EP1370742B1 - Structure de fenetre ou de porte - Google Patents

Structure de fenetre ou de porte Download PDF

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Publication number
EP1370742B1
EP1370742B1 EP02737893A EP02737893A EP1370742B1 EP 1370742 B1 EP1370742 B1 EP 1370742B1 EP 02737893 A EP02737893 A EP 02737893A EP 02737893 A EP02737893 A EP 02737893A EP 1370742 B1 EP1370742 B1 EP 1370742B1
Authority
EP
European Patent Office
Prior art keywords
casement
leaf
frame
wing
movement
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
EP02737893A
Other languages
German (de)
English (en)
Other versions
EP1370742A1 (fr
Inventor
Willi Hempelmann
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.)
Veka AG
Original Assignee
Veka AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Veka AG filed Critical Veka AG
Publication of EP1370742A1 publication Critical patent/EP1370742A1/fr
Application granted granted Critical
Publication of EP1370742B1 publication Critical patent/EP1370742B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00—Suspension arrangements for wings
    • E05D15/56—Suspension arrangements for wings with successive different movements
    • E05D15/58—Suspension arrangements for wings with successive different movements with both swinging and sliding movements
    • 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
    • E05D15/28—Suspension arrangements for wings supported on arms movable in horizontal plane
    • E05D15/32—Suspension arrangements for wings supported on arms movable in horizontal plane with two pairs of pivoted arms
    • E05D15/34—Suspension arrangements for wings supported on arms movable in horizontal plane with two pairs of pivoted arms with wings opening parallel to themselves
    • 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
    • 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
    • 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 RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2201/00—Constructional elements; Accessories therefore
    • E05Y2201/60—Suspension or transmission members; Accessories therefore
    • E05Y2201/622—Suspension or transmission members elements
    • E05Y2201/638—Cams; Ramps
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2800/00—Details, accessories and auxiliary operations not otherwise provided for
    • E05Y2800/74—Specific positions
    • E05Y2800/75—Specific positions intermediate
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2900/00—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—Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
    • E05Y2900/148—Windows

Definitions

  • the invention relates to a window or door structure with a frame and a movably mounted on the frame wings, see for example DE 196 03 768 A
  • the invention has the object of providing a Fester- or door structure of this kind so that a motor-driven operation can be easily designed.
  • Fig. 1 shows schematically the stationary frame 1 of a window and a movably mounted wing 2, wherein
  • Fig. 1a shows a parallel lifting the wing 2 from the frame 1, for example, for ventilation purposes.
  • Fig. 1b shows the tilting of the sash 2, which adjoins the parallel lifting of Fig. 1a and
  • Fig. 1c shows the pivoting of the sash 2 after the wing is lifted by a certain amount from the frame 1 in parallel.
  • FIGS. 2 to 21 show in a first embodiment according to FIGS. 2 to 21 different fitting modules on the circumference of the window structure, wherein the fitting modules together with a control element 22 are preferably attached to the wing 2.
  • two fitting modules 3.1, 3.2 and 3.3, 3.4 are provided for parallel lifting of the wing 2 from the frame 1 near the corners of the wing, whose function will be explained below.
  • Kipphebelmodul 4.1 and 4.2 are mounted on both sides in the upper area on the wing 2, which cooperate for tilting the wing 2 with the two lower fitting modules 3.2 and 3.4 for the parallel lifting:
  • a swivel lever module 5 is provided on its upper side, which cooperates with the two fitting modules 3.3 and 3.4 on the right in Fig. 2 side of the wing 2.
  • a drive module 6 is further housed in the region of a handle module 7, which performs other control functions in addition to the usual function of a window handle, as will be explained in more detail below.
  • a sensor module 9 may be attached to the wing 2, which detects the individual functions and positions of the wing relative to the frame 1 and z. B. forwards to a central monitoring and control unit corresponding information.
  • FIG. 3 shows a perspective view of the basic construction of a fitting module 3.1 to 3.4, which among other things controls the parallel lifting of the wing 2 from the frame 1.
  • a circumferential groove 21 portion of a sash profile is reproduced, which may have a per se known cross-sectional configuration, which is not reproduced in detail.
  • a control in the form of a link chain 22 is guided, which has at the individual chain links control pins 23 which protrude parallel to the window plane on the circumference.
  • a plate 24 is attached, on which on the frame 1 in Fig. 2 facing side via a pivot pin 26, a sector element 30 is pivotally mounted.
  • the chain 22 provided with the control pins 23 extends.
  • This sector element 30 has a semicircular sprocket 31 on the periphery of a semicircular disk 32, which is in engagement with the control pins 23 of the chain 22 in the illustration of FIG. With the semicircular disk 32, a circular sector-shaped holding member 33 is fixedly connected, which projects beyond the control pins 23 and is not engaged with these. At an angular distance from the pivot pin 26 recesses 34 and 34 'are formed on the two sides of the holding member, which are formed for receiving a retaining pin 11 (Fig. 4 to 7).
  • this section of the holding element 33 provided with the recesses 34 is arranged at a distance above the sprocket 31 and the control pins 23, by forming a shoulder or a spacer between the semicircular disk 32 and the holding element 33.
  • the sector element 30 with plate 24 is present in all fitting modules 3.1 to 3.4, wherein this sector element is shown schematically in the following figures to illustrate the control functions and the ring gear 31, the holding member 33 projects beyond in the radial direction.
  • Fig. 4 shows z. B. the fitting module 3.2 to explain the holding function of the wing 2 on the frame 1, which is indicated by dashed lines in Fig. 4.
  • two holding pins 11 and 11 ' are mounted at a distance in the circumferential direction, which cooperate with the two recesses 34 and 34' of the holding member 33 on the wing 2 as follows.
  • a horizontally extending guide groove 12 is formed on the frame 1, in which a roller 25 is guided, which is arranged in the Ansich of FIG. 4 in the left lower corner of the plate 24 of the fitting module and on Wing 2 is attached via a shaft 27, wherein the shaft 27 protrudes through a bore in the plate 24 (see Fig. 16).
  • the load of the wing 2 is supported on the frame 1
  • the window from the closed position in Fig. 4 can be opened, there is a pilot movement of the chain 22 from the designated in Fig. 4 with 0 starting position up or down, so that the holding member 33 is slightly pivoted by the chain 22 and one of both retaining pins 11 and 11 'comes free.
  • Fig. 5 shows this pilot motion, in which the chain 22 is moved from the position 0 in the position I down in Fig. 5 to pivot about the sprocket 31, the holding member 33 in the clockwise direction about the pivot pin 26 so far that the paragraph 36 on the upper recess 34 of the retaining element 33 is released from engagement with the upper retaining pin 11.
  • this is simplified by a shortening of the heel 36 shown on the support member 33.
  • the transition between the groove portion of the recess 34 and the shoulder 36 is designed so that in the Pivoting movement of the holding member 33 by the pilot movement of the chain of the upper pin 11 slides along this transition and is released from the shoulder 36.
  • Fig. 6 shows the position of the fitting module 3.2 after a further control movement of the chain 22 down over the distance I to II, wherein the holding member 33 has a pivoting movement in the clockwise direction about 30 ° about the pivot pin 26 executed.
  • the upper end of the retaining element 33 has been removed from the upper retaining pin 11 of the frame 1, while the lower retaining pin 11 'is still in engagement with the recess 34' of the retaining element.
  • the holding member 33 is pivoted clockwise, wherein the lower extension 35 'of the holding element against the lower retaining pin 11' is pressed, so that the Wing 2 is lifted from the frame 1 due to the lever (dotted line) between the lower retaining pin 11 'and the pivot pin 26.
  • the attached to the wing 2 roller 25 is supported in the horizontal guide 12 of the frame 1 from.
  • This control process takes place synchronously by the circulating chain 22 at the four fitting modules 3.1 to 3.4, so that the wing 2 is lifted off the frame 1 in parallel.
  • Fig. 6 shows the maximum lifted position of the wing 2 from the frame 1, wherein the roller 25 is supported at the right end of the horizontal guide 12 of the frame 1 and the frame in this way receives the weight of the lifted wing 2.
  • the chain 22 is moved back by the amount of input tax from the position I to the 0 position, the wing 2 on the lower shoulder 36 'of the support member 33, which is supported on the lower retaining pin 11', on Frame 1 is pressed while the upper retaining pin 11 comes to lie in the recess 34 of the support member so that the upper shoulder 36 in the same position as the lower shoulder 36 'on the retaining pin 11 is supported.
  • a provided between the frame 1 and wing 2 elastic seal is compressed, wherein the bias of the seal a concern of the two retaining pins 11 and 11 'at the shoulders 36 and 36th 'of the holding member 33, and thus ensures a tight closed position of the window.
  • the timing chain 22 can be moved from the 0 position up or down by the amount of pilot motion from 0 to I, so that the holding member 33 of one of the two retaining pins 11 or 11 'is released.
  • the chain 22 has been moved to a pre-selection position for tilting the window from the 0 position down to the I position.
  • the plate 24 with sector element 30 (FIG. 3) is pivotably mounted on the profile of the wing 2 by virtue of the fact that the roller 25 is fastened to the profile of the wing 2 via the shaft 27 (FIG. 14), the shaft 27 being inserted through a bore in FIG the plate 24 is guided and rotatably carries the roller 25 at the free end.
  • the plate 24 with the holding element 33 can thus be pivoted about the shaft 27 of the roller 25 relative to the wing 2, as shown in FIG. 7.
  • a parallel to the roller 25 protruding pin 13 is fixed above the horizontal guide 12 at its right end, as is schematically indicated in Figs. 4 and 5.
  • This pin 13 serves to hold the plate 24 in the vertical position relative to the tilted wing 2 ( Figure 7), as will be explained below.
  • the Kipphebelmodule 4.1 and 4.2 have already been activated or brought into engagement with the timing chain, whereby in the further control movement of the chain 22 from the position II to the position III (Fig 7), the upper part of the wing 2 is led away from the frame via the rocker arms 40 of the tilting modules (FIGS. 9 and 10), so that the lower part of the wing 2 pivots about the shaft 27 into the position of FIGS while on the pin 13, the plate 24 in the vertical Position is maintained so that the chain 22 can be released from engagement with the ring gear 31 of the support member 33.
  • the rollers 25 on the two lower fitting modules 3.1 and 3.4 are in the tilted position of FIG. 7 in the horizontal guide 12 of the frame 1, which has a predetermined distance from the lower corner of the wing 2, while the rollers 25 on the upper fitting modules 3.1 and 3.3 detached from the frame and the rocker arm modules 4.1 and 4.2 have taken over the support and guidance of the upper part of the wing 2.
  • the plate 24 of the two upper fitting modules 3.1 and 3.3 is also held in the tilted position of FIG.
  • FIGS. 8 and 9 show the fitting module 3.1 mounted above the fitting module 3.2 of FIGS. 4 to 7, wherein FIG. 8 corresponds to the position in FIG. 6 and FIG. 9 shows the lifting of the fitting module from the frame 1 when the tilting movement of the frame starts Wing 2 shows before the full tilt position of Fig. 7 is reached.
  • a control cam 320 is formed on the sector element 30 about the pivot pin 26, in which a wing 2 attached to the pin 210 engages.
  • the control cam 320 is formed on a radius about the pivot pin 26 and has radially outwardly bent ends 321.
  • the control cam 320 is symmetrical about the center line of the sector element 30 because of the use of the same fitting module on the two sides of the wing, wherein the pin 210 in the FIG.
  • the tilting movement of the wing 2 is initiated by the Kipphebelmodule 4.1 and 4.2, in which the entire fitting module 3.1 detached from the frame 1, as shown in FIG. 9.
  • the pin 210 attached to the wing 2 comes to lie in the upper bent end 321 of the control cam 320, as shown in FIG.
  • the chain 22 is still in engagement with the ring gear 31, so that the plate 24 is held in the vertical position.
  • the chain 22 is released from engagement with the ring gear 31, wherein a further pivoting of the plate 24 is prevented by contact of the pin 210 at the end of the control cam 320.
  • the plate 24 retains the relative position shown in FIG. 9 relative to the wing 2, in which the plate 24 is not pivoted so strongly relative to the wing 2 as in FIG.
  • this reduced pivoting position of FIG. 9 is sufficient to produce the same engagement conditions between timing chain 22 and ring gear 31 on the upper fitting module 3.1 when tilting back the wing 2 from the maximum tilting position as on the lower fitting module 3.2.
  • the holding elements 33 on the lower fitting modules 3.2 and 3.4 are no longer active with the lower retaining pin 11 'of the frame 1 in engagement. They are held in the position of FIG. 7 by the link 37 supported on the pin 13 of the frame.
  • the support of the wing 2 takes place solely on the rollers 25 in the horizontal guide 12 under the guidance of the tilting modules 4.1 and 4.2.
  • the sprocket 31 detached from the chain, so that the holding element 33 in the position of Fig. 7 and 9 on all four fitting modules 3: 1 to 3.4 no longer functions.
  • the tilting movement of the wing 2 according to Fig. 1b is initiated by the two Kipphebelmodule 4.1 and 4.2 on the two sides of the wing 2 (Fig. 2), while the timing chain 22 to the fitting modules 3.1 to 3.4 corresponding to the position in Fig. 6 and 8 is still engaged with the ring gear 31.
  • the end of the control movement of the chain 22 in the position II of FIG. 6 overlaps with the activation of the rocker arm modules 4.1 and 4.2, so that the timing chain 22 is still in engagement with the sprocket 31 of the fitting modules as shown in FIG.
  • Fig. 10 shows a perspective view of a wing 2 attached to the two sides of the component of the rocker arm module, which is formed substantially in the form of a rectangular plate 41.
  • a longitudinal groove is designated, in which the chain 22 is guided.
  • a gear 43 is engaged, which is fixedly connected to an underlying smaller gear 44 which engages with a rack 45 which is formed along one side of an elongated recess 46, along the the smaller gear 44 is movable, while the overlying gear 43 rests with a larger diameter on the edges of this recess 46.
  • the two gears 43 and 44 are fixedly connected to each other by a screw 47, the downwardly projecting shaft is guided in a guide groove 48 which extends along the bottom of the recess 46. At the upper end 49 of the recess 46 or the guide groove 48 in FIG. 10, this is slightly bent.
  • Fig. 11 and 12 show the reproduced in Fig. 10 component of the rocker arm module on the wing 2 in a schematic representation, wherein the wing 2 via a rocker arm 40 with the frame 1 are connected as follows.
  • FIG. 13a to 13e show a part of the rocker arm module with a catch element 400, which is articulated on the end of the lever 40, which faces the gears 43, 44.
  • the frame 1 is indicated by dash-dotted lines and the wing by solid lines.
  • Fig. 14 shows a sectional view in the region of the articulation between the lever 40 and catch element 400, which is connected via a pivot pin 402 with the lever 40, wherein the pivot pin 402 projects on both sides and engages in a U-shaped groove 14 on the frame, the is indicated in Fig. 13.
  • the pivot pin 402 projects on both sides and engages in a U-shaped groove 14 on the frame, the is indicated in Fig. 13.
  • On the opposite side of the pivot pin 402 is slightly longer and it protrudes into a guide groove 29 on the wing 2, which is open against the guide groove 14 on the frame 1.
  • the guide groove 14 is open on the frame 1 on the right side.
  • the guide groove 29 formed in the same way on the wing 2 to the left, so that the pivot pin 402 can be detached from the wing when it is fixed to the frame 1.
  • the catch element 400 has two grooves 401 and 401 ', which extend from the two sides of the sector-shaped catch element on a radius around the pivot pin 402 and terminate at a distance from the center line 403 of the catch element, on the radially outer end of a control extension 404 protrudes, which is in the position 0 in Fig. 13a with the chain 22 is engaged.
  • a catch pin 405 ( Figure 14) which engages the catch element.
  • a catch pin 406 is attached to the wing 2, which also engages with the catch element 400.
  • the timing chain 22 In the closed position of the window according to FIG. 13a, the timing chain 22 is in the position 0, wherein the center line 403 of the catch element and thus the control extension 404 is horizontal.
  • the two catch pins 405 and 406 In the open end of the grooves 401 and 401 '.
  • the pivot pin 402 is located in the guide 14 on the frame 1 and in the not shown in FIG. 13 guide 29 on the wing 2. In the pilot control movement of the chain 22 from the position 0 to the position I for tilting, as shown in FIG.
  • the catch element 400 is pivoted about the pivot pin 402 due to the engagement with the chain in a clockwise direction, so that the lower catch pin 405 of the frame 1 at the inner end of the groove 401 'is applied while the catch element 400 has completely detached from the upper catch pin 406 of the wing.
  • the rocker arm 40 is connected to the frame 1 in that the support pin 402 can not move out of the guide 14 on the frame 1 due to the support of the frame-side lower catch pin 405 in the groove 401 'of the catch element ,
  • Fig. 13c shows the preselection of the timing chain 22 from the position 0 to the position I 'to pivot the wing, which will be explained in more detail below.
  • the catch element 400 is pivoted by the opposite movement of the chain 22 in the counterclockwise direction, so that the upper wing-side catch pin 406 comes to rest in the upper groove 401 of the catch element, whereby in the pivotal movement described below the wing 2 relative to the frame 1 of the rocker arm 40th held on the wing 2 by fitting that is held on the engagement of the Fangelements 400 with the wing-side catch pin 406 of the pivot pin 402 in the guide groove 29 on the wing 2 (corresponding to the holding function in Fig. 13b in the guide groove 14 of the frame), so that when pivoting the wing, the pivot pin 402 is moved out of the guide groove 14 of the frame to the right in Fig. 13 with the wing.
  • Fig. 11 shows the onset of the parallel lifting movement of the wing 2 from the frame 1, in which the rocker arm 40 is pivoted clockwise about the pivot pin 402 fixed to the frame 1, so that the gear 43 engages with the control pins 23 of the chain 22.
  • FIG. 12 shows the tilting position of the rocker arm module, in which the shaft of the connecting screw between the gears 43 and 44 at the lower end of the guide groove 48 abuts.
  • FIG. 12 shows only the lower fitting module 3.2 in relation to the rocker arm module 4.1.
  • the intermediate upper fitting module 3.1 is located on the wing 2 in the position of FIG. 9th
  • Fig. 12 shows the wing 2 from the left side in Fig. 2 with the lower fitting module 3.2 and the rocker arm module 4.1. Since in the control movement of the revolving chain 22 on this side of the wing, the chain moves downwards, a control movement of the chain 22 results on the opposite right side of the wing upwards.
  • Such a transmission between the two gears 43 and 44, which converts the rotational movement of the one gear into a counter-movement on the other gear can be formed in various ways and is not shown in detail in the figures.
  • the wing Before a pivoting movement of the wing 2 of FIG. 1c can be initiated, the wing must be transferred to the closed position of FIG. 4 by the chain 22 is moved back from the position II to the 0 position. As a result, the holding element 33 is driven on the fitting modules 3.1 to 3.4 by the chain and pivoted counterclockwise, so that the retrograde movement is performed, which is carried out in the parallel lifting of the wing 2 from the frame 1.
  • rocker arm 40 on the wing 2 is fixed by the pre-control movement of the chain on the two rocker arm modules 4.1 and 4.2 (FIG. 13c), so that the pivot pin 402 can be moved out of the guide groove 14 of the frame 1 to the right in FIG. 13c. This takes place synchronously on both rocker arm modules 4.1 and 4.2.
  • pivot lever module 5 (Fig. 2) is activated in such a way that a pivot lever 50 is fixed with one end to the frame 1, while he is with the other end on the wing 2 is articulated.
  • the swivel lever module 5 may be formed in the same way as the rocker arm module 4.1, wherein the frame-side end of the pivot lever 50 is set in a groove on the frame via a catch element by the preselection of the chain 22 in the direction of pivoting, while in the pre-control movement of the chain in the direction of tilting the pivot lever 50 is fixed to the wing 2, as has been explained with reference to FIGS. 13 and 14.
  • Fig. 15 shows a view of the fitting module 3.4 from the right in Fig. 2, wherein the frame 1 is again indicated by dashed lines.
  • the handlebar 37 is not horizontally articulated to the vertical displacement of the support element 38 in the starting position next to the pivot pin 26 on the holding element 33, but in Fig. 15 left above the pivot 26 such that in the initial position of the holding member 33 as shown in FIG. 4, the upper pivot point 37 'is in line with the pivot pin 26, as shown in FIG. 19 shows. 15 shows the preselection position I 'of the holding element 33, in which the upper shoulder 36 of the holding element has come free from the retaining pin 11 fastened to the frame 1.
  • the position of the retaining element 33 in FIG. 15 corresponds to that in FIG. 5, but with the reverse pilot movement of the chain 22.
  • Fig. 16 shows a view of the fitting module from the left in Fig. 15.
  • a bearing block 300 is mounted adjacent to the holding member 33 which is disposed on a in Fig. 15 extending to the left extension of the plate 24 and extends with an extension approach 300 'across the width of the plate 24.
  • the bearing block 300 with projection 300 ' engages over a shoulder 305 on the frame 1 (FIG. 16) in which the horizontal guide 12 for the roller 25 is formed.
  • a bearing ball 302 is attached to the profile of the wing, in which the chain 22 is guided.
  • a positioning screw 303 is screwed into this from above, which has a contact surface corresponding to the ball radius.
  • Fig. 15 shows at 304 a section on the bearing block 300, which allows a pivoting movement of the projection 301 on the wing relative to the bearing block. In the position of Figs. 16 and 17, the wing is still in the contact position on the frame 1.
  • the holding member 33 presses with the lower extension 35' from the lower retaining pin 11 'of the frame first 15, so that the roller 25 in Fig. 15 is moved so far to the left in the horizontal guide 12 until the bearing block 300 protrudes with the pivot joint from the front plane of the frame 1, as already Fig. 15 independently shows that in this Fig. 15, the holding member 33 is shown only in the pre-selection position.
  • Fig. 18 shows the corresponding position of the bearing block 300 relative to the frame 1, while Fig. 17 shows the starting position, from which the pivot joint in Fig. 17 is moved to the left.
  • FIGS. 17 and 18 show a view of the fitting module from below in FIG. 15.
  • the wing 2 with the fitting module 3.4 mounted thereon via the pivoting joint is displaced from the position of FIG. 17 to the position of FIG. 18 to the left, the wing 2 being lifted off the frame 1 only so far until the pivoting joint is exposed.
  • the pivot lever module 5 in engagement with the chain 22, wherein the pivot lever 50 is fixed to the frame 1, so that by the further control movement of the chain 22 from the position II 'in the position III' of the wing 2 by the pivot lever 50 is pivoted in the pivoting position of FIG. 18.
  • the control pins 23 of the chain 22 are lifted transversely to the plane of the ring gear 31 on the support member 33 thereof, as is apparent from Fig. 17 and 18, so that the release of the chain 22 from the ring gear 31 can be made from an engaged position, as in Fig. 15 is shown.
  • the control movement of the chain 22 from the preset position I 'to the position II' is designed to be shorter than the control movement from the position I to the position II when tilting.
  • the required for pivoting the wing 2 chain movement from the position II 'in the position III' in which the wing 2 is fully open can be made longer to perform a corresponding pivoting range on the pivot lever 50.
  • the pivot lever 50 which is indicated schematically in Fig. 2, in the form of a reproduced in Fig. 23 multi-articulated pivot lever 50, in which the articulation points on the frame 1 on the one hand and on the wing 2 on the other face each other, as in 51 and 52 is shown in FIG.
  • pivoting lever 50 may be provided to allow a large pivoting range over at least 90 ° between the sash and the frame.
  • pivoting lever 50 are hinged to two articulated arms 501 and 502 in the central region shorter links 503 and 504, which in turn are hinged together with the ends, so that in the illustration of Fig. 23 is a diamond-shaped Arrangement between these links results.
  • the roller 25 is fixed in the pivot position of FIG. 18 in the horizontal guide 12 and thus the fitting module relative to the frame 1, the frame 1 on the horizontal guide 12 in the region of the two fitting modules 3.3 and 3.4 another pin 15th (Fig. 15) is provided which engages with the support member 38 while engaging the shaft 27 of the roller 25, so that the plate 24 is secured in the pivot position of the fitting module against tilting relative to the wing 2.
  • Fig. 15 of the attached to the frame 1 pin is referred to, which serves in the maximum lifted position of the blade of FIG. 6 for holding the plate 24 relative to the wing 2 during the tilting movement, as with reference to FIGS. 6 and 7 was explained.
  • FIGS. 19 and 20 show only relative positions of the retaining element 33 of the fitting module 3.4, FIG. 19 showing the closed position corresponding to FIG. 4, in which the link 37 extends between the raised position of the supporting element 38 via the pivot pin 26 to the upper pivot point 37 'extends to the sector element 30.
  • the guide 28 on the plate 24 has an interruption 208, so that the horizontally relative to the frame 1 with the plate 24 guided guide 28 can be moved over the pin 15, which serves to fix the pivot position, when the fitting module 3.4 in the tilted position 19, in which engagement with the pin 13 on the frame as shown in FIGS. 6 and 7 takes place.
  • the sector element 30 is pivoted counterclockwise out of the position of FIG. 19, whereby the support element 38, due to the shorter path that the link 37 executes is lowered earlier than in the pivotal movement of the sector member 30 in the clockwise direction and the oblique groove 39 on the support member 38 already comes into engagement with the frame-side pin 15 when the pivot position is reached in Fig. 15.
  • the fitting module 3.3 has the sector element 30 in the reproduced in Figs. 8 and 9 control cam 320 for fixing the plate 24 in the tilted position and at the same time a handlebar 37 which cooperates via the support member 38 with the frame-side pin 15 corresponding to FIG. 15, so that the upper fitting module 3.3 is fixed in the pivot position on the frame 1.
  • the frame-side pin 13 for the tilted position is not present, so that the support element 38 can not be fixed to the frame in the tilted position.
  • a transition from the pivot position to a tilted position of the wing is in turn only possible when the wing 2 is transferred from the pivot position to the closed position of FIG. 4 and 19 with the chain position 0, from which a preselection in the direction of tilting with the following Movements can be made.
  • An incorrect operation of the window is thus excluded after both tilting and pivoting must be assumed from the position 0 of the chain, in each case in the opposite direction from the 0 position.
  • FIG. 21 schematically shows the drive module 6 (FIG. 2), which has an electric motor 60 and a worm 61 driven by it.
  • the worm drives two spaced worm wheels, which are not shown in FIG. 21 and drive the two gears 62, which are engaged with the bearing pins 203 of the chain 22 in FIG. 21a.
  • the worm wheels are attached to the two gears 62 and to a guide member 63 which extends parallel to the worm 61.
  • This guide element 63 is supported via two spring plates 64 and 64 'on support members 202 on the wing 2, wherein between the two spring plates, which are held on a spring ring or a transverse pin 65 on the shaft of the guide element 63, a compression spring 66 is arranged.
  • the guide member 63 can move with the two gears 62 mounted thereon both to the left and to the right against the force of the spring 66.
  • This assembly of motor 60, worm 61 and guide member 63 with gears 62 is guided on a component 67 of the wing 2 in guides 68 so that the entire drive unit from the position in Fig. 21a transverse to the chain 22 in the position of Fig. 21b can be lifted, in which the gears 62 are no longer in engagement with the timing chain 22.
  • Fig. 21a and Fig. 21b On the left in Fig. 21a and Fig. 21b is an end view of the structure shown schematically.
  • the gears 62 are in this case formed so that they engage with the laterally on the chain links projecting bearing pins 203 which slide on a support surface 69 of the wing 2, so that the chain 22 is supported on engagement of the two gears 62 on a repository.
  • the supported via the spring 66 guide member 63 has a dual function.
  • a shock may occur when the gears engage, particularly when the chain is slightly moving. This pushing movement is intercepted by the spring 66 and a corresponding deflection movement of the guide element 63.
  • the chain can also be manually controlled by the handle module 7, which is shown in Fig. 22 in a schematic representation.
  • a handle 70 is pivotally mounted to which a release button 71 is attached, which can be pressed with the fingers of the handle 70 embracing hand to a non-illustrated linkage, the drive unit of motor 60, worm 61 and guide member 63 with gears 62 to move from the engaged position in Fig. 21a in the position of Fig. 21b.
  • a spring is provided between component 67 and drive unit, which acts on the drive unit in the direction of engagement and must be overcome by pressing the release button 71.
  • the handle 70 is aligned downwardly on the wing 2 corresponding to the usual closed position of a window. If the window is to be opened by hand, the handle 70 is pivoted to the horizontal position in which usually the window is opened by pivoting the wing, or pivoted in the pivoting position by 180 ° upwards, in which usually the window by tilting the Wing is to be opened.
  • a connecting link, not shown, between the handle 70 and the guide element 63 displaces it against the force of the spring 66 in one or the other direction, so that via the gears 62, a preselection position for tilting or pivoting on the chain 22 is executed according to the previously described positions I and I '.
  • buttons 72 mounted on the handle module 7 can be controlled by, for example, pressing the UP button, whereupon the motor 60 is driven via electrical connecting lines to move the wing 2 from the frame 1 lift and according to the preselection position by the handle 70 in the tilted or pivot position to convict.
  • 7 more keys are provided on the handle module, as they also Fig. 24 show.
  • the release button 71 must be pressed to disengage the drive unit from the chain 22, as shown in Fig. 21b. Then, by pulling on the handle 70, the wing 2 is lifted parallel from the frame 1, wherein due to the engagement of the fitting modules 3.1 to 3.4 with the chain 22 by the movement of the wing 2 by hand, the fitting modules are driven so that the holding elements 33, the are solved by the preselection of the handle 70 of the upper and lower retaining pins 11, 11 ', drive the chain 22, so that in this case the control movement of the chain is performed on the fitting elements.
  • the position of the wing 2 relative to the frame 1 is at any moment determined by the position of the chain 22 regardless of whether the chain 22 is driven by the motor 60 or by hand via the handle 70.
  • Fig. 22 shows five keys 72, by means of which the various functions or movements of the sash can be initiated by pressing these keys. These buttons or sensor fields are connected via an unillustrated control electronics with the drive motor 60 in connection, so that the corresponding drive movement can be triggered on the motor 60 by pressing the respective buttons.
  • Fig. 24 shows in the form of symbols the various functions on the keys such as "parallel lifting”, “tilting” and “panning” and “opening windows” and “closing windows” on a schematically represented remote control unit 100.
  • the provided on the handle module 7 keys can also be provided on another part of the wing, for example on the sash profile.
  • the preselection of the handle 70 in the tilting or pivoting position has priority over a control of the motor 60 in such a way that, for example, in a tilted position of the handle 70 by driving the motor 60 can not be moved directly into a pivot position.
  • a connection, not shown, via electrical lines between handle module 7 and drive module 6 is present, so that a tilted position of the handle 70 blocks, for example, a drive of the motor 60 in the direction of pivoting, which could be triggered by a remote control 100 from.
  • a flexible band can be provided, to which corresponding control pins are at least partially attached.
  • a toothed belt may be provided instead of a chain.
  • chain portions may be connected to each other via a spring element to compensate for an elongation of the control element by the action of temperature.
  • a spring element is designed so that it is not affected by the forces of the adjustment movements by the motor drive and by the manual operation or executes no change in length, but only by significantly higher forces, such as those that occur in temperature changes.
  • a plurality of drive modules can be provided on the circumference of a wing 2, in particular if it is a larger door leaf.
  • several of the described fitting modules 3.1 to 3.4 can also be provided, for example three on each side of the wing. Due to the predetermined sequence of the individual chain positions out of the 0 position in one direction or the other, it is also possible to control all functions of the window with only a single drive module 6 or a single drive motor 60.
  • the control of the wing 2 can be performed by key control on Griffinodul 7, by remote control, for example by means of an infrared control device or from a control center from which all windows of a building can be controlled in this way.
  • remote control for example by means of an infrared control device or from a control center from which all windows of a building can be controlled in this way.
  • a laser pointer or the like is expediently provided on the remote control device, by means of which a corresponding sensor can be activated on the individual windows, so that by aiming with the remote control device 100 to the relevant Window to be opened addresses only this window and not the adjacent windows.
  • Fig. 2 only recesses on the frame 1 and the profile of the wing 2 are indicated for the supply module 8.
  • the supply module is expediently arranged at a position of the circumference of the wing on which as few relative movements as possible are made to the frame 1. Therefore, the supply module z. B. positioned above the lower right corner.
  • the supply module not shown, includes supply cable and connector, which are inserted into the profile of the wing, wherein the cables are connected to the motor 60 of the drive module 6.
  • the control electronics may be formed on the supply module or on the drive module. The connection of the supply module on the wing with the frame 1 via connecting cable with plugs at the ends.
  • the shaft 27 on the fitting module 3.1 to 3.4 can also be determined by a spring-loaded detent in the position of FIG. 6, in which the wing occupies the maximum lifted position parallel to the frame 1.
  • the sensor module 9 is preferably provided at a corner of the window structure, occur at the least adjusting movements of the wing. Therefore, the sensor module z. B. attached to the lower right corner.
  • control in the form of the chain 22 with the various fitting modules on the wing 2 is mounted. It is also possible to attach the encircling control to the frame 1 controlled by these fitting modules, however, the attachment to the wing 2 in terms of installation and repair or replacement of individual components of advantage.
  • the engagement elements can be formed on the individual fitting modules in a different manner than shown.
  • a worm spindle for moving a fitting part may be provided or the like.
  • roller 25 which supports the load of the wing on the frame
  • a lever construction can be provided to support the wing on the frame.
  • the energy supply to the housed in the airfoil drive unit can also be done without lines, for example by inductive means.
  • control signals can be transmitted via radio to the control electronics or the drive unit, so that the control performs the corresponding control movements, so that it does not need a power supply module with electrical lines between the wing and frame.
  • a plurality of sensors may be provided on the wing periphery to directly scan the position of the wing. Due to the fact that all movement sequences of the blade relative to the frame are clearly defined by the sequential sequence of control movements of the chain 22 starting from the starting position 0 in one or the other circumferential direction, only a single sensor, for example the one indicated at 9 in FIG Sensor be provided, which is in engagement with the chain 22 and indirectly determined by the scanned position of the chain 22 relative to the starting position 0 and relative to the wing whose position. This uniqueness of the chain movement also prevents misoperation of the wing.
  • the pre-control movement of the chain 22 by the handle 70 can also be carried out in such a way that the pivoting of the handle 70 from the closed position to the tilting or pivoting position the release button 71 is pressed and a coupling element between the handle 70 and chain 22 this through the Pivoting movement of the handle in the pilot position I or I 'is moved while the drive unit is disengaged by the release button 71 of the chain. If then the window is to be opened by means of the handle, this coupling device is also released from the chain 22, so that it can be moved freely by the hand movement on the wing on the fitting elements. For this coupling between the handle 70 and chain 22 for carrying out the pilot movement with the drive unit disengaged, an additional actuating device can be provided.
  • Figs. 25 to 35 show a preferred embodiment of fitting modules on a window structure, wherein the same reference numerals as in the preceding figures are used for the same components.
  • the wing 2 of the window performs the movements shown in FIGS. 1a-1c relative to the frame 1.
  • Fig. 25 shows, corresponding to Fig. 2 shows schematically the arrangement of the various fitting modules on the periphery of the window assembly, with respect to the embodiment of Fig. 2, the Kipphebelmodule 4.1 and 4.2 omitted and the drive module 6 is arranged on the pivot lever module 5, which also fulfills the Kipphebelfunktion.
  • the Kipphebelmodule 4.1 and 4.2 omitted and the drive module 6 is arranged on the pivot lever module 5, which also fulfills the Kipphebelfunktion.
  • the fitting module 3.1 comprises a control element 22 connected to the spool 102, of which in the illustrated embodiment, four guide pin 103rd protrude, which engage in slots 104 of a plate-shaped fitting part 105 which is fixedly mounted on the wing 2 of the window, as shown in FIG. 31.
  • the spool 102 has a in Fig. 27 reproduced in detail control groove 106, which is designed approximately V-shaped in this embodiment and in which the retaining pin 101 of the frame 1 engages.
  • This retaining pin 101 also engages in a horizontal groove 107 on the fitting part 105, on which the spool 102 is slidably guided in the direction of movement of the control element 22.
  • the guided in a circumferential groove of the wing 2 control 22 may be formed as a band, chain or rope.
  • Fig. 27a shows schematically a side view of the fitting module 3.1 in the locking position, in which the retaining pin 101 of the frame 1 at the inner end of the horizontal groove 107 of the wing-fixed fitting 105 and at the same time at the vertex 106.1 of the cam 106 of the spool 102.
  • the cam 106 is at the vertex 106.1 transverse to the horizontal groove 107 somewhat flattened, so that the retaining pin 101 can assume a stable position in the locked position of the window.
  • Fig. 27b shows a position of the fitting module 3.1 during pivoting of the wing 2 relative to the frame 1, wherein the retaining pin 101 of the frame is located in a horizontal portion 106.3 of the cam 106, which is connected via an inclined portion 106.2 with the vertex 106.1.
  • This relative position in Fig. 27b corresponds to the position in which the wing 2 is unlocked from the frame 1 and it is caused by a sliding movement of the spool 102 upwardly from the position in Fig. 27a, wherein the spool 102 by means of the control element 22 through the Drive motor or manually on the handle module 7 in the direction of pivoting the wing was moved upwards.
  • FIG. 27c shows a tilted position of the fitting module 3.1 after the control slide 102 has been moved downwards by the drive module 6 or the handle module 7 from the locking position in FIG. 27a.
  • the retaining pin 101 moves along an inclined portion 106.4 of the control cam on the spool 102, while the retaining pin 101 moves simultaneously in the horizontal direction along the horizontal groove 107 of the fitting 105.
  • the longer section 106.4 of the control groove is open on the left side via a short section 106.5, so that during the further tilting movement of the wing, the retaining pin 101 can come loose from the horizontal groove 107 and the control groove 106, as in FIG Fig. 27d shows.
  • the two inclined sections 106.2 and 106.4 have substantially the same inclination relative to the horizontal and also the same length. But they can also be designed differently.
  • the section 106.4 of the control cam corresponding to the lower section 106.2 serves to unlock the sash from the frame 1 according to FIG. 27b (position 1 in FIG. 34a).
  • the extended inclined portion 106.4 serves to guide the retaining pin 101 on the wing 2 in parallel lifting and in the tilting movement, while the retaining pin 101 in the horizontal groove 107 still carries the load of the wing 2, whereupon towards the end of the movement of the retaining pin 101 to the left end of Horizontal groove 107 and in the short horizontal section 106.5 of the control cam passes, from which the retaining pin 101 can solve the fitting module 3.1, as shown in FIG. 27c and d show.
  • Fig. 28 schematically shows the different configurations, wherein all the positions represent the locking position, from which the retaining pin 101 moves in the upper or lower portion of the cam groove 106, while moving in the horizontal direction in the cam groove 107.
  • Fig. 28a corresponds to the embodiment of the fitting module 3.1, in which the two legs of the approximately V-shaped cam groove 106 are open at the outer end as well as the horizontal groove 107 on the fitting part 105, so that the retaining pin 101 can be detached from the frame 1 both in the pivoting as well as in the tilted position of the wing.
  • the position in Fig. 28a corresponds to the locking position in Fig. 27a.
  • Fig. 28b shows the shape of the cam groove 106 on the fitting module 3.2, where the wing 2 must be kept in the tilted position on the frame 1, while in the pivot position of the wing, the fitting module must be 3.2 detached from the frame 1. Therefore, the upper end 106.6 of the inclined portion 106.4 of the cam is closed on the fitting module 3.2 so that in the tilted position of the wing of the holding pin 101 of the frame is held in fitting module 3.2 by the retaining pin 101 is applied to the closed end 106.6 of the cam, while in the Pivoting the retaining pin 101 can solve the fitting module 3.2 through the lower, open portion 106.3 of the cam.
  • Fig. 27c shows at the closed end 106.6 of the upper inclined portion 106.4 of the cam groove the tilting position of the wing 2 relative to the frame 1 on the fitting module 3.2, wherein the retaining pin 101 is held by the closed end 106.6 of the cam in the fitting module, while at the same time the load of the wing 2 supported on the retaining pin 101 via the horizontal groove 107.
  • Fig. 28c shows the shape of the cam 106 on the fitting module 3.3, where the retaining pin 101 in the tilted position of the wing 2 must solve the fitting module, while in the pivot position of the wing of the retaining pin 101 must be kept close to the fitting module.
  • the lower portions of the cam 106 in Figs. 28c and d correspond to the upper portions of the cam on the fitting modules 3.1 and 3.2 of Fig. 28a and b, therefore, because the spool 102 on the right side of Wing is moved upward when the spool 102 is moved to the left side of the wing down and vice versa. Therefore, in Fig.
  • the lower leg 106.4 and 106.5 of the control groove corresponds to the upper leg in Fig. 28a, because when tilting the wing, the fitting module 3.3 must be detached from the frame 1.
  • the upper leg 106.2 which corresponds to the lower section 106.2 on the two left fitting modules 3.1 and 3.2, is provided with a closed end 106.7 in FIG Pivoting position of the wing, the connection between the wing and frame is maintained that the retaining pin 101 rests after unlocking at the end 106.7 of the cam, while it is held in the horizontal groove 107 at the same time.
  • the length of the upper portion 106.2 in Fig. 28c corresponds to the length of the lower portion 106.2 in Fig. 28a and the distance required to unlock the sash from the frame. After unlocking the wing of the retaining pin 101 comes at the closed end 106.7 of the cam groove for concern, so that it is held on the fitting module 3.1, so then a pivotal movement of the wing 2 can be introduced relative to the frame 1.
  • Fig. 28 shows by the arrows “tilting” and “pivoting” on the fitting modules 3.1 and 3.2 and in the opposite direction to the fitting modules 3.3 and 3.4 by the opposite movement of the control element 22 resulting opposite configuration of the control cam 106th
  • FIG. 28d shows the shape of the control groove 106 on the fitting module 3.4, on which the wing 2 is not detached from the frame 1 in any position. Therefore, the horizontal groove 107 is closed at the left end, so that the retaining pin 101 can not solve the fitting module 3.4 and the weight of the wing 2 is supported in each position on the retaining pin 101 of the frame. Furthermore, the two sections 106.2 and 106.4 of the control groove 106 are formed closed at the ends.
  • the section 106.4 corresponds to the upper section 106.4 in Fig. 27b, being held by the closed end 106.6 of the retaining pin 101 in the unlocked position in the fitting module 3.4 (as shown in Fig. 27c).
  • the upper, shortened limb 106.2 of the control groove in FIG. 28d corresponds to the embodiment in FIG. 28c.
  • Fig. 29 shows a sectional view through the structure of the fitting modules, wherein on the retaining pin 101 of the frame 1, two roller bearings 101.1 and 101.2 are mounted of different diameters.
  • the larger-diameter roller bearing 101.1 is located in the horizontal groove 107 of the fitting 105, while the smaller-diameter roller bearing 101.2 engages with the cam groove 106 of the spool 102.
  • Fig. 30 shows schematically a sectional view corresponding to Fig. 29, wherein the attachment of the plate-shaped fitting part 105 is indicated on the wing 2.
  • the spool 102 is guided by the pins 103 in the vertical guide slots 104 (FIG. 27) of the fitting 105, with an engagement member 108 attached to the spool 102 which engages the schematically indicated by a double-headed control 22 which is in a groove on the wing 2 is slidably guided on the circumference.
  • a fitting module combines a total of three guides, a vertical guide of the spool 102, a horizontal guide of the retaining pin 101 in the fitting 105 and the guide of the retaining pin 101 in the cam 106.
  • the fitting 105 may be formed overall as a flat housing, in which the spool 102 is guided.
  • FIG. 31 and 32 show schematically a view from above of one of the fitting modules 3.3 and 3.4 on the right side of the wing, on which a hinge must be present between frame 1 and wing 2 in order to allow a pivoting movement of the wing.
  • a part of a hinge 109, whose other part is connected to the wing 2 is fastened respectively to the fitting module 3.3 and 3.4 or to its fitting part 105.
  • Fig. 31a and Fig. 32a show the fitting module in the locking position, in which the wing 2 rests against the frame 1 or lies in the frame.
  • Fig. 31b and Fig. 32c show a pivotal position of the wing 2 of about 45 °.
  • a bow 110 which is curved concentrically about the hinge axis is fastened, which engages in a recess of the band-shaped control element 22.
  • This bracket 110 corresponds to the reproduced in Fig. 30 engaging member 108 between valve spool 102 and control element 22 through this bracket 110 is maintained in each pivot position of the wing 2, a connection between the control element 22 and spool 102, so that in each position of the wing 2, the relative position between spool 102 and control 22 is defined.
  • Fig. 32b shows the wing 2 in the lifted parallel from the frame 1 position in which the outside of the fitting module mounted hinge 109 is lifted from the frame 1, whereupon the pivoting movement is initiated, as shown in FIG. 32c.
  • Fig. 31 is denoted by 2.1 a plate of the hinge 109 which is fixed to the wing 2, while the fitting module 3.3 or 3.4 forms the other plate of the hinge 109, which is held in the parallel raised position of the wing on the frame, so that the weight of the wing is supported on the frame via the retaining pin 101.
  • Fig. 33 shows schematically a combined pivot-rocker module 5 in a pivoting position of the wing 2 in Fig. 33b and in a tilted position in Fig. 33a, wherein schematically the fitting 105 is indicated with the horizontal groove 107 on the upper fitting modules 3.1 and 3.3.
  • the swing rocker arm module 5 has a pivot lever 111 and a rocker arm 112, both hinged to a carriage 113 ( Figure 34).
  • 33 schematically indicated catch elements 114 and 115 are formed on the frame 1, wherein prior to the introduction of the tilting movement of the rocker arm 112 with the catch element 114 and before the pivoting movement of the pivot lever 111 engages with the catch element 115 engages.
  • Fig. 34 shows schematically the structure of this swing-rocker arm module 5, wherein Fig. 34a shows a top plan view of a position of the fitting module in which a tilting movement of the wing 2 relative to the frame 1 is performed. Fig. 34b shows a side view in the position of the fitting module of Fig. 34a, while Fig. 34c shows a view from the right in Fig. 34a.
  • the articulation axles 111.1 and 112.1 (FIG. 35b) of pivot lever 11 and rocker arm 112 are displaceable on the carriage in the circumferential direction of the wing 2 in a slot 117 (FIG. 34a).
  • the rotatably mounted in the bearing points 118 on the profile of the blade 2 spindle 116 is formed without self-locking and is rotated by an electric drive motor 60 of the drive module 6 in rotation, which is also arranged in the profile of the wing 2.
  • the wing 2 In the locking position of the wing 2 on the frame 1, the wing 2 is substantially within the frame 1, wherein the carriage 113 is in the position 0 and the two levers 111 and 112 are aligned circumferentially on the wing 2 and not with the catch elements 114th and 115 are engaged, which are positioned in extension of the two levers 111 and 112 on the frame.
  • the two catch elements 114 and 115 lie in line with the two levers 111 and 112, can in a displacement of the carriage 113 in one or the other direction from the position 0 out of the respective lever 111th or 112 are introduced into the associated catch element, whereupon by a further displacement of the carriage 113, the tilting or pivoting movement of the wing is initiated.
  • the balls 120 at the free ends of the levers 111 and 112 are flattened so that they can be inserted into the guide channel 119 of the catch elements 114 and 115, whereupon pivotal movement of the respective lever 111 or 112 relative to the line connecting the catch elements 114, 115 the flattened ball is reliably held by twisting in the ball socket 121.
  • wing 2 When the carriage 113 has reached the left position 1, the wing 2 is unlocked via the corresponding displacement of the spool 102 to the fitting modules 3.1 to 3.4, wherein the ball 120 is already in the ball socket 121 of the catch element 114 at the free end of the rocker arm 112 , so that in the further displacement movement of the carriage 113 in the direction of position 2, the rocker arm 112 is guided in the catch element 114 in an articulated manner.
  • Fig. 34a shows an intermediate position of the tilting movement, wherein the carriage 113 is located between the positions 1 and 2. The position 2 corresponds to the parallel lifted position of the wing.
  • the carriage 113 is guided by a in Fig. 34c schematically indicated longitudinal guide 122 on the profile of the wing 2, while the spindle 116 rotates in one or the other direction, as indicated by a double arrow in Fig. 34c.
  • the elongated hole 117 forms a longitudinal guide for the pivot axes of the levers 111 and 112.
  • the travel of the carriage 113 is designed from the locked position 0 in the unlocked position 1 in the direction of "tilting” greater than in the direction of "pivoting” so that the arranged between the wing 2 and frame 1 hinge 109 (Fig 31) clearly clears the frame 1 when the wing is tilted.
  • the displacement of the carriage 113 can be kept short in the unlocked position in the direction of pivoting, because the hinge 109 remains in the corner between the wing 2 and frame 1 during pivoting of the wing.
  • the carriage 113 is only in the locking position 0 and during the sliding movement in the position 2 for parallel lifting of the wing connected to the control element 22, while in the further adjusting movement of the carriage 113 in the direction of "tilting” or “Panning” from position 2 of the carriage 113 is decoupled from the control element 22 and the pivoting or tilting movement of the wing is controlled only via the levers 111 and 112, while the control element 22 is locked in its position on the wing 2.
  • Fig. 35 shows schematically the coupling mechanism between carriage 113 and band-shaped control element 22, wherein Fig. 35a shows the coupling position between slide 113 and control element 22 and Fig. 35b the decoupled position, in which the band-shaped control element 22 by a wing 2 by a spring 127 supported catch 128 is fixed in its position while the carriage can continue to move, without affecting the position of the control element 22 is influenced.
  • the carriage 113 is guided over a preferably provided with a roller bearing guide pin 123 in a control cam 124 which is formed on the wing 2 and at the professionssprafil.
  • a roller bearing guide pin 123 In the locking position and during the adjustment of the parallel lifting the control pin 123 is in the stepped portion 124.1 of the control cam, wherein the carriage 113 engages via an engagement member 125 in a recess 126 of the control element 22, so that the control member 22 synchronously with the carriage 113 moves.
  • the control cam 124 is provided with an inclined portion 124.2, the angle of inclination corresponds to the inclination angle of the edge of the engaging member 125 in the oblique edges provided recess 126 on the control element 22 in that in the further displacement movement of the control element 22 in the direction of "tilting” or “pivoting” the engagement element 125 slides out of engagement with the control element 22, while the engagement pin 123 is displaced into an outer section 124.3.
  • the control pin 123 is located in the portion 124.3 of the cam 124 corresponds this is a position of the carriage 113 beyond the position 2 in Fig. 34a, in which the carriage 113 is decoupled from the band-shaped control element 122, as Fig. 35b shows.
  • the coupling mechanism between carriage 113 and band-shaped control element 22 on the one hand and between control element 22 and wing 2 on the other hand has in the embodiment of FIG. 35 on a plunger 129 which engages with a V-section in the V-shaped recess 126 of the control element 22 and the opposite widened end in a corresponding widened recess 130 of the control element 22 is located.
  • Fig. 35a shows, the plunger 129 is held by the engaging member 125 adjacent to a fixed part of the wing 2, while the engagement member 125 engages in the recess 126 for connection between the control element 22 and slide 113.
  • the detents 128 acted upon by the springs 127 rest on the band-shaped control element 22, while the latter is displaced relative to the wing 2.
  • the control element 22 is also in a position in FIG of the widened recess 130 of a detent 128 opposite, so that is pushed back by the spring-loaded detent 128 of the plunger 129 in the reproduced in Fig. 35b position and the detent 128 engages in the recess 130 of the control element 22, so that this set in this position is.
  • the engagement member 125 is guided between two guides 131 transversely to the carriage movement.
  • 113.1 guide pins on the wing 2 are designated for the levers 111 and 112, wherein in the position in Fig. 34a, the non-active lever 111 is located between the spaced guide pins 113.1.
  • the lever 112 comes to rest between these guide pins, while the lever 111 is moved out of the guide, so that it can control the pivotal movement of the wing after engagement with the catch element 115.
  • the fittings 3.1 to 3.4 in the embodiment according to FIGS. 25 to 35 have substantially the same construction in contrast to the embodiment according to FIGS. 2 to 21. Furthermore, a substantial simplification results from the fact that the drive module 6 with the tilting and pivot lever module 5 is combined and the tilt and pivot levers 111 and 112 are selectively connected by hinging in the catch elements 114, 115 on the frame 1 with the frame.
  • the handle 70 on the handle module 7 can have the same configuration as in FIG. 22 with the keyboard 72 and the key 71. So that the window structure can be actuated independently of the drive motor 60 via the handle module 7, the handle 70 is connected via a cable, not shown, to a coupling 137 (FIG.
  • the carriage 113 is coupled to the control element 22 (FIG. 35).
  • the wing is moved parallel to the frame from position 2 to position 1.
  • the coupled control 22 ensures the synchronous movement.
  • the control element 22 and with this the spool 102 is moved to the fitting modules so that the wing 2 is moved to the locking position 0 on the frame 1.
  • control element 22 can also be designed as a band section which does not extend over the entire circumference of the wing 2, but only from the fitting module 3.2 via the fitting module 3.1 to the fitting module 3.4.
  • the control 22 must be designed to be correspondingly stiff.
  • the control element 22 is formed as a closed cable, which extends around the entire circumference of the wing 2.
  • pulleys are preferably arranged at the corners of the wing to make the adjustment of the rope on the circumference of the wing smoothly.
  • the wing 2 can be moved from any position to the closed position, for example, if a rain sensor reports rain and thereby controlled via a corresponding control electronics, the motor 60 to close the window.
  • the window can be moved from the parallel lifted position by the carriage 113 driving the drive motor 60 in the closed position. If the wing 2 is in a tilting or pivoting position, the wing 2 is initially moved by the motor drive of the carriage 113 into the parallel lifted position 2, from which the closing process then takes place.
  • the closed position of the wing 2 is already reached in position 1, just before the retaining pins 101 reach the apex 106.1 (FIG. 27) of the control groove 106.
  • the rest of the movement of the retaining pin 101 to the end position at the apex of the control cam corresponds to the compression of the window seal.
  • Fig. 36 shows a modified embodiment of the tilting pivot lever module 5, in which, in contrast to the embodiment of Fig. 33, only one lever 140 between the frame 1 and 2 wings for both the tilting movement and for the pivoting movement is present.
  • a parallel lifting of the wing 2 before initiating the pivoting movement d. H. the displacement between the position 0 and the right position 1 in Fig. 34a, omitted when the carriage 113 is moved from the locking position 0 in the direction of pivoting the wing.
  • the hinge 109 remains between fitting modules 3, 3 and 3, 4 and wing 2 (FIG. 31) in the same position as in the locking position, so that, starting from the locking position, a pivoting movement of the wing 2 is initiated immediately.
  • the coupling of the control element 22 with the fitting modules 3.3 and 3.4 takes place here via the axis of rotation of the hinge 109.
  • the spool of the fitting modules 3.3 and 3.4 is always mechanically engaged with the control 22nd
  • Fig. 36a shows schematically the lever position when tilting the wing 2.
  • the lever 140 is hinged at 141 on the top of the frame 1 near the right corner, while its opposite end 142 is guided in a slot 143 of the wing 2 articulated.
  • a further lever 144 is articulated at 145, the opposite end 146 is hinged to the carriage 113, which, as indicated by a double arrow, along the top of the wing 2 according to the embodiment of FIG. 34 by the drive module. 6 is displaceable.
  • the longer lever 140 is in line with the shorter lever 144 between the articulation points 142 and 146. From this locking position 0 is lifted by a carriage movement 113 in the direction of tilting the wings 2 parallel to the frame 1, as in the embodiment described above is the case. After reaching position 2 of the carriage 113 is decoupled from the control element 22, so that the further tilting movement in Fig. 34a is performed only by the lever 140 under the control of the shorter lever 144.
  • the pivot point 146 of the control lever 144 is displaced by the carriage 113 to the right in Fig. 36a, whereby the pivot point 142 is moved in the slot 143 to the left in Fig. 36a until the wing 2 lifted parallel Position 2 is reached, from which the fitting modules 3.1 to 3.4 execute the closing movement of the wing 2 in conjunction with the movement of the control element 22 guided by the slide 113 in parallel.
  • Fig. 36b shows a pivoting position of the wing 2 by means of the tilting pivot lever module 5, wherein the pivoting movement does not take place from the parallel lifted position of the wing out, but directly from the unlocked position 1.
  • the control 22 something in the direction Pivoting moves so that the retaining pin 101 is moved out of the locking position 0 at the vertex 106.1 of the control cam 106 of the fitting modules 3.1 to 3.4 in position 1.
  • a further control movement of the control element 22 is no longer necessary, so that it can already be decoupled from the control element 22 after this short positioning movement of the carriage 113, so that the further pivoting movement is carried out solely by the levers 140, 144.
  • the lever 140 is pivoted by the control lever 144 about the articulation point 141 on the frame 1 in the further sliding movement of the carriage 113 to the right on the wing 2 as shown in Fig. 36b.
  • the pivot point 142 of the lever 140 is guided in a land hole 143 on the wing 2, the pivotal movement of the wing about the axis of the hinges 109 can be performed.
  • Fig. 37 shows the arrangement of the hinge 109 on the fitting modules 3.3 and 3.4 at the outer edge of the wing 2. This arrangement of the hinges 109 on the outer edge of the wing allows pivoting of the wing directly from the reproduced in Fig. 37 closed position.
  • a ball joint between the frame and the wing can also be provided on the fitting module 3.4 because the wing is pivoted directly out of the unlocking position on the fitting module 3.4, the fitting module remaining in its position.
  • This ball joint also serves as a tilting axis when tilting the wing.

Claims (23)

  1. Structure de fenêtre ou de porte, comportant :
    un cadre (1),
    un battant (2) aménagé de façon mobile sur le cadre,
    des modules d'armature (3.1 à 3.4, 4.1, 4.2, 5) entre le cadre et le battant,
    un élément de commande (22) guidé le long de la périphérie du battant (2), lequel élément, dans les différentes positions du battant par rapport au cadre (1), est en prise avec au moins un module d'armature et commande le cycle de déplacement des modules d'armature, un moteur d'entraînement électrique (60) étant aménagé sur le battant, lequel moteur entraîne l'élément de commande guidé sur le battant dans la direction périphérique, de telle sorte que,
    à l'occasion d'une première étape de déplacement de l'élément de commande dans l'une ou l'autre des directions périphériques, le battant (2) est soulevé sensiblement parallèlement du cadre (1) au-dessus des modules d'armature,
    sur quoi, par un autre déplacement de l'élément de commande dans une des directions périphériques, un basculement du battant sur les modules d'armature est déclenché,
    tandis que par un autre déplacement de l'élément de commande dans l'autre direction périphérique, un pivotement du battant sur au moins deux modules d'armature est déclenché et le battant est libéré pour pivoter sur les modules d'armature opposés.
  2. Structure selon la revendication 1, des modules d'armature (3.1 à 3.4) distants les uns des autres étant prévus sur la périphérie du battant (2), parmi lesquels chacun comprend un galet (25) qui est mobile dans un guidage horizontal (12) du cadre (1), de sorte que le battant (2) est mobile parallèlement au cadre (1).
  3. Structure selon la revendication 2, le galet (25) des modules d'armature (3.2 et 3.4) aménagés dans la partie inférieure sur les deux côtés du battant (2) servant d'articulation pour un déplacement basculant du battant (2).
  4. Structure selon l'une quelconque des revendications 1 à 3, une articulation pivotante étant formée sur les modules d'armature (3.3, 3.4) disposés sur un côté du battant (2).
  5. Structure selon l'une quelconque des revendications précédentes, des modules de levier basculant (4.1, 4.2) étant aménagés sur les côtés opposés du battant (2) et un module de levier pivotant (5) sur le côté supérieur du battant.
  6. Structure selon l'une quelconque des revendications précédentes, l'élément de commande (22) réalisant depuis une position de départ (0) correspondant à la position fermée du battant (2) un déplacement pilote (I) dans l'une ou l'autre des directions, par lequel tous les modules d'armature (3.1 à 3.4, 4.1, 4.2, 5) sont déplacés dans une position prédéterminée.
  7. Structure selon la revendication 6, sachant que, par le déplacement pilote dans l'une ou l'autre des directions périphériques, les modules de levier basculant (4.1, 4.2) sont reliés au cadre (1), tandis que le module de levier pivotant (5) est fixé au battant (2), et par le déplacement pilote dans l'autre direction périphérique, le module de levier pivotant (5) est relié au cadre (1), tandis que les modules de levier basculant (4.1, 4.2) sont fixés au battant (2), et
    sachant que, par le déplacement pilote de l'élément de commande (22) dans l'une ou l'autre des directions, les modules d'armature (3.1 à 3.4) sont déplacés à partir de la position de verrouillage.
  8. Structure selon l'une quelconque des revendications précédentes, les modules d'armature (3.1 à 3.4) comprenant un élément de retenue (33) pivotant, qui coopère avec deux tourillons de retenue (11, 11') distants sur le cadre (1) et est en prise avec l'élément de commande (22).
  9. Structure selon l'une quelconque des revendications précédentes, un élément de capture (400) commandé par l'élément de commande (22) étant articulé sur l'extrémité côté cadre d'un levier basculant et/ou pivotant (40 ; 50), lequel élément de capture, pour fixer le levier au cadre (1) et/ou au battant (2), coopère avec une broche (405) fixée au cadre et/ou une broche (406) fixée au battant.
  10. Structure selon l'une quelconque des revendications précédentes, les modules d'armature inférieurs (3.2, 3.4) comprenant un système de blocage (38) pour le galet (25) dans le guidage horizontal (12) du cadre, et l'élément de commande (22) coopérant avec les modules de levier basculant (4.1, 4.2) sur les deux côtés du battant (2), de telle sorte que l'élément de commande (22) entre en prise avec les modules de levier basculant avant que la mise en prise de l'élément de commande avec les modules d'armature supérieurs (3.1 et 3.3) ait été détachée.
  11. Structure selon l'une quelconque des revendications précédentes, un module d'entraînement (6) étant prévu sur le battant (2), lequel module comprend un moteur d'entraînement électrique (60), qui entraîne l'élément de commande (22) dans la direction périphérique.
  12. Structure selon l'une quelconque des revendications précédentes, un module de préhension (7) doté d'une poignée (70) étant aménagé sur le battant (2), module au moyen duquel l'élément de commande (22) est mobile dans une position de présélection, et la poignée (70) comprenant une touche de déverrouillage (71), au moyen de laquelle l'élément de commande (22) peut être détaché du module d'entraînement (6).
  13. Procédé d'actionnement d'une structure de fenêtre ou de porte dotée d'un cadre (1), d'un battant (2) aménagé de façon mobile sur le cadre, de modules d'armature (3.1 à 3.4, 4.1, 4.2, 5) entre le cadre et le battant et d'un élément de commande (22) circulaire, qui commande le cycle de déplacement d'au moins une partie des modules d'armature, l'élément de commande (22) étant déplacé d'une position de départ (0) dans une des directions périphériques, afin de commander le basculement du battant, et de la position de départ (0) dans l'autre direction périphérique, afin de commander le pivotement du battant, l'ordre séquentiel des déplacements de commande de l'élément de commande dans l'une ou l'autre des directions périphériques déterminant incontestablement les positions respectives du battant par rapport au cadre.
  14. Procédé selon la revendication 14, sachant que, avant un déplacement basculant ou pivotant du battant, celui-ci est soulevé parallèlement du cadre (1) et un déplacement basculant ou pivotant n'est réalisé qu'à partir d'une position du battant soulevée parallèlement, et
    sachant que, avant le soulèvement parallèle du battant (2) depuis le cadre (1), un déplacement pilote est réalisé dans l'une ou l'autre des directions périphériques, par lequel une présélection est déterminée pour le basculement ou le pivotement du battant et un passage du pivotement au basculement et inversement n'est possible qu'en ramenant le battant dans la position fermée, à partir de laquelle la présélection s'effectue en direction du basculement ou du pivotement.
  15. Procédé selon l'une quelconque des revendications 14 et 15, un moteur (6) entraînant l'élément de commande (22) étant détaché de la mise en prise avec l'élément de commande, lorsque le battant est amené manuellement au moyen d'une poignée (70) dans une position ouverte ou fermée, sachant que, par l'intermédiaire des déplacements du battant réalisés manuellement, l'élément de commande est déplacé par le couplage avec les modules d'armature dans la position de commande correspondant à la position respective du battant.
  16. Structure de fenêtre ou de porte, comportant
    un cadre (1)
    un battant (2) aménagé de façon mobile sur le cadre,
    des modules d'armature (3.1 à 3.4, 5) entre le cadre et le battant, et
    un élément de commande (22) guidé le long de la périphérie du battant, lequel élément, dans les différentes positions du battant par rapport au cadre, est en prise avec au moins un module d'armature et commande de cycle de déplacement des modules d'armature, un moteur d'entraînement électrique (60) étant aménagé sur le battant, lequel moteur déplace dans la direction périphérique un coulisseau (113) guidé sur le battant (2),
    le coulisseau (113) étant relié par un mécanisme de couplage détachable (125) à l'élément de commande (22), de telle sorte que
    lorsqu'un déplacement pivotant ou basculant du battant est déclenché, le coulisseau (113) est détaché de l'élément de commande (22) et le coulisseau (113) entraîné par le moteur d'entraînement commande le déplacement basculant ou pivotant par l'intermédiaire d'un levier (111, 112 ; 140), qui est articulé sur le coulisseau (113) et sur le cadre (1).
  17. Structure selon la revendication 16, des tourillons de retenue (101) étant distants sur la périphérie du cadre (1), lesquels tourillons se mettent en prise dans un guidage horizontal (107) sur les modules d'armature (3.1 à 3.4) ainsi que dans une rainure de commande (106) d'un tiroir de commande (102) mobile dans le module d'armature, lequel tiroir est en prise avec l'élément de commande (22) mobile sur la périphérie du battant (2).
  18. Structure selon la revendication 17, un galet (101.1) pour la mise en prise dans le guidage horizontal (107) et un galet (101.2) pour la mise en prise du tourillon de retenue dans la rainure de commande (106) étant prévus sur le tourillon de retenue (101), lequel galet présente un diamètre plus petit que celui du galet (101.1) prévu pour recevoir les charges dans le guidage horizontal.
  19. Structure selon l'une quelconque des revendications 17 et 18, le tiroir de commande (102) étant guidé par des guidages longitudinaux (103, 104) dans une partie d'armature (105) en forme de boîtier.
  20. Structure selon l'une quelconque des revendications 16 à 19, une des parties d'une charnière (109) étant fixée aux modules d'armature (3.3 et 3.4) prévus pour le pivotement du battant, charnière dont l'autre partie est fixée au battant (2), de sorte que lorsque le battant (2) pivote, le module d'armature peut rester sur le cadre (1).
  21. Structure selon la revendication 16, un levier basculant (112) et un levier pivotant (111) étant articulés sur le coulisseau (113), leviers dont les extrémités opposées peuvent être introduites dans les éléments de capture (114, 115) sur le cadre (1) à l'occasion du déplacement du coulisseau, afin de commander le déplacement basculant et/ou pivotant du battant (2).
  22. Structure selon la revendication 21, le coulisseau (113), à l'occasion d'un soulèvement parallèle depuis la position de verrouillage, étant relié à l'élément de commande (22) et à l'occasion d'un déclenchement du déplacement basculant ou pivotant du battant (2) par le mécanisme de couplage, étant détaché de l'élément de commande (22), tandis que simultanément l'élément de commande (22) est fixé dans sa position sur le battant (2) par un système d'enclenchement (128, 130).
  23. Structure selon la revendication 16, un levier de commande (144) étant articulé sur le coulisseau (113), lequel levier est relié de façon articulée à un levier conducteur (140), dont une extrémité est articulée sur le cadre (1), tandis que l'extrémité opposée est guidée de façon articulée dans un guidage longitudinal (143) du battant (2) dans la direction périphérique du battant.
EP02737893A 2001-03-21 2002-03-21 Structure de fenetre ou de porte Expired - Lifetime EP1370742B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10113784 2001-03-21
DE10113784A DE10113784A1 (de) 2001-03-21 2001-03-21 Fenster- oder Türaufbau
PCT/EP2002/003188 WO2002086271A1 (fr) 2001-03-21 2002-03-21 Structure de fenetre ou de porte

Publications (2)

Publication Number Publication Date
EP1370742A1 EP1370742A1 (fr) 2003-12-17
EP1370742B1 true EP1370742B1 (fr) 2006-01-11

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EP02737893A Expired - Lifetime EP1370742B1 (fr) 2001-03-21 2002-03-21 Structure de fenetre ou de porte

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US (1) US20040128914A1 (fr)
EP (1) EP1370742B1 (fr)
JP (1) JP2004530818A (fr)
KR (1) KR20030090683A (fr)
CN (1) CN1261665C (fr)
AT (1) ATE315712T1 (fr)
BR (1) BR0208260A (fr)
CA (1) CA2441460A1 (fr)
CZ (1) CZ20032799A3 (fr)
DE (2) DE10113784A1 (fr)
EE (1) EE04787B1 (fr)
ES (1) ES2251597T3 (fr)
PL (1) PL365845A1 (fr)
RU (1) RU2288335C2 (fr)
SK (1) SK12912003A3 (fr)
WO (1) WO2002086271A1 (fr)

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Publication number Publication date
ES2251597T3 (es) 2006-05-01
RU2003130970A (ru) 2005-03-10
EE200300446A (et) 2003-12-15
EE04787B1 (et) 2007-02-15
DE10113784A1 (de) 2002-10-02
PL365845A1 (en) 2005-01-10
CZ20032799A3 (cs) 2004-05-12
BR0208260A (pt) 2004-03-09
ATE315712T1 (de) 2006-02-15
SK12912003A3 (sk) 2005-08-04
EP1370742A1 (fr) 2003-12-17
WO2002086271A1 (fr) 2002-10-31
RU2288335C2 (ru) 2006-11-27
JP2004530818A (ja) 2004-10-07
CN1261665C (zh) 2006-06-28
US20040128914A1 (en) 2004-07-08
DE50205585D1 (de) 2006-04-06
CN1498302A (zh) 2004-05-19
CA2441460A1 (fr) 2002-10-31
KR20030090683A (ko) 2003-11-28

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