 gegen versehentliches Schließen und damit der Flügel 3 gegen eine unerwünschte Abstellbewegung gegenüber dem festen Rahmen 2 gesichert. Eine zum Schließen der Beschlagschere 7 erforderliche Relativ-Drehbewegung der lenkerseitigen Drehlagerhülse 16 gegenüber der flügelseitigen Befestigungshülse 19 ist blockiert (Fign. 22, 24).To tilt the wing 3, the shearing scissors 7 is pivoted overall about the Flügelkippachse 5 in the position shown in FIG. Both in the tilt-ready state shown in FIG. 21 and in the tilting position shown in FIG. 23 and during the tilting movement of the wing 3, the fitting shears 7 by means of the relevant components of the fitting assembly 6 against accidental closing and thus the wing 3 against an undesirable Abstellbewegung relative to the fixed frame 2 secured. A relative rotational movement of the handlebar-side rotary bearing sleeve 16 relative to the wing-side fastening sleeve 19 required for closing the fitting shears 7 is blocked (FIGS. 22, 24).

Die sich beim Kippen des Flügels 3 um die Flügelkippachse 5 an der Beschlaganordnung 56 in dem oberen schließseitigen Eckbereich des Fensters 1 ergebenden Verhältnisse sind in den Fign. 25 bis 30 gezeigt.The resulting when tilting of the wing 3 to the Flügelkippachse 5 on the fitting assembly 56 in the upper closing side corner portion of the window 1 ratios are shown in FIGS. 25 to 30 shown.

Entsprechend den Fign. 19 und 20 zeigen die Fign. 25 bis 27 die Verhältnisse bei Schließlage des Flügels 3. Der Antriebs-Steuerzapfen 75 an dem Drehlagerbolzen 67 liegt.der Durchtrittsöffnung 77 der Zapfenaufnahme 74 gegenüber; der Sperrzapfen 81 an dem Drehlagerbolzen 67 befindet sich auf Höhe der Durchtrittsöffnung 80 der Zapfenaufnahme 79. Wird nun ausgehend von diesem Funktionszustand der Gesamtanordnung der Flügel 3 in Öffnungsrichtung um die Flügelkippachse 5 gekippt, so können sich die Drehlagerhülsen 66, 68 auf dem Drehlagerbolzen 67 gegenläufig bewegen. Es ergeben sich dann die Verhältnisse gemäß den Fign. 28 bis 30. Bei der Drehbewegung des Flügels 3 um die Flügeldrehachse 4, also bei Drehfunktionszustand der Beschlaganordnungen 6, 56 sind die Drehlagerhülsen 66, 68 gegen eine gegenläufige Bewegung gesperrt. Wesentliche Bestandteile der betreffenden Sperrvorrichtungen sind der Antriebs-Steuerzapfen 75 in der Zapfenaufnahme 74 und der Sperrzapfen 81 in der Zapfenaufnahme 79.According to FIGS. 19 and 20 show Figs. 25 to 27 the conditions in the closed position of the wing 3. The drive control pin 75 is located on the pivot bearing pin 67. the passage opening 77 of the pin receptacle 74 opposite; the locking pin 81 on the pivot bearing pin 67 is located at the level of the passage opening 80 of the pin receptacle 79. Will now starting from this Functional state of the overall arrangement of the wings 3 tilted in the opening direction about the Flügelkippachse 5, so the rotary bearing sleeves 66, 68 can move in opposite directions on the pivot pin 67. It then results in the conditions according to FIGS. 28 to 30. During the rotary movement of the blade 3 about the wing pivot axis 4, ie in the rotational state of the fitting assemblies 6, 56, the pivot bearing sleeves 66, 68 are locked against an opposite movement. Essential components of the locking devices in question are the drive control pin 75 in the pin receptacle 74 and the locking pin 81 in the pin receptacle 79th

Zum Schließen des kippgeöffneten Flügels 3 ausgehend von dem in den Fign. 28 bis 30 veranschaulichten Öffnungszustand ist der Flügel 3 um die Flügelkippachse 5 gegen den festen Rahmen 2 zu schwenken. Dabei laufen der Antriebs-Steuerzapfen 75 und der Sperrzapfen 81 durch die Durchtrittsöffnungen 77, 80 an den Drehlagerhülsen 66, 68 in ihre Positionen gemäß den Fign. 25 bis 27 ein.To close the tilt-open wing 3 starting from the in Figs. 28 to 30 illustrated opening state, the wing 3 to pivot about the Flügelkippachse 5 against the fixed frame 2. In this case, the drive control pin 75 and the locking pin 81 pass through the passage openings 77, 80 on the pivot bearing sleeves 66, 68 in their positions according to FIGS. 25 to 27 one.

Während im Falle der Beschlaganordnungen 6, 56 gemäß den Fign. 1 bis 30 die Drehbewegung des Flügels 3 um die Flügeldrehachse 4 dazu genutzt wird, die Flügeldrehachse 4 gesteuert in Querrichtung der Hauptebene des festen Rahmens 2 zu verlagern, dient im Falle einer Beschlaganordnung 106, wie sie in den Fign. 31 bis 38 gezeigt ist, zu dem selben Zweck eine an dem Flügel 3 in Flügelumfangsrichtung bewegbare Schubstangenanordnung herkömmlicher Bauart.While in the case of the fitting assemblies 6, 56 shown in FIGS. 1 to 30, the rotational movement of the blade 3 is used to the wing pivot axis 4 to move the wing pivot axis 4 controlled in the transverse direction of the main plane of the fixed frame 2, is used in the case of a fitting assembly 106, as shown in Figs. 31 to 38 is shown for the same purpose on the Wing 3 movable in the wing perimeter direction push rod assembly of conventional design.

Der Einfachheit halber ist diese Schubstangenanordnung in den Abbildungen nicht im Einzelnen dargestellt.For the sake of simplicity, this push rod arrangement is not shown in detail in the figures.

Fig. 31 zeigt die Beschlaganordnung 106 in der Ansicht von der schließseitigen vertikalen Falzfläche 15 des festen Rahmens 2 auf die schließseitige vertikale Falzfläche 32 des Flügels 3. In Fig. 31 zu erkennen ist eine kippachsnahe Beschlagschere 107 mit einem langen Scherenlenker 108 sowie einem kurzen Scherenlenker 109. Die Scherenlenker 108, 109 sind über eine Gelenkverbindung 110 aneinander angelenkt. Der lange Scherenlenker 108 ist außerdem mittels einer Gelenkverbindung 111 an einer Drehlagerhülse 116 und mittels einer Gelenkverbindung 112 an einem mit dem festen Rahmen 2 verschraubten Lagerbock 113 schwenkgelagert. Der kurze Scherenlenker 109 ist flügelseitig über eine Gelenkverbindung 114 mit einer Drehlagerhülse 118 gekoppelt. Beide Drehlagerhülsen 116, 118 sitzen auf einem flügelfesten Drehlagerbolzen 117 auf und bilden einen lenkerseitigen Drehlagerteil. Der Drehlagerbolzen 117 ist drehfest im Innern einer Befestigungshülse 119 aufgenommen, die ihrerseits an einer Befestigungslasche 120 mit dem Flügel 3 verschraubt ist. Drehlagerbolzen 117 und Befestigungshülse 119 bilden gemeinschaftlich einen flügelseitigen Drehlagerteil.FIG. 31 shows the fitting arrangement 106 in the view from the closing-side vertical folding surface 15 of the fixed frame 2 to the closing-side vertical folding surface 32 of the wing 3. FIG. 31 shows a tilting shear clip 107 with a long scissor arm 108 and a short scissor arm 109. The scissor arms 108, 109 are hinged to each other via a hinge connection 110. The long scissor arm 108 is also pivotally mounted by means of a hinge 111 to a pivot bearing sleeve 116 and by means of a hinge connection 112 to a bearing block 113 bolted to the fixed frame 2. The short scissors link 109 is coupled on the wing side via a hinge connection 114 with a rotary bearing sleeve 118. Both pivot bearing sleeves 116, 118 sit on a wing-fixed pivot bearing pin 117 and form a handlebar-side pivot bearing part. The pivot bearing pin 117 is rotatably received in the interior of a mounting sleeve 119, which in turn is bolted to a mounting bracket 120 with the wing 3. Pivot bearing pin 117 and mounting sleeve 119 jointly form a wing-side pivot bearing part.

Während die Befestigungshülse 119 ebenso wie die Drehlagerhülse 118 in Richtung der Flügeldrehachse 4 unbeweglich auf dem Drehlagerbolzen 117 aufsitzt, ist die Drehlagerhülse 116 mit einem Hülsenabschnitt 180 auf dem Drehlagerbolzen 117 in der genannten Richtung beweglich gelagert.While the mounting sleeve 119 as well as the rotary bearing sleeve 118 immovably seated in the direction of the wing pivot axis 4 on the pivot pin 117, the rotary bearing sleeve 116 is movably mounted with a sleeve portion 180 on the pivot pin 117 in the direction mentioned.

In Fig. 32 ist die Beschlaganordnung 106 in der Ansicht von der vertikalen Falzfläche 32 des Flügels 3 in Richtung auf die vertikale Falzfläche 15 des festen Rahmens 2 dargestellt. In Fig. 32 im Detail zu erkennen ist ein Schieber 182, der als Antriebselement an dem Flügel 3 in Richtung eines Doppelpfeils 183 verschiebbar geführt ist. Mit einer Antriebs-Steuerbahn 184 an der von dem Betrachter von Fig. 32 abliegenden Seite greift der Schieber 182 in eine Steuernut 185 an dem Hülsenabschnitt 180 der Drehlagerhülse 116 ein. Die Steuerbahn 184 an dem Schieber 182 liegt dabei an einer von einer Längswand der Steuernut 185 gebildeten Antriebs-Steuerbahn 186 an.In Fig. 32, the fitting assembly 106 is shown in the view of the vertical folding surface 32 of the wing 3 in the direction of the vertical folding surface 15 of the fixed frame 2. FIG. 32 shows in detail a slider 182, which is displaceably guided as a drive element on the wing 3 in the direction of a double arrow 183. With a drive control track 184 on the side remote from the viewer of FIG. 32, the slider 182 engages in a control groove 185 on the sleeve portion 180 of the rotary bearing sleeve 116. The control track 184 on the slider 182 in this case bears against a drive control track 186 formed by a longitudinal wall of the control groove 185.

Zur Umsetzung der beispielsweise mittels eines Handbetätigungsgriffs zu bewirkenden Bewegung der flügelseitigen Schubstangenanordnung in eine Bewegung des mit der Schubstangenanordnung bewegungsgekoppelten Schiebers 182 dient eine Kulissensteuerung 187. Diese umfasst einen Kulissenschlitz 188 an dem Schieber 182 sowie einen in den Kulissenschlitz 188 eingreifenden Steuerzapfen 189, der seinerseits an der flügelseitigen Schubstangenanordnung angebracht ist. Der Kulissenschlitz 188 besitzt zwei geradlinig in Richtung der Flügeldrehachse 4 verlaufende Endabschnitte 190, 191 sowie eine zwischen diesen liegende Abwinkelung 192.To implement the movement of the wing-side push rod assembly to be effected, for example, by means of a hand-operated handle in a movement of the push rod assembly movement-coupled slide 182 is a slide control 187. This includes a slide slot 188 on the slider 182 and a engaging in the slide slot 188 control pin 189, in turn to the wing-side push rod assembly is mounted. The link slot 188 has two rectilinear in the direction of the wing rotation axis 4 extending end portions 190, 191 and an angle between them 192 lying.

Die Beschlaganordnung 106 ist zur Verlagerung der Flügeldrehachse 4 quer zu der Hauptebene des festen Rahmens 2 bei Schließlage des Flügels 3 zu betätigen. Erfolgt diese Betätigung etwa mittels eines herkömmlichen Schaltgetriebes mit Handbetätigungsgriff und den üblichen Griffstellungen, so ist der horizontalen Griffstellung der in den Fign. 31 und 32 dargestellte Zustand der Beschlagschere 107 zugeordnet. Bei dieser Griffstellung ist die Flügeldrehachse 4 maximal gegenüber dem festen Rahmen 2 abgestellt. Der Flügel 3 kann folglich drehgeöffnet werden, ohne dass Kollisionen zwischen dem Flügelüberschlag 31 und dem festen Rahmen 2 zu befürchten wären.The fitting assembly 106 is to actuate the displacement of the wing pivot axis 4 transversely to the main plane of the fixed frame 2 in the closed position of the wing 3. If this operation takes place approximately by means of a conventional manual transmission with a manual operating handle and the usual gripping positions, then the horizontal gripping position of FIG. 31 and 32 illustrated state of the fitting shears 107 assigned. In this handle position, the wing pivot axis 4 is turned off at the maximum relative to the fixed frame 2. The wing 3 can consequently be rotationally opened without the risk of collisions between the wing flap 31 and the fixed frame 2.

Die Fign. 33, 34 zeigen die Beschlaganordnung 106 bei schließverriegeltem Flügel 3. Ausgehend von den Verhältnissen gemäß den Fign. 31, 32 wurde der Steuerzapfen 189 der Kulissensteuerung 187 durch die griffgesteuerte Schubstangenanordnung in dem Kulissenschlitz 188 nach unten bewegt. Von der Abwinkelung 192 kommend ist der Steuerzapfen 189 in den unteren Endabschnitt 191 des Kulissenschlitzes 188 eingelaufen. Damit verbunden war eine Querverschiebung des Schiebers 182 gegenüber Fig. 32 nach rechts. Mit dieser Querverschiebung des Schiebers 182 einher ging eine Hubbewegung der Drehlagerhülse 116. Infolge der dadurch bewirkten Bewegung der Drehlagerhülse 116 gegenüber der Drehlagerhülse.118 in Richtung der Flügeldrehachse 4 wurde die Beschlagschere 107 maximal geöffnet. Die Flügeldrehachse 4 wurde folglich in Querrichtung der Hauptebene des festen Rahmens 2 an diesen herangezogen. An der Schubstangenanordnung angebrachte Riegelzapfen gelangten mit festrahmenseitigeh Schließblechen in Eingriff. Der Betätigungsgriff der Schubstangenanordnung zeigt vertikal nach unten.The Fign. 33, 34 show the fitting arrangement 106 in the case of the locked-in wing 3. Starting from the relationships according to FIGS. 31, 32, the control pin 189 of the link control 187 was moved by the handle-controlled push rod assembly in the link slot 188 down. Coming from the bend 192, the control pin 189 has run into the lower end portion 191 of the guide slot 188. This was associated with a transverse displacement of the slider 182 with respect to FIG. 32 to the right. With this transverse displacement of the slider 182 was accompanied by a lifting movement of the rotary bearing sleeve 116. As a result of the caused movement of the rotary bearing sleeve 116 relative to the Drehlagerhülse.118 in the direction of the wing axis 4, the fitting shears 107 was opened maximum. The wing rotation axis 4 was thus used in the transverse direction of the main plane of the fixed frame 2 to this. Attached to the push rod assembly locking pins came with festrahmenseitigeh striking plates in engagement. The operating handle of the push rod assembly points vertically downwards.

Die Fign. 35 und 36 zeigen den Kippbereitschaftszustand des Flügels 3. Gegenüber den Verhältnissen nach den Fign. 31 und 32 wurde der Handbetätigungsgriff der Schübstangenanordnung in eine vertikal nach oben zeigende Position gedreht. Infolgedessen bewegte sich der Steuerzapfen 189 in dem Kulissenschlitz 188 der Kulissensteuerung 187 in den oberen Endabschnitt 190 des Kulissenschlitzes 188. Auch damit war gegenüber Fig. 32 eine Querverschiebung des Schiebers 182 nach rechts verbunden. Die Drehlagerhülse 116 wurde nach oben verschoben, die Beschlagschere 107 maximal geöffnet. Anders als in dem Betriebszustand gemäß den Fign. 33, 34 ist im Falle der Verhältnisse nach den Fign. 35, 36 der Flügel 3 zum Kippöffnen entriegelt. Ein nicht im Einzelnen gezeigtes Kipplager zwischen dem Flügel 3 und dem festen Rahmen 2 ist wirksam.The Fign. FIGS. 35 and 36 show the tilt standby state of the wing 3. Compared with the relationships shown in FIGS. 31 and 32, the handle of the push bar assembly has been rotated to a vertically upwardly facing position. As a result, the control pin 189 moved in the cam slot 188 of the link control 187 in the upper end portion 190 of the cam slot 188. Also with respect to FIG. 32, a transverse displacement of the slider 182 was connected to the right. The rotary bearing sleeve 116 has been moved upwards, the fitting shears 107 are opened to the maximum. Unlike in the operating state according to FIGS. 33, 34 is in the case of the ratios according to FIGS. 35, 36 of the wing 3 unlocked to tilt open. A not shown in detail tilt bearing between the wing 3 and the fixed frame 2 is effective.

Die Beschlaganordnung 106 bei gekipptem Flügel 3 zeigen die Fign. 37, 38. Auch im Falle der Beschlaganordnung 106 ist sichergestellt, dass der gekippte Flügel 3 kippachsseitig nicht versehentlich gegenüber dem festen Rahmen 2 abgestellt werden kann.The fitting assembly 106 with tilted wing 3 show the Fign. 37, 38. Also in the case of the fitting arrangement 106 it is ensured that the tilted wing 3 on the tipping side can not be turned off accidentally with respect to the fixed frame 2.

Claims (20)

  1. Window or door, having a fixed frame (2) and a sash (3), which is rotatably mounted on the fixed frame (2) at least about one sash axis of rotation (4), as well as having at least one scissor-like fitting assembly (7, 57, 107) between the fixed frame (2) and the sash (3), which fitting assembly includes scissor-like assembly guide means (8, 9; 58, 59; 108, 109) and is disposed with said guide means, in the closed position of the sash (3), in a notch between notch faces (15, 32) of the fixed frame (2) and of the sash (3), the scissor-like assembly guide means (8, 9; 58, 59; 108, 109) being pivotally connected to one another, as well as to the fixed frame (2) and to the sash (3), via pivotal connections (10, 11, 12, 14; 60, 61, 62, 64; 110, 111 112, 114) forming pivotal axes, and the sash (3), by the mutual pivotal movement of the scissor-like assembly guide means (8, 9; 58, 59; 108, 109) about the pivotal axes, being displaceable parallel to the sash axis of rotation (4) transversely relative to the principal plane of the fixed frame (2), characterised in that the scissor-like fitting assembly (7, 57, 107), in the closed position of the sash (3), is disposed with the scissor-like assembly guide means (8, 9; 58, 59; 108, 109) in the notch on the axis of rotation side between notch faces (15, 32) of the fixed frame (2) and of the sash (3), which notch faces are parallel to the axis of rotation, and in that the sash (3), by the mutual pivotal movement of the scissor-like assembly guide means (8, 9; 58, 59; 108, 109), about pivotal axes of the pivotal connections (10, 11, 12, 14; 60, 61, 62, 64; 110, 111, 112, 114) of the scissor-like assembly guide means (8, 9; 58, 59; 108, 109), which pivotal axes extend transversely relative to the notch face (15) of the fixed frame (2) parallel to the axis of rotation, is displaceable parallel to the sash axis of rotation (4) transversely relative to the principal plane of the fixed frame (2).
  2. Window or door according to claim 1, characterised in that at least one scissor-like fitting assembly (7, 57, 107) includes two scissor-like assembly guide means (8, 9; 58, 59; 108, 109), which are pivotally connected to each other via a pivotal connection (10, 50*, 110), and one of which guide means is moreover pivotally connected to the fixed frame (2) and to the sash (3) via pivotal connections (11, 12; 61, 62; 111, 112), and the other guide means is moreover pivotally connected at least to the sash (3) via a pivotal connection (14, 64, 114), and in that the pivotal connections (11, 14; 61, 64; 111, 114) of the scissor-like assembly guide means (8, 9; 58, 59; 108, 109) on the sash side are displaceable relative to one another in a controlled manner in the direction of the sash axis of rotation (4) by means of an actuatable drive.
    * Translator's note
    Presumably the reference numeral "50" is a clerical error for "60" in the German text.
  3. Window or door according to claim 2, characterised in that the drive for the relative displacement of the pivotal connections (11, 14; 61, 64; 111, 114) of the scissor-like assembly guide means (8, 9; 58, 59; 108, 109) on the sash side includes at least two driving elements ( 16, 19; 66, 67; 116, 182) which co-operate with one another, of which driving elements at least one has at least one driving control path (26, 25; 76; 186, 184) which ascends in the direction of the sash axis of rotation (4), and at least one other driving element has at least one control counterpiece which abuts against the driving control path (26, 25; 76; 186, 184), the driving control path (26, 25; 76; 186, 184) and the control counterpiece being displaceable along each other when the drive is actuated and, through the pivotal connections (11, 14; 61, 64; 111, 114) of the scissor-like assembly guide means (8, 9; 58, 59; 108, 109) on the sash side, being displaceable relative to each other in the direction of the sash axis of rotation (4).
  4. Window or door according to claim 2 or 3, characterised in that the drive for the relative displacement of the pivotal connections (11, 14; 61, 64) of the scissor-like assembly guide means (8, 9; 58, 59) on the sash side is actuatable by a rotational movement of the sash (3) about the sash axis of rotation (4).
  5. Window or door according to one of claims 2 to 4, characterised in that the drive for the relative displacement of the pivotal connections (11, 14; 61, 64) of the scissor-like assembly guide means (8, 9; 58, 59) on the sash side has, on one side, at least one driving element (19, 67) which is displaceably coupled to the rotational movement of the sash (3) and, on the other side, at least one driving element (16, 66) which is associated with the pivotal connections (11, 14; 61, 64) of the scissor-like assembly guide means (8, 9; 58, 59) on the sash side, and in that the driving elements (16, 19; 66, 67) on both sides co-operate with one another during the rotational movement of the sash (3), and, in consequence, the pivotal connections (11, 14; 61, 64) of the scissor-like assembly guide means (8, 9; 58, 59) on the sash side are displaceable relative to one another in the direction of the sash axis of rotation (4).
  6. Window or door according to claim 5, characterised in that one of the driving elements (19, 67) coupled to the rotational movement of the sash (3) and one of the driving elements (16, 66) associated with the pivotal connections (11, 14; 61, 64) of the scissor-like assembly guide means (8, 9; 58, 59) on the sash side, have at least one driving control path (26, 76) which ascends in the direction of the sash axis of rotation (4), and the other driving element has at least one control counterpiece which abuts against the driving control path (26, 76), and in that the driving control path (26, 76) and the control counterpiece are displaceable along each other by a rotational movement of the sash (3) and, in consequence, the pivotal connections (11, 14; 61, 64) of the scissor-like assembly guide means (8, 9; 58, 59) on the sash side are displaceable relative to one another in the direction of the sash axis of rotation (4).
  7. Window or door according to claim 5 or 6, characterised in that at least one scissor-like assembly guide means (8, 9; 58, 59) is pivotally connected to the sash (3) via a sash pivot bearing provided with at least one pivot bearing member (16, 18; 66, 68) on the guide means side and at least one pivot bearing member (17, 19; 67, 69) on the sash side, and the pivot bearing member (17, 19; 67, 69) on the sash side has the driving element (19, 67) which is displaceably coupled to the rotational movement of the sash (3), and the pivot bearing member (16, 18; 66, 68) on the guide means side has the driving element (16, 66) associated with the pivotal connections (11, 14; 61, 64) of the scissor-like assembly guide means (8, 9; 58, 59) on the sash side.
  8. Window or door according to one of claims 2 to 7, characterised in that the drive for the relative displacement between the pivotal connections (111, 114) of the scissor-like assembly guide means (108, 109) on the sash side is actuatable by means of a push-rod arrangement, which is displaceably guided on the sash (3) in the direction of the notch periphery.
  9. Window or door according to claim 8, characterised in that the drive for the relative displacement between the pivotal connections (111, 114) of the scissor-like assembly guide means (108, 109) on the sash side has, on one side, at least one driving element (182) which is displaceably coupled to the movement of the push-rod arrangement in the direction of the notch periphery and, on the other side, at least one driving element (116) which is associated with the pivotal connections (111, 114) of the scissor-like assembly guide means (108, 109) on the sash side, and in that the driving elements (182; 116) on both sides co-operate with each other during the movement of the push-rod arrangement in the direction of the notch periphery and, in consequence, the pivotal connections (111, 114) of the scissor-like assembly guide means (108, 109) on the sash side are displaceable relative to each other in the direction of the sash axis of rotation (4).
  10. Window or door according to claim 9, characterised in that, of the driving elements (182) which are displaceably coupled to the movement of the push-rod arrangement in the direction of the notch periphery, and of the driving elements (116) which are associated with the pivotal connections (111, 114) of the scissor-like assembly guide means (108, 109) on the sash side, at least one driving element (116, 182) has a driving control path (186, 184) which ascends in the direction of the sash axis of rotation (4), and the other driving element has at least one control counterpiece which abuts against the driving control path (186, 184), and in that the driving control path (186, 184) and the control counterpiece are displaceable along each other through the movement of the push-rod arrangement in the direction of the notch periphery and, in consequence, the pivotal connections (111, 114) of the scissor-like assembly guide means (108, 109) on the sash side are displaceable relative to each other in the direction of the sash axis of rotation (4).
  11. Window or door according to claim 9 or 10, characterised in that at least one scissor-like assembly guide means (108, 109) is pivotally connected to the sash (3) via a sash pivot bearing provided with at least one pivot bearing member (116, 118) on the guide means side, in that a slide (182), which is displaceably coupled to the connecting rod arrangement, is displaceably guided on the sash (3) in the transverse direction of the sash axis of rotation (4), and in that the pivot bearing member (116, 118) on the guide means side forms the driving element which is associated with the pivotal connections (111, 114) of the scissor-like assembly guide means (108, 109) on the sash slide, and the slide (182) on the sash (3) forms the driving element which is displaceably coupled to the movement of the push-rod arrangement in the direction of the notch periphery.
  12. Window or door according to claim 11, characterised in that the slide (182) is displaceably coupled to the push-rod arrangement via a link control means (187).
  13. Window or door according to one of the preceding claims, characterised in that the sash (3) is mounted on the fixed frame (2) so as to be rotatable about a sash axis of rotation (4) and so as to be tiltable about a sash axis of tilt (5) which extends in the transverse direction of the sash axis of rotation (4), a controllable sash tilt bearing being provided on the rotational opening side of the sash (3), and a fitting arrangement (69, 106) being disposed on the rotational closed side of the sash (3) in the vicinity of the axis of tilt, and an additional fitting arrangement (56) being disposed at a spacing from said arrangement in the transverse direction of the sash axis of tilt (5), remote from the axis of tilt between the fixed frame (2) and the sash (3), at least one of the fitting arrangements (6, 56, 106), preferably the two fitting arrangements (6, 56, 106), including a scissor-like fitting assembly (7, 57, 107), and the fitting arrangement (6, 106) in the vicinity of the axis of tilt and the fitting arrangement (56) remote from the axis of tilt, in a rotary operational state when the sash tilt bearing is ineffective, supporting the sash (3) on the fixed frame (2) in a rotatable manner about the sash axis of rotation (4) and in a displaceable manner parallel to the sash axis of rotation (4) transversely relative to the principal plane of the fixed frame (2), and, to tilt the sash (3) about the sash tilt of axis (5) when the sash tilt bearing is effective, the fitting arrangement (6, 106) in the vicinity of the axis of tilt being at least partially pivotable about the sash axis of tilt (5), and the sash (3) being released at the fitting arrangement (56) remote from the axis of tilt for the tilting movement about the sash axis of tilt (5).
  14. Window or door according to claim 13, characterised in that the scissor-like fitting assembly (7, 107) in the vicinity of the axis of tilt and/or the scissor-like fitting assembly (57) remote from the axis of tilt respectively include two scissor-like assembly guide means (8, 9; 58, 59; 108, 109), which are pivotally connected to each other, the pivotal connections (11, 14; 61, 64; 111, 114) of which guide means on the sash side are displaceable relative to one another in a controlled manner in the direction of the sash axis of rotation (4) by means of an actuatable drive in the rotary operational state of the fitting arrangements (6, 56, 106).
  15. Window or door according to claim 13 or 14, with at least one scissor-like fitting assembly (7, 107) in the vicinity of the axis of tilt, characterised in that, for tilting the sash (3), the pivotal connections (11, 14; 111, 114) on the sash side of the scissor-like assembly guide means (8, 9; 108, 109) of the scissor-like fitting assembly (7, 107) in the vicinity of the axis of tilt are prevented from effecting a relative movement in the transverse direction of the sash axis of tilt (5).
  16. Window or door according to one of claims 13 to 15, with at least one scissor-like fitting assembly (57) remote from the axis of tilt, characterised in that, for tilting the sash (3), said sash is released at the scissor-like fitting assembly (57) remote from the axis of tilt for the tilting movement about the sash axis of tilt (5), in that the pivotal connections (61, 64) on the sash side of the scissor-like guide means (58, 59) of the scissor-like fitting assembly (57) remote from the axis of tilt are released for a relative movement in the transverse direction of the sash axis of tilt (5).
  17. Window or door according to one of claims 13 to 16, with at least one scissor-like fitting assembly (57) remote from the axis of tilt, characterised in that, for tilting the sash (3), said sash is released at the scissor-like fitting assembly (57) remote from the axis of tilt for the tilting movement about the sash axis of tilt (5), in that the scissor-like fitting assembly (57) remote from the axis of tilt is released for a pivotal movement about the axis of tilt (5).
  18. Window or door according to one of claims 13 to 17, with at least one scissor-like fitting assembly (57) remote from the axis of tilt, characterised in that, for the pivotal connections (61, 64) on the sash side of the scissor-like assembly guide means (58, 59) of the scissor-like fitting assembly (57) remote from the axis of tilt, a controllable locking apparatus is provided, by means of which said pivotal connections (61, 64), during the rotation of the sash (3) about the sash axis of rotation (4), can be prevented from effecting a relative movement in the transverse direction of the sash axis of tilt (5), and by means of which, for tilting the sash (3), at least one of the pivotal connections (61, 64) is releasable for a relative movement of the pivotal connections (61, 64) in the transverse direction of the sash axis of tilt (5).
  19. Window or door according to claim 18, with at least one scissor-like fitting assembly (57) remote from the axis of tilt, characterised in that the locking apparatus for the pivotal connections (61, 64) on the sash side of the scissor-like assembly guide means (58, 59) of the scissor-like fitting assembly (57) remote from the axis of tilt is controllable by a rotational movement of the sash (3) about the sash axis of rotation (4) and, when the sash (3) assumes the closed position, said locking apparatus releases at least one of the pivotal connections (61, 64) for a relative movement of the pivotal connections (61, 64) in the transverse direction of the sash axis of tilt (5).
  20. Window or door according to claim 18 or 19, with at least one scissor-like fitting assembly (57) remote from the axis of tilt, characterised in that the locking apparatus for the pivotal connections (61, 64) on the sash side of the scissor-like assembly guide means (58, 59) of the scissor-like fitting assembly (57) remote from the axis of tilt has, on at least one of the scissor-like assembly guide means (58, 59) and on the sash (3), at least one locking pin (75, 81) at one end and at least one slot-like pin receiving means (74, 79) at the other end, the locking pin (75, 81) and the pin receiving means (74, 79) being displaceable relative to each other in the longitudinal direction of the pin receiving means (74, 79) during the rotation of the sash (3) about the sash axis of rotation (4), and the locking pin (75, 81) lying opposite a through-aperture (77, 80) in a lateral wall of the pin receiving means (74, 79) when the sash (3) is in the closed position, and, extending therefrom, the locking pin (75, 81) being displaceable out of the pin receiving means (74, 79) during the relative movement of the pivotal connections (61, 64) in the transverse direction of the sash axis of tilt (5).
EP03026856A 2003-11-22 2003-11-22 Window or door with at least a concealed scissor-type fitting between a fixed frame and a wing Expired - Lifetime EP1533457B1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
AT03026856T ATE335114T1 (en) 2003-11-22 2003-11-22 WINDOW OR DOOR WITH AT LEAST ONE CONCEALED FITTING BAR BETWEEN A FIXED FRAME AND A SINGLE
EP03026856A EP1533457B1 (en) 2003-11-22 2003-11-22 Window or door with at least a concealed scissor-type fitting between a fixed frame and a wing
DE50304498T DE50304498D1 (en) 2003-11-22 2003-11-22 Window or door with at least one concealed fitting shears between a fixed frame and a wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03026856A EP1533457B1 (en) 2003-11-22 2003-11-22 Window or door with at least a concealed scissor-type fitting between a fixed frame and a wing

Publications (2)

Publication Number Publication Date
EP1533457A1 EP1533457A1 (en) 2005-05-25
EP1533457B1 true EP1533457B1 (en) 2006-08-02

Family

ID=34429420

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03026856A Expired - Lifetime EP1533457B1 (en) 2003-11-22 2003-11-22 Window or door with at least a concealed scissor-type fitting between a fixed frame and a wing

Country Status (3)

Country Link
EP (1) EP1533457B1 (en)
AT (1) ATE335114T1 (en)
DE (1) DE50304498D1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004009167A1 (en) * 2004-02-25 2005-09-15 Aug. Winkhaus Gmbh & Co. Kg Window or door
DE202010012004U1 (en) * 2010-08-31 2011-12-28 Maco Technologie Gmbh Load transfer for windows, doors or the like

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1193204A (en) * 1916-08-01 William coleman
DE3442364C1 (en) * 1984-11-20 1991-01-24 Hautau Gmbh W Rebate-concealed fitting for tilt-and-pivot casement windows or doors
DE3829053C2 (en) * 1988-08-26 1994-02-17 Winkhaus Fa August Turn fittings or turn-tilt fittings for windows, doors or the like
DE9000152U1 (en) * 1990-01-09 1990-03-15 August Bilstein GmbH & Co KG, 5828 Ennepetal Lower corner bearing for pivoting, especially tilt/turn windows, doors, etc.

Also Published As

Publication number Publication date
ATE335114T1 (en) 2006-08-15
DE50304498D1 (en) 2006-09-14
EP1533457A1 (en) 2005-05-25

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