EP2354402B1 - Lock for leaf assemblies - Google Patents

Lock for leaf assemblies Download PDF

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Publication number
EP2354402B1
EP2354402B1 EP11000674.9A EP11000674A EP2354402B1 EP 2354402 B1 EP2354402 B1 EP 2354402B1 EP 11000674 A EP11000674 A EP 11000674A EP 2354402 B1 EP2354402 B1 EP 2354402B1
Authority
EP
European Patent Office
Prior art keywords
latching
locking
locking element
projection
movement
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP11000674.9A
Other languages
German (de)
French (fr)
Other versions
EP2354402A2 (en
EP2354402A3 (en
Inventor
Andreas Finke
Ralf Höher
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.)
Dormakaba Deutschland GmbH
Original Assignee
Dormakaba Deutschland GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dormakaba Deutschland GmbH filed Critical Dormakaba Deutschland GmbH
Publication of EP2354402A2 publication Critical patent/EP2354402A2/en
Publication of EP2354402A3 publication Critical patent/EP2354402A3/en
Application granted granted Critical
Publication of EP2354402B1 publication Critical patent/EP2354402B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • E05D15/06Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B65/00Locks or fastenings for special use
    • E05B65/08Locks or fastenings for special use for sliding wings
    • E05B65/087Locks or fastenings for special use for sliding wings the bolts sliding parallel to the wings
    • E05B65/0882Locks or fastenings for special use for sliding wings the bolts sliding parallel to the wings mounted on the slide guide, e.g. the rail
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D13/00Accessories for sliding or lifting wings, e.g. pulleys, safety catches
    • E05D13/04Fasteners specially adapted for holding sliding wings open
    • 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
    • E05F3/00Closers or openers with braking devices, e.g. checks; Construction of pneumatic or liquid braking devices
    • E05F3/22Additional arrangements for closers, e.g. for holding the wing in opened or other position
    • E05F3/221Mechanical power-locks, e.g. for holding the wing open or for free-moving zones
    • E05F3/222Mechanical power-locks, e.g. for holding the wing open or for free-moving zones electrically operated
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B15/00Other details of locks; Parts for engagement by bolts of fastening devices
    • E05B15/02Striking-plates; Keepers; Bolt staples; Escutcheons
    • E05B15/0205Striking-plates, keepers, staples
    • E05B2015/023Keeper shape
    • E05B2015/0235Stud-like
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B47/00Operating or controlling locks or other fastening devices by electric or magnetic means
    • E05B47/0001Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof
    • E05B47/0002Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof with electromagnets
    • E05B47/0003Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof with electromagnets having a movable core
    • E05B47/0004Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof with electromagnets having a movable core said core being linearly movable
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B47/00Operating or controlling locks or other fastening devices by electric or magnetic means
    • E05B47/02Movement of the bolt by electromagnetic means; Adaptation of locks, latches, or parts thereof, for movement of the bolt by electromagnetic means
    • E05B47/026Movement of the bolt by electromagnetic means; Adaptation of locks, latches, or parts thereof, for movement of the bolt by electromagnetic means the bolt moving rectilinearly
    • 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
    • E05F1/00Closers or openers for wings, not otherwise provided for in this subclass
    • E05F1/002Closers or openers for wings, not otherwise provided for in this subclass controlled by automatically acting means
    • E05F1/006Closers or openers for wings, not otherwise provided for in this subclass controlled by automatically acting means by emergency conditions, e.g. fire
    • 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
    • E05F15/00Power-operated mechanisms for wings
    • E05F15/60Power-operated mechanisms for wings using electrical actuators
    • 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
    • E05F3/00Closers or openers with braking devices, e.g. checks; Construction of pneumatic or liquid braking devices
    • E05F3/22Additional arrangements for closers, e.g. for holding the wing in opened or other position
    • E05F2003/228Arrangements where the end of the closer arm is sliding in a track
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2201/00Constructional elements; Accessories therefore
    • E05Y2201/20Brakes; Disengaging means, e.g. clutches; Holders, e.g. locks; Stops; Accessories therefore
    • E05Y2201/218Holders
    • E05Y2201/22Locks
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2201/00Constructional elements; Accessories therefore
    • E05Y2201/40Motors; Magnets; Springs; Weights; Accessories therefore
    • E05Y2201/46Magnets
    • E05Y2201/462Electromagnets
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2201/00Constructional elements; Accessories therefore
    • E05Y2201/60Suspension or transmission members; Accessories therefore
    • E05Y2201/622Suspension or transmission members elements
    • E05Y2201/684Rails
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2600/00Mounting or coupling arrangements for elements provided for in this subclass
    • E05Y2600/40Mounting location; Visibility of the elements
    • E05Y2600/456Mounting location; Visibility of the elements in or on a suspension member
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2600/00Mounting or coupling arrangements for elements provided for in this subclass
    • E05Y2600/50Mounting methods; Positioning
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2800/00Details, accessories and auxiliary operations not otherwise provided for
    • E05Y2800/25Emergency conditions
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/10Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
    • E05Y2900/132Doors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/08Bolts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/08Bolts
    • Y10T292/096Sliding
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/08Bolts
    • Y10T292/096Sliding
    • Y10T292/1014Operating means
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/08Bolts
    • Y10T292/096Sliding
    • Y10T292/1014Operating means
    • Y10T292/1021Motor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/08Bolts
    • Y10T292/1043Swinging
    • Y10T292/1044Multiple head
    • Y10T292/1045Operating means
    • Y10T292/1047Closure

Definitions

  • the invention relates to a lock for wing systems, in particular for sliding door systems.
  • the DE3427609 discloses all features of the preamble of claim 1.
  • Latches of the aforementioned type are known per se.
  • a locking latch for tilt windows is shown.
  • Serving as a locking element guide pin is taken in a translucent guided in a slot of a corresponding longitudinal guide and further attached to a scissor arm of a tilting fitting of an associated window sash.
  • the slot ends at one end in an end limit, which has the shape of a circular hole whose diameter is larger than the slot is wide.
  • the longitudinal guide is elastic. Therefore, it is the guide pin possible to be moved along the slot and locked in the circular hole, whereby the locking or wing detection is achieved.
  • the disadvantage is that the lock is constantly effective.
  • a sliding door lock is known in which a kind of locking bell is arranged rotationally fixed to a drive pulley of a sliding door drive. To the drive pulley, an endless traction means of the sliding door drive is performed. The bell instructs a preferably circumferentially formed, extending parallel to the axis of rotation of the bell wall recesses.
  • a locking bolt can be translationally moved transversely to the axis of rotation towards the recesses and engaged with a respective one of the recesses. This prevents rotation of the bell. As a result, the drive disk no longer rotates and thus the sliding door wings which are effectively coupled with the traction means can no longer be moved.
  • the disadvantage of this solution is that rotating parts must be present in order to accomplish the locking can.
  • An application, for example, to other door systems is hard to realize.
  • the structure is relatively large and complex. The object of the invention is to counteract the aforementioned disadvantages.
  • a device according to the invention for locking at least one wing of a wing system has a first locking element and a second locking element.
  • the first locking element comprises at one end a first latching element.
  • the second locking element comprises at a first locking element facing the end of a second locking element.
  • This second latching element is designed to be latchingly engaged in the locking position with the first latching element.
  • the second locking element is also adapted to be fixed in relation to the wing system.
  • the first locking element is arranged to be arranged with respect to the at least one wing such that the first locking element upon movement of the at least one wing with this Movement is correspondingly moved such that the first locking element is moved depending on the direction of movement of the at least one wing translationally in a locking position on the second locking element to or in an unlocked position of the second locking element.
  • the first locking element is also moved due to a wing movement, whereas the second locking element remains in one and the same place with respect to the entire wing system.
  • One of the locking elements also includes an activation element that allows the latching operative engagement between the first locking element and the second locking element according to a locking position or prevented according to a release position upon actuation. Ie.
  • the activation element causes an arming or switching off the wing lock thus formed.
  • the translational movement of the first locking element makes it possible to integrate the locking device in any type of wing system, which has a translationally moving part, which is moved by the respective wing, or which is otherwise capable of, via the wing movement a part translatorisch (to move).
  • This solution is thus completely independent of the type of any existing rempligelbetuschigers who is able to move the respective wing in at least one direction. Ie.
  • This solution can also be used in purely manually operated wing systems. In addition, this solution is easy to integrate in wing systems.
  • the second locking element is designed to be fixedly mounted in the region or in a receiving groove of a stationary with respect to the wing system or the respective wing arranged guide member.
  • This allows easy integration of the second locking element. It is in fact possible, simply insert the first locking element in the receiving groove translationally movable. It can then assume the function of a slider, for example. This results in the advantage that the space required for the locking arrangement thus formed can be kept to a minimum.
  • the first or the second latching element has a latching projection, according to which the respective other latching element has a locking part corresponding to this latching projection.
  • Suitable locking parts are in turn a latching projection or a recess.
  • the latching part comprises a first pass-through part which has a recess which serves for the latching explained below.
  • Pass-through part means that the latching projection for the purpose of locking said wing passes through this latching recess.
  • the latching recess is formed continuously in the first pass-through part. It is also movable at a right angle to the translatory movement path of the latching projection such that the latching recess is arranged in the release position so that the latching projection can move along its translatory movement path through the latching recess.
  • the Locking recess is arranged in the release position so that the locking projection along its translational movement path can freely move back and forth through it.
  • the latching part further comprises a second pass-through part, which is arranged on a latching projection facing side of the first pass-through part. It likewise has a recess, similar to the first penetration part, which recess is continuous in the second penetration part. It is stationary in relation to the second locking element arranged such that the locking projection along its translational movement path through the recess can move freely back and forth. Ie. this recess is not the lock but for example as a stop for the first locking element.
  • the recesses of the naturalgriffsmaschine are thus arranged to each other that the locking projection, if he passes through both recesses, is prevented from moving from the recess to a recess in the direction of the second passage portion at least to a predetermined extent and thus detent with the latching recess is in operative engagement.
  • the recesses take each other different positions in release and blocking position.
  • the pass-through parts abut each other.
  • the recess of the respective penetration part has a, seen in the direction of movement of the latching projection, to the outer contour ebenjenen latching projection substantially complementary inner contour.
  • the penetration parts preferably each have a portion which extend parallel to each other and are plate-like.
  • the plate-like design of the für Bachsmaschine allows, seen transversely to the direction of movement of the locking projection, a very economical space utilization.
  • the second locking element seen along the direction of movement of the locking projection, is very short and thus saves space.
  • the latching projection is preferably tapering at its end facing the latching recess in the direction of the latching recess, and is furthermore preferably mushroom-shaped. This makes it possible to push the locking projection through the recesses of the fürgriffsile through to the aforementioned operative intervention, even if they are already in the locked position.
  • the latching projection can also be designed so that the latching projection can be moved out of the latching recess by overcoming the locking or locking force produced by the operative engagement with the latching recess and also in the opposite direction of movement. Ie. With such a locking projection is a very simple and inexpensive way a wing lock with overload protection feasible.
  • the aforementioned activation element is preferably formed by means of an electromagnet which, when actuated, the first penetration part in Release or moved in locked position.
  • the electromagnet has the advantage of defined working positions (locking, unlocking) of the locking arrangement and can also be easily adapted via the energization of desired holding or locking forces.
  • pulsed current can be used.
  • at least one of the locking elements on a side facing the respective other locking element on a stop for the respective other locking element is easily a limitation for the locking projection during its movement in the direction of corresponding locking element feasible.
  • the second locking element is adapted to be fixed in relation to a guide or slide rail of the wing system.
  • the first locking element can also be accommodated in the guide or slide rail directly or indirectly in a translatory manner on the second locking element to and away from it. This allows an elegant and in the extreme case completely invisible integration of the second locking element using the already existing guide or slide rail. Thus, parts of already existing wing systems are used. Furthermore, this results in both space-technical and optical advantages, since the second locking element can be hidden optically.
  • the second locking element is adapted to be fixedly mounted on or in the guide or slide rail. This has the advantage that only on or in this rail appropriate mounting options must occur. In addition, no edits are necessary on the wing or other parts of the wing system, on the one hand the assembly or retrofitting facilitates, on the other hand, but also allows a visually-traced decommissioning.
  • the wing system thus has at least one movable wing, at least one with respect to the wing system or the at least one movable wing fixedly arranged guide or slide rail with a receiving groove and at least one of the above-described locking devices.
  • the wing system preferably comprises at least one wing designed as a pivoting wing.
  • This wing is operatively connected via a slide linkage with a Schwenkerielbetuschiger, so a swing door drive or door closer.
  • the wing system has a slide, in which a slider is added translationally guided, which in turn is freely rotatably articulated on the sliding arm of the linkage.
  • the first locking element may be part of or replace the slider.
  • the wing system has at least one wing designed as a sliding (door) wing.
  • Such wings are usually suspended above the respective wing arranged support and / or guide rails or guided along their path of movement.
  • the mounting rail can thus additionally serve for the direct or indirect guidance of the second locking element, for example via a carriage operatively connected to the wing.
  • the above-described locking arrangement is very simple and preferably invisible to the user integrated.
  • FIG. 1 shows a locking arrangement 1 according to an embodiment of the invention.
  • the arrangement 1 comprises by way of example a mounting rail 10 of an exemplary sliding door system.
  • the sliding door system is linear motor based in the example shown.
  • the support rail 10 is used in the example shown in a receiving portion 11 at least the inclusion of a stator, not shown here of the linear motor.
  • Another, separately formed receiving portion 12 is mainly used for guided recording preferably of carriage 20 one here not shown sliding sash. The sliding sash is received in the support rail 10 via aforementioned carriages 20.
  • the carriage 20 by way of example a receiving profile 21, the down, d. H. towards the wing, open.
  • This opening serves to carry out a respective driver 23, which actively connects the receiving profile 21 with said wing.
  • a rotor 22 is used, which has a series of permanent magnets in the example shown.
  • the rotor 22 enters the stator in a known manner in magnetic interaction.
  • a locking member 30 is fixedly mounted.
  • the locking element 30 is attached by means of a stop portion 31 on the front side or in the profile 21.
  • a shaft 33 connects to the stop portion 31, at the free end of a preferably plizkopfartiger locking projection 32 is formed. Ie. the locking projection 32 tapers in the direction of its free end.
  • the shaft 33 has a smaller diameter than a maximum outer diameter of the latching projection 32. Stopping section 31, shaft 33 and latching projection 32 are fastened to each other or formed integrally in part or in the entirety.
  • a locking element 100 is a locking element 100 in the region of the left end side of the support rail 10 in the region of the left end side of the support rail 10 in a locking element 100.
  • the locking element 100 has a mounting portion 102 which is received, for example, by clamping in the support rail 10 and in its receiving portion 12.
  • mounting options such as screws, locking, welding, gluing and the like are conceivable.
  • FIG. 2 shows the locking arrangement 1 of FIG. 1 in section along a line A - A in FIG. 1 ,
  • the locking element 100 comprises two so-called pass-through parts 110, 120.
  • the function of these parts will be explained later.
  • the penetration part 110 preferably has centrally a recess 111, which is formed in the example shown as a circular through hole and extends along the direction of movement of the locking projection 32, ie here along the longitudinal extent of the support rail 10 and the profile 20.
  • the penetration part 110 is transversely to the direction of movement of the locking projection 32 and the carriage 20, ie obliquely to the bottom right in FIG. 2 , guided translationally movable.
  • the locking element 100 also has an activating element here in the form of an electromagnet 101.
  • the electromagnet 101 interacts magnetically with a here partially visible armature plate 113 of the penetration part 110.
  • the electromagnet 101 is arranged so that it attracts the armature plate 113 obliquely to the bottom right transversely to the direction of movement of the locking projection 32 and along the direction of movement of the penetration part 110 when energized.
  • the anchor plate 113 is fixed to the penetration part 110 or formed integrally with it.
  • Penetration part 110 and anchor plate 113 preferably include an angle of about 90 °. Ie. the penetration part 110 is moved obliquely down to the right as soon as the electromagnet 101 attracts the anchor plate 113 during energization.
  • the attachment of the locking element 100 by means of the aforementioned, fastening portion 102, which is preferably clamping in the Support rail 10 is added.
  • fastening portion 102 which is preferably clamping in the Support rail 10
  • all other mounting options such as screws, locking, welding, gluing and the like are conceivable.
  • the solenoid 101 is fixedly attached to the mounting portion 102 by means of screws 105, one of which is visible.
  • the locking arrangement 1 is shown in a so-called locking position. Ie. the latching projection 32 is engaged with the through-engagement parts 110, 120 and engages behind the passage portion 110. As can be seen, the latching projection 32 and therefore also the shaft 33 pass through the passage portions 110, 120 or their recesses 111, 121, of which only here the recess 111 of the penetration part 110 is clearly visible. Ie. the passage portions 110, 120 are arranged between locking projection 32 and abutment portion 31.
  • the illustrated block arrow represents the direction of movement of the rotor 22 or of the carriage 20 and thus of the locking element 100 and the latching projection 33.
  • the carriage 20 connected thereto is prevented from disengaging from the locking element 100, ie obliquely to the bottom left in FIG FIG. 2 to move.
  • the operatively connected to the carriage 20 wings also prevented from moving and thus locked.
  • the stopper portion 31 is preferably in the position shown on the press-through member 120 at. However, it can also be provided that the shaft 33 is longer, so that the stopper portion 31 can move away from the penetration part 120 by a certain distance. This has the advantage that, for example, caused by temperature fluctuations changes to the system can be compensated.
  • the receiving portions 11, 12 are shown here for the profile 21 and the stator of the linear motor, also not shown here.
  • the receiving portions 11, 12 are separated by means of mutually facing, protruding projections 13 on or in the mounting rail 10 from each other.
  • the wings facing away from the surfaces of the projections 13 serve as a support surface for the stator.
  • the wings of the facing surfaces of the projections 13 are preferably used as a support surface for the mounting portion 102 of the locking element 100.
  • the projections 13 on its profile 21 facing surfaces can serve as a running surface for non-visible rollers of the carriage 20. This is particularly useful because it ensures that between rotor 22 and recording profile 21 and stator is always maintained a predetermined distance, so that the magnetic driving force of the linear motor thus formed is ensured.
  • the support rail 10 also has projections 14, which are similar to the projections 13 facing each other protruding.
  • the projections 14 may also serve as a running surface for corresponding rollers of the carriage 20 on their sides facing away from the wing.
  • the projections 13, 14 are thus preferably used to position the respective carriage 20 in the mounting rail 10th
  • FIG. 3a shows the locking member 100 in more detail and according to a first embodiment of the invention.
  • the locking element 100 is shown in a so-called locking position, which allows the aforementioned locking position.
  • the anchor plate 113 has a pin-like part 114.
  • the part 114 is preferably formed through the anchor plate 113 therethrough. This makes it possible, for example, to arrange a helical spring 106 as a restoring element between armature plate 113 and electromagnet 101.
  • the return spring 106 causes, when the solenoid 101 is not energized, that the armature plate 113th is moved to a release position, which is not shown here.
  • the part 114 can be used at its end remote from the electromagnet 101 for connection of an actuating element, such as a Bowden cable, a lever, a pull rod or the like.
  • an actuating element such as a Bowden cable, a lever, a pull rod or the like.
  • the solenoid 101 serves to hold the stationary leaf of this system.
  • the part 114 is pulled by means of the aforementioned actuating element from the other wing, ie the active leaf, or by its actuator in the release position, in which the recesses 111, 121 are preferably aligned.
  • the fastening section 102 and the penetration part 120 form a type of mounting bracket, to which the electromagnet 101 is fastened here by means of screws 105 on an inner side facing the wing.
  • the passage portions 110, 120 have circular recesses 111, 121 which are not aligned with one another in the illustration shown. In the aforementioned release position, however, the recesses 111, 121 are aligned with each other, so that the locking projection 32 can move freely through the recesses 111, 121 and thus can not be locked or locked. Thus, the locking element 100 is in the aforementioned release position.
  • the electromagnet 101 is energized, the armature plate 113 magnetically attracted and thus the penetration part 110 in the in FIG. 3a shown position moves.
  • the aforementioned, tapered design of the locking head or locking projection 32 allows in this position that this overcome both the recess 121 and the recess 111 can and can engage with the recess 111 latching into engagement. Ie. the locking projection 32 engages in the locking position due to the mismatched arrangement of the recesses 111, 121 to each other, the recess 111 and can not or only to a small extent in the direction out of the recesses 111, 121 are moved. This creates a very simple, yet effective locking of the connected wing / s.
  • FIG. 3b shows the locking element 100 in the release position.
  • the recesses 111, 121 of the passage portions 110, 120 are aligned with each other. At least they are aligned with each other so that the locking head 32 is not shown, preferably without resistance through the recesses 111, 121 can be freely moved back and forth.
  • the electromagnet 101 is preferably not energized.
  • the return spring 106 presses the penetration part 110 in the illustrated release position.
  • the electromagnet 101 can, as shown, be designed to be normally open or the latching projection 32 to be releasing. But it can just as well normally closing and thus locking projection 32 may be formed locking in the locked position.
  • the recess 111 in the in FIG. 3a shown working position of the electromagnet 101 that is, when it has magnetically attracted the armature plate 113, formed so that it is aligned with the recess 121. If the energization of the electromagnet away, the armature plate 113 is urged away from the electromagnet, and the recesses 111, 121 are increasing FIG. 3a similar alignment to each other, so no longer aligned with each other.
  • FIG. 4a shows a locking element 100 according to a second embodiment of the invention.
  • the attachment portion 102 is in cross section U-shaped and thus provides a receiving space for the electromagnet 101.
  • the solenoid 101 is preferably mounted by means of screws 105 on the mounting portion 102.
  • a wall portion connecting the two limbs 108 of the U is formed by the pass-through portion 120, which is thus embodied here as an example in one piece with the fastening portion 102.
  • the legs 108 have on their sides facing each other guide portions 107 here in the form of protruding, mutually open guide grooves or rails on. In these guide portions 107, the pass-through part 110 is movably guided between locking and release position, in this case into and out of the plane of the page.
  • Each clamping portion 109 has a first wall portion 109a, which extends from the penetration portion 120.
  • a respective second wall portion 109b follows, which preferably encloses a right angle with the associated wall portion 109a.
  • a respective third wall section 109c which extends in the direction of the penetration section 120, adjoins.
  • the clamping portions 109 are preferably parallel to each other.
  • the wall portions 109a, 109c of the clamping portions 109 are formed so that the locking element 100 can be inserted into the receiving portion 12 of the support rail 10, not shown.
  • facing away from each other surfaces 109d, 109e of the wall sections 109a, 109b each correspond to a corresponding one of the projections 13, 14 of the mounting rail 10.
  • Each wall section 109b has an unillustrated passage opening, through which a bracing element is guided here in the form of a respective screw 104.
  • the wall portions 109a, 109b of a respective clamping portion 109 have at least partially a distance a, which is smaller than a maximum outer diameter of the screw 104.
  • the screws 104 are designed so that they are screwed in the direction of solenoid 101 between the aforementioned areas of the associated Wall sections 109a, 109b with distance a to each other.
  • the third wall portion 109c is moved away from the wall portion 109a of the respective clamp portion 109, so that the distance a increases.
  • the surfaces 109c, 109d said clamping portion 109 engage with the projections 13, 14 by clamping in abutment; the locking element 100 is clamped or jammed in the support rail 10.
  • the locking element 100 thus forms a kind of module that can be used as a whole in the support rail 10.
  • FIG. 4b shows the locking element 100 from a different perspective.
  • the screws 105 for fastening the electromagnet 101 on the attachment portion 102 can be seen.
  • both surfaces 109d, 109e preferably both clamping portions 109 and the corresponding wall portions 109a, 109c have groove portions 109f, whose unspecified grooves extend transversely to the insertion direction in the support rail 10, not shown. If the clamping surface of the facing, associated projection 13, 14 of the mounting rail 10 facing the respective surface 109d, 109e has essentially complementary grooves, the locking element 100 can be gradually moved into the final insertion position in the mounting rail 10 and thereby fixed (before) which simplifies assembly.
  • FIG. 5 shows a locking element 100 according to a third embodiment of the invention in the locked position.
  • the recesses 111, 121 are therefore not aligned with each other.
  • the penetration part 110 is movably supported by means of elongated holes 112 via guide pins fastened or integrally formed on the penetration part 120 as guide section 107 along the actuation direction of the electromagnet 101.
  • the anchor plate 113 and the penetration part 110 preferably form an L-shaped part.
  • the pins 107 pass through corresponding elongated holes 112 of the penetration part 110.
  • the elongated holes 112 thus extend along the direction of movement of the penetration part 110.
  • securing washers 103 are mounted on the guide pins 107. They prevent the penetration part 110 from the penetration part 120 or the attached thereto or integrally formed with this guide pins 107 in the direction of solenoid 101 removes or dissolves.
  • other solutions such as snap rings, lock nuts and the like are possible.
  • the guide pins 107 have correspondingly formed screw threads.
  • the penetration part 110 is movably mounted on the attachment portion 102, so that the operative connection with the electromagnet 101 likewise fastened to the attachment portion 102 is freed from the weight of the penetration member.
  • the operative connection via the anchor plate and the connecting part 114 can be done very easily.
  • solenoid 101 is preferably a solenoid used.
  • the electromagnet 101 is formed bistable, so that it accomplishes both the blocking and the release position of the locking element 100. In that case, additional return elements can be omitted.
  • the part 114 can also be used in connection with a mechanical release part in the context of an exemplary single-leaf door, for example for an emergency opening or emergency closing of the connected wing.
  • Emergency opening or closing means that an opening or closing of the respective wing / s must be possible if the power supply of the wing system, ie in particular the locking arrangement 1, is eliminated.
  • the locking projection 32 is in the blocking position on the locking element 100 facing away from the surface of the recess 111 of the remote with respect to the locking element 30 penetration portion 110, thus engages behind them and thus locks the connected wing.
  • the pass-through part 120 arranged between carriage 20 and pass-through part 110 supports the pass-through part 110 in the direction of carriage 20, thus serving to ensure the locking.
  • the electromagnet 101 in the locked position do not counteract the inertial forces of the connected or the wing. He has only to apply the force required to hold the locking projection 32 in engagement, so the force to hold the recesses 111, 121 in the position not aligned. This power is for a much lower. On the other hand, this force does not or only insignificantly depends on the weights of the connected wing / s.
  • a universally deployable lock for wing systems of any kind is provided by the invention, which have a with the / n to be locked wing / n operatively connected guide or slide / n, which are thus in operative connection with this / n wing / n. Since only guide or slide rail / s are required, the lock can be independent of the respective drive mechanism of the wing system.
  • the invention is not limited to the embodiments described above. It can for example be applied to any type of sliding sash systems such as sliding door systems and the like. Furthermore, it is readily applicable to swing leaf systems, provided they are provided with a slide, for example, as part of a slide linkage. Further areas of use are, for example, windows, which are also guided on a slide rail guided by a so-called scissor arm.
  • any other cross-sectional shape is possible instead of the circular cross-sectional shape of the recesses 111, 121.
  • the cross-sectional shapes The recesses 111, 121 need not be complementary to a seen along the movement of the locking projection 32 cross-sectional shape of the locking projection 22 and not be identical to each other. For example, they can be square. Due to the non-alignment with each other of the recesses 111, 121 in the locked position of the locking projection 32 is still locked to the recess 111 at. The recess 121 of the passage member 120 is aligned in the mounting position at all times with the locking projection 32, so that it is always able to pass the recess 121 without resistance can.
  • the locking elements 30, 100 can be arranged interchanged, so that now the locking element 100 with the carriage 20, but in any case in accordance with a movement of the connected wing, is moved.
  • a locking arrangement 1 is shown, in which at one end of the support rail 10, a locking element 100 is arranged.
  • the position of the wing locked by means of the locking arrangement 1 corresponds to a closed position of this wing.
  • a further locking arrangement may be provided which is arranged in the mounting rail 10 in such a way that it locks said wing in the open position, ie serves as an open-holding device. This is useful, for example, for shops whose front door should remain open to the public.
  • the locking element 30 is placed on the front side of the receiving profile 21. But it can be just as well trained be used analogously to the locking element 100 with respect to the support rail 10 in the receiving profile 21 or inserted.
  • a motor with drive pinion can be used, which meshes with a rack, which is preferably part of the penetration part 110. This can be changed purely motor between release and blocking position. Furthermore, manual or other automatic adjustment options for the change between locking and release position are possible.

Description

Die Erfindung betrifft eine Verriegelung für Flügelanlagen, insbesondere für Schiebetüranlagen. Die DE3427609 offenbart alle Merkmale des Oberbegriffs des Anspruchs 1.The invention relates to a lock for wing systems, in particular for sliding door systems. The DE3427609 discloses all features of the preamble of claim 1.

Verriegelungen der vorgenannten Art an sich sind bekannt. In der DE 198 37 193 A1 ist eine Rastverriegelung für Kippfenster gezeigt. Ein als Rastelement dienender Führungszapfen ist in einem Langloch einer korrespondierenden Längsführung translatorisch geführt aufgenommen und ferner an einem Scherenarm eines Kippbeschlags eines zugehörigen Fensterflügels befestigt. Das Langloch endet an einem Ende in einer Endbegrenzung, die die Form eines kreisrunden Lochs aufweist, dessen Durchmesser größer ist als das Langloch breit ist. Die Längsführung ist elastisch ausgebildet. Daher ist es dem Führungszapfen möglich, entlang des Langlochs bewegt zu werden und im kreisrunden Loch arretiert zu werden, womit die Verriegelung bzw. Flügelfeststellung erreicht wird. Der Nachteil ist, dass die Verriegelung ständig wirksam ist. Ferner reibt der Führungszapfen ständig im Langloch, was zu einem erhöhten Kraftaufwand beim Bewegen des Führungszapfens in der Längsführung und zu Verschleiß führt. Zudem kann die Verriegelung nur durch Bewegen des Führungszapfens aus dem Langloch heraus aufgehoben werden. Eine Entriegelung zum expliziten Freigeben des Führungszapfens und damit des Kippfensters ist nicht vorhanden.
Aus der DE 10 2004 060 124 A1 ist eine Schiebetürverriegelung bekannt, bei der eine Art Verriegelungsglocke drehfest zu einer Antriebsscheibe eines Schiebetürantriebs angeordnet ist. Um die Antriebsscheibe ist ein endloses Zugmittel des Schiebetürantriebs geführt. Die Glocke weist an einer vorzugsweise umlaufend ausgebildeten, sich parallel zur Rotationsachse der Glocke erstreckenden Wandung Ausnehmungen auf. Ein Verriegelungsbolzen kann quer zu Rotationsachse translatorisch auf die Ausnehmungen zu bewegt und mit einer jeweiligen der Ausnehmungen in Eingriff gebracht werden. Dadurch ist eine Rotation der Glocke verhindert. Dies führt dazu, dass auch die Antriebsscheibe nicht mehr rotiert und damit die mit dem Zugmittel wirkgekuppelten Schiebetürflügel nicht mehr bewegt werden können. Der Nachteil dieser Lösung ist, dass rotierende Teile vorhanden sein müssen, um die Verriegelung bewerkstelligen zu können. Eine Anwendung beispielsweise auf andere Türanlagen ist kaum zu realisieren. Zudem ist der Aufbau relativ groß und komplex.
Aufgabe der Erfindung ist es, den vorgenannten Nachteilen zu begegnen.
Latches of the aforementioned type are known per se. In the DE 198 37 193 A1 a locking latch for tilt windows is shown. Serving as a locking element guide pin is taken in a translucent guided in a slot of a corresponding longitudinal guide and further attached to a scissor arm of a tilting fitting of an associated window sash. The slot ends at one end in an end limit, which has the shape of a circular hole whose diameter is larger than the slot is wide. The longitudinal guide is elastic. Therefore, it is the guide pin possible to be moved along the slot and locked in the circular hole, whereby the locking or wing detection is achieved. The disadvantage is that the lock is constantly effective. Furthermore, the guide pin rubs constantly in the slot, resulting in an increased force when moving the guide pin in the longitudinal guide and wear. In addition, the lock can be lifted only by moving the guide pin out of the slot out. An unlocking for explicit release of the guide pin and thus the tilting window is not present.
From the DE 10 2004 060 124 A1 a sliding door lock is known in which a kind of locking bell is arranged rotationally fixed to a drive pulley of a sliding door drive. To the drive pulley, an endless traction means of the sliding door drive is performed. The bell instructs a preferably circumferentially formed, extending parallel to the axis of rotation of the bell wall recesses. A locking bolt can be translationally moved transversely to the axis of rotation towards the recesses and engaged with a respective one of the recesses. This prevents rotation of the bell. As a result, the drive disk no longer rotates and thus the sliding door wings which are effectively coupled with the traction means can no longer be moved. The disadvantage of this solution is that rotating parts must be present in order to accomplish the locking can. An application, for example, to other door systems is hard to realize. In addition, the structure is relatively large and complex.
The object of the invention is to counteract the aforementioned disadvantages.

Diese Aufgabe wird durch den Gegenstand des Anspruchs 1 gelöst. Vorteilhafte Weiterbildungen der Erfindung sind in den Unteransprüchen angegeben.
Eine erfindungsgemäße Vorrichtung zum Verriegeln zumindest eines Flügels einer Flügelanlage weist ein erstes Verriegelungselement und ein zweites Verriegelungselement auf. Das erste Verriegelungselement umfasst an einem Ende ein erstes Rastelement. Das zweite Verriegelungselement umfasst an einem dem ersten Rastelement zugewandten Ende ein zweites Rastelement. Dieses zweite Rastelement ist gestaltet, in Verriegelungsstellung mit dem ersten Rastelement rastend in Wirkeingriff gebracht zu werden. Das zweite Verriegelungselement ist zudem eingerichtet, in Bezug auf die Flügelanlage ortsfest angeordnet zu werden. Das erste Verriegelungselement hingegen ist eingerichtet, in Bezug auf den zumindest einen Flügel derart angeordnet zu werden, dass das erste Verriegelungselement bei einer Bewegung des zumindest einen Flügels mit dieser Bewegung korrespondierend derart bewegt wird, dass das erste Verriegelungselement je nach Bewegungsrichtung des zumindest einen Flügels translatorisch in eine Verriegelungsstellung auf das zweite Verriegelungselement zu bzw. in eine Entriegelungsstellung von dem zweiten Verriegelungselement weg bewegt wird. D. h. das erste Verriegelungselement wird aufgrund einer Flügelbewegung ebenfalls bewegt, wohingegen das zweite Verriegelungselement hinsichtlich der gesamten Flügelanlage an ein und derselben Stelle verbleibt. Eines der Verriegelungselemente umfasst zudem ein Aktivierungselement, das bei Betätigung den rastenden Wirkeingriff zwischen dem ersten Rastelement und dem zweiten Rastelement gemäß einer Sperrstellung ermöglicht oder gemäß einer Freigabestellung verhindert. D. h. das Aktivierungselement bewirkt ein Scharf- oder Abschalten der so gebildeten Flügelverriegelung. Das translatorische Bewegen des ersten Verriegelungselements ermöglicht, die Verrieglungsvorrichtung in jede Art von Flügelanlage integrieren zu können, die über ein translatorisch bewegtes Teil verfügt, das vom jeweiligen Flügel (mit)bewegt wird, oder die in sonstiger Weise in der Lage ist, über die Flügelbewegung ein Teil translatorisch (mit) zu bewegen. Diese Lösung ist also völlig unabhängig von der Art eines etwaig vorhandenen Flügelbetätigers, der in der Lage ist, den jeweiligen Flügel in zumindest eine Richtung zu bewegen. D. h. diese Lösung ist auch bei rein manuell betriebenen Flügelanlagen einsetzbar. Zudem ist diese Lösung leicht in Flügelanlagen integrierbar.
This object is solved by the subject matter of claim 1. Advantageous developments of the invention are specified in the subclaims.
A device according to the invention for locking at least one wing of a wing system has a first locking element and a second locking element. The first locking element comprises at one end a first latching element. The second locking element comprises at a first locking element facing the end of a second locking element. This second latching element is designed to be latchingly engaged in the locking position with the first latching element. The second locking element is also adapted to be fixed in relation to the wing system. The first locking element, however, is arranged to be arranged with respect to the at least one wing such that the first locking element upon movement of the at least one wing with this Movement is correspondingly moved such that the first locking element is moved depending on the direction of movement of the at least one wing translationally in a locking position on the second locking element to or in an unlocked position of the second locking element. Ie. the first locking element is also moved due to a wing movement, whereas the second locking element remains in one and the same place with respect to the entire wing system. One of the locking elements also includes an activation element that allows the latching operative engagement between the first locking element and the second locking element according to a locking position or prevented according to a release position upon actuation. Ie. the activation element causes an arming or switching off the wing lock thus formed. The translational movement of the first locking element makes it possible to integrate the locking device in any type of wing system, which has a translationally moving part, which is moved by the respective wing, or which is otherwise capable of, via the wing movement a part translatorisch (to move). This solution is thus completely independent of the type of any existing Flügelbetätigers who is able to move the respective wing in at least one direction. Ie. This solution can also be used in purely manually operated wing systems. In addition, this solution is easy to integrate in wing systems.

Vorzugsweise ist das zweite Verriegelungselement gestaltet, im Bereich oder in einer Aufnahmenut eines in Bezug auf die Flügelanlage oder den jeweiligen Flügel ortsfest angeordneten Führungsteils ortsfest angebracht zu werden. Dies erlaubt eine einfache Integration des zweiten Verriegelungselements. Es ist nämlich dadurch möglich, das erste Verriegelungselement einfach in die Aufnahmenut translatorisch bewegbar einzusetzen. Es kann dann beispielsweise die Funktion eines Gleitstücks übernehmen. Damit ergibt sich der Vorteil, dass der für die so gebildete Verriegelungsanordnung benötigte Platz auf ein Minimum beschränkt werden kann.Preferably, the second locking element is designed to be fixedly mounted in the region or in a receiving groove of a stationary with respect to the wing system or the respective wing arranged guide member. This allows easy integration of the second locking element. It is in fact possible, simply insert the first locking element in the receiving groove translationally movable. It can then assume the function of a slider, for example. This results in the advantage that the space required for the locking arrangement thus formed can be kept to a minimum.

Das erste oder das zweite Rastelement weist einen Rastvorsprung auf, demzufolge das jeweils andere Rastelement ein mit diesem Rastvorsprung korrespondierendes Rastteil aufweist. Geeignete Rastteile sind wiederum ein Rastvorsprung oder eine Rastausnehmung.The first or the second latching element has a latching projection, according to which the respective other latching element has a locking part corresponding to this latching projection. Suitable locking parts are in turn a latching projection or a recess.

Das Rastteil umfasst ein erstes Durchgriffsteil, das eine Ausnehmung aufweist, die der nachstehend erläuterten Verrastung dient. Durchgriffsteil bedeutet dabei, dass der Rastvorsprung zum Zwecke des Verriegelns besagten Flügels diese Rastausnehmung durchgreift. Die Rastausnehmung ist im ersten Durchgriffsteil durchgehend ausgebildet. Sie ist ferner in einem rechten Winkel zum translatorischen Bewegungsweg des Rastvorsprungs derart bewegbar, dass die Rastausnehmung in der Freigabestellung so angeordnet ist, dass sich der Rastvorsprung entlang seines translatorischen Bewegungswegs durch die Rastausnehmung hindurch bewegen kann. Sie ist in Sperrstellung also so angeordnet, dass der Rastvorsprung, sofern er in Verriegelungsstellung die Rastausnehmung durchgreift, an einer Bewegung in eine Richtung von der ersten Rastausnehmung weg in Richtung Verriegelungselement zumindest bis zu einem vorbestimmten Maß gehindert ist und damit rastend mit der Rastausnehmung diese hintergreifend in Wirkeingriff steht. Die Rastausnehmung erstreckt sich entlang der Bewegungsrichtung des zweiten Verriegelungselements, weist also in Richtung Rastvorsprung, sodass sich dieser mit einem bestimmten Maß durch die Rastausnehmung hindurch bewegen und sie somit durchgreifen kann. Die Rastausnehmung ist in Freigabestellung so angeordnet, dass sich der Rastvorsprung entlang seines translatorischen Bewegungswegs durch sie hindurch frei hin- und her bewegen kann. Erfindungsgemäß umfasst das Rastteil ferner ein zweites Durchgriffsteil, das an einer dem Rastvorsprung zugewandten Seite des ersten Durchgriffsteils angeordnet ist. Es weist ähnlich dem ersten Durchgriffsteil ebenfalls eine Ausnehmung auf, die im zweiten Durchgriffsteil durchgehend ausgebildet ist. Sie ist in Bezug auf das zweite Verriegelungselement derart ortsfest angeordnet, dass sich der Rastvorsprung entlang seines translatorischen Bewegungswegs durch die Ausnehmung hindurch frei hin- und her bewegen kann. D. h. diese Ausnehmung dient nicht der Verriegelung sondern beispielsweise als Anschlag für das erste Verriegelungselement. In Sperrstellung sind die Ausnehmungen der Durchgriffsteile also so zueinander angeordnet, dass der Rastvorsprung, sofern er beide Ausnehmungen durchgreift, an einer Bewegung in eine Richtung von der Rastausnehmung weg in Richtung Ausnehmung des zweiten Durchgriffsteils zumindest bis zu einem vorbestimmten Maß gehindert ist und damit rastend mit der Rastausnehmung in Wirkeingriff steht. D. h. die Ausnehmungen nehmen in Freigabe- und Sperrstellung zueinander jeweils verschiedene Positionen ein. Durch diese Maßnahme ist es möglich, das Freigeben bzw. Sperren des Rastvorsprungs ausschließlich mittels zweier sehr einfach und kostengünstig herzustellender Strukturen, beispielsweise mittels Durchgangsbohrungen als Ausnehmungen, auszubilden.The latching part comprises a first pass-through part which has a recess which serves for the latching explained below. Pass-through part means that the latching projection for the purpose of locking said wing passes through this latching recess. The latching recess is formed continuously in the first pass-through part. It is also movable at a right angle to the translatory movement path of the latching projection such that the latching recess is arranged in the release position so that the latching projection can move along its translatory movement path through the latching recess. It is so arranged in blocking position so that the locking projection, if he engages in the locking position, the recess is prevented from moving from the first recess towards locking element at least to a predetermined extent and thus latching with the locking recess engages behind is in operative engagement. The latching recess extends along the direction of movement of the second locking element, that is to say in the direction of the latching projection, so that it can move through the latching recess with a certain extent and thus be able to pass through it. The Locking recess is arranged in the release position so that the locking projection along its translational movement path can freely move back and forth through it. According to the invention, the latching part further comprises a second pass-through part, which is arranged on a latching projection facing side of the first pass-through part. It likewise has a recess, similar to the first penetration part, which recess is continuous in the second penetration part. It is stationary in relation to the second locking element arranged such that the locking projection along its translational movement path through the recess can move freely back and forth. Ie. this recess is not the lock but for example as a stop for the first locking element. In the blocking position, the recesses of the Durchgriffsteile are thus arranged to each other that the locking projection, if he passes through both recesses, is prevented from moving from the recess to a recess in the direction of the second passage portion at least to a predetermined extent and thus detent with the latching recess is in operative engagement. Ie. the recesses take each other different positions in release and blocking position. By this measure, it is possible, the release or locking of the locking projection exclusively by means of two very simple and inexpensive to manufacture structures, for example by means of through holes as recesses, form.

Vorzugsweise liegen die Durchgriffsteile aneinander an. Dies hat den Vorteil, dass das zweite Durchgriffsteil als Abstützung für das erste Durchgriffsteil dienen kann und somit die Verriegelungswirkung des vorgenannten Rastvorsprungs bzw. die Verriegelungsstabilität des ersten Verriegelungselements erhöht.Preferably, the pass-through parts abut each other. This has the advantage that the second penetration part can serve as a support for the first penetration part and thus increases the locking action of the aforementioned locking projection and the locking stability of the first locking element.

Vorzugsweise weist die Ausnehmung des jeweiligen Durchgriffsteils eine, in Bewegungsrichtung des Rastvorsprungs gesehen, zur Außenkontur ebenjenen Rastvorsprungs im Wesentlichen komplementäre Innenkontur auf.Preferably, the recess of the respective penetration part has a, seen in the direction of movement of the latching projection, to the outer contour ebenjenen latching projection substantially complementary inner contour.

Die Durchgriffsteile weisen vorzugsweise jeweils einen Abschnitt auf, die zueinander parallel verlaufen und plattenartig ausgebildet sind. Die plattenartige Ausbildung der Durchgriffsteile ermöglicht, quer zur Bewegungsrichtung des Rastvorsprungs gesehen, eine sehr ökonomische Raumausnutzung.The penetration parts preferably each have a portion which extend parallel to each other and are plate-like. The plate-like design of the Durchgriffsteile allows, seen transversely to the direction of movement of the locking projection, a very economical space utilization.

Liegen die plattenartigen Abschnitte auch noch aneinander an, wird das zweite Verriegelungselement, entlang der Bewegungsrichtung des Rastvorsprungs gesehen, sehr kurz und damit platzsparend.If the plate-like sections also still abut each other, the second locking element, seen along the direction of movement of the locking projection, is very short and thus saves space.

Der Rastvorsprung ist an seinem der Rastausnehmung zugewandten Ende in Richtung Rastausnehmung weisend vorzugsweise verjüngend, weiterhin vorzugsweise pilzkopfartig ausgebildet. Dadurch ist es möglich, den Rastvorsprung auch durch die Ausnehmungen der Durchgriffsteile hindurch bis zum vorgenannten Wirkeingriff zu schieben, selbst wenn sich diese bereits in Sperrstellung befinden. Der Rastvorsprung kann zudem so gestaltet sein, dass der Rastvorsprung unter Überwindung der durch den Wirkeingriff mit der Rastausnehmung entstehenden Halte- bzw. Verriegelungskraft auch in die entgegengesetzte Bewegungsrichtung aus der Rastausnehmung heraus bewegt werden kann. D. h. mit einem derartigen Rastvorsprung ist auf sehr einfache und kostengünstige Weise eine Flügelverriegelung mit Überlastsicherung realisierbar.The latching projection is preferably tapering at its end facing the latching recess in the direction of the latching recess, and is furthermore preferably mushroom-shaped. This makes it possible to push the locking projection through the recesses of the Durchgriffsteile through to the aforementioned operative intervention, even if they are already in the locked position. The latching projection can also be designed so that the latching projection can be moved out of the latching recess by overcoming the locking or locking force produced by the operative engagement with the latching recess and also in the opposite direction of movement. Ie. With such a locking projection is a very simple and inexpensive way a wing lock with overload protection feasible.

Das vorgenannte Aktivierungselement ist vorzugsweise mittels eines Elektromagneten gebildet, der bei Betätigung das erste Durchgriffsteil in Freigabe- bzw. in Sperrstellung bewegt. Der Elektromagnet bietet den Vorteil definierter Arbeitsstellungen (Verriegelung, Entriegelung) der Verriegelungsanordnung und kann zudem einfach über dessen Bestromung an gewünschte Halte- bzw. Verriegelungskräfte angepasst werden. Beispielsweise kann gepulster Strom verwendet werden.
Vorzugsweise weist zumindest eines der Verriegelungselemente an einer dem jeweils anderen Verriegelungselement zugewandten Seite einen Anschlag für das jeweils andere Verriegelungselement auf. Damit ist auf einfache Weise eine Begrenzung für den Rastvorsprung bei seiner Bewegung in Richtung korrespondierendes Rastelement realisierbar.
The aforementioned activation element is preferably formed by means of an electromagnet which, when actuated, the first penetration part in Release or moved in locked position. The electromagnet has the advantage of defined working positions (locking, unlocking) of the locking arrangement and can also be easily adapted via the energization of desired holding or locking forces. For example, pulsed current can be used.
Preferably, at least one of the locking elements on a side facing the respective other locking element on a stop for the respective other locking element. This is easily a limitation for the locking projection during its movement in the direction of corresponding locking element feasible.

Das zweite Verriegelungselement ist eingerichtet, in Bezug auf eine Führungs- oder Gleitschiene der Flügelanlage ortsfest angeordnet zu werden. Das erste Verriegelungselement kann in dem Fall ebenfalls in der Führungs- oder Gleitschiene unmittelbar oder mittelbar translatorisch auf das zweite Verriegelungselement zu und von diesem weg bewegbar geführt aufgenommen sein. Dies erlaubt eine elegante und im Extremfall völlig unsichtbare Integration des zweiten Verriegelungselements unter Nutzung der ohnehin vorhandenen Führungs- oder Gleitschiene. Es werden somit Teile bereits vorhandener Flügelanlagen mit genutzt. Ferner ergibt dies sowohl platztechnische als auch optische Vorteile, da das zweite Verriegelungselement optisch versteckt werden kann.The second locking element is adapted to be fixed in relation to a guide or slide rail of the wing system. The first locking element can also be accommodated in the guide or slide rail directly or indirectly in a translatory manner on the second locking element to and away from it. This allows an elegant and in the extreme case completely invisible integration of the second locking element using the already existing guide or slide rail. Thus, parts of already existing wing systems are used. Furthermore, this results in both space-technical and optical advantages, since the second locking element can be hidden optically.

Das zweite Verriegelungselement ist eingerichtet, an oder in der Führungs- oder Gleitschiene ortsfest angebracht zu werden. Dies hat den Vorteil, dass lediglich an bzw. in dieser Schiene entsprechende Befestigungsmöglichkeiten vorkommen müssen. Zudem sind am Flügel bzw. anderen Teilen der Flügelanlage keine Bearbeitungen notwendig, was einerseits die Montage bzw. Nachrüstung erleichtert, andererseits aber auch einen optisch spurlosen Rückbau ermöglicht. Die Flügelanlage weist somit zumindest einen bewegbaren Flügel, zumindest eine in Bezug auf die Flügelanlage oder den zumindest einen bewegbaren Flügel ortsfest angeordnete Führungs- oder Gleitschiene mit einer Aufnahmenut und zumindest eine der vorbeschriebenen Verriegelungsvorrichtungen auf.
Die Flügelanlage umfasst vorzugsweise zumindest einen als Schwenkflügel ausgebildeten Flügel. Dieser Flügel ist über ein Gleitgestänge mit einem Schwenkflügelbetätiger, also einem Schwenkflügelantrieb oder Türschließer wirkverbunden. D. h. die Flügelanlage verfügt über eine Gleitschiene, in der ein Gleitstück translatorisch geführt aufgenommen ist, das seinerseits frei rotierbar am Gleitarm des Gestänges angelenkt ist. Das erste Verriegelungselement kann Teil des Gleitstücks sein oder dieses ersetzen.
Alternativ oder zusätzlich weist die Flügelanlage zumindest einen als Schiebe(tür)flügel ausgebildeten Flügel auf. Derartige Flügel sind in der Regel in oberhalb des jeweiligen Flügels angeordneten Trag- und/oder Führungsschienen aufgehängt bzw. entlang ihres Bewegungswegs geführt. Die Tragschiene kann im Rahmen der Erfindung somit zusätzlich der unmittelbaren oder mittelbaren Führung des zweiten Verriegelungselements beispielsweise über einen mit dem Flügel wirkverbundenen Laufwagen dienen. D. h. auch in Schiebeanlagen wie Schiebetüren, Faltflügeltüren, Trennwänden und dergleichen ist die vorbeschriebene Verriegelungsanordnung sehr einfach und vorzugsweise für Benutzer unsichtbar integrierbar.
The second locking element is adapted to be fixedly mounted on or in the guide or slide rail. This has the advantage that only on or in this rail appropriate mounting options must occur. In addition, no edits are necessary on the wing or other parts of the wing system, on the one hand the assembly or retrofitting facilitates, on the other hand, but also allows a visually-traced decommissioning. The wing system thus has at least one movable wing, at least one with respect to the wing system or the at least one movable wing fixedly arranged guide or slide rail with a receiving groove and at least one of the above-described locking devices.
The wing system preferably comprises at least one wing designed as a pivoting wing. This wing is operatively connected via a slide linkage with a Schwenkflügelbetätiger, so a swing door drive or door closer. Ie. the wing system has a slide, in which a slider is added translationally guided, which in turn is freely rotatably articulated on the sliding arm of the linkage. The first locking element may be part of or replace the slider.
Alternatively or additionally, the wing system has at least one wing designed as a sliding (door) wing. Such wings are usually suspended above the respective wing arranged support and / or guide rails or guided along their path of movement. In the context of the invention, the mounting rail can thus additionally serve for the direct or indirect guidance of the second locking element, for example via a carriage operatively connected to the wing. Ie. Also in sliding systems such as sliding doors, folding doors, partitions and the like, the above-described locking arrangement is very simple and preferably invisible to the user integrated.

Weitere Merkmale und Vorteile der Erfindung ergeben sich aus der nachfolgenden Beschreibung bevorzugter Ausführungsformen.Further features and advantages of the invention will become apparent from the following description of preferred embodiments.

Es zeigen:

Figur 1
eine Verriegelungsanordnung gemäß einer Ausführungsform der Erfindung in Entriegelungsstellung,
Figur 2
die Verriegelungsanordnung von Figur 1 in Verriegelungsstellung und im Schnitt entlang einer Linie A - A in Figur 1 aus einer anderen Perspektive,
Figur 3
das Verriegelungselement von Figur 1 und Figur 2 in größerem Detail, gemäß einer ersten Ausführungsform der Erfindung,
Figur 4
ein Verriegelungselement gemäß einer zweiten Ausführungsform der Erfindung und
Figur 5
ein Verriegelungselement gemäß einer dritten Ausführungsform der Erfindung.
Show it:
FIG. 1
a locking arrangement according to an embodiment of the invention in the unlocked position,
FIG. 2
the locking arrangement of FIG. 1 in locking position and in section along a line A - A in FIG. 1 from a different perspective,
FIG. 3
the locking element of FIG. 1 and FIG. 2 in greater detail, according to a first embodiment of the invention,
FIG. 4
a locking element according to a second embodiment of the invention and
FIG. 5
a locking element according to a third embodiment of the invention.

Figur 1 zeigt eine Verriegelungsanordnung 1 gemäß einer Ausführungsform der Erfindung. Die Anordnung 1 umfasst exemplarisch eine Tragschiene 10 einer beispielhaften Schiebetüranlage. Die Schiebetüranlage ist im gezeigten Beispiel linearmotorbasiert. Die Tragschiene 10 dient im gezeigten Beispiel in einem Aufnahmeabschnitt 11 zumindest der Aufnahme eines hier nicht dargestellten Stators des Linearmotors. Ein anderer, davon separiert ausgebildeter Aufnahmeabschnitt 12 dient hauptsächlich der geführten Aufnahme vorzugsweise von Laufwagen 20 eines hier nicht dargestellten Schiebeflügels. Der Schiebeflügel ist über vorgenannte Laufwagen 20 in der Tragschiene 10 geführt aufgenommen. FIG. 1 shows a locking arrangement 1 according to an embodiment of the invention. The arrangement 1 comprises by way of example a mounting rail 10 of an exemplary sliding door system. The sliding door system is linear motor based in the example shown. The support rail 10 is used in the example shown in a receiving portion 11 at least the inclusion of a stator, not shown here of the linear motor. Another, separately formed receiving portion 12 is mainly used for guided recording preferably of carriage 20 one here not shown sliding sash. The sliding sash is received in the support rail 10 via aforementioned carriages 20.

Dazu weist der Laufwagen 20 exemplarisch ein Aufnahmeprofil 21 auf, das nach unten, d. h. in Richtung Flügel, offen ist. Diese Öffnung dient dem Durchführen eines jeweiligen Mitnehmers 23, der das Aufnahmeprofil 21 mit besagtem Flügel diesen mitnehmend wirkverbindet. In das Aufnahmeprofil 21 ist ein Läufer 22 eingesetzt, der im gezeigten Beispiel eine Reihe von Permanentmagneten aufweist. Der Läufer 22 tritt mit dem Stator in bekannter Weise in magnetische Wechselwirkung.For this purpose, the carriage 20 by way of example a receiving profile 21, the down, d. H. towards the wing, open. This opening serves to carry out a respective driver 23, which actively connects the receiving profile 21 with said wing. In the receiving profile 21, a rotor 22 is used, which has a series of permanent magnets in the example shown. The rotor 22 enters the stator in a known manner in magnetic interaction.

Am hier linken Ende des Laufwagens 20 bzw. dessen Aufnahmeprofils 21 ist ein Verriegelungselement 30 ortsfest angebracht. Vorzugsweise ist das Verriegelungselement 30 mittels eines Anschlagabschnitts 31 stirnseitig an oder in das Profil 21 angesetzt. An der dem Profil 21 abgewandten Seite schließt sich an den Anschlagabschnitt 31 ein Schaft 33 an, an dessen freiem Ende ein vorzugsweise plizkopfartiger Rastvorsprung 32 ausgebildet ist. D. h. der Rastvorsprung 32 verjüngt sich in Richtung dessen freien Endes. Der Schaft 33 hat einen geringeren Durchmesser als ein maximaler Außendurchmesser des Rastvorsprungs 32. Anschlagabschnitt 31, Schaft 33 und Rastvorsprung 32 sind aneinander befestigt oder teilweise bzw. in der Gesamtheit einstückig ausgebildet.At the left end of the carriage 20 and its receiving profile 21, a locking member 30 is fixedly mounted. Preferably, the locking element 30 is attached by means of a stop portion 31 on the front side or in the profile 21. On the side facing away from the profile 21, a shaft 33 connects to the stop portion 31, at the free end of a preferably plizkopfartiger locking projection 32 is formed. Ie. the locking projection 32 tapers in the direction of its free end. The shaft 33 has a smaller diameter than a maximum outer diameter of the latching projection 32. Stopping section 31, shaft 33 and latching projection 32 are fastened to each other or formed integrally in part or in the entirety.

Vorzugsweise im Bereich der linken Stirnseite der Tragschiene 10 befindet sich ein Verriegelungselement 100. Das Verriegelungselement 100 weist einen Befestigungsabschnitt 102 auf, der beispielsweise klemmend in der Tragschiene 10 bzw. in deren Aufnahmeabschnitt 12 aufgenommen ist. Es sind jedoch alle anderen Befestigungsmöglichkeiten wie Schrauben, Verrasten, Schweißen, Verkleben und dergleichen denkbar.Preferably, in the region of the left end side of the support rail 10 is a locking element 100. The locking element 100 has a mounting portion 102 which is received, for example, by clamping in the support rail 10 and in its receiving portion 12. However, all other mounting options such as screws, locking, welding, gluing and the like are conceivable.

Figur 2 zeigt die Verriegelungsanordnung 1 von Figur 1 im Schnitt entlang einer Linie A - A in Figur 1. FIG. 2 shows the locking arrangement 1 of FIG. 1 in section along a line A - A in FIG. 1 ,

Das Verriegelungselement 100 umfasst zwei so genannte Durchgriffsteile 110, 120. Die Funktion dieser Teile wird später näher erläutert. Das Durchgriffsteil 110 weist vorzugsweise mittig liegend eine Ausnehmung 111 auf, die im gezeigten Beispiel als kreisrundes Durchgangsloch ausgebildet ist und sich entlang der Bewegungsrichtung des Rastvorsprungs 32, also hier entlang der Längserstreckung der Tragschiene 10 bzw. des Profils 20 erstreckt. Das Durchgriffsteil 110 ist quer zur Bewegungsrichtung des Rastvorsprungs 32 bzw. des Laufwagens 20, d. h. schräg nach rechts unten in Figur 2, translatorisch bewegbar geführt.The locking element 100 comprises two so-called pass-through parts 110, 120. The function of these parts will be explained later. The penetration part 110 preferably has centrally a recess 111, which is formed in the example shown as a circular through hole and extends along the direction of movement of the locking projection 32, ie here along the longitudinal extent of the support rail 10 and the profile 20. The penetration part 110 is transversely to the direction of movement of the locking projection 32 and the carriage 20, ie obliquely to the bottom right in FIG. 2 , guided translationally movable.

Am dem Rastvorsprung 32 abgewandten Ende weist das Verriegelungselement 100 ferner ein Aktivierungselement hier in Form eines Elektromagneten 101 auf. Der Elektromagnet 101 wirkt mit einer hier teilweise sichtbaren Ankerplatte 113 des Durchgriffsteils 110 magnetisch zusammen. Der Elektromagnet 101 ist so angeordnet, dass er bei Bestromung die Ankerplatte 113 schräg nach rechts unten quer zur Bewegungsrichtung des Rastvorsprungs 32 bzw. entlang der Bewegungsrichtung des Durchgriffsteils 110 anzieht.At the end remote from the latching projection 32, the locking element 100 also has an activating element here in the form of an electromagnet 101. The electromagnet 101 interacts magnetically with a here partially visible armature plate 113 of the penetration part 110. The electromagnet 101 is arranged so that it attracts the armature plate 113 obliquely to the bottom right transversely to the direction of movement of the locking projection 32 and along the direction of movement of the penetration part 110 when energized.

Die Ankerplatte 113 ist am Durchgriffsteil 110 befestigt bzw. einstückig mit ihm ausgebildet. Durchgriffsteil 110 und Ankerplatte 113 schließen vorzugsweise einen Winkel von etwa 90° ein. D. h. das Durchgriffsteil 110 wird schräg nach rechts unten bewegt, sobald der Elektromagnet 101 die Ankerplatte 113 bei einem Bestromen anzieht.The anchor plate 113 is fixed to the penetration part 110 or formed integrally with it. Penetration part 110 and anchor plate 113 preferably include an angle of about 90 °. Ie. the penetration part 110 is moved obliquely down to the right as soon as the electromagnet 101 attracts the anchor plate 113 during energization.

Die Anbringung des Verriegelungselements 100 erfolgt mittels des vorgenannten, Befestigungsabschnitts 102, der vorzugsweise klemmend in der Tragschiene 10 aufgenommen ist. Es sind jedoch alle anderen Befestigungsmöglichkeiten wie Schrauben, Verrasten, Schweißen, Verkleben und dergleichen denkbar. Der Elektromagnet 101 ist hier mittels Schrauben 105, von denen eine sichtbar ist, am Befestigungsabschnitt 102 ortsfest angebracht.The attachment of the locking element 100 by means of the aforementioned, fastening portion 102, which is preferably clamping in the Support rail 10 is added. However, all other mounting options such as screws, locking, welding, gluing and the like are conceivable. The solenoid 101 is fixedly attached to the mounting portion 102 by means of screws 105, one of which is visible.

Die Verriegelungsanordnung 1 ist in einer so genannten Verriegelungsstellung dargestellt. D. h. der Rastvorsprung 32 befindet sich mit den Durchgriffsteilen 110, 120 in Eingriff und hintergreift das Durchgriffsteil 110. Wie zu erkennen, durchgreifen der Rastvorsprung 32 und damit auch der Schaft 33 die Durchgriffsteile 110, 120 bzw. deren Ausnehmungen 111, 121, von denen hier nur die Ausnehmung 111 des Durchgriffsteils 110 deutlich sichtbar ist. D. h. die Durchgriffsteile 110, 120 sind zwischen Rastvorsprung 32 und Anschlagabschnitt 31 angeordnet.The locking arrangement 1 is shown in a so-called locking position. Ie. the latching projection 32 is engaged with the through-engagement parts 110, 120 and engages behind the passage portion 110. As can be seen, the latching projection 32 and therefore also the shaft 33 pass through the passage portions 110, 120 or their recesses 111, 121, of which only here the recess 111 of the penetration part 110 is clearly visible. Ie. the passage portions 110, 120 are arranged between locking projection 32 and abutment portion 31.

Der dargestellte Blockpfeil stellt die Bewegungsrichtung des Läufers 22 bzw. des Laufwagens 20 und damit des Verriegelungselements 100 und des Rastvorsprungs 33 dar. Damit ist der damit verbundene Laufwagen 20 daran gehindert, sich vom Verriegelungselement 100 zu lösen, also schräg nach links unten in Figur 2 zu bewegen. Dadurch ist selbstverständlich der mit dem Laufwagen 20 wirkverbundene Flügel ebenfalls an seiner Bewegung gehindert und somit verriegelt.The illustrated block arrow represents the direction of movement of the rotor 22 or of the carriage 20 and thus of the locking element 100 and the latching projection 33. Thus, the carriage 20 connected thereto is prevented from disengaging from the locking element 100, ie obliquely to the bottom left in FIG FIG. 2 to move. As a result, of course, the operatively connected to the carriage 20 wings also prevented from moving and thus locked.

Der Anschlagabschnitt 31 liegt in der gezeigten Stellung vorzugsweise press am Durchgriffsteil 120 an. Es kann jedoch auch vorgesehen sein, dass der Schaft 33 länger ausgebildet ist, so dass sich der Anschlagabschnitt 31 um einen gewissen Weg vom Durchgriffsteil 120 entfernen kann. Dies hat den Vorteil, dass beispielsweise durch Temperaturschwankungen hervorgerufene Änderungen an der Anlage ausgeglichen werden können.The stopper portion 31 is preferably in the position shown on the press-through member 120 at. However, it can also be provided that the shaft 33 is longer, so that the stopper portion 31 can move away from the penetration part 120 by a certain distance. This has the advantage that, for example, caused by temperature fluctuations changes to the system can be compensated.

Ferner sind die Aufnahmeabschnitte 11, 12 hier für das Profil 21 und den hier ebenfalls nicht dargestellten Stator des Linearmotors abgebildet. Die Aufnahmeabschnitte 11, 12 werden mittels einander zugewandter, hervorstehender Vorsprünge 13 an bzw. in der Tragschiene 10 voneinander separiert. Die dem Flügel abgewandten Flächen der Vorsprünge 13 dienen als Auflagefläche für den Stator. Die dem Flügel zugewandten Flächen der Vorsprünge 13 dienen vorzugsweise als Auflagefläche für den Befestigungsabschnitt 102 des Verriegelungselements 100. Zudem können die Vorsprünge 13 an ihrer dem Profil 21 zugewandten Flächen als Lauffläche für nicht sichtbare Laufrollen des Laufwagens 20 dienen. Dies ist insbesondere sinnvoll, da dadurch sichergestellt ist, dass zwischen Läufer 22 bzw. Aufnahmeprofil 21 und Stator immer ein vorbestimmter Abstand eingehalten ist, sodass die magnetische Antriebskraft des so gebildeten Linearmotors gewährleistet ist. An der dem nicht dargestellten Flügel zugewandten Seite weist die Tragschiene 10 ferner Vorsprünge 14 auf, die ähnlich den Vorsprüngen 13 einander zugewandt hervorstehend ausgebildet sind. Die Vorsprünge 14 können an ihren dem Flügel abgewandten Seiten ebenfalls als Lauffläche für entsprechende Laufrollen des Laufwagens 20 dienen. Die Vorsprünge 13, 14 dienen somit vorzugsweise dem Positionieren des jeweiligen Laufwagens 20 in der Tragschiene 10.Further, the receiving portions 11, 12 are shown here for the profile 21 and the stator of the linear motor, also not shown here. The receiving portions 11, 12 are separated by means of mutually facing, protruding projections 13 on or in the mounting rail 10 from each other. The wings facing away from the surfaces of the projections 13 serve as a support surface for the stator. The wings of the facing surfaces of the projections 13 are preferably used as a support surface for the mounting portion 102 of the locking element 100. In addition, the projections 13 on its profile 21 facing surfaces can serve as a running surface for non-visible rollers of the carriage 20. This is particularly useful because it ensures that between rotor 22 and recording profile 21 and stator is always maintained a predetermined distance, so that the magnetic driving force of the linear motor thus formed is ensured. At the side facing the wing, not shown, the support rail 10 also has projections 14, which are similar to the projections 13 facing each other protruding. The projections 14 may also serve as a running surface for corresponding rollers of the carriage 20 on their sides facing away from the wing. The projections 13, 14 are thus preferably used to position the respective carriage 20 in the mounting rail 10th

Figur 3a zeigt das Verriegelungselement 100 in größerem Detail und gemäß einer ersten Ausführungsform der Erfindung. Das Verriegelungselement 100 ist in einer so genannten Sperrstellung gezeigt, die die vorgenannte Verriegelungsstellung ermöglicht. Die Ankerplatte 113 weist ein stiftartiges Teil 114 auf. Das Teil 114 ist vorzugsweise durch die Ankerplatte 113 hindurchgehend ausgebildet. Dadurch ist es möglich, beispielsweise eine Schraubenfeder 106 als Rückstellelement zwischen Ankerplatte 113 und Elektromagnet 101 anzuordnen. Die Rückstellfeder 106 bewirkt, wenn der Elektromagnet 101 nicht bestromt wird, dass die Ankerplatte 113 in eine Freigabestellung bewegt wird, die hier nicht dargestellt ist. Zudem kann das Teil 114 an seinem dem Elektromagnet 101 entfernten Ende zum Anschluss eines Betätigungselements, wie eines Bowdenzugs, eines Hebels, einer Zugstange oder dergleichen genutzt werden. Dadurch ist es möglich, das Verriegelungselement 100 bzw. die Verriegelungsanordnung 1 auch im Rahmen einer Schließfolgeregelung bei einer zweiflügeligen Schwenktüranlage einzusetzen. In dem Fall dient der Elektromagnet 101 dem Festhalten des Standflügels dieser Anlage. Zum Freigeben des Rastvorsprungs 32 wird das Teil 114 mittels des vorgenannten Betätigungselements vom anderen Flügel, also dem Gangflügel, bzw. von dessen Betätiger in Freigabestellung gezogen, in der die Ausnehmungen 111, 121 vorzugsweise miteinander fluchten. FIG. 3a shows the locking member 100 in more detail and according to a first embodiment of the invention. The locking element 100 is shown in a so-called locking position, which allows the aforementioned locking position. The anchor plate 113 has a pin-like part 114. The part 114 is preferably formed through the anchor plate 113 therethrough. This makes it possible, for example, to arrange a helical spring 106 as a restoring element between armature plate 113 and electromagnet 101. The return spring 106 causes, when the solenoid 101 is not energized, that the armature plate 113th is moved to a release position, which is not shown here. In addition, the part 114 can be used at its end remote from the electromagnet 101 for connection of an actuating element, such as a Bowden cable, a lever, a pull rod or the like. This makes it possible to use the locking element 100 and the locking assembly 1 also in the context of a closing sequence control in a two-leaf swing door system. In that case, the solenoid 101 serves to hold the stationary leaf of this system. To release the locking projection 32, the part 114 is pulled by means of the aforementioned actuating element from the other wing, ie the active leaf, or by its actuator in the release position, in which the recesses 111, 121 are preferably aligned.

Wie zu erkennen, bilden Befestigungsabschnitt 102 und Durchgriffsteil 120 eine Art Montagewinkel, an dem an einer dem Flügel zugewandten Innenseite der Elektromagnet 101 hier mittels Schrauben 105 befestigt ist. Die Durchgriffsteile 110, 120 weisen im gezeigten Beispiel kreisrunde Ausnehmungen 111, 121 auf, die in der gezeigten Darstellung nicht miteinander fluchten. In der vorgenannten Freigabestellung hingegen fluchten die Ausnehmungen 111, 121 miteinander, so dass sich der Rastvorsprung 32 frei durch die Ausnehmungen 111, 121 hindurch bewegen kann und damit nicht gesperrt bzw. verriegelt werden kann. Damit befindet sich das Verriegelungselement 100 in vorgenannter Freigabestellung.As can be seen, the fastening section 102 and the penetration part 120 form a type of mounting bracket, to which the electromagnet 101 is fastened here by means of screws 105 on an inner side facing the wing. In the example shown, the passage portions 110, 120 have circular recesses 111, 121 which are not aligned with one another in the illustration shown. In the aforementioned release position, however, the recesses 111, 121 are aligned with each other, so that the locking projection 32 can move freely through the recesses 111, 121 and thus can not be locked or locked. Thus, the locking element 100 is in the aforementioned release position.

Ist eine Verriegelung des vorgenannten Rastvorsprungs 32 gewünscht, werden der Elektromagnet 101 bestromt, die Ankerplatte 113 magnetisch angezogen und damit das Durchgriffsteil 110 in die in Figur 3a gezeigte Stellung bewegt. Die vorgenannte, sich verjüngende Ausbildung des Rastkopfes bzw. Rastvorsprungs 32 ermöglicht in dieser Stellung, dass dieser sowohl die Ausnehmung 121 als auch die Ausnehmung 111 überwinden kann und mit der Ausnehmung 111 rastend in den Eingriff gelangen kann. D. h. der Rastvorsprung 32 hintergreift in Verriegelungsstellung aufgrund der nicht miteinander fluchtenden Anordnung der Ausnehmungen 111, 121 zueinander die Ausnehmung 111 und kann nicht oder nur in geringfügigem Maß in Richtung wieder heraus aus den Ausnehmungen 111, 121 bewegt werden. Damit entsteht eine sehr einfache und doch wirksame Verriegelung des bzw. der angeschlossenen Flügel/s.If a locking of the aforementioned locking projection 32 is desired, the electromagnet 101 is energized, the armature plate 113 magnetically attracted and thus the penetration part 110 in the in FIG. 3a shown position moves. The aforementioned, tapered design of the locking head or locking projection 32 allows in this position that this overcome both the recess 121 and the recess 111 can and can engage with the recess 111 latching into engagement. Ie. the locking projection 32 engages in the locking position due to the mismatched arrangement of the recesses 111, 121 to each other, the recess 111 and can not or only to a small extent in the direction out of the recesses 111, 121 are moved. This creates a very simple, yet effective locking of the connected wing / s.

Figur 3b zeigt das Verriegelungselement 100 in Freigabestellung. Wie zu erkennen, fluchten die Ausnehmungen 111, 121 der Durchgriffsteile 110, 120 miteinander. Zumindest sind sie so zueinander ausgerichtet, dass der nicht dargestellte Rastkopf 32 vorzugsweise ohne Widerstand durch die Ausnehmungen 111, 121 hindurch frei hin- und her bewegt werden kann. In dem Fall ist der Elektromagnet 101 vorzugsweise nicht bestromt. Die nicht dargestellte Rückstellfeder 106 drückt das Durchgriffsteil 110 in die dargestellte Freigabestellung. FIG. 3b shows the locking element 100 in the release position. As can be seen, the recesses 111, 121 of the passage portions 110, 120 are aligned with each other. At least they are aligned with each other so that the locking head 32 is not shown, preferably without resistance through the recesses 111, 121 can be freely moved back and forth. In that case, the electromagnet 101 is preferably not energized. The return spring 106, not shown, presses the penetration part 110 in the illustrated release position.

Der Elektromagnet 101 kann, wie gezeigt, stromlos öffnend bzw. den Rastvorsprung 32 freigebend ausgebildet sein. Er kann aber genauso gut stromlos schließend und damit den Rastvorsprung 32 in Verriegelungsstellung sperrend ausgebildet sein. In dem Fall ist die Ausnehmung 111 in der in Figur 3a gezeigten Arbeitsstellung des Elektromagneten 101, also wenn dieser die Ankerplatte 113 magnetisch angezogen hat, so ausgebildet, dass sie mit der Ausnehmung 121 fluchtet. Fällt die Bestromung des Elektromagneten weg, wird die Ankerplatte 113 vom Elektromagneten weg gedrängt, und die Ausnehmungen 111, 121 nehmen eine zu Figur 3a ähnliche Ausrichtung zueinander ein, fluchten also nicht mehr miteinander.The electromagnet 101 can, as shown, be designed to be normally open or the latching projection 32 to be releasing. But it can just as well normally closing and thus locking projection 32 may be formed locking in the locked position. In that case, the recess 111 in the in FIG. 3a shown working position of the electromagnet 101, that is, when it has magnetically attracted the armature plate 113, formed so that it is aligned with the recess 121. If the energization of the electromagnet away, the armature plate 113 is urged away from the electromagnet, and the recesses 111, 121 are increasing FIG. 3a similar alignment to each other, so no longer aligned with each other.

Figur 4a zeigt ein Verriegelungselement 100 gemäß einer zweiten Ausführungsform der Erfindung. Der Befestigungsabschnitt 102 ist im Querschnitt U-förmig ausgebildet und bietet so einen Aufnahmeraum für den Elektromagneten 101. Der Elektromagnet 101 ist vorzugsweise mittels Schrauben 105 am Befestigungsabschnitt 102 angebracht. Ein die beiden Schenkel 108 des U verbindender Wandabschnitt ist durch das Durchgriffsteil 120 gebildet, das hier also exemplarisch einstückig mit dem Befestigungsabschnitt 102 ausgebildet ist. Die Schenkel 108 weisen an ihren einander zugewandten Seiten Führungsabschnitte 107 hier in Form hervorstehender, zueinander offener Führungsnuten bzw. -schienen auf. In diesen Führungsabschnitten 107 ist das Durchgriffsteil 110 zwischen Sperr- und Freigabestellung bewegbar geführt aufgenommen, hier also in die Blattebene hinein und aus dieser heraus. FIG. 4a shows a locking element 100 according to a second embodiment of the invention. The attachment portion 102 is in cross section U-shaped and thus provides a receiving space for the electromagnet 101. The solenoid 101 is preferably mounted by means of screws 105 on the mounting portion 102. A wall portion connecting the two limbs 108 of the U is formed by the pass-through portion 120, which is thus embodied here as an example in one piece with the fastening portion 102. The legs 108 have on their sides facing each other guide portions 107 here in the form of protruding, mutually open guide grooves or rails on. In these guide portions 107, the pass-through part 110 is movably guided between locking and release position, in this case into and out of the plane of the page.

An der den Schenkeln 108 abgewandten Seite des Durchgriffsteils 120 schließen sich zwei in Richtung vom Elektromagneten 101 weg erstreckende, klauenartig aussehende Klemmabschnitte 109 an. D. h. jeder Klemmabschnitt 109 weist einen ersten Wandabschnitt 109a auf, der vom Durchgriffsteil 120 abgeht. Am dem Durchgriffsteil 120 abgewandten Ende des Wandabschnitts 109a schließt sich ein jeweiliger zweiter Wandabschnitt 109b an, der mit dem zugehörigen Wandabschnitt 109a vorzugsweise einen rechten Winkel einschließt. Nun am dem ersten Wandabschnitt 109a abgewandten Ende des zweiten Wandabschnitts 109b schließt sich ein jeweiliger dritter Wandabschnitt 109c an, der sich in Richtung Durchgriffsteil 120 erstreckt.On the side facing away from the legs 108 of the passage member 120, two in the direction of the electromagnet 101 away, claw-like looking clamping portions 109 close. Ie. Each clamping portion 109 has a first wall portion 109a, which extends from the penetration portion 120. At the end of the wall portion 109a facing away from the passage portion 120, a respective second wall portion 109b follows, which preferably encloses a right angle with the associated wall portion 109a. At the end of the second wall section 109b facing away from the first wall section 109a, a respective third wall section 109c, which extends in the direction of the penetration section 120, adjoins.

Die Klemmabschnitte 109 verlaufen zueinander vorzugsweise parallel. Die Wandabschnitte 109a, 109c der Klemmabschnitte 109 sind so ausgebildet, dass das Verriegelungselement 100 in den Aufnahmeabschnitt 12 der nicht abgebildeten Tragschiene 10 eingeschoben werden kann. Dabei stehen einander abgewandte Flächen 109d, 109e der Wandabschnitte 109a, 109b jeweils einem korrespondierenden der Vorsprünge 13, 14 der Tragschiene 10 gegenüber.The clamping portions 109 are preferably parallel to each other. The wall portions 109a, 109c of the clamping portions 109 are formed so that the locking element 100 can be inserted into the receiving portion 12 of the support rail 10, not shown. In this case, facing away from each other surfaces 109d, 109e of the wall sections 109a, 109b each correspond to a corresponding one of the projections 13, 14 of the mounting rail 10.

Jeder Wandabschnitt 109b weist eine nicht bezeichnete Durchgangsöffnung auf, durch die ein Verspannelement hier in Form einer jeweiligen Schraube 104 hindurchgeführt ist. Die Wandabschnitte 109a, 109b eines jeweiligen Klemmabschnitts 109 weisen zueinander zumindest bereichsweise eine Abstand a auf, der geringer als ein maximaler Außendurchmesser der Schraube 104. Die Schrauben 104 hingegen sind so ausgebildet, dass sie beim Einschrauben in Richtung Elektromagnet 101 zwischen die vorgenannten Bereiche der zugehörigen Wandabschnitte 109a, 109b mit Abstand a zueinander gelangen. Dabei wird der dritte Wandabschnitt 109c vom Wandabschnitt 109a des jeweiligen Klemmabschnitts 109 weg bewegt, sodass sich der Abstand a vergrößert. Dabei gelangen die Flächen 109c, 109d besagten Klemmabschnitts 109 mit den Vorsprüngen 13, 14 klemmend in Anlage; das Verriegelungselement 100 wird in der Tragschiene 10 verspannt bzw. verklemmt.Each wall section 109b has an unillustrated passage opening, through which a bracing element is guided here in the form of a respective screw 104. The wall portions 109a, 109b of a respective clamping portion 109 have at least partially a distance a, which is smaller than a maximum outer diameter of the screw 104. The screws 104, however, are designed so that they are screwed in the direction of solenoid 101 between the aforementioned areas of the associated Wall sections 109a, 109b with distance a to each other. At this time, the third wall portion 109c is moved away from the wall portion 109a of the respective clamp portion 109, so that the distance a increases. The surfaces 109c, 109d said clamping portion 109 engage with the projections 13, 14 by clamping in abutment; the locking element 100 is clamped or jammed in the support rail 10.

Das Verriegelungselement 100 bildet also eine Art Modul, das als Ganzes in die Tragschiene 10 eingesetzt werden kann.The locking element 100 thus forms a kind of module that can be used as a whole in the support rail 10.

Anstelle von Schrauben 105 kann jeweils auch ein Aufspreizstift Verwendung finden.Instead of screws 105 can each also find a Aufspreizstift use.

Figur 4b zeigt das Verriegelungselement 100 aus einer anderen Perspektive. Hier sind insbesondere die Schrauben 105 zum Befestigen des Elektromagneten 101 am Befestigungsabschnitt 102 zu erkennen. FIG. 4b shows the locking element 100 from a different perspective. Here, in particular, the screws 105 for fastening the electromagnet 101 on the attachment portion 102 can be seen.

Vorzugsweise beide Flächen 109d, 109e wiederum vorzugsweise beider Klemmabschnitte 109 bzw. der entsprechenden Wandabschnitte 109a, 109c weisen Rillenabschnitte 109f auf, deren nicht näher bezeichnete Rillen sich quer zur Einschieberichtung in die nicht dargestellte Tragschiene 10 erstrecken. Weist die der jeweiligen Fläche 109d, 109e zugewandte Klemmfläche des zugewandten, zugehörigen Vorsprungs 13, 14 der Tragschiene 10 im Wesentlichen komplementär ausgebildete Rillen auf, kann das Verriegelungselement 100 nach und nach in die endgültige Einsetzposition in der Tragschiene 10 bewegt und dabei (vor)fixiert werden, was die Montage vereinfacht.Preferably, both surfaces 109d, 109e, in turn, preferably both clamping portions 109 and the corresponding wall portions 109a, 109c have groove portions 109f, whose unspecified grooves extend transversely to the insertion direction in the support rail 10, not shown. If the clamping surface of the facing, associated projection 13, 14 of the mounting rail 10 facing the respective surface 109d, 109e has essentially complementary grooves, the locking element 100 can be gradually moved into the final insertion position in the mounting rail 10 and thereby fixed (before) which simplifies assembly.

Figur 5 zeigt ein Verriegelungselement 100 gemäß einer dritten Ausführungsform der Erfindung in Sperrstellung. Die Ausnehmungen 111, 121 fluchten also nicht miteinander. Das Durchgriffsteil 110 ist mittels Länglöchern 112 über am Durchgriffsteil 120 befestigte oder einstückig ausgebildete Führungsstifte als Führungsabschnitt 107 entlang der Betätigungsrichtung des Elektromagneten 101 bewegbar gelagert. Die Ankerplatte 113 und das Durchgriffsteil 110 bilden vorzugsweise ein L-förmiges Teil. Die Stifte 107 durchgreifen korrespondierende Langlöcher 112 des Durchgriffsteils 110. Die Langlöcher 112 erstrecken sich somit entlang der Bewegungsrichtung des Durchgriffsteils 110. FIG. 5 shows a locking element 100 according to a third embodiment of the invention in the locked position. The recesses 111, 121 are therefore not aligned with each other. The penetration part 110 is movably supported by means of elongated holes 112 via guide pins fastened or integrally formed on the penetration part 120 as guide section 107 along the actuation direction of the electromagnet 101. The anchor plate 113 and the penetration part 110 preferably form an L-shaped part. The pins 107 pass through corresponding elongated holes 112 of the penetration part 110. The elongated holes 112 thus extend along the direction of movement of the penetration part 110.

Wie ferner zu erkennen, sind im Bereich des Durchgriffsteils 110 auf den Führungsstiften 107 Sicherungsscheiben 103 angebracht. Sie verhindern, dass sich das Durchgriffsteil 110 vom Durchgriffsteil 120 bzw. den daran befestigten oder mit diesem einstückig ausgebildeten Führungsstiften 107 in Richtung Elektromagnet 101 entfernt bzw. löst. Es sind jedoch auch andere Lösungen wie Sprengringe, Kontermuttern und dergleichen möglich. Im letzten Fall weisen die Führungsstifte 107 entsprechend ausgebildete Schraubgewinde auf.As can also be seen, in the region of the penetration part 110, securing washers 103 are mounted on the guide pins 107. They prevent the penetration part 110 from the penetration part 120 or the attached thereto or integrally formed with this guide pins 107 in the direction of solenoid 101 removes or dissolves. However, other solutions such as snap rings, lock nuts and the like are possible. In the latter case, the guide pins 107 have correspondingly formed screw threads.

D. h. das Durchgriffsteil 110 ist am Befestigungsabschnitt 102 bewegbar angebracht, sodass die Wirkverbindung mit dem ebenfalls am Befestigungsabschnitt 102 befestigten Elektromagneten 101 vom Gewicht des Durchgriffsteils befreit ist. Damit kann die Wirkverbindung über die Ankerplatte und das Anschlussteil 114 sehr einfach erfolgen.Ie. the penetration part 110 is movably mounted on the attachment portion 102, so that the operative connection with the electromagnet 101 likewise fastened to the attachment portion 102 is freed from the weight of the penetration member. Thus, the operative connection via the anchor plate and the connecting part 114 can be done very easily.

Als Elektromagnet 101 kommt vorzugsweise ein Hubmagnet zur Anwendung. Alternativ oder zusätzlich ist der Elektromagnet 101 bistabil ausgebildet, so dass er sowohl die Sperr- als auch die Freigabestellung des Verriegelungselements 100 bewerkstelligt. In dem Fall können zusätzliche Rückstellelemente entfallen.As solenoid 101 is preferably a solenoid used. Alternatively or additionally, the electromagnet 101 is formed bistable, so that it accomplishes both the blocking and the release position of the locking element 100. In that case, additional return elements can be omitted.

Das Teil 114 kann in Verbindung mit einem mechanischen Auslöseteil auch im Rahmen einer exemplarisch einflügeligen Tür beispielsweise für eine Notöffnung oder Notschließung des angeschlossenen Flügels verwendet werden. Notöffnung oder -Schließung bedeutet, dass eine Öffnung bzw. Schließung des/r jeweiligen Flügel/s möglich sein muss, wenn die Stromversorgung der Flügelanlage, also insbesondere der Verriegelungsanordnung 1, wegfällt.The part 114 can also be used in connection with a mechanical release part in the context of an exemplary single-leaf door, for example for an emergency opening or emergency closing of the connected wing. Emergency opening or closing means that an opening or closing of the respective wing / s must be possible if the power supply of the wing system, ie in particular the locking arrangement 1, is eliminated.

Wie vorstehend erläutert, liegt der Rastvorsprung 32 in Sperrstellung an der dem Verriegelungselement 100 abgewandten Fläche der Ausnehmung 111 des in Bezug auf das Verriegelungselement 30 entfernten Durchgriffsteils 110 an, hintergreift sie somit und verriegelt so den angeschlossenen Flügel. Das zwischen Laufwagen 20 und Durchgriffsteil 110 angeordnete Durchgriffsteil 120 stützt das Durchgriffsteil 110 in Richtung Laufwagen 20 ab, dient also der Gewährleistung der Verriegelung.As explained above, the locking projection 32 is in the blocking position on the locking element 100 facing away from the surface of the recess 111 of the remote with respect to the locking element 30 penetration portion 110, thus engages behind them and thus locks the connected wing. The pass-through part 120 arranged between carriage 20 and pass-through part 110 supports the pass-through part 110 in the direction of carriage 20, thus serving to ensure the locking.

Da der Rastvorsprung 32 das quer zur Bewegungsrichtung des Rastvorsprungs 32 bewegbare Durchgriffsteil 110 hintergreift, muss der Elektromagnet 101 in Sperrstellung nicht den Trägheitskräften des bzw. der angeschlossenen Flügel entgegenwirken. Er muss lediglich die Kraft aufbringen, die erforderlich ist, den Rastvorsprung 32 in Eingriff zu halten, also die Kraft, um die Ausnehmungen 111, 121 in der nicht miteinander fluchtenden Stellung zu halten. Diese Kraft ist zum einen wesentlich geringer. Zum anderen hängt diese Kraft nicht oder nur unwesentlich von den Gewichten des/r angeschlossenen Flügel/s ab.
Im Ergebnis ist durch die Erfindung eine universell einsetzbare Verriegelung für Flügelanlagen jedweder Art geschaffen, die über eine mit dem/n zu verriegelnden Flügel/n wirkverbundenen Führungs- oder Gleitschiene/n verfügen, die also mit diesem/n Flügel/n in Wirkverbindung stehen. Da lediglich Führungs- oder Gleitschiene/n erforderlich sind, kann die Verriegelung unabhängig vom jeweiligen Antriebsmechanismus der Flügelanlage sein.
Die Erfindung ist nicht auf die vorstehend beschriebenen Ausführungen beschränkt. Sie kann beispielsweise auf jegliche Art von Schiebeflügelanlagen wie Schiebetüranlagen und dergleichen angewendet werden. Ferner ist sie ohne weiteres auf Schwenkflügelanlagen anwendbar, sofern sie mit einer Gleitschiene beispielsweise als Teil eines Gleitgestänges versehen sind. Weitere Einsatzgebiete sind beispielsweise Fenster, die über einen so genannten Scherenarm ebenfalls gleitschienengeführt geführt sind.
Since the latching projection 32 engages behind the transverse to the direction of movement of the latching projection 32 movable passage portion 110, the electromagnet 101 in the locked position do not counteract the inertial forces of the connected or the wing. He has only to apply the force required to hold the locking projection 32 in engagement, so the force to hold the recesses 111, 121 in the position not aligned. This power is for a much lower. On the other hand, this force does not or only insignificantly depends on the weights of the connected wing / s.
As a result, a universally deployable lock for wing systems of any kind is provided by the invention, which have a with the / n to be locked wing / n operatively connected guide or slide / n, which are thus in operative connection with this / n wing / n. Since only guide or slide rail / s are required, the lock can be independent of the respective drive mechanism of the wing system.
The invention is not limited to the embodiments described above. It can for example be applied to any type of sliding sash systems such as sliding door systems and the like. Furthermore, it is readily applicable to swing leaf systems, provided they are provided with a slide, for example, as part of a slide linkage. Further areas of use are, for example, windows, which are also guided on a slide rail guided by a so-called scissor arm.

Anstelle der kreisrunden Querschnittsform der Ausnehmungen 111, 121 ist selbstverständlich jede andere Querschnittsform möglich. Die Querschnittsformen der Ausnehmungen 111, 121 müssen auch nicht komplementär zu einer entlang der Bewegung des Rastvorsprungs 32 gesehenen Querschnittsform des Rastvorsprung 22 ausgebildet und auch nicht zueinander identisch sein. Sie können beispielsweise quadratisch sein. Durch das Nicht-Miteinander-Fluchten der Ausnehmungen 111, 121 in Sperrstellung liegt der Rastvorsprung 32 weiterhin an der Ausnehmung 111 verriegelt an. Die Ausnehmung 121 des Durchgriffsteils 120 fluchtet in Montageposition zu jeder Zeit mit dem Rastvorsprung 32, so dass dieser immer in der Lage ist, die Ausnehmung 121 ohne Widerstand passieren zu können.
Die Verriegelungselemente 30, 100 können gegeneinander vertauscht angeordnet sein, sodass nunmehr das Verriegelungselement 100 mit dem Laufwagen 20, auf jeden Fall aber korrespondierend mit einer Bewegung des angeschlossenen Flügels, bewegt wird.
In den Figuren ist eine Verriegelungsanordnung 1 gezeigt, bei der an einem Ende der Tragschiene 10 ein Verriegelungselement 100 angeordnet ist. Beispielhaft entspricht die Stellung des mittels der Verriegelungsanordnung 1 verriegelten Flügels einer Schließstellung dieses Flügels. Alternativ oder zusätzlich kann eine weitere Verriegelungsanordnung vorgesehen sein, die so in der Tragschiene 10 angeordnet ist, dass sie besagten Flügel in Offenstellung verriegelt, also als Offenhaltevorrichtung dient. Dies ist beispielsweise bei Geschäften sinnvoll, deren Eingangstür für den Publikumsverkehr offen stehen bleiben soll.
Gemäß Figuren 1 und 2 ist das Verriegelungselement 30 stirnseitig auf das Aufnahmeprofil 21 aufgesetzt. Es kann aber genauso gut ausgebildet sein, analog zum Verriegelungselement 100 in Bezug auf die Tragschiene 10 in das Aufnahmeprofil 21 eingesetzt bzw. eingeschoben zu werden.
Of course, any other cross-sectional shape is possible instead of the circular cross-sectional shape of the recesses 111, 121. The cross-sectional shapes The recesses 111, 121 need not be complementary to a seen along the movement of the locking projection 32 cross-sectional shape of the locking projection 22 and not be identical to each other. For example, they can be square. Due to the non-alignment with each other of the recesses 111, 121 in the locked position of the locking projection 32 is still locked to the recess 111 at. The recess 121 of the passage member 120 is aligned in the mounting position at all times with the locking projection 32, so that it is always able to pass the recess 121 without resistance can.
The locking elements 30, 100 can be arranged interchanged, so that now the locking element 100 with the carriage 20, but in any case in accordance with a movement of the connected wing, is moved.
In the figures, a locking arrangement 1 is shown, in which at one end of the support rail 10, a locking element 100 is arranged. By way of example, the position of the wing locked by means of the locking arrangement 1 corresponds to a closed position of this wing. Alternatively or additionally, a further locking arrangement may be provided which is arranged in the mounting rail 10 in such a way that it locks said wing in the open position, ie serves as an open-holding device. This is useful, for example, for shops whose front door should remain open to the public.
According to FIGS. 1 and 2 the locking element 30 is placed on the front side of the receiving profile 21. But it can be just as well trained be used analogously to the locking element 100 with respect to the support rail 10 in the receiving profile 21 or inserted.

Anstelle eines Elektromagneten 101 kann beispielsweise auch ein Motor mit Antriebsritzel eingesetzt werden, das mit einer Zahnstange kämmt, die vorzugsweise Teil des Durchgriffsteils 110 ist. Damit kann rein motorisch zwischen Freigabe- und Sperrstellung gewechselt werden. Ferner sind auch manuelle oder andere automatische Verstellmöglichkeiten für den Wechsel zwischen Sperr- und Freigabestellung möglich.Instead of an electromagnet 101, for example, a motor with drive pinion can be used, which meshes with a rack, which is preferably part of the penetration part 110. This can be changed purely motor between release and blocking position. Furthermore, manual or other automatic adjustment options for the change between locking and release position are possible.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
Verriegelungsanordnunglock assembly
1010
Tragschienerail
1111
Aufnahmeabschnittreceiving portion
1212
Aufnahmeabschnittreceiving portion
1313
Vorsprunghead Start
1414
Vorsprunghead Start
2020
Laufwagencarriage
2121
AufnahmeprofilUp profile
2222
Läuferrunner
2323
Mitnehmertakeaway
3030
Verriegelungselementlocking element
3131
Anschlagabschnittstop section
3232
Rastvorsprungcatch projection
3333
Schaftshaft
100100
Verriegelungselementlocking element
101101
Elektromagnetelectromagnet
102102
Befestigungsabschnittattachment section
103103
Sicherungsscheibelock washer
104104
Klemmschraubeclamping screw
105105
Schraubescrew
106106
RückstellfederReturn spring
107107
Führungguide
108108
Schenkelleg
109109
Klemmabschnittclamping section
109a109a
Wandabschnittwall section
109b109b
Wandabschnittwall section
109c109c
Wandabschnittwall section
109d109d
Klemmflächeclamping surface
109e109e
Klemmflächeclamping surface
109f109f
Rillenabschnittgroove section
110110
DurchgriffsteilBy gripping part
111111
Ausnehmungrecess
112112
LanglochLong hole
113113
Ankerplatteanchor plate
114114
Anschlussteilconnector
120120
DurchgriffsteilBy gripping part
121121
Ausnehmungrecess
aa
Abstanddistance

Claims (5)

  1. A device (1) for locking at least one leaf of a leaf installation,
    • including
    - a first locking element (30) comprising a first latching element (32) at one end, and
    - a second locking element (100),
    • comprising, at an end facing the first latching element (32), a second latching element (110, 120), in the locking position, configured to be brought in a latching manner into an operative engagement with the first latching element (32), and
    • adapted to be stationarily disposed with regard to the leaf installation, wherein
    • the first locking element (30) is adapted to be disposed with regard to the at least one leaf such that, during a movement of the at least one leaf, the first locking element (30) is moved correspondingly to said movement in such a way that the first locking element (30), depending on the direction of movement of the at least one leaf, is moved translationally into a locking position towards the second locking element (100), respectively into an unlocking position away from the second locking element (100),
    • wherein one of the locking elements (100) furthermore comprises an activating element (101), which, upon actuation, prevents the latching operative engagement between the first latching element (32) and the second latching element (110, 120) according to a blocking position, or allows for it according to a release position,
    wherein
    • the first or the second latching element (32) includes a latching projection (32), and
    • the second, respectively the first latching element (110, 120) includes a latching part (110, 120) corresponding to the latching projection (32),
    wherein the latching part (110, 120) comprises a first reach-through part (110), which
    • has a latching opening (111), which is configured end-to-end in the first reach-through part (110), and
    • is movable at an acute or right angle with regard to the translational path of movement of the latching projection (32) in such a way that the latching opening (111)
    - in the release position, is disposed such that the latching projection (32), along its translational path of movement, can freely move through the latching opening (111), and
    - in the blocking position, is disposed such that the latching projection (32), as long as it passes through the latching opening (111) in the locking position, is prevented, at least to a predetermined degree, from a movement in a direction away from the first latching opening (111) into the direction of the locking element (30), and is thus in a latching operative engagement with the latching opening (111) while engaging it from behind,
    wherein the latching part (110, 120) furthermore comprises a second reach-through part (120), which
    • is disposed at a side of the first reach-through part (110) facing the latching projection (32),
    • has a latching opening (121), which is configured end-to-end in the first reach-through part (120), and
    • with regard to the second locking element (100), is stationarily disposed such that the latching projection (32), along its translational path of movement, may freely move back and forth through the opening (121),
    • wherein at least one of the locking elements (30), at a side facing the respective other locking element (100), has an abutment (31) for the respective other locking element (100),
    • wherein the second locking element (100) is adapted to be stationarily disposed at or in a guiding or sliding rail (20) of the leaf installation.
  2. The device (1) according to claim 1, wherein the second locking element (100) is configured to be stationarily fastened in the area of a reception groove of a guiding part (20), which is stationarily disposed with regard to the leaf installation or with regard to the respective leaf, or in the reception groove.
  3. The device (1) according to claim 1, wherein the reach-through parts (110,120) bear against each other.
  4. The device (1) according to claim 1, wherein the latching projection (32), at its end facing the latching opening (111) in the direction of the latching opening (111), is configured as tapering or in a mushroom head-shape.
  5. The device (1) according to claim 1, 3 or 4, wherein the activating element (101) is formed by means of an electromagnet (101), which, upon actuation, moves the first reach-through part (110) into the release position or into the blocking position.
EP11000674.9A 2010-02-10 2011-01-28 Lock for leaf assemblies Active EP2354402B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102010007657A DE102010007657A1 (en) 2010-02-10 2010-02-10 Lock for wing systems

Publications (3)

Publication Number Publication Date
EP2354402A2 EP2354402A2 (en) 2011-08-10
EP2354402A3 EP2354402A3 (en) 2015-01-28
EP2354402B1 true EP2354402B1 (en) 2018-03-07

Family

ID=43983692

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11000674.9A Active EP2354402B1 (en) 2010-02-10 2011-01-28 Lock for leaf assemblies

Country Status (4)

Country Link
US (1) US8651534B2 (en)
EP (1) EP2354402B1 (en)
CN (1) CN102155129B (en)
DE (1) DE102010007657A1 (en)

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CN104574609B (en) * 2015-01-22 2017-03-01 北京英奇芯片技术有限公司 A kind of intelligent access control system of building
CN104574607B (en) * 2015-01-22 2017-03-15 湖南海龙国际智能科技股份有限公司 A kind of intelligent building gate control system of flat damping
DE202016101097U1 (en) 2016-03-01 2017-02-10 Agtatec Ag Locking device and associated sliding door system
AT519593B1 (en) 2017-01-18 2019-05-15 Facc Ag locking device
CN107701058B (en) * 2017-10-30 2019-07-09 广东坚朗五金制品股份有限公司 Locking mechanism and sliding door seal assembly
DE102019108273B4 (en) * 2019-03-29 2021-06-24 Dormakaba Deutschland Gmbh Locking device for a sliding door system and sliding door system
DE102019108275B4 (en) * 2019-03-29 2022-12-01 Dormakaba Deutschland Gmbh Linear motor for moving a locking means, locking device for a sliding door system and such a sliding door system

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Also Published As

Publication number Publication date
CN102155129A (en) 2011-08-17
DE102010007657A1 (en) 2011-08-11
EP2354402A2 (en) 2011-08-10
CN102155129B (en) 2016-08-03
EP2354402A3 (en) 2015-01-28
US20110192090A1 (en) 2011-08-11
US8651534B2 (en) 2014-02-18

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