EP1122389B1 - Pull-in device for moving a wing - Google Patents

Pull-in device for moving a wing Download PDF

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Publication number
EP1122389B1
EP1122389B1 EP00127750A EP00127750A EP1122389B1 EP 1122389 B1 EP1122389 B1 EP 1122389B1 EP 00127750 A EP00127750 A EP 00127750A EP 00127750 A EP00127750 A EP 00127750A EP 1122389 B1 EP1122389 B1 EP 1122389B1
Authority
EP
European Patent Office
Prior art keywords
pull
edge
wing
tightening
frame
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
EP00127750A
Other languages
German (de)
French (fr)
Other versions
EP1122389A2 (en
EP1122389A3 (en
Inventor
Dieter Renz
André Wulfert
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.)
Aug Winkhaus GmbH and Co KG
Original Assignee
Aug Winkhaus GmbH and Co KG
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Filing date
Publication date
Application filed by Aug Winkhaus GmbH and Co KG filed Critical Aug Winkhaus GmbH and Co KG
Publication of EP1122389A2 publication Critical patent/EP1122389A2/en
Publication of EP1122389A3 publication Critical patent/EP1122389A3/en
Application granted granted Critical
Publication of EP1122389B1 publication Critical patent/EP1122389B1/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
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C9/00—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing
    • E05C9/18—Details of fastening means or of fixed retaining means for the ends of bars
    • E05C9/1825—Fastening means
    • E05C9/1833—Fastening means performing sliding movements
    • E05C9/185—Fastening means performing sliding movements parallel with actuating bar
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B17/00—Accessories in connection with locks
    • E05B17/0025—Devices for forcing the wing firmly against its seat or to initiate the opening of the wing
    • E05B17/0029—Devices for forcing the wing firmly against its seat or to initiate the opening of the wing motor-operated
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B47/00—Operating or controlling locks or other fastening devices by electric or magnetic means
    • E05B47/0001—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof
    • E05B2047/0014—Constructional features of actuators or power transmissions therefor
    • E05B2047/0015—Output elements of actuators
    • E05B2047/0016—Output elements of actuators with linearly reciprocating motion
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B47/00—Operating or controlling locks or other fastening devices by electric or magnetic means
    • E05B47/0001—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof
    • E05B47/0012—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof with rotary electromotors
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C9/00—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing
    • E05C9/18—Details of fastening means or of fixed retaining means for the ends of bars
    • E05C9/1808—Keepers
    • 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
    • E05D15/5205—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis with horizontally-extending checks
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F15/00—Power-operated mechanisms for wings
    • E05F15/60—Power-operated mechanisms for wings using electrical actuators
    • E05F15/603—Power-operated mechanisms for wings using electrical actuators using rotary electromotors
    • E05F15/611—Power-operated mechanisms for wings using electrical actuators using rotary electromotors for swinging wings
    • E05F15/63—Power-operated mechanisms for wings using electrical actuators using rotary electromotors for swinging wings operated by swinging arms
    • 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 tightening device for moving a wing in the closed position against a frame with a suitably arranged on a first spar skirt, with a pivotable on a relative to the first spar Holm suit part and means for moving the tightening part in the mounted state along its spar to Schugreifung the suit edge, wherein the suit edge is inclined relative to the direction of movement of the tightening part in the closed position.
  • the DE 3719040 discloses such a tightening device.
  • the tightening edge is arranged on a frame-fixed closing latch.
  • the wing has a locking pin attached to a drive rod of a drive rod fitting.
  • the lock pin comes against the suit edge and slides along it.
  • the wing is pulled against the frame.
  • the locking pin thus serves as a suit part. Subsequently, the locking pin can penetrate into the latch and lock the wing to the frame.
  • a disadvantage of the known tightening device is that they only abut the wing in a directly on the frame Position against the frame. Since the suit edge may not hinder the movement of the wing, its length is naturally limited to the dimensions of the spar of the frame.
  • a tightening device without a suit edge in which a pivoting arm is arranged on a faceplate of an intended for locking the wing to the frame espagnolette fitting.
  • the faceplate has along its longest Siegrekkung an angled, designed as a slot control cam for receiving a connected to a drive rod, the swivel arm-driving sliding block.
  • Upon movement of the drive rod in the wing locking direction of the sliding block pivots the swivel arm. This engages behind the suit part and pulls the wing against the frame.
  • a disadvantage of the known tightening device is that the control of the movement of the swing arm designed very complex and prone to failure.
  • the invention is based on the problem, a tightening device of the type mentioned in such a way that it allows movement of the frame with at least a small distance opposite wing and structurally particularly simple design.
  • the tightening edge is at least partially disposed on a movable tightening element and that the tightening element in the open position of the wing in a protruding, in the assembled state his Holm superior position and in the closed position of the wing in a retracted, in the region of his spar located position is located.
  • the suit edge can protrude in the open position of the wing over the respective spar and tighten the distance standing in front of the frame wings.
  • the blade moves against the frame, at least the portion of the tightening edge projecting beyond the spar is moved to the retracted position. Subsequently, the wing can be easily locked with the frame.
  • the tightening device according to the invention does not require a guide curve with a sliding sliding along sliding block and is therefore particularly susceptible to interference.
  • the tightening device according to the invention also structurally particularly simple.
  • the tightening device according to the invention is also particularly compact.
  • the susceptibility to failure of the tightening device according to the invention is particularly advantageous when used on motorized tilting and to be locked wings advantageous because no pressure forces are exerted by hand on the wing.
  • the tightening part can be fastened on the drive rod like the locking pin of the known tightening device. As a result, the movement of the tightening part requires no additional construction effort, since the drive rod is driven anyway when opening, closing and locking the wing.
  • the tightening element is provided for arrangement on the frame.
  • the movement of the tightening element is particularly simple according to another advantageous development of the invention and requires a particularly low structural complexity when the tightening element is mounted on a fixed holding part and resiliently biased in its protruding position.
  • the tightening element can move when closing the wing of the wing and therefore can not jam this.
  • the range of movement of the tightening element can be kept particularly low according to another advantageous embodiment of the invention, when the tightening part is provided for closer arrangement to the frame as a movable in a frame-locking latch locking pin of the espagnolette fitting.
  • the tightening element can be particularly easy to assemble according to another advantageous embodiment of the invention, when a holding part of the tightening element is designed with the locking latch as a structural unit. This also allows the tightening element and the latch against the tightening part and the locking pin at the same time align during assembly.
  • the closing latch and the holding part can be made, for example, of cast aluminum component.
  • the suit part is particularly simple in construction according to another advantageous embodiment of the invention, if it is designed sword-shaped.
  • the tightening part can be manufactured in particular as a cost-effective, angled sheet-metal strip.
  • the tightening device requires a particularly small number to be manufactured and assembled components when the tightening part is designed as a locking pin of the espagnolette fitting.
  • the tightening device requires only a single tightening member for moving the wing against the frame and locking the wing when a tightening edge of the locking catch is aligned with the tightening edge of the tightening element in the protruding position, and when a locking edge provided for retaining the tightening part in the closed position the closing latch is arranged outside the movement range of the tightening element.
  • Trained as a locking pin tightening part is performed particularly reliable behind the locking edge according to another advantageous embodiment of the invention, when portions of the tightening edge of the latch and located in the protruding position of the tightening suit of the tightening element are arranged side by side.
  • the tightening part can first move against the tightening edge of the tightening element during its movement along the spar of the wing. From this suit edge the suit part slides into the sub-area of the adjoining suit edges to behind the locking edge. Subsequently, the tightening element can move to its retracted position and allow the locking of the wing.
  • a suit edge of the latch can be avoided according to another advantageous embodiment of the invention, when the tightening edge of the tightening element in the closed position is movable to immediately before the locking edge of the latch.
  • the intended for movement against the tightening edge of the tightening element suit part can according to another advantageous embodiment of the invention particularly evenly along the suit edge when the suit part has a suitably aligned to the tightening edge of the tightening element on running slope.
  • the range of movement of the tightening edge in the direction provided on the wing can be easily limited according to another advantageous embodiment of the invention, when a support arm of the located in the protruding position tightening element is biased against a stop of the holding part.
  • the support arm can also support high forces generated when the tightening part slides over the tightening edge.
  • the control of the movement of the tightening element requires according to another advantageous embodiment of the invention, a particularly low cost when the tightening edge of the tightening element is arranged on a tightening arm and when the tightening arm has a stop for the wing at its free end.
  • FIG. 1 shows a pivotally mounted on a fixed frame 1 wings 2 with a drive rod fitting 3 in a side view.
  • the wing 2 is here in a tilted position.
  • the wing 2 may be, for example, a turn-tilt wing of a window or a French window.
  • the wing 2 may be a pure tilting wing or a ventilation flap.
  • the frame 1 is shown cut in the region of two horizontal bars 4, 5.
  • the wing 2 has a wing flap 6 resting in a tilted position against the frame 1.
  • the sliding rod fitting 3 has a drive rod 7 which is longitudinally movable perpendicular to the drawing plane and which is covered by a face plate 8 fastened to the wing 2.
  • the faceplate 8 in the range of slots 9 penetrating locking pins 10 are attached.
  • a single locking pin 10 is shown in the drawing.
  • the frame 1 has a closing latch 11.
  • the drive rod 7 can be moved by an electric motor drive 13 fastened to a horizontal rail 12 of the blade 2 and shown schematically in the drawing.
  • At its lower part of the wing 2 is connected via a tilting bearing 14 with the frame 1.
  • In the upper part of the wing 2 is held by a stay arm 15 of 16 Ausstellschere.
  • the Ausstellschere 16 is adjusted and the wing 2 is pivoted against the frame 1.
  • the locking pin 10 moves into the latch 11 and locks the wing 2 in the frame first
  • FIG. 2a shows the frame 1 from FIG. 1 In a view perpendicular to the latch 11 with a tightening device 17.
  • the wing 2 here stands opposite the frame 1 with a small distance and is in a position immediately before its locking with the frame 1.
  • the wing flap 6 of the wing 2, the locking pin 10th and a suit part 18 of the tightening device 17 are shown cut here.
  • the tightening device 17 has a tightening element 19 which is pivotably mounted on the frame 1.
  • the tightening part 18, like the locking pin 10, is arranged on the wing 2, and in FIG FIG. 1 illustrated drive rod 7 attached.
  • the tightening element 19 has a tightening arm 20 with a tightening edge 21 and is located in a protruding, the spar 4 of the frame 1 on which it is mounted in the direction of the wing 2 superior position.
  • a spring 22 biases the tightening element 19 in the drawn position, in which it is supported by a support arm 23 to a stop 24.
  • the support arm 23 and the arm 20 are made in one piece and have a common storage 25.
  • the latch 11 and a storage 25 of the tightening element 19 exhibiting holding part 26 are integrally formed and bolted to the frame 1.
  • the locking latch 11 also has a tightening edge 27.
  • the locking pin 10 with the latch 11 and the tightening edge 27 together form substantially known from practice tightening device.
  • the suit part 18 is designed as an angled sheet metal strip and sword-shaped and has a suit edge 21 of the tightening element 19 correspondingly shaped leading edge 28. Furthermore, the tightening part 18 further away from the wing flap 6 of the wing 2 arranged as the inserted into the latch 11 locking pin 10th
  • FIG. 2a shown tightening position of the tightening device 17 is the suit part 18 on the tightening element 19 at.
  • a drive of in FIG. 1 illustrated drive rod 7 by means of the electric motor drive 13 the locking pin 10 and the tightening member 18 move to the right.
  • the directions of movement of the locking pin 10 and the tightening part 18 and the wing flap 6 of the wing 2 are marked with arrows in the drawing.
  • the tightening part 18 slides along the tightening edge 21 of the tightening element 19.
  • the wing 2 is thereby attracted to the frame 1.
  • a middle suit position is in FIG. 2b shown. Compared to the suit position off FIG.
  • FIG. 3a shows a tightening device 31 in which a tightening part 32 is formed as a locking pin.
  • a holding part 33 of a tightening element 34 of the tightening device 31 and a closing catch 35 are designed in one piece.
  • the closing latch 35 has a locking edge 36 and a suiting edge 37 projecting therefrom.
  • the tightening edge 37 is arranged in alignment with a tightening edge 38 of the tightening element 34.
  • the suit edges 37, 38 overlap in a region in which they are partially arranged one above the other.
  • a suit arm 40 of the tightening element 34 made in one piece with a support arm 39 and resiliently biased in the direction of the wing 2.
  • FIG. 4a shows a tightening device 42, in which a single tightening edge 43 is arranged on a tightening element 44.
  • This tightening device 42 can be provided, for example, in conjunction with a suit device known from practice for moving the wing 2.
  • a suit device known from practice for moving the wing 2 is for example in the FIGS. 2a to 2c through the latch 11, the locking pin 10 and the tightening edge 27th shown.
  • the wing 2 is usually with several in the FIGS. 2a to 2c Locks shown 11 locked.
  • the locking enabling position suffice depending on the size of the wing 2 a few in the Figures 3 and 4 illustrated tightening devices 31, 42.
  • the tightening element 44 is substantially like that of the tightening device 17 from FIG. 2a designed.
  • a suit part 45 of the tightening device 42 is designed as a locking pin and can be by means of in FIG. 1 Move shown drive rod 7 to the right until it reaches the suit edge 43. At this suit edge 43, the suit part 45 slides along and pulls the wing 2 to the frame 1.
  • a middle attracting position is in FIG. 4b shown.
  • the suit part 45 passes behind a locking edge 46 of a latch 47 and holds the wing 2 on the frame 1.
  • This tightening position is in Figure 4c shown.
  • the wing of the in FIG. 2 shown suit edge 27 of the latch 11 moves.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Closing And Opening Devices For Wings, And Checks For Wings (AREA)
  • Mechanical Pencils And Projecting And Retracting Systems Therefor, And Multi-System Writing Instruments (AREA)
  • Details Of Spanners, Wrenches, And Screw Drivers And Accessories (AREA)
  • Basic Packing Technique (AREA)

Abstract

The pull-in arrangement (17) consists of a pull-to edge (21) with a pull-to part (18) positioned on the first frame (1) strut. At least part of the pull-to edge is positioned on a movable pull-to element (19) which, when the casement (2) or leaf is open, protrudes beyond the frame-strut (4). When the casement or leaf is closed, the pull-to element is in a retracted position in relation to the frame-strut.

Description

Die Erfindung betrifft eine Anzugseinrichtung zur Bewegung eines Flügels in Schließstellung gegen einen Rahmen mit einer an einem ersten Holm anzuordnenden Anzugskante, mit einem an einem gegenüber dem ersten Holm schwenkbaren Holm anzuordnenden Anzugsteil und mit Mitteln zur Bewegung des Anzugsteils im montierten Zustand längs seines Holms zur Hintergreifung der Anzugskante, wobei die Anzugskante gegenüber der Bewegungsrichtung des Anzugsteils in Schließstellung geneigt angeordnet ist.The invention relates to a tightening device for moving a wing in the closed position against a frame with a suitably arranged on a first spar skirt, with a pivotable on a relative to the first spar Holm suit part and means for moving the tightening part in the mounted state along its spar to Hintergreifung the suit edge, wherein the suit edge is inclined relative to the direction of movement of the tightening part in the closed position.

Die DE 3719040 offenbart eine solche Anzugseinrichtung.The DE 3719040 discloses such a tightening device.

Solche Anzugseinrichtungen werden in der Praxis häufig eingesetzt und sind damit bekannt. Im einfachsten Fall der Anzugseinrichtung ist die Anzugskante auf einer rahmenfesten Schließfalle angeordnet. Der Flügel hat einen auf einer Treibstange eines Treibstangenbeschlages befestigten Schließzapfen. Bei einem Schließen wird der Flügel zunächst in eine an dem Rahmen anliegende Stellung bewegt und anschließend die Treibstange angetrieben. Dabei gelangt der Schließzapfen gegen die Anzugskante und gleitet an dieser entlang. Hierbei wird der Flügel gegen den Rahmen gezogen. Der Schließzapfen dient damit als Anzugsteil. Anschließend kann der Schließzapfen in die Schließfalle eindringen und den Flügel mit dem Rahmen verriegeln. Diese Gestaltung der Anzugseinrichtung ist besonders einfach aufgebaut und kostengünstig herstellbar.Such tightening devices are often used in practice and are known. In the simplest case of the tightening device, the tightening edge is arranged on a frame-fixed closing latch. The wing has a locking pin attached to a drive rod of a drive rod fitting. When closing the wing is first moved to a position adjacent to the frame and then driven the drive rod. The lock pin comes against the suit edge and slides along it. Here, the wing is pulled against the frame. The locking pin thus serves as a suit part. Subsequently, the locking pin can penetrate into the latch and lock the wing to the frame. This design of the tightening device is particularly simple and inexpensive to produce.

Nachteilig bei der bekannten Anzugseinrichtung ist, daß sie den Flügel nur in einer unmittelbar an dem Rahmen anliegenden Stellung gegen den Rahmen ziehen kann. Da die Anzugskante die Bewegung des Flügels nicht behindern darf, ist deren Länge naturgemäß auf die Abmessungen des Holms des Rahmens begrenzt.A disadvantage of the known tightening device is that they only abut the wing in a directly on the frame Position against the frame. Since the suit edge may not hinder the movement of the wing, its length is naturally limited to the dimensions of the spar of the frame.

Weiterhin ist aus der FR 24 20 634 eine Anzugseinrichtung ohne Anzugskante bekannt, bei der ein Schwenkarm auf einer Stulpschiene eines zur Verriegelung des Flügels an dem Rahmen vorgesehenen Treibstangenbeschlages angeordnet ist. Die Stulpschiene hat längs seiner längsten Erstrekkung eine abgewinkelte, als Langloch ausgebildete Steuerkurve zur Aufnahme eines mit einer Treibstange verbundenen, den Schwenkarm ansteuernden Kulissensteins. Bei einer Bewegung der Treibstange in die den Flügel verriegelnde Richtung verschwenkt der Kulissenstein den Schwenkarm. Dieser hintergreift das Anzugsteil und zieht damit den Flügel gegen den Rahmen. Nachteilig bei der bekannten Anzugseinrichtung ist, daß sich die Steuerung der Bewegung des Schwenkarms sehr aufwendig und störanfällig gestaltet.Furthermore, from the FR 24 20 634 a tightening device without a suit edge is known, in which a pivoting arm is arranged on a faceplate of an intended for locking the wing to the frame espagnolette fitting. The faceplate has along its longest Erstrekkung an angled, designed as a slot control cam for receiving a connected to a drive rod, the swivel arm-driving sliding block. Upon movement of the drive rod in the wing locking direction of the sliding block pivots the swivel arm. This engages behind the suit part and pulls the wing against the frame. A disadvantage of the known tightening device is that the control of the movement of the swing arm designed very complex and prone to failure.

Aus der DE 195 15 708 A1 ist eine Anzugseinrichtung bekannt geworden, bei der die Steuerkurve in einer Zwischenplatte angeordnet ist. Hierdurch läßt sich der Schwenkarm um einen großen Winkelbereich verschwenken. Nachteilig ist jedoch hierbei die sehr aufwendige Gestaltung der Steuerkurve und die hohe Anzahl der zu montierenden und zu fertigenden Bauteile. Hierdurch gestaltet sich diese Anzugseinrichtung ebenfalls besonders aufwendig und störanfällig.From the DE 195 15 708 A1 is a tightening device has become known, in which the control cam is arranged in an intermediate plate. As a result, the swivel arm can be pivoted about a large angular range. However, the disadvantage here is the very complex design of the control curve and the high number of components to be assembled and manufactured. As a result, this tightening device also designed particularly complex and prone to failure.

Der Erfindung liegt das Problem zugrunde, eine Anzugseinrichtung der eingangs genannten Art so weiterzubilden, daß sie eine Bewegung des dem Rahmen mit zumindest geringem Abstand gegenüberstehenden Flügels ermöglicht und konstruktiv besonders einfach aufgebaut ist.The invention is based on the problem, a tightening device of the type mentioned in such a way that it allows movement of the frame with at least a small distance opposite wing and structurally particularly simple design.

Dieses Problem wird erfindungsgemäß dadurch gelöst, daß die Anzugskante zumindest teilweise auf einem beweglichen Anzugselement angeordnet ist und daß das Anzugselement in Offenstellung des Flügels in einer hervorstehenden, im montierten Zustand seinen Holm überragenden Stellung und in Schließstellung des Flügels in einer zurückgezogenen, im Bereich seines Holms befindlichen Stellung angeordnet ist.This problem is inventively solved in that the tightening edge is at least partially disposed on a movable tightening element and that the tightening element in the open position of the wing in a protruding, in the assembled state his Holm superior position and in the closed position of the wing in a retracted, in the region of his spar located position is located.

Durch diese Gestaltung kann die Anzugskante in Offenstellung des Flügels über den jeweiligen Holm hinausragen und den mit Abstand vor dem Rahmen stehenden Flügel anziehen. Bei der Bewegung des Flügels gegen den Rahmen wird zumindest der den Holm überragende Bereich der Anzugskante in die zurückgezogene Stellung bewegt. Anschließend läßt sich der Flügel mit dem Rahmen einfach verriegeln. Die erfindungsgemäße Anzugseinrichtung benötigt keine Führungskurve mit einem darin entlanggleitenden Kulissenstein und ist daher besonders störungsunanfällig. Hierdurch gestaltet sich die erfindungsgemäße Anzugseinrichtung zudem konstruktiv besonders einfach. Die erfindungsgemäße Anzugseinrichtung ist zudem besonders kompakt aufgebaut. Die Störungsunanfälligkeit der erfindungsgemäßen Anzugseinrichtung ist insbesondere bei einem Einsatz an motorisch zu kippenden und zu verriegelnden Flügeln von Vorteil, da hier keine Druckkräfte von Hand auf den Flügel ausgeübt werden. Das Anzugsteil kann wie der Schließzapfen der bekannten Anzugseinrichtung auf der Treibstange befestigt sein. Hierdurch erfordert die Bewegung des Anzugsteils keinen zusätzlichen baulichen Aufwand, da die Treibstange beim Öffnen, Schließen und Verriegeln des Flügels ohnehin angetrieben wird.By this design, the suit edge can protrude in the open position of the wing over the respective spar and tighten the distance standing in front of the frame wings. As the blade moves against the frame, at least the portion of the tightening edge projecting beyond the spar is moved to the retracted position. Subsequently, the wing can be easily locked with the frame. The tightening device according to the invention does not require a guide curve with a sliding sliding along sliding block and is therefore particularly susceptible to interference. As a result, the tightening device according to the invention also structurally particularly simple. The tightening device according to the invention is also particularly compact. The susceptibility to failure of the tightening device according to the invention is particularly advantageous when used on motorized tilting and to be locked wings advantageous because no pressure forces are exerted by hand on the wing. The tightening part can be fastened on the drive rod like the locking pin of the known tightening device. As a result, the movement of the tightening part requires no additional construction effort, since the drive rod is driven anyway when opening, closing and locking the wing.

Zur weiteren Verringerung des baulichen Aufwands der erfindungsgemäßen Anzugseinrichtung trägt es bei, wenn das Anzugselement zur Anordnung an dem Rahmen vorgesehen ist.To further reduce the structural complexity of the tightening device according to the invention, it is helpful if the tightening element is provided for arrangement on the frame.

Die Bewegung des Anzugselementes gestaltet sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders einfach und erfordert einen besonders geringen baulichen Aufwand, wenn das Anzugselement auf einem feststehenden Halteteil gelagert und federelastisch in seine hervorstehende Stellung vorgespannt ist. Durch diese Gestaltung läßt sich das Anzugselement beim Schließen des Flügels von dem Flügel bewegen und kann diesen daher nicht verklemmen.The movement of the tightening element is particularly simple according to another advantageous development of the invention and requires a particularly low structural complexity when the tightening element is mounted on a fixed holding part and resiliently biased in its protruding position. By this design, the tightening element can move when closing the wing of the wing and therefore can not jam this.

Der Bewegungsbereich des Anzugselementes läßt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders gering halten, wenn das Anzugsteil zur näheren Anordnung zum Rahmen hin vorgesehen ist als ein in eine rahmenfeste Schließfalle bewegbarer Schließzapfen des Treibstangenbeschlages.The range of movement of the tightening element can be kept particularly low according to another advantageous embodiment of the invention, when the tightening part is provided for closer arrangement to the frame as a movable in a frame-locking latch locking pin of the espagnolette fitting.

Das Anzugselement läßt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders einfach montieren, wenn ein Halteteil des Anzugselementes mit der Schließfalle als bauliche Einheit gestaltet ist. Hierdurch lassen sich zudem das Anzugselement und die Schließfalle gegenüber dem Anzugsteil und dem Schließzapfen bei der Montage gleichzeitig ausrichten. Die Schließfalle und das Halteteil können beispielsweise aus gegossenem Aluminiumbauteil gefertigt sein.The tightening element can be particularly easy to assemble according to another advantageous embodiment of the invention, when a holding part of the tightening element is designed with the locking latch as a structural unit. This also allows the tightening element and the latch against the tightening part and the locking pin at the same time align during assembly. The closing latch and the holding part can be made, for example, of cast aluminum component.

Das Anzugsteil ist gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders einfach aufgebaut, wenn es schwertförmig gestaltet ist. Hierdurch kann das Anzugsteil insbesondere als kostengünstigen, abgewinkelten Blechstreifen gefertigt sein.The suit part is particularly simple in construction according to another advantageous embodiment of the invention, if it is designed sword-shaped. As a result, the tightening part can be manufactured in particular as a cost-effective, angled sheet-metal strip.

Die Anzugseinrichtung erfordert eine besonders geringe Anzahl zu fertigender und zu montierender Bauteile, wenn das Anzugsteil als Schließzapfen des Treibstangenbeschlages ausgebildet ist.The tightening device requires a particularly small number to be manufactured and assembled components when the tightening part is designed as a locking pin of the espagnolette fitting.

Die Anzugseinrichtung erfordert nur ein einziges Anzugsteil zur Bewegung des Flügels gegen den Rahmen und zur Verriegelung des Flügels, wenn eine Anzugskante der Schließfalle fluchtend zu der Anzugskante des in der hervorstehenden Stellung befindlichen Anzugselementes angeordnet ist, und wenn eine zur Halterung des Anzugsteils in Schließstellung vorgesehene Verriegelungskante der Schließfalle außerhalb des Bewegungsbereichs des Anzugselementes angeordnet ist.The tightening device requires only a single tightening member for moving the wing against the frame and locking the wing when a tightening edge of the locking catch is aligned with the tightening edge of the tightening element in the protruding position, and when a locking edge provided for retaining the tightening part in the closed position the closing latch is arranged outside the movement range of the tightening element.

Das als Schließzapfen ausgebildete Anzugsteil wird gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders zuverlässig hinter die Verriegelungskante geführt, wenn Teilbereiche der Anzugskante der Schließfalle und der in der hervorstehenden Stellung befindlichen Anzugskante des Anzugselementes nebeneinander angeordnet sind. Hierdurch kann das Anzugsteil bei seiner Bewegung entlang des Holms des Flügels zunächst gegen die Anzugskante des Anzugselementes gelangen. Von dieser Anzugskante gleitet das Anzugsteil in den Teilbereich der nebeneinander angeordneten Anzugskanten bis hinter die Verriegelungskante. Anschließend kann sich das Anzugselement in seine zurückgezogene Stellung bewegen und die Verriegelung des Flügels ermöglichen.Trained as a locking pin tightening part is performed particularly reliable behind the locking edge according to another advantageous embodiment of the invention, when portions of the tightening edge of the latch and located in the protruding position of the tightening suit of the tightening element are arranged side by side. In this way, the tightening part can first move against the tightening edge of the tightening element during its movement along the spar of the wing. From this suit edge the suit part slides into the sub-area of the adjoining suit edges to behind the locking edge. Subsequently, the tightening element can move to its retracted position and allow the locking of the wing.

Eine Anzugskante der Schließfalle läßt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung vermeiden, wenn die Anzugskante des Anzugselementes in Schließstellung bis unmittelbar vor die Verriegelungskante der Schließfalle bewegbar ist.A suit edge of the latch can be avoided according to another advantageous embodiment of the invention, when the tightening edge of the tightening element in the closed position is movable to immediately before the locking edge of the latch.

Das zur Bewegung gegen die Anzugskante des Anzugselementes vorgesehene Anzugsteil vermag gemäß einer anderen vorteilhaften Weiterbildung der Erfindung besonders gleichmäßig an der Anzugskante entlangzugleiten, wenn das Anzugsteil eine entsprechend der Anzugskante des Anzugselementes ausgerichtete Auf lauf schräge hat.The intended for movement against the tightening edge of the tightening element suit part can according to another advantageous embodiment of the invention particularly evenly along the suit edge when the suit part has a suitably aligned to the tightening edge of the tightening element on running slope.

Der Bewegungsbereich der Anzugskante in die auf den Flügel vorgesehene Richtung läßt sich gemäß einer anderen vorteilhaften Weiterbildung der Erfindung einfach begrenzen, wenn ein Abstützarm des in der hervorstehenden Stellung befindlichen Anzugselementes gegen einen Anschlag des Halteteils vorgespannt ist. Der Abstützarm kann zudem hohe, beim Gleiten des Anzugsteiles über die Anzugskante erzeugte Kräfte abstützen.The range of movement of the tightening edge in the direction provided on the wing can be easily limited according to another advantageous embodiment of the invention, when a support arm of the located in the protruding position tightening element is biased against a stop of the holding part. The support arm can also support high forces generated when the tightening part slides over the tightening edge.

Die Steuerung der Bewegung des Anzugselementes erfordert gemäß einer anderen vorteilhaften Weiterbildung der Erfindung einen besonders geringen Aufwand, wenn die Anzugskante des Anzugselementes auf einem Anzugsarm angeordnet ist und wenn der Anzugsarm an seinem freien Ende einen Anschlag für den Flügel hat.The control of the movement of the tightening element requires according to another advantageous embodiment of the invention, a particularly low cost when the tightening edge of the tightening element is arranged on a tightening arm and when the tightening arm has a stop for the wing at its free end.

Die Erfindung läßt zahlreiche Ausführungsformen zu. Zur weiteren Verdeutlichung ihres Grundprinzips sind drei davon in der Zeichnung dargestellt und werden nachfolgend beschrieben. Diese zeigt in

Fig.1
eine schematische Seitenansicht im Teilschnitt eines gegen einen Rahmen schwenkbaren Flügels mit einem Treibstangenbeschlag,
Fig.2a - 2c
eine erfindungsgemäße Anzugseinrichtung für den Flügel aus Figur 1 in verschiedenen Anzugsstellungen des Flügels,
Fig.3a - 3c
eine weitere Ausführungsform der erfindungsgemäßen Anzugseinrichtung in verschiedenen Anzugsstellungen des Flügels,
Fig.4a - 4c
eine weitere Ausführungsform der erfindungsgemäßen Anzugseinrichtung in verschiedenen Anzugsstellungen des Flügels.
The invention allows numerous embodiments. To further clarify its basic principle, three of them are shown in the drawing and will be described below. This shows in
Fig.1
1 is a schematic side view in partial section of a wing pivotable against a frame with a drive rod fitting,
Fig.2a - 2c
a tightening device according to the invention for the wing FIG. 1 in different positions of the wing,
Fig.3a - 3c
a further embodiment of the tightening device according to the invention in different tightening positions of the wing,
Fig.4a - 4c
a further embodiment of the tightening device according to the invention in different tightening positions of the wing.

Figur 1 zeigt einen an einem feststehenden Rahmen 1 schwenkbar gelagerten Flügel 2 mit einem Treibstangenbeschlag 3 in einer Seitenansicht. Der Flügel 2 befindet sich hier in einer gekippten Stellung. Bei dem Flügel 2 kann es sich beispielsweise um einen Dreh-Kippflügel eines Fensters oder einer Fenstertür handeln. Ebenso kann der Flügel 2 ein reiner Kipp-Flügel oder eine Lüftungsklappe sein. Der Rahmen 1 ist im Bereich zweier horizontaler Holme 4, 5 geschnitten dargestellt. Der Flügel 2 hat einen in einer gegen den Rahmen 1 gekippten Stellung anliegenden Flügelüberschlag 6. Der Treibstangenbeschlag 3 weist eine senkrecht zur Zeichenebene längsbewegliche Treibstange 7 auf, welche von einer auf dem Flügel 2 befestigten Stulpschiene 8 abgedeckt wird. Auf der Treibstange 7 sind die Stulpschiene 8 im Bereich von Langlöchern 9 durchdringende Schließzapfen 10 befestigt. Beispielhaft ist in der Zeichnung nur ein einziger Schließzapfen 10 dargestellt. Im dem Schließzapfen 10 gegenüberstehenden Bereich hat der Rahmen 1 eine Schließfalle 11. Die Treibstange 7 läßt sich von einem auf einem horizontalen Holm 12 des Flügels 2 befestigten und in der Zeichnung schematisch dargestellten elektromotorischen Antrieb 13 bewegen. An seinem unteren Bereich ist der Flügel 2 über ein Kipplager 14 mit dem Rahmen 1 verbunden. Im oberen Bereich wird der Flügel 2 von einem Ausstellarm 15 einer Ausstellschere 16 gehalten. Bei einem Antrieb der Treibstange 7 wird die Ausstellschere 16 verstellt und der Flügel 2 gegen den Rahmen 1 geschwenkt. Bei einem weiteren Antrieb bewegt sich der Schließzapfen 10 in die Schließfalle 11 und verriegelt den Flügel 2 in dem Rahmen 1. FIG. 1 shows a pivotally mounted on a fixed frame 1 wings 2 with a drive rod fitting 3 in a side view. The wing 2 is here in a tilted position. The wing 2 may be, for example, a turn-tilt wing of a window or a French window. Likewise, the wing 2 may be a pure tilting wing or a ventilation flap. The frame 1 is shown cut in the region of two horizontal bars 4, 5. The wing 2 has a wing flap 6 resting in a tilted position against the frame 1. The sliding rod fitting 3 has a drive rod 7 which is longitudinally movable perpendicular to the drawing plane and which is covered by a face plate 8 fastened to the wing 2. On the drive rod 7, the faceplate 8 in the range of slots 9 penetrating locking pins 10 are attached. By way of example only a single locking pin 10 is shown in the drawing. In the region facing the locking pin 10, the frame 1 has a closing latch 11. The drive rod 7 can be moved by an electric motor drive 13 fastened to a horizontal rail 12 of the blade 2 and shown schematically in the drawing. At its lower part of the wing 2 is connected via a tilting bearing 14 with the frame 1. In the upper part of the wing 2 is held by a stay arm 15 of 16 Ausstellschere. In a drive of the drive rod 7, the Ausstellschere 16 is adjusted and the wing 2 is pivoted against the frame 1. In a further drive, the locking pin 10 moves into the latch 11 and locks the wing 2 in the frame first

Die Figur 2a zeigt den Rahmen 1 aus Figur 1 in einer Ansicht senkrecht auf die Schließfalle 11 mit einer Anzugseinrichtung 17. Der Flügel 2 steht hier dem Rahmen 1 mit geringem Abstand gegenüber und befindet sich in einer Stellung unmittelbar vor seiner Verriegelung mit dem Rahmen 1. Der Flügelüberschlag 6 des Flügels 2, der Schließzapfen 10 und ein Anzugsteil 18 der Anzugseinrichtung 17 sind hierbei geschnitten dargestellt. Die Anzugseinrichtung 17 hat ein an dem Rahmen 1 schwenkbar gelagertes Anzugselement 19. Das Anzugsteil 18 ist wie der Schließzapfen 10 an der an dem Flügel 2 angeordneten, und in Figur 1 dargestellten Treibstange 7 befestigt. Das Anzugselement 19 weist einen Anzugsarm 20 mit einer Anzugskante 21 auf und befindet sich in einer hervorstehenden, den Holm 4 des Rahmens 1, auf dem es befestigt ist, in Richtung des Flügels 2 überragenden Stellung. Eine Feder 22 spannt das Anzugselement 19 in die eingezeichnete Stellung vor, in der es sich mittels eines Abstützarms 23 an einem Anschlag 24 abstützt. Der Abstützarm 23 und der Anzugsarm 20 sind einteilig gefertigt und weisen eine gemeinsame Lagerung 25 auf. Die Schließfalle 11 und ein die Lagerung 25 des Anzugselementes 19 aufweisendes Halteteil 26 sind einteilig gestaltet und mit dem Rahmen 1 verschraubt. Die Schließfalle 11 hat ebenfalls eine Anzugskante 27. Der Schließzapfen 10 mit der Schließfalle 11 und der Anzugskante 27 bilden zusammen im wesentlichen die aus der Praxis bekannte Anzugseinrichtung. Das Anzugsteil 18 ist als abgewinkelter Blechstreifen und schwertförmig gestaltet und hat eine der Anzugskante 21 des Anzugselementes 19 entsprechend gestaltete Auflaufkante 28. Weiterhin ist das Anzugsteil 18 weiter von dem Flügelüberschlag 6 des Flügels 2 entfernt angeordnet als der in die Schließfalle 11 einzuführende Schließzapfen 10.The FIG. 2a shows the frame 1 from FIG. 1 In a view perpendicular to the latch 11 with a tightening device 17. The wing 2 here stands opposite the frame 1 with a small distance and is in a position immediately before its locking with the frame 1. The wing flap 6 of the wing 2, the locking pin 10th and a suit part 18 of the tightening device 17 are shown cut here. The tightening device 17 has a tightening element 19 which is pivotably mounted on the frame 1. The tightening part 18, like the locking pin 10, is arranged on the wing 2, and in FIG FIG. 1 illustrated drive rod 7 attached. The tightening element 19 has a tightening arm 20 with a tightening edge 21 and is located in a protruding, the spar 4 of the frame 1 on which it is mounted in the direction of the wing 2 superior position. A spring 22 biases the tightening element 19 in the drawn position, in which it is supported by a support arm 23 to a stop 24. The support arm 23 and the arm 20 are made in one piece and have a common storage 25. The latch 11 and a storage 25 of the tightening element 19 exhibiting holding part 26 are integrally formed and bolted to the frame 1. The locking latch 11 also has a tightening edge 27. The locking pin 10 with the latch 11 and the tightening edge 27 together form substantially known from practice tightening device. The suit part 18 is designed as an angled sheet metal strip and sword-shaped and has a suit edge 21 of the tightening element 19 correspondingly shaped leading edge 28. Furthermore, the tightening part 18 further away from the wing flap 6 of the wing 2 arranged as the inserted into the latch 11 locking pin 10th

In der in Figur 2a dargestellten Anzugsstellung der Anzugseinrichtung 17 liegt das Anzugsteil 18 an dem Anzugselement 19 an. Bei einem Antrieb der in Figur 1 dargestellten Treibstange 7 mittels des elektromotorischen Antriebs 13 bewegen sich der Schließzapfen 10 und das Anzugsteil 18 nach rechts. Zur Verdeutlichung sind die Bewegungsrichtungen des Schließzapfens 10 und des Anzugsteils 18 sowie des Flügelüberschlags 6 des Flügels 2 in der Zeichnung mit Pfeilen gekennzeichnet. Bei der Bewegung der Treibstange 7 gleitet das Anzugsteil 18 entlang der Anzugskante 21 des Anzugselementes 19. Der Flügel 2 wird dabei zu dem Rahmen 1 hingezogen. Eine mittlere Anzugsstellung ist in Figur 2b dargestellt. Im Vergleich zu der Anzugsstellung aus Figur 2a ist hier nur noch ein sehr geringer Spalt zwischen dem Flügelüberschlag 6 des Flügels 2 und dem Rahmen 1 vorhanden. Beim weiteren Antrieb der Treibstange 7 wird der Flügel 6 schließlich weiterbewegt bis sein Flügelüberschlag 6 zunächst gegen einen auf dem freien Ende des Anzugsarms 20 angeordneten Anschlag 29 gelangt. Dabei wird der Anzugsarm 20 von dem Flügelüberschlag 6 des Flügels 2 in eine zurückgezogene, vollständig im Bereich des Holmes 4 des Rahmens 1 befindliche Stellung verschwenkt. Anschließend gelangt der Flügelüberschlag 6 des Flügels 2 gegen den Rahmen 1. Diese Anzugsstellung ist in Figur 2c dargestellt. Das Anzugsteil 18 ist vollständig über das Anzugselement 19 entlanggeglitten und befindet sich in einer von dem Anzugselement 19 getrennten Stellung. Der Flügel 2 wird von dem sich an einer Verriegelungskante 30 der Schließfalle 11 abstützenden Schließzapfen 10 gehalten.In the in FIG. 2a shown tightening position of the tightening device 17 is the suit part 18 on the tightening element 19 at. In a drive of in FIG. 1 illustrated drive rod 7 by means of the electric motor drive 13, the locking pin 10 and the tightening member 18 move to the right. For clarity, the directions of movement of the locking pin 10 and the tightening part 18 and the wing flap 6 of the wing 2 are marked with arrows in the drawing. During the movement of the drive rod 7, the tightening part 18 slides along the tightening edge 21 of the tightening element 19. The wing 2 is thereby attracted to the frame 1. A middle suit position is in FIG. 2b shown. Compared to the suit position off FIG. 2a Here is only a very small gap between the wing flap 6 of the wing 2 and the frame 1 is present. Upon further drive of the drive rod 7, the wing 6 is finally moved to its wing flap 6 first comes against a arranged on the free end of the Anzugsarms 20 stop 29. Here, the Anzugsarm 20 is pivoted by the wing flap 6 of the wing 2 in a retracted, completely located in the region of the spar 4 of the frame 1 position. Subsequently, the wing flap 6 of the wing 2 comes against the frame 1. This tightening position is in Figure 2c shown. The tightening member 18 is completely slid over the tightening element 19 and is in a separate position from the tightening element 19. The wing 2 is held by the locking pin 10 which is supported on a locking edge 30 of the latch 11.

Figur 3a zeigt eine Anzugseinrichtung 31 bei der ein Anzugsteil 32 als Schließzapfen ausgebildet ist. Ein Halteteil 33 eines Anzugselementes 34 der Anzugseinrichtung 31 und eine Schließfalle 35 sind einteilig gestaltet. Die Schließfalle 35 hat eine Verriegelungskante 36 und eine davon abstehende Anzugskante 37. Die Anzugskante 37 ist fluchtend zu einer Anzugskante 38 des Anzugselementes 34 angeordnet. Die Anzugskanten 37, 38 überlappen sich in einem Bereich, in welchem sie teilweise übereinander angeordnet sind. Wie bei der Anzugseinrichtung 17 aus Figur 2a ist ein Anzugsarm 40 des Anzugselementes 34 einteilig mit einem Abstützarm 39 gefertigt und federelastisch in Richtung des Flügels 2 vorgespannt. Bei einer Bewegung des als Schließzapfen ausgebildeten Anzugsteils 32 nach rechts gelangt dieses zunächst gegen die Anzugskante 38 des Anzugselementes 34 und gleitet an dieser entlang. Diese Anzugsstellung ist in Figur 3b dargestellt. Der Flügel 2 bewegt sich dabei auf den Rahmen 1 zu. Bei einer Weiterbewegung des Anzugselementes 34 nach rechts gelangt dieses über die Anzugskante 37 der Schließfalle 35 hinter die Verriegelungskante 36. Diese Anzugsstellung ist in Figur 3c dargestellt. Hierbei wird der Flügel 2 von dem Anzugselement 34 in seiner an dem Rahmen 1 anliegenden Stellung gehalten. Das Anzugselement 34 liegt mit einem Anschlag 41 an dem Flügelüberschlag 6 des Flügels 2 an und ist in eine zurückgezogene, vollständig über den Rahmen 1 befindliche Stellung geschwenkt. FIG. 3a shows a tightening device 31 in which a tightening part 32 is formed as a locking pin. A holding part 33 of a tightening element 34 of the tightening device 31 and a closing catch 35 are designed in one piece. The closing latch 35 has a locking edge 36 and a suiting edge 37 projecting therefrom. The tightening edge 37 is arranged in alignment with a tightening edge 38 of the tightening element 34. The suit edges 37, 38 overlap in a region in which they are partially arranged one above the other. As with the tightening device 17 off FIG. 2a is a suit arm 40 of the tightening element 34 made in one piece with a support arm 39 and resiliently biased in the direction of the wing 2. During a movement of the trained as a locking pin tightening part 32 to the right this first comes against the tightening edge 38 of the tightening element 34 and slides along it. This position is in FIG. 3b shown. The wing 2 moves towards the frame 1. Upon further movement of the tightening element 34 to the right this passes over the suit edge 37 of the latch 35 behind the locking edge 36. This tightening position is in Figure 3c shown. Here, the wing 2 is held by the tightening element 34 in its resting on the frame 1 position. The tightening element 34 rests with a stop 41 against the wing flap 6 of the wing 2 and is pivoted into a retracted, completely over the frame 1 located position.

Figur 4a zeigt eine Anzugseinrichtung 42, bei der eine einzige Anzugskante 43 auf einem Anzugselement 44 angeordnet ist. Diese Anzugseinrichtung 42 kann beispielsweise in Verbindung mit einer aus der Praxis bekannten Anzugseinrichtung zur Bewegung des Flügels 2 vorgesehen sein. Eine solche bekannte Anzugseinrichtung ist beispielsweise in den Figuren 2a bis 2c durch die Schließfalle 11, dem Schließzapfen 10 und der Anzugskante 27 dargestellt. Der Flügel 2 wird in der Regel mit mehreren in den Figuren 2a bis 2c dargestellten Schließfallen 11 verriegelt. Beim Anziehen des Flügels 2 in eine vorgesehene, dessen Verriegelung ermöglichende Position genügen in Abhängigkeit von der Größe des Flügels 2 einige wenige in den Figuren 3 und 4 dargestellte Anzugseinrichtungen 31, 42. Das Anzugselement 44 ist im wesentlichen wie das der Anzugseinrichtung 17 aus Figur 2a gestaltet. Ein Anzugsteil 45 der Anzugseinrichtung 42 ist als Schließzapfen ausgebildet und läßt sich mittels der in Figur 1 dargestellten Treibstange 7 nach rechts bewegen, bis es an die Anzugskante 43 gelangt. An dieser Anzugskante 43 gleitet das Anzugsteil 45 entlang und zieht den Flügel 2 an den Rahmen 1. Eine mittlere Anzugsstellung ist in Figur 4b dargestellt. Schließlich gelangt das Anzugsteil 45 hinter eine Verriegelungskante 46 einer Schließfalle 47 und hält den Flügel 2 an dem Rahmen 1. Diese Anzugsstellung ist in Figur 4c dargestellt. Bei dem Übergang des Anzugsteils von der in Figur 4b in die in 4c dargestellte Position wird der Flügel von der in Figur 2 dargestellten Anzugskante 27 der Schließfalle 11 bewegt. FIG. 4a shows a tightening device 42, in which a single tightening edge 43 is arranged on a tightening element 44. This tightening device 42 can be provided, for example, in conjunction with a suit device known from practice for moving the wing 2. Such a known tightening device is for example in the FIGS. 2a to 2c through the latch 11, the locking pin 10 and the tightening edge 27th shown. The wing 2 is usually with several in the FIGS. 2a to 2c Locks shown 11 locked. When tightening the wing 2 in an envisaged, the locking enabling position suffice depending on the size of the wing 2 a few in the Figures 3 and 4 illustrated tightening devices 31, 42. The tightening element 44 is substantially like that of the tightening device 17 from FIG. 2a designed. A suit part 45 of the tightening device 42 is designed as a locking pin and can be by means of in FIG. 1 Move shown drive rod 7 to the right until it reaches the suit edge 43. At this suit edge 43, the suit part 45 slides along and pulls the wing 2 to the frame 1. A middle attracting position is in FIG. 4b shown. Finally, the suit part 45 passes behind a locking edge 46 of a latch 47 and holds the wing 2 on the frame 1. This tightening position is in Figure 4c shown. At the transition of the tightening part of the in FIG. 4b in the position shown in Fig. 4c, the wing of the in FIG. 2 shown suit edge 27 of the latch 11 moves.

Claims (13)

  1. Pull-in device (17) for moving a wing (2) in the closed position against a frame (1) comprising a pull-in edge (21, 38, 43), to be arranged on a first spar (4), with a pull-in part (18) to be arranged on a pivotal spar (12) facing the first spar (4) and with means (7) for moving the pull-in part (18) in the installed condition along its spar (12) to grip behind the pull-in edge (21, 38, 43), wherein the pull-in edge (21, 38, 43) is arranged in an inclined manner facing the direction of movement of the pull-in part (18) in the closed position, characterized in that the pull-in edge (21, 38, 43) is arranged at least partly on a movable pull-in element (19, 34, 44) of the pull-in device (17), and in that the pull-in element (19, 34, 44), in the open position of the wing (2), is arranged in a projecting position, protruding in the installed condition over its spar (4) and, in the closed position of the wing (2), is arranged in a retracted position, located in the vicinity of its spar (4).
  2. Pull-in device according to Claim 1, characterized in that the pull-in element (19, 34, 44) is provided for arranging on the frame (1).
  3. Pull-in device according to Claim 1 or 2, characterized in that the pull-in element (19, 34, 44) is mounted on a static support part (26) and is resiliently pre-tensioned in its projecting position.
  4. Pull-in device according to at least one of the preceding claims, characterized in that the pull-in part (19) for closer arrangement on the frame (1) is provided as a closing spigot (10) of the driving bar fitting (3), movable into a closing latch (11) firmly attached to the frame.
  5. Pull-in device according to Claim 4, characterized in that a support part (26) of the pull-in element (19, 34, 44) is formed as a structural unit with the closing latch (11, 35, 47).
  6. Pull-in device according to at least one of the preceding claims, characterized in that the pull-in part (18) is configured in the shape of a sword.
  7. Pull-in device according to at least one of the preceding claims, characterized in that the pull-in part (32, 45) is configured as a closing spigot of the driving bar fitting (3).
  8. Pull-in device according to at least either of Claims 4 and 5, characterized in that a pull-in edge (37) of the closing latch (35) is arranged flush with the pull-in edge (38) of the pull-in element (34) located in the projecting position, and characterized in that a locking edge (36) of the closing latch (35), provided for mounting the pull-in part (32), in the closed position is arranged outside the movement range of the pull-in element (34).
  9. Pull-in device according to at least either of Claims 4 and 5, characterized in that partial areas of the pull-in edge (37) of the closing latch (35) and of the pull-in edge (38), located in the projecting position, of the pull-in element (34) are arranged adjacent to one another.
  10. Pull-in device according to at least either of Claims 4 and 5, characterized in that the pull-in edge (43) of the pull-in element (44), in the closed position, can be moved up to directly in front of the locking edge (46) of the closing latch (47).
  11. Pull-in device according to at least one of the preceding claims, characterized in that the pull-in part (18) has a run-on edge (28) aligned with the pull-in edge (21) of the pull-in element (19).
  12. Pull-in device according to at least one of Claims 3 and 5, characterized in that a support arm (23, 39) of the pull-in element (19, 34, 44), located in the projecting position, is pre-tensioned against a stop (24) of the support part (26, 33).
  13. Pull-in device according to at least one of the preceding claims, characterized in that the pull-in edge (21, 38, 43) of the pull-in element (19, 34, 44) is arranged on a pull-in arm (20, 40) and in that the pull-in arm (20, 40) at its free end has a stop (29, 41) for the wing (2).
EP00127750A 2000-02-04 2000-12-19 Pull-in device for moving a wing Expired - Lifetime EP1122389B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10005055 2000-02-04
DE10005055A DE10005055A1 (en) 2000-02-04 2000-02-04 Pull-to arrangement for casement or leaf incorporates pull-to edge, part and element, and frame struts

Publications (3)

Publication Number Publication Date
EP1122389A2 EP1122389A2 (en) 2001-08-08
EP1122389A3 EP1122389A3 (en) 2006-03-15
EP1122389B1 true EP1122389B1 (en) 2009-02-11

Family

ID=7629910

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00127750A Expired - Lifetime EP1122389B1 (en) 2000-02-04 2000-12-19 Pull-in device for moving a wing

Country Status (5)

Country Link
EP (1) EP1122389B1 (en)
AT (1) ATE422594T1 (en)
DE (2) DE10005055A1 (en)
DK (1) DK1122389T3 (en)
ES (1) ES2319499T3 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004011880A1 (en) * 2004-03-11 2005-09-29 Aug. Winkhaus Gmbh & Co. Kg Locking catch for window of building has holding member with groove accommodating peg on lock actuator strap and has holding arm with hooked end
DE102008043240A1 (en) 2008-10-28 2011-03-17 Aug. Winkhaus Gmbh & Co. Kg Tightening device for a drive rod fitting

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2420634A1 (en) 1978-03-23 1979-10-19 Ferco Internal Usine Ferrur Ba Single-handle window fitting - has coupling lever with elongated slide hole including straight and oblique portions
DE3140855A1 (en) * 1981-10-14 1983-04-28 Geze Gmbh, 7250 Leonberg Device for actuating a scissor-type swivel mechanism for the wings of windows, doors or the like
AT386451B (en) * 1986-06-19 1988-08-25 Frank Gmbh Wilh CLEAR VENTILATION DEVICE FOR A Tilt & Turn Wing Of A Window, Door Or. DGL.
DE3939043C2 (en) * 1989-11-25 1994-02-24 Fuhr Carl Gmbh & Co Fitting for windows, doors or the like
DE19515708A1 (en) * 1995-04-28 1996-10-31 Winkhaus Fa August Display device for windows, doors or the like

Also Published As

Publication number Publication date
DK1122389T3 (en) 2009-05-25
ATE422594T1 (en) 2009-02-15
ES2319499T3 (en) 2009-05-08
DE50015553D1 (en) 2009-03-26
DE10005055A1 (en) 2001-08-09
EP1122389A2 (en) 2001-08-08
EP1122389A3 (en) 2006-03-15

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