EP0924376B1 - Aussenliegendes Lager für einen Schwingflügel - Google Patents
Aussenliegendes Lager für einen Schwingflügel Download PDFInfo
- Publication number
- EP0924376B1 EP0924376B1 EP98124141A EP98124141A EP0924376B1 EP 0924376 B1 EP0924376 B1 EP 0924376B1 EP 98124141 A EP98124141 A EP 98124141A EP 98124141 A EP98124141 A EP 98124141A EP 0924376 B1 EP0924376 B1 EP 0924376B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- casement
- bearing
- axis
- blind frame
- wing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
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- 238000005452 bending Methods 0.000 claims 1
- 230000008859 change Effects 0.000 description 15
- 238000007789 sealing Methods 0.000 description 15
- 238000006073 displacement reaction Methods 0.000 description 6
- 230000002441 reversible effect Effects 0.000 description 5
- 235000015095 lager Nutrition 0.000 description 4
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 238000013016 damping Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 241001416181 Axis axis Species 0.000 description 1
- 241001295925 Gegenes Species 0.000 description 1
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- 238000010276 construction Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 210000001061 forehead Anatomy 0.000 description 1
- 239000002655 kraft paper Substances 0.000 description 1
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- 238000003825 pressing Methods 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D11/00—Additional features or accessories of hinges
- E05D11/10—Devices for preventing movement between relatively-movable hinge parts
- E05D11/1028—Devices for preventing movement between relatively-movable hinge parts for maintaining the hinge in two or more positions, e.g. intermediate or fully open
- E05D11/1078—Devices for preventing movement between relatively-movable hinge parts for maintaining the hinge in two or more positions, e.g. intermediate or fully open the maintaining means acting parallel to the pivot
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D7/00—Hinges or pivots of special construction
- E05D7/08—Hinges or pivots of special construction for use in suspensions comprising two spigots placed at opposite edges of the wing, especially at the top and the bottom, e.g. trunnions
- E05D7/082—Hinges or pivots of special construction for use in suspensions comprising two spigots placed at opposite edges of the wing, especially at the top and the bottom, e.g. trunnions the pivot axis of the wing being situated at a considerable distance from the edges of the wing, e.g. for balanced wings
- E05D7/083—Hinges or pivots of special construction for use in suspensions comprising two spigots placed at opposite edges of the wing, especially at the top and the bottom, e.g. trunnions the pivot axis of the wing being situated at a considerable distance from the edges of the wing, e.g. for balanced wings with a fixed pivot axis
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D11/00—Additional features or accessories of hinges
- E05D11/10—Devices for preventing movement between relatively-movable hinge parts
- E05D11/1007—Devices for preventing movement between relatively-movable hinge parts with positive locking
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
- E05Y2900/13—Type of wing
- E05Y2900/148—Windows
Definitions
- the invention relates to a fitting so the storage for one to about central axis rotatable and mounted on a frame wings.
- Such wings can be swinging wings or reversible blades, in which the swing axle or Turning axis runs horizontally or vertically.
- One for such a swinging wing or Reversible wing suitable bearing includes a left and right or an upper and lower wing bearing part on one side and on the other side on the spar of the Sash or frame. These two bearings can be configured the same.
- the invention has set itself the task for a variety of types of profiles, in particular change profiles, and system designs of wings and frame and for a variety of dimensions to create a uniform swing bearings or spiral bearings, which can therefore fulfill its intended function, regardless of its location.
- a swing bearing or Wendeanagerung is by discontinuing the Rotary axis out of the wing spar and an arrangement of the axis of rotation clearly reached above the rollover.
- the swing axis or turning axis is no longer in the range the wing or in the frame of the frame, but above the rollover, which in the area of the respective bearing of the wing of a mitverschwenkten, vom Wing outbound rollover ("wing rollover”) in a not mitverschwenkten and firmly on the frame remaining and from this rollover (“Frame flashover”) changes, which in the closed state in full run.
- wing rollover vom Wing outbound rollover
- Fre flashover a not mitverschwenkten and firmly on the frame remaining and from this rollover
- the aforementioned arcing starts in each case from the change profile.
- the butt ends of the fixed rollover and the with the wing movable rollover are tailored so that in the closed Condition the cut edges rest on each other and in the open state, the two straight (blunt) ends form a plane in which the Oscillating axis of the wing - or the turning axis - runs.
- the two further outward Sealing lips are fully continuous in the outward-facing Rollovers in their closely adjacent facing each other Edge areas.
- the respective interchangeable profile, the half around the Wing and half running around the frame, is on each of the Sealing lips put on and covers them. In these areas takes over one Sealing strip on the opposite side of the exchange profile, the sealing function, so that in the closed state of the wing always two - in one direction perpendicular spaced to the frame frame - sealing strips fully on the wing are effective.
- Claim 1 describes a warehouse with two pieces, a wing-side and a frame-side building piece, which is used for the displacement of the axis of rotation (the Oscillating or turning axis of a swinging vane or turning wing) from the Frame and sash out, or from the respective spar of the respective Frame out, serve. With them, a distance is created, the axis of rotation (Swing axle or turning axis) receives from the respective spar, so that the Building pieces can also be referred to as spacers, see. the in this regard, description of the wing in claim 2. From the camps of the Claim 1, two bearings are used for a swing wing or reversing wing. Either a left and a right bearing for a swinging wing or an upper and a a lower bearing for a reversible wing.
- the axis of rotation the Oscillating or turning axis of a swinging vane or turning wing
- the axis of rotation clearly outside Level of the sash and the plane of the frame positioned.
- the axis runs above the flashovers and thus in the room and no longer by the material of the Frame or wing or the exchange profile through.
- a displacement of the pivot axis allows the formation of the change profile in Storage area so that a blunt abutment takes place in the closed position.
- the Completely closed position is the end of the change profile of the frame dull on the end of the change profile of the wing, which last with the Movement of the wing moved.
- the fully open position so in one Position in which the frame is swiveled through 180 ° and the upper wing area parallel to the lower frame area comes to lie, the two blunt ends in a flat plane, in which also the axis of rotation of the wing runs.
- the said plane runs horizontal; if it is a reversible wing, then the said plane runs vertical and the above-described upper and lower portions of the wing are then the right and left regions, or left and right regions, as appropriate Opening direction of the wing.
- this closing torque can be overridden (Claim 16).
- the compensation force can be by a prestressed Spring are applied (claim 18), which in the wing-side building piece in A spring receiving space is arranged (claim 19, 18).
- a cross to the Extension of the wing-building piece oriented latch bolt accesses from the Frame attachment body or the intermediate bearing axis holding piece over to the inside of the wing-building piece, there in a recess to intervene and specify a rotational movement blocking locking position.
- the Engagement opening may be the extension of the spring-receiving space, so that directly when engaging the locking lug the compensation force on the intervening Lock bolt can be applied perpendicular to the orientation of the axis.
- the position of the spring-receiving space is slightly inclined relative to the Center plane through the bearing axis bolt, which center plane also perpendicular to the closed wing runs, on which the building piece is arranged.
- Figure 5 illustrates in side view the insertion of a laterally projecting bearing 40, which may be a bolt. It is directed laterally outwards and runs parallel to the plane of the wing.
- the pivot axis 100 which can also be a turning axis in a vertical arrangement, is fixed on each side of the sash frame.
- the extent of the bolt does not go beyond the lateral extent of the rollover U1 of the wing in Figure 1 , they are rather only so far extending in this direction formed that they can be accommodated in a receiving groove 31 within the long oval bearing piece receptacle 30 of the bezel-side attachment piece 10 protrudes laterally and also engages over the wing flap.
- the wing can be used from above with its laterally extending bearing pin 40 in the receiving troughs 31, which can then be covered 32.
- the long oval bearing piece receptacle 30 (the lower bearing cover) forms with the bezel-side building block 10 an L-shaped configuration, wherein the short leg the building block and the longer leg bearing support for the bearing pin 40th form the wing.
- FIGS. 3 and 4 show , in two sectional views, the course of the exchangeable profile WP0, WP1, once above and once below the bearing with the two attachment pieces 10, 20 and the intermediate flat-oval bearing shell 30.
- the change profile WP1 is attached to the wing F. It moves with the wing when opening inwards / downwards in FIG . 1 .
- a guide groove N1 is formed, which receives a drive rod; with her, the lock on the operating handle G is possible.
- the drive rod extends in the groove N1 in the upper half of the wing under the interchangeable profile, ie between the end face of the sash F and the fixed thereto interchangeable profile WP1.
- the seal D3 in Figures 3 and 4 is ineffective for the operational sequence (movement of the wing), instead seal the two sealing strips D2 and D1 in the closed state, the change profile relative to the frame BR.
- the groove N0 facing away from the frame in FIG. 4 and pointing towards the frame in FIG. 3 does not receive a drive rod in those areas which are drawn vertically in FIG. 1, ie those bars of frame and wings which originate from the storage area.
- the guided in N1 drive rod breaks through suitable openings the removable profile and with a deflection, the linkage is then in the upper area in there according to Figure 3 outwardly facing groove N0 (not shown) and led there to provide locking lugs can.
- the pointing to the wing F groove N0 is suitable as a continuation of the figure 4 to the corner, z. B. locking plates to provide over the continue guided in the groove N1 of the wing drive rod locking options when the lock plates certain projections are opposed, which are actuated via the drive rod.
- the blunt stop at the level of the axis 100 which is shown at 101 in Figs. 5 and 6 as a plane perpendicular to the plane of the frame of Fig. 1, permits easy change of the sealing plane and easy adaptation of the change profile to the Sash frame or frame.
- the height of the building chocks 10,20 is the same height on both sides of the wing, which is apparent from Figure 6 , showing the open state of the wing F with respect to the frame BR. This creates the plane 101, which form the blunt end faces of the alternating profile WP0, WP1 (on the frame BR and the wing F) on both sides, on which bearings are arranged.
- the blunt ends of the alternating profile of wing and frame abut each other and can be sealed by a damping layer 25 in the closed state.
- the distance d of the axis 100 from the surface of the window frame or wing in the closed state is shown most clearly in section in FIG . This distance d is chosen so that the axis 100 is just next to the wing flap, that the long oval shot 30 in half still fits between the axis and the surface of the flashover U1.
- the flat-oval bearing shell 30 in Figure 2 consists of a jacket which protrudes from the projecting from the frame BR building block 10 in the direction parallel to the frame plane.
- the flat oval shape is visually appealing, but not essential for the function.
- In the mounted state it is exposed above the rollover and obscures the blunt separation area of the exchangeable profile.
- each bearing acts as if it U-shaped overlaps the interchangeable profile with rollover and is fixed on both sides in the flashovers, once on the frame and once on the sash. The entire visible from the handle side area of the exchange profile is bridged.
- Figure 7 illustrates a partial section through the U-shaped overlapping the frame frame bearing, which is shown in plan view in Figure 2 and in perspective in Figure 1 (left bearing).
- a first axis 100 and a second axis 102 can be seen on this side and on the other side (top and bottom) of an imaginary center plane, the former being the axis of rotation passing through the bearing pin 40 fixedly connected to its hat-shaped end 40a in the building block 20 is arranged on the window frame and rests on the bottom of an upwardly open receptacle 31 and can be rotated there, according to the pivoting movement or the turning movement of the wing F.
- the rotational movement is designated by w.
- the in length to the length of the bearing pin 40 adapted receiving portion 31 is covered by a matched to the upper end of the central part 30 of the bearing cover 32. Approximately in the middle of the bearing pin 40, a collar 41 is provided, which is better visible in Figure 9 in a view in the direction of the axis 100.
- the collar 41 engages in the cover 32 and through the bottom of the Receiving portion 31 through into an elongated bore 51 through the Middle part 30 of the camp runs. It is slightly into this hole and points spaced latching troughs 42a, 42b, 42c circumferentially into which the collar 53 of a Pin 50 can grip when pushed by a spring 52 in the blind hole End of the bore 51 is biased so that the collar 41 straight from the Collar 53 is blocked in its pivoting movement.
- the collar 53 of the long, but thin pin 50 is very small compared to the collar 41 much stronger Bolt 40, preferably less than one third of the diameter.
- FIG 8 an alternative Riegel folkkeit is shown, in which the pin 50 in the bore 51 extends continuously and the collar 41 on the bearing pin 40 is not blocked, instead having a front locking lug 49 which is able to engage in the flat side of the wing-Avembau mixes 20 and there can intervene in a circle provided latch troughs 48a or depressions blocking, as the detail enlargement AV shows.
- the pin 50 is resiliently biased in the other direction, and pulling out of the pin 51 results in a release of the wing, while in Figure 7, a pushing in of the pin 50 for releasing the wing pivoting movement was.
- the two movements are called axial movements ⁇ P for fixing the pivot position.
- the control of the bezel side is advantageous because they are independent of the Rotary position of the wing is always possible in the same place.
- FIG. 10 illustrates a perspective view of a wing-side structural part 21, 20, as can be largely seen in FIG.
- FIG. 10 shows the frame-side building piece 10, 11 and a cover or receptacle 30 arranged therebetween, which is designed substantially long-oval, here with a distinctly round area and a short rectangular area adjoining it and one to the wing and Blendrahmen out flattened area, as shown in the sectional view of Figure 11 .
- This substantially flat-oval design allows the insertion of the Lagerachs Cultures 40 which is fixed (non-rotatable) is arranged in the building block 20 on the frame side and engages in a corresponding pivot bearing of the receptacle 30, which receptacle is in turn fixedly arranged on the frame side mounting piece 10.
- FIG. 10 The internal structure of the bearing according to FIG. 10 is shown in the sectional views of FIG. 11 and Figure 8 as well as from the top view on the inside of the wing side Building piece 20, which side is hidden in FIG.
- a cross bar 49 is pin-shaped, having at its operating end a handle portion 50a, corresponding to the protruding pin 50 of Figure 7, only here as an elongated web with an orientation as the building block 10, seen in its two axial positions in the enlarged detail AV.
- the cross bar is offset relative to the axis 100 in the respective bearing and allows a blocking of the turning or swinging movement of the wing, which can be solved by tools or by hand on the handle portion 50a.
- the cross bar 49 is biased and spring-loaded biased to engage in one or more recesses 48 b, 48 a, which are arranged on the wing side 20 about the bearing pin 40 around. Moving the pin 50 in the axle 102 against the force of a spring (not shown) allows the pivoting movement of the blade to be released.
- the grip portion 50a is to be grasped and (in the figure 10 to the right / rear) to operate, so that the locking is released, so the engagement of the pin 49 in the locking recess 48a.
- a further locking position may be provided with the locking recess 48b, which has a position such that it is offset slightly less than 180 ° relative to the first locking recess.
- This latch well defines the full open position of the turnover blade, while the first latch recess 48a is arranged so that it defines a first rotational position of the wing at a small angle of 15 ° to 20 ° relative to the open position.
- the aforementioned first rotational position can be biased spring loaded, for Applying a compensation torque to the wing, by his displaced axis of rotation 40, outside the profile of the frame or pogelholms runs, a leading closed position closing torque experiences.
- This generated by the weight of the wing, the displacement of the axis of rotation Closing torque is compensated by the spring force of a spring 60 on the described locking pin 49, which in the recess 48a on the wing side Building piece engages. If it is solved, no transfer finds one Force component instead, the wing can then be freely operated and in order 180 ° pivoted position in the locking recess 48b engage again.
- FIG. 12 An obliquely inclined in their orientation 103 oblong recess receives a spring 60 which is biased via an overhead coupling piece 61 in the space 48c.
- the space 48c goes directly into the described latch recess 48a, however, is slightly wider, so that the coupling piece 61 experiences a stop and despite bias of the spring 60 of the locking pin can engage in the extension of the spring-receiving space 48c.
- the resulting coupling via the intermediate piece 61 now leads during the rotational movement of the wing-side building block 20 relative to the frame-side building block 10 to an additional compression of the spring 60, which is opposite to the axis 100 of the bearing axis piece 40 to apply a torque is capable.
- the entire spring chamber 62 extending from the lower portion 48c and the upper Region 48a is wider at the bottom than at the top and has an upper one at the top cylindrical shape, for receiving the locking bolt 49th
- the compensation force can be determined by the distance of the axis 103 from the axis 100 can also be set by selecting the Spring constant of the cylinder spring 60.
- this spring is interchangeable to different sash weights can be adjusted.
- the drawn in Figure 11 angle ⁇ is about 10 ° to 20 °, preferably about 15 °.
- This first rotational position of the wing may be a safety position or a ventilation position, which can be additionally secured by the transversely oriented locking bolt 49 or 50 is locked with its operating portion 50a by a hard to reach screw 50b or a hexagon socket screw, not by unauthorized persons or difficult to solve.
- the hard to reach screw 50b is in the enlarged detail AV of in FIG. 10, right-hand building block 10.
- This building piece is in his for Handle side of the wing of Figure 1 facing upper surface area with a approximately square recess 50c provided deep in the web section 10th extends.
- the here as hexagon socket screw shown hard-to-reach screw 50b provided partially from the Handle portion 50a of the bolt is covered with its locking lug 49.
- the handle 50a is shown in two axial positions, the bolt position (left) and the unlocked position (dashed). In the locked position covers the about rectangular handle portion 50a, guided in the aforementioned recess 50c the Partially screw 50b.
- the angular position of Figure 11 may also be oriented so that it reaches a balancing of the wing.
- This balancing position results from the fact that the opening torque and the torque tending to close are both substantially equal, so that the first rotational position ⁇ only by locking the locking bolt 49 and the front nose of the locking bolt with the rear handle 50a leads to a determination, but in terms of strength but is not substantially applied in one direction or in the other direction.
- an equilibrium of the torques is thus achieved approximately, from which the locking on the handle 50a can be released without risk of immediate pivoting in order either to completely close the wing from the first rotational position ⁇ or to open it further.
- each Wing-side building piece 21, 20 This bearing seat is designed slot-like, so that from above or from above obliquely in the case of a horizontally extending Rotary axis of a rocker wing of the wings with the protruding bearing pin in the Bearing is inserted in the receptacle 30 when the cover 32 is removed.
- the slot-like defines a receptacle at least in the front portion, for Inserting the respective bearing pin of the wing-side building piece 20.
- a in the Bearing receiving provided collar which opposite the obliquely upwardly projecting Tongue is spaced apart, serves to absorb lateral forces and corresponds to a in the bearing pin mounted groove. In this way, a rotary motion possible, with a secured in bolt direction storage.
- the invention has set itself the task for various types of profiles, especially change profiles, and system designs of wings and Frame and for a variety of dimensions a uniform swing bearing or Wendelager to create, regardless of its location can fulfill the intended function.
- Proposed is a storage for each a spar of a wing (F), the pivot axis (100) near the middle Area of the wing spar runs, for mounting on two opposite bars the wing and a frame.
- Two pieces (10,11; 20,21) becomes one Distance (d) to the frame (BR) and the wing (F) given so that the Rotary axis (100) adjacent to the plane of the wing (F).
- the Restraints (10, 11; 20, 21) are used to create the distance (d) of the axis of rotation (100) from the level of the wing to the resting one. Mounting on the frame (BR) and on the Wing (F) adapted.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Hinges (AREA)
- Closing And Opening Devices For Wings, And Checks For Wings (AREA)
- Wing Frames And Configurations (AREA)
- Support Of The Bearing (AREA)
Description
- Figur 1
- ist eine perspektivische Ansicht eines Schwingflügels F mit einer horizontalen Schwingachse 100 und zwei an den vertikalen Flügelholmen vorgesehenen Schwinglagern. Der Betätigungsgriff G verriegelt und entriegelt den Flügel über Treibstangen im Flügelrahmen.
- Figur 2
- ist eine Aufsicht auf eines dieser Schwinglager mit einer langovalen Abdeckung 30, hier herausgegriffen das linke Lager von Figur 1.
- Figur 3
- ist ein Schnitt B-B oberhalb des linken Schwinglagers von Figur 1. Hier bewegt sich der Überschlag U1 mit der Bewegung des Flügels F mit (beim Öffnen in Richtung einwärts/abwärts).
- Figur 4
- ist ein Schnitt A-A unterhalb des linken Schwinglagers von Figur 1. Hier bewegt sich der Überschlag U0, der auf der Blendrahmenseite BR an einem Wechselprofil WP0 angeordnet ist, nicht mit der Bewegung des Flügels F mit. Der Überschlag außen am Flügelrahmen wird dagegen mitbewegt, bei Schwenkung des Flügels (beim Öffnen nach außen/aufwärts).
- Figur 5, Figur 6
- veranschaulichen die geschlossene Stellung und die offene Stellung des Schwingflügels F von Figur 1. Dargestellt ist in Seitenansicht das linke Schwinglager, das in Aufsicht auch in Figur 2 ersichtlich ist.
- Figur 7, Figur 8
- veranschaulicht einen eigenständig interessanten Querriegel 50, der gegenüber der Achse 100 im jeweiligen Lager versetzt eine Sperrung der Wende- oder Schwingbewegung des Flügels erlaubt, die durch Hilfsmittel oder von Hand in Richtung P (oder -P) gelöst werden kann. Der Querriegel 50 ist stiftförmig und federbelastet vorgespannt, zum Eingriff in eine von mehreren Ausnehmungen 42a, 42b auf der Flügelseite 20 oder direkt am Lagerbolzen 40. Eine Axialbewegung des Stiftes 50 gegen die Kraft einer Feder 52 erlaubt ein Freigeben der Schwenkbewegung des Flügels F. Dazu kann ein Benutzer den auf der Blendrahmenseite in Richtung der Blendrahmenebene seitlich nach außen hervorstehenden Stift 50, der durch eine Öffnung 51 des Aufbaustücks 10 leicht hervorstehen kann, ergreifen und die gegenüber der Achse 100 in Blendrahmenrichtung versetzte Riegelung des Flügels lösen. Es können mehrere Riegelstellungen vorgesehen sein, entlang eines Kreisstücks auf der Flügelseite oder innerhalb der Abdeckung 30 an dem dortigen Lagerbolzen 40, in den jeweils der Stift 50 riegelnd eingreift. Die mehreren Riegelmulden 42a,42b,42c definieren dabei mehrere Öffnungsstellungen des Flügels, in denen er als Schwenkflügel oder Wendeflügel arretiert werden kann.
- Figur 9
- veranschaulicht eine Möglichkeit der Arretierung der Schwenkbewegungen an vorgegebenen Drehwinkellagen.
- Figur 10
- ist eine perspektivische Darstellung eines Lagers, bei dem die flachovale Abdeckung oder Aufnahme 30 ersichtlich ist und das auf beiden Seiten dieser Aufnahme ein flügelseitiges Aufbaustück 21, 20 und ein blendrahmenseitiges Aufbaustück 11, 10 aufweist, wobei flügelseitigen Aufbaustück 21, 20 das Lagerachsstück 40 fest angeordnet ist, das in der Lageraufnahme drehbar gelagert ist, die mit dem Deckel 32 abgedeckt ist.
- Figur 11
- veranschaulicht einen Schnitt durch das Lager gemäß Figur 10, wobei eine erste Drehstellung im Winkel α gezeigt wird, in der ein von der Aufnahme 30 ausgehender Riegelbolzen 49 in eine Sperrausnehmung 48a eingreift, gleichzeitig aber ein von der Feder 60 ausgeübtes Drehmoment in Richtung der Öffnungsstellung des Flügels übertragen wird.
- Figur 12
- veranschaulicht deutlicher die Erzeugung des Drehmomentes durch eine Aufsicht auf die Innenseite des flügelseitigen Aufbaustücks 21, 20, die in Figur 10 nicht sichtbar ist.
Claims (20)
- Lagerung für jeweils einen Holm eines Flügels (F) mit Überschlag, welcher eine Schwenkachse (100) aufweist, die nahe eines mittleren Bereiches des Flügelholms verläuft, zur Montage an zwei gegenüberliegenden Holmen des Flügels und eines Blendrahmens, bei welcher Lagerung(a) mit zwei Aufbaustücken (10,11;20,21) ein Abstand (d) zum Blendrahmen (BR) und zum Flügel (F) vorgegeben ist, so daß die Schwenkachse (100) neben einer Ebene des Flügels (F) verläuft;
dadurch gekennzeichnet, daß(b) die Aufbaustücke (10,11;20,21) in Richtung der Schwenkachse (100) um zumindest eine Breite des Überschlags beabstandet sind, um den Überschlag U-förmig übergreifen zu lassen und beiderseits des Überschlags zur aufliegenden Montage am Blendrahmen (BR) und am Flügel (F) angepaßt sind. - Lagerung nach Anspruch 1, mit zwei Lagern, die nicht in den stirnseitigen Randbereichen des Flügels (F) montiert sind, wobei jeweils ein Lager in jeweils einem flügelseitigen Abstandsstück (20,21) ein Lagerachsstück (40) trägt, um gemeinsam eine durchgehende Schwing- oder Wendeachse (100) des Flügels zu definieren, welche Lagerachsstücke (40) sich außerhalb oder oberhalb eines Überschlages (U1) des Flügels (F) über diesen Überschlag hinweg und außerhalb des Flügelrahmens (F) in Richtung zum Blendrahmen (BR) erstrecken und dort über einen blendrahmenseitigen Lagerachsen-Halter (10,11;30) zur Bildung einer Achse (100) festgelegt werden, wobei eine Höhe des blendrahmenseitigen Lagerachsen-Halters (10,11;30), senkrecht zur Ebene des Blendrahmens (BR), im wesentlichen einer jeweiligen Höhe des jeweils zugehörigen, flügelseitig korrespondierenden Abstandsstücks (21,20) entspricht.
- Lagerung nach Anspruch 2, wobei im Bereich des Lagers eine Nut (N1) zur Aufnahme einer Treibstange an der Schmalseite des Flügels (F) durchgehend verläuft, ohne eine dort zu führende Treib- oder Riegelstange kröpfen oder umsetzen zu müssen.
- Lagerung für Schwing- oder Wendeflügel (F), insbesondere großer Fläche, nach Anspruch 1, wobei eine Schwenkachse (100), um die sich der Flügel (F) mit einem Überschlag (U0,U1) bei seiner Schwing- oder Wendebewegung gegenüber einem fest verbleibenden Blendrahmen (BR) verschwenkt, deutlich außerhalb und neben (d) der Ebene des Flügels, der Ebene des Blendrahmens und der Ebene von Überschlägen (U0,U1) eines Wechselprofilstücks am Blendrahmen oder Flügel verläuft.
- Schwingflügel oder Wendeflügel (F) mit einem Überschlag (U1) für eine Lagerung nach Anspruch 1, und mit einer aus der Flügelebene deutlich herausverlagerten Drehachse (d,100), zum Einsetzen in eine Öffnung in einem Blendrahmen (BR), bei welchem Flügel im Bereich der Lagerung (10,20,30) der Überschlag (U0,U1) am Flügel bzw. am Blendrahmen einen, in einer Ebene senkrecht zur Ebene des geschlossenen oder ganz geöffneten Flügels, gerichteten Verlauf hat (101), entsprechend einem stumpfen Anstoßen des unteren Endes des oberen Überschlags (U1) und des oberen Endes des unteren Überschlags (U0) bei geschlossenem Flügel (F).
- Flügel nach Anspruch 5, bei dem eine senkrecht zu der Ebene des Blendrahmens (BR) verlaufende Trennebene (101) - bei offenem Flügel (F) in seiner gegenüber der Schließlage um etwa 180° geschwenkten Offenstellung - flach verläuft, und die beiden stumpfen Enden des verschwenkten und des unbeweglichen Überschlags (U1,U0) sowie die Achse (100,40) der Lagerung jeweils eines der beiden Lager in der flachen Trennebene zu liegen kommen.
- Lagerung nach einem der vorigen Ansprüche 1 bis 4, bei der die Aufbaustücke (10,20) einen Anbringungsflansch (11,21) und einen in Richtung senkrecht zur Ebene des Flügels (F) verlaufenden Stegabschnitt (10,20) haben, in dem insbesondere außermittig die Lagerachsstücke (40) der Drehachse (100) verlaufen.
- Lagerung nach einem der vorigen Ansprüche 1 bis 4, bei dem die Lagerachsstücke (40) in einer im wesentlichen flachovalen Abdeckung oder Aufnahme (30) verlaufen, die zwischen dem blendrahmenseitigen und dem flügelseitigen Aufbaustück (10,20) ausgebildet ist und am blendrahmenseitigen Aufbaustück (10) unverdrehbar angeordnet ist.
- Lagerung nach einem der vorigen Lageransprüche, bei der das Flügel-Aufbaustück (20) mit fest daran angeordnetem Lagerachsstück (40) gegenüber einer Abdeckung oder Aufnahme (30) auf der Blendrahmenseite verschwenkbar ist, insbesondere am Flügel-Aufbaustück (20) Drehwinkel-Arretierstellungen (42a,42b,42c; 48a,48b) fest vorgegeben sind, die mit einer von außen im blendrahmenseitigen Lagerseitenbereich (30,11,10) zugänglichen Riegeleinrichtung (50,50a,49) zusammenwirken.
- Lagerung nach einem der vorigen Lageransprüche, bei der die Aufbaustücke (10,20) in beide Richtungen des Holmes, an dem sie anbringbar sind, L-förmig zur aufliegenden Montage angepaßt sind, mit einem zur Anbringung am Blendrahmen (BR) bzw. Flügel (F) jeweils wenig breiten Fußabschnitt (11,21) und einem deutlich abragenden Stegabschnitt (10,20), der in Richtung des Holmes des Blendrahmens zumindest so breit ausgestaltet ist, daß zwei Lagerachsstücke (40) nebeneinander zwischen jeweils zwei Aufbaustücken Platz finden würden.
- Lagerung nach Anspruch 1 oder 10, bei der auf der einen Seite der Mittelebene des Aufbaustücks (20) eine lösbare Sperre (50,50a) vorgesehen ist, die im Abstand (e) von der Drehachse (100), aber parallel dazu (102), eine Sperrung der Wende- oder Kippbewegung des Flügels (F) ermöglicht, insbesondere in mehreren abgestuften Winkelstellungen (42a,42b,42c; 48a,48b).
- Lagerung nach einem der vorigen Lageransprüche, bei der die Lagerachsstücke als Lagerbolzen (40) jedes von zwei Lagern eines Flügels (F) nach außen ragen und in eine nach oben offene langlochartige Ausnehmung (31) zur Bildung von zwei vollständigen Lagern an zwei horizontalen oder vertikalen (beabstandeten) Holmen des Blendrahmens (BR) einsetzbar sind und nach Einsetzen die Lagerbolzen (40) am unteren Ende der Langloch-Ausnehmung (31) drehbar gelagert sind.
- Lagerung nach einem der vorigen Lageransprüche, bei der die Lagerachsstücke, insbesondere Lagerbolzen (40), über der Oberfläche des Überschlages (U1,U0) verlaufen und über zwei L-förmige Böcke (30,10,11) mit dem Blendrahmen (BR) verdrehbar verbunden sind.
- Lagerung nach Anspruch 10 oder 13, bei der die L-Form eine Doppel-L-Form ist, so daß sich eine T-Form für die Aufbaustücke (10,11; 20,21) ergibt.
- Lagerung nach Anspruch 11 oder einem der Ansprüche 1 oder 2, bei welcher Lagerung zwischen dem flügelseitigen Aufbaustück (20,21) und dem blendrahmenseitigen Aufbaustück (10,11) eine Vorspannkraft (K), insbesondere eine Federkraft (60), zumindest auf der einen Lagerseite des Flügels (F) wirksam ist, um ausgehend von der Schließlage in einem begrenzten Schwenkwinkelbereich (α) eine Kompensationskraft aufzubringen, zur Kompensation des Schließ-Drehmomentes, das durch die außerhalb des Flügelholms gelegene Drehachse (100) entsteht und den Flügel (F) in der Schließstellung hält.
- Lagerung nach Anspruch 15, bei dem(a) die Vorspannkraft als Kompensationskraft außer Wirkung setzbar ist (49,50,50a), insbesondere zur Montage des Flügels; oder(b) die Vorspannkraft ein solches Drehmoment im Öffnungssinn auf den Flügel ausübt, daß das Kompensations-Drehmoment zumindest gleich, insbesondere etwas größer, als das durch das Gewicht des Flügels vorgegebene Schließ-Drehmoment ist.
- Lagerung nach Anspruch 12, bei der die langlochartige Ausnehmung (31) schräg nach oben ragt - nach oben und nach vorne -, wobei sie insbesondere durch eine schräg aufwärts ragende Zunge gebildet wird, die an dem Ende der langlochartigen Ausnehmung ausgebildet ist, das dem flügelseitigen Aufbaustück (20,21) direkt benachbart ist.
- Lagerung nach Anspruch 15, bei der die Kompensations-Vorspannkraft (K) durch eine Feder (60) aufbringbar ist, die in einem insbesondere schräg (103) in dem flügelseitigen Aufbaustück (20,21) eingebrachten Raum (62; 48c,48a) liegt und dort vorgespannt gehalten wird.
- Lagerung nach Anspruch 18, bei der sich der Raum auch oberhalb der vorgespannten Feder erstreckt (48a), zur Aufnahme eines Riegelbolzens (49), auf den die Kompensationskraft (K) ausgeübt wird, senkrecht zu seiner Erstreckung.
- Lagerung nach Anspruch 19 oder 18, bei der die Kompensationskraft (K) zwischen der Schließstellung und der durch eine Raumerhöhung (48a) und den Eingriff des Riegelbolzens definierten ersten Drehstellung wirksam ist.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19756521 | 1997-12-18 | ||
DE19756521 | 1997-12-18 | ||
DE19846216 | 1998-10-07 | ||
DE19846216 | 1998-10-07 |
Publications (3)
Publication Number | Publication Date |
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EP0924376A2 EP0924376A2 (de) | 1999-06-23 |
EP0924376A3 EP0924376A3 (de) | 2002-07-17 |
EP0924376B1 true EP0924376B1 (de) | 2005-11-23 |
Family
ID=26042609
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP98124141A Expired - Lifetime EP0924376B1 (de) | 1997-12-18 | 1998-12-18 | Aussenliegendes Lager für einen Schwingflügel |
Country Status (3)
Country | Link |
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EP (1) | EP0924376B1 (de) |
AT (1) | ATE310880T1 (de) |
DE (2) | DE19857650A1 (de) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
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DE102015100543A1 (de) * | 2015-01-15 | 2016-07-21 | SCHÜCO International KG | Schwing-Wendefenster mit einer Dichtungsanordnung |
CN109552602A (zh) * | 2018-12-24 | 2019-04-02 | 深圳市道通智能航空技术有限公司 | 一种无人飞行器 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1364312A (en) * | 1916-11-02 | 1921-01-04 | Francis J Plym | Interlocking molding for pivoted or swinging frames |
GB1086948A (en) * | 1963-09-10 | 1967-10-11 | Automatic Pressings Ltd | Improvements in and relating to hinges |
GB1079354A (en) * | 1965-05-06 | 1967-08-16 | Crompton Nettlefold Stenman | Limited movement safety hinge for windows and the like |
DE2448226A1 (de) * | 1974-10-09 | 1976-04-22 | Hoeganaes Ab | Rauchabzug-verschlussklappe |
FR2372948A1 (fr) * | 1976-12-03 | 1978-06-30 | Salvado Cugat Jose | Perfectionnements apportes aux baies pivotantes |
GB8803571D0 (en) * | 1988-02-16 | 1988-03-16 | Magnet Plc | Emergency window system |
DE3935521A1 (de) * | 1989-10-25 | 1991-05-02 | Hautau Gmbh W | Schwingfluegellager-baureihe |
DE29813095U1 (de) * | 1998-07-23 | 1998-11-26 | Gretsch-Unitas GmbH Baubeschläge, 71254 Ditzingen | Schwing- oder Wendeflügel eines Fensters |
-
1998
- 1998-12-14 DE DE19857650A patent/DE19857650A1/de not_active Withdrawn
- 1998-12-18 AT AT98124141T patent/ATE310880T1/de not_active IP Right Cessation
- 1998-12-18 DE DE59813217T patent/DE59813217D1/de not_active Expired - Lifetime
- 1998-12-18 EP EP98124141A patent/EP0924376B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
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ATE310880T1 (de) | 2005-12-15 |
DE59813217D1 (de) | 2005-12-29 |
EP0924376A2 (de) | 1999-06-23 |
DE19857650A1 (de) | 1999-06-24 |
EP0924376A3 (de) | 2002-07-17 |
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