EP0379866B1 - Window, door or the like - Google Patents

Window, door or the like Download PDF

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Publication number
EP0379866B1
EP0379866B1 EP90100180A EP90100180A EP0379866B1 EP 0379866 B1 EP0379866 B1 EP 0379866B1 EP 90100180 A EP90100180 A EP 90100180A EP 90100180 A EP90100180 A EP 90100180A EP 0379866 B1 EP0379866 B1 EP 0379866B1
Authority
EP
European Patent Office
Prior art keywords
wing
fixed frame
panel
window
pull member
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.)
Revoked
Application number
EP90100180A
Other languages
German (de)
French (fr)
Other versions
EP0379866A1 (en
Inventor
Karl Heinz Fischbach
Horst Loos
Alfred Schneider
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siegenia Aubi KG
Original Assignee
Siegenia Frank KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=27198964&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP0379866(B1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority claimed from DE19893901944 external-priority patent/DE3901944A1/en
Priority claimed from DE8903678U external-priority patent/DE8903678U1/en
Priority claimed from DE19893920360 external-priority patent/DE3920360C2/en
Application filed by Siegenia Frank KG filed Critical Siegenia Frank KG
Publication of EP0379866A1 publication Critical patent/EP0379866A1/en
Application granted granted Critical
Publication of EP0379866B1 publication Critical patent/EP0379866B1/en
Anticipated expiration legal-status Critical
Revoked legal-status Critical Current

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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/48Suspension arrangements for wings allowing alternative movements
    • E05D15/52Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
    • E05D15/5211Concealed suspension fittings
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05FDEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F7/00Accessories for wings not provided for in other groups of this subclass
    • E05F7/06Devices for taking the weight of the wing, arranged away from the hinge axis
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Type of wing
    • E05Y2900/148Windows

Definitions

  • the invention relates to a window or a door with a tilt and turn sash, which is mounted on or near an upright boundary edge by means of joint fittings on the fixed frame.
  • the hinge fittings connecting the sash to the fixed frame can, on the one hand, be arranged lying or visible in front of the opening-side end face of the fixed frame, the lateral swivel joints then lying on the upright limiting edge of the sash (see DE-C-10 78 010 and DE-C-11 74 649).
  • hinge fittings which are installed in a position completely hidden in a chamber between the folds of the sash and the fixed frame.
  • the lateral swivel joints are then provided in the vicinity of the upright wing edge (see. DE-C-21 13 665).
  • the object of the invention is to show a way through which, in the case of windows or doors of the type described at the outset - also subsequently - with simple means, extensive relief of the hinge fittings connecting the sash to the fixed frame can be achieved by the sash weight acting in the axial direction thereof without impairing the system-specific mode of action of the joint fittings used in each case.
  • the solution to this problem is characterized according to the invention by a tension member that engages on the one hand in the area of the joint fittings and on the other hand anchored against the weight or load of the wing on the fixed frame, which is installed above but near the lower corner joint between the wing and the fixed frame.
  • this relieves the pressure on the corner joint at the intersection between the lateral, upright hinge axis and the lower, horizontal hinge axis of the tilt-and-turn sash to the fixed frame. This applies not only in the closed position and in the turning open position of the wing, but rather also in the tilt open position of the same.
  • DE-C- 329 280 is already considered to transfer the sash weight directly to the frame via a tension member.
  • the arrangement of an element subject to tension between the sash frame and the fixed frame is expressly considered to be possible only with a pure rotating fitting.
  • DE-C-329 280 nor the previously reported DE-A-38 29 053 are any suggestions or pointers in the direction of the use according to the invention of an element acting on the sash frame and the fixed frame and thereby subject to tension on windows or doors with tilt and turn sashes remove.
  • DE-A-38 29 053 explicitly shows only the direction for windows and doors with a tilt-and-turn fitting to use a support rod that is under pressure as a relief element for the articulated fittings, in order to open the sash forces both when opening and tilting of the wing in the fixed frame.
  • the tension member can be hung with its upper end directly on the fixed frame, while at the same time it engages with its lower end on the wing.
  • the tension member according to the teaching of claim 3, is kept constantly under tension, the vertical component can be introduced directly from the weight or load of the sash into the fixed frame, so that the hinge fittings have to absorb practically only stresses , which result from horizontal components of the weight or load of the wing and are directed essentially transversely to their hinge axes.
  • This measure ensures in a simple manner that the hinge fittings forming the lower corner joint remain largely relieved of the weight of the sash not only when the sash is in the closed position and when the sash is in the rotational opening position, but also when the sash is in the tilt opening position.
  • the tension member is formed by a rope or a cable or possibly also consists of a Bowden cable.
  • a tension member designed in this way not only requires a small installation space, but it can easily adapt to the relative movements of the wing relative to the fixed frame when the window or door is opened and closed while maintaining its effect.
  • the tension member is concealed according to the invention in the air space between the folds of sash and frame.
  • the tension member is at least limitedly adjustable in length.
  • the tension member consist of a rigid tension rod, the ends of which engage by gimbal or spherical connecting links on the wing and on the fixed frame.
  • the tension member on the fixed frame around the stationary abutment e.g. be guided around by means of a roller and placed under tension by the counterforce, for example the counterweight.
  • the invention also proposes to use at least one twistable flat strip material, in particular spring steel strip, as the tension member.
  • the flat strip material has a width which is a multiple, e.g. B. about sixteen times to twenty times its thickness, while this flat strip material is in the closed position on the fixed frame wing over its entire length with its broad side at least approximately parallel to the folded surfaces or transversely to the main planes of the wing and the fixed frame extends.
  • the wing-side joint part has a hook extension projecting over the boundary surface of the upright wing spar with an angular slot that is open sideways at its lower end, that the hook approach has two parallel to the wing plane and separated by a spacing gap hook parts and that the tension member is provided at its lower end with a block-shaped thickening, the cross-sectional dimension of which is adapted to the width of the angular slot, while the spacing gap forms a receptacle for the tension member.
  • the block-shaped thickening consists of a cylindrical or spherical body in which the tension member is firmly or releasably anchored.
  • the releasable anchoring can take place, for example, with the aid of a clamping screw which has such a position or arrangement in the block-shaped thickening that it is not accessible on the wing-side joint part when the tension member is hooked on.
  • the wing-side joint part is an angle piece which can be used in the area of the wing corner with its two angle legs in a step-shaped profiled groove on the circumferential surface of the fold.
  • the tension member is first coupled to the wing during the hooking-in process and then the wing is hooked into the hinge fittings.
  • the tension member can then already introduce the sash weight into the fixed frame while the sash is connected to the hinge fittings.
  • the wing associated end When using a rope or cable as a tension member, it is conceivable to provide the wing associated end with a loop that can be attached to a wing part on the hinge part and a thickened head part or a circumferential groove bearing pin.
  • the loop narrows under the influence of the wing weight, it can be difficult if the tension member has to be uncoupled from the wing when it becomes necessary to unhook it.
  • the angled slot of the hook extension in accordance with claim 12 can be assigned a nose-like narrowing projection in the area of the sideways opening or immediately above it, in such a way that an undesired unhooking of the tension member from the wing-side joint part is prevented.
  • the narrowing protrusion according to the invention can consist of a spring tongue or a snap catch, which is provided on the wing-side joint part.
  • the narrowing projection is located at the free end of one lever arm of a two-armed lever which is pivotally held in the wing-side joint part and which, in turn, carries an actuating cam at the free end of its other lever arm which fits into the angle slot of the Hook approach protrudes as long as the narrowing projection does not engage in the angular slot of the hook approach.
  • a window or door 21 can be seen, which comprises a fixed frame 22 and a wing 23.
  • the wing 23 is optionally arranged in the fixed frame 22 so as to be movable about a laterally perpendicular axis 24-24 in a rotational opening position or about a lower horizontal axis 25-25 in a tilt opening position.
  • the wing 23 is supported on the fixed frame 22 at the intersection of the two hinge axes 24-24 and 25-25 by a corner joint or a tilt and turn corner bearing 26.
  • a drive rod fitting 31, which can be adjusted via an operating handle 30, is accommodated in the wing 23 in such a way that, on the one hand, locking and unlocking of the wing 23 in the closed position on the fixed frame 22 can be effected by means of locking cams 32 and associated locking engagements 33.
  • the connecting rod fitting 31 is also designed so that it can be used to engage and disengage both a coupling 34, 35 between the wing 23 and the opening device 28 and the tilt lock 29.
  • the clutch 34, 35 is in its engagement position between the wing 23 and the opening device 28.
  • the clutch 34, 35 In the tilt-open switching position of the connecting rod fitting 31, however, the clutch 34, 35 is disengaged.
  • the tilt lock 29 is in the disengaged position when the espagnolette fitting 31 assumes its closed switch position and its rotary open switch position while it is engaged in the tilt open switch position.
  • the opening device 28 is designed as a so-called supporting opening device, ie it is suitable for the weight of the wing 23 in the closed position and in the rotary opening switch position of the connecting rod fitting 31 to hold and to initiate in the upper frame hinge 27.
  • the opening device 28 has an opening arm 36 which is pivotally held in the frame-side swivel joint 27 and which at its other end engages in a sliding guide 38, which can pivot and also slide longitudinally, via a collar pin 37 and extends essentially parallel to the upper edge of the wing 23.
  • the opening device 28 has an additional arm 39, which on the one hand is articulated only pivotably on the wing 23 via a hinge pin 40, but on the other hand, if only pivotable, is connected to the opening arm 36 via a hinge pin 41.
  • the opening device 28 is designed in its kinematics so that it keeps the upper wing spar aligned in every possible tilt position parallel to the upper spar of the fixed frame 2 when the wing 23 is opened.
  • the sash 23 is held on the fixed frame 22 by means of hinge fittings which are completely concealed in the air space between the rebates of sash 23 and the fixed frame 22.
  • hinge fittings can be used which, in their mode of operation, e.g. based on the pantograph or cranesbill principle - see e.g. B. DE-OS 25 08 174 and DE-PS 35 19 988 -.
  • a tension member 42 is also used in the window or in the door 21 according to FIG. 1. It is effective in the direction of the vertical hinge axis 24-24 and for this purpose is hung with its upper end on a fixed abutment 43 of the fixed frame 22, while its lower end engages an abutment 44 which sits on the wing 23.
  • the tension member 42 with its abutments 43 and 44 is overall above, but still installed in the immediate vicinity of the lower corner joint or rotary tilt corner bearing 26 between the wing 23 and the fixed frame 22, as can be clearly seen in FIG. 1.
  • the tension member 42 of Fig. 1 is e.g. hidden in the air space between the rebates of wing 23 and fixed frame 22 of the window 21 installed.
  • FIGS. 2 to 5 of the drawing show a window or a door 21, in which the wing 23 on the fixed frame 22 is completely hidden between the horizontal folds of sash 23 and fixed frame 22 lying joint fittings (corner joint 26 and pivot joint 27) is suspended.
  • the joint fittings according to FIGS. 2 to 4 are based on a type and mode of operation which is already known in principle, for example from GB-PS 496 829.
  • Fig. 2 of the drawing the articulated fitting designed as a corner joint or turn-tilt corner bearing 26 is shown in a detailed longitudinal section. He has a design that not only allows the wing 23 to be rotated about the upright axis 24-24, but also supports the wing 23 for tilt opening about the lower, horizontal axis 25-25.
  • the upper hinge fitting forming the swivel joint 27, on the other hand, is part of the opening device 28, which holds, supports and guides the wing 23 both in the closed position and during the swivel opening and tilt opening.
  • each steering lever transmission has a supporting link 45, which via a joint 46 - according to FIG a ball joint 46 - at its rear end rests on a mounting rail 47 which is rigidly attached to the circumferential surface of the fixed frame 22.
  • the steering lever gearbox also has a main link 49 mounted on the rebate circumferential surface of the wing 23, for example inserted into a stepped profile groove 48 running parallel to its main plane, which is coupled to the supporting link 45 by two connecting links 50 and 51.
  • the connecting link 50 is arranged on the supporting link 45 exclusively via a pivot pin 52, while it acts on the main link 49 via a link pin 53, also exclusively pivotable.
  • the connecting link 51 is also held exclusively on the supporting link 45 in a pivotable manner by means of a pivot pin 54, while it only acts pivotably on the main link 49 with a pivot pin 55.
  • Both connecting links 50 and 51 have the same length between their hinge pins 52, 53 and 54, 55 and are arranged so that they form a parallelogram steering lever mechanism with the supporting link 45 and the main link 49.
  • a control arm 56 which rigidly engages one of the two connecting links 50 and 51, preferably on the connecting link 51, is used for the compulsory movement control of each joint fitting (corner joint 26 or swivel joint 27) formed by a parallelogram steering lever transmission. On the other hand, it can be moved via a sliding pin 57 in a slot guide 58 which extends parallel to the main plane of the fixed frame 22 and can be arranged in an extension of the screw-on plate 47.
  • a control of the joint fittings (corner joint 26 and pivot joint 27) is brought about with the help of the control arm 56, in such a way that over an opening angle of the wing 23 of at least 90 ° at no time the wing flap 23a with the room side End face 22a of the fixed frame 22 can collide. Only when the wing 23 comes to rest in the closed position on the fixed frame 22 does the wing flap 23a rest with its rear surface against the end face 22a of the frame 22 on the room side.
  • the locking device in the region of the lower joint joint which acts as a corner joint or tilt-turn corner bearing 26, on the other hand, preferably has an arrangement, design and mode of operation as is explained in detail in DE-PS 38 34 388.
  • this locking device 59 consists of a locking slide 60 which is movably guided on the wing 23 parallel to its plane and a locking projection 61 fixed to the fixed frame 22.
  • the locking slide 60 carries an actuating projection 62 which at least temporarily protrudes into the movement path of a control cam 63 which is seated on the control arm 56 of the parallelogram steering lever mechanism.
  • the actuating projection 62 on the locking slide 60 and the control cam 63 on the control arm 56 are arranged relative to one another such that when the wing 23 approaches the closing movement of the fixed frame 22, the actuating projection 62 already hits the control cam 63 before the wing 23 assumes its closed position .
  • the actuating projection 62 is then moved in the course of the further closing movement of the wing 23 and, via this, the locking slide 60 is moved in the direction of the locking projection 61 until it engages behind it in a locking manner.
  • the tension member 42 lies in the area of the rebate air between the fixed frame 22 and the wing 23, so that when the wing 23 is in the closed position it is completely concealed between the rebate peripheral surfaces 22c and 23c, as can be clearly seen in FIG. 2.
  • the tension member 42 can be formed by a tension rod made of rigid material.
  • a cable or cable, in particular made of steel wires, is used as the tension member 42 or a Bowden cable is used.
  • the abutment 44 is preferably arranged on the wing 23 with the smallest possible distance above the lower joint fitting or corner joint 26, the tension member 42 between the two abutments 43 and 44 being kept constantly under tight tension, so that the vertical component of the weight or load is held by it of the wing 23 is received without this can act on the hinge fitting 26 in the direction of the axis 24-24.
  • the hinge fitting 26 has to absorb only those forces which result from the horizontal component of the weight or load of the wing 23 and are directed normal to the axis 24-24, as in FIGS. 2 to 4 in each case the arrow 63 is indicated.
  • the abutments 43 and 44 for the tension member 42 can consist of bolts equipped with transverse bores or fork slots, which are fastened to the fold peripheral surfaces 22c and 23c by a fixed frame 22 and wing 23.
  • the tension member 42 is then inserted into the transverse bores or fork slots thereof, the effective length of which can be appropriately matched and / or adjusted appropriately for the distance between the two abutments 43 and 44.
  • the latter can be made possible in that the tension member 42 is equipped with support stops 64 and 65, of which at least one, for example the support stop 65, forms a clamping sleeve which can be displaced in the longitudinal direction of the tension member 42 and can be fixed on the latter in any displacement position. At least one of the support stops 64 and 65 of the tension member 42 could also be made infinitely adjustable in its effective length by using suitable screw members.
  • FIGS. 1 to 5 it would also be possible according to FIGS. 1 to 5 to switch on spring elements between one of the abutments 43 and 44 and the tension member 42, the pretensioning force of which change as necessary and thus - within certain limits - adjust or adjust to the respective weight of the wing 23 leaves.
  • the change in position of the tension member 42 between its abutments 43 resulting from each movement of the wing 23 to the fixed frame 22 and 44 can be easily mastered. If the tension member 42 consists of a rigid material, then it only needs to have gimbal or spherical connections to the abutments 43 and 44 for this purpose. However, if the tension member 42 is designed to be bendable (rope, cable, Bowden cable), then it can easily follow the displacement movements of the wing 23 relative to the fixed frame 22.
  • a tension rod can be used, the ends of which engage by means of cardanic or spherical connecting links on the fixed frame 22 and on the wing 23, specifically on the abutments 43 and 44 suitably designed for this purpose.
  • At least one twistable flat strip material in particular spring steel strip, can also be used as the tension member 42.
  • Such a ribbon material has the advantage that it can have a relatively large width with a relatively small thickness, which width is basically limited by the width of the folded peripheral surfaces of the fixed frame 22 and the wing 23. It has proven particularly useful if the flat strip material or the spring steel strip is used with a width which corresponds to sixteen to twenty times its thickness.
  • tension member 42 consists of a rigid tension rod or a twistable flat strip material, it is possible to design its effective length between the abutments 43 and 44 to be infinitely adjustable, for example with the aid of screw members.
  • a window or a door 121 can be seen which comprises a fixed frame 122 and a wing 123.
  • the wing 123 is arranged in the fixed frame 122 either movably about a laterally perpendicular axis 124-124 in a rotational opening position or about a lower horizontal axis 125-125 in a tilt opening position.
  • the wing 123 is supported on the fixed frame 122 at the intersection of the two hinge axes 124-124 and 125-125 by a corner joint or a tilt and turn corner bearing 126.
  • a swivel joint 127 and an opening device 128 are located at the top between the wing 123 and the fixed frame, while a tilt lock 129 is provided on the lower corner of the wing 123 and the fixed frame 122 on the lock side.
  • a drive rod fitting 131 which can be adjusted via an operating handle 130, is accommodated in the wing 123 in such a way that, on the one hand, locking and unlocking of the wing 123 in the closed position on the fixed frame 122 can be effected by means of locking cams 132 and associated locking engagements 133.
  • the connecting rod fitting 131 is also designed so that it can be used to engage and disengage both a coupling 134, 135 between the wing 123 and the opening device 128 and the tilt lock 129. Both in the closed switching position and in the rotary opening switching position of the connecting rod fitting 131, the coupling 134, 135 is located between the wing 123 and the opening device 128 in its engagement position.
  • the clutch 134, 135 is disengaged.
  • the Tilt lock 129 is in the disengaged position when the espagnolette fitting 131 assumes its closed switch position and its rotary open switch position while it is engaged in the tilt open switch position.
  • the opening device 128 is designed as a so-called supporting opening device - according to the elliptical link principle - i. that is, it is suitable for holding the weight of the wing 123 in the closed and in the rotary opening switch position of the connecting rod fitting 131 and for introducing it into the upper, frame-side pivot joint 127.
  • the opening device 128 has an opening arm 136 which is pivotally held in the frame-side swivel joint 127 and which at its other end engages in a sliding guide 138, which can pivot and also slide longitudinally, via a collar bolt 137, which extends essentially parallel to the upper edge of the wing 123.
  • the opening device 128 has an additional arm 139, which on the one hand is articulated only pivotably on the wing 123 via a pivot pin 140, but on the other hand, also exclusively pivotable, is connected to the opening arm 136 via a pivot pin 141.
  • the opening device 128 is designed in its kinematics so that when the wing 123 is tilted open it keeps the upper wing spar aligned parallel to the upper spar of the fixed frame 122 in any possible tilting position.
  • the hinge fittings 126 and 127 are completely concealed in the air space between the folds of sash 123 and fixed frame 122.
  • Joint fittings based on the so-called cross-scissors principle, such as that described in either US Pat. No. 1,864,164 or US Pat. No. 3, can be used to form the corner joint or tilt-swivel corner bearing 126 and the swivel joint 127 722 142 can be seen as known.
  • a tension member 142 is used in the window or in the door 121. It is there effective in the direction of the vertical hinge axis 124-124 and for this purpose hung with its upper end on a fixed abutment 143 of the fixed frame 122, while its lower end engages an abutment 144 that sits on the wing 123.
  • the tension member 142 with its abutments 143 and 144 is installed above, but still in the immediate vicinity of the lower corner joint or tilt-turn corner bearing 126 between the wing 123 and the fixed frame 122, as can be clearly seen in FIG. 6.
  • FIGS. 7, 8 and 9 of the drawing show a window or a door 121, in which or which the wing 123 on the fixed frame 122 is completely covered hinge fittings lying between the horizontal folds, namely the corner joint 126 and the swivel joint 127 according to FIG. 6, is suspended.
  • the wing-side joint part 145 has the shape of an angle piece with two legs 146 and 147 directed at right angles to one another.
  • the wing-side hinge part 145 is inserted with its angle legs 146 and 147 into a stepped profile groove 148 of the rebate peripheral surface 149 of the wing 133 so that its outside is flush with the rebate peripheral surface 149.
  • the upright angle leg 147 of the wing fitting part 145 has a hook projection 150 projecting over the folded peripheral surface of the upright wing spar with an angle slot 151 which is open at the side at its lower end.
  • the hook shoulder 150 is separated from one another by two parallel to the wing plane and by a spacing gap 150c separate hook parts 150a and 150b formed, which can be clearly seen in Fig. 8.
  • the tension member 142 is provided at its lower end with a block-shaped thickening 152, preferably in the form of a cylindrical or spherical body, in which the tension member 142 is either firmly or releasably anchored.
  • the firm anchoring can take place, for example, in that the block-shaped thickening 152 is cast or pressed with the tension member 142.
  • the tension member 142 can be inserted into a diametrical bore of the block-shaped thickening 152 and subsequently fixed therein by tightening a clamping screw.
  • the tension member 142 with its block-shaped thickening 152 can be brought into coupling engagement with the hook extension 150 by simultaneously inserting the tension member 142 from the side into the spacing gap 150c between the two hook parts 150a and 150b (FIG . 8th).
  • the block-shaped thickening 152 fits snugly in the upper end region of the angle slot 151 against the flanks of the hook parts 150a and 150b of the hook attachment 150, as can be clearly seen in FIG. 7.
  • the hook extension 150 thus forms the wing-side abutment 144 according to FIG. 6.
  • the angled slot 151 in the hook attachment 150 is assigned a nose-like narrowing projection 153 in the region of its sideways opening or immediately above it.
  • This narrowing projection 153 is preferably formed by a spring tongue 154 or a snap catch, which or which is provided on or in the angle leg 147 of the wing fitting part 145, as clearly shown in FIGS. 7 and 8 of the drawing.
  • the spring tongue 154 or the snap catch elastically deflects and thereby gives the upper end region of the hook slot 151 free for the entry of the block-shaped thickening 152. If this is then inserted into the hook extension 150, the spring tongue 154 or the snap catch automatically returns to its or its blocking position and engages under the block-shaped thickening 152 while simultaneously narrowing the cross section in the hook slot 151. Only by manually pushing back the spring tongue or of the catch, the block-shaped thickening 152 of the tension member 142 can now be released again for the purpose of unhooking.
  • the narrowing projection 153 is located at the free end of the one lever arm of a two-armed lever 155, which is pivotably mounted about an axis 156 in the upright angle leg 147 of the wing fitting part 145.
  • the free end of the other lever arm of this two-armed lever 155 carries an actuating cam 157, which is pivoted into the area of the upper end of the angle slot 151, provided that the constriction projection 153 is outside the angle slot 151.
  • the tension member 142 with its block-shaped thickening 152 is now inserted into the angle slot 151 of the hook extension 150, then the block-shaped thickening 152 hits the actuating or starting cam 157 at the top and displaces it from the area of the angle slot 151 on the hook extension 150. This then results the constriction protrusion 153 below the block-shaped thickening 152 in the angular slot 151 and narrows its cross-section so that the thickening 152 can no longer escape therefrom easily.
  • the two-armed lever 155 is inserted into the wing fitting part 145 in such a way that it can move in the region of the spacing gap 150c between the two hook parts 150a and 150b.

Landscapes

  • Mechanical Engineering (AREA)
  • Engineering & Computer Science (AREA)
  • Hinges (AREA)
  • Liquid Crystal (AREA)
  • Glass Compositions (AREA)
  • Liquid Crystal Substances (AREA)
  • Window Of Vehicle (AREA)
  • Collating Specific Patterns (AREA)
  • Securing Of Glass Panes Or The Like (AREA)
  • Wing Frames And Configurations (AREA)
  • Laminated Bodies (AREA)
  • Preparation Of Compounds By Using Micro-Organisms (AREA)
  • Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)
  • Door And Window Frames Mounted To Openings (AREA)
  • Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)

Abstract

There is described a window or door 21 with a wing 23 which is mounted on a fixed frame 22 by means of articulated fittings 26, 27 at or in the vicinity of a vertical limiting edge, the window or door being characterised, for relieving the articulated fittings 26, 27 of the vertical component of the weight or load of the wing 23, by a tension member 42 which, on the one hand, engages on the wing 23 in the region of the articulated fittings 26, 27 and, on the other hand, is anchored to the fixed frame 22 counter to the weight or load of the wing 23. <IMAGE>

Description

Die Erfindung betrifft ein Fenster oder eine Tür mit Drehkippflügel, der an oder in der Nähe einer aufrechten Begrenzungskante durch Gelenkbeschläge am feststehenden Rahmen gelagert ist.The invention relates to a window or a door with a tilt and turn sash, which is mounted on or near an upright boundary edge by means of joint fittings on the fixed frame.

Derartige Fenster oder Türen sind bekannt.Such windows or doors are known.

Die den Flügel mit dem feststehenden Rahmen verbindenden Gelenkbeschläge können bei derartigen Fenstern einerseits aufliegend bzw. sichtbar vor der öffnungsseitigen Stirnfläche des feststehenden Rahmens angeordnet werden, wobei dann die seitlichen Drehgelenke an der aufrechten Begrenzungskante des Flügels liegen (vergl. DE-C- 10 78 010 und DE-C- 11 74 649).In such windows, the hinge fittings connecting the sash to the fixed frame can, on the one hand, be arranged lying or visible in front of the opening-side end face of the fixed frame, the lateral swivel joints then lying on the upright limiting edge of the sash (see DE-C-10 78 010 and DE-C-11 74 649).

Andererseits ist es aber auch möglich, Gelenkbeschläge in Benutzung zu nehmen, die eine in einer Kammer zwischen den Fälzen von Flügel und feststehenden Rahmen völlig verdeckte Einbaulage erhalten. In diesem Falle sind dann die seitlichen Drehgelenke in der Nähe der aufrechten Flügelbegrenzungskante vorgesehen (vergl. DE-C- 21 13 665).On the other hand, however, it is also possible to use hinge fittings which are installed in a position completely hidden in a chamber between the folds of the sash and the fixed frame. In this case, the lateral swivel joints are then provided in the vicinity of the upright wing edge (see. DE-C-21 13 665).

In jedem Falle werden bei diesen bekannten Fenstern oder Türen die aus dem Gewicht bzw. der Last des Flügels resultierenden Beanspruchungen in vollem Umfang über die zwischengeschalteten Gelenkbeschläge in den feststehenden Rahmen eingeleitet.In any case, in these known windows or doors, the stresses resulting from the weight or the load of the sash are fully introduced into the fixed frame via the interposed hinge fittings.

Da die Flügel der modernen Fenster- oder Türkonstruktionen ein relativ hohes Gewicht, z.B. bis zu 130 kg, aufweisen können, sind die sie mit dem feststehenden Rahmen verbindenden Gelenkbeschläge entsprechend hohen Beanspruchungen ausgesetzt. Diese führen dann hauptsächlich an den normal zur Achsrichtung der Gelenke gerichteten sowie auf- und gegeneinander abgestützten - also nach Art eines Drucklagers wirkenden - Gleitlagerflächen zu beträchtlichen Verschleißerscheinungen, wenn nicht ständig für eine einwandfreie Schmierung derselben Sorge getragen wird.Since the sash of modern window or door constructions has a relatively high weight, e.g. up to 130 kg, the hinge fittings connecting them to the fixed frame are exposed to correspondingly high loads. These then lead mainly to the normal to the axial direction of the joints and supported on and against each other - so acting in the manner of a thrust bearing - sliding bearing surfaces to considerable wear and tear, if proper lubrication is not always taken care of the same.

Darüberhinaus können sich an den Gelenkbeschlägen selbst und/oder im Verbindungsbereich derselben mit dem Flügel und dem feststehenden Rahmen bleibende Verformungen einstellen, die zu einer nachhaltigen Beeinträchtigung der ordnungsgemäßen Fenster- oder Türfunktion Anlaß geben.In addition, permanent deformations can occur on the hinge fittings themselves and / or in the connection area thereof with the sash and the fixed frame, which give rise to a lasting impairment of the proper window or door function.

Bei den bekannten Scharnieren der vorgenannten Bauart kommt es somit darauf an, den Nachteil zu vermeiden, daß hohe Flügelgewichte zu bleibenden Verformungen an den Scharnierteilen selbst und/oder an den Verbindungsstellen derselben mit dem feststehenden Rahmen und dem Flügel führen können.In the known hinges of the aforementioned type, it is therefore important to avoid the disadvantage that high sash weights can lead to permanent deformations on the hinge parts themselves and / or at the junctures thereof with the fixed frame and the sash.

Aufgabe der Erfindung ist es, eine Möglichkeit aufzuzeigen, durch die bei Fenstern oder Türen der eingangs beschriebenen Gattung - auch nachträglich noch - mit einfachen Mitteln eine weitgehende Entlastung der den Flügel mit dem feststehenden Rahmen verbindenden Gelenkbeschläge von dem in deren Achsrichtung wirkenden Flügelgewicht erreicht werden kann, ohne daß hierdurch die systembedingt vorgegebene Wirkungsweise der jeweils in Gebrauch genommenen Gelenkbeschläge beeinträchtigt wird.The object of the invention is to show a way through which, in the case of windows or doors of the type described at the outset - also subsequently - with simple means, extensive relief of the hinge fittings connecting the sash to the fixed frame can be achieved by the sash weight acting in the axial direction thereof without impairing the system-specific mode of action of the joint fittings used in each case.

Nach den Merkmalen des Anspruchs 1 ist die Lösung dieser Aufgabe erfindungsgemäß gekennzeichnet
durch ein einerseits im Bereich der Gelenkbeschläge am Flügel angreifendes sowie andererseits entgegen der Gewichtskraft bzw. Last des Flügel am feststehenden Rahmen verankertes Zugglied, das oberhalb, aber in der Nähe des unteren Eckgelenkes zwischen Flügel und feststehendem Rahmen eingebaut ist. Besonders das im Schnittpunkt zwischen der seitlichen, aufrechten Gelenkachse und der unteren, waagerechten Gelenkachse des Drehkippflügels befindliche Eckgelenk zum feststehenden Rahmen wird hierdurch entlastet. Dies gilt nicht nur bei Schließlage und in der Drehöffnungsstellung des Flügels, sondern vielmehr auch in der Kippöffnungsstellung desselben.
According to the features of claim 1, the solution to this problem is characterized according to the invention
by a tension member that engages on the one hand in the area of the joint fittings and on the other hand anchored against the weight or load of the wing on the fixed frame, which is installed above but near the lower corner joint between the wing and the fixed frame. In particular, this relieves the pressure on the corner joint at the intersection between the lateral, upright hinge axis and the lower, horizontal hinge axis of the tilt-and-turn sash to the fixed frame. This applies not only in the closed position and in the turning open position of the wing, but rather also in the tilt open position of the same.

Nach der vorangemeldeten - aber nicht vorveröffentlichten - DE-A- 38 29 053 wird - ebenso wie nach der DE-C- 329 280 - schon in Betracht gezogen, das Flügelgewicht über ein Zugglied direkt auf den Rahmen zu übertragen. Es wird jedoch in beiden Fällen die Anordnung eines auf Zug belasteten Elementes zwischen Flügelrahmen und feststehendem Rahmen ausdrücklich nur bei einem reinen Drehbeschlag für möglich gehalten. Weder der DE-C- 329 280 noch der vorangemeldeten DE-A- 38 29 053 sind aber irgendwelche Anregungen oder Hinweise in Richtung auf die erfindungsgemäße Nutzung eines zwischen Flügelrahmen und feststehendem Rahmen wirkenden und dabei auf Zug belasteten Elementes an Fenstern oder Türen mit Drehkippflügel zu entnehmen. Die DE-A- 38 29 053 weist vielmehr für Fenster und Türen mit Drehkippbeschlag ausdrücklich nur die Richtung, als Entlastungselement für die Gelenkbeschläge einen auf Druck beanspruchten Stützstab in Benutzung zu nehmen, um die Flügelkräfte sowohl beim Dreh-Öffnen als auch beim Kipp-Öffnen des Flügels in den feststehenden Rahmen einzuleiten.According to the previously reported - but not previously published - DE-A-38 29 053 - as well as according to DE-C- 329 280 - is already considered to transfer the sash weight directly to the frame via a tension member. In both cases, however, the arrangement of an element subject to tension between the sash frame and the fixed frame is expressly considered to be possible only with a pure rotating fitting. Neither DE-C-329 280 nor the previously reported DE-A-38 29 053 are any suggestions or pointers in the direction of the use according to the invention of an element acting on the sash frame and the fixed frame and thereby subject to tension on windows or doors with tilt and turn sashes remove. Rather, DE-A-38 29 053 explicitly shows only the direction for windows and doors with a tilt-and-turn fitting to use a support rod that is under pressure as a relief element for the articulated fittings, in order to open the sash forces both when opening and tilting of the wing in the fixed frame.

Im einfachsten und zugleich auch zweckmäßigsten Falle kann nach der Erfindung, nämlich gemäß Anspruch 2, das Zugglied mit seinem oberen Ende unmittelbar am feststehenden Rahmen aufgehängt werden, während es zugleich mit seinem unteren Ende am Flügel angreift.In the simplest and at the same time the most practical case, according to the invention, namely according to claim 2, the tension member can be hung with its upper end directly on the fixed frame, while at the same time it engages with its lower end on the wing.

Wenn in diesem Falle das Zugglied, entsprechend der Lehre des Anspruchs 3, ständig unter straffer Zugspannung gehalten ist, kann die Vertikalkomponente aus der Gewichtskraft bzw. Last des Flügels unmittelbar in den feststehenden Rahmen eingeleitet werden, so daß die Gelenkbeschläge praktisch nur noch Beanspruchungen aufzunehmen haben, welche aus Horizontalkomponenten der Gewichtskraft bzw. Last des Flügels resultieren und im wesentlichen quer zu deren Gelenkachsen gerichtet sind.If in this case the tension member, according to the teaching of claim 3, is kept constantly under tension, the vertical component can be introduced directly from the weight or load of the sash into the fixed frame, so that the hinge fittings have to absorb practically only stresses , which result from horizontal components of the weight or load of the wing and are directed essentially transversely to their hinge axes.

Denkbar wäre es nach der Erfindung zwar auch, auf das Zugglied relativ zu seinem am feststehenden Rahmen befindlichen Widerlager eine Gegenkraft, beispielsweise in Form eines das Flügelgewicht ausbalanciernden Gegegengewichtes oder aber in Form einer entsprechend vorgespannten Feder, einwirken zu lassen. Für die Unterbringung derartiger Zusatzelemente muß dann jedoch ein entsprechender Einbauraum zu Verfügung stehen, der aber bei herkommlichen Fenster- und Türkonstruktionen nicht ausnahmslos vorhanden ist.It would also be conceivable according to the invention to have a counterforce act on the tension member relative to its abutment located on the fixed frame, for example in the form of a counterweight balancing the sash weight or in the form of a correspondingly preloaded spring. A corresponding installation space must then be available for the accommodation of such additional elements, but this is not without exception available in conventional window and door constructions.

Bei Fenstern oder Türen, die mit einem Drehkippflügel ausgestattet sind, der also im Schnittpunkt zwischen seiner seitlichen, aufrechten Gelenkachse und seiner unteren, waagerechten Gelenkachse über ein sogenanntes Eckgelenk am feststehenden Rahmen abgestützt ist, erweist es sich als funktionswesentlich, daß das Zugglied oberhalb, aber in der Nähe des unteren Eckgelenkes zwischen Flügel und feststehendem Rahmen eingebaut ist.For windows or doors that are equipped with a tilt and turn sash, which is supported at the intersection between its lateral, upright hinge axis and its lower, horizontal hinge axis via a so-called corner joint on the fixed frame, it proves to be functionally essential that the tension member is above, but is installed near the lower corner joint between sash and fixed frame.

Durch diese Maßnahme wird nämlich auf einfache Art und Weise sichergestellt, daß die das untere Eckgelenk bildenden Gelenkbeschläge nicht nur bei Schließlage und in der Drehöffnungsstellung des Flügels, sondern vielmehr auch in der Kippöffnungsstellung desselben weitestgehend von der Gewichtskraft des Flügels entlastet bleiben.This measure ensures in a simple manner that the hinge fittings forming the lower corner joint remain largely relieved of the weight of the sash not only when the sash is in the closed position and when the sash is in the rotational opening position, but also when the sash is in the tilt opening position.

Nach Anspruch 4 ist erfindungsgemäß weiterhin vorgesehen, daß das Zugglied von einem Seil oder einem Kabel gebildet ist oder ggf. auch aus einem Bowdenzug besteht.According to claim 4 it is further provided according to the invention that the tension member is formed by a rope or a cable or possibly also consists of a Bowden cable.

Ein solchermaßen ausgebildetes Zugglied benötigt nicht nur einen geringen Einbauraum, sondern es kann sich den beim Öffnen und Schließen des Fensters oder der Tür vorkommenden Relativbewegungen des Flügels zum feststehenden Rahmen unter Aufrechterhaltung seiner Wirkung problemlos anpassen.A tension member designed in this way not only requires a small installation space, but it can easily adapt to the relative movements of the wing relative to the fixed frame when the window or door is opened and closed while maintaining its effect.

Als besonders zweckmäßig hat es sich erwiesen, wenn das Zugglied nach dem Vorschlag des Anspruchs 5 erfindungsgemäß verdeckt im luftraum zwischen den Fälzen von Flügel und Rahmen untergebracht ist.It has proven particularly expedient if, according to the invention, the tension member is concealed according to the invention in the air space between the folds of sash and frame.

Auch kann es sich nach Anspruch 6 zwecks problemloser Anpassung an unterschiedliche Bedarfsfälle als vorteilhaft erweisen, wenn das Zugglied zumindest begrenzt längenverstellbar ausgebildet ist.It can also prove to be advantageous for the purpose of easy adaptation to different needs if the tension member is at least limitedly adjustable in length.

Abweichend von Anspruch 4 ist es nach der Erfindung gemäß Anspruch 7 aber auch möglich, das Zugglied aus einem starren Zugstab bestehen zu lassen, dessen Enden durch kardanische bzw. kugelige Verbindungsglieder am Flügel und am feststehenden Rahmen angreifen.Deviating from claim 4, it is also possible according to the invention according to claim 7, to let the tension member consist of a rigid tension rod, the ends of which engage by gimbal or spherical connecting links on the wing and on the fixed frame.

Im Rahmen der Erfindung liegt es nach Anspruch 8 auch, das Zugglied relativ zu dem am feststehenden Rahmen befindlichen Widerlager unter eine Gegenkraft, z.B. ein das Flügelgewicht ausbalancierendes Gegengewicht oder eine entsprechend vorgespannte Feder, zu setzen.It is also within the scope of the invention, according to claim 8, to place the tension member relative to the abutment located on the fixed frame under a counterforce, for example a counterweight balancing the sash weight or a correspondingly preloaded spring.

Dabei kann nach Anspruch 9 das Zugglied am feststehenden Rahmen um das ortsfeste Widerlager, z.B. mittels einer Rolle, herumgeführt und durch die Gegenkraft, beispielsweise das Gegengewicht, unter Zugspannung gesetzt werden.According to claim 9, the tension member on the fixed frame around the stationary abutment, e.g. be guided around by means of a roller and placed under tension by the counterforce, for example the counterweight.

Darüberhinaus schlägt die Erfindung gemäß Anspruch 10 aber auch vor, als Zugglied mindestens ein tordierbares Flachband-Material, insbesondere Federstahlband, zu benutzten. In diesem Falle hat es sich bewährt, wenn das Flachband-Material eine Breite hat, die einem Vielfachen, z. B. etwa dem Sechzehnfachen bis Zwanzigfachen, seiner Dicke entspricht, während dieses Flachband-Material sich bei in Schließlage am feststehenden Rahmen anliegendem Flügel über seine ganze Länge mit seiner Breitseite wenigstens annähernd parallel zu den Falzflächen bzw. quer zu den Hauptebenen von Flügel und feststehendem Rahmen erstreckt.In addition, however, the invention also proposes to use at least one twistable flat strip material, in particular spring steel strip, as the tension member. In this case, it has proven useful if the flat strip material has a width which is a multiple, e.g. B. about sixteen times to twenty times its thickness, while this flat strip material is in the closed position on the fixed frame wing over its entire length with its broad side at least approximately parallel to the folded surfaces or transversely to the main planes of the wing and the fixed frame extends.

Bei Fenstern oder Türen mit Drehflügel ist bereits vorgeschlagen worden, das Zugglied im Bereich der Gelenkbeschläge praktisch in beliebiger Höhezwischen dem Flügel und dem feststehenden Rahmen einzubauen. Bei Fenstern oder Türen mit Drehkippflügel ist es jedoch - wie bereits erwähnt - von wesentlicher Bedeutung, daß das Zugglied zumindest in der Nähe des unteren Eckgelenkes am Flügel angreift.In the case of windows or doors with rotating sashes, it has already been proposed to install the tension member in the area of the hinge fittings practically at any height between the sash and the fixed frame. In the case of windows or doors with a tilt and turn sash, however - as already mentioned - it is essential that the tension member acts on the sash at least in the vicinity of the lower corner joint.

In der Praxis ist es dabei nicht nur notwendig, den Flügel über die Gelenkbeschjäge relativ zum feststehenden Rahmen dauerhaft funktionssicher zu halten und zu führen. Vielmehr erweist es sich auch als wichtig, die Anordnung des Zuggliedes zwischen dem feststehenden Rahmen und dem Flügel so zu treffen, daß dieses sich beim Einhängevorgang des Flügels ebenfalls leicht und funktionssicher in Halteeingriff bringen läßt, während es beim Aushängen des Flügels auch ebenso leicht entkuppelt werden kann.In practice, it is not only necessary to keep the sash functionally stable and to guide it in relation to the fixed frame. Rather, it also proves to be important to arrange the tension member between the fixed frame and the wing in such a way that it can also be easily and functionally securely engaged when the wing is hooked in, while it can also be uncoupled just as easily when the wing is unhooked can.

Es kommt also darauf an, zumindest den Verbindungsbereich zwischen dem Zugglied und dem in seiner Funktionsstellung von diesem entgegen seiner Gewichtskraft gehaltenem Flügel mit baulich einfachen Mitteln so zu gestalten, daß ein leichtes und manuell einfaches Kuppeln und Entkuppeln der Verbindungselemente gewährleistet ist.It is therefore important to design at least the connection area between the tension member and the wing held in its functional position by the latter against its weight, using structurally simple means, that an easy and manually simple coupling and uncoupling of the connecting elements is guaranteed.

Erreicht wird dieses Ziel nach der Erfindung gemäß Anspruch 11 dadurch, daß das flügelseitige Gelenkteil einen über die Begrenzungsfläche des aufrechten Flügelholmes auslegerartig vorspringenden Hakenansatz mit einem an seinem unteren Ende seitwärts offenen Winkelschlitz aufweist,
daß der Hakenansatz zwei zur Flügelebene parallele und durch einen Abstandsspalt voneinander getrennte Hakenteile aufweist
und daß das Zugglied an seinem unteren Ende mit einer blockförmigen Verdikkung versehen ist, deren Querschnittsabmessung an die Breite des Winkelschlitzes angepaßt ist, während der Abstandsspalt eine Aufnahme für das Zugglied bildet.
This aim is achieved according to the invention in that the wing-side joint part has a hook extension projecting over the boundary surface of the upright wing spar with an angular slot that is open sideways at its lower end,
that the hook approach has two parallel to the wing plane and separated by a spacing gap hook parts
and that the tension member is provided at its lower end with a block-shaped thickening, the cross-sectional dimension of which is adapted to the width of the angular slot, while the spacing gap forms a receptacle for the tension member.

Der besondere Vorteil dieses lösungsprinzips liegt darin, daß die zusammenwirkenden Kupplungselemente relativ groß und kräftig ausgeführt werden können und dadurch eine leichte Handhabung beim Ein- und Aushängevorgang ermöglichen.The particular advantage of this solution principle lies in the fact that the interacting coupling elements can be made relatively large and powerful and thereby enable easy handling during the hanging and unhooking process.

Als besonders vorteilhaft hat es sich aber auch erwiesen, wenn nach der Erfindung die blockförmige Verdickung aus einem Zylinder- oder Kugelkörper besteht, in dem das Zugglied fest oder lösbar verankert ist. Die lösbare Verankerung kann dabei beispielsweise mit Hilfe einer Klemmschraube erfolgen, die eine solche lage bzw. Anordnung in der blockförmigen Verdickung aufweist, daß sie im Einhängezustand des Zuggliedes am flügelseitigen Gelenkteil nicht zugänglich ist.However, it has also proven to be particularly advantageous if, according to the invention, the block-shaped thickening consists of a cylindrical or spherical body in which the tension member is firmly or releasably anchored. The releasable anchoring can take place, for example, with the aid of a clamping screw which has such a position or arrangement in the block-shaped thickening that it is not accessible on the wing-side joint part when the tension member is hooked on.

Erfindungsgemäß hat es sich auch als vorteilhaft erwiesen, wenn das flügelseitige Gelenkteil ein Winkelstück ist, das im Bereich der Flügelecke mit seinen beiden Winkelschenkeln in eine stufenförmig profilierte Nut an der Falzumfangsfläche einsetzbar ist.According to the invention, it has also proven to be advantageous if the wing-side joint part is an angle piece which can be used in the area of the wing corner with its two angle legs in a step-shaped profiled groove on the circumferential surface of the fold.

Dabei hat sich herausgestellt, daß es besonders zweckmäßig ist, wenn beim Einhängevorgang für den Flügel zunächst das Zugglied mit diesem gekuppelt wird und erst daran anschließend der Einhängevorgang des Flügels in die Gelenkbeschläge stattfindet. Das Zugglied kann dann nämlich schon das Flügelgewicht in den feststehenden Rahmen einleiten, während die Verbindung der Flügels mit den Gelenkbeschlägen vorgenommen wird.It has been found that it is particularly useful if the tension member is first coupled to the wing during the hooking-in process and then the wing is hooked into the hinge fittings. The tension member can then already introduce the sash weight into the fixed frame while the sash is connected to the hinge fittings.

Bei der Benutzung eines Seiles oder Kabels als Zugglied ist es zwar denkbar, dessen dem Flügel zugeordnetes Ende mit einer Schlaufe zu versehen, die sich in einen am flügelseitigen Gelenkteil vorgesehenen und ein verdicktes Kopfteil oder eine Umfangsnut aufweisenden Tragzapfen einhängen läßt. Da sich aber unter der Einwirkung des Flügelgewichtes die Schlaufe verengt, kann es Schwierigkeiten bereiten, wenn bei einem notwendig werdenden Aushängen des Flügels das Zugglied von diesem entkuppelt werden muß.When using a rope or cable as a tension member, it is conceivable to provide the wing associated end with a loop that can be attached to a wing part on the hinge part and a thickened head part or a circumferential groove bearing pin. However, since the loop narrows under the influence of the wing weight, it can be difficult if the tension member has to be uncoupled from the wing when it becomes necessary to unhook it.

Nach einem weiterbildenden Ausgestaltungsmerkmal der Erfindung kann dem Winkelschlitz des Hakenansatzes gemäß Anspruch 12 im Bereich der seitwärts gerichteten Öffnung oder unmittelbar oberhalb derselben ein nasenartiger Verengungsvorsprung zugeordnet werden, und zwar so, daß ein unerwünschtes Aushängen des Zuggliedes aus dem flügelseitigen Gelenkteil verhindert wird. Im einfachsten Falle kann dabei der Verengungsvorsprung erfindungsgemäß aus einer Federzunge oder aber einem R astschnäpper bestehen, die bzw. der am flügelseitigen Gelenkteil vorgesehen ist.According to a further development feature of the invention, the angled slot of the hook extension in accordance with claim 12 can be assigned a nose-like narrowing projection in the area of the sideways opening or immediately above it, in such a way that an undesired unhooking of the tension member from the wing-side joint part is prevented. In the simplest case, the narrowing protrusion according to the invention can consist of a spring tongue or a snap catch, which is provided on the wing-side joint part.

Schließlich wird es auch als im Rahmen der Erfindung liegend angesehen, wenn der Verengungvorsprung sich am freien Ende des einen Hebelarms eines schwenkbeweglich im flügelseitigen Gelenkteil gehaltenen, zweiarmigen Hebels befindet, der am freien Ende seines anderen Hebelarms wiederum einen Stellnocken trägt, der in den Winkelschlitz des Hakenansatzes hineinragt, solange der Verengungsvorsprung nicht in den Winkelschlitz des Hakenansatzes eingreift.Finally, it is also considered to be within the scope of the invention if the narrowing projection is located at the free end of one lever arm of a two-armed lever which is pivotally held in the wing-side joint part and which, in turn, carries an actuating cam at the free end of its other lever arm which fits into the angle slot of the Hook approach protrudes as long as the narrowing projection does not engage in the angular slot of the hook approach.

In der Zeichnung ist der Gegenstand der Erfindung an Ausführungsbeispielen dargestellt. Es zeigt

  • Fig. 1 eine schematische Darstellung eines Fensters oder einer Tür, bei welchem bzw. welcher der Flügel am feststehenden Rahmen als Drehkippflügel angeschlagen ist und die Gelenkbeschläge verdeckt zwischen den Fälzen von Flügel und Rahmen untergebracht sind,
  • Fig. 2 in größerem Maßstab einen parallel zur Zeichnungsebene der Fig. 1 liegenden Teilschnitt durch den Flügel und den feststehenden Rahmen des Fensters oder der Tür bei ausführlicher Darstellung eines Gelenkbeschlages,
  • Fig. 3 in schematisch vereinfachter Darstellung eine Ansicht in Pfeilrichtung III des Fensters bzw. der Tür nach Fig. 2 bei gegenüber dem feststehenden Rahmen in Drehstellung geöffnetem Flügel,
  • Fig. 4 wiederum in schematisch vereinfachter Darstellung eine Ansicht des Fensters bzw. der Tür in Pfeilrichtung IV der Fig. 3 und
  • Fig. 5 eine der Fig. 4 ähnliche schematisch vereinfachte Ansicht des Fensters bzw. der Tür, jedoch bei gegenüber dem feststehenden Rahmen in Kippstellung geöffnetem Flügel;
  • Fig. 6 ein Fenster oder eine Tür, bei welchem bzw. welcher der Flügel am feststehenden Rahmen als Drehkippflügel angeschlagen ist und die Gelenkbeschläge verdeckt zwischen den Fälzen von Flügel und Rahmen untergebracht sind,
  • Fig. 7 im größeren Maßstab den in Fig. 6 mit VII gekennzeichneten Ausschnittbereich in ausführlicher Ansichtsdarstellung,
  • Fig. 8 eine Ansicht in Pfeilrichtung VIII der Fig. 7 und
  • Fig. 9 den erfindungswesentlichen Teilbereich der Fig. 7 in abgewandelter baulicher Ausführung.
In the drawing, the object of the invention is shown in exemplary embodiments. It shows
  • 1 is a schematic representation of a window or a door, in which the wing is attached to the fixed frame as a tilt and turn wing and the hinge fittings are concealed between the rebates of the wing and frame,
  • 2 is a partial section parallel to the plane of the drawing of FIG. 1 through the sash and the fixed frame of the window or door with a detailed representation of a hinge fitting,
  • 3 shows, in a schematically simplified representation, a view in the direction of arrow III of the window or door according to FIG. 2 with the sash open relative to the fixed frame in the rotational position,
  • Fig. 4 again in a schematic simplified representation a view of the window or the door in the direction of arrow IV of Fig. 3 and
  • 5 shows a schematically simplified view of the window or door similar to FIG. 4, but with the sash open in relation to the fixed frame in the tilted position;
  • 6 a window or a door in which the wing is attached to the fixed frame as a tilt and turn wing and the hinge fittings are concealed between the rebates of the wing and frame,
  • 7 on a larger scale the detail area marked VII in FIG. 6 in a detailed view,
  • Fig. 8 is a view in the direction of arrow VIII of Fig. 7 and
  • FIG. 9 shows the partial area of FIG. 7 essential to the invention in a modified structural design.

In Fig. 1 der Zeichnung ist ein Fenster bzw. eine Tür 21 zu sehen, das bzw. die einen feststehenden Rahmen 22 und einen Flügel 23 umfaßt. Der Flügel 23 ist dabei im feststehenden Rahmen 22 wahlweise.um eine seitlich lotrechte Achse 24-24 in eine Drehöffnungsstellung oder um eine untere horizontale Achse 25-25 in eine Kippöffnungsstellung beweglich angeordnet. Der Flügel 23 wird zu diesem Zweck am feststehenden Rahmen 22 im Schnittpunkt der beiden Gelenkachsen 24-24 und 25-25 durch ein Eckgelenk bzw. ein Drehkipp-Ecklager 26 abgestützt. Darüberhinaus befindet sich oben zwischen dem Flügel 23 und dem feststehenden Rahmen 22 ein Drehgelenk 27 einer Ausstellvorrichtung 28, während zwischen der verschlußseitigen unteren Ecke von Flügel 23 und feststehendem Rahmen 22 eine Kippverriegelung 29 vorgesehen ist.In Fig. 1 of the drawing, a window or door 21 can be seen, which comprises a fixed frame 22 and a wing 23. The wing 23 is optionally arranged in the fixed frame 22 so as to be movable about a laterally perpendicular axis 24-24 in a rotational opening position or about a lower horizontal axis 25-25 in a tilt opening position. For this purpose, the wing 23 is supported on the fixed frame 22 at the intersection of the two hinge axes 24-24 and 25-25 by a corner joint or a tilt and turn corner bearing 26. In addition, there is a swivel joint 27 of an opening device 28 between the wing 23 and the fixed frame 22, while a tilt lock 29 is provided between the lower corner of the wing 23 and the fixed frame 22 on the lock side.

Ein über eine Bedienungshandhabe 30 verstellbarer Treibstangenbeschlag 31 ist im Flügel 23 so untergebracht, daß damit einerseits eine Verriegelung und Entriegelung des in der Schließlage befindlichen Flügels 23 am feststehenden Rahmen 22 über Riegelnocken 32 und zugehörige Riegeleingriffe 33 bewirkt werden kann. Andererseits ist der Treibstangenbeschlag 31 jedoch auch noch so ausgelegt, daß sich mit seiner Hilfe sowohl eine Kupplung 34, 35 zwischen dem Flügel 23 und der Ausstellvorrichtung 28 als auch die Kippverriegelung 29 ein- und ausrücken läßt. Sowohl in der Verschluß-Schaltstellung als auch in der Drehöffnungs-Schaltstellung des Treibstangenbeschlages 31 befindet sich die Kupplung 34, 35 zwischen dem Flügel 23 und der Ausstellvorrichtung 28 in ihrer Einrückstellung. In der Kippöffnungs-Schaltstellung des Treibstangenbeschlages 31 ist hingegen die Kupplung 34, 35 ausgerückt. Die Kippverriegelung 29 befindet sich in ausgerückter Stellung, wenn der Treibstangenbeschlag 31 seine Verschluß-Schaltstellung und seine Drehöffnungs-Schaltstellung einnimmt, während sie in der Kippöffnungs-Schaltstellung eingerückt ist.A drive rod fitting 31, which can be adjusted via an operating handle 30, is accommodated in the wing 23 in such a way that, on the one hand, locking and unlocking of the wing 23 in the closed position on the fixed frame 22 can be effected by means of locking cams 32 and associated locking engagements 33. On the other hand, the connecting rod fitting 31 is also designed so that it can be used to engage and disengage both a coupling 34, 35 between the wing 23 and the opening device 28 and the tilt lock 29. Both in the closed switching position and in the rotary opening switching position of the connecting rod fitting 31, the clutch 34, 35 is in its engagement position between the wing 23 and the opening device 28. In the tilt-open switching position of the connecting rod fitting 31, however, the clutch 34, 35 is disengaged. The tilt lock 29 is in the disengaged position when the espagnolette fitting 31 assumes its closed switch position and its rotary open switch position while it is engaged in the tilt open switch position.

Die Ausstellvorrichtung 28 ist als sogenannte tragende Ausstellvorrichtung ausgebildet, d.h., sie ist geeignet, in der Verschluß- und in der DrehöffnungsSchaltstellung des Treibstangenbeschlages 31 das Gewicht des Flügels 23 zu halten sowie in das obere, blendrahmenseitige Drehgelenk 27 einzuleiten. Zu diesem Zweck weist die Ausstellvorrichtung 28 einen im rahmenseitigen Drehgelenk 27 schwenkbar gehaltenen Ausstellarm 36 auf, der an seinem anderen Ende über einen Bundbolzen 37 sowohl schwenkbeweglich als auch längsschiebbar in eine Gleitführung 38 eingreift, die sich im wesentlichen parallel zur Oberkante des Flügels 23 erstreckt. Außerdem hat die Ausstellvorrichtung 28 einen Zusatzarm 39, welcher einerseits über einen Gelenkzapfen 40 ausschließlich schwenkbar am Flügel 23 angelenkt ist, andererseits aber, eben falls ausschließlich schwenkbar, über einen Gelenkzapfen 41 mit dem Ausstellarm 36 in Verbindung steht.The opening device 28 is designed as a so-called supporting opening device, ie it is suitable for the weight of the wing 23 in the closed position and in the rotary opening switch position of the connecting rod fitting 31 to hold and to initiate in the upper frame hinge 27. For this purpose, the opening device 28 has an opening arm 36 which is pivotally held in the frame-side swivel joint 27 and which at its other end engages in a sliding guide 38, which can pivot and also slide longitudinally, via a collar pin 37 and extends essentially parallel to the upper edge of the wing 23. In addition, the opening device 28 has an additional arm 39, which on the one hand is articulated only pivotably on the wing 23 via a hinge pin 40, but on the other hand, if only pivotable, is connected to the opening arm 36 via a hinge pin 41.

Die Ausstellvorrichtung 28 ist dabei in ihrer Kinematik so ausgelegt, daß sie beim Kippöffnen des Flügels 23 den oberen Flügelholm in jeder möglichen Kipplage parallel zum oberen Holm des feststehenden Rahmens 2 ausgerichtet hält.The opening device 28 is designed in its kinematics so that it keeps the upper wing spar aligned in every possible tilt position parallel to the upper spar of the fixed frame 2 when the wing 23 is opened.

Beim Fenster 21 nach Fig. 1 wird der Flügel 23 am feststehenden Rahmen 22 über Gelenkbeschläge gehalten, die völlig verdeckt im Luftraum zwischen den Fälzen von Flügel 23 und feststehendem Rahmen 22 untergebracht sind. Sowohl zur Bildung des Eckgelenkes bzw. Drehkipp-Ecklagers 26 als auch des Drehgelenkes 27 können dabei Gelenkbeschläge in Benutzung genommen werden, die in ihrer Wirkungsweise z.B. auf dem Pantographen- bzw. Storchschnabelprinzip basieren - siehe z. B. DE-OS 25 08 174 und DE-PS 35 19 988 -.In the window 21 according to FIG. 1, the sash 23 is held on the fixed frame 22 by means of hinge fittings which are completely concealed in the air space between the rebates of sash 23 and the fixed frame 22. In order to form the corner joint or tilt and turn corner bearing 26 and the swivel joint 27, joint fittings can be used which, in their mode of operation, e.g. based on the pantograph or cranesbill principle - see e.g. B. DE-OS 25 08 174 and DE-PS 35 19 988 -.

Zur Entlastung des Eckgelenkes bzw. Drehkipp-Ecklagers 26 von der Vertikalkomponente der Gewichteskraft bzw. Last des Flügels 23 wird auch beim Fenster bzw. bei der Tür 21 nach Fig. 1 ein Zugglied 42 in Benutzung genommen. Es ist dabei in Richtung der vertikalen Gelenkachse 24-24 wirksam und zu diesem Zweck mit seinem oberen Ende an einem ortsfesten Widerlager 43 des feststehenden Rahmens 22 aufgehängt, während sein unteres Ende an einem Widerlager 44 angreift, das am Flügel 23 sitzt. In diesem Falle ist das Zugglied 42 mit seinen Widerlagern 43 und 44 insgesamt zwar oberhalb, aber noch in nächster Nähe des unteren Eckgelenkes bzw. Drehkipp-Ecklagers 26 zwischen dem Flügel 23 und dem feststehenden Rahmen 22 eingebaut, wie das deutlich aus Fig. 1 hervorgeht.To relieve the corner joint or turn-tilt corner bearing 26 from the vertical component of the weight or load of the wing 23, a tension member 42 is also used in the window or in the door 21 according to FIG. 1. It is effective in the direction of the vertical hinge axis 24-24 and for this purpose is hung with its upper end on a fixed abutment 43 of the fixed frame 22, while its lower end engages an abutment 44 which sits on the wing 23. In this case, the tension member 42 with its abutments 43 and 44 is overall above, but still installed in the immediate vicinity of the lower corner joint or rotary tilt corner bearing 26 between the wing 23 and the fixed frame 22, as can be clearly seen in FIG. 1.

Das Zugglied 42 nach Fig. 1 ist z.B. verdeckt im Luftraum zwischen den Fälzen von Flügel 23 und feststehendem Rahmen 22 des Fensters 21 eingebaut.The tension member 42 of Fig. 1 is e.g. hidden in the air space between the rebates of wing 23 and fixed frame 22 of the window 21 installed.

Anordnung, Ausbildung und Wirkungsweise des Zuggliedes 42 nach Fig. 1 ergeben sich aus den Fig. 2 bis 5 der Zeichnung, welche ein Fenster, oder eine Tür 21 zeigen, bei welchem bzw. welcher der Flügel 23 am feststehenden Rahmen 22 über völlig verdeckt zwischen den horizontalen Fälzen von Flügel 23 und feststehendem Rahmen 22 liegende Gelenkbeschläge (Eckgelenk 26 und Drehgelenk 27) aufgehängt ist. Die Gelenkbeschläge nach den Fig. 2 bis 4 beruhen dabei auf einer Bauart und Wirkungsweise, wie sie grundsätzlich, beispielsweise durch die GB-PS 496 829, bereits vorbekannt ist.The arrangement, design and mode of operation of the tension member 42 according to FIG. 1 result from FIGS. 2 to 5 of the drawing, which show a window or a door 21, in which the wing 23 on the fixed frame 22 is completely hidden between the horizontal folds of sash 23 and fixed frame 22 lying joint fittings (corner joint 26 and pivot joint 27) is suspended. The joint fittings according to FIGS. 2 to 4 are based on a type and mode of operation which is already known in principle, for example from GB-PS 496 829.

In Fig. 2 der Zeichnung ist der als Eckgelenk bzw. Drehkipp-Ecklager 26 ausgeführte Gelenkbeschlag in einer ausführlichen Längsschnitt-Darstellung gezeigt. Er hat dabei eine Ausbildung, die nicht nur ein Drehöffnen des Flügels 23 um die aufrechte Achse 24-24 ermöglicht, sondern darüberhinaus den Flügel 23 auch für ein Kippöffnen um die untere, waagerechte Achse 25-25 abstützt.In Fig. 2 of the drawing, the articulated fitting designed as a corner joint or turn-tilt corner bearing 26 is shown in a detailed longitudinal section. He has a design that not only allows the wing 23 to be rotated about the upright axis 24-24, but also supports the wing 23 for tilt opening about the lower, horizontal axis 25-25.

Der das Drehgelenk 27 bildende obere Gelenkbeschlag ist hingegen Teil der Ausstellvorrichtung 28, die den Flügel 23 sowohl in der Schließlage als auch beim Drehöffnen und Kippöffnen hält, trägt und führt.The upper hinge fitting forming the swivel joint 27, on the other hand, is part of the opening device 28, which holds, supports and guides the wing 23 both in the closed position and during the swivel opening and tilt opening.

Beide Gelenkbeschläge, also Eckgelenk 26 und Drehgelenk 27, sind als Lenkhebelgetriebe ausgeführt, die eine weitgehend übereinstimmende Kinematik aufweisen. Dabei ist aus Fig. 3 ersichtlich, daß jedes Lenkhebelgetriebe einen Traglenker 45 aufweist, der über ein Gelenk 46 - gemäß Fig. 2 über ein Kugelgelenk 46 - an seinem hinteren Ende auf einer Befestigungsschiene 47 ruht, die an der Falzumfangsfläche des feststehenden Rahmens 22 anliegend, starr befestigt ist.Both joint fittings, that is to say corner joint 26 and swivel joint 27, are designed as steering lever gears which have largely identical kinematics. It can be seen from FIG. 3 that each steering lever transmission has a supporting link 45, which via a joint 46 - according to FIG a ball joint 46 - at its rear end rests on a mounting rail 47 which is rigidly attached to the circumferential surface of the fixed frame 22.

Das Lenkhebelgetriebe hat weiterhin einen an der Falzumfangsfläche des Flügels 23 montierten, beispielsweise in eine parallel zu dessen Hauptebene verlaufende, abgesetzte Profilnut 48 eingesetzten Hauptlenker 49, der mit dem Traglenker 45 durch zwei Verbindungslenker 50 und 51 gekuppelt ist. Dabei ist der Verbindungslenker 50 über einen Gelenkbolzen 52 ausschließlich schwenkbeweglich auf dem Traglenker 45 angeordnet, während er über einen Gelenkbolzen 53, ebenfalls ausschließlich schwenkbeweglich, am Hauptlenker 49 angreift.The steering lever gearbox also has a main link 49 mounted on the rebate circumferential surface of the wing 23, for example inserted into a stepped profile groove 48 running parallel to its main plane, which is coupled to the supporting link 45 by two connecting links 50 and 51. In this case, the connecting link 50 is arranged on the supporting link 45 exclusively via a pivot pin 52, while it acts on the main link 49 via a link pin 53, also exclusively pivotable.

Auch der Verbindungslenker 51 ist ausschließlich schwenkbeweglich durch einen Gelenkbolzen 54 auf dem Traglenker 45 gehalten, während er mit einem Gelenkbolzen 55 lediglich schwenkbeweglich am Hauptlenker 49 angreift. Beide Verbindungslenker 50 und 51 haben zwischen ihren Gelenkbolzen 52, 53 bzw. 54, 55 übereinstimmende Länge und sind dabei so angeordnet, daß sie mit dem Traglenker 45 und dem Hauptlenker 49 ein Parallelogramm-Lenkhebelgetriebe bilden.The connecting link 51 is also held exclusively on the supporting link 45 in a pivotable manner by means of a pivot pin 54, while it only acts pivotably on the main link 49 with a pivot pin 55. Both connecting links 50 and 51 have the same length between their hinge pins 52, 53 and 54, 55 and are arranged so that they form a parallelogram steering lever mechanism with the supporting link 45 and the main link 49.

Zur zwangsweisen Bewegungssteuerung jedes von einem Parallelogramm-Lenkhebelgetriebe gebildeten Gelenkbeschlages (Eckgelenk 26 bzw. Drehgelenk 27) dient ein Steuerarm 56, der starr an einem der beiden Verbindungslenker 50 bzw. 51, und zwar vorzugsweise am Verbindungslenker 51, angreift. Andererseits ist er über einen Gleitzapfen 57 in einer Schlitzführung 58 beweglich, die sich parallel zur Hauptebene des feststehenden Rahmens 22 erstreckt und in einer Verlängerung der Anschraubplatte 47 angeordnet werden kann.A control arm 56, which rigidly engages one of the two connecting links 50 and 51, preferably on the connecting link 51, is used for the compulsory movement control of each joint fitting (corner joint 26 or swivel joint 27) formed by a parallelogram steering lever transmission. On the other hand, it can be moved via a sliding pin 57 in a slot guide 58 which extends parallel to the main plane of the fixed frame 22 and can be arranged in an extension of the screw-on plate 47.

Bei der Öffnungs- und Schließbewegung des Flügels 23 um die lotrechte Achse 24-24 wird mit Hilfe des Steuerarms 56 eine Zwangssteuerung der Gelenkbeschläge (Eckgelenk 26 und Drehgelenk 27) herbeigefügt, und zwar in der Weise, daß über einen Offnungswinkel des Flügels 23 von mindestens 90° hinweg zu keiner Zeit der Flügelüberschlag 23a mit der raumseitigen Stirnfläche 22a des feststehenden Rahmens 22 kollidieren kann. Lediglich bei in Schließlage am feststehenden Rahmen 22 zur Anlage kommendem Flügel 23 legt sich der Flügelüberschlag 23a mit seiner rückseitigen Fläche gegen die raumseitige Stirnfläche 22a des Blendrahmens 22 an.During the opening and closing movement of the wing 23 about the vertical axis 24-24, a control of the joint fittings (corner joint 26 and pivot joint 27) is brought about with the help of the control arm 56, in such a way that over an opening angle of the wing 23 of at least 90 ° at no time the wing flap 23a with the room side End face 22a of the fixed frame 22 can collide. Only when the wing 23 comes to rest in the closed position on the fixed frame 22 does the wing flap 23a rest with its rear surface against the end face 22a of the frame 22 on the room side.

Da allein mit Hilfe der die Gelenkbeschläge (Eckgelenk 26 und Drehgelenk 27) bildenden Parallelogramm-Lenkhebelgetriebe in der Schließlage des Flügels 23, und zwar insbesondere im Bereich der vertikalen Achse 24-24, kein ausreichender Dichtungs-Anpreßdruck in Richtung gegen den feststehenden Rahmen 22 hervorgebracht werden kann, sind diesen noch besondere Riegelvorrichtungen zugeordnet. Im Bereich des das Drehgelenk 27 bildenden - oberen - Gelenkbeschlages handelt es sich dabei um die bereits im Zusammenhang mit der Ausstellvorrichtung 28 weiter oben erläuterte Kupplung 34 und 35.Since with the help of the joint fittings (corner joint 26 and swivel joint 27) forming the parallelogram steering lever mechanism in the closed position of the wing 23, in particular in the area of the vertical axis 24-24, no sufficient sealing contact pressure in the direction against the fixed frame 22 is produced special locking devices are assigned to them. In the area of the upper joint fitting forming the swivel joint 27, this is the coupling 34 and 35 already explained above in connection with the opening device 28.

Die Riegelvorrichtung im Bereich des als Eckgelenk bzw. Drehkipp-Ecklager 26 wirkenden - unteren - Gelenkbeschlages hat hingegen vorzugsweise eine Anordnung, Ausbildung und Wirkungsweise, wie sie in der DE-PS 38 34 388 ausführlich erläutert wird.The locking device in the region of the lower joint joint, which acts as a corner joint or tilt-turn corner bearing 26, on the other hand, preferably has an arrangement, design and mode of operation as is explained in detail in DE-PS 38 34 388.

Diese Riegelvorrichtung 59 besteht gemäß Fig. 2 aus einem am Flügel 23 parallel zu dessen Ebene beweglich geführten Riegelschieber 60 und einem am feststehenden Rahmen 22 fixierten Riegelansatz 61.According to FIG. 2, this locking device 59 consists of a locking slide 60 which is movably guided on the wing 23 parallel to its plane and a locking projection 61 fixed to the fixed frame 22.

Der Riegelschieber 60 trägt dabei einen Stellansatz 62, der wenigstens zeitweilig in die Bewegungsbahn eines Steuernockens 63 hineinragt, welcher am Steuerarm 56 des Parallelogramm-Lenkhebelgetriebes sitzt.The locking slide 60 carries an actuating projection 62 which at least temporarily protrudes into the movement path of a control cam 63 which is seated on the control arm 56 of the parallelogram steering lever mechanism.

Der Stellansatz 62 am Riegelschieber 60 und der Steuernocken 63 am Steuerarm 56 sind relativ zueinander so angeordnet, daß bei der Schließbewegungs-Annäherung des Flügels 23 an den feststehenden Rahmen 22 der Stellansatz 62 auf den Steuernocken 63 bereits auftrifft, bevor der Flügel 23 seine Schließlage einnimmt.The actuating projection 62 on the locking slide 60 and the control cam 63 on the control arm 56 are arranged relative to one another such that when the wing 23 approaches the closing movement of the fixed frame 22, the actuating projection 62 already hits the control cam 63 before the wing 23 assumes its closed position .

Über die, beispielsweise als Schrägfläche ausgeführte, Andrückkurve des Steuernockens 63 wird dann im Verlauf der weiteren Schließbewegung des Flügels 23 der Stellansatz 62 und über diesen wiederum der Riegelschieber 60 in Richtung auf den Riegelansatz 61 zu verschoben, bis er diesen riegelnd hintergreift.Via the pressure curve of the control cam 63, which is designed, for example, as an inclined surface, the actuating projection 62 is then moved in the course of the further closing movement of the wing 23 and, via this, the locking slide 60 is moved in the direction of the locking projection 61 until it engages behind it in a locking manner.

Wie schon in Fig. 1 schematisch angedeutet ist, so ergibt sich auch aus den Fig. 2 bis 5 der Zeichnung, daß oberhalb des beispielsweise als Eckgelenk bzw. Drehkipp-Ecklager 26 wirksamen Gelenkbeschlags dem aufrechten Holm 22b des feststehenden Rahmens 22 und dem aufrechten Holm 23b des Flügels 23 das Zugglied 42 angeordnet ist, und zwar derart, daß es im wesentlichen in Richtung der aufrechten Achse 24-24 seine Wirkung entfalten kann.As already indicated schematically in Fig. 1, it also follows from FIGS. 2 to 5 of the drawing that above the joint fitting effective, for example, as a corner joint or tilt-turn corner bearing 26, the upright spar 22b of the fixed frame 22 and the upright spar 23b of the wing 23, the tension member 42 is arranged in such a way that it can develop its effect essentially in the direction of the upright axis 24-24.

Das Zugglied 42 liegt dabei im Bereich der Falzluft zwischen feststehendem Rahmen 22 und Flügel 23, damit es sich bei Schließlage des Flügels 23 völlig verdeckt zwischen den Falzumfangsflächen 22c und 23c befindet, wie das deutlich aus Fig. 2 erkennbar ist. Das Zugglied 42 kann von einem Zugstab aus starrem Material gebildet werden. Vorzugsweise wird als Zugglied 42 jedoch ein Seil oder Kabel, insbesondere aus Stahldrähten, verwendet oder aber ein Bowdenzug eingesetzt.The tension member 42 lies in the area of the rebate air between the fixed frame 22 and the wing 23, so that when the wing 23 is in the closed position it is completely concealed between the rebate peripheral surfaces 22c and 23c, as can be clearly seen in FIG. 2. The tension member 42 can be formed by a tension rod made of rigid material. Preferably, however, a cable or cable, in particular made of steel wires, is used as the tension member 42 or a Bowden cable is used.

Wichtig ist dabei in jedem Falle, daß das obere Ende des Zuggliedes 42 an der Falzumfangsfläche 22c des feststehenden Rahmens 22 in dem ortsfesten Widerlager 43 aufgehängt ist, während sein unteres Ende an dem Widerlager 44 angreift, das der Falzumfangsfläche 23c des Flügels 23 zugeordnet ist.It is important in any case that the upper end of the tension member 42 is suspended from the peripheral circumferential surface 22c of the fixed frame 22 in the fixed abutment 43, while its lower end engages the abutment 44 which is associated with the circumferential fold surface 23c of the wing 23.

Bevorzugt wird das Widerlager 44 am Flügel 23 mit möglichst geringem Abstand oberhalb des unteren Gelenkbeschlages bzw. Eckgelenks 26 angeordnet, wobei das Zugglied 42 zwischen den beiden Widerlagern 43 und 44 ständig unter straffer Zugspannung gehalten ist, damit von ihm die Vertikalkomponente der Gewichtskraft bzw. Last des Flügels 23 aufgenommen wird, ohne daß diese in Richtung der Achse 24-24 auf den Gelenkbeschlag 26 einwirken kann.The abutment 44 is preferably arranged on the wing 23 with the smallest possible distance above the lower joint fitting or corner joint 26, the tension member 42 between the two abutments 43 and 44 being kept constantly under tight tension, so that the vertical component of the weight or load is held by it of the wing 23 is received without this can act on the hinge fitting 26 in the direction of the axis 24-24.

Es wird hierdurch erreicht, daß der Gelenkbeschlag 26 nur noch solche Kräfte aufzunehmen hat, die aus der Horizontalkomponente der Gewichtskraft bzw. Last des Flügels 23 resultieren und normal zur Achse 24-24 gerichtet sind, wie das in den Fig. 2 bis 4 jeweils durch den Pfeil 63 angedeutet ist.It is hereby achieved that the hinge fitting 26 has to absorb only those forces which result from the horizontal component of the weight or load of the wing 23 and are directed normal to the axis 24-24, as in FIGS. 2 to 4 in each case the arrow 63 is indicated.

Im einfachsten Falle können die Widerlager 43 und 44 für das Zugglied 42 aus mit Querbohrungen oder Gabelschlitzen ausgestatteten Bolzen bestehen, die an den Falzumfangsflächen 22c und 23c von feststehendem Rahmen 22 und Flügel 23 befestigt werden. In die Querbohrungen bzw. Gabelschlitze derselben wird dann das Zugglied 42 eingeführt, wobei es in seiner wirksamen Länge auf den Abstand zwischen den beiden Widerlagern 43 und 44 zweckentsprechend exakt abgestimmt und/oder einstellbar ist. Letzteres kann dadurch ermöglicht werden, daß das Zugglied 42 mit Stützanschlägen 64 und 65 ausgestattet wird, von denen wenigstens einer, beispielsweise der Stützanschlag 65, eine Klemmuffe bildet, die sich in Längsrichtung des Zuggliedes 42 verschieben und in jeder Verschiebelage auf diesem festlegen läßt. Zumindest einer der Stützanschläge 64 und 65 des Zuggliedes 42 könnte aber auch durch Benutzung geeigneter Schraubglieder in seiner wirksamen Länge stufenlos verstellbar ausgebildet werden.In the simplest case, the abutments 43 and 44 for the tension member 42 can consist of bolts equipped with transverse bores or fork slots, which are fastened to the fold peripheral surfaces 22c and 23c by a fixed frame 22 and wing 23. The tension member 42 is then inserted into the transverse bores or fork slots thereof, the effective length of which can be appropriately matched and / or adjusted appropriately for the distance between the two abutments 43 and 44. The latter can be made possible in that the tension member 42 is equipped with support stops 64 and 65, of which at least one, for example the support stop 65, forms a clamping sleeve which can be displaced in the longitudinal direction of the tension member 42 and can be fixed on the latter in any displacement position. At least one of the support stops 64 and 65 of the tension member 42 could also be made infinitely adjustable in its effective length by using suitable screw members.

Es wäre aber auch nach den Fig. 1 bis 5 möglich, zwischen eines der Widerlager 43 und 44 sowie das Zugglied 42 Federelemente einzuschalten, deren Vorspannkraft sich bedarfsweise verändern und damit - innerhalb gewisser Grenzen - auf das jeweilige Gewicht des Flügels 23 abstimmen bzw. einjustieren läßt.However, it would also be possible according to FIGS. 1 to 5 to switch on spring elements between one of the abutments 43 and 44 and the tension member 42, the pretensioning force of which change as necessary and thus - within certain limits - adjust or adjust to the respective weight of the wing 23 leaves.

Den Fig. 2 bis 5 der Zeichnung kann entnommen werden, daß das Zugglied 42 bei verschiedenen Relativlagen des Flügels 23 zum feststehenden Rahmen 22 auch in unterschiedliche Wirklagen gelangt, dabei aber in jedem Falle die ihm zugedachte Funktion sicher erfüllt.2 to 5 of the drawing it can be seen that the tension member 42 also comes into different operative positions at different relative positions of the wing 23 to the fixed frame 22, but in this case certainly fulfills the function intended for it.

Die aus jeder Bewegung des Flügels 23 zum feststehenden Rahmen 22 resultierende Lagenänderung des Zuggliedes 42 zwischen seinen Widerlagern 43 und 44 läßt sich problemlos beherrschen. Wenn das Zugglied 42 aus einem starren Material besteht, dann braucht es zu diesem Zweck lediglich kardanische bzw. kugelige Verbindungen mit den Widerlagern 43 und 44 aufzuweisen. Ist jedoch das Zugglied 42 biegeverformbar ausgelegt (Seil, Kabel, Bowdenzug), dann kann es den Verlagerungsbewegungen des Flügels 23 relativ zum feststehenden Rahmen 22 ohne weiteres folgen.The change in position of the tension member 42 between its abutments 43 resulting from each movement of the wing 23 to the fixed frame 22 and 44 can be easily mastered. If the tension member 42 consists of a rigid material, then it only needs to have gimbal or spherical connections to the abutments 43 and 44 for this purpose. However, if the tension member 42 is designed to be bendable (rope, cable, Bowden cable), then it can easily follow the displacement movements of the wing 23 relative to the fixed frame 22.

Als aus starrem Material gefertigtes Zugglied 42 kann ein Zugstab verwendet werden, dessen Enden durch kardanische bzw. kugelige Verbindungsglieder am feststehenden Rahmen 22 und am Flügel 23 angreifen, und zwar an den hierzu passend ausgelegten Widerlagern 43 und 44.As a tension member 42 made of rigid material, a tension rod can be used, the ends of which engage by means of cardanic or spherical connecting links on the fixed frame 22 and on the wing 23, specifically on the abutments 43 and 44 suitably designed for this purpose.

Als Zugglied 42 kann aber auch mindestens ein tordierbares Flachband-Material, insbesondere Federstahlband, in Benutzung genommen werden.However, at least one twistable flat strip material, in particular spring steel strip, can also be used as the tension member 42.

Ein solches Flachbandmaterial hat nämlich den Vorteil, daß es bei relativ geringer Dicke eine verhältnismäßig große Breite aufweisen kann, wobei diese Breite im Grunde genommen durch die Breite der Falzumfangsflächen des feststehenden Rahmens 22 und des Flügels 23 begrenzt ist. Bewährt hat es sich besonders, wenn das Flachband-Material bzw. der Federstahlstreifen mit einer Breite verwendet wird, die dem Sechzehnfachen bis Zwanzigfachen seiner Dicke entspricht.Such a ribbon material has the advantage that it can have a relatively large width with a relatively small thickness, which width is basically limited by the width of the folded peripheral surfaces of the fixed frame 22 and the wing 23. It has proven particularly useful if the flat strip material or the spring steel strip is used with a width which corresponds to sixteen to twenty times its thickness.

Als vorteilhaft hat es sich im letzteren Falle auch herausgestellt, wenn das Flachband-Material des Zuggliedes 42 bei in Schließlage am feststehenden Rahmen 22 anliegendem Flügel 23 über seine ganze Länge hinweg mit seiner Breitseite wenigstens annähernd parallel zu den Falzumfangsflächen bzw. quer zu den Hauptebenen von feststehendem Rahmen 22 und Flügel 23 ausgerichtet ist, so daß es bei Schließlage und beim Kippöffnen des Flügels 23 nur wenig Einbauraum benötigt, während es beim Drehöffnen des Flügels 23 um seine aufrechte Achse 24-24 - über einen Winkel von etwa 90 Grad hinweg - auf Torsion beansprucht wird.In the latter case, it has also proven to be advantageous if the flat band material of the tension member 42 with the wing 23 lying in the closed position on the fixed frame 22 over its entire length with its broad side at least approximately parallel to the fold peripheral surfaces or transversely to the main planes of fixed frame 22 and wing 23 is aligned so that it requires little installation space in the closed position and when tilting the wing 23, while when turning the wing 23 about its upright axis 24-24 - over an angle of about 90 degrees - on Torsion is claimed.

Auch wenn das Zugglied 42 aus einem starren Zugstab oder aber einem tordierbaren Flachband-Material besteht, ist es möglich, seine wirksame Länge zwischen den Widerlagern 43 und 44, beispielsweise mit Hilfe von Schraubgliedern, stufenlos verstellbar auszubilden.Even if the tension member 42 consists of a rigid tension rod or a twistable flat strip material, it is possible to design its effective length between the abutments 43 and 44 to be infinitely adjustable, for example with the aid of screw members.

In Fig.6 der Zeichnung ist ein Fenster bzw. eine Tür 121 zu sehen, das bzw. die einen feststehenden Rahmen 122 und einen Flügel 123 umfaßt. Der Flügel 123 ist dabei im feststehenden Rahmen 122 wahlweise um eine seitlich lotrechte Achse 124-124 in eine Drehöffnungsstellung oder um eine untere horizontale Achse 125- 125 in eine Kippöffnungsstellung beweglich angeordnet.In FIG. 6 of the drawing, a window or a door 121 can be seen which comprises a fixed frame 122 and a wing 123. The wing 123 is arranged in the fixed frame 122 either movably about a laterally perpendicular axis 124-124 in a rotational opening position or about a lower horizontal axis 125-125 in a tilt opening position.

Der Flügel 123 wird zu diesem Zweck am feststehenden Rahmen 122 im Schnittpunkt der beiden Gelenkachsen 124-124 und 125-125 durch ein Eckgelenk bzw. ein Drehkipp-Ecklager 126 abgestützt. Darüberhinaus befinden sich oben zwischen dem Flügel 123 und dem feststehenden Rahmen ein Drehgelenk 127 und eine Ausstellvorrichtung 128, während an der verschlußseitigen unteren Ecke von Flügel 123 und feststehendem Rahmen 122 eine Kippverriegelung 129 vorgesehen ist.For this purpose, the wing 123 is supported on the fixed frame 122 at the intersection of the two hinge axes 124-124 and 125-125 by a corner joint or a tilt and turn corner bearing 126. In addition, a swivel joint 127 and an opening device 128 are located at the top between the wing 123 and the fixed frame, while a tilt lock 129 is provided on the lower corner of the wing 123 and the fixed frame 122 on the lock side.

Ein über eine Bedienungshandhabe 130 verstellbarer Treibstangenbeschlag 131 ist im Flügel 123 so untergebracht, daß damit einerseits eine Verriegelung und Entriegelung des in der Schließlage befindlichen Flügels 123 am feststehenden Rahmen 122 über Riegelnocken 132 und zugehörige Riegeleingriffe 133 bewirkt werden kann. Andererseits ist der Treibstangenbeschlag 131 jedoch auch noch so ausgelegt, daß sich mit seiner Hilfe sowohl eine Kupplung 134, 135 zwischen dem Flügel 123 und der Ausstellvorrichtung 128 als auch die Kippverriegelung 129 ein- und ausrücken läßt. Sowohl in der Verschluß-Schaltstellung als auch in Drehöffnungs-Schaltstellung des Treibstangenbeschlages 131 befindet sich die Kupplung 134, 135 zwischen dem Flügel 123 und der Ausstellvorrichtung 128 in ihrer Einrückstellung. In der Kippöffnungs-Schaltstellung des Treibstangenbeschlages 131 ist hingegen die Kupplung 134, 135 ausgerückt. Die Kippverriegelung 129 befindet sich in ausgerückter Stellung, wenn der Treibstangenbeschlag 131 seine Verschluß-Schaltstellung und seine DrehöffnungsSchaltstellung einnimmt, während sie in der Kippöffnungs-Schaltstellung eingerückt ist.A drive rod fitting 131, which can be adjusted via an operating handle 130, is accommodated in the wing 123 in such a way that, on the one hand, locking and unlocking of the wing 123 in the closed position on the fixed frame 122 can be effected by means of locking cams 132 and associated locking engagements 133. On the other hand, the connecting rod fitting 131 is also designed so that it can be used to engage and disengage both a coupling 134, 135 between the wing 123 and the opening device 128 and the tilt lock 129. Both in the closed switching position and in the rotary opening switching position of the connecting rod fitting 131, the coupling 134, 135 is located between the wing 123 and the opening device 128 in its engagement position. In the tilt opening position of the connecting rod fitting 131, however, the clutch 134, 135 is disengaged. The Tilt lock 129 is in the disengaged position when the espagnolette fitting 131 assumes its closed switch position and its rotary open switch position while it is engaged in the tilt open switch position.

Die Ausstellvorrichtung 128 ist als sogenannte tragende Ausstellvorrichtung - nach dem Ellipsenlenker-Prinzip - ausgebildet, d. h., sie ist geeignet, in der Verschluß- und in der Drehöffnungs-Schaltstellung des Treibstangenbeschlages 131 das Gewicht des Flügel 123 zu halten sowie in das obere, blendrahmenseitige Drehgelenk 127 einzuleiten. Zu diesem Zweck weist die Ausstellvorrichtung 128 einen im rahmenseitigen Drehgelenk 127 schwenkbar gehaltenen Ausstellaram 136 auf, der an seinem anderen Ende über einen Bundbolzen 137 sowohl schwenkbeweglich als auch längsschiebbar in eine Gleitführung 138 eingreift, die sich im wesentlichen parallel zur Oberkante des Flügels 123 erstreckt. Außerdem hat die Ausstellvorrichtung 128 einen Zusatzarm 139, welcher einerseits über einen Gelenkzapfen 140 ausschließlich schwenkbar am Flügel 123 angelenkt ist, andererseits aber, ebenfalls ausschließlich schwenkbar, über einen Gelenkzapfen 141 mit dem Ausstellarm 136 in Verbindung steht.The opening device 128 is designed as a so-called supporting opening device - according to the elliptical link principle - i. that is, it is suitable for holding the weight of the wing 123 in the closed and in the rotary opening switch position of the connecting rod fitting 131 and for introducing it into the upper, frame-side pivot joint 127. For this purpose, the opening device 128 has an opening arm 136 which is pivotally held in the frame-side swivel joint 127 and which at its other end engages in a sliding guide 138, which can pivot and also slide longitudinally, via a collar bolt 137, which extends essentially parallel to the upper edge of the wing 123. In addition, the opening device 128 has an additional arm 139, which on the one hand is articulated only pivotably on the wing 123 via a pivot pin 140, but on the other hand, also exclusively pivotable, is connected to the opening arm 136 via a pivot pin 141.

Die Ausstellvorrichtung 128 ist dabei in ihrer Kinematik so ausgelegt, daß sie beim Kippöffnen des Flügels 123 den oberen Flügelholm in jeder möglichen Kipplage parallel zum oberen Holm des feststehenden Rahmens 122 ausgerichtet hält. Die Gelenkbeschläge 126 und 127 sind völlig verdeckt im luftraum zwischen den Fälzen von Flügel 123 und feststehendem Rahmen 122 untergebracht. Sowohl zur Bildung des Eckgelenkes bzw. Drehkipp-Ecklagers 126 als auch des Drehgelenkes 127 können dabei Gelenkbeschläge in Benutzung genommen werden, die auf dem sogenannten Kreuzscheren-Prinzip basieren, wie es entweder der US-PS 1 864 164 oder aber der US-PS 3 722 142 als bekannt entnommen werden kann.The opening device 128 is designed in its kinematics so that when the wing 123 is tilted open it keeps the upper wing spar aligned parallel to the upper spar of the fixed frame 122 in any possible tilting position. The hinge fittings 126 and 127 are completely concealed in the air space between the folds of sash 123 and fixed frame 122. Joint fittings based on the so-called cross-scissors principle, such as that described in either US Pat. No. 1,864,164 or US Pat. No. 3, can be used to form the corner joint or tilt-swivel corner bearing 126 and the swivel joint 127 722 142 can be seen as known.

Zur Entlastung des Eckgelenkes bzw. Drehkipp-Ecklagers 126 von der Vertikalkomponente der Gewichtskraft bzw. last des Flügels 123 wird beim Fenster bzw. bei der Tür 121 ein Zugglied 142 in Benutzung genommen. Es ist dabei in Richtung der vertikalen Gelenkachse 124-124 wirksam und zu diesem Zweck mit seinem oberen Ende an einem ortsfesten Widerlager 143 des feststehenden Rahmens 122 aufgehängt, während sein unteres Ende an einem Widerlager 144 angreift, daß am Flügel 123 sitzt. Das Zugglied 142 mit seinen Widerlagern 143 und 144 ist zwar insgesamt oberhalb, jedoch noch in nächster Nähe des unteren Eckgelenkes bzw. Drehkipp-Ecklagers 126 zwischen dem Flügel 123 und dem feststehenden Rahmen 122 eingebaut, wie das deutlich der Fig. 6 entnommen werden kann.To relieve the corner joint or turn-tilt corner bearing 126 from the vertical component of the weight or load of the wing 123, a tension member 142 is used in the window or in the door 121. It is there effective in the direction of the vertical hinge axis 124-124 and for this purpose hung with its upper end on a fixed abutment 143 of the fixed frame 122, while its lower end engages an abutment 144 that sits on the wing 123. The tension member 142 with its abutments 143 and 144 is installed above, but still in the immediate vicinity of the lower corner joint or tilt-turn corner bearing 126 between the wing 123 and the fixed frame 122, as can be clearly seen in FIG. 6.

Anordnung, Ausbildung und Wirkungsweise des Zuggliedes 142 nach Fig. 6 ergeben sich aus den Fig. 7, 8 und 9 der Zeichnung, die ein Fenster oder eine Tür 121 zeigen, bei welchem bzw. welcher der Flügel 123 am feststehenden Rahmen 122 über völlig verdeckt zwischen den horizontalen Fälzen liegende Gelenkbeschläge, nämlich gemäß Fig. 6 das Eckgelenk 126 und das Drehgelenk 127, aufgehängt ist.The arrangement, design and mode of operation of the tension member 142 according to FIG. 6 result from FIGS. 7, 8 and 9 of the drawing, which show a window or a door 121, in which or which the wing 123 on the fixed frame 122 is completely covered hinge fittings lying between the horizontal folds, namely the corner joint 126 and the swivel joint 127 according to FIG. 6, is suspended.

Bei den Fig. 7 bis 9 der Zeichnung ist nur das Eckgelenk bzw. Drehkipp-Ecklager 126 zu sehen, weil es in Verbindung mit dem Zugglied 142 allein um die besondere Ausgestaltung des flügelseitigen Gelenkteils 145 dieses Eckgelenkes bzw. Drehkipp-Ecklager 126 geht.7 to 9 of the drawing, only the corner joint or tilt and turn corner bearing 126 can be seen, because in connection with the tension member 142 it is all about the special design of the wing-side joint part 145 of this corner joint or tilt and turn corner bearing 126.

Es ist aus Fig. 7 ersichtlich, daß das flügelseitige Gelenkteil 145 die Form eines Winkelstücks mit zwei rechtwinklig zueinander gerichteten Schenkeln 146 und 147 aufweist. Dabei wird das flügelseitige Gelenkteil 145 mit seinen Winkelschenkeln 146 und 147 in eine abgestufte Profilnut 148 der Falzumfangsfläche 149 des Flügels 133 so eingesetzt, daß seine Außenseite bündig mit der Falzumfangsfläche 149 abschließt.It can be seen from FIG. 7 that the wing-side joint part 145 has the shape of an angle piece with two legs 146 and 147 directed at right angles to one another. The wing-side hinge part 145 is inserted with its angle legs 146 and 147 into a stepped profile groove 148 of the rebate peripheral surface 149 of the wing 133 so that its outside is flush with the rebate peripheral surface 149.

Der aufrechte Winkelschenkel 147 des Flügelbeschlagteils 145 weist einen über die Falzumfangsfläche des aufrechten Flügelholmes auslegerartig vorspringenden Hakenansatz 150 mit einem an seinem unteren Ende seitswärts offenen Winkelschlitz 151 auf. Dabei wird der Hakenansatz 150 von zwei zur Flügelebene parallelen und durch einen Abstandsspalt 150c voneinander getrennten Hakenteilen 150a und 150b gebildet, welche deutlich in Fig. 8 zu sehen sind.The upright angle leg 147 of the wing fitting part 145 has a hook projection 150 projecting over the folded peripheral surface of the upright wing spar with an angle slot 151 which is open at the side at its lower end. The hook shoulder 150 is separated from one another by two parallel to the wing plane and by a spacing gap 150c separate hook parts 150a and 150b formed, which can be clearly seen in Fig. 8.

Das Zugglied 142 ist an seinem unteren Ende mit einer blockförmigen Verdickung 152, vorzugsweise in Form eines Zylinder- oder Kugelkörpers, versehen, in der bzw. dem das Zugglied 142 entweder fest oder aber lösbar verankert ist. Die feste Verankerung kann beispielsweise dadurch geschehen, daß die blockförmige Verdickung 152 mit dem Zugglied 142 vergossen oder verpreßt wird. Zur lösbaren Verbindung kann hingegen das Zugglied 142 in eine diametrale Bohrung der blockförmigen Verdickung 152 eingesteckt und darin anschließend durch Anziehen einer Klemmschraube festgelegt werden.The tension member 142 is provided at its lower end with a block-shaped thickening 152, preferably in the form of a cylindrical or spherical body, in which the tension member 142 is either firmly or releasably anchored. The firm anchoring can take place, for example, in that the block-shaped thickening 152 is cast or pressed with the tension member 142. For the releasable connection, however, the tension member 142 can be inserted into a diametrical bore of the block-shaped thickening 152 and subsequently fixed therein by tightening a clamping screw.

Durch die seitwärts gerichtete Offnung des Winkelschlitzes 151 läßt sich das Zugglied 142 mit seiner blockförmigen Verdickung 152 mit dem Hakenansatz 150 in Kupplungseingriff bringen, in dem zugleich das Zugglied 142 von der Seite her in den Abstandsspalt 150c zwischen beiden Hakenteilen 150a und 150b eingeführt wird (Fig. 8). Dabei legt sich die blockförmige Verdickung 152 passend im oberen Endbereich des Winkelschlitzes 151 an die Flanken der Hakenteile 150a und 150b des Hakenansatzes 150 an, wie das deutlich der Fig. 7 zu entnehmen ist. Der Hakenansatz 150 bildet also das flügelseitige Widerlager 144 gemäß Fig. 6.Due to the sideways opening of the angle slot 151, the tension member 142 with its block-shaped thickening 152 can be brought into coupling engagement with the hook extension 150 by simultaneously inserting the tension member 142 from the side into the spacing gap 150c between the two hook parts 150a and 150b (FIG . 8th). The block-shaped thickening 152 fits snugly in the upper end region of the angle slot 151 against the flanks of the hook parts 150a and 150b of the hook attachment 150, as can be clearly seen in FIG. 7. The hook extension 150 thus forms the wing-side abutment 144 according to FIG. 6.

Damit das Zugglied 142 mit dem Flügelbeschlagteil 145 zwar leicht gekuppelt, jedoch nicht ohne eine bestimmte Zusatzmanipulation wieder entkuppelt werden kann, ist dem Winkelschlitz 151 im Hakenansatz 150 im Bereich seiner seitwärts gerichteten Öffnung bzw. unmittelbar oberhalb derselben ein nasenartiger Verengungsvorsprung 153 zugeordnet. Dieser Verengungsvorsprung 153 wird dabei vorzugsweise von einer Federzunge 154 oder einem Rastschnäpper gebildet, welche bzw. welcher am oder im Winkelschenkel 147 des Flügelbeschlagteils 145 vorgesehen ist, wie das die Fig. 7 und 8 der Zeichnung deutlich zeigen. Beim Einrücken der blockförmigen Verdickung 152 des Zuggliedes 142 in den Winkelschlitz 151 weicht die Federzunge 154 bzw. der Rastschnäpper elastisch aus und gibt dadurch den oberen Endbereich des Hakenschlitzes 151 für den Eintritt der blockförmigen Verdickung 152 frei. Ist diese dann in den Hakenansatz 150 eingerückt, dann stellt sich die Federzunge 154 bzw. der Rastschnäpper selbsttätig in ihre bzw. seine Sperrlage zurück und untergreift die blockförmige Verdickung 152 unter gleichzeitiger Verengung des Querschnitts im Hakenschlitz 151. Nur durch manuelles Zurückdrücken der Federzunge bzw. des Rastschnäppers läßt sich nunmehr die blockförmige Verdickung 152 des Zuggliedes 142 zum Zwecke des Aushängens wieder freigeben.So that the tension member 142 can be easily coupled to the wing fitting part 145, but not uncoupled again without a certain additional manipulation, the angled slot 151 in the hook attachment 150 is assigned a nose-like narrowing projection 153 in the region of its sideways opening or immediately above it. This narrowing projection 153 is preferably formed by a spring tongue 154 or a snap catch, which or which is provided on or in the angle leg 147 of the wing fitting part 145, as clearly shown in FIGS. 7 and 8 of the drawing. When the block-shaped thickening 152 of the tension member 142 is inserted into the angled slot 151, the spring tongue 154 or the snap catch elastically deflects and thereby gives the upper end region of the hook slot 151 free for the entry of the block-shaped thickening 152. If this is then inserted into the hook extension 150, the spring tongue 154 or the snap catch automatically returns to its or its blocking position and engages under the block-shaped thickening 152 while simultaneously narrowing the cross section in the hook slot 151. Only by manually pushing back the spring tongue or of the catch, the block-shaped thickening 152 of the tension member 142 can now be released again for the purpose of unhooking.

Beim Ausführungsbeispiel nach Fig. 9 befindet sich der Verengungsvorsprung 153 am freien Ende des einen Hebelarms eines zweiarmigen Hebels 155, welcher um eine Achse 156 schwenkbeweglich im aufrechten Winkelschenkel 147 des Flügelbeschlagteils 145 lagert. Das freie Ende des anderen Hebelarms dieses zweiarmigen Hebels 155 trägt einen Stell- bzw. Anlaufnocken 157, welcher in den Bereich des oberen Endes des Winkelschlitzes 151 eingeschwenkt ist, sofern sich der Verengungsvorsprung 153 außerhalb des Winkelschlitzes 151 befindet. Wird nun das Zugglied 142 mit seiner blockförmigen Verdickung 152 in den Winkelschlitz 151 des Hakenansatzes 150 eingeführt, dann trifft die blockförmige Verdickung 152 oben gegen den Stell- bzw. Anlaufnocken 157 und verdrängt diesen aus dem Bereich des Winkelschlitzes 151 am Hakenansatz 150. Hierdurch gelangt dann der Verengungsvorsprung 153 unterhalb der blockförmigen Verdickung 152 in den Winkelschlitz 151 und verengt dessen Querschnitt so, daß die Verdickung 152 hieraus nicht mehr ohne weiteres entweichen kann. Erwähnt sei hier noch, daß der zweiarmige Hebel 155 so in das Flügelbeschlagteil 145 eingesetzt ist, daß er sich im Bereich des Abstandsspaltes 150c zwischen den beiden Hakenteilen 150a und 150b bewegen kann.In the exemplary embodiment according to FIG. 9, the narrowing projection 153 is located at the free end of the one lever arm of a two-armed lever 155, which is pivotably mounted about an axis 156 in the upright angle leg 147 of the wing fitting part 145. The free end of the other lever arm of this two-armed lever 155 carries an actuating cam 157, which is pivoted into the area of the upper end of the angle slot 151, provided that the constriction projection 153 is outside the angle slot 151. If the tension member 142 with its block-shaped thickening 152 is now inserted into the angle slot 151 of the hook extension 150, then the block-shaped thickening 152 hits the actuating or starting cam 157 at the top and displaces it from the area of the angle slot 151 on the hook extension 150. This then results the constriction protrusion 153 below the block-shaped thickening 152 in the angular slot 151 and narrows its cross-section so that the thickening 152 can no longer escape therefrom easily. It should also be mentioned here that the two-armed lever 155 is inserted into the wing fitting part 145 in such a way that it can move in the region of the spacing gap 150c between the two hook parts 150a and 150b.

Claims (12)

1. A window or door (21) having a turn-tilt moving member (panel) (23) mounted by pivot devices (26, 27) on the fixed frame (22) on or rear a vertical boundary edge, characterised by a pull member (42) which is secured to the panel (23) near the pivot devices (26, 27), is fixed to the fixed frame (22) against the weight or load of the panel (23) and is fitted between the panel (23) and the frame (22) above but near the bottom corner pivot (26).
2. A window or door according to claim 1, characterised in that the pull member (42) is suspended (43) at its top end on the fixed frame (22) and is connected (44) at its bottom end to the panel (23).
3. A window or door according to claim 1 and/or 2, characterised in that the pull member (42) is continuously in tension.
4. A window or door according to any of claims 1 to 3, characterised in that the pull member (42) is a rope or a cable or a Bowden cable.
5. A window or door according to any of claims 1 to 4, characterised in that the pull member (42) is concealed in the air gap between the rebate (23a) in the panel (23) and the rebate (22a) in the frame (22).
6. A window or door according to any one of claims 1 to 5, characterised in that the pull member (42) is longitudinally adjustable.
7. A window or door according to any of claims 1 to 3 and 5 and 6, characterised in that the pull member (42) is in the form of a rigid pull rod having cardan or ball connections to the bearings (43, 44).
8. A window or door according to any one of claims 1 to 7, characterized in that the pull member (42) experiences an opposing force relatively to the bearing (43) disposed on the fixed frame (22), the opposing force being, for example, a counterweight which balances the panel weight or a correspondingly biased spring.
9. A window or door according to any of claims 1 to 5 and 8, characterised in that on the fixed frame (22) the pull member (42) extends around the stationary bearing (43), for example, by means of a roller, and is tensioned by the opposing force, for example, the counterweight.
10. A window or door according to any of claims 1 to 3 and 5 and 6, characterised in that the pull member (42) is made of at least one twistable flat strip material, more particularly spring steel strip and, with advantage, has a width corresponding to a multiple of its thickness, for example, to approximately 16 to 20 times such thickness, it being convenient if, when the panel (23) is in engagement with the fixed frame (22) in the closed position, the flat strip material of the pull member (42) extends over its whole length with its wide side at least substantially parallel to the rebate peripheral surfaces or transversely to the main planes of the fixed frame (22) and of the panel (23).
11. A window or door (121) according to any of claims 1 to 6 and 8 and 9, characterised in that the panel-associated pivot part (145) has a hook projection (150) which projects cantilever-fashion beyond the boundary surface (rebate peripheral surface 149) of the vertical panel member and which is formed with an angular slot (151) open laterally at its bottom end, the hook projection (150) has two hook parts (150a and 150b) which are parallel to the panel ylane and separated frown one another by a gap (150c), and the pull member (142) has at its bottom end a block-like thickening (152) whose cross-sectionaldimension is adapted to the width of the angular slot (151), the gap (150c) being adapted to receive the pull member (142), the block-like thickening (152) preferably being in the form of a cylindrical or spherical member in which the pull member (42) is fixedly or releasably secured, while the panel-associated pivot part (145) is, conveniently, an angle member engageable by way of its two angle arms (146 and 147) near the panel corner in a stepped groove (148) in the rebate peripheral surface (149) of the panel (133).
12. A window or door according to claim 1, characterised in that a beak-like restricting projection (153) is associated with the hook projection slot (151) near or immediately above the laterally directed aperture, the latter projection (153) being either in the form of a resilient tongue (154) or of a spring latch or being disposed at the free end of a first arm of a two-armed lever (155) mounted for pivoting around a pivot (156) in the panel-associated pivot part (145) and carrying at the free end of its other arm an actuating or striker cam (157) adapted to be pivoted into the angular slot (151) alternately with the projection (153).
EP90100180A 1989-01-24 1990-01-05 Window, door or the like Revoked EP0379866B1 (en)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
DE19893901944 DE3901944A1 (en) 1989-01-24 1989-01-24 Window or door
DE3901944 1989-01-24
DE8903678U 1989-03-23
DE8903678U DE8903678U1 (en) 1989-03-23 1989-03-23 Window or door
DE19893920360 DE3920360C2 (en) 1989-06-22 1989-06-22 Window or door
DE3920360 1989-06-22

Publications (2)

Publication Number Publication Date
EP0379866A1 EP0379866A1 (en) 1990-08-01
EP0379866B1 true EP0379866B1 (en) 1992-03-11

Family

ID=27198964

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90100180A Revoked EP0379866B1 (en) 1989-01-24 1990-01-05 Window, door or the like

Country Status (9)

Country Link
US (1) US5009034A (en)
EP (1) EP0379866B1 (en)
AT (1) ATE73522T1 (en)
CA (1) CA2008331C (en)
DE (1) DE59000060D1 (en)
DK (1) DK0379866T3 (en)
ES (1) ES2031011T3 (en)
FI (1) FI92516C (en)
NO (1) NO176933C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1837472A1 (en) 2006-03-25 2007-09-26 Roto Frank Ag Window, door or similar with a load alleviation device
DE202014007902U1 (en) 2014-10-06 2014-10-28 Siegenia-Aubi Kg Angled fitting

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3906794A1 (en) * 1989-03-03 1990-09-06 Bilstein August Gmbh Co Kg WINDOW WITH A ROTATING, IN PARTICULAR ROTATING WING
DE20002467U1 (en) * 2000-02-11 2000-05-04 Gretsch Unitas Gmbh Tilt & Turn hardware
DE20012351U1 (en) 2000-07-14 2001-11-15 Siegenia Frank Kg Window or door with relief device
IL151244A (en) * 2002-08-14 2006-10-31 Chagim Nechalim Ind Ltd Panel for modular construction
PT1700284E (en) * 2003-12-31 2011-11-28 Schueco Int Kg Window and window handle
DE202008011516U1 (en) * 2008-08-29 2009-12-31 Siegenia-Aubi Kg Window or door with a fitting
US20120124774A1 (en) * 2009-07-31 2012-05-24 Oehman Hans Device At A Control Mechanism For A Window Fixture At A Turntable Window
DE202013009352U1 (en) * 2013-10-23 2013-11-12 Siegenia-Aubi Kg Window or door with a fitting
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Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE26176C (en) * M. FLÜRSCHEIM Eisenwerke Gaggenau in Gaggenau, Baden Door closers
DE588193C (en) * 1933-11-24 Fritz Belz Door closer
US1328168A (en) * 1917-04-19 1920-01-13 Arthur W Kroon Gate
DE329280C (en) * 1919-09-17 1920-11-19 Oskar Schulz Automatic door closer
US1864164A (en) * 1929-07-05 1932-06-21 American Cabinet Hardware Corp Hinge
GB496829A (en) * 1937-09-02 1938-12-07 Wallace Scott Improvements in and relating to hinges and the like
CH218319A (en) * 1941-06-14 1941-12-15 Fahrner Fritz Fish tape on doors, windows and other devices having a pivoting sash.
FR1117003A (en) * 1954-05-08 1956-05-15 Hardware for doors, gates, windows, etc.
DE1913993A1 (en) * 1969-03-19 1970-10-01 Siemens Ag Electrical welding of wires and balls
US3722142A (en) * 1971-06-16 1973-03-27 Anderberg A Mfg Co Mounting bracket for overhead window
DE2508174A1 (en) * 1975-02-26 1976-09-16 Siegenia Frank Kg Pantograph linkage stay mechanism for windows - has long and short levers and guide lever for saving space
US4158271A (en) * 1978-01-23 1979-06-19 William S. Hawkes Door closure
AT386040B (en) * 1983-08-13 1988-06-27 Rsb Holding & Management Ag ONE-HAND TURNTABLE FITTING FOR A WINDOW
DE3519988A1 (en) * 1985-06-04 1986-12-04 Siegenia-Frank Kg, 5900 Siegen Setting-out device for turn-and-tilt wings of windows, doors or the like

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1837472A1 (en) 2006-03-25 2007-09-26 Roto Frank Ag Window, door or similar with a load alleviation device
DE202014007902U1 (en) 2014-10-06 2014-10-28 Siegenia-Aubi Kg Angled fitting

Also Published As

Publication number Publication date
DK0379866T3 (en) 1992-04-21
ES2031011T3 (en) 1992-11-16
NO176933B (en) 1995-03-13
NO894977D0 (en) 1989-12-12
FI92516C (en) 1994-11-25
FI900156A0 (en) 1990-01-11
US5009034A (en) 1991-04-23
FI900156A (en) 1990-07-25
NO176933C (en) 1995-06-21
ATE73522T1 (en) 1992-03-15
DE59000060D1 (en) 1992-04-16
EP0379866A1 (en) 1990-08-01
FI92516B (en) 1994-08-15
CA2008331C (en) 1995-03-14
CA2008331A1 (en) 1990-07-24
NO894977L (en) 1990-07-25

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