EP1122389A2 - Pull-in device for moving a wing - Google Patents
Pull-in device for moving a wing Download PDFInfo
- Publication number
- EP1122389A2 EP1122389A2 EP00127750A EP00127750A EP1122389A2 EP 1122389 A2 EP1122389 A2 EP 1122389A2 EP 00127750 A EP00127750 A EP 00127750A EP 00127750 A EP00127750 A EP 00127750A EP 1122389 A2 EP1122389 A2 EP 1122389A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- tightening
- edge
- wing
- frame
- tightening device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000033001 locomotion Effects 0.000 claims description 19
- 238000011161 development Methods 0.000 description 9
- 230000018109 developmental process Effects 0.000 description 9
- 238000010276 construction Methods 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 241001295925 Gegenes Species 0.000 description 1
- 235000003332 Ilex aquifolium Nutrition 0.000 description 1
- 241000209027 Ilex aquifolium Species 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000005352 clarification Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
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 E05DÂ 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 movement of a wing in the closed position against a frame with a suit edge to be arranged on a first spar, with one swiveling on one in relation to the first spar Tie bar to be arranged and with means for movement of the suit part in the assembled state along its Holms to reach behind the suit edge, the suit edge opposite to the direction of movement of the suit part is inclined.
- the tightening device is the tightening edge on a frame-fixed Lock latch arranged.
- the wing has one fastened on a connecting rod of a connecting rod fitting Locking pin.
- the locking pin comes against the tightening edge and slides along this.
- the locking pin thus serves as a tightening part.
- the locking pin can then be inserted into the Lock latch penetrate and the wing with the frame lock.
- a disadvantage of the known tightening device is that the wing only adjoins the frame Position against the frame. Since the Tightening edge does not hinder the movement of the wing , the length of which is naturally related to the dimensions of the Spar of the frame limited.
- a tightening device is from FR 24 20 634 known without a suit edge, in which a swivel arm on a Forend rail one to lock the wing arranged frame provided drive rod fitting is.
- the faceplate has its longest extension an angled control curve designed as an elongated hole to accommodate a connecting rod connected to a drive rod the link arm controlling the sliding block.
- the sliding block pivots towards Swivel arm. This engages behind the suit part and pulls thus the wing against the frame.
- a disadvantage of the known Suit is that the control of the Movement of the swivel arm is very complex and prone to failure designed.
- a tightening device is known from DE 195 15 708 A1 become, in which the control curve in an intermediate plate is arranged. This allows the Swivel the swivel arm through a large angular range.
- the disadvantage here is the very complex design the control curve and the high number of to be assembled and components to be manufactured. Designed this way this tightening device is also particularly expensive and prone to failure.
- the invention is based on the problem of a tightening device of the type mentioned at the beginning, that they have a movement of the frame with at least little Distance opposite wing allows and is structurally particularly simple.
- the tightening device according to the invention does not require a guide curve with a sliding block sliding along it and is therefore particularly susceptible to interference.
- the tightening device according to the invention is designed in addition, it is particularly simple in construction.
- the invention The tightening device is also particularly compact.
- the tightening device is particularly suitable for use Wings to be tilted and locked by motor Advantage, since there is no hand pressure on the wing be exercised.
- the tightening part can be like the locking pin the known tightening device on the drive rod be attached. This requires the movement of the Part of the suit does not require any additional construction work since the Driving rod when opening, closing and locking the Wing is driven anyway.
- Suit device helps if that A tightening element is provided for arrangement on the frame.
- the movement of the tightening element takes place according to a other advantageous development of the invention particularly simple and requires a particularly small one construction effort when the tightening element is on a fixed Holding part stored and resilient in its protruding position is biased.
- This design can the tightening element when closing the Moving wing of the wing and can therefore this do not jam.
- the range of motion of the tightening element can be adjusted accordingly another advantageous development of the invention Keep it particularly low when the suit part is closer Arrangement towards the frame is provided as one in one frame-fixed locking latch movable locking pin of the Espagnolette fitting.
- the tightening element can be advantageous according to another Further development of the invention is particularly easy to assemble, if a holding part of the tightening element with the The latch is designed as a structural unit.
- the latch and the holding part can, for example, from cast Aluminum component to be made.
- the suit part is according to another advantageous development of the invention is particularly simple, if it is sword-shaped.
- This can Suit part in particular as an inexpensive, angled Metal strips to be made.
- the tightening device according to the invention requires a special one small number to be manufactured and assembled Components if the tightening part as the locking pin of the Espagnolette fitting is formed.
- the tightening device only requires one only tightening part for moving the wing against the Frame and to lock the wing when a tightening edge the latch is aligned with the edge of the suit of the tightening element in the protruding position is arranged, and if one for mounting the locking part provided in the closed position the locking latch outside the range of motion the suit element is arranged.
- the tightening part designed as a locking pin is in accordance with another advantageous development of the invention guided particularly reliably behind the locking edge, if partial areas of the tightening edge of the locking latch and the pulling edge in the protruding position the suit element arranged side by side are. This allows the suit part to move along the spar of the wing first against the edge of the suit of the tightening element. From this suit edge the suit piece slides into the section of the side by side arranged tightening edges up to behind the locking edge. The tightening element can then move in move to its retracted position and lock of the wing.
- a tightening edge of the latch can be according to one avoid other advantageous developments of the invention, when the tightening edge of the tightening element is in the closed position until just before the locking edge of the The latch is movable.
- the intended tightening part is capable of another advantageous development of the invention particularly slide evenly along the edge of the suit if that Tightening part one corresponding to the tightening edge of the tightening element has aligned incline.
- the range of motion of the suit edge in on the wing intended direction can be according to another simply limit advantageous further development of the invention, if a support arm is in the protruding position located tightening element against a stop of the holding part is biased.
- the support arm can also high, when sliding the suit part over the suit edge support generated forces.
- Controlling the movement of the tightening element requires according to another advantageous development of the invention a particularly low effort if the tightening edge the suit element arranged on a suit arm and if the arm is at its free end has a stop for the wing.
- FIG. 1 shows one on a fixed frame 1 pivotable wing 2 with an espagnolette fitting 3 in a side view.
- the wing 2 is located here in a tilted position. With wing 2 it can be, for example, a tilt and turn sash Window or a French window act. Likewise can the wing 2 is a pure tilt wing or a ventilation flap his.
- the frame 1 is horizontal in the area of two Spars 4, 5 shown in section.
- the wing 2 has one in a tilted position against the frame 1 adjacent wing flap 6.
- the espagnolette fitting 3 has a longitudinally movable perpendicular to the plane of the drawing Driving rod 7, which is attached to the wing 2 by one Face plate 8 is covered.
- the faceplate 8 On the Drive rod 7 are the faceplate 8 in the range of Elongated holes 9 penetrating locking pin 10 attached. Only one is shown as an example in the drawing Locking pin 10 shown.
- frame 1 has a latch 11.
- the drive rod 7 can be from one to one horizontal spar 12 of the wing 2 attached and in the Drawing schematically illustrated electromotive Move drive 13.
- the Wing 2 At its bottom is the Wing 2 connected to the frame 1 via a tilting bearing 14.
- the wing 2 In the upper area, the wing 2 is by an extension arm 15 a stay scissors 16 held.
- the stay scissors 16 At a Driving the drive rod 7, the stay scissors 16 is adjusted and the wing 2 pivoted against the frame 1.
- the locking pin moves 10 in the latch 11 and locks the wing 2 in the frame 1.
- FIG. 2a shows the frame 1 from FIG. 1 in a view perpendicular to the latch 11 with an inventive Tightening device 17.
- the wing 2 stands here the frame 1 with a small distance opposite and is in a position immediately before it is locked with the frame 1.
- the wing flap 6 des Wing 2, the locking pin 10 and a tightening part 18 of the The tightening device 17 is shown in section.
- the tightening device 17 has a on the frame 1 swivel-mounted tightening element 19.
- the tightening part 18 is like the locking pin 10 on the arranged on the wing 2, and drive rod 7 shown in Figure 1 attached.
- the tightening element 19 has a tightening arm 20 with a suit edge 21 and is in one protruding, the spar 4 of the frame 1 on which it is attached is, in the direction of the wing 2 outstanding position.
- a spring 22 clamps the tightening element 19 in the drawn position before, in which it is by means of a Support arm 23 is supported on a stop 24.
- the support arm 23 and the arm 20 are made in one piece and have a common bearing 25.
- the latch 11 and a bearing 25 of the tightening element 19 having holding part 26 are designed in one piece and screwed to the frame 1.
- the latch 11 has also a tightening edge 27.
- the locking pin 10 with the latch 11 and the tightening edge 27 form together essentially the tightening device known from practice.
- the suit part 18 is angled Metal strips and sword-shaped and has one corresponding to the tightening edge 21 of the tightening element 19 designed leading edge 28. Furthermore, the pull-on part 18 further away from the wing flap 6 of the wing 2 arranged as the one to be inserted into the latch 11 Locking pin 10.
- the drive rod 7 is the wing 6 finally moved on until his wing flap 6 initially countered one arranged on the free end of the arm 20 Stop 29 arrives.
- the arm 20 is the Wing flap 6 of wing 2 in a retracted, located completely in the area of the spar 4 of the frame 1 Position pivoted. Then the wing overlap 6 of the wing 2 against the frame 1.
- This Tightening position is shown in Figure 2c.
- the suit part 18 has completely slid along the tightening element 19 and is located in one of the tightening elements 19 separate position.
- the wing 2 is from which is on a locking edge 30 of the latch 11 supporting locking pin 10 held.
- FIG. 3a shows a tightening device 31 with a tightening part 32 is designed as a locking pin.
- a holding part 33 of a tightening element 34 of the tightening device 31 and a latch 35 are made in one piece.
- the latch 35 has a locking edge 36 and one protruding edge 37.
- the edge 37 is aligned with a tightening edge 38 of the tightening element 34 arranged.
- the suit edges 37, 38 overlap in an area in which they are partially stacked are.
- a tightening arm 40 of the tightening element 34 is in one piece manufactured with a support arm 39 and resilient in Biased towards the wing 2.
- FIG 4a shows a tightening device 42, in which a only the pulling edge 43 is arranged on a pulling element 44 is.
- This tightening device 42 can for example in connection with a tightening device known from practice provided for moving the wing 2 his.
- a known tightening device is, for example in Figures 2a to 2c through the latch 11, the locking pin 10 and the tightening edge 27 shown.
- the wing 2 is usually with several Closing latches 11 shown in FIGS. 2a to 2c locked.
- the tightening element 44 is essentially like that the tightening device 17 from Figure 2a.
- a suit part 45 of the tightening device 42 is as a locking pin trained and can be by means of those shown in Figure 1 Move drive rod 7 to the right until it comes on the tightening edge 43 arrives. On this suit edge 43 slides the suit part 45 and pulls the wing 2 to the frame 1. A middle tightening position is in figure 4b. Finally, the tightening part 45 arrives behind a locking edge 46 of a latch 47 and holds the wing 2 on the frame 1. This tightening position is shown in Figure 4c. At the transition of the Tightening part from that shown in Figure 4b in that shown in 4c Position is the wing of that shown in Figure 2 Pull 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)
- Mechanical Pencils And Projecting And Retracting Systems Therefor, And Multi-System Writing Instruments (AREA)
- Closing And Opening Devices For Wings, And Checks For Wings (AREA)
- Details Of Spanners, Wrenches, And Screw Drivers And Accessories (AREA)
- Basic Packing Technique (AREA)
Abstract
Description
Die Erfindung betrifft eine Anzugseinrichtung zur Bewegung eines FlĂ¼gels in SchlieĂŸstellung gegen einen Rahmen mit einer an einem ersten Holm anzuordnenden Anzugskante, mit einem an einem gegenĂ¼ber 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 gegenĂ¼ber der Bewegungsrichtung des Anzugsteils geneigt angeordnet ist.The invention relates to a tightening device for movement of a wing in the closed position against a frame with a suit edge to be arranged on a first spar, with one swiveling on one in relation to the first spar Tie bar to be arranged and with means for movement of the suit part in the assembled state along its Holms to reach behind the suit edge, the suit edge opposite to the direction of movement of the suit part is inclined.
Solche Anzugseinrichtungen werden in der Praxis häufig eingesetzt und sind damit bekannt. Im einfachsten Fall der Anzugseinrichtung ist die Anzugskante auf einer rahmenfesten SchlieĂŸfalle angeordnet. Der FlĂ¼gel hat einen auf einer Treibstange eines Treibstangenbeschlages befestigten SchlieĂŸzapfen. Bei einem SchlieĂŸen wird der FlĂ¼gel zunächst in eine an dem Rahmen anliegende Stellung bewegt und anschlieĂŸend die Treibstange angetrieben. Dabei gelangt der SchlieĂŸzapfen gegen die Anzugskante und gleitet an dieser entlang. Hierbei wird der FlĂ¼gel gegen den Rahmen gezogen. Der SchlieĂŸzapfen dient damit als Anzugsteil. AnschlieĂŸend kann der SchlieĂŸzapfen in die SchlieĂŸfalle eindringen und den FlĂ¼gel mit dem Rahmen verriegeln. Diese Gestaltung der Anzugseinrichtung ist besonders einfach aufgebaut und kostengĂ¼nstig herstellbar.Such tightening devices are common in practice used and are therefore known. In the simplest case the tightening device is the tightening edge on a frame-fixed Lock latch arranged. The wing has one fastened on a connecting rod of a connecting rod fitting Locking pin. When closing the wing initially in a position against the frame moved and then driven the drive rod. there the locking pin comes against the tightening edge and slides along this. Here the wing is against pulled the frame. The locking pin thus serves as a tightening part. The locking pin can then be inserted into the Lock latch penetrate and the wing with the frame lock. This design of the tightening device is particularly simple and inexpensive to manufacture.
Nachteilig bei der bekannten Anzugseinrichtung ist, daĂŸ sie den FlĂ¼gel nur in einer unmittelbar an dem Rahmen anliegenden Stellung gegen den Rahmen ziehen kann. Da die Anzugskante die Bewegung des FlĂ¼gels nicht behindern darf, ist deren Länge naturgemĂ¤ĂŸ auf die Abmessungen des Holms des Rahmens begrenzt.A disadvantage of the known tightening device is that the wing only adjoins the frame Position against the frame. Since the Tightening edge does not hinder the movement of the wing , the length of which is naturally related to the dimensions of the Spar of the frame limited.
Weiterhin ist aus der FR 24 20 634 eine Anzugseinrichtung
ohne Anzugskante bekannt, bei der ein Schwenkarm auf einer
Stulpschiene eines zur Verriegelung des FlĂ¼gels 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 FlĂ¼gel verriegelnde
Richtung verschwenkt der Kulissenstein den
Schwenkarm. Dieser hintergreift das Anzugsteil und zieht
damit den FlĂ¼gel gegen den Rahmen. Nachteilig bei der bekannten
Anzugseinrichtung ist, daĂŸ sich die Steuerung der
Bewegung des Schwenkarms sehr aufwendig und störanfällig
gestaltet.Furthermore, a tightening device is from
Aus der DE 195 15 708 A1 ist eine Anzugseinrichtung bekannt geworden, bei der die Steuerkurve in einer Zwischenplatte angeordnet ist. Hierdurch lĂ¤ĂŸt sich der Schwenkarm um einen groĂŸen 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.A tightening device is known from DE 195 15 708 A1 become, in which the control curve in an intermediate plate is arranged. This allows the Swivel the swivel arm through a large angular range. The disadvantage here is the very complex design the control curve and the high number of to be assembled and components to be manufactured. Designed this way this tightening device is also particularly expensive and prone to failure.
Der Erfindung liegt das Problem zugrunde, eine Anzugseinrichtung der eingangs genannten Art so weiterzubilden, daĂŸ sie eine Bewegung des dem Rahmen mit zumindest geringem Abstand gegenĂ¼berstehenden FlĂ¼gels ermöglicht und konstruktiv besonders einfach aufgebaut ist. The invention is based on the problem of a tightening device of the type mentioned at the beginning, that they have a movement of the frame with at least little Distance opposite wing allows and is structurally particularly simple.
Dieses Problem wird erfindungsgemĂ¤ĂŸ dadurch gelöst, daĂŸ die Anzugskante zumindest teilweise auf einem beweglichen Anzugselement angeordnet ist und daĂŸ das Anzugselement in Offenstellung des FlĂ¼gels in einer hervorstehenden, im montierten Zustand seinen Holm Ă¼berragenden Stellung und in SchlieĂŸstellung des FlĂ¼gels in einer zurĂ¼ckgezogenen, im Bereich seines Holms befindlichen Stellung angeordnet ist.This problem is solved according to the invention in that the tightening edge at least partially on a movable Suit element is arranged and that the suit element in Open position of the wing in a protruding, in assembled state its spar outstanding position and in the closed position of the wing in a retracted, located in the area of his spar is.
Durch diese Gestaltung kann die Anzugskante in Offenstellung des FlĂ¼gels Ă¼ber den jeweiligen Holm hinausragen und den mit Abstand vor dem Rahmen stehenden FlĂ¼gel anziehen. Bei der Bewegung des FlĂ¼gels gegen den Rahmen wird zumindest der den Holm Ă¼berragende Bereich der Anzugskante in die zurĂ¼ckgezogene Stellung bewegt. AnschlieĂŸend lĂ¤ĂŸt sich der FlĂ¼gel mit dem Rahmen einfach verriegeln. Die erfindungsgemĂ¤ĂŸe Anzugseinrichtung benötigt keine FĂ¼hrungskurve mit einem darin entlanggleitenden Kulissenstein und ist daher besonders störungsunanfällig. Hierdurch gestaltet sich die erfindungsgemĂ¤ĂŸe Anzugseinrichtung zudem konstruktiv besonders einfach. Die erfindungsgemĂ¤ĂŸe Anzugseinrichtung ist zudem besonders kompakt aufgebaut. Die Störungsunanfälligkeit der erfindungsgemĂ¤ĂŸen Anzugseinrichtung ist insbesondere bei einem Einsatz an motorisch zu kippenden und zu verriegelnden FlĂ¼geln von Vorteil, da hier keine Druckkräfte von Hand auf den FlĂ¼gel ausgeĂ¼bt werden. Das Anzugsteil kann wie der SchlieĂŸzapfen der bekannten Anzugseinrichtung auf der Treibstange befestigt sein. Hierdurch erfordert die Bewegung des Anzugsteils keinen zusätzlichen baulichen Aufwand, da die Treibstange beim Ă–ffnen, SchlieĂŸen und Verriegeln des FlĂ¼gels ohnehin angetrieben wird. This design allows the edge of the suit to be in the open position of the wing protrude beyond the respective spar and tighten the sash standing in front of the frame. When the wing moves against the frame at least the area of the suit edge protruding over the spar in the retracted position moves. Then leaves the wing simply locks into the frame. The The tightening device according to the invention does not require a guide curve with a sliding block sliding along it and is therefore particularly susceptible to interference. Hereby the tightening device according to the invention is designed in addition, it is particularly simple in construction. The invention The tightening device is also particularly compact. The susceptibility to failure of the invention The tightening device is particularly suitable for use Wings to be tilted and locked by motor Advantage, since there is no hand pressure on the wing be exercised. The tightening part can be like the locking pin the known tightening device on the drive rod be attached. This requires the movement of the Part of the suit does not require any additional construction work since the Driving rod when opening, closing and locking the Wing is driven anyway.
Zur weiteren Verringerung des baulichen Aufwands der erfindungsgemĂ¤ĂŸen Anzugseinrichtung trägt es bei, wenn das Anzugselement zur Anordnung an dem Rahmen vorgesehen ist.To further reduce the structural complexity of the invention Suit device helps if that A tightening element is provided for arrangement on the frame.
Die Bewegung des Anzugselementes gestaltet sich gemĂ¤ĂŸ 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 lĂ¤ĂŸt sich das Anzugselement beim SchlieĂŸen des FlĂ¼gels von dem FlĂ¼gel bewegen und kann diesen daher nicht verklemmen.The movement of the tightening element takes place according to a other advantageous development of the invention particularly simple and requires a particularly small one construction effort when the tightening element is on a fixed Holding part stored and resilient in its protruding position is biased. Through this design can the tightening element when closing the Moving wing of the wing and can therefore this do not jam.
Der Bewegungsbereich des Anzugselementes lĂ¤ĂŸt sich gemĂ¤ĂŸ 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 SchlieĂŸfalle bewegbarer SchlieĂŸzapfen des Treibstangenbeschlages.The range of motion of the tightening element can be adjusted accordingly another advantageous development of the invention Keep it particularly low when the suit part is closer Arrangement towards the frame is provided as one in one frame-fixed locking latch movable locking pin of the Espagnolette fitting.
Das Anzugselement lĂ¤ĂŸt sich gemĂ¤ĂŸ einer anderen vorteilhaften Weiterbildung der Erfindung besonders einfach montieren, wenn ein Halteteil des Anzugselementes mit der SchlieĂŸfalle als bauliche Einheit gestaltet ist. Hierdurch lassen sich zudem das Anzugselement und die SchlieĂŸfalle gegenĂ¼ber dem Anzugsteil und dem SchlieĂŸzapfen bei der Montage gleichzeitig ausrichten. Die SchlieĂŸfalle und das Halteteil können beispielsweise aus gegossenem Aluminiumbauteil gefertigt sein.The tightening element can be advantageous according to another Further development of the invention is particularly easy to assemble, if a holding part of the tightening element with the The latch is designed as a structural unit. Hereby can also the suit element and Locking latch opposite the tightening part and the locking pin align during assembly. The latch and the holding part can, for example, from cast Aluminum component to be made.
Das Anzugsteil ist gemĂ¤ĂŸ einer anderen vorteilhaften Weiterbildung der Erfindung besonders einfach aufgebaut, wenn es schwertförmig gestaltet ist. Hierdurch kann das Anzugsteil insbesondere als kostengĂ¼nstigen, abgewinkelten Blechstreifen gefertigt sein. The suit part is according to another advantageous development of the invention is particularly simple, if it is sword-shaped. This can Suit part in particular as an inexpensive, angled Metal strips to be made.
Die erfindungsgemĂ¤ĂŸe Anzugseinrichtung erfordert eine besonders geringe Anzahl zu fertigender und zu montierender Bauteile, wenn das Anzugsteil als SchlieĂŸzapfen des Treibstangenbeschlages ausgebildet ist.The tightening device according to the invention requires a special one small number to be manufactured and assembled Components if the tightening part as the locking pin of the Espagnolette fitting is formed.
Die erfindungsgemĂ¤ĂŸe Anzugseinrichtung erfordert nur ein einziges Anzugsteil zur Bewegung des FlĂ¼gels gegen den Rahmen und zur Verriegelung des FlĂ¼gels, wenn eine Anzugskante der SchlieĂŸfalle fluchtend zu der Anzugskante des in der hervorstehenden Stellung befindlichen Anzugselementes angeordnet ist, und wenn eine zur Halterung des Anzugsteils in SchlieĂŸstellung vorgesehene Verriegelungskante der SchlieĂŸfalle auĂŸerhalb des Bewegungsbereichs des Anzugselementes angeordnet ist.The tightening device according to the invention only requires one only tightening part for moving the wing against the Frame and to lock the wing when a tightening edge the latch is aligned with the edge of the suit of the tightening element in the protruding position is arranged, and if one for mounting the locking part provided in the closed position the locking latch outside the range of motion the suit element is arranged.
Das als SchlieĂŸzapfen ausgebildete Anzugsteil wird gemĂ¤ĂŸ einer anderen vorteilhaften Weiterbildung der Erfindung besonders zuverlässig hinter die Verriegelungskante gefĂ¼hrt, wenn Teilbereiche der Anzugskante der SchlieĂŸfalle und der in der hervorstehenden Stellung befindlichen Anzugskante des Anzugselementes nebeneinander angeordnet sind. Hierdurch kann das Anzugsteil bei seiner Bewegung entlang des Holms des FlĂ¼gels zunächst gegen die Anzugskante des Anzugselementes gelangen. Von dieser Anzugskante gleitet das Anzugsteil in den Teilbereich der nebeneinander angeordneten Anzugskanten bis hinter die Verriegelungskante. AnschlieĂŸend kann sich das Anzugselement in seine zurĂ¼ckgezogene Stellung bewegen und die Verriegelung des FlĂ¼gels ermöglichen.The tightening part designed as a locking pin is in accordance with another advantageous development of the invention guided particularly reliably behind the locking edge, if partial areas of the tightening edge of the locking latch and the pulling edge in the protruding position the suit element arranged side by side are. This allows the suit part to move along the spar of the wing first against the edge of the suit of the tightening element. From this suit edge the suit piece slides into the section of the side by side arranged tightening edges up to behind the locking edge. The tightening element can then move in move to its retracted position and lock of the wing.
Eine Anzugskante der SchlieĂŸfalle lĂ¤ĂŸt sich gemĂ¤ĂŸ einer anderen vorteilhaften Weiterbildung der Erfindung vermeiden, wenn die Anzugskante des Anzugselementes in SchlieĂŸstellung bis unmittelbar vor die Verriegelungskante der SchlieĂŸfalle bewegbar ist. A tightening edge of the latch can be according to one avoid other advantageous developments of the invention, when the tightening edge of the tightening element is in the closed position until just before the locking edge of the The latch is movable.
Das zur Bewegung gegen die Anzugskante des Anzugselementes vorgesehene Anzugsteil vermag gemĂ¤ĂŸ einer anderen vorteilhaften Weiterbildung der Erfindung besonders gleichmĂ¤ĂŸig an der Anzugskante entlangzugleiten, wenn das Anzugsteil eine entsprechend der Anzugskante des Anzugselementes ausgerichtete Auf lauf schräge hat.That for movement against the tightening edge of the tightening element the intended tightening part is capable of another advantageous development of the invention particularly slide evenly along the edge of the suit if that Tightening part one corresponding to the tightening edge of the tightening element has aligned incline.
Der Bewegungsbereich der Anzugskante in die auf den FlĂ¼gel vorgesehene Richtung lĂ¤ĂŸt sich gemĂ¤ĂŸ einer anderen vorteilhaften Weiterbildung der Erfindung einfach begrenzen, wenn ein AbstĂ¼tzarm des in der hervorstehenden Stellung befindlichen Anzugselementes gegen einen Anschlag des Halteteils vorgespannt ist. Der AbstĂ¼tzarm kann zudem hohe, beim Gleiten des Anzugsteiles Ă¼ber die Anzugskante erzeugte Kräfte abstĂ¼tzen.The range of motion of the suit edge in on the wing intended direction can be according to another simply limit advantageous further development of the invention, if a support arm is in the protruding position located tightening element against a stop of the holding part is biased. The support arm can also high, when sliding the suit part over the suit edge support generated forces.
Die Steuerung der Bewegung des Anzugselementes erfordert gemĂ¤ĂŸ 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 fĂ¼r den FlĂ¼gel hat.Controlling the movement of the tightening element requires according to another advantageous development of the invention a particularly low effort if the tightening edge the suit element arranged on a suit arm and if the arm is at its free end has a stop for the wing.
Die Erfindung lĂ¤ĂŸt zahlreiche AusfĂ¼hrungsformen 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 FlĂ¼gels mit einem Treibstangenbeschlag,
- Fig.2a - 2c
- eine erfindungsgemĂ¤ĂŸe Anzugseinrichtung
fĂ¼r den FlĂ¼gel aus
Figur 1 in verschiedenen Anzugsstellungen des FlĂ¼gels, - Fig.3a - 3c
- eine weitere AusfĂ¼hrungsform der erfindungsgemĂ¤ĂŸen Anzugseinrichtung in verschiedenen Anzugsstellungen des FlĂ¼gels,
- Fig.4a - 4c
- eine weitere AusfĂ¼hrungsform der erfindungsgemĂ¤ĂŸen Anzugseinrichtung in verschiedenen Anzugsstellungen des FlĂ¼gels.
- Fig. 1
- 2 shows a schematic side view in partial section of a wing which can be pivoted against a frame and has an espagnolette fitting,
- Fig.2a - 2c
- 1 a tightening device according to the invention for the wing from FIG. 1 in different tightening positions of the wing,
- Fig.3a - 3c
- another 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 FlĂ¼gel 2 mit einem Treibstangenbeschlag
3 in einer Seitenansicht. Der FlĂ¼gel 2 befindet
sich hier in einer gekippten Stellung. Bei dem FlĂ¼gel 2
kann es sich beispielsweise um einen Dreh-KippflĂ¼gel eines
Fensters oder einer FenstertĂ¼r handeln. Ebenso kann
der FlĂ¼gel 2 ein reiner Kipp-FlĂ¼gel oder eine LĂ¼ftungsklappe
sein. Der Rahmen 1 ist im Bereich zweier horizontaler
Holme 4, 5 geschnitten dargestellt. Der FlĂ¼gel 2
hat einen in einer gegen den Rahmen 1 gekippten Stellung
anliegenden FlĂ¼gelĂ¼berschlag 6. Der Treibstangenbeschlag
3 weist eine senkrecht zur Zeichenebene längsbewegliche
Treibstange 7 auf, welche von einer auf dem FlĂ¼gel 2 befestigten
Stulpschiene 8 abgedeckt wird. Auf der
Treibstange 7 sind die Stulpschiene 8 im Bereich von
Langlöchern 9 durchdringende SchlieĂŸzapfen 10 befestigt.
Beispielhaft ist in der Zeichnung nur ein einziger
SchlieĂŸzapfen 10 dargestellt. Im dem SchlieĂŸzapfen 10 gegenĂ¼berstehenden
Bereich hat der Rahmen 1 eine SchlieĂŸfalle
11. Die Treibstange 7 lĂ¤ĂŸt sich von einem auf einem
horizontalen Holm 12 des FlĂ¼gels 2 befestigten und in der
Zeichnung schematisch dargestellten elektromotorischen
Antrieb 13 bewegen. An seinem unteren Bereich ist der
FlĂ¼gel 2 Ă¼ber ein Kipplager 14 mit dem Rahmen 1 verbunden.
Im oberen Bereich wird der FlĂ¼gel 2 von einem Ausstellarm
15 einer Ausstellschere 16 gehalten. Bei einem
Antrieb der Treibstange 7 wird die Ausstellschere 16 verstellt
und der FlĂ¼gel 2 gegen den Rahmen 1 geschwenkt.
Bei einem weiteren Antrieb bewegt sich der SchlieĂŸzapfen
10 in die SchlieĂŸfalle 11 und verriegelt den FlĂ¼gel 2 in
dem Rahmen 1.FIG. 1 shows one on a fixed
Die Figur 2a zeigt den Rahmen 1 aus Figur 1 in einer Ansicht
senkrecht auf die SchlieĂŸfalle 11 mit einer erfindungsgemĂ¤ĂŸen
Anzugseinrichtung 17. Der FlĂ¼gel 2 steht
hier dem Rahmen 1 mit geringem Abstand gegenĂ¼ber und befindet
sich in einer Stellung unmittelbar vor seiner Verriegelung
mit dem Rahmen 1. Der FlĂ¼gelĂ¼berschlag 6 des
FlĂ¼gels 2, der SchlieĂŸzapfen 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 SchlieĂŸzapfen 10 an der an dem FlĂ¼gel 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 FlĂ¼gels 2 Ă¼berragenden Stellung.
Eine Feder 22 spannt das Anzugselement 19 in die
eingezeichnete Stellung vor, in der es sich mittels eines
AbstĂ¼tzarms 23 an einem Anschlag 24 abstĂ¼tzt. Der AbstĂ¼tzarm
23 und der Anzugsarm 20 sind einteilig gefertigt
und weisen eine gemeinsame Lagerung 25 auf. Die SchlieĂŸfalle
11 und ein die Lagerung 25 des Anzugselementes 19
aufweisendes Halteteil 26 sind einteilig gestaltet und
mit dem Rahmen 1 verschraubt. Die SchlieĂŸfalle 11 hat
ebenfalls eine Anzugskante 27. Der SchlieĂŸzapfen 10 mit
der SchlieĂŸfalle 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 FlĂ¼gelĂ¼berschlag 6 des FlĂ¼gels 2 entfernt
angeordnet als der in die SchlieĂŸfalle 11 einzufĂ¼hrende
SchlieĂŸzapfen 10.FIG. 2a shows the
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 SchlieĂŸzapfen 10 und das Anzugsteil
18 nach rechts. Zur Verdeutlichung sind die Bewegungsrichtungen
des SchlieĂŸzapfens 10 und des Anzugsteils
18 sowie des FlĂ¼gelĂ¼berschlags 6 des FlĂ¼gels 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 FlĂ¼gel 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 FlĂ¼gelĂ¼berschlag 6 des
FlĂ¼gels 2 und dem Rahmen 1 vorhanden. Beim weiteren Antrieb
der Treibstange 7 wird der FlĂ¼gel 6 schlieĂŸlich
weiterbewegt bis sein FlĂ¼gelĂ¼berschlag 6 zunächst gegen
einen auf dem freien Ende des Anzugsarms 20 angeordneten
Anschlag 29 gelangt. Dabei wird der Anzugsarm 20 von dem
FlĂ¼gelĂ¼berschlag 6 des FlĂ¼gels 2 in eine zurĂ¼ckgezogene,
vollständig im Bereich des Holmes 4 des Rahmens 1 befindliche
Stellung verschwenkt. AnschlieĂŸend gelangt der FlĂ¼gelĂ¼berschlag
6 des FlĂ¼gels 2 gegen den Rahmen 1. Diese
Anzugsstellung ist in Figur 2c dargestellt. Das Anzugsteil
18 ist vollständig Ă¼ber das Anzugselement 19 entlanggeglitten
und befindet sich in einer von dem Anzugselement
19 getrennten Stellung. Der FlĂ¼gel 2 wird von
dem sich an einer Verriegelungskante 30 der SchlieĂŸfalle
11 abstĂ¼tzenden SchlieĂŸzapfen 10 gehalten. In the tightening position of the tightening device shown in FIG.
Figur 3a zeigt eine Anzugseinrichtung 31 bei der ein Anzugsteil
32 als SchlieĂŸzapfen ausgebildet ist. Ein Halteteil
33 eines Anzugselementes 34 der Anzugseinrichtung 31
und eine SchlieĂŸfalle 35 sind einteilig gestaltet. Die
SchlieĂŸfalle 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 Ă¼berlappen sich in
einem Bereich, in welchem sie teilweise Ă¼bereinander angeordnet
sind. Wie bei der Anzugseinrichtung 17 aus Figur
2a ist ein Anzugsarm 40 des Anzugselementes 34 einteilig
mit einem AbstĂ¼tzarm 39 gefertigt und federelastisch in
Richtung des FlĂ¼gels 2 vorgespannt. Bei einer Bewegung
des als SchlieĂŸzapfen 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
FlĂ¼gel 2 bewegt sich dabei auf den Rahmen 1 zu. Bei einer
Weiterbewegung des Anzugselementes 34 nach rechts gelangt
dieses Ă¼ber die Anzugskante 37 der SchlieĂŸfalle 35 hinter
die Verriegelungskante 36. Diese Anzugsstellung ist in
Figur 3c dargestellt. Hierbei wird der FlĂ¼gel 2 von dem
Anzugselement 34 in seiner an dem Rahmen 1 anliegenden
Stellung gehalten. Das Anzugselement 34 liegt mit einem
Anschlag 41 an dem FlĂ¼gelĂ¼berschlag 6 des FlĂ¼gels 2 an
und ist in eine zurĂ¼ckgezogene, vollständig Ă¼ber den Rahmen
1 befindliche Stellung geschwenkt.FIG. 3a shows a tightening
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 FlĂ¼gels 2 vorgesehen
sein. Eine solche bekannte Anzugseinrichtung ist beispielsweise
in den Figuren 2a bis 2c durch die SchlieĂŸfalle
11, dem SchlieĂŸzapfen 10 und der Anzugskante 27
dargestellt. Der FlĂ¼gel 2 wird in der Regel mit mehreren
in den Figuren 2a bis 2c dargestellten SchlieĂŸfallen 11
verriegelt. Beim Anziehen des FlĂ¼gels 2 in eine vorgesehene,
dessen Verriegelung ermöglichende Position genĂ¼gen
in Abhängigkeit von der GrĂ¶ĂŸe des FlĂ¼gels 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 SchlieĂŸzapfen
ausgebildet und lĂ¤ĂŸt 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 FlĂ¼gel 2
an den Rahmen 1. Eine mittlere Anzugsstellung ist in Figur
4b dargestellt. SchlieĂŸlich gelangt das Anzugsteil 45
hinter eine Verriegelungskante 46 einer SchlieĂŸfalle 47
und hält den FlĂ¼gel 2 an dem Rahmen 1. Diese Anzugsstellung
ist in Figur 4c dargestellt. Bei dem Ăœbergang des
Anzugsteils von der in Figur 4b in die in 4c dargestellte
Position wird der FlĂ¼gel von der in Figur 2 dargestellten
Anzugskante 27 der SchlieĂŸfalle 11 bewegt.Figure 4a shows a tightening
Claims (13)
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 true EP1122389A2 (en) | 2001-08-08 |
EP1122389A3 EP1122389A3 (en) | 2006-03-15 |
EP1122389B1 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) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2182149A1 (en) | 2008-10-28 | 2010-05-05 | Aug. Winkhaus GmbH & Co. KG | Pulling device for an espagnolette fitting |
Families Citing this family (1)
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 |
Citations (2)
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 |
DE19515708A1 (en) | 1995-04-28 | 1996-10-31 | Winkhaus Fa August | Display device for windows, doors or the like |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3140855C2 (en) * | 1981-10-14 | 1987-02-12 | Geze Gmbh, 7250 Leonberg | Device for operating a scissor mechanism for the sashes 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 |
-
2000
- 2000-02-04 DE DE10005055A patent/DE10005055A1/en not_active Withdrawn
- 2000-12-19 DE DE50015553T patent/DE50015553D1/en not_active Expired - Lifetime
- 2000-12-19 EP EP00127750A patent/EP1122389B1/en not_active Expired - Lifetime
- 2000-12-19 AT AT00127750T patent/ATE422594T1/en active
- 2000-12-19 ES ES00127750T patent/ES2319499T3/en not_active Expired - Lifetime
- 2000-12-19 DK DK00127750T patent/DK1122389T3/en active
Patent Citations (2)
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 |
DE19515708A1 (en) | 1995-04-28 | 1996-10-31 | Winkhaus Fa August | Display device for windows, doors or the like |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2182149A1 (en) | 2008-10-28 | 2010-05-05 | Aug. Winkhaus GmbH & Co. KG | Pulling device for an espagnolette fitting |
Also Published As
Publication number | Publication date |
---|---|
ES2319499T3 (en) | 2009-05-08 |
DE10005055A1 (en) | 2001-08-09 |
DK1122389T3 (en) | 2009-05-25 |
EP1122389B1 (en) | 2009-02-11 |
EP1122389A3 (en) | 2006-03-15 |
DE50015553D1 (en) | 2009-03-26 |
ATE422594T1 (en) | 2009-02-15 |
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