EP2484462B1 - Method for producing a forge preform and warm upsetting device - Google Patents

Method for producing a forge preform and warm upsetting device Download PDF

Info

Publication number
EP2484462B1
EP2484462B1 EP12000767.9A EP12000767A EP2484462B1 EP 2484462 B1 EP2484462 B1 EP 2484462B1 EP 12000767 A EP12000767 A EP 12000767A EP 2484462 B1 EP2484462 B1 EP 2484462B1
Authority
EP
European Patent Office
Prior art keywords
forming tool
forming
subspace
diameter
cavity
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.)
Not-in-force
Application number
EP12000767.9A
Other languages
German (de)
French (fr)
Other versions
EP2484462A3 (en
EP2484462A2 (en
Inventor
Volker Wengenroth
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.)
SMS Group GmbH
Original Assignee
SMS Group 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 SMS Group GmbH filed Critical SMS Group GmbH
Publication of EP2484462A2 publication Critical patent/EP2484462A2/en
Publication of EP2484462A3 publication Critical patent/EP2484462A3/en
Application granted granted Critical
Publication of EP2484462B1 publication Critical patent/EP2484462B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J1/00Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
    • B21J1/04Shaping in the rough solely by forging or pressing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J13/00Details of machines for forging, pressing, or hammering
    • B21J13/02Dies or mountings therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/06Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
    • B21J5/08Upsetting

Definitions

  • the invention relates to a method for producing a forging preform for forging a forged part, in which a contour of a workpiece is formed into a forging contour using a forming tool, wherein the forging contour corresponds to a first forged part contour with a required volume predistribution of the forging to be forged.
  • the invention relates to a forming device or a hot forging device for producing a forging preform for forging a forged part with a forming tool, wherein the forming tool has a workpiece forming contour with variable cross sections, by means of which a volume predistribution of the forging preform can be generated.
  • the forming of the substantially cylindrical workpiece to the forging preform is done in the prior art by means of transverse and / or stretching rolling process, in which a forging preform with an already defined volume pre-distribution is worked on the substantially cylindrical workpiece. This makes it much easier to get started in the actual forging process.
  • a upsetting is carried out in a cavity in which a cavity is formed by matrices, in which an upsetting die dips to appropriately transform the workpiece into the cavity, so that its surface then essentially the Surface of the Werk Swissumforminnenkontur the cavity corresponds.
  • Generic methods and devices are for example from the EP 0 786 296 A1 or from the JP 59-054440 A known.
  • the object is achieved by a method according to claim 1 or by a forming device according to claim 6.
  • Forming device 1 shown comprises a forming tool 2, which in the illustration according to the FIG. 1 is shown open.
  • the forming device 1 in this embodiment is a hot-swaging device 3.
  • the forming tool 2 is radially configured in two parts in an upper part 6 and in a lower part 7.
  • the upsetting punch 5 is guided through a punch guide 5A and it can be moved by a drive not shown here in alignment with the upsetting axis 4 in the forming tool 2 or out of the forming tool 2 out.
  • the forming tool 2 has a cavity 8 with variable cross sections 9, which accordingly provides an asymmetrical workpiece forming inner contour 10 within the forming tool 2.
  • the forming tool 2 is additionally divided in this embodiment into three longitudinal segments 11, 12 and 13, wherein the front longitudinal segment 11, a front Festmatrize 14 and a front clamping die 15, the middle longitudinal segment 12, a middle Festmatrize 16 and a central clamping die 17 and the rear longitudinal segment 13 comprises a rear fixed die 18 and a rear clamping die 19.
  • the cavity 8 is designed both radially and axially in several parts.
  • Each of the clamping matrices 15, 17 and 19, respectively, is fixed but hinged to its associated fixed die 14, 16 and 18, respectively, by means of a corresponding hinge connection 20. It is understood that in other embodiments, other arrangements of the different matrices and deviating measures to a positioning of the same can be provided to each other.
  • the forming device 2 of this embodiment is also characterized by a common Axial Installations worn 21, to which all Festmatrizen 14, 16 and 18 via the respective hinge joint 20 - and thus indirectly also all clamping matrices 15, 17 and 19 - are mounted axially displaceable one behind the other.
  • the Axial Environments Republic 21 is in this embodiment structurally simple designed as a single linear crossmember. But it can also be implemented as a multi-part component or group of components, should this be necessary.
  • the forming device 1 still has a holding device 22 with holding elements 23, 24 and 25th
  • the longitudinal segments 11, 12 and 13 are fixed in a displaceable manner on the common axial guide device 21.
  • the individual fixed matrices 14, 16 and 18 are screwed in the present embodiment by means of screw 26 to the respective holding elements 23, 24 and 15. It is understood that other connection options, such as quick release or positive connection, can be provided here.
  • the forming device 1 Since in particular two axially adjacent fixed dies 14, 16, 18 of the forming tool 2 are arranged axially loosely adjacent to one another, the forming device 1 has an axial stop 27, on which especially the fixed dies 14, 16, 18 can be axially supported during an upsetting process.
  • the axial stop 27 is designed in this embodiment structurally simple as a replaceable component of the axial guide 21.
  • a workpiece 33 with a substantially cylindrical contour 34 is inserted into the cavity 8 (see FIG. 2 ).
  • the forming tool 2 is closed, as it is in the FIG. 3 is shown.
  • the respectively on the fixed matrices 14, 16 and 18 lowered clamping matrices 15, 17 and 19 are respectively locked by means of a quick clamping device 35, 36 and 37 respectively. In this respect, a popping of the forming device 2 is excluded during the compression process.
  • the forging preform 30 now has a defined volume distribution which substantially corresponds to that of a forging part after a first forging step.
  • a hot upsetting method for producing a forging preform 30 with variable cross sections 32 for producing a forged part is used for the first time.
  • the sectional view according to the FIG. 5 shows the forming device 1 in the region of the front longitudinal segment 11 with the forming tool 2 open.
  • the front fixed die 14 of the forming tool 2 is fastened with two first screws 40 and 41 of the screw connection 26 to the first holding element 23 of the holding device 22.
  • the first holding element 23 has an upper part 42 facing the front solid die 14 and a lower part 43 facing the axial guiding device 21.
  • the upper part 42 is in this case screwed with two hexagon socket screws 44 and 45 to the lower part 43, it being understood that in this regard in other embodiments, other types of fastening or a one-piece design of Solid die 14 may be provided.
  • the remaining fixed matrices 16, 18 are similar in this embodiment, but this need not necessarily be the case.
  • the axial guide device 21 comprises a foot part 46 and a guide part 47, on which the longitudinal segments 11, 12 and 13 of the forming tool 2 are displaceably mounted.
  • the guide member 47 is screwed along the Axial arrangements adopted 21 with a number of other screws 48 to the foot part 46.
  • the first quick-clamp connection 35 of the hinge joint 20 is flanged with a Flanschverschraubung 49.
  • the quick-clamping connection 35 has a lever mechanism 50, by means of which the front longitudinal segment 11 of the forming tool 2 can be manually opened or closed.
  • the quick-clamp connection 35 corresponds to the upper part 42 by means of a lower leg 51
  • the quick-clamp connection 35 is screwed to a corresponding upper leg 52 on the front clamping template 15.
  • a screw 53 is provided.
  • the sectional view according to the FIG. 6 shows the forming device 1 in a closed state, in which the front clamping die 15 is lowered onto the front Festmatrize 14.
  • the cavity 8 is closed at least in the region of the front longitudinal segment 11.
  • the quick clamping mechanism 35 is here in a locked position 54, so that the front clamping die 15 does not lift off from the front fixed die 14 during a forming process and thereby the forming tool 2 would be at least partially opened.
  • first longitudinal segment 11 explained here can be transferred to the further longitudinal segments 12 and 13 so that they are not additionally explained
  • each in a schematic plan according to the FIGS. 7 and 8th For example, the front solid die 14, the middle solid die 16, and the rear solid die 18 are again exemplified.
  • the Festmatrizen 14, 16 and 18 are arranged along the upsetting axis 4 axially behind one another and in particular during the upsetting axially of the arrangement according to FIG. 7 to the arrangement FIG. 8 moved together.
  • this procedure is not mandatory and it is conceivable that the matrices are already collapsed before upsetting or even in the axial direction only one die is used, but this to relatively large axial movements between the workpiece and tool just in the inner wall of the Workpiece, which on the one hand increase wear and on the other hand energy consumption.
  • the front fixed die 14 configures a first lower subspace 55 of the cavity 8 of the forming tool 2. Accordingly, the middle fixed die 16 form a second lower subspace 56 and the rear fixed die 18 form a third lower subspace 57 of the cavity 8.
  • the subspaces 55, 56 and 57 of the fixed matrices 14, 16, 18 and the corresponding subspaces of the clamping matrices 15, 17, 19 are procedurally relatively simple in this embodiment by means of an erosion process in the respective die 14, 15, 16, 17, 18 and 19 incorporated.
  • the front Festmatrize 14 has two countersunk bores 58 and 59 for the two previously described screws 40 and 41.
  • Corresponding counterbores (not numbered separately here) can be found on the two fixed matrices 16 and 18.
  • first subspace 55 has a subspace diameter 60 that is critically greater than an associated subspace length 61 of the first subspace 55
  • means 62 for partially reducing the subspace diameter 60 are provided in the subspace 55, which are implemented as a flank dome 63 in this embodiment.
  • flank mandrel 63 comprises a clamping mandrel-side fixed longitudinal mandrel 64 and a fixed-die-side fixed longitudinal mandrel 65 (see FIG Figures 5 and 8th ), which protrude into the cavity 8.
  • a means for indexing a desired flow behavior is arranged within the cavity 8; in areas of the cavity 8, in which the subspace diameter 60 is greater than a designated inner diameter 66 of the forming tool 2, in which the upsetting die 5 is arranged or guided.
  • radial pressure jaws can be exerted on the workpiece 33 in a structurally particularly simple manner, which in particular run essentially perpendicular to the axial upsetting direction 38.
  • the workpiece 33 is thereby at least partially reshaped, so that the corresponding workpiece material flows within the subspace 55 before the actual Axialstauchrea with a desired flow behavior, whereby a breaking of the workpiece 33 during the axial upsetting is almost impossible.
  • FIG. 9 illustrated embodiment substantially corresponds to the embodiment according to FIGS. 1 to 8 , so that identically acting assemblies are also numbered identically.
  • the embodiment according to FIG. 9 Means 62 for partially reducing the subspace diameter 60, which protrude much less into the cavity 8 and the workpiece 33 when closing the matrices 14 to 19 substantially only frictionally in the radial direction, ie parallel to the subspace diameter 60, fix.
  • an elastic deformation by means of corresponding molding areas 67, 68 of the means 62 for partially reducing the partial space diameter 60 is sufficient for this purpose, in which case a plastic deformation may also be provided.

Description

Die Erfindung betrifft ein Verfahren zum Erzeugen einer Schmiedevorform für das Schmieden eines Schmiedeteils, bei welchem mit einem Umformwerkzeug eine Kontur eines Werkstücks zu einer Schmiedevorformkontur umgeformt wird, wobei die Schmiedevorformkontur einer ersten Schmiedeteilkontur mit einer erforderlichen Volumenvorverteilung des zu schmiedenden Schmiedeteils entspricht.The invention relates to a method for producing a forging preform for forging a forged part, in which a contour of a workpiece is formed into a forging contour using a forming tool, wherein the forging contour corresponds to a first forged part contour with a required volume predistribution of the forging to be forged.

Des Weiteren betrifft die Erfindung eine Umformvorrichtung oder eine Warmstauchvorrichtung zum Erzeugen einer Schmiedevorform für das Schmieden eines Schmiedeteils mit einem Umformwerkzeug, bei welcher das Umformwerkzeug eine Werkstückumformkontur mit veränderlichen Querschnitten aufweist, mittels welcher eine Volumenvorverteilung an der Schmiedevorform erzeugbar ist.Furthermore, the invention relates to a forming device or a hot forging device for producing a forging preform for forging a forged part with a forming tool, wherein the forming tool has a workpiece forming contour with variable cross sections, by means of which a volume predistribution of the forging preform can be generated.

Es ist bekannt, für ein Schmieden von Schmiedeteilen noch vor einer ersten Schmiedestufe aus einem im Wesentlichen zylindrischen Werkstück eine Schmiedevorform mit veränderlichen Querschnitten zu erzeugen, die anschließend in Gestalt eines Halbzeugs für eine erste Schmiedestufe bereitgestellt wird. Hierbei dient das Erzeugen einer Vorform insbesondere dazu, bereits Volumemmhäufungen zu erzielen, so dass die nachfolgenden Schmiedestufen einfacher und insbesondere unter minimalem Materialverlust durchgeführt werden können.It is known to produce forging of forged parts before a first forging step from a substantially cylindrical workpiece a forging preform with variable cross-sections, which is then provided in the form of a semi-finished product for a first forging stage. In this case, the production of a preform serves, in particular, to already achieve volume accumulations, so that the subsequent forging stages can be carried out more simply and in particular with minimal material loss.

Das Umformen des im Wesentlichen zylindrischen Werkstücks zu der Schmiedevorform geschieht im Stand der Technik mittels Quer- und/oder Reckwalzverfahren, bei welchen an dem im Wesentlichen zylindrischen Werkstück eine Schmiedevorform mit einer bereits definierten Volumenvorverteilung angearbeitet wird. Hierdurch gelingt der Einstieg in den eigentlichen Schmiedeprozess wesentlich leichter.The forming of the substantially cylindrical workpiece to the forging preform is done in the prior art by means of transverse and / or stretching rolling process, in which a forging preform with an already defined volume pre-distribution is worked on the substantially cylindrical workpiece. This makes it much easier to get started in the actual forging process.

Entsprechende Walzwerkzeuge für die bekannten Quer- und/oder Reckwazverfahren sind jedoch nicht nur kostenintensiv in der Herstellung, sondern bieten darüber hinaus speziell hinsichtlich einer erforderlichen Volumenverteilung an der Schmiedevorform nur geringe Nachstell- bzw. Korrekturmöglichkeiten.However, corresponding rolling tools for the known transverse and / or Reckwazverfahren are not only costly to manufacture, but also offer special with regard to a required volume distribution at the forging preform only small Nachstell- or correction options.

Andererseits ist es aus der DE 199 16 590 A1 bekannt, Schmiedevorformen durch Stauchen bereitzustellen, wobei hierzu ein Stauchen in eine Kavität vorgenommen wird, bei welchem durch Matrizen eine Kavität gebildet wird, in welche ein Stauchstempel eintaucht, um das Werkstück entsprechend in die Kavität hinein umzuformen, so dass dessen Oberfläche anschließend im Wesentlichen der Oberfläche der Werkstückumforminnenkontur der Kavität entspricht.On the other hand it is from the DE 199 16 590 A1 known to provide Schmiedevorformen by upsetting, for this purpose, a upsetting is carried out in a cavity in which a cavity is formed by matrices, in which an upsetting die dips to appropriately transform the workpiece into the cavity, so that its surface then essentially the Surface of the Werkstückumforminnenkontur the cavity corresponds.

Beim Stauchen ist allerdings zu unterscheiden zwischen einem Stauchen in eine Kavität, wie dieses in der DE 199 16 590 A1 offenbart ist, und einem freiem Stauchen, wie dieses in der DE 1 301 297 B1 offenbart ist und bei welchem keine Kavität vorgesehen ist und ein Werkstück beidseits eines Verformungsbereichs mittels Klemmbacken eingeklemmt wird, die dann stauchend aufeinander zu bewegt werden, wobei sich das Material beim Stauchen in den Zwischenraum zwischen den beiden Klemmbacken frei aufbaut.When upsetting, however, a distinction must be made between a compression in a cavity, as this in the DE 199 16 590 A1 is disclosed, and a free compression, like this in the DE 1 301 297 B1 is disclosed and in which no cavity is provided and a workpiece is clamped on both sides of a deformation region by means of clamping jaws, which are then moved toward each other in compression, wherein the material builds up during upsetting in the space between the two jaws.

Während ein freies Stauchen naturgemäß nur wenige Eingriffsmöglichkeiten zur Erzeugung von Masseunterschieden über den Halbzeugquerschnitt im gestauchten Bereich ermöglicht, offenbart gerade die DE 199 16 590 A1 eine Vorrichtung und ein Verfahren zur Erzeugung großer Masseunterschiede über den Halbzeugquerschnitt, wobei dieses jedoch für komplexe zu schmiedende Produkte immer noch zu erheblichem Ausschuss führt, so dass weiterhin auf herkömmliche Quer- und/oder Reckwalzverfahren zurückgegriffen werden muss.While free upsetting naturally only allows a few possibilities of intervention to produce mass differences across the semifinished product cross section in the compressed area, this is precisely what the DE 199 16 590 A1 a device and a method for generating large differences in mass across the semi-finished product, but this still leads to considerable rejects for complex products to be forged, so that must continue to resort to conventional transverse and / or stretching roll.

Gattungsgemäße Verfahren und Vorrichtungen sind beispielsweise aus der EP 0 786 296 A1 oder aus der JP 59-054440 A bekannt.Generic methods and devices are for example from the EP 0 786 296 A1 or from the JP 59-054440 A known.

Es ist Aufgabe vorliegender Erfindung insbesondere die vorstehend genannten Nachteile beim Erzeugen einer Schmiedevorform mittels herkömmlicher Quer- und/oder Reckwalzverfahren zu beheben.It is an object of the present invention, in particular, to overcome the abovementioned disadvantages when producing a forging preform by means of conventional transverse and / or stretching rolling methods.

Die Aufgabe wird durch ein Verfahren nach Anspruch 1 bzw. durch eine Umformvorrichtung nach Anspruch 6 gelöst.The object is achieved by a method according to claim 1 or by a forming device according to claim 6.

Weitere vorteilhafte Ausführungsformen sind in den abhängigen Ansprüchen definiert.Further advantageous embodiments are defined in the dependent claims.

Weitere Vorteile, Ziele und Eigenschaften vorliegender Erfindung werden anhand anliegender Zeichnung und nachfolgender Beschreibung erläutert, in welchen einerseits beispielhaft eine Warmstauchvorrichtung, welche erfindungsgemäß ein Schmiedevorform-Werkzeug aufweist, und andererseits eine Umformvorrichtung zum Umformen eines Werkstücks dargestellt und beschrieben sind.Further advantages, objects and features of the present invention will be explained with reference to the appended drawing and the following description, in which on the one hand by way of example a hot-swaging device which according to the invention has a forging preform tool and on the other hand a forming device for forming a workpiece are shown and described.

In der Zeichnung zeigen:

Figur 1
schematisch eine erste Ansicht einer Warmstauchvorrichtung mit einem geöffneten Umformwerkzeug zum Erzeugen einer Schmiedevorformkontur an einem Werkstück;
Figur 2
schematisch eine weitere Ansicht des geöffneten Umformwerkzeugs aus der Figur 1 mit eingelegtem Werkstück vor einer Stauchphase;
Figur 3
schematisch eine Ansicht des Umformwerkzeugs aus den Figuren 1 und 2 in geschlossenem Zustand während einer Stauchphase;
Figur 4
schematisch nochmals eine Ansicht des wiedergeöffneten Umformwerkzeugs aus den Figuren 1 bis 3 mit einer fertig gestauchten Schmiedevorform nach der Stauchphase;
Figur 5
schematisch eine Querschnittsansicht durch ein vorderes Längssegment der Warmstauchvorrichtung aus den Figuren 1 bis 4 bei geöffnetem Umformwerkzeug;
Figur 6
schematisch eine Querschnittsansicht durch das vordere Laingssegment der Warmstauchvorrichtung aus den Figuren 1 bis 5 bei geschlossenem Umformwerkzeug;
Figur 7
schematisch eine Ansicht einer vorderen, mittleren und hinteren Festmatrize des Umformwerkzeugs;
Figur 8
schematisch eine Ansicht der Festmatrizen des Umformwerkzeugs nach Figur 7 in zusammengeschobenem Zustand mit vier zugehörigen Querschnitten; und
Figur 9
schematisch eine Ansicht weiterer vorderer, mittlerer und hinterer Festmatrizen eines Umformwerkzeugs in zusammengeschobenem Zustand mit vier zugehörigen Querschnitten in ähnlicher Darstellung wie Figur 8.
In the drawing show:
FIG. 1
schematically a first view of a hot-swaging device with an open forming tool for producing a Schmiedevorformkontur on a workpiece;
FIG. 2
schematically another view of the open forming tool from the FIG. 1 with inserted workpiece before a compression phase;
FIG. 3
schematically a view of the forming tool from the Figures 1 and 2 in the closed state during an upsetting phase;
FIG. 4
schematically again a view of the reopened forming tool from the FIGS. 1 to 3 with a finished blacksmith preform after the compression phase;
FIG. 5
schematically a cross-sectional view through a front longitudinal segment of the heat-upsetting of the FIGS. 1 to 4 with open forming tool;
FIG. 6
schematically a cross-sectional view through the front Laingssegment of the hot-swaging device from the FIGS. 1 to 5 with closed forming tool;
FIG. 7
schematically a view of a front, middle and rear fixed die of the forming tool;
FIG. 8
schematically a view of the fixed dies of the forming tool after FIG. 7 in collapsed condition with four associated cross sections; and
FIG. 9
schematically a view of further front, middle and rear fixed dies of a forming tool in the collapsed state with four corresponding cross sections in a similar representation as FIG. 8 ,

Die in den Figuren 1 bis 4 gezeigte Umformvorrichtung 1 umfasst ein Umformwerkzeug 2, welches in der Darstellung gemäß der Figur 1 geöffnet abgebildet ist.The in the FIGS. 1 to 4 Forming device 1 shown comprises a forming tool 2, which in the illustration according to the FIG. 1 is shown open.

Die Umformvorrichtung 1 ist in diesem Ausführungsbeispiel eine Warmstauchvorrichtung 3.The forming device 1 in this embodiment is a hot-swaging device 3.

Das Umformwerkzeug 2 ist hinsichtlich einer Stauchachse 4 eines Stauchstempels 5 der Umformvorrichtung 1 radial in ein Oberteil 6 und in ein Unterteil 7 zweigeteilt ausgestaltet.With regard to an upsetting axis 4 of an upsetting die 5 of the forming device 1, the forming tool 2 is radially configured in two parts in an upper part 6 and in a lower part 7.

Der Stauchstempel 5 ist durch eine Stempelführung 5A hindurch geführt und er kann durch einen hier nicht weiter gezeigten Antrieb fluchtend zur Stauchachse 4 in das Umformwerkzeug 2 hinein oder aus dem Umformwerkzeug 2 heraus bewegt werden.The upsetting punch 5 is guided through a punch guide 5A and it can be moved by a drive not shown here in alignment with the upsetting axis 4 in the forming tool 2 or out of the forming tool 2 out.

Das Umformwerkzeug 2 weist eine Kavität 8 mit veränderlichen Querschnitten 9 auf, die dementsprechend innerhalb des Umformwerkzeugs 2 eine unsymmetrische Werkstückumforminnenkontur 10 bereitstellt.The forming tool 2 has a cavity 8 with variable cross sections 9, which accordingly provides an asymmetrical workpiece forming inner contour 10 within the forming tool 2.

Das Umformwerkzeug 2 ist in diesem Ausführungsbeispiel zusätzlich in drei Längssegmente 11, 12 und 13 unterteilt, wobei das vordere Längssegment 11 eine vordere Festmatrize 14 und eine vordere Klemmmatrize 15, das mittlere Längssegment 12 eine mittlere Festmatrize 16 und eine mittlere Klemmmatrize 17 sowie das hintere Längssegment 13 eine hintere Festmatrize 18 und eine hintere Klemmmatrize 19 umfasst.The forming tool 2 is additionally divided in this embodiment into three longitudinal segments 11, 12 and 13, wherein the front longitudinal segment 11, a front Festmatrize 14 and a front clamping die 15, the middle longitudinal segment 12, a middle Festmatrize 16 and a central clamping die 17 and the rear longitudinal segment 13 comprises a rear fixed die 18 and a rear clamping die 19.

Insofern ist die Kavität 8 sowohl radial als auch axial mehrteilig ausgestaltet.In this respect, the cavity 8 is designed both radially and axially in several parts.

Jede der Klemmmatrizen 15, 17 bzw. 19 ist an der ihr zugeordneten Festmatrize 14, 16 bzw. 18 mittels einer entsprechenden Gelenkverbindung 20 fest, aber gelenkig angeordnet. Es versteht sich, dass in anderen Ausführungsformen auch andere Anordnungen der unterschiedlichen Matrizen sowie abweichende Maßnahmen zu einer Positionierung derselben zueinander vorgesehen sein können.Each of the clamping matrices 15, 17 and 19, respectively, is fixed but hinged to its associated fixed die 14, 16 and 18, respectively, by means of a corresponding hinge connection 20. It is understood that in other embodiments, other arrangements of the different matrices and deviating measures to a positioning of the same can be provided to each other.

Die Umformvorrichtung 2 dieses Ausführungsbeispiels zeichnet sich darüber hinaus durch eine gemeinsame Axialführungseinrichtung 21 aus, an welcher alle Festmatrizen 14, 16 und 18 über die jeweilige Gelenkverbindung 20 - und somit indirekt auch alle Klemmmatrizen 15, 17 und 19 - axial verschieblich hintereinander befestigt sind.The forming device 2 of this embodiment is also characterized by a common Axialführungseinrichtung 21, to which all Festmatrizen 14, 16 and 18 via the respective hinge joint 20 - and thus indirectly also all clamping matrices 15, 17 and 19 - are mounted axially displaceable one behind the other.

Die Axialführungseinrichtung 21 ist in diesem Ausführungsbeispiel konstruktiv einfach als eine einzige Lineartraverse ausgestaltet. Sie kann aber auch als mehrteiliges Bauteil bzw. Bauteilgruppe realisiert sein, sollte dies erforderlich sein.The Axialführungseinrichtung 21 is in this embodiment structurally simple designed as a single linear crossmember. But it can also be implemented as a multi-part component or group of components, should this be necessary.

Damit die einzelnen Längssegmente 11, 12 und 13 an der gemeinsamen Axialführungseinrichtung 21 zudem schnell ausgetauscht werden können, verfügt die Umformvorrichtung 1 noch über eine Halteeinrichtung 22 mit Halteelementen 23, 24 und 25.In order that the individual longitudinal segments 11, 12 and 13 on the common Axialführungseinrichtung 21 also can be quickly replaced, the forming device 1 still has a holding device 22 with holding elements 23, 24 and 25th

Mittels der Halteelemente 23, 24 und 25 werden die Längssegmente 11, 12 bzw. 13 verschieblich an der gemeinsamen Axialführungseinrichtung 21 fixiert.By means of the holding elements 23, 24 and 25, the longitudinal segments 11, 12 and 13 are fixed in a displaceable manner on the common axial guide device 21.

Die einzelnen Festmatrizen 14, 16 bzw. 18 sind bei vorliegendem Ausführungsbeispiel mittels Schraubverbindungen 26 an den jeweiligen Halteelementen 23, 24 und 15 angeschraubt. Es versteht sich, dass hier auch andere Verbindungsmöglichkeiten, wie beispielsweise Schnellspanner oder Formschlussverbindungen, vorgesehen sein können.The individual fixed matrices 14, 16 and 18 are screwed in the present embodiment by means of screw 26 to the respective holding elements 23, 24 and 15. It is understood that other connection options, such as quick release or positive connection, can be provided here.

Da insbesondere zwei jeweils axial benachbarte Festmatrize 14, 16, 18 des Umformwerkzeugs 2 axial lose aneinander liegend angeordnet sind, weist die Umformvorrichtung 1 einen Axialanschlag 27 auf, an welchem sich speziell die Festmatrize 14, 16, 18 während eines Stauchprozesses axial abstützen können.Since in particular two axially adjacent fixed dies 14, 16, 18 of the forming tool 2 are arranged axially loosely adjacent to one another, the forming device 1 has an axial stop 27, on which especially the fixed dies 14, 16, 18 can be axially supported during an upsetting process.

Der Axialanschlag 27 ist in diesem Ausführungsbeispiel konstruktiv einfach als eine austauschbare Komponente der Axialführungseinrichtung 21 ausgebildet.The axial stop 27 is designed in this embodiment structurally simple as a replaceable component of the axial guide 21.

Zum Erzeugen einer Schmiedevorform 30 (siehe Figur 4) mit einer Schmiedevorformkontur 31 mit veränderlichen Querschnitten 32 für das anschließende Schmieden eines hier nicht gezeigten Schmiedeteils wird in die Kavität 8 ein Werkstück 33 mit einer im Wesentlichen zylindrischen Kontur 34 eingelegt (siehe Figur 2).To create a forging preform 30 (see FIG. 4 ) with a Schmiedevorformkontur 31 with variable cross-sections 32 for the subsequent forging of a forgings, not shown here, a workpiece 33 with a substantially cylindrical contour 34 is inserted into the cavity 8 (see FIG. 2 ).

Anschließend wird das Umformwerkzeug 2 geschlossen, so wie es in der Figur 3 dargestellt ist. Die jeweils auf die Festmatrizen 14, 16 bzw. 18 abgesenkten Klemmmatrizen 15, 17 bzw. 19 werden jeweils mittels einer Schnellklemmeinrichtung 35, 36 bzw. 37 verriegelt. Insofern ist ein Aufspringen der Umformvorrichtung 2 während des Stauchprozesses ausgeschlossen.Subsequently, the forming tool 2 is closed, as it is in the FIG. 3 is shown. The respectively on the fixed matrices 14, 16 and 18 lowered clamping matrices 15, 17 and 19 are respectively locked by means of a quick clamping device 35, 36 and 37 respectively. In this respect, a popping of the forming device 2 is excluded during the compression process.

Nun kann die eigentliche Stauchphase gemäß einer Stauchbewegung 38 (siehe Figur 3) erfolgen, in welchem die Anordnung um den Stauchstempel 5 und der Stempelführung 5A herum einerseits die einzelnen Längssegmente 11, 12 und 13 gegen den Axialanschlag 27 schiebt und andererseits gleichzeitig der Stauchstempel 5 das Werkstück 33 innerhalb der Kavität 8 staucht, wobei das Werkstück 33 zu der Schmiedevorform 30 mit den veränderlichen Querschnitten 32 umgeformt wird.Now the actual compression phase according to a compression movement 38 (see FIG. 3 ) take place, in which the arrangement around the upsetting die 5 and the punch guide 5A on the one hand pushes the individual longitudinal segments 11, 12 and 13 against the axial stop 27 and on the other hand simultaneously upsetting punch 5, the workpiece 33 within the cavity 8 compresses, the workpiece 33 to the forging preform 30 is deformed with the variable cross sections 32.

Vorteilhafter Weise hat die Schmiedevorform 30 nun eine definierte Volumenverteilung, welche im Wesentlichen derjenigen eines Schmiedeteils nach einem ersten Schmiedeschritt entspricht.Advantageously, the forging preform 30 now has a defined volume distribution which substantially corresponds to that of a forging part after a first forging step.

Insofern wird erfindungsgemäß erstmals ein Warmstauchverfahren zum Erzeugen einer Schmiedevorform 30 mit veränderlichen Querschnitten 32 zum Herstellen eines Schmiedeteils verwendet.In this respect, according to the invention, a hot upsetting method for producing a forging preform 30 with variable cross sections 32 for producing a forged part is used for the first time.

Die Schnittdarstellung gemäß der Figur 5 zeigt die Umformvorrichtung 1 im Bereich des vorderen Längssegmentes 11 mit geöffnetem Umformwerkzeug 2.The sectional view according to the FIG. 5 shows the forming device 1 in the region of the front longitudinal segment 11 with the forming tool 2 open.

Die vordere Festmatrize 14 des Umformwerkzeugs 2 ist mit zwei ersten Schrauben 40 und 41 der Schraubverbindung 26 an dem ersten Halteelement 23 der Halteeinrichtung 22 befestigt.The front fixed die 14 of the forming tool 2 is fastened with two first screws 40 and 41 of the screw connection 26 to the first holding element 23 of the holding device 22.

Nach der gezeigten Schnittdarstellung erkennt man gut, dass das erste Halteelement 23 einen der vorderen Festmatrize 14 zugewandten oberen Teil 42 und einen der Axialführungseinrichtung 21 zugewandten unteren Teil 43 aufweist.After the sectional illustration shown, it can be seen well that the first holding element 23 has an upper part 42 facing the front solid die 14 and a lower part 43 facing the axial guiding device 21.

Das obere Teil 42 ist hierbei mit zwei Innensechskantschrauben 44 und 45 an dem unteren Teil 43 angeschraubt, wobei es sich versteht, dass diesbezüglich bei anderen Ausführungsformen auch andere Befestigungsarten oder auch eine einstückige Ausgestaltung der Festmatrize 14 vorgesehen sein kann. Die übrigen Festmatrizen 16, 18 sind bei diesem Ausführungsbeispiel ähnlich aufgebaut, was jedoch nicht zwingend der Fall sein muss.The upper part 42 is in this case screwed with two hexagon socket screws 44 and 45 to the lower part 43, it being understood that in this regard in other embodiments, other types of fastening or a one-piece design of Solid die 14 may be provided. The remaining fixed matrices 16, 18 are similar in this embodiment, but this need not necessarily be the case.

Die Axialführungseinrichtung 21 umfasst ein Fußteil 46 und ein Führungsteil 47, an welchem die Längssegmente 11, 12 und 13 des Umformwerkzeugs 2 verschieblich gelagert sind.The axial guide device 21 comprises a foot part 46 and a guide part 47, on which the longitudinal segments 11, 12 and 13 of the forming tool 2 are displaceably mounted.

Das Führungsteil 47 ist entlang der Axialführungseinrichtung 21 mit einer Reihe von weiteren Schrauben 48 an das Fußteil 46 geschraubt.The guide member 47 is screwed along the Axialführungseinrichtung 21 with a number of other screws 48 to the foot part 46.

An das obere Teil 42 des ersten Halteelements 23 ist die erste Schnellklemmverbindung 35 der Gelenkverbindung 20 mit einer Flanschverschraubung 49 angeflanscht.At the upper part 42 of the first holding member 23, the first quick-clamp connection 35 of the hinge joint 20 is flanged with a Flanschverschraubung 49.

Die Schnellklemmverbindung 35 weist einen Hebelmechanismus 50 auf, mittels welchem das vordere Längssegment 11 des Umformwerkzeugs 2 manuell geöffnet bzw. geschlossen werden kann.The quick-clamping connection 35 has a lever mechanism 50, by means of which the front longitudinal segment 11 of the forming tool 2 can be manually opened or closed.

Während die Schnellklemmverbindung 35 mittels eines unteren Schenkels 51 mit dem oberen Teil 42 korrespondiert, ist die Schnellklemmverbindung 35 mit einem entsprechenden oberen Schenkel 52 an der vorderen Klemmmatrize 15 angeschraubt. Hierfür ist eine Schraubbefestigung 53 vorgesehen.While the quick-clamp connection 35 corresponds to the upper part 42 by means of a lower leg 51, the quick-clamp connection 35 is screwed to a corresponding upper leg 52 on the front clamping template 15. For this purpose, a screw 53 is provided.

Es versteht sich, dass statt einer manuellen Bedienung auch ein motorischer, insbesondere auch ein hydraulischer oder pneumatischer, Antrieb vorgesehen sein kann.It is understood that instead of a manual operation and a motor, especially a hydraulic or pneumatic drive can be provided.

Die Schnittdarstellung gemäß der Figur 6 zeigt die Umformvorrichtung 1 in einem geschlossen Zustand, bei welchem die vordere Klemmmatrize 15 auf die vordere Festmatrize 14 abgesenkt ist. Hierbei ist die Kavität 8 zumindest im Bereich des vorderen Längssegmentes 11 geschlossen.The sectional view according to the FIG. 6 shows the forming device 1 in a closed state, in which the front clamping die 15 is lowered onto the front Festmatrize 14. Here, the cavity 8 is closed at least in the region of the front longitudinal segment 11.

Der Schnellklemmmechanismus 35 befindet sich hierbei in einer verriegelten Position 54, so dass sich die vordere Klemmmatrize 15 während eines Umformprozesses von der vorderen Festmatrize 14 nicht abhebt und dadurch das Umformwerkzeug 2 zumindest teilweise geöffnet werden würde.The quick clamping mechanism 35 is here in a locked position 54, so that the front clamping die 15 does not lift off from the front fixed die 14 during a forming process and thereby the forming tool 2 would be at least partially opened.

Die Merkmale zu dem hier erläuterten ersten Längssegment 11 können auf die weiteren Längssegmente 12 und 13 übertragen werden, so dass diese nicht zusätzlich erläutert werdenThe features of the first longitudinal segment 11 explained here can be transferred to the further longitudinal segments 12 and 13 so that they are not additionally explained

Jeweils in einer schematischen Aufsicht gemäß der Figuren 7 und 8 sind die vordere Festmatrize 14, die mittlere Festmatrize 16 und die hintere Festmatrize 18 nochmals beispielhaft gezeigt. Die Festmatrizen 14, 16 und 18 sind entlang der Stauchachse 4 axial hintereinander angeordnet und werden insbesondere während des Stauchens axial von der Anordnung nach Figur 7 zur der Anordnung nach Figur 8 zusammengefahren. Zwar ist diese Verfahrensführung nicht zwingend und es ist denkbar, dass die Matrizen bereits vor dem Stauchen zusammengefahren sind bzw. sogar in axialer Richtung lediglich eine Matrize zur Anwendung kommt, wobei dieses jedoch zu verhältnismäßigen großen Axialbewegungen zwischen Werkstück und Werkzeug gerade im Bereich der Innenwandung des Werkstücks führt, welche einerseits den Verschleiß und andererseits den Energieverbrauch erhöhen.Each in a schematic plan according to the FIGS. 7 and 8th For example, the front solid die 14, the middle solid die 16, and the rear solid die 18 are again exemplified. The Festmatrizen 14, 16 and 18 are arranged along the upsetting axis 4 axially behind one another and in particular during the upsetting axially of the arrangement according to FIG. 7 to the arrangement FIG. 8 moved together. Although this procedure is not mandatory and it is conceivable that the matrices are already collapsed before upsetting or even in the axial direction only one die is used, but this to relatively large axial movements between the workpiece and tool just in the inner wall of the Workpiece, which on the one hand increase wear and on the other hand energy consumption.

Die vordere Festmatrize 14 gestaltet einen ersten unteren Teilraum 55 der Kavität 8 des Umformwerkzeugs 2 aus. Entsprechend bilden die mittlere Festmatrize 16 einen zweiten unteren Teilraum 56 und die hintere Festmatrize 18 einen dritten unteren Teilraum 57 der Kavität 8 aus. Hinzu kommen noch entsprechende obere Teilräume (nicht gezeigt) der Klemmmatrizen 15, 17 und 19. Es ist leicht verständlich, dass hierdurch die Kavität 8 hinsichtlich der Werkstückumforminnenkontur 10 insgesamt komplex und vielseitig variiert werden kann und insbesondere unterschiedlichste veränderliche Querschnitte 9 der Kavität 8 dargestellt sein können, wie sie in Figur 8 exemplarisch dargestellt sind, die dann zu entsprechend veränderlichen Querschnitten 32 der Schmiedevorform 30 führen können.The front fixed die 14 configures a first lower subspace 55 of the cavity 8 of the forming tool 2. Accordingly, the middle fixed die 16 form a second lower subspace 56 and the rear fixed die 18 form a third lower subspace 57 of the cavity 8. In addition, corresponding upper subspaces (not shown) of the clamping matrices 15, 17 and 19. It is easy to understand that thereby the cavity 8 with respect to the Werkstückumforminnenkontur 10 can be varied overall complex and versatile and in particular a variety of variable cross sections 9 of the cavity 8 to be represented can, as in FIG. 8 are exemplified, which can then lead to correspondingly variable cross-sections 32 of the forging preform 30.

Die Teilräume 55, 56 und 57 der Festmatrizen 14, 16, 18 sowie die entsprechenden Teilräume der Klemmmatrizen 15, 17, 19 sind in diesem Ausführungsbeispiel mittels eines Erodierverfahrens verfahrenstechnisch relativ einfach in die jeweilige Matrize 14, 15, 16, 17, 18 und 19 eingearbeitet.The subspaces 55, 56 and 57 of the fixed matrices 14, 16, 18 and the corresponding subspaces of the clamping matrices 15, 17, 19 are procedurally relatively simple in this embodiment by means of an erosion process in the respective die 14, 15, 16, 17, 18 and 19 incorporated.

Hierdurch und durch die hohe Vielzahl an einzelnen Teilräumen 55, 56 und 57 etc. sind wesentlich komplexere Schmiedevorformkonturen 31 herstellbar als dies mit herkömmlichen Walzverfahren hinsichtlich des Erzeugens einer Schmiedevorform 30 möglich ist.As a result of this and due to the large number of individual subspaces 55, 56 and 57 etc., substantially more complex forging contour contours 31 can be produced than is possible with conventional rolling methods with regard to the production of a forging preform 30.

Die vordere Festmatrize 14 weist zwei Senkbohrungen 58 und 59 für die beiden zuvor beschriebenen Schrauben 40 und 41 auf.The front Festmatrize 14 has two countersunk bores 58 and 59 for the two previously described screws 40 and 41.

Entsprechende Senkbohrungen (hier nicht mehr gesondert beziffert) finden sich an den beiden Festmatrizen 16 und 18.Corresponding counterbores (not numbered separately here) can be found on the two fixed matrices 16 and 18.

Da der erste Teilraum 55 einen Teilraumdurchmesser 60 aufweist, der kritisch größer ist als eine dazugehörigen Teilraumlänge 61 des ersten Teilraums 55, sind in dem Teilraum 55 Mittel 62 zum partiellen Reduzieren des Teilraumdurchmessers 60 vorgesehen, welche in diesem Ausführungsbeispiel als ein Flankendom 63 realisiert sind.Since the first subspace 55 has a subspace diameter 60 that is critically greater than an associated subspace length 61 of the first subspace 55, means 62 for partially reducing the subspace diameter 60 are provided in the subspace 55, which are implemented as a flank dome 63 in this embodiment.

Der Flankendorn 63 umfasst vorliegend einen klemmmatrizenseitigen feststehenden Längsdorn 64 und einen festmatrizenseitigen feststehenden Längsdom 65 (siehe Figuren 5 und 8), die in die Kavität 8 hineinragen.In the present case, the flank mandrel 63 comprises a clamping mandrel-side fixed longitudinal mandrel 64 and a fixed-die-side fixed longitudinal mandrel 65 (see FIG Figures 5 and 8th ), which protrude into the cavity 8.

Insofern ist innerhalb der Kavität 8 ein Mittel zum Indizieren eines Sollfließverhaltens angeordnet; und zwar in Bereichen der Kavität 8, in welchen der Teilraumdurchmesser 60 größer ist als ein designierter Innendurchmesser 66 des Umformwerkzeugs 2, in welchem der Stauchstempel 5 angeordnet bzw. geführt ist.In this respect, a means for indexing a desired flow behavior is arranged within the cavity 8; in areas of the cavity 8, in which the subspace diameter 60 is greater than a designated inner diameter 66 of the forming tool 2, in which the upsetting die 5 is arranged or guided.

Somit können konstruktiv besonders einfach bereits während des Schließens des Umformwerkzeugs 2 zumindest bereichsweise auf das Werkstück 33 Radialpresskraifte ausgeübt werden, die insbesondere im Wesentlichen senkrecht zur axialen Stauchrichtung 38 verlaufen.Thus, even during the closing of the forming tool 2, at least in regions, radial pressure jaws can be exerted on the workpiece 33 in a structurally particularly simple manner, which in particular run essentially perpendicular to the axial upsetting direction 38.

Insofern wird hierdurch das Werkstück 33 zumindest partiell umgeformt, so dass das entsprechende Werkstückmaterial innerhalb des Teilraums 55 vor dem eigentlichen Axialstauchprozess mit einem gewünschten Fließverhalten fließt, wodurch ein Ausbrechen des Werkstücks 33 während des axialen Stauchens nahezu ausgeschlossen ist.In this respect, the workpiece 33 is thereby at least partially reshaped, so that the corresponding workpiece material flows within the subspace 55 before the actual Axialstauchprozess with a desired flow behavior, whereby a breaking of the workpiece 33 during the axial upsetting is almost impossible.

Die in Figur 9 dargestellte Ausführungsform entspricht im Wesentlichen der Ausführungsform nach Figuren 1 bis 8, so dass hier identisch wirkende Baugruppen auch identisch beziffert sind. In Abweichung von der Ausführungsform nach Figuren 1 bis 8 weist die Ausführungsform nach Figur 9 Mittel 62 zum partiellen Reduzierens des Teilraumdurchmessers 60 auf, die wesentlich weniger in die Kavität 8 hineinragen und das Werkstück 33 bei Schließen der Matrizen 14 bis 19 im Wesentlichen lediglich reibschlüssig in radialer Richtung, also parallel zum Teilraumdurchmesser 60, fixieren. Je nach konkreter Verfahrensführung reicht hierzu bereits eine elastische Verformung durch entsprechende Anformbereiche 67, 68 der Mittel 62 zum partiellen Reduzierens des Teilraumdurchmessers 60 aus, wobei hier ggf. auch eine plastische Verformung vorgesehen sein kann. bereits durch eine elastische Verformung bzw. durch lediglich einen Reibschluss lässt sich die Gefahr eines seitlichen Ausbrechens erfolgreich minimieren, um auch große, insbesondere über die axiale Erstreckung des Werkstücks 33 variierende Querschnitte, betriebssicher ausfüllen zu können. Bezugsziffernliste: 1 Umformvorrichtung 30 Schmiedevorform 2 Umformwerkzeug 31 Schmiedevorformkontur 3 Warmstauchvorrichtung 32 veränderliche Querschnitte 4 Stauchachse 33 Werkstück 5 Stauchstempel 34 zylindrische Kontur 5A Stempelführung 35 erste Schnellklemmeinrichtung 6 Oberteil 36 zweite Schnellklemmeinrichtung 7 Unterteil 37 dritte Schnellklemmeinrichtung 8 Kavität 38 Stauchbewegung 9 veränderliche Querschnitte 40 erste Schraube 10 Werkstückumforminnenkontur 41 zweite Schraube 11 vorderes Längssegment 42 oberer Teil 12 mittleres Längssegment 43 unterer Teil 13 hinteres Längssegment 44 erste Innensechskantschraube 14 vordere Festmatrize 45 zweite Innensechskantschraube 15 vordere Klemmmatrize 46 Fußteil 16 mittlere Festmatrize 47 Führungsteil 17 mittlere Klemmmatrize 48 weitere Schrauben 18 hintere Festmatrize 49 Flanschverschraubung 19 hintere Klemmmatrize 50 Hebelmechani smus 20 Gelenkverbindung 51 unterer Schenkel 21 Axialführungseinrichtung 52 oberer Schenkel 22 Halteeinrichtung 53 Schraubbefestigung 23 erstes Halteelement 54 verriegelte Position 24 zweites Halteelement 55 erster unterer Teilraum 25 drittes Halteelement 56 zweiter unterer Teilraum 26 S chraubverbindungen 57 dritter unterer Teilraum 27 Axialanschlag 58 erste Senkbohrung 59 zweite Senkbohrung 60 Teilraumdurchmesser 61 Teilraumlänge 62 Mittel zum Reduzieren 63 Flankendorn 64 Längsdom 65 Längsdom 66 designierter Innendurchmesser 67 Anformbereich 68 Anformbereich In the FIG. 9 illustrated embodiment substantially corresponds to the embodiment according to FIGS. 1 to 8 , so that identically acting assemblies are also numbered identically. In deviation from the embodiment according to FIGS. 1 to 8 the embodiment according to FIG. 9 Means 62 for partially reducing the subspace diameter 60, which protrude much less into the cavity 8 and the workpiece 33 when closing the matrices 14 to 19 substantially only frictionally in the radial direction, ie parallel to the subspace diameter 60, fix. Depending on the specific process control, an elastic deformation by means of corresponding molding areas 67, 68 of the means 62 for partially reducing the partial space diameter 60 is sufficient for this purpose, in which case a plastic deformation may also be provided. Already by an elastic deformation or by only one frictional engagement, the risk of lateral breakage can be successfully minimized in order to be able to reliably fill also large cross-sections, in particular over the axial extension of the workpiece 33. List of reference numerals: 1 reshaping 30 forging preform 2 forming tool 31 Forging preform contour 3 Warm clincher 32 variable cross sections 4 compression axis 33 workpiece 5 swaging dies 34 cylindrical contour 5A punch guide 35 first quick-clamping device 6 top 36 second quick-clamping device 7 lower part 37 third quick-clamping device 8th cavity 38 upsetting movement 9 variable cross sections 40 first screw 10 Werkstückumforminnenkontur 41 second screw 11 front longitudinal segment 42 upper part 12 middle longitudinal segment 43 lower part 13 rear longitudinal segment 44 first hexagon socket screw 14 front solid die 45 second hexagon socket screw 15 front clamping die 46 footboard 16 medium solid die 47 guide part 17 middle clamping die 48 more screws 18 rear fixed die 49 flange bolting 19 rear clamping die 50 Lever mechanism 20 articulation 51 lower thigh 21 axial guidance 52 upper leg 22 holder 53 Screw 23 first holding element 54 locked position 24 second holding element 55 first lower subspace 25 third retaining element 56 second lower subspace 26 Screw connections 57 third lower subspace 27 axial stop 58 first counterbore 59 second counterbore 60 Subspace diameter 61 Subspace length 62 Means for reducing 63 edge Dorn 64 Längsdom 65 Längsdom 66 designated inner diameter 67 shaping area 68 shaping area

Claims (14)

  1. A method for producing a forge preform (30) for forging a forged component, in which, using a forming tool (2), a contour (34) of a workpiece (33) is reshaped to obtain a forge preform contour (31), characterised in that the workpiece (33) is placed into a cavity (8) of the forming tool (2) and during closing of the cavity (8) is shaped at least partially, the workpiece (33) is then upset in the closed forming tool (2) to obtain a forge preform (30) and thereafter can be provided as a forge preform (30) with a defined volume pre-distribution for use in a subsequent forging process.
  2. The method according to claim 1, characterised in that the workpiece (33) is plastically shaped.
  3. The method according to claim 1, characterised in that the workpiece (33) is merely elastically shaped.
  4. The method according to one of claims 1 to 3, characterised in that the workpiece (33) is already held in a friction lock prior to upsetting.
  5. The method according to one of claims 1 to 4, characterised in that the forming tool (2) comprises more than one longitudinal segment (11, 12, 13), which are arranged spaced apart from one another at the start of the upsetting process and during upsetting are positioned so as to form a common cavity in relation to one another.
  6. A forming device (1) or warm upsetting device (3) for producing a forge preform (30) for forging a forged component by means of a forming tool (2), in which the forming tool (2) comprises a workpiece forming contour (10) with variable cross-sections (9), by means of which a volume pre-distribution can be produced on the forge preform (30), characterised in that the forming tool (2) comprises a designated inner diameter (66) on a side facing a header die (5), wherein the forming tool (2), in subspaces (55) of the cavity (8) with a subspace diameter (60) larger than the designated inner diameter (66), comprises means (62) for partially reducing the subspace diameter (60).
  7. The forming device (1) or warm upsetting device (3) according to claim 6, characterised in that the forming tool (2) comprises a cavity (8) with variable cross-sections (9).
  8. The forming device (1) or warm upsetting device (3) according to claim 6 or 7, characterised in that the forming tool (2) comprises more than one longitudinal segment (11, 12, 13) and in that the longitudinal segments (11, 12, 13) are arranged axially one behind the other on a common axial guidance unit (21).
  9. The forming device (1) or warm upsetting device (3) according to claim 8, characterised in that the longitudinal segments (11, 12, 13) of the forming tool (2) are arranged so as to be exchangeable on the common axial guidance unit (21).
  10. The forming device (1) or warm upsetting device (3) according to one of claims 6 to 9, characterised in that the cavity (8) is designed in several parts both radially and axially, in particular is designed so as to be variable.
  11. The forming device (1) or warm upsetting device (3) according to one of claims 6 to 10, characterised in that the forming tool (2), in subspaces (55) of the cavity (8) with a subspace diameter (60) larger than the designated inner diameter (66), comprises means (62) for partially reducing the subspace diameter (60) vertically to the larger subspace diameter (60).
  12. The forming device (1) or warm upsetting device (3) according to one of claims 6 to 11, characterised in that the forming tool (2), in subspaces (55, 56, 57) with a subspace length (61) greater than 1.5 times the subspace diameter of the respective subspace (55), comprises means (62) for partially reducing the subspace diameter (60).
  13. The forming device (1) or warm upsetting device (3) according to claim 11 or 12, characterised in that the means (62) for partially reducing the subspace diameter (60) comprises a flank thorn (63) which partially protrudes into the cavity (8) of the forming tool (2).
  14. The forming device (1) or warm upsetting device (3) according to one of claims 11 to 13, characterised in that the means (62) for partially reducing the subspace diameter (60) comprise at least one friction-lock-forming shaping area (67, 68).
EP12000767.9A 2011-02-04 2012-02-06 Method for producing a forge preform and warm upsetting device Not-in-force EP2484462B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102011010446 2011-02-04
DE102011105244A DE102011105244A1 (en) 2011-02-04 2011-06-10 Use of a heat upsetting method, use of a forming tool, method of producing a forging preform and forming apparatus or heat upsetting apparatus

Publications (3)

Publication Number Publication Date
EP2484462A2 EP2484462A2 (en) 2012-08-08
EP2484462A3 EP2484462A3 (en) 2012-10-24
EP2484462B1 true EP2484462B1 (en) 2017-07-26

Family

ID=45654868

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12000767.9A Not-in-force EP2484462B1 (en) 2011-02-04 2012-02-06 Method for producing a forge preform and warm upsetting device

Country Status (2)

Country Link
EP (1) EP2484462B1 (en)
DE (1) DE102011105244A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102873237A (en) * 2012-10-17 2013-01-16 西南铝业(集团)有限责任公司 T-shaped forge piece blank-manufacturing processing technology and device thereof
CN109317588B (en) * 2018-10-16 2020-07-24 中国航发南方工业有限公司 Forging method and die for blade of aero-engine
CN113477865B (en) * 2021-08-19 2022-10-28 中国航发沈阳黎明航空发动机有限责任公司 Adjustable forging die of short centre gripping semi-closed
CN113680939B (en) * 2021-08-28 2023-09-01 湖北三环锻造有限公司 T-arm sinking upsetting die
CN114309405B (en) * 2021-12-30 2023-05-05 广东联塑阀门有限公司 Warm upsetting process and system for stainless steel inserts
CN114603320B (en) * 2022-03-28 2023-02-14 伊莱特能源装备股份有限公司 Manufacturing method of large-scale special-shaped tower flange forging

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1050460A (en) * 1911-12-20 1913-01-14 Reinhold G Housdorfer Die for forming axles.
DE1301297B (en) * 1964-09-02 1969-08-21 Ts Lab Obro Bki Plastycznej Device for upsetting elongated workpieces on presses
JPS608892B2 (en) * 1981-10-08 1985-03-06 株式会社神戸製鋼所 Seamless forging method
JPS5954440A (en) * 1982-09-21 1984-03-29 Sumitomo Heavy Ind Ltd Rough forging device for hot forging
DE19603035C2 (en) * 1996-01-29 1998-03-26 Cdp Aluminiumtechnik Gmbh & Co Method and device for producing semi-finished products
DE19916590A1 (en) * 1999-04-13 2000-10-26 Cdp Aluminiumtechnik Gmbh & Co Method and device for producing a semi-finished product
DE10119839C2 (en) * 2001-04-23 2003-09-11 Benteler Automobiltechnik Gmbh Method for manufacturing an axle element for motor vehicles
JP2004261857A (en) * 2003-03-04 2004-09-24 Saitama Press Tanzo Kk Forming method for forging, and preforming device used in forming method for forging
US7406852B2 (en) * 2005-01-31 2008-08-05 Showa Denko K.K. Upsetting method and upsetting apparatus

Non-Patent Citations (1)

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

Also Published As

Publication number Publication date
DE102011105244A1 (en) 2012-08-09
EP2484462A3 (en) 2012-10-24
EP2484462A2 (en) 2012-08-08

Similar Documents

Publication Publication Date Title
EP2484462B1 (en) Method for producing a forge preform and warm upsetting device
EP2641673B1 (en) Method and apparatus for producing a connecting section as part of a tool
DE2462641C3 (en) Device for the non-cutting cold forming of a blank into a workpiece with a central body with radial extensions
EP2440341A2 (en) Method and device for producing elongated metal components having helical grooves, especially twist drills or endless screws
EP2344288A2 (en) Method and device for the non-cutting production of an outside thread on hollow metal work pieces
EP2458131B1 (en) Method for manufacturing the insertion end of a drill
DE4401674C2 (en) Method and device for punching workpieces
DE1627707A1 (en) Process for the production of a metal molding
DE2535155A1 (en) DEVICE AND METHOD FOR MANUFACTURING A BALL BEARING
EP1689556A2 (en) Cold forming method for producing ball journals
EP1252947B1 (en) Method for the manufacture of an axle element for a motor vehicle
DE1292107B (en) Die for electro upsetting
EP2839900B1 (en) Method and device for manufacturing a connection section with an end section as part of a tool
DE102014212732B4 (en) Process and upsetting device for the production of offset workpieces such as shafts or rods
DE4207964A1 (en) Cold forming process and equipment esp. for screw driver bits of cross slot form - with hexagonal head formed at one end of round bar blank and cross-slot profile formed at other end with concentric closing pile
EP2271449B1 (en) Threaded nut, method and tool for producing the same
DE2808198A1 (en) METHOD AND DEVICE FOR THE FORMATION OF A JOURNAL ON A HOLLOW BLANK AXLE
EP3221068B1 (en) Method for manufacturing a rotationally symmetrical shaped article
DE3101123A1 (en) METHOD AND DEVICE FOR DEFORMING A METAL BAR INTO A TULIP-SHAPED PART BY FLOW-PRESSING IN A CLOSED CHAMBER
EP1345715B1 (en) Forging press comprising an adjusting device on the matrix side thereof
DE102019002187B4 (en) Method and device for producing a component with a thread
DE202010013183U1 (en) Press for forming cylindrical workpieces
DE19930015B4 (en) Method for producing a plurality of molded parts by hydroforming
DE2413745A1 (en) METHOD AND DEVICE FOR FORMING METAL PARTS BY COLD PRESSING
WO2014044271A1 (en) Method and device for producing grooved bolts

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

AK Designated contracting states

Kind code of ref document: A2

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

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

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

RIC1 Information provided on ipc code assigned before grant

Ipc: B21J 1/04 20060101AFI20120920BHEP

Ipc: B21J 13/02 20060101ALI20120920BHEP

Ipc: B21J 5/08 20060101ALI20120920BHEP

17P Request for examination filed

Effective date: 20130424

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

Owner name: SMS GROUP 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: 20170217

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

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

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 911968

Country of ref document: AT

Kind code of ref document: T

Effective date: 20170815

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: R096

Ref document number: 502012010835

Country of ref document: DE

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20170726

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: FI

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

Effective date: 20170726

Ref country code: SE

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

Effective date: 20170726

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: 20171026

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: 20170726

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: 20170726

Ref country code: NL

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

Effective date: 20170726

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

Ref country code: RS

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

Effective date: 20170726

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: 20171027

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: 20170726

Ref country code: ES

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

Effective date: 20170726

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: 20171026

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: 20170726

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: 20171126

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

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: 20170726

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: 20170726

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: 20170726

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502012010835

Country of ref document: DE

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

Ref country code: IT

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

Effective date: 20170726

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: 20170726

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: 20170726

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: 20170726

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: 20180430

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: 20170726

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: MT

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

Effective date: 20170726

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: 20170726

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

Effective date: 20180206

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20180228

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: 20180228

Ref country code: LU

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

Effective date: 20180206

Ref country code: CH

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

Effective date: 20180228

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20181031

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: 20180206

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

Ref country code: GB

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

Effective date: 20180206

Ref country code: FR

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

Effective date: 20180228

Ref country code: BE

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

Effective date: 20180228

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 911968

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180206

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: 20180206

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

Ref country code: TR

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

Effective date: 20170726

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: 20120206

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: 20170726

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: 20170726

Ref country code: MK

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

Effective date: 20170726

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: 20170726

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

Ref country code: DE

Payment date: 20220225

Year of fee payment: 11

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

Effective date: 20230514

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502012010835

Country of ref document: DE

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

Ref country code: DE

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

Effective date: 20230901