EP2823916A1 - Composite casting - Google Patents
Composite casting Download PDFInfo
- Publication number
- EP2823916A1 EP2823916A1 EP13175828.6A EP13175828A EP2823916A1 EP 2823916 A1 EP2823916 A1 EP 2823916A1 EP 13175828 A EP13175828 A EP 13175828A EP 2823916 A1 EP2823916 A1 EP 2823916A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- insert
- producing
- casting
- composite casting
- composite
- 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.)
- Granted
Links
- 238000005266 casting Methods 0.000 title claims abstract description 72
- 239000002131 composite material Substances 0.000 title claims abstract description 30
- 239000000463 material Substances 0.000 claims abstract description 87
- 238000000034 method Methods 0.000 claims abstract description 23
- 238000004519 manufacturing process Methods 0.000 claims abstract description 17
- 229910000831 Steel Inorganic materials 0.000 claims description 22
- 239000010959 steel Substances 0.000 claims description 22
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 7
- 229910001018 Cast iron Inorganic materials 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 5
- 230000008569 process Effects 0.000 claims description 5
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 4
- 239000011777 magnesium Substances 0.000 claims description 4
- 229910052749 magnesium Inorganic materials 0.000 claims description 4
- 229910052751 metal Inorganic materials 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 4
- 238000003466 welding Methods 0.000 claims description 4
- 239000011230 binding agent Substances 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 claims description 3
- 239000007800 oxidant agent Substances 0.000 claims description 3
- 229910001369 Brass Inorganic materials 0.000 claims description 2
- 229910000906 Bronze Inorganic materials 0.000 claims description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 2
- 229910004298 SiO 2 Inorganic materials 0.000 claims description 2
- 229910052910 alkali metal silicate Inorganic materials 0.000 claims description 2
- 239000010951 brass Substances 0.000 claims description 2
- 239000010974 bronze Substances 0.000 claims description 2
- 229910052802 copper Inorganic materials 0.000 claims description 2
- 239000010949 copper Substances 0.000 claims description 2
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 claims description 2
- LIKBJVNGSGBSGK-UHFFFAOYSA-N iron(3+);oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[Fe+3].[Fe+3] LIKBJVNGSGBSGK-UHFFFAOYSA-N 0.000 claims description 2
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 claims description 2
- 239000011248 coating agent Substances 0.000 description 6
- 238000009792 diffusion process Methods 0.000 description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 239000007769 metal material Substances 0.000 description 4
- 229910001208 Crucible steel Inorganic materials 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 239000000155 melt Substances 0.000 description 3
- 238000007711 solidification Methods 0.000 description 3
- 230000008023 solidification Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 239000012778 molding material Substances 0.000 description 2
- 238000007712 rapid solidification Methods 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910000677 High-carbon steel Inorganic materials 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 1
- 125000004432 carbon atom Chemical group C* 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 239000011133 lead Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000011089 mechanical engineering Methods 0.000 description 1
- 239000002905 metal composite material Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000011135 tin Substances 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/04—Casting in, on, or around objects which form part of the product for joining parts
Definitions
- the invention relates to a method for producing a composite casting comprising an insert and casting material, wherein the insert is materially connected to the casting material.
- the DE 10 2006 041 901 A1 discloses a method for producing metal composite parts from steel and / or cast iron.
- the einzug manende part which is made of steel or cast iron, coated by flux.
- the coating aims at a reduction, that is to say that during the pouring, the oxide skin of the casting is dissolved and washed away, as a result of which the casting material can form a metallurgical bond.
- the DE 10 2011 053 858 B3 discloses a method of using a pourable component in a lost mold, wherein a coating agent is applied to a surface of the inflowing component.
- the coating agent forms a separation-active surface, which prevents adhesion of the material to the component and corrosion before casting with casting material.
- the DE 100 43 105 B4 discloses a method of forming a tough, resilient and / or at least substantially defect free bond between an insert and a cast metal material having a melting point below that of the feedstock.
- the insert is coated with a thin layer of a metallic material derived from the group of silver, antimony, bismuth, chromium, gold, lead, magnesium, silicon, tin, titanium and zinc. This is followed by casting of the casting material against the coated surface of the insert.
- the thermal expansion coefficient of the coating is greater than that of the insert and less than that of the casting material.
- the coated insert is also maintained at a temperature of at least 100 ° C for a period of at least 5 minutes.
- Object of the present invention is to provide a method and a corresponding composite casting, which achieved over the prior art, an improved bond between an insert and casting material, and ensures economic production.
- the sheathing or embedding of the insert is formed by an exothermic material which ignites due to the contact with the inflowing casting material or by reaching the ignition temperature. This energy is released and released to the environment, resulting in a reduced temperature gradient between the solidifying melt and the insert.
- Exothermic materials are in addition to the use in welding (Thermitsch Stammsgemische) in exothermic feeders in the foundry used. Upon contact of the melt with the exothermic mass, a combustion reaction is triggered, which ensures in the feeder that there is the last solidifying melt and so that the changing volume during solidification in the casting can be compensated.
- welding Thermitschweissgemische
- a combustion reaction is triggered, which ensures in the feeder that there is the last solidifying melt and so that the changing volume during solidification in the casting can be compensated.
- such a known material causing an exothermic reaction is used as a sheath for the inflowing insert.
- the material ignites.
- the insert is heated from both sides, which prevents rapid solidification of the casting material in the border region to the insert, since the insert loses its quenching effect for the casting material.
- the temperature gradient between casting material and insert is minimized. This, in turn, promotes carbon diffusion between the casting material and the insert, whereby a cohesive or metallurgical bond can be produced.
- the insert is preferably made of steel, copper, bronze, brass, aluminum or an aluminum alloy.
- the process or the composite casting is versatile due to the wide choice of materials.
- the exothermic material preferably has an easily oxidizable metal, in particular aluminum and / or magnesium.
- the exothermic material has an oxidizing agent for the readily oxidizable metal, in particular iron (III) oxide.
- the backfill material used is preferably an oxide, in particular SiO 2 .
- the backfill material serves as a filling material, which is mixed with the other substances such as aluminum and / or magnesium and an oxidizing agent.
- the exothermic material preferably comprises a binder which serves the cohesion of the exothermic material.
- the preferred binder is an alkali silicate in use.
- a preferred embodiment is that a cast iron is used as the casting material, preferably GJS, GJL and / or GJV.
- a cast iron is used as the casting material, preferably GJS, GJL and / or GJV.
- a high strength and elongation at break can be achieved at designated locations in the cast component, or additional, positive properties for a subsequent further treatment can be given to the composite cast component.
- an aluminum alloy is used as the casting material, thereby, for example, aluminum components can be combined with various metallic materials, whereby the advantage of the weight reduction can be used by the light aluminum.
- the inventive method is used with lost molds.
- an insert which has a sufficient thickness or wall thickness, which makes it possible to subject the insert after the casting process nor a heat treatment or welding process.
- Methods which are known from the prior art allow only the pouring of a steel part, which is very thin-walled, in order to counteract the rapid solidification and the impeded carbon diffusion by the contact of the room temperature-controlled steel part with the casting material something.
- a hollow body is used as an insert.
- the cavity fills with the casting material and connects cohesively with the insert.
- the outer surface of the insert is coated with the exothermic material or embedded in the material.
- the mass Due to the exothermic reaction of the mass after contact with the melt, the mass also gives off heat to the insert, resulting in a unified temperature gradient between the solidifying melt and the insert.
- the insert can also be unilaterally, or in hollow execution from the inside with the exothermic material in combination.
- the exothermic material can be easily removed and the outer surface or inner surface of the insert emerges.
- Post-processing is then possible, but in some cases not necessary because the dimensional accuracy and the surface finish are already of good quality.
- the inventive method is economically highly interesting. Furthermore, these methods provide extended possibilities to after-treat the cast component, such as e.g. Welding or heat treatment (even partially on the insert).
- Such composite castings produced by the method according to the invention are particularly suitable for general mechanical engineering, construction machinery and vehicle construction. It can thereby different materials economically combined with each other and the preferred properties of the individual materials are combined with each other, without the problem of insufficient connection of the materials by early solidification of the casting material occurs.
- Fig. 1 shows a partial section of a mold in which a composite casting 1 was shed.
- the casting material 2 flows into the mold 5 formed by the mold in which an insert 3 is inserted in order to enter into a cohesive or metallurgical bond with the cast material 2.
- GJS preferably GJS, GJL or GJV
- the exothermic material 4 this ignites, whereby heat is released to the environment.
- the insert is thereby heated and the temperature gradient between the solidifying melt and the insert is reduced.
- the carbon diffusion between casting material 2, which directly touches the insert 3, and the insert 3 is driven forward.
- a cohesive or metallurgical connection at the direct contact points between insert 3 and casting material 2 is achieved.
- the exothermic material 4 can be easily removed from the insert 3.
- the area covered by the exothermic material 4 / n of the insert 3 is free of casting material, thus a reworking of the surface of the insert is not necessarily necessary, which in turn makes the inventive method economically very interesting.
- FIG. 2-4 Another embodiment is by the Fig. 2-4 demonstrated.
- insert 3 a cylindrical steel tube made of a high-carbon steel with wall thicknesses of 5 mm is used and molded into exothermic material 4 with a defined wall thickness.
- This steel pipe 3 with surrounding exothermic material 4 is inserted into the mold 5 to be cast as from Fig. 2 seen.
- the closed mold 5 is filled with melt 2 for producing a GJS, wherein the interior of the steel pipe 3 is flowed through by melt 2 and a part of the exothermic material 4 has direct melt contact. After the ignition temperature of the exothermic material 4 is reached, this gives off heat to the environment and the steel pipe 3. This is greatly heated and the temperature gradient between steel pipe 3 and solidifying melt 2 is reduced.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Abstract
Verfahren zur Herstellung eines Verbundgussteils enthaltend ein Einlegeteil und Gussmaterial, wobei das Einlegeteil stoffschlüssig mit dem Gussmaterial verbunden ist und das Verfahren folgende Schritte umfasst: Herstellen des Einlegeteils, Ummanteln bzw. Einbetten des Einlegeteils, Einlegen des ummantelten/eingebetteten Einlegeteils in die Giessform, Füllen der Form mit Schmelze, wobei die Ummantelung/Einbettung des Einlegeteils durch ein exothermes Material gebildet wird, das sich durch die Kontaktierung mit dem einfliessenden Gussmaterials oder durch Erreichen der Zündtemperatur der exothermen Masse entzündet wodurch der Temperaturgradient zwischen erstarrender Schmelze und dem Einlegeteil verringert wird.A method for producing a composite casting comprising an insert and cast material, wherein the insert is materially bonded to the cast material and the method comprises the steps of: Making the insert, Wrapping or embedding the insert, Inserting the coated / embedded insert into the mold, Filling the mold with melt, wherein the sheath / embedding of the insert is formed by an exothermic material which ignites by contacting with the inflowing casting material or by reaching the ignition temperature of the exothermic mass whereby the temperature gradient between solidifying melt and the insert is reduced.
Description
Die Erfindung betrifft ein Verfahren zur Herstellung eines Verbundgussteils enthaltend ein Einlegeteil und Gussmaterial, wobei das Einlegeteil stoffschlüssig mit dem Gussmaterial verbunden ist.The invention relates to a method for producing a composite casting comprising an insert and casting material, wherein the insert is materially connected to the casting material.
Die Herstellung von Verbundgussteilen ermöglicht eine Kombination der bevorzugten Eigenschaften der Materialien an den entsprechenden Stellen. So können Bauteile entsprechend ihren Anforderungen und Einsatzgebieten aufgrund der Materialkombination optimal zusammengestellt werden. Das bedingt aber einer stoffschlüssigen bzw. metallurgischen Verbindung zwischen den Materialien. Beim Eingiessen von Stahlteilen in Gusseisen oder Aluminiumlegierungen tritt häufig das Problem der unzureichenden Verbindung zwischen eingegossenem Stahlteil und umschliessenden bzw. eingegossenem Werkstoff auf. Durch das frühe Erstarren der Schmelze aufgrund des Kontakts mit dem raumtemperierten Einlegeteil, wird ein metallurgisches bzw. stoffschlüssiges Verbinden zwischen Gusswerkstoff und Stahlteil behindert, wodurch Spalten zwischen den Verbundpartnern entstehen können.The production of composite castings allows a combination of the preferred properties of the materials in the appropriate locations. So components can be optimally assembled according to their requirements and applications due to the combination of materials. However, this requires a cohesive or metallurgical connection between the materials. When pouring steel parts into cast iron or aluminum alloys, the problem often arises of insufficient connection between cast-in steel part and enclosing or cast-in material. The early solidification of the melt due to the contact with the space-tempered insert, a metallurgical or cohesive bonding between the casting material and steel part is hindered, which can cause gaps between the composite partners.
Die
Die
Die
Aufgabe der vorliegenden Erfindung ist es, ein Verfahren und ein entsprechendes Verbundgussteil zu schaffen, welches gegenüber dem Stand der Technik eine verbesserte Bindung zwischen einem Einlegeteil und Gussmaterial erzielt, sowie eine wirtschaftliche Herstellung gewährleistet.Object of the present invention is to provide a method and a corresponding composite casting, which achieved over the prior art, an improved bond between an insert and casting material, and ensures economic production.
Diese Aufgabe wird erfindungsgemäss dadurch gelöst, dass die Ummantelung bzw. Einbettung des Einlegeteils durch ein exothermes Material gebildet wird, welches sich durch die Kontaktierung mit dem einfließenden Gussmaterials oder durch Erreichen der Zündtemperatur entzündet. Dabei wird Energie freigesetzt und an die Umgebung abgegeben, wodurch es zu einem verringert Temperaturgradienten zwischen der erstarrenden Schmelze und dem Einlegeteil kommt.This object is achieved according to the invention in that the sheathing or embedding of the insert is formed by an exothermic material which ignites due to the contact with the inflowing casting material or by reaching the ignition temperature. This energy is released and released to the environment, resulting in a reduced temperature gradient between the solidifying melt and the insert.
Das erfindungsgemässe Verfahren umfasst folgende Schritte:
- Herstellen des Einlegeteils,
- Ummanteln bzw. Einbetten des Einlegeteils mittels exothermen Material,
- Einlegen des ummantelten/eingebetteten Einlegeteils in die Giessform,
- Füllen der Form mit Schmelze.
- Making the insert,
- Wrapping or embedding the insert by means of exothermic material,
- Inserting the coated / embedded insert into the mold,
- Filling the mold with melt.
Exotherme Materialien werden neben dem Einsatz beim Schweissen (Thermitschweissgemische) auch in exothermen Speisern in der Giesserei eingesetzt. Bei der Berührung der Schmelze mit der exothermen Masse wird eine Verbrennungsreaktion ausgelöst, welche im Speiser gewährleistet, dass sich dort die zuletzt erstarrende Schmelze befindet und sodass das verändernde Volumen während der Erstarrung im Gussteil ausgeglichen werden kann. Solche Materialien sind aus dem Stand der Technik bekannt, die
In der vorliegenden Erfindung wird ein solch bekanntes Material das eine exotherme Reaktion verursacht, als Ummantelung bzw. Einbettung für das einzugiessende Einlegeteil eingesetzt. Durch die Berührung des exothermen Materials mit dem flüssigen Gussmaterialoder durch Erreichen der Zündtemperatur der exothermen Masse entzündet sich das Material. Dadurch wird das Einlegeteil von beiden Seiten aufgeheizt, was ein rasches Erstarren des Gussmaterials im Grenzbereich zum Einlegeteil verhindert, da das Einlegeteil seine Abschreckwirkung für das Gussmaterial verliert. Der Temperaturgradient zwischen Gussmaterial und Einlegeteil wird minimiert. Das wiederum treibt die Kohlenstoffdiffusion zwischen Gussmaterial und Einlegeteil voran, wodurch eine stoffschlüssige bzw. metallurgische Verbindung erzeugt werden kann.In the present invention, such a known material causing an exothermic reaction is used as a sheath for the inflowing insert. By contacting the exothermic material with the liquid casting material or by reaching the ignition temperature of the exothermic mass, the material ignites. As a result, the insert is heated from both sides, which prevents rapid solidification of the casting material in the border region to the insert, since the insert loses its quenching effect for the casting material. The temperature gradient between casting material and insert is minimized. This, in turn, promotes carbon diffusion between the casting material and the insert, whereby a cohesive or metallurgical bond can be produced.
Das Einlegeteil ist vorzugsweise aus Stahl, Kupfer, Bronze, Messing, Aluminium oder einer Aluminiumlegierung hergestellt. Das Verfahren bzw. das Verbundgussteil ist durch die breite Materialauswahl vielseitig einsetzbar.The insert is preferably made of steel, copper, bronze, brass, aluminum or an aluminum alloy. The process or the composite casting is versatile due to the wide choice of materials.
Vorzugsweise weist das exotherme Material ein leicht oxidierbares Metall insbesondere Aluminium und/oder Magnesium auf.The exothermic material preferably has an easily oxidizable metal, in particular aluminum and / or magnesium.
Zudem ist es Vorteilhaft, dass das exotherme Material ein Oxidationsmittel für das leicht oxidierbare Metall aufweist insbesondere Eisen(III)-oxid.In addition, it is advantageous that the exothermic material has an oxidizing agent for the readily oxidizable metal, in particular iron (III) oxide.
Als Hinterfüllstoff wird vorzugsweise ein Oxid eingesetzt, insbesondere SiO2. Der Hinterfüllstoff dient als Füllmaterial, welcher mit den weiteren Stoffen wie Aluminium und/oder Magnesium sowie einem Oxidationsmittel vermengt wird.The backfill material used is preferably an oxide, in particular SiO 2 . The backfill material serves as a filling material, which is mixed with the other substances such as aluminum and / or magnesium and an oxidizing agent.
Das exotherme Material weist vorzugsweise ein Bindemittel auf, welches dem Zusammenhalt des exothermen Materials dient. Als bevorzugtes Bindemittel ist ein Alkalisilicat im Einsatz.The exothermic material preferably comprises a binder which serves the cohesion of the exothermic material. The preferred binder is an alkali silicate in use.
Eine bevorzugte Ausgestaltung besteht darin, dass als Gussmaterial ein Gusseisen eingesetzt wird, vorzugsweise GJS, GJL und/oder GJV. Durch das eingegossene Einlegeteil kann an dafür vorgesehenen Stellen im Gussbauteil eine hohe Festigkeit und Bruchdehnung erreicht werden, bzw. zusätzliche, positive Eigenschaften für eine nachfolgende Weiterbehandlung dem Verbundgussbauteil gegeben werden.A preferred embodiment is that a cast iron is used as the casting material, preferably GJS, GJL and / or GJV. Through the cast-in insert, a high strength and elongation at break can be achieved at designated locations in the cast component, or additional, positive properties for a subsequent further treatment can be given to the composite cast component.
Bei Verbundgussteilen, die durch Verfahren hergestellt wurden, die aus dem Stand der Technik bekannt sind, sind die Verbindungen zwischen Gussmaterial und Einlegeteil meist ungenügend. Verbundgussteile die durch das erfindungsgemäss Verfahren hergestellt wurden, weisen eine verbesserte stoffschlüssige Verbindung zwischen den Materialien auf.In composite castings produced by methods known in the art, the connections between the cast material and the insert are usually insufficient. Composite castings which have been produced by the method according to the invention have an improved cohesive connection between the materials.
Der Einsatz solcher hergestellten Verbundgussteile bietet eine gute Alternative Stahlguss- bzw. Stahlschweisskonstruktionen mit dem Vorteil der bekannten Gusseisenlegierungen und deren Herstellungsverfahren zu substituieren.The use of such manufactured composite castings offers a good alternative to substituting cast steel or steel welded constructions with the advantage of the known cast iron alloys and their method of manufacture.
Als bevorzugte Ausführungsform wird als Gussmaterial eine Aluminiumlegierung eingesetzt, dadurch können bspw. Aluminiumbauteile mit verschiedenen metallischen Materialien kombiniert werden, wodurch der Vorteil der Gewichtsreduktion durch das leichte Aluminium genutzt werden kann.As a preferred embodiment, an aluminum alloy is used as the casting material, thereby, for example, aluminum components can be combined with various metallic materials, whereby the advantage of the weight reduction can be used by the light aluminum.
Vorzugsweise wird das erfindungsgemässe Verfahren mit verlorenen Giessformen angewandt.Preferably, the inventive method is used with lost molds.
Durch dieses Verfahren besteht die Möglichkeit ein Einlegeteil einzusetzen, welches eine genügende Dicke bzw. Wandstärke aufweist, die es ermöglicht, das Einlegeteil nach dem Giessverfahren noch einem Wärmebehandlungs- bzw. Schweissverfahren zu unterziehen. Verfahren, die aus den Stand der Technik bekannt sind, ermöglichen nur das Eingiessen eines Stahlteils, welches sehr dünnwandig ist, um dem raschen Erstarren und der behinderten Kohlenstoffdiffusion durch den Kontakt des raumtemperierten Stahlteils mit dem Gussmaterials etwas entgegen zu halten. Vorzugsweise wird ein Hohlkörper als Einlegeteil eingesetzt. Der Hohlraum füllt sich mit dem Gussmaterial und verbindet sich stoffschlüssig mit dem Einlegeteil. Die äussere Oberfläche des Einlegeteils ist mit dem exothermen Material ummantelt bzw. in das Material eingebettet. Durch die exotherme Reaktion der Masse nach der Berührung mit der Schmelze, gibt die Masse Wärme auch an das Einlegeteil ab, wodurch es zu einem vereinheitlichtem Temperaturgradienten zwischen der erstarrenden Schmelze und dem Einlegeteil kommt. Das Einlegeteil kann auch einseitig, oder bei hohler Ausführung von innen mit dem exothermen Material in Verbindung stehen.By this method, it is possible to use an insert, which has a sufficient thickness or wall thickness, which makes it possible to subject the insert after the casting process nor a heat treatment or welding process. Methods which are known from the prior art, allow only the pouring of a steel part, which is very thin-walled, in order to counteract the rapid solidification and the impeded carbon diffusion by the contact of the room temperature-controlled steel part with the casting material something. Preferably, a hollow body is used as an insert. The cavity fills with the casting material and connects cohesively with the insert. The outer surface of the insert is coated with the exothermic material or embedded in the material. Due to the exothermic reaction of the mass after contact with the melt, the mass also gives off heat to the insert, resulting in a unified temperature gradient between the solidifying melt and the insert. The insert can also be unilaterally, or in hollow execution from the inside with the exothermic material in combination.
Nach dem Giessvorgang und dem Entformen kann das exotherme Material leicht entfernt werden und die äussere Oberfläche oder die innere Fläche des Einlegeteils tritt zum Vorschein. Ein Nachbearbeiten ist anschliessend möglich, aber in manchen Fällen auch nicht von Nöten da die Massgenauigkeit und die Oberflächenbeschaffenheit bereits von guter Qualität sind. Auch durch das mögliche Einsparen von weiteren Bearbeitungsschritten ist das erfindungsgemässe Verfahren wirtschaftlich hoch interessant. Weiterhin ergeben sich durch diese Verfahren erweiterte Möglichkeiten das Gussbauteil nachzubehandeln, wie z.B. Schweissen oder Wärmebehandeln (auch nur partiell am Einlegeteil).After the casting and demolding, the exothermic material can be easily removed and the outer surface or inner surface of the insert emerges. Post-processing is then possible, but in some cases not necessary because the dimensional accuracy and the surface finish are already of good quality. Also by the possible savings of further processing steps, the inventive method is economically highly interesting. Furthermore, these methods provide extended possibilities to after-treat the cast component, such as e.g. Welding or heat treatment (even partially on the insert).
Solche Verbundgussteile hergestellt nach dem erfindungsgemässen Verfahren eignen sich insbesondre für den allgemeinen Maschinenbau, für Baumaschinen und den Fahrzeugbau. Es können dadurch unterschiedliche Materialien auch bei hohen Stückzahlen wirtschaftlich miteinander verbunden und die bevorzugten Eigenschaften der einzelnen Materialien miteinander kombiniert werden, ohne dass die Problematik einer ungenügenden Verbindung der Materialien durch frühes Erstarren des Gussmaterials auftritt.Such composite castings produced by the method according to the invention are particularly suitable for general mechanical engineering, construction machinery and vehicle construction. It can thereby different materials economically combined with each other and the preferred properties of the individual materials are combined with each other, without the problem of insufficient connection of the materials by early solidification of the casting material occurs.
Ausführungsbeispiele der Erfindung werden anhand der Figuren beschrieben, wobei sich die Erfindung nicht nur auf die Ausführungsbeispiele beschränkt. Es zeigt:
- Fig. 1
- einen Teilschnitt einer Giessform mit eingesetztem ummantelten Einlegeteil,
- Fig. 2
- eine fotographische Abbildung eines mit exothermem Material ummantelten Stahlrohrs,
- Fig. 3
- ein Schliffbild durch einen Ausschnitt des Verbundgussteils und
- Fig.4
- ein Ausschnitt eines Verbundgussbauteil mit eingegossenem Stahlteil
- Fig. 1
- a partial section of a mold with inserted jacketed insert,
- Fig. 2
- a photographic image of a steel tube encased with exothermic material,
- Fig. 3
- a microsection through a section of the composite casting and
- Figure 4
- a section of a composite cast component with cast steel part
Ein weiteres Ausführungsbeispiel ist durch die
- 11
- VerbundgussteilComposite casting
- 22
- Gussmaterialcast material
- 33
- Einlegeteil / StahlrohrInsert / steel tube
- 44
- Exothermes MaterialExothermic material
- 55
- Giessform aus FormmaterialCasting mold made of molding material
Claims (13)
dadurch gekennzeichnet, dass die Ummantelung/Einbettung des Einlegeteils durch ein exothermes Material gebildet wird, das sich durch die Kontaktierung mit dem einfliessenden Gussmaterials oder durch Erreichen der Zündtemperatur der exothermen Masse entzündet wodurch der Temperaturgradient zwischen erstarrender Schmelze und dem Einlegeteil verringert wird.
characterized in that the sheathing / embedding of the insert is formed by an exothermic material which ignites by contacting with the inflowing casting material or by reaching the ignition temperature of the exothermic mass whereby the temperature gradient between solidifying melt and the insert is reduced.
vorangehenden Ansprüche, dadurch gekennzeichnet, dass das Verbundgussteil zumindest am Einlegeteil einer Wärmebehandlung bzw. einem Schweissverfahren unterzogen werden kannProcess for producing a composite casting according to one of
previous claims, characterized in that the composite casting at least at the insert part of a heat treatment or a welding process can be subjected
nach dem Verfahren nach einem der vorangehenden Ansprüche, dadurch gekennzeichnet, dass das Einlegeteil mit dem Gussmaterial stoffschlüssig verbunden ist.Composite casting include an insert and a cast material made
according to the method according to one of the preceding claims, characterized in that the insert is materially connected to the casting material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP13175828.6A EP2823916B1 (en) | 2013-07-10 | 2013-07-10 | Method of manufacturing a composite casting |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP13175828.6A EP2823916B1 (en) | 2013-07-10 | 2013-07-10 | Method of manufacturing a composite casting |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2823916A1 true EP2823916A1 (en) | 2015-01-14 |
EP2823916B1 EP2823916B1 (en) | 2018-12-26 |
Family
ID=48748015
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13175828.6A Active EP2823916B1 (en) | 2013-07-10 | 2013-07-10 | Method of manufacturing a composite casting |
Country Status (1)
Country | Link |
---|---|
EP (1) | EP2823916B1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108262466A (en) * | 2017-12-13 | 2018-07-10 | 浙江灿根智能科技有限公司 | A kind of bi-metal casting process |
DE102016104351B4 (en) | 2016-03-10 | 2018-08-23 | Knorr-Bremse Systeme für Nutzfahrzeuge GmbH | Cast iron brake caliper of a disc brake and method of making a caliper |
CN114029450A (en) * | 2021-11-10 | 2022-02-11 | 北京星航机电装备有限公司 | Light alloy casting embedded pipeline assembly and preparation method thereof and casting method of light alloy part with embedded pipeline |
Citations (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3433282A (en) * | 1965-12-14 | 1969-03-18 | Us Army | Method for eliminating hot tear cracks in castings |
JPS57187159A (en) * | 1981-05-13 | 1982-11-17 | Mitsubishi Heavy Ind Ltd | Formation of surface coating layer |
JPS5953641A (en) * | 1982-09-20 | 1984-03-28 | Toyota Motor Corp | Production of composite material utilizing exothermic reaction |
JPS60174244A (en) * | 1984-02-21 | 1985-09-07 | Mitsubishi Heavy Ind Ltd | Production of composite casting |
EP0659899A1 (en) * | 1993-12-20 | 1995-06-28 | General Motors Corporation | Metallurgical bonding of metals and/or ceramics |
DE19642838A1 (en) | 1996-10-17 | 1997-07-31 | Daimler Benz Ag | Feeder for metal casting comprising exothermic material with flat ring set on one end |
DE19650056A1 (en) * | 1996-12-03 | 1998-06-04 | Thyssen Guss Ag | Method for producing a brake disc, in particular as an axle or wheel brake disc for rail vehicles |
EP1050358A1 (en) * | 1999-05-06 | 2000-11-08 | KS Aluminium-Technolgie Aktiengesellschaft | Moulding method using a precursor |
EP1050354A1 (en) | 1999-05-04 | 2000-11-08 | Chemex Gmbh | Formable exothermic composition and feeder made therefrom |
EP0888199B1 (en) | 1996-03-25 | 2002-10-09 | Ashland Inc. | Sleeves, their preparation, and use |
DE10043105B4 (en) | 1999-08-31 | 2007-06-14 | Cummins Inc., Columbus | Metallurgical bonding of coated inserts within metal castings |
DE102006041901A1 (en) | 2006-09-07 | 2008-03-27 | Daimler Ag | Production of composite metal articles from steel or cast iron, comprises coating steel or cast iron with flux and drying it, then casting steel or cast iron around it, flux comprising e.g. alkali metal borate or alkaline earth metal borate |
DE102007059771A1 (en) * | 2007-12-12 | 2009-06-18 | Daimler Ag | Cylinder bush or cylinder liner made of gray iron- or aluminum alloy for casting in a light metal alloy on the basis of aluminum or aluminum/magnesium, comprises a conditioning coating for casting |
DE102011053858B3 (en) | 2011-09-22 | 2013-03-14 | Preiss Metallwaren Gmbh & Co. Kg | Applying castable component in a lost mold, comprises applying a coating agent at least in sections, on a surface of the component, and applying the component before blowing out the lost mold |
-
2013
- 2013-07-10 EP EP13175828.6A patent/EP2823916B1/en active Active
Patent Citations (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3433282A (en) * | 1965-12-14 | 1969-03-18 | Us Army | Method for eliminating hot tear cracks in castings |
JPS57187159A (en) * | 1981-05-13 | 1982-11-17 | Mitsubishi Heavy Ind Ltd | Formation of surface coating layer |
JPS5953641A (en) * | 1982-09-20 | 1984-03-28 | Toyota Motor Corp | Production of composite material utilizing exothermic reaction |
JPS60174244A (en) * | 1984-02-21 | 1985-09-07 | Mitsubishi Heavy Ind Ltd | Production of composite casting |
EP0659899A1 (en) * | 1993-12-20 | 1995-06-28 | General Motors Corporation | Metallurgical bonding of metals and/or ceramics |
EP0888199B1 (en) | 1996-03-25 | 2002-10-09 | Ashland Inc. | Sleeves, their preparation, and use |
DE19642838A1 (en) | 1996-10-17 | 1997-07-31 | Daimler Benz Ag | Feeder for metal casting comprising exothermic material with flat ring set on one end |
DE19650056A1 (en) * | 1996-12-03 | 1998-06-04 | Thyssen Guss Ag | Method for producing a brake disc, in particular as an axle or wheel brake disc for rail vehicles |
EP1050354A1 (en) | 1999-05-04 | 2000-11-08 | Chemex Gmbh | Formable exothermic composition and feeder made therefrom |
EP1050358A1 (en) * | 1999-05-06 | 2000-11-08 | KS Aluminium-Technolgie Aktiengesellschaft | Moulding method using a precursor |
DE10043105B4 (en) | 1999-08-31 | 2007-06-14 | Cummins Inc., Columbus | Metallurgical bonding of coated inserts within metal castings |
DE102006041901A1 (en) | 2006-09-07 | 2008-03-27 | Daimler Ag | Production of composite metal articles from steel or cast iron, comprises coating steel or cast iron with flux and drying it, then casting steel or cast iron around it, flux comprising e.g. alkali metal borate or alkaline earth metal borate |
DE102007059771A1 (en) * | 2007-12-12 | 2009-06-18 | Daimler Ag | Cylinder bush or cylinder liner made of gray iron- or aluminum alloy for casting in a light metal alloy on the basis of aluminum or aluminum/magnesium, comprises a conditioning coating for casting |
DE102011053858B3 (en) | 2011-09-22 | 2013-03-14 | Preiss Metallwaren Gmbh & Co. Kg | Applying castable component in a lost mold, comprises applying a coating agent at least in sections, on a surface of the component, and applying the component before blowing out the lost mold |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102016104351B4 (en) | 2016-03-10 | 2018-08-23 | Knorr-Bremse Systeme für Nutzfahrzeuge GmbH | Cast iron brake caliper of a disc brake and method of making a caliper |
CN108262466A (en) * | 2017-12-13 | 2018-07-10 | 浙江灿根智能科技有限公司 | A kind of bi-metal casting process |
CN114029450A (en) * | 2021-11-10 | 2022-02-11 | 北京星航机电装备有限公司 | Light alloy casting embedded pipeline assembly and preparation method thereof and casting method of light alloy part with embedded pipeline |
Also Published As
Publication number | Publication date |
---|---|
EP2823916B1 (en) | 2018-12-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE19650613B4 (en) | Component with a metal foam core | |
DE102007023152A1 (en) | Method for producing a casting, casting mold and casting produced therewith | |
DE102017201583A1 (en) | Method for producing a cooling device | |
DE10043748B4 (en) | Cylindrical sputtering target, process for its production and use | |
DE102016114580B4 (en) | METHOD FOR FORMING A TWIN METAL CASTING PIECE | |
EP2823916B1 (en) | Method of manufacturing a composite casting | |
EP3027341B1 (en) | Method of manufacturing a light metal piston using an insert | |
EP2176627B1 (en) | Pipeline or measuring tube having at least one layer which insulates at least in certain regions, and process for the production thereof | |
DE3642978C1 (en) | Method for the production of holes | |
DE112010001446B4 (en) | A method of making a metal matrix composite cylinder liner and method of making the same | |
DE102013015431A1 (en) | Method for producing a cast metallic component and cast metallic component | |
DE102017208000A1 (en) | Method for producing an engine block | |
DE3200641A1 (en) | METHOD AND DEVICE FOR THE CASTING OF A LIGHT METAL PISTON HAVING AN ABRASION-RESISTANT INSERT | |
DE1508993B1 (en) | METHOD OF MANUFACTURING A MULTI-LAYER BODY | |
DE102012104820B4 (en) | Process for the production of composite castings | |
EP3194636B1 (en) | Casting mould and method for producing same | |
DE102004030780A1 (en) | Composite material used in chassis production comprises cast metallic hollow balls and/or cast metal foams made from steel and cast from the same or similar cast material | |
DE102007060502B4 (en) | Method for producing a cylinder crankcase | |
US10105755B2 (en) | Composite casting part | |
EP3687714B1 (en) | Cast component having a cast-in pipe and production method | |
CN105251973B (en) | Compound casting | |
DE2929812C2 (en) | Wheel for automobiles | |
DE102018106725A1 (en) | Process for producing a casting mold for filling melt and casting mold | |
DE102012016739A1 (en) | Producing structural element useful for motor vehicle, comprises producing first component of structural element by casting, and producing second component of structural element by casting first component partially with casting material | |
DE2115910C3 (en) | Composite casting process |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
17P | Request for examination filed |
Effective date: 20130710 |
|
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 |
|
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 |
|
R17P | Request for examination filed (corrected) |
Effective date: 20150708 |
|
RBV | Designated contracting states (corrected) |
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 |
|
17Q | First examination report despatched |
Effective date: 20160511 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
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: 20180515 |
|
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 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: GF CASTING SOLUTIONS LEIPZIG GMBH Owner name: GF CASTING SOLUTIONS HERZOGENBURG IRON GMBH Owner name: GF CASTING SOLUTIONS METTMANN GMBH Owner name: GF CASTING SOLUTIONS SINGEN GMBH Owner name: GF CASTING SOLUTIONS KUNSHAN CO. LTD. |
|
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: 1080720 Country of ref document: AT Kind code of ref document: T Effective date: 20190115 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502013011885 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20181226 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: 20181226 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: 20181226 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: 20190326 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: 20190326 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: 20181226 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20181226 |
|
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: 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: 20181226 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: 20190327 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: 20181226 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20181226 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20181226 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: 20190426 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: 20181226 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: 20181226 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: 20181226 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 502013011885 Country of ref document: DE Owner name: GF CASTING SOLUTIONS LEIPZIG GMBH, DE Free format text: FORMER OWNERS: GF CASTING SOLUTIONS HERZOGENBURG IRON GMBH, HERZOGENBURG, AT; GF CASTING SOLUTIONS KUNSHAN CO. LTD., KUNSHAN CITY, CN; GF CASTING SOLUTIONS LEIPZIG GMBH, 04249 LEIPZIG, DE; GF CASTING SOLUTIONS METTMANN GMBH, 40822 METTMANN, DE; GF CASTING SOLUTIONS SINGEN GMBH, 78224 SINGEN, DE Ref country code: DE Ref legal event code: R081 Ref document number: 502013011885 Country of ref document: DE Owner name: GF CASTING SOLUTIONS KUNSHAN CO. LTD., CN Free format text: FORMER OWNERS: GF CASTING SOLUTIONS HERZOGENBURG IRON GMBH, HERZOGENBURG, AT; GF CASTING SOLUTIONS KUNSHAN CO. LTD., KUNSHAN CITY, CN; GF CASTING SOLUTIONS LEIPZIG GMBH, 04249 LEIPZIG, DE; GF CASTING SOLUTIONS METTMANN GMBH, 40822 METTMANN, DE; GF CASTING SOLUTIONS SINGEN GMBH, 78224 SINGEN, DE |
|
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: 20181226 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: 20190426 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: 20181226 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: 20181226 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: 20181226 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502013011885 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20181226 |
|
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: 20190927 |
|
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: 20181226 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: 20181226 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20190710 |
|
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: 20181226 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20190731 |
|
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: 20190710 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190731 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190731 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190710 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190731 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190731 |
|
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: 20190710 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 1080720 Country of ref document: AT Kind code of ref document: T Effective date: 20190710 |
|
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: 20190710 |
|
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: 20181226 |
|
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: 20130710 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: 20181226 |
|
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: 20181226 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230529 |
|
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: 11 Ref country code: DE Payment date: 20230719 Year of fee payment: 11 |