EP2795028B1 - Device for transmitting electrical energy from a wall to a wing fixed on the wall - Google Patents

Device for transmitting electrical energy from a wall to a wing fixed on the wall Download PDF

Info

Publication number
EP2795028B1
EP2795028B1 EP12816466.2A EP12816466A EP2795028B1 EP 2795028 B1 EP2795028 B1 EP 2795028B1 EP 12816466 A EP12816466 A EP 12816466A EP 2795028 B1 EP2795028 B1 EP 2795028B1
Authority
EP
European Patent Office
Prior art keywords
wing
wall
transmitter
spindle
adjusting spindle
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
EP12816466.2A
Other languages
German (de)
French (fr)
Other versions
EP2795028A1 (en
Inventor
Tibor Herglotz
Ingo Steinfeld
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.)
Dr Hanh GmbH and Co KG
Original Assignee
Dr Hanh GmbH and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dr Hanh GmbH and Co KG filed Critical Dr Hanh GmbH and Co KG
Priority to PL12816466T priority Critical patent/PL2795028T3/en
Publication of EP2795028A1 publication Critical patent/EP2795028A1/en
Application granted granted Critical
Publication of EP2795028B1 publication Critical patent/EP2795028B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00Hinges or pivots of special construction
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D11/00Additional features or accessories of hinges
    • E05D11/0081Additional features or accessories of hinges for transmitting energy, e.g. electrical cable routing

Definitions

  • the invention relates to a device for transmitting electrical energy and / or electrical signals from a fixed wall to a wing hinged to the wall about a hinge axis, with a wall part fastened to the wall, with a wing part fastened to the wing, with an energy - And / or signal transmitter, which comprises a wall transmitter part provided in the hinge part and a wing transmitter part provided in the wing, at least one of the wall or wing transmitter parts being arranged displaceably in the direction of the hinge axis.
  • Hinges that serve to connect a wing to a hinge on a wall have been known for a long time. They have proven themselves many times in different technical configurations and are also used for doors for objects such as houses, shops or also for escape doors.
  • Such doors increasingly have safety or comfort-improving devices that are operated by means of electrical energy.
  • These devices can include sensors, for example glass break sensors, which send signals to a wall-side device, for example a burglar alarm center.
  • these devices are therefore regularly connected to an external energy source via flexible cables.
  • These cable connections significantly impair the visual appearance and can be trapped between the wing and the wall, which can lead to damage or even destruction of the cables.
  • the contactless energy and / or signal transmitter comprises a first coil arranged in the frame hinge part and a second coil arranged in a wing hinge part.
  • the magnetic coupling of the two coils, which are spaced apart in the direction of the hinge axis, is provided by a band bolt passing through both coils.
  • a band is known with a band bolt passing through both the wall part and the wing part.
  • a bearing bush for the hinge pin is provided in the wall part and in the wing part.
  • each bearing bush has an electrical coil.
  • the bearing bush of the wall part is included their lower end face on a threaded spindle, which is screwed from below into a threaded hole in the wall part.
  • a generic device is from the WO 2011/067010 A2 known.
  • the wall and wing transmitter parts which comprise induction coil arrangements, are mounted displaceably in the wall or wing part in the direction of the hinge axis.
  • Spring arrangements are provided both in the wall part and in the wing part, by means of which the wall and wing transmission parts are pressed against one another. This measure ensures that the facing each other The end faces of the two coils are always in direct contact. This is of particular importance since, in particular in the case of inductively acting energy and / or signal transmitters, the power loss increases sharply as the distance between the wall and wing transmitter parts increases.
  • the invention is therefore based on the object of improving the generic device with regard to its mountability and functionality.
  • the device according to the invention comprises an optionally actuatable displacement drive, by means of which the wall and / or wing transmitter part of the energy and / or signal transmitter can be displaced in the direction of the hinge axis S. Because of this configuration, the wall and / or wing transmitter parts can be brought into a position in which the device can be joined together using the displacement drive.
  • the displacement drive prevents the transmitter parts, as in the prior art, from being displaced in an uncontrolled manner due to the spring force in the direction of the hinge axis.
  • the wall and / or wing transmitter parts can be shifted into retracted assembly positions and then, with the device assembled, can be shifted to one another with the help of the shift drive in which their mutually facing sides are at a very small but well-defined distance from one another in which the sides do not rub against each other under the action of spring elements.
  • the wall transmitter part and the wing transmitter part of an energy and / or signal transmitter must be arranged such that they can be displaced in the direction of the hinge axis S by means of the displacement drive. Rather, it is sufficient and, because of the lower construction effort, preferred to simply connect either the wall transmitter part or the wing transmitter part to the displacement drive and to arrange the other part in a fixed manner in the respectively associated wall or wing part.
  • the displacement drive preferably comprises an adjusting spindle which is rotatably mounted about the hinge axis.
  • the adjusting spindle is then preferably arranged approximately such that its axis of rotation coincides approximately with the hinge axis.
  • the adjusting spindle is preferably arranged stationary in the direction of the hinge axis. When actuated, it therefore does not move in relation to the wall and wing parts, but the wall and / or wing transmitter parts move in the direction of the hinge axis relative to the adjusting spindle when actuated by rotation.
  • the adjusting spindle is preferably in engagement with a spindle nut provided on or connected to the at least one wall or wing transmitter part.
  • the adjusting spindle can be double-acting, ie it can include a right-hand thread in one area and a left-hand thread in another area.
  • This embodiment is particularly suitable for use in a device according to the invention, which has approximately the shape of a three-part band.
  • a band has two wall parts which are spaced apart from one another in the hinge axis direction and a wing part which engages in the space between the two wall parts.
  • Such a device is particularly suitable for receiving two transmitters, each with a wall transmitter part and a wing transmitter part. One of the transmitters can then be used to transmit electrical energy, the other transmitter can be used to transmit electrical signals.
  • the double-acting adjusting spindle can be inside the wing part be arranged stationary in the direction of the hinge axis S and cooperate with one area with the wing transmitter part of the energy transmitter, with the other area with the wing transmitter part of the signal transmitter.
  • a rotary actuation of the adjusting spindle then causes the two wing transmitter parts to move toward or away from one another, depending on the direction of rotation.
  • the adjusting spindle preferably has a device for attaching a rotary actuating tool.
  • a rotary actuating tool can comprise, for example, an external toothing to which, for example, a screwdriver blade serving as a rotary actuating tool can be attached.
  • a worm wheel in engagement with the external toothing, the axis of rotation of which runs perpendicular to the hinge axis and which itself can be rotated using a turning tool. This configuration would be characterized by a more sensitive operability.
  • a setting wheel which is connected to the spindle and has crown teeth.
  • This crown toothing can be designed such that it can be brought into engagement, for example, with a commercially available polygonal turning tool (for example Torx®).
  • Torx® a commercially available polygonal turning tool
  • This embodiment is characterized by a particularly sensitive adjustability, without the need for gear components provided in the device, with the exception of the adjusting wheel.
  • no additional tool provided specifically for the rotary actuation is necessary, since the toothing is preferably adapted to a polygonal turning tool, which is required anyway for mounting the device.
  • a drive device which is in engagement with the crown toothing and is mounted in a spindle receptacle in which the adjusting spindle is provided.
  • the drive device can be designed for actuation with the aid of a specific tool provided for this purpose or for manual actuation.
  • the drive device particularly preferably comprises a shaft with an external toothing which is in engagement with the crown toothing.
  • the drive device preferably has a conical surface which interacts with a locking surface provided on the spindle receptacle and ensures a captive fit in a receptacle of the drive device in the spindle receptacle.
  • a locking element is preferably provided for optionally locking the displacement drive.
  • This locking element can comprise a stud screw, which can optionally be tightened against the adjusting spindle.
  • transformers which are technically very differently configured or operative can be used in connection with the device according to the invention.
  • transformers which are technically very differently configured or operative can be used in connection with the device according to the invention.
  • the device according to the invention is provided for the use of induction coil arrangements in the wall and wing transmitter parts.
  • the wall and / or wing transmitter parts can comprise housings for shielding electrical or magnetic fields, which are open on the mutually facing sides of the wall and wing transmitter parts. So that manufacturing tolerances are automatically compensated for, the actual transmitter components can be floatingly supported in the housings, for example by a flexible layer in a gap between the transmitter component and the housing.
  • the device according to the invention preferably also has means for securing the wall or wing transmitter parts against rotation in the band or the Wing part on. This prevents any entrainment forces that arise between the wall and the wing transmitter parts when the wing is opened or closed, for example due to the ingress of contaminants, from tearing off any existing connection cables of the transmitter parts.
  • the means for securing against rotation can comprise a projection provided on the wall or wing transmission part, which protrudes into a recess provided on the wall or wing part.
  • This recess can include boundary surfaces running approximately perpendicular to the hinge axis, which form adjustment path limitations for the wall or wing transmitter part.
  • the projection can have a channel for the passage of connecting cables of the wall or wing transmitter part, in order to provide particularly effective protection against damage to the connecting cable.
  • the embodiment of an apparatus according to the invention is modeled on a three-part band. It comprises two wall parts 1, 2 spaced apart from one another in the direction of the hinge axis S, onto which fastening parts 3, 4 are molded.
  • a wing part 6 is arranged in the space 5 between the two wall parts 1, 2.
  • the wing part 6 can be pivoted about the hinge axis S. It comprises a fastening part 7, by means of which it can be fastened to a wing, not shown in the drawing.
  • the device 100 comprises an energy transmitter 8, which is used in particular to transmit electrical actuating power from a wall into the wing, which is required by consumers provided on the wing to drive it.
  • the energy transmitter 8 comprises a wall transmitter part 9 provided in the wall part 1 and a wing transmitter part 10 provided in the wing part 6.
  • the wall and wing transmitter parts 9, 10 are designed as induction coils for mutual inductive coupling. They each comprise a soft magnetic coil body 11, 12 which completely surrounds a respective coil winding 13, 14, with the exception of the sides facing one another. Both coil formers each have a central core 15, 16, which are solid in this embodiment of the device 100. The mutually facing end faces of the coil former 11, 12 including the cores 15, 16 are flat.
  • the bobbins 11, 12 and thus the actual transmitter parts 9, 10 are surrounded by housings 17, 18, which serve to shield external interference, in particular external magnetic fields in the exemplary embodiment shown.
  • the housings 17, 18 are designed such that they overlap on the mutually facing side by integrally formed, complementary chamfers.
  • the housing 17 of the wall transmitter part 9 has a radially protruding circumferential collar 19, which immediately forms a contact surface for the purpose of positioning the housing 17 in the wall part 1.
  • a layer 20 of a resilient material is provided, which ensures a kind of floating mounting of the bobbins 11, 12. This ensures that the two bobbins 11, 12 align themselves in the assembled state, or at least essentially lie against one another over the entire surface.
  • the device 100 has a signal transmitter 21, the basic structure of which corresponds to that of the energy transmitter 8. Accordingly, it also includes Wall transmitter part 22, which is provided in the second wall part 2. The wing transmitter part 23 is in turn arranged in the wing part 6, but on the side facing away from the wing transmitter part 10 of the energy transmitter 8.
  • the components of the energy transmitter 8 and those of the signal transmitter 21 can also be designed differently with regard to their electrical and electromagnetic properties and their dimensions, in order to adapt the two transmitters as best as possible to the powers or signals to be transmitted.
  • the wing transmission parts 10, 23 are arranged displaceably in the wing part 6 in the direction of the hinge axis S.
  • recesses 24, 25 are provided in the wing part 6, which are adapted to the outer contours of the housings 17, 18 of the wing transmitter parts 10, 23 such that they are received by the recesses essentially without lateral play.
  • a displacement drive 26 is arranged between the two cutouts 24, 25 in the direction of the hinge axis S. It is shown in a single representation together with a turning tool intended for its actuation Fig. 5 displayed. It comprises a spindle receptacle 27 consisting, for example, of a plastic molded part, which has an opening 28 which is approximately keyhole-shaped in cross section and which extends through the in FIG Fig. 5 extends sidewall 29 facing the viewer. Furthermore, the opening 28 comprises a laterally widening, approximately slot-shaped region 30. The opening 28 serves to support an adjusting spindle 31, it comprises a central, cylindrical region 32 which is mounted within the opening 28 essentially without play.
  • the contour of the keyhole-shaped opening 28 is adapted to the outer diameter of the area 32 such that the adjusting spindle 31 overcomes an elastic one Force can be clipped into the spindle receptacle 27 from the side wall 29 through the narrow region of the keyhole-shaped opening.
  • a crown wheel 39 protruding radially outward is formed on the area 32 and bears a toothing 40 which is provided for the engagement of an optionally applicable polygonal turning tool 41.
  • a bore is provided on the spindle receptacle 27 Fig. 5 is not recognizable.
  • a partial length of this bore is provided with an external thread, into which a stud screw 37 forming a locking element 36 can be screwed for optional locking of the adjusting spindle 31. In the fully screwed-in state, the stud 37 presses with its leading end in the screwing-in direction against the adjusting spindle 31.
  • Threaded areas 42, 43 adjoin area 32 of adjusting spindle 31 in the direction of axis of rotation D of adjusting spindle 31.
  • the external thread of one thread area is designed as a right-hand thread, and the external thread of the other thread area is designed as a left-hand thread.
  • the adjusting spindle 31 engages, as in particular in Fig. 2 is recognizable, in complementary threaded bores 44, 45, which serve as spindle nuts 34, 35, the housing of the wing transmission parts 10, 23, so that these are moved toward or away from one another by rotary actuation of the adjusting spindle, depending on the direction of rotation.
  • blind bores 46, 47 are provided on the bobbins, into which parts of the threaded areas 42, 43 can protrude.
  • Such blind bores are also provided in the bobbins of the wall transmitter parts (but here inoperative) so that the same bobbins can be used to reduce manufacturing costs.
  • the two wing transmitter parts 10, 23 can be moved towards each other by turning the adjusting spindle 31 with the help of a turning tool, so that they - as in Fig. 3 is shown - be moved back into the space 5 between the band parts 1, 2, so that the wing part 6 can be moved out of the space 5.
  • Fig. 4 . 6 and 7 it can be seen that means for securing against rotation 48 in the form of projections 49 are provided on the wing transmitter parts 10, 23. These projections 49 engage in depressions 50 in the fastening part 7, which are covered by a cover cap 53 when the device is fully assembled. This cover cap is secured using a retaining screw 51.
  • the depressions 50 comprise boundary surfaces 54 which run approximately perpendicular to the hinge axis S and which form adjustment path limitations for the wall or wing transmitter part.
  • the projections 49 comprise - as in particular in FIG Fig. 7 is recognizable - in each case a channel 52 through which connecting cables of the respective wing transmitter part, which cannot be seen in the drawing, can be guided in a protected manner.
  • the frame transmitter parts can also have appropriately designed means for securing against rotation.
  • FIGS 8 and 9 Another exemplary embodiment 200 of a device according to the invention is shown in FIGS 8 and 9 shown.
  • exemplary embodiment 100 In order to avoid repetitions, only the differences from the exemplary embodiment 100 will be discussed below. Reference is made to the description of exemplary embodiment 100 in its entirety, provided that the explanations below do not contradict this.
  • the displacement drive 126 is provided in the upper wall part 101. It comprises an adjusting spindle 131, which is screwed into a threaded receptacle 154 within the wall part 101.
  • the adjusting spindle 131 has a central through bore 155, at the upper end of which a polygonal recess 156 is provided for attaching a turning tool.
  • the wall transmitter part 109 is positively connected to the adjusting spindle 131 and is arranged displaceably in the direction of the hinge axis S within the wall part 101.
  • the wall transmitter part 109 can thus be between the in Fig. 8 shown operating position and in Fig. 9 shift illustrated assembly position, whereby an assembly and disassembly of the wing part 106 is possible in a simple manner.
  • the exemplary embodiment 200 differs from the previously described exemplary embodiment 100 in that all the coil bodies comprise a central longitudinal bore 157.
  • a single or multi-part hinge pin 158 which aligns the transmitter parts to one another, can be inserted into this.
  • the displacement drive 226 in turn has a spindle receptacle 227, which can consist, for example, of a metal molded part.
  • the spindle receptacle 227 like the spindle receptacle 27 of the exemplary embodiment 100, has an opening 228 which is approximately keyhole-shaped in cross section and which is defined by the in FIG Fig. 11 extends sidewall 229 facing away from the viewer.
  • the opening 228 again comprises a laterally widening, approximately slit-shaped region 230 (see in particular Fig. 12 ,
  • the opening 228 serves to support the adjusting spindle 231. It comprises a central, cylindrical region 232 which is mounted within the opening 228 essentially without play.
  • the contour of the keyhole-shaped opening 228 is adapted to the outer diameter of the area 232 in such a way that the adjusting spindle 231 can be inserted, preferably clipped, into the spindle receptacle 227 through the narrow area of the keyhole-shaped opening from the side wall 229.
  • a crown wheel 239 protruding outwards is formed on the area 232 and bears a toothing 240. It is - as in particular in 12 and 13 is recognizable - provided for the engagement of a drive device 259. It comprises a cylindrical shaft 260, which comprises an external toothing 261, which is in engagement with the toothing 240 of the crown gear 239.
  • a head 262 adjoins the shaft 260 towards the outside, which head has a conically tapering shape towards the outside.
  • the conical surface 263 of the head lies against a locking surface 264 of the head, so that the drive device 259, although rotatable about its longitudinal axis L, is mounted in the spindle receptacle 227 essentially without play in the direction of the longitudinal axis L.
  • the locking surface 264 is formed by a tab 267 provided on the lower two projections 265.
  • the two projections 265 delimit a receiving opening 266 in which the drive device 259 is mounted.
  • the tab 267 is initially in a position projecting approximately perpendicularly from the side wall of the spindle receptacle. After the drive device has been fitted, the tab 267 is plastically bent so that it rests on the cone surface 263 of the drive device 259.
  • the drive device has a hexagon socket 268 for attaching a turning tool. It goes without saying that other means, such as slots, cross slots, etc., can also be used for attaching a turning tool.
  • the spindle receptacle 227 comprises a threaded bore 269 which is arranged offset to the receptacle opening 266.
  • the threaded bore 269 serves to receive a stud screw 270 which can be rotated against the area 232 of the adjusting spindle 231 in order to lock it in a desired position against automatic rotation.
  • the adjusting spindle 231 engages with its threaded areas 242, 243 in bores of coil bodies 211, 212.
  • the thread areas have opposite threads, that is, a left-hand and a right-hand thread, so that when the adjusting spindle 231 is actuated in rotation, the two coil bodies are moved away from one another or towards one another, depending on the direction of rotation.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pivots And Pivotal Connections (AREA)

Description

Die Erfindung betrifft eine Vorrichtung zur Übertragung von elektrischer Energie und/oder elektrischen Signalen von einer feststehenden Wand auf einen an der Wand um eine Scharnierachse scharniergelenkig befestigten Flügel, mit einem an der Wand befestigbaren Bandteil, mit einem an dem Flügel befestigbaren Flügelteil, mit einem Energie- und/oder Signalübertrager, der ein in dem Bandteil vorgesehenes Wandübertragerteil und ein im Flügel vorgesehenes Flügelübertragerteil umfasst, wobei zumindest eines der Wand- oder Flügelübertragerteile in Richtung der Scharnierachse verlagerbar angeordnet ist.The invention relates to a device for transmitting electrical energy and / or electrical signals from a fixed wall to a wing hinged to the wall about a hinge axis, with a wall part fastened to the wall, with a wing part fastened to the wing, with an energy - And / or signal transmitter, which comprises a wall transmitter part provided in the hinge part and a wing transmitter part provided in the wing, at least one of the wall or wing transmitter parts being arranged displaceably in the direction of the hinge axis.

Bänder, die zur scharniergelenkigen Verbindung eines Flügels an einer Wand dienen, sind bereits seit langem bekannt. Sie haben sich in unterschiedlichen technischen Ausgestaltungen vielfach bewährt und finden auch bei Türen für Objekte wie Häuser, Geschäfte oder auch bei Fluchttüren Verwendung.Hinges that serve to connect a wing to a hinge on a wall have been known for a long time. They have proven themselves many times in different technical configurations and are also used for doors for objects such as houses, shops or also for escape doors.

Derartige Türen weisen in zunehmendem Maße die Sicherheit oder den Komfort verbessernde Einrichtungen auf, die mittels elektrischer Energie betrieben werden. Diese Einrichtungen können Sensoren, beispielsweise Glasbruchsensoren umfassen, welche Signale an eine wandseitige Einrichtung, beispielsweise eine Einbruchmeldezentrale, senden.Such doors increasingly have safety or comfort-improving devices that are operated by means of electrical energy. These devices can include sensors, for example glass break sensors, which send signals to a wall-side device, for example a burglar alarm center.

Zur Energie- und/oder Signalübertragung sind diese Einrichtungen daher regelmäßig über flexible Kabel mit einer externen Energiequelle verbunden. Diese Kabelverbindungen beeinträchtigen das optische Erscheinungsbild deutlich und können zwischen dem Flügel und der Wand eingeklemmt werden, was zu Beschädigungen oder sogar zu Zerstörungen der Kabel führen kann.For energy and / or signal transmission, these devices are therefore regularly connected to an external energy source via flexible cables. These cable connections significantly impair the visual appearance and can be trapped between the wing and the wall, which can lead to damage or even destruction of the cables.

Aus der DE 39 15 812 A1 und aus der DE 10 2004 017 341 A1 sind Bänder mit kontaktlos arbeitenden Energie- und/oder Signalübertragern bekannt. Diese sind bei der DE 39 15 812 A1 als konzentrisch angeordnete Spulen oder als zylindrischer Kondensator ausgebildet. Im Falle der DE 10 2004 017 341 A1 umfasst der kontaktlos arbeitende Energie- und/oder Signalübertrager eine in dem Rahmenbandteil angeordnete erste Spule und eine in einem Flügelbandteil angeordnete zweite Spule. Der magnetischen Ankopplung beider Spulen, die in Richtung der Scharnierachse voneinander beabstandet sind, dient ein beide Spulen durchsetzender Bandbolzen.From the DE 39 15 812 A1 and from the DE 10 2004 017 341 A1 tapes with contactless energy and / or signal transmitters are known. These are with the DE 39 15 812 A1 designed as a concentrically arranged coils or as a cylindrical capacitor. In case of DE 10 2004 017 341 A1 The contactless energy and / or signal transmitter comprises a first coil arranged in the frame hinge part and a second coil arranged in a wing hinge part. The magnetic coupling of the two coils, which are spaced apart in the direction of the hinge axis, is provided by a band bolt passing through both coils.

Zwar ist grundsätzlich die kontaktlose Energieübertragung von einem feststehenden Rahmen in einen schwenkbar an dem Rahmen angeordneten Flügel mit den aus den vorzitierten Druckschriften bekannten Vorrichtungen möglich, Versuche haben jedoch gezeigt, dass die maximal übertragbaren Leistungen für viele wünschenswerte Anwendungsbereiche zu niedrig sind, da die Verlustleistung bei der Übertragung sehr hoch ist.In principle, contactless energy transfer from a fixed frame into a wing that can be pivoted on the frame is possible with the devices known from the above-cited publications, but tests have shown that the maximum transmissible powers are too low for many desirable fields of application, since the power loss at the transmission is very high.

Aus der DE 20 2008 014 318 U1 ist ein Band mit einem sowohl durch das Wandteil, als auch durch das Flügelteil hindurch gehenden Bandbolzen bekannt. Es ist in dem Wandteil und in dem Flügelteil jeweils eine Lagerbuchse für den Bandbolzen vorgesehen. jede Lagerbuchse umfasst eine elektrische Spule. Zur vertikalen Justierbarkeit eines derartigen Bandes liegt die Lagerbuchse des Wandteils mit ihrer unteren Stirnfläche auf einer Gewindespindel auf, die von unten in eine Gewindebohrung des Wandteils eingedreht ist.From the DE 20 2008 014 318 U1 a band is known with a band bolt passing through both the wall part and the wing part. A bearing bush for the hinge pin is provided in the wall part and in the wing part. each bearing bush has an electrical coil. For the vertical adjustability of such a band, the bearing bush of the wall part is included their lower end face on a threaded spindle, which is screwed from below into a threaded hole in the wall part.

Eine gattungsgemäße Vorrichtung ist aus der WO 2011/067010 A2 bekannt. Um die übertragbare Leistung zu erhöhen, sind bei dieser Vorrichtung die Wand- und Flügelübertragerteile, die Induktionsspulenanordnungen umfassen, in Richtung der Scharnierachse verlagerbar in dem Wand- oder Flügelteil gelagert. Es sind sowohl in dem Wandteil, als auch in dem Flügelteil Federanordnungen vorgesehen, mittels welcher die Wand- und Flügelübertragerteile gegeneinander gedrückt werden. Aufgrund dieser Maßnahme ist gewährleistet, dass die einander zugewandten Stirnseiten der beiden Spulen sich stets in direktem Kontakt befinden. Dies ist von besonderer Bedeutung, da insbesondere bei induktiv wirkenden Energie- und/oder Signalübertragern die Verlustleistung mit Zunahme des Abstandes der Wand- und Flügelübertragerteile zueinander stark ansteigt.A generic device is from the WO 2011/067010 A2 known. In order to increase the power that can be transmitted, in this device the wall and wing transmitter parts, which comprise induction coil arrangements, are mounted displaceably in the wall or wing part in the direction of the hinge axis. Spring arrangements are provided both in the wall part and in the wing part, by means of which the wall and wing transmission parts are pressed against one another. This measure ensures that the facing each other The end faces of the two coils are always in direct contact. This is of particular importance since, in particular in the case of inductively acting energy and / or signal transmitters, the power loss increases sharply as the distance between the wall and wing transmitter parts increases.

Allerdings hat sich gezeigt, dass die Montierbarkeit einer derartigen Vorrichtung insbesondere dann, wenn kein die Scharnierachse definierender Bandbolzen vorgesehen ist und die Vorrichtung lediglich zur Übertragung von elektrischer Energie und/oder elektrischen Signalen und nicht von mechanischen Kräften dient, wesentlich erschwert ist. Darüber hinaus führt die Anlage der Wand- und Flügelübertragerteile aneinander unter der Federkraft dazu, dass die beiden sich während des Öffnens und Schließens des Flügels aneinander gleitenden Seiten der Flügel- und Wandübertragerteile verschleißen.However, it has been shown that it is considerably more difficult to assemble such a device, in particular when no hinge pin defining the hinge axis is provided and the device is only used to transmit electrical energy and / or electrical signals and not mechanical forces. In addition, the abutment of the wall and wing transmitter parts against one another under the spring force causes the two sides of the wing and wall transmitter parts sliding against one another to wear during the opening and closing of the wing.

Der Erfindung liegt daher die Aufgabe zugrunde, die gattungsgemäße Vorrichtung hinsichtlich ihrer Montierbarkeit und Funktionalität zu verbessern.The invention is therefore based on the object of improving the generic device with regard to its mountability and functionality.

Diese Aufgabe wird durch die in Anspruch 1 wiedergegebene Vorrichtung gelöst.This object is achieved by the device reproduced in claim 1.

Die erfindungsgemäße Vorrichtung umfasst einen wahlweise betätigbaren Verlagerantrieb, mittels welchem das Wand- und/oder Flügelübertragerteil des Energie- und/oder Signalübertragers in Richtung der Scharnierachse S verlagern lässt. Aufgrund dieser Ausgestaltung können mit Hilfe des Verlagerantriebs die Wand- und/oder Flügelübertragerteile in eine Position gebracht werden, in welcher ein Zusammenfügen der Vorrichtung möglich ist. Der Verlagerantrieb verhindert, dass die Übertragerteile, wie im Stand der Technik, sich aufgrund der Federkraft in Richtung der Scharnierachse unkontrolliert verlagern können. Vielmehr können zur Montage der Vorrichtung die Wand- und/oder Flügelübertragerteile in zurückgezogenen Montagepositionen verlagert und anschließend bei zusammengefügter Vorrichtung mit Hilfe des Verlagerantriebs in Positionen zueinander verlagert werden, in welcher ihre einander zugewandten Seiten sich in einem sehr geringen, jedoch wohl definierten Abstand zueinander befinden, in denen die Seiten nicht unter der Wirkung von Federelementen aufeinander schleifen. Um die mit der Erfindung verbundenen Vorteile zu erzielen, ist es nicht erforderlich, dass sowohl das Wandübertragerteil, als auch das Flügelübertragerteil eines Energie- und/oder Signalübertragers mit Hilfe des Verlagerantriebs in Richtung der Scharnierachse S verlagerbar angeordnet sein müssen. Vielmehr ist es ausreichend und wegen des geringeren konstruktiven Aufwandes bevorzugt, lediglich entweder das Wandübertragerteil, oder das Flügelübertragerteil mit dem Verlagerantrieb wirkzuverbinden und das jeweils andere Teil in dem jeweils zugehörigen Wand- oder Flügelteil feststehend anzuordnen.The device according to the invention comprises an optionally actuatable displacement drive, by means of which the wall and / or wing transmitter part of the energy and / or signal transmitter can be displaced in the direction of the hinge axis S. Because of this configuration, the wall and / or wing transmitter parts can be brought into a position in which the device can be joined together using the displacement drive. The displacement drive prevents the transmitter parts, as in the prior art, from being displaced in an uncontrolled manner due to the spring force in the direction of the hinge axis. Rather, to assemble the device, the wall and / or wing transmitter parts can be shifted into retracted assembly positions and then, with the device assembled, can be shifted to one another with the help of the shift drive in which their mutually facing sides are at a very small but well-defined distance from one another in which the sides do not rub against each other under the action of spring elements. To those with the invention To achieve associated advantages, it is not necessary that both the wall transmitter part and the wing transmitter part of an energy and / or signal transmitter must be arranged such that they can be displaced in the direction of the hinge axis S by means of the displacement drive. Rather, it is sufficient and, because of the lower construction effort, preferred to simply connect either the wall transmitter part or the wing transmitter part to the displacement drive and to arrange the other part in a fixed manner in the respectively associated wall or wing part.

Der Verlagerantrieb umfasst vorzugsweise eine etwa um die Scharnierachse rotierbar gelagerte Stellspindel. Die Stellspindel ist dann vorzugsweise etwa derart angeordnet, dass ihre Drehachse etwa mit der Scharnierachse zusammenfällt.The displacement drive preferably comprises an adjusting spindle which is rotatably mounted about the hinge axis. The adjusting spindle is then preferably arranged approximately such that its axis of rotation coincides approximately with the hinge axis.

Vorzugsweise ist die Stellspindel in Richtung der Scharnierachse ortsfest angeordnet. Sie bewegt sich bei Betätigung somit nicht gegenüber den Wand- und Flügelteilen, sondern die Wand- und/oder Flügelübertragerteile bewegen sich bei Drehbetätigung relativ zu der Stellspindel in Richtung der Scharnierachse.The adjusting spindle is preferably arranged stationary in the direction of the hinge axis. When actuated, it therefore does not move in relation to the wall and wing parts, but the wall and / or wing transmitter parts move in the direction of the hinge axis relative to the adjusting spindle when actuated by rotation.

Hierzu steht die Stellspindel bevorzugt mit einer an dem zumindest einen Wand- oder Flügelübertragerteil vorgesehenen oder mit diesen verbundenen Spindelmutter in Eingriff.For this purpose, the adjusting spindle is preferably in engagement with a spindle nut provided on or connected to the at least one wall or wing transmitter part.

Die Stellspindel kann doppelt wirkend ausgebildet sein, d.h. in einem Bereich ein Rechtsgewinde, in einem anderen Bereich ein Linksgewinde umfassen. Diese Ausgestaltung ist insbesondere zur Verwendung in einer erfindungsgemäßen Vorrichtung geeignet, welche etwa die Gestalt eines dreiteiligen Bandes aufweist. Ein derartiges Band weist zwei in Scharnierachsenrichtung voneinander beabstandete Wandteile sowie ein in den Abstandsraum zwischen den beiden Wandteilen eingreifendes Flügelteil auf. Eine derartige Vorrichtung ist insbesondere geeignet, zwei Übertrager aufzunehmen, jeweils mit einem Wandübertragerteil und einem Flügelübertragerteil. Einer der Übertrager kann dann der Übertragung elektrischer Energie, der andere Übertrager der Übertragung von elektrischen Signalen dienen. In diesem Fall kann die doppelt wirkende Stellspindel innerhalb des Flügelteils in Richtung der Scharnierachse S ortsfest angeordnet sein und mit dem einen Bereich mit dem Flügelübertragerteil des Energieübertragers, mit dem anderen Bereich mit dem Flügelübertragerteil des Signalübertragers zusammenwirken. Eine Drehbetätigung der Stellspindel führt dann dazu, dass sich die beiden Flügelübertragerteile - je nach Drehrichtung - aufeinander zu oder voneinander fort bewegen.The adjusting spindle can be double-acting, ie it can include a right-hand thread in one area and a left-hand thread in another area. This embodiment is particularly suitable for use in a device according to the invention, which has approximately the shape of a three-part band. Such a band has two wall parts which are spaced apart from one another in the hinge axis direction and a wing part which engages in the space between the two wall parts. Such a device is particularly suitable for receiving two transmitters, each with a wall transmitter part and a wing transmitter part. One of the transmitters can then be used to transmit electrical energy, the other transmitter can be used to transmit electrical signals. In this case, the double-acting adjusting spindle can be inside the wing part be arranged stationary in the direction of the hinge axis S and cooperate with one area with the wing transmitter part of the energy transmitter, with the other area with the wing transmitter part of the signal transmitter. A rotary actuation of the adjusting spindle then causes the two wing transmitter parts to move toward or away from one another, depending on the direction of rotation.

Die Stellspindel weist vorzugsweise eine Einrichtung zum Ansetzen eines Drehbetätigungswerkzeugs auf. Hierzu kann sie beispielsweise eine Außenverzahnung umfassen, an die beispielsweise eine als Drehbetätigungswerkzeug dienende Schraubenzieherklinge angesetzt werden kann. Oder es befindet sich ein Schneckenrad im Eingriff mit der Außenverzahnung, dessen Drehachse senkrecht zur Scharnierachse verläuft und welches selbst mit einem Drehwerkzeug drehbetätigbar ist. Diese Ausgestaltung würde sich durch eine feinfühligere Betätigbarkeit auszeichnen.The adjusting spindle preferably has a device for attaching a rotary actuating tool. For this purpose, it can comprise, for example, an external toothing to which, for example, a screwdriver blade serving as a rotary actuating tool can be attached. Or there is a worm wheel in engagement with the external toothing, the axis of rotation of which runs perpendicular to the hinge axis and which itself can be rotated using a turning tool. This configuration would be characterized by a more sensitive operability.

Besonders bevorzugt ist es jedoch, wenn ein mit der Spindel verbundenes Stellrad vorgesehen ist, welches eine Kronenverzahnung aufweist. Diese Kronenverzahnung kann derart ausgestaltet sein, dass sie beispielsweise mit einem handelsüblichen Vielkantdrehwerkzeug (beispielsweise Torx®) in Eingriff bringbar ist. Diese Ausgestaltung zeichnet sich durch eine besonders feinfühlige Verstellbarkeit aus, ohne dass es hierzu in der Vorrichtung vorgesehener Getriebebestandteile, mit Ausnahme des Stellrades, bedürfte. Darüber hinaus ist auch kein extra für die Drehbetätigung vorgesehenes Zusatzwerkzeug notwendig, da die Verzahnung vorzugsweise an einen Mehrkantdrehwerkzeug, welches ohnehin zur Montage der Vorrichtung benötigt wird, angepasst ist.However, it is particularly preferred if a setting wheel is provided which is connected to the spindle and has crown teeth. This crown toothing can be designed such that it can be brought into engagement, for example, with a commercially available polygonal turning tool (for example Torx®). This embodiment is characterized by a particularly sensitive adjustability, without the need for gear components provided in the device, with the exception of the adjusting wheel. In addition, no additional tool provided specifically for the rotary actuation is necessary, since the toothing is preferably adapted to a polygonal turning tool, which is required anyway for mounting the device.

Es ist ebenfalls möglich, eine Antriebseinrichtung vorzusehen, die sich im Eingriff mit der Kronenverzahnung befindet und in einer Spindelaufnahme, in welcher die Stellspindel vorgesehen ist, gelagert ist. Die Antriebseinrichtung kann an die Betätigung mit Hilfe eines bestimmten, hierzu vorgesehenen Werkzeugs oder zur manuellen Betätigung ausgebildet sein.It is also possible to provide a drive device which is in engagement with the crown toothing and is mounted in a spindle receptacle in which the adjusting spindle is provided. The drive device can be designed for actuation with the aid of a specific tool provided for this purpose or for manual actuation.

Besonders bevorzugt umfasst die Antriebseinrichtung einen Schaft mit einer Außenverzahnung, welche sich mit der Kronenverzahnung in Eingriff befindet.The drive device particularly preferably comprises a shaft with an external toothing which is in engagement with the crown toothing.

Darüber hinaus weist die Antriebseinrichtung vorzugsweise eine Konusfläche auf, die mit einer an der Spindelaufnahme vorgesehenen Arretierfläche zusammenwirkt und einen verliersicheren Sitz in einer Aufnahme der Antriebseinrichtung in der Spindelaufnahme sicherstellt.In addition, the drive device preferably has a conical surface which interacts with a locking surface provided on the spindle receptacle and ensures a captive fit in a receptacle of the drive device in the spindle receptacle.

Um eine mit Hilfe des Verlagerantriebs erzielte Positionierung der Übertragerteile dauerhaft aufrechterhalten zu können, ist vorzugsweise ein Arretierelement zur wahlweisen Arretierung des Verlagerungsantriebs vorgesehen.In order to be able to permanently maintain a positioning of the transmitter parts achieved with the aid of the displacement drive, a locking element is preferably provided for optionally locking the displacement drive.

Dieses Arretierelement kann eine Stiftschraube umfasst, die wahlweise gegen die Stellspindel festziehbar ist.This locking element can comprise a stud screw, which can optionally be tightened against the adjusting spindle.

Grundsätzlich können im Zusammenhang mit der erfindungsgemäßen Vorrichtung technisch unterschiedlichst ausgestaltete oder wirkende Übertrager Verwendung finden. So ist es beispielsweise auch denkbar, optoelektronisch oder kapazitiv wirkende Übertrager einzusetzen und aufgrund der erfindungsgemäßen Ausgestaltung optimal positionieren zu können. Insbesondere ist die erfindungsgemäße Vorrichtung jedoch zur Verwendung von Induktionsspulenanordnungen bei den Wand- und Flügelübertragerteilen vorgesehen.In principle, transformers which are technically very differently configured or operative can be used in connection with the device according to the invention. For example, it is also conceivable to use optoelectronic or capacitive transformers and to be able to position them optimally on the basis of the configuration according to the invention. In particular, however, the device according to the invention is provided for the use of induction coil arrangements in the wall and wing transmitter parts.

Die Wand- und/oder Flügelübertragerteile können Gehäuse zur Abschirmung elektrischer oder magnetischer Felder umfassen, die auf den einander zugewandten Seiten der Wand- und Flügelübertragerteile offen sind. Damit Fertigungstoleranzen selbsttätig ausgeglichen werden, können die eigentlichen Übertragerbauteile in den Gehäusen schwimmend gelagert sein, beispielsweise durch eine nachgiebige Schicht in einem zwischen dem Übertragerbauteil und dem Gehäuse befindlichen Spaltraum.The wall and / or wing transmitter parts can comprise housings for shielding electrical or magnetic fields, which are open on the mutually facing sides of the wall and wing transmitter parts. So that manufacturing tolerances are automatically compensated for, the actual transmitter components can be floatingly supported in the housings, for example by a flexible layer in a gap between the transmitter component and the housing.

Die erfindungsgemäße Vorrichtung weist vorzugsweise darüber hinaus Mittel zur Verdrehsicherung der Wand- oder Flügelübertragerteile in dem Band- oder dem Flügelteil auf. Es wird so verhindert, dass eventuelle beim Öffnen oder Schließen des Flügels zwischen den Wand- und den Flügelübertragerteilen entstehende Mitnahmekräfte, beispielsweise durch eingedrungene Verunreinigungen, zu einem Abriss von eventuell vorhandenen Anschlusskabeln der Übertragerteile führen.The device according to the invention preferably also has means for securing the wall or wing transmitter parts against rotation in the band or the Wing part on. This prevents any entrainment forces that arise between the wall and the wing transmitter parts when the wing is opened or closed, for example due to the ingress of contaminants, from tearing off any existing connection cables of the transmitter parts.

Die Mittel zur Verdrehsicherung können einen an dem Wand- oder Flügelübertragerteil vorgesehenen Vorsprung umfassen, der in eine an dem Wand- oder Flügelteil vorgesehene Ausnehmung hineinragt. Diese Ausnehmung kann etwa senkrecht zur Scharnierachse verlaufende Begrenzungsflächen umfassen, die Verstellwegbegrenzungen für das Wand- oder das Flügelübertragerteil bilden.The means for securing against rotation can comprise a projection provided on the wall or wing transmission part, which protrudes into a recess provided on the wall or wing part. This recess can include boundary surfaces running approximately perpendicular to the hinge axis, which form adjustment path limitations for the wall or wing transmitter part.

Der Vorsprung kann einen Kanal zum Durchführen von Anschlusskabeln des Wand- oder des Flügelübertragerteils aufweisen, um so einen besonders wirksamen Schutz gegen Anschlusskabelbeschädigungen zu bewirken.The projection can have a channel for the passage of connecting cables of the wall or wing transmitter part, in order to provide particularly effective protection against damage to the connecting cable.

Die Erfindung soll anhand der beigefügten Zeichnungen weiter erläutert werden. Es zeigen:

Fig. 1
ein erstes Ausführungsbeispiel einer erfindungsgemäßen Vorrichtung in einer perspektivischen Ansicht mit Energie- und Signalübertragern in Funktionspositionen;
Fig. 2
dasselbe Ausführungsbeispiel im Längsschnitt durch die Scharnierachse;
Fig. 3
dasselbe Ausführungsbeispiel in einer Fig. 1 entsprechenden Ansicht, jedoch mit Energie- und Signalübertragern in Montageposition;
Fig. 4
dasselbe Ausführungsbeispiel in einer Fig. 1 und 3 entsprechenden Ansicht, jedoch mit Flügelteil in Explosionsdarstellung;
Fig. 5
den Verlagerantrieb mit angesetztem Drehwerkzeug in einer Einzeldarstellung;
Fig. 6
einen Schnitt entlang der Schnittebene VI in Fig. 1;
Fig. 7
den Ausschnitt A in Fig. 6 in einer vergrößerten Darstellung;
Fig. 8
ein zweites Ausführungsbeispiel einer erfindungsgemäßen Vorrichtung in einem Längsschnitt durch die Scharnierachse mit in Funktionsposition befindlichen Energie- und Signalübertragern;
Fig. 9
dasselbe Ausführungsbeispiel wie in Fig. 8 in einer entsprechenden Ansicht, jedoch mit Energie- und Signalübertragern in Montageposition;
Fig. 10
das Flügelteil eines dritten Ausführungsbeispiels einer erfindungsgemäßen Vorrichtung in einer perspektivischen Explosionsdarstellung;
Fig. 11
den Verlagerungsantrieb dieses dritten Ausführungsbeispiels in einer Einzeldarstellung;
Fig. 12
den Verlagerungsantrieb gemäß Fig. 11 in einer teilgeschnittenen Darstellung sowie
Fig. 13
die Einzelheit X in Fig. 12 in einer vergrößerten Darstellung.
The invention will be further explained with reference to the accompanying drawings. Show it:
Fig. 1
a first embodiment of an apparatus according to the invention in a perspective view with energy and signal transmitters in functional positions;
Fig. 2
the same embodiment in longitudinal section through the hinge axis;
Fig. 3
the same embodiment in one Fig. 1 corresponding view, but with energy and signal transmitters in the mounting position;
Fig. 4
the same embodiment in one Fig. 1 and 3 corresponding view, but with the wing part in an exploded view;
Fig. 5
the displacement drive with attached turning tool in a single view;
Fig. 6
a section along the section plane VI in Fig. 1 ;
Fig. 7
the section A in Fig. 6 in an enlarged view;
Fig. 8
a second embodiment of a device according to the invention in a longitudinal section through the hinge axis with energy and signal transmitters in the functional position;
Fig. 9
the same embodiment as in Fig. 8 in a corresponding view, but with energy and signal transmitters in the mounting position;
Fig. 10
the wing part of a third embodiment of a device according to the invention in a perspective exploded view;
Fig. 11
the displacement drive of this third embodiment in an individual representation;
Fig. 12
the displacement drive according to Fig. 11 in a partially sectioned representation as well
Fig. 13
the detail X in Fig. 12 in an enlarged view.

Das in der Zeichnung als Ganzes mit 100 bezeichnete Ausführungsbeispiel einer erfindungsgemäßen Vorrichtung ist einem dreiteiligen Band nachgebildet. Es umfasst zwei in Richtung der Scharnierachse S voneinander beabstandete Wandteile 1, 2, an welche Befestigungsteile 3, 4 angeformt sind.The embodiment of an apparatus according to the invention, designated 100 as a whole in the drawing, is modeled on a three-part band. It comprises two wall parts 1, 2 spaced apart from one another in the direction of the hinge axis S, onto which fastening parts 3, 4 are molded.

In dem Abstandsraum 5 zwischen den beiden Wandteilen 1, 2 ist ein Flügelteil 6 angeordnet. Das Flügelteil 6 ist um die Scharnierachse S verschwenkbar. Es umfasst ein Befestigungsteil 7, mittels welchem es an einem in der Zeichnung nicht dargestellten Flügel befestigbar ist.A wing part 6 is arranged in the space 5 between the two wall parts 1, 2. The wing part 6 can be pivoted about the hinge axis S. It comprises a fastening part 7, by means of which it can be fastened to a wing, not shown in the drawing.

Wie insbesondere in Fig. 2 erkennbar ist, umfasst die Vorrichtung 100 einen Energieübertrager 8, der insbesondere der Übertragung von elektrischer Betätigungsleistung von einer Wand in den Flügel dient, die von an dem Flügel vorgesehenen Verbrauchern zu deren Antrieb benötigt wird. Der Energieübertrager 8 umfasst ein in dem Wandteil 1 vorgesehenes Wandübertragerteil 9 sowie ein in dem Flügelteil 6 vorgesehenes Flügelübertragerteil 10. Wand- und Flügelübertragerteil 9, 10 sind als Induktionsspulen zur gegenseitigen induktiven Ankopplung ausgebildet. Sie umfassen jeweils einen weichmagnetischen Spulenkörper 11, 12, welcher eine jeweilige Spulenwicklung 13, 14 mit Ausnahme auf den einander zugewandten Seiten vollständig umgibt. Beide Spulenkörper weisen jeweils einen zentralen Kern 15, 16 auf, die in diesem Ausführungsbeispiel der Vorrichtung 100 massiv ausgebildet sind. Die einander zugewandten Stirnseiten der Spulenkörper 11, 12 inklusive der Kerne 15, 16 sind eben ausgebildet.As especially in Fig. 2 As can be seen, the device 100 comprises an energy transmitter 8, which is used in particular to transmit electrical actuating power from a wall into the wing, which is required by consumers provided on the wing to drive it. The energy transmitter 8 comprises a wall transmitter part 9 provided in the wall part 1 and a wing transmitter part 10 provided in the wing part 6. The wall and wing transmitter parts 9, 10 are designed as induction coils for mutual inductive coupling. They each comprise a soft magnetic coil body 11, 12 which completely surrounds a respective coil winding 13, 14, with the exception of the sides facing one another. Both coil formers each have a central core 15, 16, which are solid in this embodiment of the device 100. The mutually facing end faces of the coil former 11, 12 including the cores 15, 16 are flat.

Mit Ausnahme der einander zugewandten Seiten sind die Spulenkörper 11, 12 und damit die eigentlichen Übertragerteile 9, 10 von Gehäusen 17, 18 umgeben, welche der Abschirmung äußerer Störgrößen, bei dem dargestellten Ausführungsbeispiel insbesondere äußerer Magnetfelder dienen. Die Gehäuse 17, 18 sind derart ausgestaltet, dass sie auf der einander zugewandten Seite durch angeformte, komplementäre Fasen überlappen. Das Gehäuse 17 des Wandübertragerteils 9 weist hierzu einen radial vorstehenden Umfangsbund 19 auf, welcher sogleich eine Anlagefläche zwecks Positionierung des Gehäuses 17 in dem Wandteil 1 bildet.With the exception of the sides facing each other, the bobbins 11, 12 and thus the actual transmitter parts 9, 10 are surrounded by housings 17, 18, which serve to shield external interference, in particular external magnetic fields in the exemplary embodiment shown. The housings 17, 18 are designed such that they overlap on the mutually facing side by integrally formed, complementary chamfers. For this purpose, the housing 17 of the wall transmitter part 9 has a radially protruding circumferential collar 19, which immediately forms a contact surface for the purpose of positioning the housing 17 in the wall part 1.

Zwischen den Gehäusen 17, 18 und den jeweiligen Spulenkörpern 11, 12 ist jeweils eine Schicht 20 aus einem nachgiebigen Material vorgesehen, welche für eine Art schwimmende Lagerung der Spulenkörper 11, 12 sorgt. Durch diese wird sichergestellt, dass die beiden Spulenkörper 11, 12 im montierten Zustand selbst ausrichten, zumindest im Wesentlichen vollflächig aneinanderliegen.Between the housings 17, 18 and the respective bobbins 11, 12, a layer 20 of a resilient material is provided, which ensures a kind of floating mounting of the bobbins 11, 12. This ensures that the two bobbins 11, 12 align themselves in the assembled state, or at least essentially lie against one another over the entire surface.

Die erfindungsgemäße Vorrichtung 100 weist zusätzlich zu dem Energieübertrager 8 einen Signalübertrager 21 auf, dessen grundsätzlicher Aufbau demjenigen des Energieübertragers 8 entspricht. Er umfasst dementsprechend ebenfalls ein Wandübertragerteil 22, welches in dem zweiten Wandteil 2 vorgesehen ist. Das Flügelübertragerteil 23 ist wiederum in dem Flügelteil 6, jedoch auf der dem Flügelübertragerteil 10 des Energieübertragers 8 fort weisenden Seite angeordnet. Zwecks Vermeidung von Wiederholungen sei hinsichtlich des Weiteren konstruktiven Aufbaus der Wand- und Flügelübertragerteile 22, 23 des Signalübertragers 21 und deren Anordnung in dem Wandteil 2 bzw. dem Flügelteil 6 auf die Ausführungen zum Energieübertrager 8 verwiesen. Es versteht sich, dass die Bauteile des Energieübertragers 8 und diejenigen des Signalübertragers 21 hinsichtlich ihrer elektrischen und elektromagnetischen Eigenschaften sowie ihrer Dimensionierungen auch unterschiedlich ausgebildet sein können, um die beiden Übertrager bestmöglich an die zu übertragenden Leistungen bzw. Signalen anzupassen.In addition to the energy transmitter 8, the device 100 according to the invention has a signal transmitter 21, the basic structure of which corresponds to that of the energy transmitter 8. Accordingly, it also includes Wall transmitter part 22, which is provided in the second wall part 2. The wing transmitter part 23 is in turn arranged in the wing part 6, but on the side facing away from the wing transmitter part 10 of the energy transmitter 8. In order to avoid repetitions, with regard to the further structural design of the wall and wing transmitter parts 22, 23 of the signal transmitter 21 and their arrangement in the wall part 2 or the wing part 6, reference is made to the explanations for the energy transmitter 8. It goes without saying that the components of the energy transmitter 8 and those of the signal transmitter 21 can also be designed differently with regard to their electrical and electromagnetic properties and their dimensions, in order to adapt the two transmitters as best as possible to the powers or signals to be transmitted.

Um das mit den Flügelübertragerteilen 10, 23 vormontierte Flügelteil 6 in den Abstandsraum 5 zwischen den Wandteilen 1, 2 einsetzen zu können, sind die Flügelübertragerteile 10, 23 in Richtung der Scharnierachse S verlagerbar in dem Flügelteil 6 angeordnet. Hierzu sind in dem Flügelteil 6 Aussparungen 24, 25 vorgesehen, welche derart an die Außenkonturen der Gehäuse 17, 18 der Flügelübertragerteile 10, 23 angepasst sind, dass diese im Wesentlichen ohne seitliches Spiel von den Aussparungen aufgenommen werden.In order to be able to insert the wing part 6 preassembled with the wing transmission parts 10, 23 into the space 5 between the wall parts 1, 2, the wing transmission parts 10, 23 are arranged displaceably in the wing part 6 in the direction of the hinge axis S. For this purpose, recesses 24, 25 are provided in the wing part 6, which are adapted to the outer contours of the housings 17, 18 of the wing transmitter parts 10, 23 such that they are received by the recesses essentially without lateral play.

Zwischen den beiden Aussparungen 24, 25 in Richtung der Scharnierachse S fixiert ist ein Verlagerantrieb 26 angeordnet. Er ist in einer Einzeldarstellung zusammen mit einem zu seiner Betätigung vorgesehenen Drehwerkzeug in Fig. 5 abgebildet. Er umfasst eine beispielsweise aus einem Kunststoffformteil bestehende Spindelaufnahme 27, welche eine im Querschnitt etwa schlüssellochförmige Öffnung 28 aufweist, die sich durch die in Fig. 5 dem Betrachter zugewandte Seitenwand 29 hindurch erstreckt. Ferner umfasst die Öffnung 28 einen sich seitlich erweiternden, etwa schlitzförmigen Bereich 30. Die Öffnung 28 dient der Lagerung einer Stellspindel 31, sie umfasst einen zentralen, zylinderförmigen Bereich 32, welcher im Wesentlichen spielfrei innerhalb der Öffnung 28 gelagert ist. Die Kontur der schlüssellochförmigen Öffnung 28 ist derart an den Außendurchmesser des Bereichs 32 angepasst, dass die Stellspindel 31 unter Überwindung einer elastischen Kraft durch den Schmalbereich der schlüssellochförmigen Öffnung von der Seitenwand 29 her in die Spindelaufnahme 27 eingeclipst werden kann.A displacement drive 26 is arranged between the two cutouts 24, 25 in the direction of the hinge axis S. It is shown in a single representation together with a turning tool intended for its actuation Fig. 5 displayed. It comprises a spindle receptacle 27 consisting, for example, of a plastic molded part, which has an opening 28 which is approximately keyhole-shaped in cross section and which extends through the in FIG Fig. 5 extends sidewall 29 facing the viewer. Furthermore, the opening 28 comprises a laterally widening, approximately slot-shaped region 30. The opening 28 serves to support an adjusting spindle 31, it comprises a central, cylindrical region 32 which is mounted within the opening 28 essentially without play. The contour of the keyhole-shaped opening 28 is adapted to the outer diameter of the area 32 such that the adjusting spindle 31 overcomes an elastic one Force can be clipped into the spindle receptacle 27 from the side wall 29 through the narrow region of the keyhole-shaped opening.

An den Bereich 32 angeformt ist ein radial nach außen überstehendes Kronenrad 39, welches eine Verzahnung 40 trägt, die für den Eingriff eines wahlweise ansetzbaren Vielkantdrehwerkzeugs 41 vorgesehen ist. Um dieses Drehwerkzeug 41 ansetzen zu können, ist an der Spindelaufnahme 27 eine Bohrung vorgesehen, die in Fig. 5 nicht erkennbar ist. Eine Teillänge dieser Bohrung ist mit einem Außengewinde versehen, in welches eine ein Arretierelement 36 bildende Stiftschraube 37 zur wahlweisen Arretierung der Stellspindel 31 eindrehbar ist. Im vollständig eingedrehten Zustand drückt die Stiftschraube 37 mit ihrem in Eindrehrichtung voreilenden Ende gegen die Stellspindel 31.A crown wheel 39 protruding radially outward is formed on the area 32 and bears a toothing 40 which is provided for the engagement of an optionally applicable polygonal turning tool 41. In order to be able to apply this turning tool 41, a bore is provided on the spindle receptacle 27 Fig. 5 is not recognizable. A partial length of this bore is provided with an external thread, into which a stud screw 37 forming a locking element 36 can be screwed for optional locking of the adjusting spindle 31. In the fully screwed-in state, the stud 37 presses with its leading end in the screwing-in direction against the adjusting spindle 31.

An den Bereich 32 der Stellspindel 31 schließen sich in Richtung der Drehachse D der Stellspindel 31 Gewindebereiche 42, 43 an. Das Außengewinde des einen Gewindebereichs ist als Rechtsgewinde, das Außengewinde des anderen Gewindebereichs als Linksgewinde ausgebildet. Mit diesen Gewindebereichen greift die Stellspindel 31, wie insbesondere in Fig. 2 erkennbar ist, in komplementäre Gewindebohrungen 44, 45, die als Spindelmuttern 34, 35 dienen, der Gehäuse der Flügelübertragerteile 10, 23, so dass diese durch Drehbetätigung der Stellspindel - je nach Drehsinn - aufeinander zu oder voneinander fort bewegt werden. Um eine Begrenzung des Verlagerungsweges durch Anschlagen der stirnseitigen Enden der Gewindebereiche 42, 43 an Spulenkörpern der Flügelübertragerteile zu vermeiden, sind an den Spulenkörpern Blindbohrungen 46, 47 vorgesehen, in welche Teile der Gewindebereiche 42, 43 hineinragen können. Derartige Blindbohrungen sind auch bei den Spulenkörpern der Wandübertragerteile vorgesehen (hier jedoch funktionslos), damit zur Reduzierung von Fertigungskosten dieselben Spulenkörper verwendet werden können.Threaded areas 42, 43 adjoin area 32 of adjusting spindle 31 in the direction of axis of rotation D of adjusting spindle 31. The external thread of one thread area is designed as a right-hand thread, and the external thread of the other thread area is designed as a left-hand thread. With these threaded areas, the adjusting spindle 31 engages, as in particular in Fig. 2 is recognizable, in complementary threaded bores 44, 45, which serve as spindle nuts 34, 35, the housing of the wing transmission parts 10, 23, so that these are moved toward or away from one another by rotary actuation of the adjusting spindle, depending on the direction of rotation. In order to avoid limiting the displacement path by striking the ends of the threaded areas 42, 43 on the bobbins of the wing transmitter parts, blind bores 46, 47 are provided on the bobbins, into which parts of the threaded areas 42, 43 can protrude. Such blind bores are also provided in the bobbins of the wall transmitter parts (but here inoperative) so that the same bobbins can be used to reduce manufacturing costs.

Wie insbesondere aus Fig. 2 sinnfällig wird, können die beiden Flügelübertragerteile 10, 23 durch Drehbetätigung der Stellspindel 31 mit Hilfe eines Drehwerkzeugs aufeinander zu bewegt werden, so dass sie - wie in Fig. 3 dargestellt ist - in den Abstandsraum 5 zwischen den Bandteilen 1, 2 zurückverlagert werden, so dass das Flügelteil 6 aus dem Abstandsraum 5 heraus verlagert werden kann.How especially out Fig. 2 is obvious, the two wing transmitter parts 10, 23 can be moved towards each other by turning the adjusting spindle 31 with the help of a turning tool, so that they - as in Fig. 3 is shown - be moved back into the space 5 between the band parts 1, 2, so that the wing part 6 can be moved out of the space 5.

Insbesondere in Fig. 4, 6 und 7 ist erkennbar, dass an den Flügelübertragerteilen 10, 23 Mittel zur Verdrehsicherung 48 in Form von Vorsprüngen 49 vorgesehen sind. Diese Vorsprünge 49 greifen in Vertiefungen 50 in dem Befestigungsteil 7 ein, die bei vollständig montierter Vorrichtung durch eine Abdeckkappe 53 überdeckt sind. Diese Abdeckkappe wird mit Hilfe einer Halteschraube 51 gesichert. Die Vertiefungen 50 umfassen etwa senkrecht zur Scharnierachse S verlaufende Begrenzungsflächen 54, die Verstellwegbegrenzungen für das Wand- oder das Flügelübertragerteil bilden.Especially in Fig. 4 . 6 and 7 it can be seen that means for securing against rotation 48 in the form of projections 49 are provided on the wing transmitter parts 10, 23. These projections 49 engage in depressions 50 in the fastening part 7, which are covered by a cover cap 53 when the device is fully assembled. This cover cap is secured using a retaining screw 51. The depressions 50 comprise boundary surfaces 54 which run approximately perpendicular to the hinge axis S and which form adjustment path limitations for the wall or wing transmitter part.

Die Vorsprünge 49 umfassen - wie insbesondere in Fig. 7 erkennbar ist - jeweils einen Kanal 52, durch den in der Zeichnung nicht erkennbare Anschlusskabel des jeweiligen Flügelübertragerteils geschützt hindurchführbar sind.The projections 49 comprise - as in particular in FIG Fig. 7 is recognizable - in each case a channel 52 through which connecting cables of the respective wing transmitter part, which cannot be seen in the drawing, can be guided in a protected manner.

Es versteht sich, dass auch die Rahmenübertragerteile entsprechend ausgestaltete Mittel zur Verdrehsicherung aufweisen können.It goes without saying that the frame transmitter parts can also have appropriately designed means for securing against rotation.

Ein weiteres Ausführungsbeispiel 200 einer erfindungsgemäßen Vorrichtung ist in den Fig. 8 und 9 dargestellt. Nachfolgend soll zwecks Vermeidung von Wiederholungen lediglich auf die Unterschiede zum Ausführungsbeispiel 100 eingegangen werden. Es wird auf die Beschreibung des Ausführungsbeispiels 100 voll umfänglich Bezug genommen, sofern die nachfolgenden Erläuterungen nicht hierzu im Widerspruch stehen.Another exemplary embodiment 200 of a device according to the invention is shown in FIGS 8 and 9 shown. In order to avoid repetitions, only the differences from the exemplary embodiment 100 will be discussed below. Reference is made to the description of exemplary embodiment 100 in its entirety, provided that the explanations below do not contradict this.

Bei dem Ausführungsbeispiel 200 ist der Verlagerantrieb 126 in dem oberen Wandteil 101 vorgesehen. Er umfasst eine Stellspindel 131, die in eine Gewindeaufnahme 154 innerhalb des Wandteils 101 eingedreht ist. Die Stellspindel 131 weist eine zentrale Durchgangsbohrung 155 auf, an deren oberen Ende eine Mehrkantausnehmung 156 zum Ansetzen eines Drehwerkzeugs vorgesehen ist.In the exemplary embodiment 200, the displacement drive 126 is provided in the upper wall part 101. It comprises an adjusting spindle 131, which is screwed into a threaded receptacle 154 within the wall part 101. The adjusting spindle 131 has a central through bore 155, at the upper end of which a polygonal recess 156 is provided for attaching a turning tool.

In Richtung der Scharnierachse S formschlüssig mit der Stellspindel 131 verbunden ist das Wandübertragerteil 109, welches in Richtung der Scharnierachse S verlagerbar innerhalb des Wandteils 101 angeordnet ist. Durch Drehbetätigung der Stellspindel 131 lässt sich somit das Wandübertragerteil 109 zwischen der in Fig. 8 dargestellten Betriebsstellung und der in Fig. 9 dargestellten Montagestellung verlagern, wodurch eine Montage und Demontage des Flügelteils 106 auf einfache Weise möglich ist.In the direction of the hinge axis S, the wall transmitter part 109 is positively connected to the adjusting spindle 131 and is arranged displaceably in the direction of the hinge axis S within the wall part 101. By rotating the adjusting spindle 131, the wall transmitter part 109 can thus be between the in Fig. 8 shown operating position and in Fig. 9 shift illustrated assembly position, whereby an assembly and disassembly of the wing part 106 is possible in a simple manner.

Weiterhin unterscheidet sich das Ausführungsbeispiel 200 von dem zuvor beschriebenen Ausführungsbeispiel 100, dass sämtliche Spulenkörper eine zentrale Längsbohrung 157 umfassen. In diese kann ein ein- oder auch mehrteilig ausgebildeter Bandbolzen 158 eingeführt werden, der die Übertragerteile zueinander ausrichtet.Furthermore, the exemplary embodiment 200 differs from the previously described exemplary embodiment 100 in that all the coil bodies comprise a central longitudinal bore 157. A single or multi-part hinge pin 158, which aligns the transmitter parts to one another, can be inserted into this.

Bei dem in Fig. 10 dargestellten, dritten Ausführungsbeispiel 300, von welchem lediglich das Flügelteil in Explosionsdarstellung wiedergegeben ist, weist der Verlagerungsantrieb 226 wiederum eine Spindelaufnahme 227 auf, die beispielsweise aus einem Metallformteil bestehen kann. Die Spindelaufnahme 227 weist - wie auch die Spindelaufnahme 27 des Ausführungsbeispiels 100 - ein im Querschnitt etwa schlüssellochförmige Öffnung 228 auf, die sich durch die in Fig. 11 dem Betrachter abgewandte Seitenwand 229 hindurch erstreckt. Ferner umfasst die Öffnung 228 wiederum einen sich seitlich erweiternden, etwa schlitzförmigen Bereich 230 (s. insbesondere Fig. 12.At the in Fig. 10 The illustrated third exemplary embodiment 300, of which only the wing part is shown in an exploded view, the displacement drive 226 in turn has a spindle receptacle 227, which can consist, for example, of a metal molded part. The spindle receptacle 227, like the spindle receptacle 27 of the exemplary embodiment 100, has an opening 228 which is approximately keyhole-shaped in cross section and which is defined by the in FIG Fig. 11 extends sidewall 229 facing away from the viewer. Furthermore, the opening 228 again comprises a laterally widening, approximately slit-shaped region 230 (see in particular Fig. 12 ,

Die Öffnung 228 dient der Lagerung der Stellspindel 231. Sie umfasst einen zentralen, zylindrischen Bereich 232, welcher im Wesentlichen spielfrei innerhalb der Öffnung 228 gelagert ist.The opening 228 serves to support the adjusting spindle 231. It comprises a central, cylindrical region 232 which is mounted within the opening 228 essentially without play.

Die Kontur der schlüssellochförmigen Öffnung 228 ist derart an den Außendurchmesser des Bereichs 232 angepasst, dass die Stellspindel 231 durch den Schmalbereich der schlüssellochförmigen Öffnung von der Seitenwand 229 her in die Spindelaufnahme 227 eingeführt, vorzugsweise eingeclipst werden kann.The contour of the keyhole-shaped opening 228 is adapted to the outer diameter of the area 232 in such a way that the adjusting spindle 231 can be inserted, preferably clipped, into the spindle receptacle 227 through the narrow area of the keyhole-shaped opening from the side wall 229.

An den Bereich 232 angeformt ist ein nach außen überstehendes Kronenrad 239, welches eine Verzahnung 240 trägt. Sie ist - wie insbesondere in Fig. 12 und 13 erkennbar ist - für den Eingriff einer Antriebseinrichtung 259 vorgesehen. Sie umfasst einen zylindrischen Schaft 260, welcher eine Außenverzahnung 261 umfasst, welche sich in Eingriff mit der Verzahnung 240 des Kronenrads 239 befindet.A crown wheel 239 protruding outwards is formed on the area 232 and bears a toothing 240. It is - as in particular in 12 and 13 is recognizable - provided for the engagement of a drive device 259. It comprises a cylindrical shaft 260, which comprises an external toothing 261, which is in engagement with the toothing 240 of the crown gear 239.

An den Schaft 260 schließt sich nach außen hin ein Kopf 262 an, welcher eine sich nach außen hin konisch verjüngende Form hat. Die Konusfläche 263 des Kopfes liegt an einer Arretierfläche 264 des Kopfes an, so dass die Antriebseinrichtung 259 zwar um ihre Längsachse L drehbar, jedoch in Richtung der Längsachse L im Wesentlichen spielfrei in der Spindelaufnahme 227 gelagert ist.A head 262 adjoins the shaft 260 towards the outside, which head has a conically tapering shape towards the outside. The conical surface 263 of the head lies against a locking surface 264 of the head, so that the drive device 259, although rotatable about its longitudinal axis L, is mounted in the spindle receptacle 227 essentially without play in the direction of the longitudinal axis L.

Die Arretierfläche 264 ist gebildet von einer am unteren zweier Vorsprünge 265 vorgesehenen Lasche 267. Die beiden Vorsprünge 265 begrenzen eine Aufnahmeöffnung 266, in welcher die Antriebseinrichtung 259 gelagert ist. Die Lasche 267 befindet sich vor der Bestückung der Spindelaufnahme 227 mit der Antriebseinrichtung zunächst in einer etwa senkrecht von der Seitenwand der Spindelaufnahme vorstehenden Position. Nach der Bestückung mit der Antriebseinrichtung wird die Lasche 267 plastisch gebogen, so dass sie an der Konusfläche 263 der Antriebseinrichtung 259 anliegt.The locking surface 264 is formed by a tab 267 provided on the lower two projections 265. The two projections 265 delimit a receiving opening 266 in which the drive device 259 is mounted. Before the spindle receptacle 227 is equipped with the drive device, the tab 267 is initially in a position projecting approximately perpendicularly from the side wall of the spindle receptacle. After the drive device has been fitted, the tab 267 is plastically bent so that it rests on the cone surface 263 of the drive device 259.

Zum Ansetzen eines Drehwerkzeugs weist die Antriebseinrichtung einen Innensechskant 268 auf. Es versteht sich, dass auch andere Mittel, wie Schlitze, Kreuzschlitze etc. zum Ansetzen eines Drehwerkzeugs Verwendung finden können.The drive device has a hexagon socket 268 for attaching a turning tool. It goes without saying that other means, such as slots, cross slots, etc., can also be used for attaching a turning tool.

Ferner umfasst die Spindelaufnahme 227 eine Gewindebohrung 269, die versetzt zu der Aufnahmeöffnung 266 angeordnet ist. Die Gewindebohrung 269 dient der Aufnahme einer Stiftschraube 270, die gegen den Bereich 232 der Stellspindel 231 drehbar ist, um diese in einer gewünschten Position gegen selbsttätiges Verdrehen zu arretieren.Furthermore, the spindle receptacle 227 comprises a threaded bore 269 which is arranged offset to the receptacle opening 266. The threaded bore 269 serves to receive a stud screw 270 which can be rotated against the area 232 of the adjusting spindle 231 in order to lock it in a desired position against automatic rotation.

Die Stellspindel 231 greift mit ihren Gewindebereichen 242, 243 in Bohrungen von Spulenkörpern 211, 212 ein. Die Gewindebereiche weisen gegensinnige Gewinde, d.h. ein Links- und ein Rechtsgewinde auf, so dass bei einer Drehbetätigung der Verstellspindel 231 die beiden Spulenkörper je nach Drehrichtung voneinander fort, oder aufeinander zu bewegt werden.The adjusting spindle 231 engages with its threaded areas 242, 243 in bores of coil bodies 211, 212. The thread areas have opposite threads, that is, a left-hand and a right-hand thread, so that when the adjusting spindle 231 is actuated in rotation, the two coil bodies are moved away from one another or towards one another, depending on the direction of rotation.

Bezugszeichenliste:LIST OF REFERENCE NUMBERS

100, 200, 300100, 200, 300
Vorrichtungcontraption
1, 1011, 101
Wandteilwall part
22
Wandteilwall part
33
Befestigungsteilattachment portion
44
Befestigungsteilattachment portion
55
Abstandsraumdistance space
6, 106, 2066, 106, 206
Flügelteilwing part
77
Befestigungsteilattachment portion
88th
EnergieübertragerPower transformer
99
WandübertragerteilWandübertragerteil
1010
FlügelübertragerteilFlügelübertragerteil
1111
Spulenkörperbobbins
1212
Spulenkörperbobbins
1313
Spulenwicklungcoil winding
1414
Spulenwicklungcoil winding
1515
Kerncore
1616
Kerncore
1717
Gehäusecasing
1818
Gehäusecasing
1919
Umfangsbundcircumferential collar
2020
Schichtlayer
2121
SignalübertragerA signal transmitter
2222
WandübertragerteilWandübertragerteil
2323
FlügelübertragerteilFlügelübertragerteil
2424
Aussparungrecess
2525
Aussparungrecess
26, 126, 22626, 126, 226
Verlagerungsantriebdisplacement drive
27, 22727, 227
SpindelaufnahmeSpindle taper
28, 22828, 228
Öffnungopening
29, 22929, 229
SeitenwandSide wall
30, 23030, 230
BereichArea
31, 131, 23131, 131, 231
Stellspindeladjusting spindle
32, 23232, 232
BereichArea
3434
Spindelmutterspindle nut
3535
Spindelmutterspindle nut
3636
Arretierelementlocking
3737
Stiftschraubestud
39, 23939, 239
Kronenradcrown
40, 24040, 240
Verzahnunggearing
4141
Vielkant-DrehwerkzeugPolygon turning tool
42, 24242, 242
Gewindebereichthreaded portion
43, 24343, 243
Gewindebereichthreaded portion
4444
Gewindebohrungthreaded hole
4545
Gewindebohrungthreaded hole
4646
Blindbohrungblind hole
4747
Blindbohrungblind hole
4848
Mittel zur VerdrehsicherungAnti-rotation device
4949
Vorsprüngeprojections
5050
Vertiefungenwells
5151
Halteschrauberetention screw
5252
Kanalchannel
5353
Abdeckkappecap
154154
Gewindeaufnahmethreaded receptacle
155155
DurchgangsbohrungThrough Hole
156156
Mehrkantausnehmungpolygonal
157157
Längsbohrunglongitudinal bore
158158
Bandbolzenhinge bolts
259259
Antriebseinrichtungdriving means
260260
Schaftshaft
261261
Außenverzahnungexternal teeth
262262
Kopfhead
263263
Konusflächeconical surface
264264
Arretierflächelocking surface
265265
Vorsprüngeprojections
266266
Aufnahmeöffnungreceiving opening
267267
Lascheflap
268268
InnensechskantAllen
269269
Gewindebohrungthreaded hole
270270
Stiftschraubestud
DD
Drehachseaxis of rotation
LL
Längsachselongitudinal axis
SS
Scharnierachsehinge axis

Claims (15)

  1. Device (100, 200, 300) for transmitting electrical energy and/or electrical signals from a fixed wall to a wing hingedly fastened to the wall about a hinge axis (S), the device comprising a wall part (1, 101; 2) which can be fastened to the wall, comprising a wing part (6, 106, 206) which can be fastened to the wing, and comprising an energy and/or signal transmitter (8, 21) which comprises a wall transmitter part (9, 22) provided in the wall part (1, 101; 2) and a wing transmitter part (10, 23) provided in the wing part (6), at least one of the wall transmitter part or wing transmitter part being arranged such that it can be displaced in the direction of the hinge axis (S),
    characterized in that
    a selectively actuatable displacement drive (26, 126, 226) is provided, by means of which the at least one of the wall transmitter part or wing transmitter part can be displaced in the direction of the hinge axis (S) between a retracted mounting position, in which it is possible to assemble the device, and an extended functional position, in which their mutually facing sides are at a very small defined distance from one another such that they do not rub against one another.
  2. Device according to claim 1, characterized in that the displacement drive (26, 126, 226) comprises an adjusting spindle (31, 131, 231) which is, for example, mounted rotatably about the hinge axis.
  3. Device according to claim 2, characterized in that the adjusting spindle (31, 231) is, for example, arranged so as to be stationary in the hinge axis.
  4. Device according to claim 3, characterized in that the adjusting spindle (31, 231) is engaged with a spindle nut provided on the at least one wall transmitter part or wing transmitter part or connected thereto.
  5. Device according to either claim 3 or claim 4, characterized in that one threaded region (42, 242) of the adjusting spindle (31, 231) comprises a right-hand thread and another threaded region (43, 243) comprises a left-hand thread.
  6. Device according to any of claims 2 to 5, characterized in that the adjusting spindle (31, 131) comprises an apparatus for attaching a rotary actuation tool.
  7. Device according to claim 6, characterized in that the apparatus comprises external toothing.
  8. Device according to claim 6, characterized in that the apparatus comprises crown toothing.
  9. Device according to claim 8, characterized in that the crown toothing is provided on a crown gear (33) connected to the adjusting spindle (31).
  10. Device according to any of claims 1 to 5, characterized in that the adjusting spindle (231) is provided in a spindle receptacle (227) and a drive apparatus (259) for the adjusting spindle (231) is mounted in the spindle receptacle (227).
  11. Device according to claim 10, characterized in that the drive apparatus (259) comprises a shaft (260) comprising external toothing (261).
  12. Device according to claim 11, characterized in that the drive apparatus (259) has a conical surface (263) which cooperates with a locking surface (264) provided on the spindle receptacle (227).
  13. Device according to any of claims 1 to 12, characterized in that the displacement drive (26) is provided in the wing part.
  14. Device according to claim 13, a wall part (1, 2) being provided on both sides of the wing part (6) in each case as seen in the direction of the hinge axis (S), characterized in that the displacement drive (26) is arranged between two wing transmitter parts (10, 23), and two threaded regions (42, 43) of the adjusting spindle (31), one provided with a right-hand thread and the other provided with a left-hand thread, each engage in a spindle nut (34, 35) of the relevant wing transmitter part (10, 23).
  15. Device according to any of claims 1 to 14, characterized in that a locking element (36) for selectively locking the displacement drive (26, 226) is provided, which element preferably comprises a stud bolt (37, 270) which can be selectively tightened against the adjusting spindle (31, 231).
EP12816466.2A 2011-12-23 2012-12-11 Device for transmitting electrical energy from a wall to a wing fixed on the wall Active EP2795028B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL12816466T PL2795028T3 (en) 2011-12-23 2012-12-11 Device for transmitting electrical energy from a wall to a wing fixed on the wall

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE202011052457U DE202011052457U1 (en) 2011-12-23 2011-12-23 Device for transmitting electrical energy and / or electrical signals from a fixed wall to a wall-mounted wing
PCT/EP2012/075070 WO2013092297A1 (en) 2011-12-23 2012-12-11 Device for transmitting electrical energy from a wall to a swivellable element fastened on the wall

Publications (2)

Publication Number Publication Date
EP2795028A1 EP2795028A1 (en) 2014-10-29
EP2795028B1 true EP2795028B1 (en) 2020-02-12

Family

ID=47594617

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12816466.2A Active EP2795028B1 (en) 2011-12-23 2012-12-11 Device for transmitting electrical energy from a wall to a wing fixed on the wall

Country Status (8)

Country Link
US (1) US9115518B2 (en)
EP (1) EP2795028B1 (en)
CN (1) CN104053847B (en)
BR (1) BR112014015164A2 (en)
DE (1) DE202011052457U1 (en)
PL (1) PL2795028T3 (en)
RU (1) RU2014130270A (en)
WO (1) WO2013092297A1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012112854A1 (en) * 2012-12-21 2014-06-26 Dr. Hahn Gmbh & Co. Kg Method and apparatus for transmitting electrical power and signals between a fixed wall and a wing pivotally mounted to said wall
US9973241B2 (en) 2012-12-21 2018-05-15 Dr. Hahn Gmbh & Co. Kg Method and device for transmitting electric power and signals between a stationary wall and a leaf pivotably mounted on said wall
DE102013114319A1 (en) * 2013-12-18 2015-06-18 Dr. Hahn Gmbh & Co. Kg Method and device for transmitting electric power and signals between a wall and a wing which is pivotable with respect to it
US9935413B1 (en) * 2016-02-18 2018-04-03 Apple Inc. Hinge pin with electrical connection through a cylindrical pin body
CN205638004U (en) * 2016-05-27 2016-10-12 中山市富深家用制品有限公司 Utilize electrically conductive metal cabinet of hinge
US11211847B2 (en) 2017-07-13 2021-12-28 Panasonic Intellectual Property Management Co., Ltd. Hinge device provided with power generating device and capable of extracting energy from user's living activities to generate electric power
CA3193058A1 (en) * 2022-03-29 2023-09-29 Lmpg Inc. Joint assembly for luminaires

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE805361C (en) * 1948-04-08 1951-05-17 Johannes Hoercher Fish tape for doors and windows
DE812652C (en) * 1948-10-02 1951-09-03 August Lueg Adjustable hinge by means of a thread
US2729473A (en) * 1951-06-28 1956-01-03 Warshawsky Irving Electrical fixture swivel joint constructions
DE2740415A1 (en) * 1977-09-08 1979-03-22 Roemer Fa Walter Hinge assembly with threaded hinge pin - has adjusting nut with slot engaging hinge sleeve rib
US4168409A (en) * 1978-08-14 1979-09-18 Lawrence Brothers, Inc. Security hinge with sealed switch and operator concealed therein
US4412711A (en) * 1981-12-03 1983-11-01 The Stanley Works Two knuckle electrical hinge
DE3915812A1 (en) 1989-05-13 1990-11-15 Oscar Von Wedekind Breakage detector for double glazed window - has alarm sensor and source between window panes supplied via conductive strips
FR2664438B1 (en) * 1990-07-04 1994-07-22 Alcatel Radiotelephone DEVICE FORMED FROM TWO ARTICULATED ELEMENTS AROUND A HINGE AND CONNECTED BY AN ELECTRICAL CONNECTION.
US5586895A (en) * 1995-10-23 1996-12-24 Zehrung; Raymond E. Power transfer hinge
DE29921535U1 (en) * 1999-12-08 2001-04-12 Hahn Gmbh & Co Kg Dr Tape for doors, windows or the like.
DE20009082U1 (en) * 2000-05-19 2001-09-27 Dr. Hahn GmbH & Co. KG, 41189 Mönchengladbach Hinge for doors, windows and the like
TW486024U (en) * 2001-09-14 2002-05-01 Jian-Cheng Wu Improved structure of hinge of tube-like spring
DE20305769U1 (en) 2003-04-09 2003-10-30 Staude, Wolfgang, 34513 Waldeck Hinge with built-in transformer for contactless energy transfer
DE102004017314A1 (en) * 2004-04-06 2005-10-27 Valett, Klaus Device for connecting a sail to a mast comprises spacer elements provided between the mast and the luff
IT1391920B1 (en) * 2008-09-19 2012-02-02 Euroinvest S P A ADJUSTABLE HINGE FOR WINDOWS
DE202008014318U1 (en) * 2008-10-28 2010-04-01 Dr. Hahn Gmbh & Co. Kg Band to hinged about a hinge axis connecting a wing to a frame
DE102009025917B3 (en) * 2009-06-04 2011-03-03 Dr. Hahn Gmbh & Co. Kg Band to hinged about a hinge axis connecting a wing to a frame
DE102009025916B4 (en) * 2009-06-04 2011-05-12 Dr. Hahn Gmbh & Co. Kg Band to hinged about a hinge axis connecting a wing with a frame
CA2714685C (en) * 2009-09-09 2014-04-08 Paul Justus Rodgers Apparatus for transferring electric power between a closable member and a frame
DE102009044728A1 (en) 2009-12-02 2011-06-09 Dr. Hahn Gmbh & Co. Kg Method and device for transmitting electrical power from a wall to a wing hinged to this wall

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
DE202011052457U1 (en) 2013-03-25
US20140345084A1 (en) 2014-11-27
US9115518B2 (en) 2015-08-25
BR112014015164A2 (en) 2015-11-10
CN104053847A (en) 2014-09-17
RU2014130270A (en) 2016-02-20
CN104053847B (en) 2016-06-01
PL2795028T3 (en) 2020-07-13
WO2013092297A1 (en) 2013-06-27
EP2795028A1 (en) 2014-10-29

Similar Documents

Publication Publication Date Title
EP2795028B1 (en) Device for transmitting electrical energy from a wall to a wing fixed on the wall
EP2841667B1 (en) Drive for pivoting door
EP2295683B1 (en) Loop lock with offset cylinder axle
EP2527574B1 (en) Device for contactless transfer of electrical energy between a wall and a leaf fixed to this wall
WO2012123040A1 (en) Device for transmitting electric power and/or electric signals from a stationary wall to a wing fixed to the wall
WO2004071244A2 (en) Electromotive linear drive unit
WO2001036903A1 (en) Measuring rope-path sensor
WO2010049292A1 (en) Hinge for connecting a leaf to a frame so as to be hinged about a hinge axis
EP2840203A1 (en) Door or window fitting, with multi-part covering plate
EP2507886B1 (en) Device for transmitting electric power from a wall to a leaf hingeably fastened to said wall
WO2007090487A1 (en) Hinge for doors, windows or the like
DE3316834A1 (en) ACTUATING SPIN FOR THE DOOR LOCKING OF A CONTROL CABINET
DE102011006023B3 (en) Adjustable hinge strap
DE19715055C2 (en) Deadbolt
DE102012110484B4 (en) Electromechanical coupling for a panic lock
DE102006008525A1 (en) Vehicle door fixing device for motor vehicle, has anchor and rotor guided on top of each other in direction of door opening movement so that pressure between brake surface and brake anti surface is increased with increasing opening angle
DE29722488U1 (en) Cam lock for thick-walled doors, flaps or the like.
EP3284886A1 (en) Closing device for a door
DE102013211864B4 (en) Arrangement for fixing a post to a plastic frame strip of a window or a door by means of a post connector made of plastic
EP2750269B1 (en) Pump power unit
DE102013205061A1 (en) Operating device for plate, particularly for attachment to control element on operating shaft of plate, is aligned for locking quick locking ring in recess, where rosette is provided for positioning between operating device and plate
EP2634342B1 (en) Drive for a wing of a window or the like and method for fitting the drive
EP1922467B1 (en) Hinge for doors, windows or the like
EP2764189B1 (en) Spring mounting cone for a torsion spring having a torque-transmitting leg bent inward or outward
DE102007023389A1 (en) Shaft starting arrangement; Actuator and window regulator

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20140710

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: E05D 11/00 20060101AFI20190801BHEP

Ipc: E05D 7/00 20060101ALI20190801BHEP

INTG Intention to grant announced

Effective date: 20190823

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20191025

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1232310

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200215

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502012015769

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200512

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20200212

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200512

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200612

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200513

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200705

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502012015769

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20201113

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20201211

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20201231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201211

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201211

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201231

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201211

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201231

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 1232310

Country of ref document: AT

Kind code of ref document: T

Effective date: 20201211

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201211

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201211

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200212

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201231

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 502012015769

Country of ref document: DE

Representative=s name: PATENTANWAELTE KLUIN DEBELIUS WEBER PARTG MBB, DE

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230523

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20231231

Year of fee payment: 12

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: PL

Payment date: 20231208

Year of fee payment: 12