EP3030388B1 - Transfer/punching process - Google Patents

Transfer/punching process Download PDF

Info

Publication number
EP3030388B1
EP3030388B1 EP14741235.7A EP14741235A EP3030388B1 EP 3030388 B1 EP3030388 B1 EP 3030388B1 EP 14741235 A EP14741235 A EP 14741235A EP 3030388 B1 EP3030388 B1 EP 3030388B1
Authority
EP
European Patent Office
Prior art keywords
punching
layer
carrier
carrier layer
punched
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
EP14741235.7A
Other languages
German (de)
French (fr)
Other versions
EP3030388A1 (en
Inventor
Martin Bohn
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.)
BW Papersystems Stuttgart GmbH
Original Assignee
BW Papersystems Stuttgart GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BW Papersystems Stuttgart GmbH filed Critical BW Papersystems Stuttgart GmbH
Publication of EP3030388A1 publication Critical patent/EP3030388A1/en
Application granted granted Critical
Publication of EP3030388B1 publication Critical patent/EP3030388B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D7/00Details of apparatus for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
    • B26D7/01Means for holding or positioning work
    • B26D7/018Holding the work by suction
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D3/00Cutting work characterised by the nature of the cut made; Apparatus therefor
    • B26D3/08Making a superficial cut in the surface of the work without removal of material, e.g. scoring, incising
    • B26D3/085On sheet material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D7/00Details of apparatus for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
    • B26D7/18Means for removing cut-out material or waste
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26FPERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
    • B26F1/00Perforating; Punching; Cutting-out; Stamping-out; Apparatus therefor
    • B26F1/38Cutting-out; Stamping-out
    • B26F1/384Cutting-out; Stamping-out using rotating drums
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26FPERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
    • B26F1/00Perforating; Punching; Cutting-out; Stamping-out; Apparatus therefor
    • B26F1/38Cutting-out; Stamping-out
    • B26F1/44Cutters therefor; Dies therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26FPERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
    • B26F1/00Perforating; Punching; Cutting-out; Stamping-out; Apparatus therefor
    • B26F1/38Cutting-out; Stamping-out
    • B26F1/40Cutting-out; Stamping-out using a press, e.g. of the ram type
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26FPERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
    • B26F1/00Perforating; Punching; Cutting-out; Stamping-out; Apparatus therefor
    • B26F1/38Cutting-out; Stamping-out
    • B26F1/44Cutters therefor; Dies therefor
    • B26F2001/4436Materials or surface treatments therefore
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26FPERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
    • B26F1/00Perforating; Punching; Cutting-out; Stamping-out; Apparatus therefor
    • B26F1/38Cutting-out; Stamping-out
    • B26F1/44Cutters therefor; Dies therefor
    • B26F2001/4472Cutting edge section features

Definitions

  • the invention relates to a punch transfer device and a method for operating such a punch transfer device according to the respective preamble of the two independent claims.
  • Such inlays consist of a carrier, for example a carrier film made of PET, an antenna arranged on the carrier made of stamped or etched aluminum and a chip that is operatively connected to the antenna.
  • such an inlay is built into a label, a textile tag or a paper ticket as a separate layer, i.e. the end product, also known as a smart label, smart tag or smart ticket, consists of 3 layers, in particular the printed or unprinted cover material, the inlay and the printed or unprinted carrier material.
  • the WO 2009/118455 A1 describes a method for producing an inlay antenna directly on paper by gluing a metal foil over the entire surface of a carrier web that has been glued to the exact contour and then punching out the antenna contour with a laser without damaging the carrier web.
  • the waste of the unnecessary antenna contour which is not connected to the carrier web by the glue contour, does not represent a continuous, removable grid structure, as is the case with a stamped label grid, but individual separate sections that have to be removed and disposed of in a laborious manner.
  • a punch transfer device of the same generic type and a method for operating the same are known from the patent DE 10 2007 041752 A1 .
  • the invention is therefore based on the object of specifying a punching transfer device and a method for operating such a punching device with which the disadvantages described above are avoided.
  • the way in which the antenna is produced and the application of the antenna to a target component, such as a printed paper web, and the disposal of the metal foil parts of the antenna that are not required are to be facilitated.
  • the punch transfer device has a punching tool with a vacuum connection, the vacuum connection interacting with a porous elastomer.
  • a multi-layer composite can be punched out in a desired contour by means of the punching tool, the desired punched out contour being retained by means of the vacuum connection for generating a vacuum acting on the punched-out part.
  • the punched out desired contour can be transferred to a target component.
  • this target component is, for example, a product such as, for example, a paper web printed on the back, packaging or the like onto which the punched-out contour is delivered.
  • the punched-out contour is applied to a further carrier and there, for example, one punched-out contour after the other is applied to this carrier, in order to arrange a plurality of composite layers arranged one behind the other and punched out in the desired contour.
  • a multi-layer composite which consists of at least a carrier layer, an adhesive layer and a metal layer interacting therewith, is punched out in the desired contour. It is important here that the entire multilayer composite is not punched out in the desired contour, but at least only the metal layer and the adhesive layer that is operatively connected to it. Because after punching out, at least the metal layer and the adhesive layer applied to it remain in the punching tool. In order to achieve this, the vacuum connection is provided on the one hand, which holds the multilayer composite in the punching tool.
  • porous elastomer in particular with regard to its thickness and its material properties, ensures that, in interaction with the vacuum generated, the multi-layer composite is moved precisely and, above all, position-defined so far into the punching tool or the punching tool can act as far during punching, that at least the metal layer and the adhesive layer located thereon are punched, but the carrier layer is not touched by the punching tool.
  • the multilayer composite consisting of at least a metal layer, adhesive layer and carrier layer
  • the multilayer composite consisting of at least a metal layer, adhesive layer and carrier layer
  • the carrier layer can be removed together with the layers of the multilayer composite that are not required (that is, the processing waste, in particular the punching waste).
  • the adhesive layer of the metal layer for example an antenna or antenna structure
  • the metal layer can be released for further processing via its adhesive layer.
  • an antenna for an RFID inlay can be produced in a very simple manner, and this can be done in particular on a large scale.
  • the multilayer composite can be punched out rotationally and one behind the other and the punched out contours can be fed to further processing.
  • the punching tool has a cutting angle ⁇ 45 °, preferably in the range between 30 ° and 35 °. This advantageously enables precise contouring, so that the metal layer, which later forms the antenna of the RFID inlay, for example, can not only be punched out with the highest precision, but can also be held in the punching tool. This contributes to the holding by the vacuum force.
  • the punching flanks of the punching tool can be aligned symmetrically at an angle to the punching direction.
  • a punching flank of the punching tool is aligned parallel to a punching direction (asymmetrically). This has the effect that the cut edge of the metal layer is aligned parallel to the punching direction.
  • the punched-out multilayer composite consisting of at least an adhesive layer and a metal layer, is held in a defined manner in the punching tool, in addition to the interaction of the porous elastomer and the vacuum force, which in this state causes the porous elastomer to contract.
  • the carrier layer can be removed, so that the adhesive layer is initially exposed and is arranged within the axial extension of the punching flanks or within the punching tool.
  • the vacuum force can removed or at least reduced or maintained compared to the previously applied vacuum force, so that the porous elastomer, which was compressed during the punching process, can only relax in a defined manner due to its elasticity (independent of the vacuum force), so that the plane in which the The adhesive layer is moved out of the plane in which the end area of the punching flanks lies. This means that the adhesive layer is freely accessible for further processing.
  • the multilayer composite has been such a composite, which consists of a metal layer, an adhesive layer and a carrier layer.
  • a multilayer composite is, for example, a paper-aluminum composite (also referred to as a PAL composite).
  • PAL composite paper-aluminum composite
  • the multilayer composite for example the PAL composite
  • the additional adhesive layer can be punched out by means of the punching tool, with the additionally applied carrier layer is not reached by the punching tool.
  • the porous elastomer can press the multilayer composite, which was thereby previously held in the punching tool, out of the punching tool to the desired extent, so that the additional adhesive layer is exposed after peeling off the further carrier layer, and this multilayer composite can be made available for further processing.
  • the vacuum force essentially serves to hold the multilayer composite within the punching tool. It will also cause the porous elastomer to contract very slightly, if at all. However, the porous elastomer is essentially or only compressed by the forces acting during the punching process and, after the punching process, relaxes largely or completely independently of the vacuum force.
  • the Figures 1 and 2 show a punch transfer device 1 at the moment of the punching process ( Figure 1 ) and at the time of transfer of the punched contour ( Figure 2 ) before submission to further processing.
  • the punching transfer device 1 comprises a punching tool 2, such a punching tool 2 being arranged as a stand-alone tool or, for example, also present several times on a punching roller.
  • the punching tool 2 has a vacuum connection 3, a vacuum force acting on the inner contour of the punching tool 2 being able to be generated via this vacuum connection 3. This vacuum force can be changed in a controlled manner.
  • a desired contour is to be given to a multilayer composite by punching.
  • FIG. 1 and 2 it is a multi-layer composite with a first carrier layer 4, a first adhesive layer 5 present thereon, the first adhesive layer 5 being connected to a second carrier layer 6.
  • the second carrier layer 6 in turn comprises a large area of a second adhesive layer 7 on which a metal layer 8 is arranged over a large area.
  • the first carrier layer 4 is, for example, a silicone film
  • the second carrier layer 6 consists, for example, of paper
  • the metal layer 8 consists of aluminum.
  • This multilayer composite can be implemented particularly simply and inexpensively if the layers 6, 7 and 8 form the PAL composite described above. This can be used inexpensively from the roll.
  • the multi-layer composite 4 to 8 described above is fed to the punching tool 2.
  • the punching tool 2 is moved starting from the metal layer 8 in the direction of the first carrier layer 4, namely moved axially until the when the Figure 1 Lowermost contour of the punching tool 2 protrudes as far as the upper level of the first carrier layer 4 or into the level in which the first adhesive layer 5 is located.
  • the first carrier layer 4 can be supported on a counter-support (for example, flat or designed as a counter-pressure roller). So that the contour to be punched out, consisting of layers 5 to 8, is guided and held in the punching tool, punching tool 2 has a punching flank 10, this punching flank 10 advantageously running parallel (asymmetrically) to a punching direction 11.
  • the other punching flank of the punching tool 2 is provided at an angle ⁇ , preferably 45 °, more preferably in the range between 30 ° and 35 °.
  • This configuration of the punching flank 10 results in an almost right-angled punching contour with respect to the surface of the multilayer composite.
  • Both flanks of the punching tool can also be aligned symmetrically with respect to the punching direction 11.
  • This transfer to the subsequent processing takes place in that, after this punching-out process, the first carrier layer, for example the silicone film, is peeled off.
  • the remaining layers 5 to 8, which lie outside the contour of the punching tool 2 are also removed. It is important here that the adhesive forces of the adhesive layer 7 are significantly greater than those of the adhesive layer 5 in order to prevent the layers 6, 8 arranged thereon from also being pulled off when the first carrier layer 4 is peeled off.
  • the punching tool 2 not only the punching process but also the transfer process for the further processing of the punched-out multilayer composite can take place.
  • the first carrier layer 4 with the layers present around the punched out contour area is removed in a subsequent step.
  • the metal layer 8 which has been brought into the desired contour and which is connected to the further carrier layer 6 via the adhesive layer 7 thus remains within the punching tool 2.
  • This is the already mentioned PAL network.
  • this is not a limitation, since other materials can also be used.
  • this adhesive layer 5 lies during the punching process approximately in the plane that is defined by the outer edges (when looking at the Figures 1 or 3 the downwardly pointing cutting edges) of the punching flanks 10 is formed.
  • the adhesive layer 5 was not yet accessible in a defined manner for further processing.
  • the porous elastomer 9 can relax in a defined manner (the porous elastomer 9 having previously been compressed in a defined manner during the punching process due to the design of the punching tool 2).
  • the vacuum force acts on the multilayer composite located inside the punching tool 2 in order to hold it there.
  • the vacuum force applied via the vacuum connection 3 is maintained, reduced or canceled. It is advantageously retained in order to hold the multi-layer composite now punched inside the punching tool 2 there. However, it can also be reduced or canceled if the multilayer composite is transferred to the target component directly after the punching process. In any case, it is important that the adhesive forces of the adhesive layer 5 are greater than the holding forces within of the punching tool, so that by means of these adhesive forces the punched-out multilayer composite can be removed from the punching process and fed to the target component and glued there.
  • the porous elastomer 9 can relax again in a defined manner after the punching process (because the counter support has been removed), so that it presses the punched-out multilayer composite to a desired extent in the direction of a delivery direction 12 from the punching tool 2.
  • This amount of pushing out is selected such that preferably the entire adhesive layer 5 and possibly also part of the second carrier layer 6 is moved out of the plane which is delimited by the lower edges of the punching flanks 10.
  • This point in time after the reduction or removal of the vacuum force and relaxation of the porous elastomer 9 that is, an increase in the axial extent in the direction of the delivery direction 12
  • this punched-out multilayer composite 5 to 8 can be passed on to further processing (transfer).
  • the multi-layer composite within the punching tool 2 consisted of layers 5 to 8 over a large area.
  • a desired contour is given by a further, in particular preceding, machining process, in particular also a punching process.
  • the desired contour can be, for example, a recess 14 in the metal layer, but also a more complex geometry.
  • the further, in particular upstream, machining process does not have to be a punching process, but can also be carried out, for example, by a process using a laser or the like.
  • the desired overall contour to be given to the metal layer 8 is exemplified in the plan view in FIG Figure 5 shown, with the layers 5 to 8 punched out here as a multilayer composite and placed on a Target component 13 (for example a paper web) have been delivered (transferred).
  • a Target component 13 for example a paper web
  • more or fewer layers are transferred to the target component 13 after the punching process.
  • at least the metal layer 8 can be brought into a desired shape, in particular a recess 14, before the multilayer composite 4 to 8 is fed to the punching tool 2.
  • the metal layer 8 is advantageously brought into the desired contour (for example the antenna structure required for an RFID inlay) and can be subjected to the further stamping and transfer process.
  • the desired contour for example the antenna structure required for an RFID inlay
  • the second carrier layer 6 is detached from the first carrier layer 4 before the punching process and then these two layers 4, 6 are brought together again.
  • the so-called release value between the two layers 4, 6, which are connected to one another via the adhesive layer 5, is reduced.
  • a certain force must first be applied in order to overcome the adhesive forces of the adhesive layer 5 connecting the two layers 4, 6. If these two carrier layers 4, 6 are now brought together again and again detached from one another, the force (release) required for this is lower.
  • This fact is used to feed the multi-layer composite to the punching process so that it can be Execution of the punching process requires less force in order to remove the first carrier layer 4 from the punched-out multilayer composite.
  • This has an advantageous effect because it also means that only reduced forces are required to hold the multi-layer punched composite 5 to 8 in the punching tool 2 either only by shaping the punching flank 10 (possibly also by omitting the vacuum force). If the vacuum force is present, it can turn out to be smaller, since the release value of the connection between the two carrier layers 4, 6 was reduced by the previous loosening and bringing them back together. This has an advantageous effect, above all, when punching and transferring the multilayer composite in large numbers.
  • the process of bringing the two carrier layers 4, 6 together can be carried out congruently or offset from one another. If the process of bringing the two carrier layers 4, 6 together is carried out congruently, the release value is advantageously reduced, as already described. If the two carrier layers 4, 6 are brought together offset from one another, this has the advantage that the punched or otherwise processed machining of the metal layer 8, which may have reached in the direction of the first carrier layer 4, is no longer congruent after the joining . This makes it possible to advantageously ensure that when the metal layer 8 has received a filigree structure, for example an antenna structure, as a result of the further processing operation, it is easily removed from the first carrier layer 4 after the transfer, above all without damage during further processing can.
  • a filigree structure for example an antenna structure
  • the punched-out multilayer composite consisting of the carrier layer 6, the adhesive layers 5, 7 and the metal layer 8, is transferred to a further carrier layer by means of the adhesive layer 5.
  • the metal layers 8 can be traced onto the further carrier layer in their desired contour, in particular the filigree antenna structure submit for processing and transfer.
  • the carrier layer 4 is then finally removed, the multilayer composite 5 to 8 can be fed to the target component in its given contour.
  • the part of the multilayer composite that is not required outside the punching contour of the punching tool remains on the first carrier layer 4 and is disposed of together with it, for example wound up on a roll without the formation of disruptive waste.
  • the invention thus offers the very decisive advantage that, by means of the punch transfer device, only that part of the multilayer composite is punched out and fed to further processing that is also required for further processing.
  • the remaining part (remainder) of the multi-layer composite can be disposed of in the simplest possible way and individual layers do not have to be picked up and disposed of, as was previously the case in the prior art.
  • the multilayer composite can consist of layers 4 to 8 as described. However, more layers than this are also conceivable, just as a multi-layer composite can only consist of a carrier layer or adhesive layer and a further layer, in particular a metal layer, which are connected to one another via an adhesive layer.
  • the previously mentioned metal layer 8 is advantageously used to produce an antenna or antenna structure and therefore consists of an electrically conductive material (for example aluminum foil).
  • the metal layer described so far can also consist of an electrically non-conductive material (such as, for example, textile, paper, plastic film or the like).

Landscapes

  • Life Sciences & Earth Sciences (AREA)
  • Forests & Forestry (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
  • Laminated Bodies (AREA)
  • Details Of Aerials (AREA)
  • Details Of Cutting Devices (AREA)

Description

Transfer-StanzenTransfer punching

Die Erfindung betrifft eine Stanztransfervorrichtung sowie ein Verfahren zum Betreiben einer solchen Stanztransfervorrichtung gemäß dem jeweiligen Oberbegriff der beiden unabhängigen Patentansprüche.The invention relates to a punch transfer device and a method for operating such a punch transfer device according to the respective preamble of the two independent claims.

Vorrichtungen und Verfahren zum Herstellen von RFID-Inlays sind bekannt. Solche Inlays bestehen aus einem Träger, beispielsweise einer Trägerfolie aus PET, einer auf dem Träger angeordneten Antenne aus gestanztem oder geätzten Aluminium und einen mit der Antenne in Wirkverbindung stehenden Chip.Devices and methods for producing RFID inlays are known. Such inlays consist of a carrier, for example a carrier film made of PET, an antenna arranged on the carrier made of stamped or etched aluminum and a chip that is operatively connected to the antenna.

Normalerweise wird ein solches Inlay in ein Etikett, einen Textilanhänger oder ein Papierticket als eigne Lage verbaut, das heißt, das Endprodukt, auch als Smart Label, Smart Tag oder Smart Ticket bezeichnet, besteht aus 3 Lagen, wie insbesondere dem bedruckten oder unbedruckten Deckmaterial, dem Inlay und dem bedruckten oder unbedruckten Trägermaterial.Normally, such an inlay is built into a label, a textile tag or a paper ticket as a separate layer, i.e. the end product, also known as a smart label, smart tag or smart ticket, consists of 3 layers, in particular the printed or unprinted cover material, the inlay and the printed or unprinted carrier material.

Die WO 2009/118455 A1 beschreibt ein Verfahren zur Herstellung einer Inlayantenne direkt auf Papier, indem eine Metallfolie vollflächig auf eine zuvor konturgenau beleimte Trägerbahn aufgeklebt wird und anschließend die Antennenkontur mit einem Laser ausgestanzt wird, ohne die Trägerbahn zu beschädigen. Der Abfall der nicht benötigten Antennenkontur, der nicht durch die Leimkontur mit der Trägerbahn verbunden ist, stellt nicht wie bei einem Etikettenstanzgitter eine durchgehende, abziehbare Gitternetzstruktur dar, sondern einzelne getrennte Abschnitte, die aufwendig abgenommen und entsorgt werden müssen.The WO 2009/118455 A1 describes a method for producing an inlay antenna directly on paper by gluing a metal foil over the entire surface of a carrier web that has been glued to the exact contour and then punching out the antenna contour with a laser without damaging the carrier web. The waste of the unnecessary antenna contour, which is not connected to the carrier web by the glue contour, does not represent a continuous, removable grid structure, as is the case with a stamped label grid, but individual separate sections that have to be removed and disposed of in a laborious manner.

Eine gattungsgleiche Stanztransfervorrichtung und ein Verfahren zum Betreiben derselben sind bekannt aus der Patentschrift DE 10 2007 041752 A1 . Der Erfindung liegt daher die Aufgabe zugrunde, eine Stanztransfervorrichtung sowie ein Verfahren zum Betreiben einer solchen Stanzvorrichtung anzugeben, mit dem die eingangs geschilderten Nachteile vermieden werden. Insbesondere soll die Art und Weise der Antennenherstellung und die Aufbringung der Antenne auf ein Zielbauteil, wie zum Beispiel einer bedruckten Papierbahn, sowie die Entsorgung der nicht benötigten Metallfolienanteile der Antenne erleichtert werden.A punch transfer device of the same generic type and a method for operating the same are known from the patent DE 10 2007 041752 A1 . The invention is therefore based on the object of specifying a punching transfer device and a method for operating such a punching device with which the disadvantages described above are avoided. In particular, the way in which the antenna is produced and the application of the antenna to a target component, such as a printed paper web, and the disposal of the metal foil parts of the antenna that are not required are to be facilitated.

Diese Aufgabe ist durch die Merkmale der beiden unabhängigen Patentansprüche gelöst.This object is achieved by the features of the two independent claims.

Hinsichtlich der Stanztransfervorrichtung zur Herstellung von RFID-Inlays ist erfindungsgemäß vorgesehen, dass die Stanztransfervorrichtung ein Stanzwerkzeug mit einem Vakuumanschluss aufweist, wobei der Vakuumanschluss mit einem porösen Elastomer zusammenwirkt. Mittels des Stanzwerkzeuges kann ein mehrschichtiger Verbund in einer gewünschten Kontur ausgestanzt werden, wobei die gewünschte ausgestanzte Kontur mittels des Vakuumanschlusses zur Erzeugung eines auf das ausgestanzte Teil wirkende Vakuum festgehalten wird. Nachdem dieser Ausstanzvorgang stattgefunden hat, ist es möglich, dass die ausgestanzte gewünschte Kontur an ein Zielbauteil übergeben werden kann. In der einfachsten Form ist dieses Zielbauteil beispielsweise ein Produkt wie beispielsweise eine rückseitig bedruckte Papierbahn, eine Verpackung oder dergleichen, auf die die ausgestanzte Kontur abgegeben wird. Alternativ dazu ist es auch denkbar, dass die ausgestanzte Kontur auf einen weiteren Träger aufgebracht wird und dort beispielsweise eine ausgestanzte Kontur nach der anderen auf diesen Träger aufgebracht wird, um so eine Vielzahl von hintereinander angeordneten in der gewünschten Kontur ausgestanzten Verbundschichten anzuordnen.With regard to the punch transfer device for producing RFID inlays, it is provided according to the invention that the punch transfer device has a punching tool with a vacuum connection, the vacuum connection interacting with a porous elastomer. A multi-layer composite can be punched out in a desired contour by means of the punching tool, the desired punched out contour being retained by means of the vacuum connection for generating a vacuum acting on the punched-out part. After this punching process has taken place, it is possible that the punched out desired contour can be transferred to a target component. In its simplest form, this target component is, for example, a product such as, for example, a paper web printed on the back, packaging or the like onto which the punched-out contour is delivered. Alternatively, it is also conceivable that the punched-out contour is applied to a further carrier and there, for example, one punched-out contour after the other is applied to this carrier, in order to arrange a plurality of composite layers arranged one behind the other and punched out in the desired contour.

Mittels des Stanzwerkzeuges wird ein mehrschichtiger Verbund, der zumindest aus einer Trägerschicht, einer Klebeschicht und einer damit zusammenwirkenden Metallschicht besteht, in der gewünschten Kontur ausgestanzt. Hierbei ist es wichtig, dass nicht der gesamte mehrschichtige Verbund in der gewünschten Kontur ausgestanzt wird, sondern zumindest nur die Metallschicht und die damit in Wirkverbindung stehende Klebeschicht. Denn nach dem Ausstanzen soll mindestens die Metallschicht und die daran darauf aufgebrachte Klebeschicht in dem Stanzwerkzeug verbleiben. Um dies zu realisieren, ist einerseits der Vakuumanschluss vorgesehen, der den mehrschichtigen Verbund in dem Stanzwerkzeug hält. Gleichzeitig muss sichergestellt werden (vor allen Dingen mit höchster Präzision), dass die Schneide des Stanzwerkzeuges der Metallschicht und der darauf aufgebrachten Klebeschicht die gewünschte Kontur gibt, indem sie ausgestanzt wird, jedoch die Trägerschicht nicht gestanzt wird. Dies ist erforderlich, da sie nach dem Stanzen entfernt werden soll und der Metallschicht-Klebeschicht-Verbund der ausgestanzt wurde, für die nachfolgende Bearbeitung beziehungsweise Weiterverarbeitung bereitgestellt werden soll. Um mittels des Vakuumanschlusses erzeugtes Vakuum auf den mehrschichtigen Verbund wirken zu lassen, ist weiterhin ein poröses Elastomer vorhanden. Dieses poröse Elastomer hat zum Einen den Vorteil, dass das Vakuum, welches einen Unterdruck zum Festhalten des mehrschichtigen Verbundes in dem Stanzwerkzeug erzeugt, flächig auf den mehrschichtigen Verbund wirken kann. Außerdem bewirkt eine entsprechende Abstimmung des porösen Elastomers, insbesondere hinsichtlich seiner Dicke und seiner Materialeigenschaften, dass im Zusammenspiel mit dem erzeugten Vakuum der mehrschichtige Verbund präzise und vor allen Dingen lagedefiniert so weit in das Stanzwerkzeug hinein bewegt wird beziehungsweise das Stanzwerkzeug soweit beim Stanzen wirken kann, dass mindestens die Metallschicht und die darauf befindliche Klebeschicht gestanzt wird, die Trägerschicht aber von dem Stanzwerkzeug nicht berührt wird. Dadurch wird in dem Zusammenspiel zwischen dem verformbaren porösen Elastomer und dem erzeugten Vakuum sichergestellt, dass der mehrschichtige Verbund, bestehend mindestens aus Metallschicht, Klebeschicht und Trägerschicht, so in dem Stanzwerkzeug ausgestanzt und festgehalten wird, dass nach dem Stanzvorgang mindestens die Metallschicht mit ihrer Klebeschicht in dem Stanzwerkzeug verbleibt und die Trägerschicht zusammen mit den nicht benötigten Schichten des mehrschichtigen Verbundes (also der Bearbeitungsabfall, insbesondere der Stanzabfall) entfernt werden kann. Nach dem Entfernen der Trägerschicht liegt die Klebeschicht der Metallschicht (zum Beispiel einer Antenne oder Antennenstruktur) frei, so dass dadurch die Metallschicht über ihre Klebeschicht der weiteren Verarbeitung abgegeben werden kann. Damit lässt sich in sehr einfacher Art und Weise eine Antenne für ein RFID-Inlay herstellen, wobei dies insbesondere massenweise erfolgen kann. Hierzu ist in Weiterbildung der Erfindung vorgesehen, dass mehrere Stanzwerkzeuge auf einer Stanzwalze auf deren Umfang verteilt angeordnet sind. Somit kann mittels dieser auf der Stanzwalze angeordneten Stanzwerkzeuge rotatorisch und hintereinander der mehrschichtige Verbund ausgestanzt und die ausgestanzten Konturen der weiteren Verarbeitung zugeführt werden.By means of the punching tool, a multi-layer composite, which consists of at least a carrier layer, an adhesive layer and a metal layer interacting therewith, is punched out in the desired contour. It is important here that the entire multilayer composite is not punched out in the desired contour, but at least only the metal layer and the adhesive layer that is operatively connected to it. Because after punching out, at least the metal layer and the adhesive layer applied to it remain in the punching tool. In order to achieve this, the vacuum connection is provided on the one hand, which holds the multilayer composite in the punching tool. At the same time, it must be ensured (above all with the highest precision) that the cutting edge of the punching tool gives the metal layer and the adhesive layer applied to it the desired contour by being punched out, but the carrier layer is not punched. This is necessary because it is to be removed after punching and the metal layer-adhesive layer composite that was punched out is to be made available for subsequent processing or further processing. In order to allow the vacuum generated by the vacuum connection to act on the multilayer composite, a porous elastomer is also present. This porous elastomer has the advantage, on the one hand, that the vacuum, which generates a negative pressure to hold the multilayer composite in place in the punching tool, can act on the multilayer composite over a large area. In addition, appropriate coordination of the porous elastomer, in particular with regard to its thickness and its material properties, ensures that, in interaction with the vacuum generated, the multi-layer composite is moved precisely and, above all, position-defined so far into the punching tool or the punching tool can act as far during punching, that at least the metal layer and the adhesive layer located thereon are punched, but the carrier layer is not touched by the punching tool. This ensures in the interaction between the deformable porous elastomer and the vacuum generated that the multilayer composite, consisting of at least a metal layer, adhesive layer and carrier layer, is punched out and held in the punching tool in such a way that after the punching process at least the metal layer with its adhesive layer is in the punching tool remains and the carrier layer can be removed together with the layers of the multilayer composite that are not required (that is, the processing waste, in particular the punching waste). After removing the carrier layer, the adhesive layer of the metal layer (for example an antenna or antenna structure), so that the metal layer can be released for further processing via its adhesive layer. In this way, an antenna for an RFID inlay can be produced in a very simple manner, and this can be done in particular on a large scale. For this purpose, it is provided in a further development of the invention that several punching tools are arranged on a punching roller distributed over its circumference. Thus, by means of these punching tools arranged on the punching roller, the multilayer composite can be punched out rotationally and one behind the other and the punched out contours can be fed to further processing.

In Weiterbildung der Erfindung ist vorgesehen, dass das Stanzwerkzeug einen Schneidwinkel ≤ 45°, vorzugsweise im Bereich zwischen 30° und 35°, aufweist. Dadurch ist in vorteilhafter Weise eine präzise Konturgebung möglich, so dass die Metallschicht, die beispielsweise später die Antenne des RFID-Inlays bildet, nicht nur mit höchster Präzision ausgestanzt, sondern auch in dem Stanzwerkzeug festgehalten werden kann. Dies trägt zu dem Halten mittels der Vakuumkraft bei. Die Stanzflanken des Stanzwerkzeuges können symmetrisch abgewinkelt zu der Stanzrichtung ausgerichtet sein.In a further development of the invention it is provided that the punching tool has a cutting angle ≤ 45 °, preferably in the range between 30 ° and 35 °. This advantageously enables precise contouring, so that the metal layer, which later forms the antenna of the RFID inlay, for example, can not only be punched out with the highest precision, but can also be held in the punching tool. This contributes to the holding by the vacuum force. The punching flanks of the punching tool can be aligned symmetrically at an angle to the punching direction.

In Weiterbildung der Erfindung ist eine Stanzflanke des Stanzwerkzeuges parallel zu einer Stanzrichtung ausgerichtet (asymmetrisch). Dadurch wird bewirkt, dass die Schnittkante der Metallschicht parallel zu der Stanzrichtung ausgerichtet ist. Dies hat den Vorteil, dass dadurch der ausgestanzte mehrschichtige Verbund, bestehend mindestens aus Klebeschicht und Metallschicht, definiert in dem Stanzwerkzeug gehalten wird, zusätzlich zu dem Zusammenwirken des porösen Elastomers und der Vakuumkraft, die in diesem Zustand ein Zusammenziehen des porösen Elastomers bewirkt. Nachdem der Stanzvorgang beendet ist kann die Trägerschicht entfernt werden, so dass dadurch zunächst die Klebeschicht freiliegt und innerhalb der axialen Erstreckung der Stanzflanken oder innerhalb des Stanzwerkzeuges angeordnet ist. In diesem Zustand ist es nicht möglich oder nicht großflächig möglich, die Klebeschicht für die weitere Verarbeitung heranzuziehen. Die Vakuumkraft kann weggenommen oder zumindest gegenüber der vorher aufgebrachten Vakuumkraft reduziert oder beibehalten werden, so dass sich das poröse Elastomer, welches während des Stanzvorganges zusammengedrückt wurde, definiert nur aufgrund seiner Elastizität (unabhängig von der Vakuumkraft) entspannen kann, so dass dadurch die Ebene, in der die Klebeschicht liegt, aus der Ebene, in der der Endbereich der Stanzflanken liegt, herausbewegt wird. Damit ist die Klebeschicht für die weitere Verarbeitung frei zugänglich.In a further development of the invention, a punching flank of the punching tool is aligned parallel to a punching direction (asymmetrically). This has the effect that the cut edge of the metal layer is aligned parallel to the punching direction. This has the advantage that the punched-out multilayer composite, consisting of at least an adhesive layer and a metal layer, is held in a defined manner in the punching tool, in addition to the interaction of the porous elastomer and the vacuum force, which in this state causes the porous elastomer to contract. After the punching process has ended, the carrier layer can be removed, so that the adhesive layer is initially exposed and is arranged within the axial extension of the punching flanks or within the punching tool. In this state it is not possible or not possible over a large area to use the adhesive layer for further processing. The vacuum force can removed or at least reduced or maintained compared to the previously applied vacuum force, so that the porous elastomer, which was compressed during the punching process, can only relax in a defined manner due to its elasticity (independent of the vacuum force), so that the plane in which the The adhesive layer is moved out of the plane in which the end area of the punching flanks lies. This means that the adhesive layer is freely accessible for further processing.

Bisher handelte es sich bei dem mehrschichtigen Verbund um einen solchen Verbund, der aus einer Metallschicht, einer Klebeschicht und einer Trägerschicht besteht. Ein solcher mehrschichtiger Verbund ist beispielsweise ein Papier-Aluminium-Verbund (auch als PAL-Verbund bezeichnet). Je nach Art und Weise, in welcher Form die ausgestanzte Metallschicht der weiteren Verarbeitung zugeführt werden soll, ist es nicht ausreichend, nur wie vorstehend beschrieben, der Metallschicht mit der anhaftenden Klebeschicht die gewünschte Kontur mittels eines Stanzvorganges zu geben. Daher ist es denkbar, dass dieser mehrschichtige Verbund über eine weitere Klebeschicht auf eine weitere Trägerschicht aufzubringen. Durch entsprechende Formgebung (insbesondere Dicke) und Materialeigenschaften (insbesondere Elastizität) des porösen Elastomers in Verbindung mit der über den Vakuumanschluss aufgebrachten Vakuumkraft kann also der mehrschichtige Verbund (zum Beispiel der PAL-Verbund) und die zusätzliche Klebeschicht mittels des Stanzwerkzeuges ausgestanzt werden, wobei die zusätzlich aufgebrachte Trägerschicht von dem Stanzwerkzeug nicht erreicht wird. Auch in diesem Fall kann nach Reduzierung oder Aufhebung der Vakuumkraft das poröse Elastomer den mehrschichtigen Verbund, der dadurch vorher in dem Stanzwerkzeug gehalten wurde, in einem gewünschten Maß aus dem Stanzwerkzeug herausdrücken, so dass nach dem Abziehen der weiteren Trägerschicht die zusätzliche Klebeschicht freiliegt, und dieser mehrschichtige Verbund der weiteren Verarbeitung zur Verfügung gestellt werden kann.So far, the multilayer composite has been such a composite, which consists of a metal layer, an adhesive layer and a carrier layer. Such a multilayer composite is, for example, a paper-aluminum composite (also referred to as a PAL composite). Depending on the way in which the punched metal layer is to be fed to further processing, it is not sufficient just to give the metal layer with the adhering adhesive layer the desired contour by means of a punching process, as described above. It is therefore conceivable that this multilayer composite can be applied to a further carrier layer via a further adhesive layer. By appropriate shaping (in particular thickness) and material properties (in particular elasticity) of the porous elastomer in connection with the vacuum force applied via the vacuum connection, the multilayer composite (for example the PAL composite) and the additional adhesive layer can be punched out by means of the punching tool, with the additionally applied carrier layer is not reached by the punching tool. In this case, too, after reducing or removing the vacuum force, the porous elastomer can press the multilayer composite, which was thereby previously held in the punching tool, out of the punching tool to the desired extent, so that the additional adhesive layer is exposed after peeling off the further carrier layer, and this multilayer composite can be made available for further processing.

Bezüglich der Vakuumkraft wird allgemein noch auf folgendes hingewiesen: die Vakuumkraft dient im Wesentlichen zum Halten des mehrschichtigen Verbundes innerhalb des Stanzwerkzeuges. Sie wird zwar auch, wenn überhaupt, ein äußerst geringfügiges Zusammenziehen des porösen Elastomers bewirken. Das poröse Elastomer wird aber im Wesentlichen oder nur durch die beim Stanzen wirkenden Kräfte zusammengedrückt und entspannt sich nach dem Stanzvorgang ganz überwiegend oder vollständig unabhängig von der Vakuumkraft.With regard to the vacuum force, the following is generally pointed out: the vacuum force essentially serves to hold the multilayer composite within the punching tool. It will also cause the porous elastomer to contract very slightly, if at all. However, the porous elastomer is essentially or only compressed by the forces acting during the punching process and, after the punching process, relaxes largely or completely independently of the vacuum force.

Für eine Reduzierung der Stückkosten zur Herstellung dieser Produkte und eine einheitliche Auswahl der Werkstoffe hinsichtlich der Umweltverträglichkeit ist es notwendig sowie erfindungswesentlich; die Antenne direkt auf der Deck- oder Trägerbahn aufzubauen und damit in vorteilhafter Weise eine einheitliche Werkstoffauswahl und eine Reduzierung auf 2 Lagen zu ermöglichen.It is necessary and essential to the invention to reduce the unit costs for the manufacture of these products and to ensure a uniform selection of materials with regard to environmental compatibility; to build the antenna directly on the cover or carrier web and thus advantageously enable a uniform material selection and a reduction to 2 layers.

Das erfindungsgemäße Verfahren zum Betreiben einer Stanztransfervorrichtung zur Herstellung von RFID-Inlays, genauer von Antennen von RFID-Inlays, wird im Zusammenhang mit dem dabei verwendeten erfindungsgemäßen Stanzwerkzeug im Folgenden im Zusammenhang mit den Figuren näher erläutert und beschrieben.The method according to the invention for operating a punch transfer device for producing RFID inlays, more precisely antennas for RFID inlays, is explained and described in more detail below in connection with the figures in connection with the punch tool according to the invention used therein.

Die Figuren 1 und 2 zeigen eine Stanztransfervorrichtung 1 im Augenblick des Stanzvorganges (Figur 1) und im Zeitpunkt des Transfers der ausgestanzten Kontur (Figur 2) vor der Abgabe an die weitere Verarbeitung.The Figures 1 and 2 show a punch transfer device 1 at the moment of the punching process ( Figure 1 ) and at the time of transfer of the punched contour ( Figure 2 ) before submission to further processing.

Die Stanztransfervorrichtung 1 umfasst ein Stanzwerkzeug 2, wobei ein solches Stanzwerkzeug 2 als Stand-alone-Werkzeug oder beispielsweise auch mehrfach vorhanden auf einer Stanzwalze angeordnet ist. Das Stanzwerkzeug 2 weist einen Vakuumanschluss 3 auf, wobei über diesen Vakuumanschluss 3 ein auf die Innenkontur des Stanzwerkzeuges 2 wirkende Vakuumkraft erzeugt werden kann. Diese Vakuumkraft kann gesteuert geändert werden.The punching transfer device 1 comprises a punching tool 2, such a punching tool 2 being arranged as a stand-alone tool or, for example, also present several times on a punching roller. The punching tool 2 has a vacuum connection 3, a vacuum force acting on the inner contour of the punching tool 2 being able to be generated via this vacuum connection 3. This vacuum force can be changed in a controlled manner.

Mittels des Stanzwerkzeuges 2 soll einem mehrschichtigen Verbund durch Stanzen eine gewünschte Kontur gegeben werden.By means of the punching tool 2, a desired contour is to be given to a multilayer composite by punching.

Bei dem Ausführungsbeispiel gemäß der Verarbeitungsschritte, die in Figur 1 und 2 dargestellt sind, handelt es sich um einen mehrschichtigen Verbund mit einer ersten Trägerschicht 4, einer darauf vorhandenen ersten Klebeschicht 5, wobei die erste Klebeschicht 5 mit einer zweiten Trägerschicht 6 in Verbindung steht. Die zweite Trägerschicht 6 wiederum umfasst großflächig eine zweite Klebeschicht 7, auf der flächig eine Metallschicht 8 angeordnet ist. Die erste Trägerschicht 4 ist beispielsweise eine Silikonfolie, die zweite Trägerschicht 6 besteht beispielsweise aus Papier und die Metallschicht 8 besteht aus Aluminium. Besonders einfach und kostengünstig lässt sich dieser mehrschichtige Verbund realisieren, wenn die Schichten 6, 7 und 8 den zuvor schon beschriebenen PAL-Verbund bilden. Dieser ist von der Rolle kostengünstig einzusetzen.In the embodiment according to the processing steps shown in FIG Figures 1 and 2 are shown, it is a multi-layer composite with a first carrier layer 4, a first adhesive layer 5 present thereon, the first adhesive layer 5 being connected to a second carrier layer 6. The second carrier layer 6 in turn comprises a large area of a second adhesive layer 7 on which a metal layer 8 is arranged over a large area. The first carrier layer 4 is, for example, a silicone film, the second carrier layer 6 consists, for example, of paper and the metal layer 8 consists of aluminum. This multilayer composite can be implemented particularly simply and inexpensively if the layers 6, 7 and 8 form the PAL composite described above. This can be used inexpensively from the roll.

Der zuvor beschriebene mehrschichtige Verbund 4 bis 8 wird dem Stanzwerkzeug 2 zugeführt. Das Stanzwerkzeug 2 wird ausgehend von der Metallschicht 8 in Richtung der ersten Trägerschicht 4 bewegt, und zwar so weit axial bewegt, bis die bei Betrachtung der Figur 1 unterste Kontur des Stanzwerkzeuges 2 bis an die obere Ebene der ersten Trägerschicht 4 beziehungsweise in die Ebene, in der sich die erste Klebeschicht 5 befindet, hineinragt. Hierzu kann sich die erste Trägerschicht 4 an einer Gegenstütze (zum Beispiel flächig oder als Gegendruckwalze ausgebildet) abstützen. Damit die auszustanzende Kontur, bestehend aus den Schichten 5 bis 8, in dem Stanzwerkzeug geführt und gehalten wird, weist das Stanzwerkzeug 2 eine Stanzflanke 10 auf, wobei diese Stanzflanke 10 in vorteilhafter Weise parallel (asymmetrisch) zu einer Stanzrichtung 11 verläuft. Die andere Stanzflanke des Stanzwerkzeuges 2 ist in einem Winkel a, vorzugsweise ≤ 45°, weiter vorzugsweise im Bereich zwischen 30° und 35°, vorgesehen. Durch diese Ausgestaltung der Stanzflanke 10 ergibt sich eine nahezu rechtwinklige Stanzkontur bezüglich der Oberfläche des mehrschichtigen Verbundes. Beide Flanken des Stanzwerkzeuges können auch symmetrisch in Bezug auf die Stanzrichtung 11 ausgerichtet sein.The multi-layer composite 4 to 8 described above is fed to the punching tool 2. The punching tool 2 is moved starting from the metal layer 8 in the direction of the first carrier layer 4, namely moved axially until the when the Figure 1 Lowermost contour of the punching tool 2 protrudes as far as the upper level of the first carrier layer 4 or into the level in which the first adhesive layer 5 is located. For this purpose, the first carrier layer 4 can be supported on a counter-support (for example, flat or designed as a counter-pressure roller). So that the contour to be punched out, consisting of layers 5 to 8, is guided and held in the punching tool, punching tool 2 has a punching flank 10, this punching flank 10 advantageously running parallel (asymmetrically) to a punching direction 11. The other punching flank of the punching tool 2 is provided at an angle α, preferably 45 °, more preferably in the range between 30 ° and 35 °. This configuration of the punching flank 10 results in an almost right-angled punching contour with respect to the surface of the multilayer composite. Both flanks of the punching tool can also be aligned symmetrically with respect to the punching direction 11.

Um die auszustanzende Kontur dieses mehrschichtigen Verbundes hinsichtlich der Stanzrichtung 11 zu führen und auch in dem Stanzwerkzeug 2 zu halten, wird in diesem Fall über den Vakuumanschluss 3 eine Vakuumkraft über ein poröses Elastomer großflächig auf die Metallschicht 8 wirken lassen. Dadurch, dass sich insbesondere die erste Trägerschicht 4 definiert abstützt, aber auch eine definierte Vakuumkraft auf den mehrschichtigen Verbund wirkt, wird das poröse Elastomer 9 in definierter Weise in seiner axialen Erstreckung in Bezug auf die Stanzrichtung 11 zusammengezogen. Dadurch wird in vorteilhafter Weise bewirkt, dass mittels der Stanzflanke 10 des Stanzwerkzeuges 2 der mehrschichtige Verbund 5 bis 8 ausgestanzt und in dem Stanzwerkzeug 2 gehalten wird. Aufgrund der Materialeigenschaften des porösen Elastomers 9 und der aufgebrachten Vakuumkraft wird sichergestellt, dass der Endbereich der Stanzflanke 10 nicht bis in die erste Trägerschicht 4 hineinreicht. Somit wird mittels des Stanzwerkzeuges 2 aus einem mehrschichtigen Verbund eine gewünschte Kontur ausgestanzt und festgehalten und anschließend durch Veränderung der Form des porösen Elastomers 9, insbesondere seiner Dicke, und / oder durch Veränderung des Vakuums abgegeben.In order to guide the contour of this multilayer composite to be punched out in terms of punching direction 11 and also to hold it in punching tool 2, a vacuum force is applied over a large area to metal layer 8 via vacuum connection 3 via a porous elastomer. Because the first carrier layer 4 in particular is supported in a defined manner, but a defined vacuum force also acts on the multilayer composite, the porous elastomer 9 is contracted in a defined manner in its axial extension with respect to the punching direction 11. This advantageously has the effect that the multi-layer composite 5 to 8 is punched out by means of the punching flank 10 of the punching tool 2 and held in the punching tool 2. Due to the material properties of the porous elastomer 9 and the vacuum force applied, it is ensured that the end region of the punched flank 10 does not extend into the first carrier layer 4. Thus, by means of the punching tool 2, a desired contour is punched out of a multilayer composite and held, and then released by changing the shape of the porous elastomer 9, in particular its thickness, and / or by changing the vacuum.

Diese Abgabe an die nachfolgende Verarbeitung erfolgt dadurch, dass nach diesem Ausstanzvorgang die erste Trägerschicht, beispielsweise die Silikonfolie, abgezogen wird. Dabei werden auch die übrigen Schichten 5 bis 8, die außerhalb der Kontur des Stanzwerkzeuges 2 liegen, mit entfernt. Hierbei ist wichtig, dass die Adhäsionskräfte der Klebeschicht 7 deutlich größer sind als die der Klebeschicht 5, um zu verhindern, dass mit dem Abziehen der ersten Trägerschicht 4 auch die darauf angeordneten Schichten 6, 8 mit abgezogen werden. Somit kann mittels des Stanzwerkzeuges 2 nicht nur der Stanzvorgang, sondern auch der Transfervorgang für die weitere Verarbeitung des ausgestanzten mehrschichtigen Verbundes erfolgen.This transfer to the subsequent processing takes place in that, after this punching-out process, the first carrier layer, for example the silicone film, is peeled off. The remaining layers 5 to 8, which lie outside the contour of the punching tool 2, are also removed. It is important here that the adhesive forces of the adhesive layer 7 are significantly greater than those of the adhesive layer 5 in order to prevent the layers 6, 8 arranged thereon from also being pulled off when the first carrier layer 4 is peeled off. Thus, by means of the punching tool 2, not only the punching process but also the transfer process for the further processing of the punched-out multilayer composite can take place.

Während in den Figuren 1 und 2 ein erstes Beispiel für den mehrschichtigen Verbund gezeigt ist, ist der gleiche Vorgang (Ausstanzen und Transfer) in den Figuren 3 und 4 ebenfalls dargestellt, wobei hier die weitere Trägerschicht 6 und die Metallschicht 8 bezüglich der Klebeschicht 7 miteinander vertauscht sind. Dies kann für die nachfolgende Verarbeitung des ausgestanzten mehrschichtigen Verbundes von Bedeutung sein.While in the Figures 1 and 2 a first example of the multilayer composite is shown, the same process (punching and transfer) is in the Figures 3 and 4 also shown, the further carrier layer 6 and the metal layer 8 here with respect to the adhesive layer 7 are interchanged. This can be important for the subsequent processing of the punched-out multilayer composite.

Bezug nehmend auf die Figuren 2 beziehungsweise 4 wird noch der eigentliche Transfervorgang beschrieben. Nachdem gemäß den Figuren 1 und 3 der mehrschichtige Verbund 5 bis 8 ausgestanzt worden ist, wird in einem nachfolgenden Schritt die erste Trägerschicht 4 mit den um den ausgestanzten Konturbereich vorhandenen Schichten entfernt. Damit verbleibt innerhalb des Stanzwerkzeuges 2 die in die gewünschte Kontur gebrachte Metallschicht 8, die über die Klebeschicht 7 mit der weiteren Trägerschicht 6 verbunden ist. Hierbei handelt es sich um den schon genannten PAL-Verbund. Dies stellt jedoch keine Einschränkung dar, da auch andere Materialien eingesetzt werden können.Referring to the Figures 2 or 4 the actual transfer process is described. After according to the Figures 1 and 3 the multilayer composite 5 to 8 has been punched out, the first carrier layer 4 with the layers present around the punched out contour area is removed in a subsequent step. The metal layer 8 which has been brought into the desired contour and which is connected to the further carrier layer 6 via the adhesive layer 7 thus remains within the punching tool 2. This is the already mentioned PAL network. However, this is not a limitation, since other materials can also be used.

Bei Betrachtung der Figuren 1 beziehungsweise 3 liegt diese Klebeschicht 5 während des Stanzvorganges in etwa in der Ebene, die durch die äußeren Kanten (bei Betrachtung der Figuren 1 oder 3 die nach unten weisenden Schneidkanten) der Stanzflanken 10 gebildet ist. Damit war zu diesem Zeitpunkt (also während und direkt nach dem Ausstanzen) die Klebeschicht 5 noch nicht für die weitere Verarbeitung definiert zugänglich. Nach dem Stanzvorgang kann sich das poröse Elastomer 9 definiert entspannen (wobei vorher der poröse Elastomer 9 während des Stanzvorganges aufgrund der Gestaltung des Stanzwerkzeuges 2 definiert zusammengedrückt wurde). Während des Stanzvorganges wirkt die Vakuumkraft auf den innerhalb des Stanzwerkzeuges 2 befindlichen mehrschichtigen Verbund, um diesen dort zu halten. Nach dem Stanzvorgang wird die über den Vakuumanschluss 3 aufgebrachte Vakuumkraft beibehalten, reduziert beziehungsweise aufgehoben. In vorteilhafter Weise wird sie beibehalten, um den innerhalb des Stanzwerkzeuges 2 befindlichen, jetzt gestanzten mehrschichtigen Verbund dort zu halten. Sie kann aber auch reduziert oder aufgehoben werden, wenn der mehrschichtige Verbund direkt nach dem Stanzvorgang an das Zielbauteil übertragen wird. Wichtig ist auf jeden Fall, dass die Klebekräfte der Klebeschicht 5 größer sind als die Haltekräfte innerhalb des Stanzwerkzeuges, damit mittels dieser Adhäsionskräfte der ausgestanzte mehrschichtige Verbund aus dem Stanzvorgang entnommen und dem Zielbauteil zugeführt und dort aufgeklebt werden kann.When looking at the Figures 1 or 3, this adhesive layer 5 lies during the punching process approximately in the plane that is defined by the outer edges (when looking at the Figures 1 or 3 the downwardly pointing cutting edges) of the punching flanks 10 is formed. At this point in time (that is, during and directly after the punching out) the adhesive layer 5 was not yet accessible in a defined manner for further processing. After the punching process, the porous elastomer 9 can relax in a defined manner (the porous elastomer 9 having previously been compressed in a defined manner during the punching process due to the design of the punching tool 2). During the punching process, the vacuum force acts on the multilayer composite located inside the punching tool 2 in order to hold it there. After the punching process, the vacuum force applied via the vacuum connection 3 is maintained, reduced or canceled. It is advantageously retained in order to hold the multi-layer composite now punched inside the punching tool 2 there. However, it can also be reduced or canceled if the multilayer composite is transferred to the target component directly after the punching process. In any case, it is important that the adhesive forces of the adhesive layer 5 are greater than the holding forces within of the punching tool, so that by means of these adhesive forces the punched-out multilayer composite can be removed from the punching process and fed to the target component and glued there.

Somit kann sich also das poröse Elastomer 9 nach dem Stanzvorgang wieder definiert entspannen (weil die Gegenstütze weggenommen wurde), so dass es den ausgestanzten mehrschichtigen Verbund in einem gewünschten Maß in Richtung einer Abgaberichtung 12 aus dem Stanzwerkzeug 2 herausdrückt. Dieses Maß des Herausdrückens ist so gewählt, dass vorzugsweise die gesamte Klebeschicht 5 und gegebenenfalls auch ein Teil der zweiten Trägerschicht 6 aus der Ebene, die durch die Unterkanten der Stanzflanken 10 begrenzt ist, herausbewegt wird. Dieser Zeitpunkt nach der Reduzierung oder auf Aufhebung der Vakuumkraft und dem Entspannen des porösen Elastomers 9 (also einer Vergrößerung der axialen Erstreckung in Richtung der Abgaberichtung 12) ist in den Figuren 2 und 4 dargestellt. Nachdem dies erfolgt ist, kann dieser ausgestanzte mehrschichtige Verbund 5 bis 8 an eine weitere Verarbeitung abgegeben werden (Transfer).Thus, the porous elastomer 9 can relax again in a defined manner after the punching process (because the counter support has been removed), so that it presses the punched-out multilayer composite to a desired extent in the direction of a delivery direction 12 from the punching tool 2. This amount of pushing out is selected such that preferably the entire adhesive layer 5 and possibly also part of the second carrier layer 6 is moved out of the plane which is delimited by the lower edges of the punching flanks 10. This point in time after the reduction or removal of the vacuum force and relaxation of the porous elastomer 9 (that is, an increase in the axial extent in the direction of the delivery direction 12) is in the Figures 2 and 4 shown. After this has taken place, this punched-out multilayer composite 5 to 8 can be passed on to further processing (transfer).

Bis zu diesem Zeitpunkt bestand der mehrschichtige Verbund innerhalb des Stanzwerkzeuges 2 großflächig aus den Schichten 5 bis 8. Da es aber erforderlich sein kann, insbesondere zur Herstellung einer Antenne eines RFID-Inlays, der Metallschicht 8 ebenfalls eine gewünschte Kontur zu geben, kann in Weiterbildung der Erfindung daran gedacht werden, dass vor dem bisher beschriebenen Vorgang des Ausstanzens der Metallschicht 8 durch einen weiteren, insbesondere vorgelagerten, Bearbeitungsvorgang, insbesondere ebenfalls einen Stanzvorgang, eine gewünschte Kontur gegeben wird. Die gewünschte Kontur kann beispielsweise eine Ausnehmung 14 in der Metallschicht, aber auch eine komplexere Geometrie sein. Der weitere, insbesondere vorgelagerte Bearbeitungsvorgang muss nicht ein Stanzvorgang sein, sondern kann beispielsweise auch durch einen Vorgang mittels eines Lasers oder dergleichen erfolgen. Die der Metallschicht 8 zu gebende gewünschte Gesamtkontur ist beispielhaft bei Draufsicht in Figur 5 dargestellt, wobei hier als mehrschichtiger Verbund die Schichten 5 bis 8 ausgestanzt und auf ein Zielbauteil 13 (zum Beispiel eine Papierbahn) abgegeben (transferiert) worden sind. Je nach Vorhandensein von mehr oder weniger Schichten werden in Abhängigkeit dessen auch mehr oder weniger Schichten (zum Beispiel nur die Metallschicht mit ihrer Klebeschicht) nach dem Stanzvorgang auf das Zielbauteil 13 transferiert. Somit kann also in einem Ausführungsfall zumindest die Metallschicht 8 in eine gewünschte Form, insbesondere einer Ausnehmung 14, gebracht werden, bevor der mehrschichtige Verbund 4 bis 8 dem Stanzwerkzeug 2 zugeführt wird. Dadurch wird in vorteilhafter Weise die Metallschicht 8 in die gewünschte Kontur (zum Beispiel die für ein RFID-Inlay erforderliche Antennenstruktur) gebracht und kann dem weiteren Stanz- und Transfervorgang unterzogen werden. Insbesondere im Hinblick auf den mehrschichtigen Verbund 4 bis 8 und den nachfolgenden Stanz- und Transfervorgang wird in besonders vorteilhafter und erfindungswesentlicher Weise erreicht, dass für die Herstellung von Antennen für RFID-Inlays eine Antennenstruktur hergestellt wird, so dass nur noch die Antennenstruktur mit ihrer Klebeschicht auf das Zielbauteil aufgebracht werden muss.Up to this point in time, the multi-layer composite within the punching tool 2 consisted of layers 5 to 8 over a large area. However, since it may be necessary to give the metal layer 8 a desired contour, in particular for producing an antenna of an RFID inlay, a further development According to the invention, before the previously described process of punching out the metal layer 8, a desired contour is given by a further, in particular preceding, machining process, in particular also a punching process. The desired contour can be, for example, a recess 14 in the metal layer, but also a more complex geometry. The further, in particular upstream, machining process does not have to be a punching process, but can also be carried out, for example, by a process using a laser or the like. The desired overall contour to be given to the metal layer 8 is exemplified in the plan view in FIG Figure 5 shown, with the layers 5 to 8 punched out here as a multilayer composite and placed on a Target component 13 (for example a paper web) have been delivered (transferred). Depending on the presence of more or fewer layers, depending on this, more or fewer layers (for example only the metal layer with its adhesive layer) are transferred to the target component 13 after the punching process. Thus, in one embodiment, at least the metal layer 8 can be brought into a desired shape, in particular a recess 14, before the multilayer composite 4 to 8 is fed to the punching tool 2. As a result, the metal layer 8 is advantageously brought into the desired contour (for example the antenna structure required for an RFID inlay) and can be subjected to the further stamping and transfer process. In particular with regard to the multilayer composite 4 to 8 and the subsequent punching and transfer process, it is achieved in a particularly advantageous and inventive way that an antenna structure is produced for the production of antennas for RFID inlays, so that only the antenna structure with its adhesive layer must be applied to the target component.

Hierbei handelt es sich also um einen ganz entscheidenden und wesentlichen Vorteil der erfindungsgemäßen Stanztransfervorrichtung und dem damit durchzuführenden Verfahren.This is a very decisive and essential advantage of the punch transfer device according to the invention and the method to be carried out with it.

Weiterhin ist erfindungsgemäß vorgesehen, dass vor dem Stanzvorgang die zweite Trägerschicht 6 von der ersten Trägerschicht 4 gelöst und danach diese beiden Schichten 4, 6 wieder zusammengebracht werden. Dadurch wird der sogenannte Releasewert zwischen den beiden Schichten 4, 6, die über die Klebeschicht 5 miteinander verbunden sind, herabgesetzt. Das bedeutet, dass zum Trennen der beiden Trägerschichten 4, 6 voneinander zunächst eine bestimmte Kraft aufgebracht werden muss, um die Adhäsionskräfte der die beiden Schichten 4, 6 verbindende Klebeschicht 5 zu überwinden. Werden nun diese beiden Trägerschichten 4, 6 wieder zusammengebracht und erneut voneinander gelöst, ist die hierfür erforderliche Kraft (Release) geringer. Diesen Umstand macht man sich zunutze, um den mehrschichtigen Verbund dem Stanzvorgang zuzuführen, so dass es nach Ausführung des Stanzvorganges geringerer Kräfte bedarf, um die erste Trägerschicht 4 von dem ausgestanzten mehrschichtigen Verbund zu entfernen. Dies wirkt sich vorteilhaft deshalb aus, weil dadurch auch nur verringerte Kräfte erforderlich sind, um den mehrschichtigen ausgestanzten Verbund 5 bis 8 in dem Stanzwerkzeug 2 entweder nur durch die Formgebung der Stanzflanke 10 (gegebenenfalls auch unter Weglassung der Vakuumkraft) zu halten. Ist die Vakuumkraft vorhanden, kann diese kleiner ausfallen, da der Releasewert der Verbindung zwischen den beiden Trägerschichten 4, 6 durch das vorher erfolgte Lösen und wieder Zusammenbringen reduziert wurde. Dies wirkt sich vor allen Dingen bei dem Stanzen und dem Transfer von dem mehrschichtigen Verbünden in großer Stückzahl vorteilhaft aus.Furthermore, it is provided according to the invention that the second carrier layer 6 is detached from the first carrier layer 4 before the punching process and then these two layers 4, 6 are brought together again. As a result, the so-called release value between the two layers 4, 6, which are connected to one another via the adhesive layer 5, is reduced. This means that in order to separate the two carrier layers 4, 6 from one another, a certain force must first be applied in order to overcome the adhesive forces of the adhesive layer 5 connecting the two layers 4, 6. If these two carrier layers 4, 6 are now brought together again and again detached from one another, the force (release) required for this is lower. This fact is used to feed the multi-layer composite to the punching process so that it can be Execution of the punching process requires less force in order to remove the first carrier layer 4 from the punched-out multilayer composite. This has an advantageous effect because it also means that only reduced forces are required to hold the multi-layer punched composite 5 to 8 in the punching tool 2 either only by shaping the punching flank 10 (possibly also by omitting the vacuum force). If the vacuum force is present, it can turn out to be smaller, since the release value of the connection between the two carrier layers 4, 6 was reduced by the previous loosening and bringing them back together. This has an advantageous effect, above all, when punching and transferring the multilayer composite in large numbers.

Ergänzend dazu kann erfindungsgemäß der Vorgang des Zusammenbringens der beiden Trägerschichten 4, 6 deckungsgleich oder zueinander versetzt erfolgen. Erfolgt der Vorgang des Zusammenbringens der beiden Trägerschichten 4, 6 deckungsgleich, wird wie schon beschrieben der Releasewert in vorteilhafter Weise reduziert. Erfolgt das Zusammenbringen der beiden Trägerschichten 4, 6 versetzt zueinander, hat dies den Vorteil, dass dadurch die ausgestanzt oder in anderer Weise erfolgte Bearbeitung der Metallschicht 8, die möglicherweise bis in Richtung der ersten Trägerschicht 4 gereicht hat, nicht mehr deckungsgleich nach dem Zusammenbringen sind. Dadurch lässt sich in vorteilhafter Weise sicherstellen, dass dann, wenn durch den weiteren Bearbeitungsvorgang die Metallschicht 8 insbesondere eine filigrane, zum Beispiel Antennenstruktur erhalten hat, ohne Weiteres, vor allen Dingen ohne Beschädigungen beim weiteren Verarbeiten nach dem Transfer von der ersten Trägerschicht 4 entfernt werden kann.In addition to this, according to the invention, the process of bringing the two carrier layers 4, 6 together can be carried out congruently or offset from one another. If the process of bringing the two carrier layers 4, 6 together is carried out congruently, the release value is advantageously reduced, as already described. If the two carrier layers 4, 6 are brought together offset from one another, this has the advantage that the punched or otherwise processed machining of the metal layer 8, which may have reached in the direction of the first carrier layer 4, is no longer congruent after the joining . This makes it possible to advantageously ensure that when the metal layer 8 has received a filigree structure, for example an antenna structure, as a result of the further processing operation, it is easily removed from the first carrier layer 4 after the transfer, above all without damage during further processing can.

Schließlich ist vorgesehen, dass der ausgestanzte mehrschichtige Verbund, bestehend aus der Trägerschicht 6, den Klebeschichten 5, 7 sowie der Metallschicht 8, mittels der Klebeschicht 5 auf eine weitere Trägerschicht abgegeben wird. Dadurch lassen sich die Metallschichten 8 in ihrer gewünschten Kontur, insbesondere der filigranen Antennenstruktur, auf die weitere Trägerschicht nach dem Bearbeiten und dem Transfer abgeben. Wird danach schließlich die Trägerschicht 4 entfernt, kann der mehrschichtige Verbund 5 bis 8 in ihrer gegebenen Kontur dem Zielbauteil zugeführt werden. Der nicht benötigte Teil des mehrschichtigen Verbundes außerhalb der Stanzkontur des Stanzwerkzeuges verbleibt auf der ersten Trägerschicht 4 und wird zusammen mit dieser entsorgt, zum Beispiel auf einer Rolle ohne Bildung von störenden Abfällen aufgewickelt.Finally, it is provided that the punched-out multilayer composite, consisting of the carrier layer 6, the adhesive layers 5, 7 and the metal layer 8, is transferred to a further carrier layer by means of the adhesive layer 5. As a result, the metal layers 8 can be traced onto the further carrier layer in their desired contour, in particular the filigree antenna structure submit for processing and transfer. If the carrier layer 4 is then finally removed, the multilayer composite 5 to 8 can be fed to the target component in its given contour. The part of the multilayer composite that is not required outside the punching contour of the punching tool remains on the first carrier layer 4 and is disposed of together with it, for example wound up on a roll without the formation of disruptive waste.

Die Erfindung bietet somit den ganz entscheidenden Vorteil, dass mittels der Stanztransfervorrichtung nur derjenige Teil des mehrschichtigen Verbundes ausgestanzt und der weiteren Verarbeitung zugeführt wird, der auch für die weitere Verarbeitung benötigt wird. Der übrige Teil (Rest) des mehrschichtigen Verbundes kann auf einfachste Art und Weise entsorgt werden und es müssen nicht, wie bisher im Stand der Technik, einzelne Schichten aufgenommen und entsorgt werden.The invention thus offers the very decisive advantage that, by means of the punch transfer device, only that part of the multilayer composite is punched out and fed to further processing that is also required for further processing. The remaining part (remainder) of the multi-layer composite can be disposed of in the simplest possible way and individual layers do not have to be picked up and disposed of, as was previously the case in the prior art.

Der mehrschichtige Verbund kann wie beschrieben aus den Schichten 4 bis 8 bestehen. Es sind aber auch mehr Schichten als diese denkbar, genauso wie ein mehrschichtiger Verbund nur aus einer Trägerschicht oder Klebeschicht und einer weiteren Schicht, insbesondere einer Metallschicht, bestehen kann, die über eine Klebeschicht miteinander verbunden sind. Die bisher genannte Metallschicht 8 wird in vorteilhafter Weise zur Herstellung einer Antenne bzw. Antennenstruktur verwendet und besteht daher aus einem elektrisch leitfähigen Material (zum Beispiel Aluminiumfolie). Je nach Einsatzzweck des ausgestanzten mehrschichtigen Verbundes kann die bisher beschriebene Metallschicht auch aus einem elektrisch nicht leitfähigen Material (wie zum Beispiel aus Textil, Papier, Kunststofffolie oder dergleichen) bestehen.The multilayer composite can consist of layers 4 to 8 as described. However, more layers than this are also conceivable, just as a multi-layer composite can only consist of a carrier layer or adhesive layer and a further layer, in particular a metal layer, which are connected to one another via an adhesive layer. The previously mentioned metal layer 8 is advantageously used to produce an antenna or antenna structure and therefore consists of an electrically conductive material (for example aluminum foil). Depending on the intended use of the punched-out multilayer composite, the metal layer described so far can also consist of an electrically non-conductive material (such as, for example, textile, paper, plastic film or the like).

BezugszeichenlisteList of reference symbols

1.1.
StanztransfervorrichtungPunch transfer device
2.2.
StanzwerkzeugPunching tool
3.3.
VakuumanschlussVacuum connection
4.4th
Erste TrägerschichtFirst carrier layer
5.5.
Erste KlebeschichtFirst adhesive layer
6.6th
Zweite TrägerschichtSecond carrier layer
7.7th
Zweite KlebeschichtSecond adhesive layer
8.8th.
MetallschichtMetal layer
9.9.
Poröser ElastomerPorous elastomer
10.10.
StanzflankePunch edge
11.11.
StanzrichtungPunching direction
12.12.
AbgaberichtungDelivery direction
13.13.
ZielbauteilTarget component
14.14th
AusnehmungRecess

Claims (12)

  1. Punching transfer apparatus (1) for manufacturing an RFID antenna, characterized in that the punching transfer apparatus (1) comprises a punching tool (2) with a vacuum connection (3), wherein the vacuum connection (3) interacts with a porous elastomer (9).
  2. Punching transfer apparatus (1) according to claim 1, characterized in that the punching tool (2) comprises a cutting angle (α) which is symmetrically or asymmetrically aligned with respect to a punching direction (11) and is smaller than or equal to 45 degrees, in particular in the range between 30 degrees and 35 degrees.
  3. Punching transfer apparatus (1) according to claim 1 or 2, characterized in that a punching flank (10) of the punching tool (2) is aligned parallel to a punching direction (11).
  4. Punching transfer apparatus (1) according to claim 1, 2 or 3, characterized in that several punching tools (2) are arranged on a punching roller distributed around its circumference.
  5. Method for operating a punching transfer apparatus (1), in particular for manufacturing RFID antennas, characterized in that the punching transfer apparatus (1) comprises a punching tool (2) with a vacuum connection (3), wherein the vacuum connection (3) interacts with a porous elastomer (9) in such a way that by means of the punching tool (2) a desired contour is punched out of a multi-layer composite, held in place and afterwards released by changing the shape of the porous elastomer (9) and/or by changing the vacuum.
  6. Method according to claim 5, characterized in that the multi-layer composite consists of a first carrier layer (4) and at least one second carrier layer (6), which are connected to one another by means of a removable first adhesive layer (5), and the at least second carrier layer (6) is connected to a metal layer (8) via a second adhesive layer (7), wherein the desired contour is punched out of all layers (5 to 8) with the exception of the first carrier layer (4) by means of the punching tool (2).
  7. Method according to claim 5 or 6, characterized in that before punching, the multi-layer composite, in particular comprising the layers 5 to 8, is given a desired contour, in particular a recess (14), by a further, in particular preceding processing operation, in particular a punching operation.
  8. Method according to claim 5, 6 or 7, characterized in that before the punching process the second carrier layer (6) is detached from the first carrier layer (4) and then brought together again.
  9. Method according to claim 8, characterized in that the process of bringing together the two carrier layers (4, 6) is carried out congruently or offset to each other.
  10. Method according to one of claims 5 to 9, characterized in that the punched-out multi-layer composite, consisting of the carrier layer (6), the adhesive layers (5, 7) and the metal layer (8), is transferred to a further carrier layer by means of the adhesive layer (5).
  11. Method according to one of claims 5 to 10, characterized in that the waste is disposed of around the punched multi-layer composite, in particular wound up on a roll.
  12. Method according to claim 11, characterized in that the waste around the punched multi-layer composite remains on the first carrier layer (4) through the first adhesive layer (5) and is disposed of with it, in particular is wound up on a roll.
EP14741235.7A 2013-08-08 2014-07-08 Transfer/punching process Active EP3030388B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102013215706.1A DE102013215706A1 (en) 2013-08-08 2013-08-08 Transfer presses
PCT/EP2014/064615 WO2015018587A1 (en) 2013-08-08 2014-07-08 Transfer/punching process

Publications (2)

Publication Number Publication Date
EP3030388A1 EP3030388A1 (en) 2016-06-15
EP3030388B1 true EP3030388B1 (en) 2020-08-26

Family

ID=51211196

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14741235.7A Active EP3030388B1 (en) 2013-08-08 2014-07-08 Transfer/punching process

Country Status (9)

Country Link
US (1) US9981398B2 (en)
EP (1) EP3030388B1 (en)
JP (1) JP6415558B2 (en)
CN (1) CN105980116B (en)
DE (1) DE102013215706A1 (en)
ES (1) ES2833290T3 (en)
HK (1) HK1226026A1 (en)
MY (1) MY183430A (en)
WO (1) WO2015018587A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3007681B1 (en) * 2013-07-01 2015-07-17 Oberthur Technologies MANUFACTURE OF A PLATE OF LARGE THICKNESS COMPRISING A DETACHABLE CARD OF SMALL THICKNESS
CH711043A1 (en) * 2015-05-06 2016-11-15 Berhalter Ag Device for the punching of thin-walled materials.

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5240078B2 (en) * 1972-04-05 1977-10-08
GB1436544A (en) * 1972-05-25 1976-05-19 Smiths Industries Ltd Methods of and apparatus for working sheet material
JPS49117586U (en) * 1973-02-01 1974-10-08
US5382404A (en) * 1989-05-04 1995-01-17 Murata Manufacturing Co., Ltd. Method of cutting out a portion of a weak sheet
JPH068199A (en) * 1992-06-30 1994-01-18 Diafoil Co Ltd Perforating method for tape
JPH077900U (en) * 1993-07-12 1995-02-03 栄一 上石 Punching device for sheet material
CH690844A5 (en) * 1995-08-04 2001-02-15 Bobst Sa blank separating equipment within a machine for cutting plate-like workpieces.
US5788999A (en) * 1996-07-04 1998-08-04 Fuji Photo Film Co., Ltd. Disk producing apparatus for a photo film cassette
US6173632B1 (en) * 1998-11-23 2001-01-16 Semiconductor Technologies & Instruments, Inc. Single station cutting apparatus for separating semiconductor packages
TW558727B (en) * 2001-09-19 2003-10-21 Matsushita Electric Ind Co Ltd Manufacturing method of ceramic electronic components and its manufacturing equipment
JP4169565B2 (en) * 2002-10-11 2008-10-22 三星ダイヤモンド工業株式会社 Brittle material substrate break method, apparatus and processing apparatus therefor
JP2007000338A (en) * 2005-06-23 2007-01-11 Nichiban Co Ltd Medical adhesive composition
JP4545681B2 (en) * 2005-12-01 2010-09-15 日本メクトロン株式会社 Adsorption conveyance device and conveyance method for plate workpiece
CN200956712Y (en) * 2006-08-25 2007-10-03 鸿富锦精密工业(深圳)有限公司 Punching-cutting assembling device
DE102007041752A1 (en) 2007-09-04 2009-03-05 Bielomatik Leuze Gmbh + Co Kg Chip module for an RFID system
JP2009166487A (en) * 2007-12-18 2009-07-30 Nichigo Morton Co Ltd Flat pressing machine, laminating apparatus and laminating method using them
FI121592B (en) 2008-03-26 2011-01-31 Tecnomar Oy Process for making PCB laminates, especially RFID antenna laminates and PCB laminates
ES2386614T3 (en) * 2010-02-06 2012-08-23 Textilma Ag Mounting device for applying an RFID chip module on a substrate, especially a label
CN202498586U (en) * 2011-12-05 2012-10-24 苏州源德福科技有限公司 Die cutting device
DE202012011193U1 (en) * 2012-09-25 2013-02-27 Jürgen Teufel counter-tool
WO2016086095A1 (en) * 2014-11-25 2016-06-02 Biodelivery Sciences International, Inc. Patches, methods for forming and testing pharmaceutical agent delivery patches

Non-Patent Citations (1)

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

Also Published As

Publication number Publication date
US20160151928A1 (en) 2016-06-02
CN105980116A (en) 2016-09-28
HK1226026A1 (en) 2017-09-22
ES2833290T3 (en) 2021-06-14
DE102013215706A1 (en) 2015-02-12
CN105980116B (en) 2019-07-23
EP3030388A1 (en) 2016-06-15
MY183430A (en) 2021-02-18
WO2015018587A1 (en) 2015-02-12
JP2016533909A (en) 2016-11-04
JP6415558B2 (en) 2018-10-31
US9981398B2 (en) 2018-05-29

Similar Documents

Publication Publication Date Title
EP2864133B2 (en) Method for transferring a decorative section of an embossing foil
EP2754541B1 (en) Method for adjusting the pressing force a punching and embossing machine
EP1914049A1 (en) Flat-bed cutting press for sheets
EP2183707A1 (en) Method and device for producing an rfid label
EP3509806B1 (en) Method for processing a substrate using a punch
DE102008053096A1 (en) Method and device for the production of data carriers and semi-finished media, as well as data carriers and semi-finished media
EP3030388B1 (en) Transfer/punching process
EP3313670B1 (en) Method and device for transferring a decorative segment of an embossing film
EP2851168B1 (en) Device for punching out labels with counter punch tape
DE102012005005B4 (en) Method and arrangement for the production of electrical sheets
DE4232211B4 (en) Method for cutting a blank from a metal strip
EP1640938B1 (en) Method and system for cutting and embossing of folded box blanks
EP4274738A1 (en) Method for producing a multilayer laminated document substrate having an insert
DE102006041494B3 (en) Production of a friction bearing element from a strip of layer composite or solid material comprises punching an inner waste strip from the strip producing two spaced parallel flat strips and further processing
EP3760439B1 (en) Method and device for manufacturing a strip of material with an integrated electronic component
DE10004593C1 (en) Method for manufacturing vehicle number plates involves supplying sheet metal strip and printed foil having undersized repeating graphic elements with scanners to detect spacings to allow tolerances
EP2774752A1 (en) Method and device for producing folding box blanks from a sheet of material
EP3736062A1 (en) Method for stamp packaging of metal parts to stacks of metal sheets
DE10016811A1 (en) Method and device for punching thin film
DE102013018995A1 (en) Plant for the rotary cutting of electrical sheets
EP4303026B1 (en) Method and apparatus for creating a booklet
AT500076B1 (en) DEVICE AND METHOD FOR APPLYING A SURFACE CONNECTOR TO A CONTACT AREA OF A WATER
DE102007048657A1 (en) Rotary embosser
DE102018222729A1 (en) Processing method of flat material
EP2184141A1 (en) Method and device for manufacturing a punch

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: 20160108

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

AX Request for extension of the european patent

Extension state: BA ME

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: BIELOMATIK LEUZE GMBH + CO. KG

DAX Request for extension of the european patent (deleted)
RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: BW PAPERSYSTEMS STUTTGART GMBH

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: 20200406

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: DE

Ref legal event code: R096

Ref document number: 502014014674

Country of ref document: DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1305928

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200915

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 502014014674

Country of ref document: DE

Representative=s name: VON ROHR PATENTANWAELTE PARTNERSCHAFT MBB, DE

REG Reference to a national code

Ref country code: FI

Ref legal event code: FGE

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: NL

Ref legal event code: FP

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

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

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: 20201228

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: 20200826

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: 20200826

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: 20201126

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: 20201126

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: 20201127

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

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: 20201226

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: 20200826

Ref country code: PL

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: 20200826

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: 20200826

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

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: 20200826

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: 20200826

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: 20200826

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: 20200826

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: 20200826

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502014014674

Country of ref document: DE

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

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: 20200826

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2833290

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20210614

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: 20200826

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: 20210527

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: 20200826

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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: 20200826

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20210731

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

Ref country code: LI

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

Effective date: 20210731

Ref country code: CH

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

Effective date: 20210731

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

Ref country code: LU

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

Effective date: 20210708

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: 20210708

Ref country code: BE

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

Effective date: 20210731

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 1305928

Country of ref document: AT

Kind code of ref document: T

Effective date: 20210708

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: 20210708

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

Ref country code: HU

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

Effective date: 20140708

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

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: 20200826

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

Ref country code: NL

Payment date: 20230719

Year of fee payment: 10

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

Ref country code: IT

Payment date: 20230724

Year of fee payment: 10

Ref country code: GB

Payment date: 20230721

Year of fee payment: 10

Ref country code: FI

Payment date: 20230719

Year of fee payment: 10

Ref country code: ES

Payment date: 20230926

Year of fee payment: 10

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

Ref country code: SE

Payment date: 20230719

Year of fee payment: 10

Ref country code: FR

Payment date: 20230726

Year of fee payment: 10

Ref country code: DE

Payment date: 20230720

Year of fee payment: 10

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: 20200826