EP3401037B1 - Mold for producing a casting core - Google Patents
Mold for producing a casting core Download PDFInfo
- Publication number
- EP3401037B1 EP3401037B1 EP18171173.0A EP18171173A EP3401037B1 EP 3401037 B1 EP3401037 B1 EP 3401037B1 EP 18171173 A EP18171173 A EP 18171173A EP 3401037 B1 EP3401037 B1 EP 3401037B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- mould
- shell
- guides
- shells
- guide
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000005266 casting Methods 0.000 title claims description 32
- 239000011162 core material Substances 0.000 claims description 46
- 239000002826 coolant Substances 0.000 claims description 28
- 230000007246 mechanism Effects 0.000 claims description 20
- 238000001816 cooling Methods 0.000 claims description 12
- 238000005516 engineering process Methods 0.000 claims description 3
- 238000000465 moulding Methods 0.000 description 8
- 239000000969 carrier Substances 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 4
- 239000004576 sand Substances 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 241001136792 Alle Species 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 1
- 239000012809 cooling fluid Substances 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C17/00—Moulding machines characterised by the mechanism for separating the pattern from the mould or for turning over the flask or the pattern plate
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C13/00—Moulding machines for making moulds or cores of particular shapes
- B22C13/12—Moulding machines for making moulds or cores of particular shapes for cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C7/00—Patterns; Manufacture thereof so far as not provided for in other classes
- B22C7/06—Core boxes
Definitions
- the invention relates to a mold for producing a casting core, which maps coolant channels and coolant inflows and outflows of a cooling jacket of an electric motor.
- the production of the cooling jacket in a casting process may be useful.
- this type of production requires a suitable casting core, which must be placed within the casting mold in order to map the coolant channels and also the necessary coolant inflows and outflows in terms of casting technology.
- the casting core required for this is also designed to be relatively complex.
- the JP 2015 044217 A discloses a mold for producing a casting core with a core mold space that can be filled with core material. Eight molded shells can be moved between a radially outer position with a closed outer circular shape and an inwardly displaced position. For this purpose, the first four molded shells, in each case two of the four molded shells lying opposite each other, and subsequently the remaining four second molded shells each arranged between the first molded shells, wherein two of the four molded shells also lying opposite each other, are displaced radially inward into the gap which arises. A respective demolding technique with guides, which are fastened to the mold shells, is provided for demolding the casting core. Other forms for producing a casting core are from the US 2008/0274289 A1 as well as the JP H07 266000 A known.
- the aim is therefore to enable the molding of a casting core, which maps the coolant channels and coolant inflows and outflows of the cooling jacket of an electric motor, and which can be removed from the mold easily and non-destructively after molding.
- Such a cooling jacket typically has coolant channels shaped in a meandering manner in its interior, which combine to form an essentially cylindrical shape.
- the core mold space filled with core material during the production of the casting core is primarily determined by an outer shape and an inner shape.
- the outer shape forms the outer wall of the core molding space
- the inner shape forms the inner wall of the core molding space.
- the cylindrical inner shape is enclosed over its entire circumference by the cylindrical outer shape.
- Components of the inner mold are two first mold shells and two second mold shells, with all four mold shells jointly shaping and delimiting the inner wall of the core mold space, and wherein the second mold shells are each movably arranged between the first mold shells.
- Part of the inner mold is a first demolding mechanism, which is arranged between the first mold shells and designed to move them towards one another. Also part of the inner mold is a second demolding mechanism, which is arranged between the second mold shells and is designed to move these second mold shells toward one another.
- this one in the direction the central axis comprises longitudinally movably arranged shell supports with two guides arranged thereon, the one of the first and the other of the two first molded shells being displaceably mounted on one guide, and the longitudinal directions of these two guides converge to one another. Converging means that the virtual axes of the two longitudinal directions meet at a point outside the shell carrier.
- the second demoulding mechanism it is proposed that it comprise a shell support arranged to be longitudinally movable in the direction of the central axis, with two guides arranged thereon, the one of the two and the other of the two second shell shells being displaceably mounted on one guide, and wherein the longitudinal directions of these two guides converge to one another. Converging means that the virtual axes of the two longitudinal directions meet at a point outside the shell carrier.
- the two shell supports are longitudinally movable in the direction of the central axis, for. B. by the one shell carrier is slidably disposed in the other shell carrier.
- the guides on one shell carrier and the guides on the other shell carrier are each aligned such that they converge in the same direction or both diverge in the opposite direction.
- stops are formed on the shell supports, which limit the mutual longitudinal mobility of the shell carriers at least in the opposite direction to the convergence of the guides.
- one of the shell carriers including the guides arranged on them is formed in one piece, whereas the other shell carrier including the guides arranged on it is made of two parts in the direction of the central axis formed one behind the other carrier sections.
- the division of the guide arranged on the other shell carrier is such that guide sections are present on each of the carrier sections, the guide sections being aligned with one another.
- the one-piece shell support is preferably divided into two segments by a longitudinal slot, and the segments are connected to one another only by means of webs.
- one of the shell carriers has a frustoconical basic shape
- the other shell carrier has a basic shape comprising a cylinder and arms projecting radially from the cylinder.
- the cylinder is longitudinally guided in the other, ie the frustoconical shell support. This contributes to a nested and thus compact structure of the two mechanisms, which pull the mold shell pairs back during demolding.
- the guides have a T-shaped cross section and they engage in grooves provided with corresponding undercuts on the inner sides of the respective shaped shells.
- the mutually facing inner sides of the first mold shells forming the first pair of mold shells successively each have an end section, a middle section and a further end section, and that the inner sides spring back on the middle section in comparison to the two end sections to form a recess.
- Fig. 1 a casting core 1 made of casting sand.
- the casting core 1 is used to cast coolant channels 2, a coolant inflow 3 and a coolant outflow 4 of a cooling jacket of an electric motor. If the casting core 1 is therefore placed within a casting mold, it defines those areas where the coolant channels 2, the coolant inflow 3 and the coolant outflow 4 are located after the casting has been completed.
- Fig. 2 the form designed according to the invention is reproduced in its entirety. It consists of an outer shape 9 and an inner shape 10, both of which are arranged around a central axis A.
- the core mold space whose shape in Fig. 1 is reproduced on the basis of the object produced (casting core), is accordingly also essentially cylindrical.
- the outer wall of the core mold space is formed by the outer mold 9, and the inner wall of the core mold space by the inner mold 10.
- the core material for. B. pouring a pouring sand into the core mold space, in which the pouring sand then solidifies to the pouring core.
- the outer shape 9 is composed of a total of four segments, of which each segment extends approximately over a quarter circle. During the demolding, the four segments are moved radially outward, with the result that the cast core 1 produced is then exposed on its outside.
- the internal mold 10 on the other hand, cannot be removed from the mold by a simple radial movement of individual segments, since these would collide with one another when they moved inwards towards the longitudinal axis A.
- Fig. 4 also part of the inner mold 10 four segments, which add up to a cylinder and form the inner wall of the core mold space on their outer sides.
- the four segments are not of uniform size and shape. Instead, two segments are designed as first molded shells 11 and two further segments as second molded shells 13. All four molded shells 11, 13 jointly delimit the inner wall of the core molding space, the second molded shells 13 each being arranged between the first molded shells 11. Since the second molded shells 13 are each arranged between the first molded shells 11, the two second molded shells 13 can be moved inwards towards the central axis A of the inner mold 10 without abutting the two first molded shells 11.
- Fig. 4 and Fig. 4a the consequence of this different design is shown on the one hand of the molded shells 11 and on the other hand of the molded shells 13: the two second molded shells 13 have been moved radially inwards here, but are still located between the first molded shells 11. At the same time, the first molded shells 11 are located where in according to the operating position Fig. 4 the circumferential edges of the second molded shells 13 are each provided with a recess 17.
- Fig. 4a The recesses 17 in the first molded shells 11 are achieved in that the mutually facing inner sides of the two first molded shells 11 each have an end section 18a, a middle section 19 and a further end section 18b in succession.
- the inner sides of the first molded shells 11 spring back on the middle section 19 in comparison to the two end sections 18a, 18b, each forming the recess 17.
- Fig. 4a additionally illustrated by the fact that one of the two second molded shells 13 is also sketched in dashed lines.
- the Figures 4 and 10 which represent the mold shell pairs 11, 13 each in the operating position of maximum demolding, which recognize the different circumferential size of the mold shells 11 on the one hand and the mold shells 13 on the other hand.
- the first molded shells 11 each extend over a larger circumferential angle than the second molded shells 13.
- the first molded shells 11 can each extend over a circumferential angle of 100 °, while the second molded shells 13 each only over a circumferential angle of 80 °.
- Components of the inner mold 10 are also two demolding mechanisms by means of which the mold shells 11, 13 can be moved in the direction of the central axis A.
- a first demolding mechanism is arranged between the first mold shells 11 and designed to move these first mold shells 11 towards one another.
- a second demolding mechanism is arranged between the second mold shells 13 and designed to move the second mold shells 13 towards one another.
- the first shell support 20 has a basic shape composed of a central cylinder 21 and four arms 22 projecting radially therefrom.
- the cylinder 21 is of such a size that it can slide essentially without play in a cylindrical opening 24 with which the second shell support 30 is provided.
- Guides 25A, 25B are formed on the outer ends of the four arms 22.
- the guides 25A, 25B are each of a T-shaped cross section and designed to be in undercut grooves 26 slide on the inner sides of the first molded shells 11 without play.
- the first shell support 20 is formed in two parts from two support sections 20A, 20B arranged one behind the other in the direction of the axis A.
- the carrier section 20A includes the cylinder 21 and the two radially projecting arms on which the two guide sections 25A are located.
- the other, comparably shorter support section 20B comprises the other two arms 22, at the ends of which the two guide sections 25B are formed.
- the design of the first shell carrier 20 is such that the guide sections 25A and 25B arranged on the same side of the axis A are aligned with one another and therefore together form a guide 25 which is interrupted in a central section.
- the guide 25 composed of the guide portions 25A and 25B on one side of the axis A, and the guide 25 composed of the guide portions 25A and 25B on the other side of the axis A are inclined to the axis A, respectively, and they converge toward each other as in Fig. 5 the dashed line representing the direction of the guide 25 illustrates.
- the in Fig. 6 reproduced second shell support 30 has a frustoconical basic shape. On its sides opposite one another with respect to the central axis A, guides 35 of T-shaped cross section are formed in each case, which engage in grooves 36 on the second molded shells 13 in a slidable manner. For this purpose, the grooves 36 on the second molded shells 13 are provided with corresponding undercuts.
- the frustoconical shell carrier 30 has the cylindrical opening 24 in the center, in which the cylinder 21 of the other shell carrier 20 is mounted so as to be longitudinally movable.
- the shell support 30 is formed in one piece and is divided by a longitudinal slot 38, which provides space for the arms 22, into two essentially semi-conical segments, these segments being connected to one another only via two webs 39.
- a longitudinal slot 38 At the end of each longitudinal slot 38 there is a stop 37.
- the corresponding counter stop 27 is located on the two longer arms 22 of the first shell carrier 20.
- FIGS. 9a and 9b illustrate the operation of the two demolding mechanisms in two different operating positions: In the operating position according to Fig. 9a is moved inward by a longitudinal movement of the second shell support 30 in the direction of the central axis A, each of the two second molded shells 13. The first two molded shells 11 do not yet perform an inward movement at this time.
- the demolding takes place in two stages (first the second molded shells 13, then only the first molded shells 11), but by means of a single, preferably continuously, drive movement.
- This drive movement is achieved by a continuous longitudinal movement of the second shell carrier 30, which automatically takes along the first shell carrier 20 after a certain longitudinal path.
- Materials for the inner mold 10 can be plastic, metal or wood.
- Suitable as the core material of the casting core 1 are sand or free-flowing oxidic substances or mixtures of substances which contain inorganic or organic binders, these substances or mixtures of substances hardening either thermally and / or chemically.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Description
Die Erfindung betrifft eine Form zum Herstellen eines Gießkerns, welcher Kühlmittelkanäle sowie Kühlmittelzu- und -abflüsse eines Kühlmantels eines Elektromotors gießtechnisch abbildet.The invention relates to a mold for producing a casting core, which maps coolant channels and coolant inflows and outflows of a cooling jacket of an electric motor.
Die Effizienz moderner Elektromotoren und vor allem von Elektromotoren, die dem Fahrantrieb von Fahrzeugen dienen, hängt stark von der Kühlung des Elektromotors ab. Häufig sind derartige Elektromotoren daher mit einem Kühlmantel mit darin verlaufenden Kühlmittelkanälen versehen, die von einem Kühlfluid, z. B. Wasser, durchströmt werden.The efficiency of modern electric motors, and especially of electric motors that serve to drive vehicles, depends heavily on the cooling of the electric motor. Often, such electric motors are therefore provided with a cooling jacket with coolant channels running therein, which from a cooling fluid, for. B. water.
Wegen der Komplexität der Form der Kühlmittelkanäle, die z. B. mäanderförmig sein können, kann die Herstellung des Kühlmantels in einem Gießverfahren sinnvoll sein. Diese Art der Herstellung setzt allerdings einen geeigneten Gießkern voraus, der innerhalb der Gießform platziert werden muss, um die Kühlmittelkanäle und ferner die notwendigen Kühlmittelzu- und -abflüsse gießtechnisch abzubilden. Entsprechend der Komplexität der Kühlmittelkanäle ist auch der hierfür erforderliche Gießkern relativ komplex gestaltet.Because of the complexity of the shape of the coolant channels, the z. B. may be meandering, the production of the cooling jacket in a casting process may be useful. However, this type of production requires a suitable casting core, which must be placed within the casting mold in order to map the coolant channels and also the necessary coolant inflows and outflows in terms of casting technology. Depending on the complexity of the coolant channels, the casting core required for this is also designed to be relatively complex.
Die
Ziel ist es daher, das Formen eines Gießkerns zu ermöglichen, der die Kühlmittelkanäle sowie Kühlmittelzu- und -abflüsse des Kühlmantels eines Elektromotors gießtechnisch abbildet, und der nach dem Formen gut und zerstörungsfrei entformbar ist.The aim is therefore to enable the molding of a casting core, which maps the coolant channels and coolant inflows and outflows of the cooling jacket of an electric motor, and which can be removed from the mold easily and non-destructively after molding.
Vorgeschlagen wird daher eine Form zum Herstellen eines Gießkerns, welcher Kühlmittelkanäle sowie Kühlmittelzu- und -abflüsse eines Kühlmantels eines Elektromotors gießtechnisch abbildet, mit einem mit Kernmaterial verfüllbaren Kernformraum, der um eine zentrale Achse herum im Wesentlichen zylindrisch gestaltet ist. Die Außenwand des Kernformraums wird durch eine Außenform, und die Innenwand durch eine von der Außenform vollumfänglich umschlossene Innenform gebildet. Bestandteile der Innenform sind:
- zwei erste Formschalen und zwei zweite Formschalen, die alle vier gemeinsam die Innenwand des Kernformraums begrenzen, wobei die zweiten Formschalen jeweils zwischen den ersten Formschalen angeordnet sind,
- ein erster Entformmechanismus, welcher zwischen den ersten Formschalen angeordnet und dazu ausgebildet ist, diese aufeinander zu zu bewegen, wobei die erste Entformmechanik einen in Richtung der Achse längsbeweglich angeordneten Schalenträger mit zwei daran angeordneten Führungen umfasst, wobei auf der einen Führung die eine, und auf der anderen Führung die andere der beiden ersten Formschalen verschieblich gelagert ist, und wobei die Längsrichtungen der zwei Führungen zueinander konvergieren,
- ein zweiter Entformmechanismus, welcher zwischen den zweiten Formschalen angeordnet und dazu ausgebildet ist, diese aufeinander zu zu bewegen, wobei die zweite Entformmechanik einen in Richtung der Achse längsbeweglich angeordneten Schalenträger mit zwei daran angeordneten Führungen umfasst, wobei auf der einen Führung die eine, und auf der anderen Führung die andere der beiden zweiten Formschalen verschieblich gelagert ist, und wobei die Längsrichtungen der zwei Führungen zueinander konvergieren,
- two first molded shells and two second molded shells, all of which together delimit the inner wall of the core molding space, the second molded shells each being arranged between the first molded shells,
- a first demoulding mechanism which is arranged between the first mold shells and is designed to move them towards one another, the first demoulding mechanism comprising a shell carrier which is arranged to be longitudinally movable in the direction of the axis and has two guides arranged thereon, the one, and on the one guide the other guide, the other of the first two molded shells is slidably mounted, and the longitudinal directions of the two guides converge towards one another,
- a second demoulding mechanism, which is arranged between the second mold shells and is designed to move them towards one another, the second demoulding mechanism comprising a shell carrier which is arranged to be longitudinally movable in the direction of the axis and has two guides arranged thereon, the one and the one guide the other guide, the other of the two second molded shells is displaceably mounted, and the longitudinal directions of the two guides converge towards one another,
Mit einer solchen Form lassen sich komplex gestaltete, zylindrische Gießkerne herstellen, welche Kühlmittelkanäle sowie Kühlmittelzu- und -abflüsse des Kühlmantels eines Elektromotors gießtechnisch abbilden können. Ein solcher Kühlmantel verfügt in seinem Inneren typischerweise über mäanderartig geformte Kühlmittelkanäle, die sich insgesamt zu einer im Wesentlichen zylindrischen Gestalt verbinden. Entsprechend wird der beim Herstellen des Gießkerns mit Kernmaterial verfüllte Kernformraum primär durch eine Außenform und eine Innenform bestimmt. Dabei bildet die Außenform die Außenwand des Kernformraums, und die Innenform bildet die Innenwand des Kernformraums. Die zylindrische Innenform ist über ihren gesamten Umfang von der zylindrischen Außenform umschlossen ist.With such a shape, complexly designed, cylindrical casting cores can be produced, which can map the coolant channels and coolant inflows and outflows of the cooling jacket of an electric motor. Such a cooling jacket typically has coolant channels shaped in a meandering manner in its interior, which combine to form an essentially cylindrical shape. Accordingly, the core mold space filled with core material during the production of the casting core is primarily determined by an outer shape and an inner shape. The outer shape forms the outer wall of the core molding space, and the inner shape forms the inner wall of the core molding space. The cylindrical inner shape is enclosed over its entire circumference by the cylindrical outer shape.
Bestandteile der Innenform sind zwei erste Formschalen und zwei zweite Formschalen, wobei alle vier Formschalen gemeinsam die Innenwand des Kernformraums gestalten und begrenzen, und wobei die zweiten Formschalen jeweils beweglich zwischen den ersten Formschalen angeordnet sind.Components of the inner mold are two first mold shells and two second mold shells, with all four mold shells jointly shaping and delimiting the inner wall of the core mold space, and wherein the second mold shells are each movably arranged between the first mold shells.
Bestandteil der Innenform ist ein erster Entformmechanismus, welcher zwischen den ersten Formschalen angeordnet und dazu ausgebildet ist, diese aufeinander zu zu bewegen. Bestandteil der Innenform ist außerdem ein zweiter Entformmechanismus, welcher zwischen den zweiten Formschalen angeordnet und dazu ausgebildet ist, diese zweiten Formschalen aufeinander zu zu bewegen.Part of the inner mold is a first demolding mechanism, which is arranged between the first mold shells and designed to move them towards one another. Also part of the inner mold is a second demolding mechanism, which is arranged between the second mold shells and is designed to move these second mold shells toward one another.
Es ist also eine durch die beiden Entformmechaniken erzielte Bewegung nach innen zur Längsachse der Innenform hin, durch welche bei der Entformung der Kernformraum geöffnet bzw. freigegeben wird.It is therefore a movement inward towards the longitudinal axis of the inner mold achieved by the two demolding mechanisms, by means of which the core mold space is opened or released during the demolding.
Hinsichtlich der ersten Entformmechanik wird vorgeschlagen, dass diese einen in Richtung der zentralen Achse längsbeweglich angeordneten Schalenträger mit zwei daran angeordneten Führungen umfasst, wobei auf der einen Führung die eine, und auf der anderen Führung die andere der beiden ersten Formschalen verschieblich gelagert ist, und wobei die Längsrichtungen dieser zwei Führungen zueinander konvergieren. Konvergieren bedeutet, dass sich die virtuellen Achsen der beiden Längsrichtungen an einem Punkt außerhalb des Schalenträgers treffen.With regard to the first demolding mechanism, it is proposed that this one in the direction the central axis comprises longitudinally movably arranged shell supports with two guides arranged thereon, the one of the first and the other of the two first molded shells being displaceably mounted on one guide, and the longitudinal directions of these two guides converge to one another. Converging means that the virtual axes of the two longitudinal directions meet at a point outside the shell carrier.
Hinsichtlich der zweiten Entformmechanik wird vorgeschlagen, dass diese einen in Richtung der zentralen Achse längsbeweglich angeordneten Schalenträger mit zwei daran angeordneten Führungen umfasst, wobei auf der einen Führung die eine, und auf der anderen Führung die andere der beiden zweiten Formschalen verschieblich gelagert ist, und wobei die Längsrichtungen dieser zwei Führungen zueinander konvergieren. Konvergieren bedeutet, dass sich die virtuellen Achsen der beiden Längsrichtungen an einem Punkt außerhalb des Schalenträgers treffen.With regard to the second demoulding mechanism, it is proposed that it comprise a shell support arranged to be longitudinally movable in the direction of the central axis, with two guides arranged thereon, the one of the two and the other of the two second shell shells being displaceably mounted on one guide, and wherein the longitudinal directions of these two guides converge to one another. Converging means that the virtual axes of the two longitudinal directions meet at a point outside the shell carrier.
Vorzugsweise sind die beiden Schalenträger in Richtung der zentralen Achse längsbeweglich zueinander, z. B. indem der eine Schalenträger gleitbeweglich in dem anderen Schalenträger angeordnet ist.Preferably, the two shell supports are longitudinally movable in the direction of the central axis, for. B. by the one shell carrier is slidably disposed in the other shell carrier.
Um an der Innenform durch eine einzige, kontinuierliche Antriebsbewegung zu einer vollständigen Entformung zu kommen, sind die Führungen an dem einen Schalenträger sowie die Führungen an dem anderen Schalenträger jeweils so ausgerichtet, dass sie in dieselbe Richtung konvergieren bzw. in die entgegengesetzte Richtung beide divergieren.In order to achieve complete demolding on the inner mold by means of a single, continuous drive movement, the guides on one shell carrier and the guides on the other shell carrier are each aligned such that they converge in the same direction or both diverge in the opposite direction.
Damit sich durch eine einzige, kontinuierliche Antriebsbewegung zunächst nur das Paar erster Formschalen und erst später das Paar zweiter Formschalen nach innen zurückzieht, sind an den Schalenträgern Anschläge ausgebildet, welche die gegenseitige Längsbeweglichkeit der Schalenträger zumindest in die dem Konvergieren der Führungen entgegengesetzte Richtung begrenzen.So that at first only the pair of first molded shells and only later the pair of second molded shells retract inwards through a single, continuous drive movement, stops are formed on the shell supports, which limit the mutual longitudinal mobility of the shell carriers at least in the opposite direction to the convergence of the guides.
Um die beiden Mechanismen, die die Formschalenpaare für das Entformen zurückziehen, kompakt und platzsparend ineinander bauen zu können, ist einer der Schalenträger einschließlich der an ihm angeordneten Führungen einteilig ausgebildet, hingegen der andere Schalenträger einschließlich der an ihm angeordneten Führungen zweiteilig aus zwei in Richtung der zentralen Achse hintereinander angeordneten Trägerabschnitten ausgebildet. In diesem Fall ist die Aufteilung der an dem anderen Schalenträger angeordneten Führung dergestalt, dass Führungsabschnitte an jedem der Trägerabschnitte vorhanden sind, wobei die Führungsabschnitte zueinander fluchten.In order to be able to build the two mechanisms that retract the mold shell pairs for demolding compactly and space-savingly into one another, one of the shell carriers including the guides arranged on them is formed in one piece, whereas the other shell carrier including the guides arranged on it is made of two parts in the direction of the central axis formed one behind the other carrier sections. In this case, the division of the guide arranged on the other shell carrier is such that guide sections are present on each of the carrier sections, the guide sections being aligned with one another.
Vorzugsweise ist der einteilig ausgebildete Schalenträger durch einen Längsschlitz in zwei Segmente aufgeteilt, und die Segmente sind nur über Stege miteinander verbunden.The one-piece shell support is preferably divided into two segments by a longitudinal slot, and the segments are connected to one another only by means of webs.
Gemäß einer weiteren Ausgestaltung der Form weist einer der Schalenträger eine kegelstumpfförmige Grundform auf, und der andere Schalenträger eine Grundform aus einem Zylinder und radial von dem Zylinder abstehenden Armen. Der Zylinder ist in dem anderen, also dem kegelstumpfförmigen Schalenträger längsgeführt. Dies trägt zu einem ineinander geschachtelten und damit kompakten Aufbau der zwei Mechaniken bei, die die Formschalenpaare beim Entformen zurückziehen.According to a further embodiment of the shape, one of the shell carriers has a frustoconical basic shape, and the other shell carrier has a basic shape comprising a cylinder and arms projecting radially from the cylinder. The cylinder is longitudinally guided in the other, ie the frustoconical shell support. This contributes to a nested and thus compact structure of the two mechanisms, which pull the mold shell pairs back during demolding.
Gemäß einer weiteren Ausgestaltung der Form sind die Führungen von T-förmigem Querschnitt, und sie greifen in mit entsprechenden Hinterschnitten versehene Nuten an den Innenseiten der jeweiligen Formschalen ein.According to a further embodiment of the form, the guides have a T-shaped cross section and they engage in grooves provided with corresponding undercuts on the inner sides of the respective shaped shells.
Schließlich wird vorgeschlagen, dass die einander zugewandten Innenseiten der das erste Formschalenpaar bildenden ersten Formschalen aufeinanderfolgend jeweils einen Endabschnitt, einen Mittelabschnitt und einen weiteren Endabschnitt aufweisen, und dass die Innenseiten auf dem Mittelabschnitt im Vergleich zu den beiden Endabschnitten unter Ausbildung einer Ausnehmung zurückspringen.Finally, it is proposed that the mutually facing inner sides of the first mold shells forming the first pair of mold shells successively each have an end section, a middle section and a further end section, and that the inner sides spring back on the middle section in comparison to the two end sections to form a recess.
Weitere Einzelheiten und Vorteile erschließen sich aus der nachfolgenden Beschreibung einer Form zum Herstellen eines Gießkerns. Dazu wird auf die Zeichnungen Bezug genommen. Darin zeigen
- Fig. 1
- in perspektivischer Darstellung nur das mittels der hier beschriebenen Form herstellbare Produkt, nämlich ein Gießkern, der Kühlmittelkanäle sowie Kühlmittelzu- und -abflüsse des Kühlmantels eines Elektromotors gießtechnisch abbildet;
- Fig. 2
- in perspektivischer Darstellung die komplette Form zum Herstellen des in
Fig. 1 illustrierten Gießkerns; - Fig. 3
- ebenfalls die Form, jedoch im Vergleich zu
Fig. 2 ohne die Bestandteile der Außenform; - Fig. 4
- eine Stirnansicht auf die Formschalenpaare der Innenform, und zwar in der Betriebsstellung maximaler Entformung;
- Fig. 4a
- den Bereich IV der
Fig. 4 in einer vergrößerten Darstellung; - Fig. 5
- in perspektivischer Einzeldarstellung nur einen ersten Schalenträger der Innenform;
- Fig. 6
- in perspektivischer Einzeldarstellung nur einen zweiten Schalenträger der Innenform;
- Fig. 7
- die beiden ineinandergesetzten Schalenträger, und zwar in der Formstellung;
- Fig. 8
- im rechten Bildteil die beiden ineinandergesetzten Schalenträger in der Betriebsstellung maximaler Entformung;
- Fig. 9a
- die Form in einer Betriebsstellung, in der nur die beiden zweiten Formschalen entformt sind;
- Fig. 9b
- dieselben Gegenstände in einer fortgeschrittenen Betriebsstellung, in der auch die beiden ersten Formschalen entformt sind, und
- Fig. 10
- eine Stirnansicht auf alle Formschalen in der Betriebsstellung nach
Fig. 9b .
- Fig. 1
- in a perspective view, only the product that can be produced by means of the mold described here, namely a casting core, which depicts coolant channels and coolant inflows and outflows of the cooling jacket of an electric motor in terms of casting technology;
- Fig. 2
- in perspective the complete form for producing the in
Fig. 1 illustrated casting core; - Fig. 3
- also the shape, but compared to
Fig. 2 without the components of the outer shape; - Fig. 4
- an end view of the mold shell pairs of the inner mold, in the operating position of maximum demolding;
- Fig. 4a
- the area IV of the
Fig. 4 in an enlarged view; - Fig. 5
- in perspective individual representation only a first shell support of the inner shape;
- Fig. 6
- in perspective individual representation only a second shell support of the inner shape;
- Fig. 7
- the two nested shell supports, in the form position;
- Fig. 8
- in the right part of the picture the two nesting shell supports in the operating position of maximum demolding;
- Fig. 9a
- the mold in an operating position in which only the two second mold shells are removed;
- Fig. 9b
- the same objects in an advanced operating position, in which the first two molded shells are removed, and
- Fig. 10
- an end view of all molded shells in the operating position
Fig. 9b ,
In
Wegen der Komplexität der Form der Kühlmittelkanäle 2, die gemäß
Im Folgenden vorgeschlagen wird eine Form, mit der sich der Gießkern 1 herstellen lässt, wobei vor allem eine gute und zerstörungsfreie Entformung angestrebt ist.In the following, a form is proposed with which the
In
Gemäß
Das Entformen der Innenform 10 hingegen ist nicht durch eine einfache radiale Bewegung einzelner Segmente durchführbar, da diese bei ihrer Bewegung nach innen zu der Längsachse A hin miteinander kollidieren würden.The
Zwar sind gemäß
In
Gemäß
Ferner lassen die
Bestandteile der Innenform 10 sind außerdem zwei Entformmechaniken, durch welche sich die Formschalen 11, 13 in Richtung zu der zentralen Achse A hin bewegen lassen. Eine erste Entformmechanik ist zwischen den ersten Formschalen 11 angeordnet und dazu ausgebildet, diese ersten Formschalen 11 aufeinander zu zu bewegen. Analog ist eine zweite Entformmechanik zwischen den zweiten Formschalen 13 angeordnet und dazu ausgebildet, die zweiten Formschalen 13 aufeinander zu zu bewegen.Components of the
In beiden Fällen ist der Mechanismus eine Schrägführung der zwei Formschalen an einem Schalenträger. Insgesamt sind zwei Schalenträger vorhanden.
Der erste Schalenträger 20 weist eine aus einem zentralen Zylinder 21 und vier davon radial abstehenden Armen 22 zusammengesetzte Grundform auf. Der Zylinder 21 ist von solcher Größe, dass er im Wesentlichen spielfrei in einer zylindrischen Öffnung 24, mit der der zweite Schalenträger 30 versehen ist, gleiten kann.The
An den äußeren Enden der vier Arme 22 sind Führungen 25A, 25B angeformt. Die Führungen 25A, 25B sind jeweils von T-förmigem Querschnitt und so gestaltet, dass sie in hinterschnitten gestalteten Nuten 26 an den Innenseiten der ersten Formschalen 11 spielfrei gleiten.
Damit die beiden Schalenträger 20, 30, wie in
Die Gestaltung des ersten Schalenträgers 20 ist dergestalt, dass die auf derselben Seite der Achse A angeordneten Führungsabschnitte 25A und 25B zueinander fluchten, und daher gemeinsam eine in einem Mittelabschnitt unterbrochene Führung 25 bilden. Die auf der einen Seite der Achse A aus den Führungsabschnitten 25A und 25B zusammengesetzte Führung 25, und die auf der anderen Seite der Achse A aus den Führungsabschnitten 25A und 25B zusammengesetzte Führung 25 verlaufen jeweils schräg zu der Achse A, und sie konvergieren zueinander, wie in
Der in
Der kegelstumpfförmige Schalenträger 30 weist zentral die zylindrische Öffnung 24 auf, in welcher der Zylinder 21 des anderen Schalenträgers 20 längsbeweglich gelagert ist.The
Der Schalenträger 30 ist einstückig ausgebildet und ist durch einen den Armen 22 Platz bietenden Längsschlitz 38 in zwei im Wesentlichen halbkegelförmige Segmente unterteilt, wobei diese Segmente nur über zwei Stege 39 miteinander verbunden sind. Am Ende jedes Längsschlitzes 38 befindet sich ein Anschlag 37. Der entsprechende Gegenanschlag 27 befindet sich an den beiden längeren Armen 22 des ersten Schalenträgers 20. Die an dem Schalenträger 30 ausgebildeten Anschläge 37 begrenzen zusammen mit den an dem Schalenträger 20 ausgebildeten Anschlägen 27 die gegenseitige Längsbeweglichkeit der Schalenträger 30, 20 in die dem Konvergieren der Führungen 35, 25 entgegengesetzte Richtung.The
Die
In der Betriebsstellung gemäß
In the operating position according to
In der Betriebsstellung nach
Insgesamt erfolgt also die Entformung in zwei Stufen (zunächst die zweiten Formschalen 13, dann erst die ersten Formschalen 11), jedoch mittels einer einzigen, vorzugsweise kontinuierlich durchgeführten Antriebsbewegung. Diese Antriebsbewegung wird durch eine kontinuierliche Längsbewegung des zweiten Schalenträgers 30 erreicht, der nach einem gewissen Längsweg automatisch den ersten Schalenträger 20 mitnimmt.All in all, the demolding takes place in two stages (first the second molded
Materialien für die Innenform 10 können Kunststoff, Metall oder Holz sein.Materials for the
Als Kernmaterial des Gießkerns 1 geeignet sind Sand oder rieselfähige oxydische Stoffe oder Stoffgemische, die anorganische oder organische Bindemittel enthalten, wobei diese Stoffe oder Stoffgemische entweder thermisch und / oder chemisch aushärten.Suitable as the core material of the
- 11
- Gießkerncasting core
- 22
- KühlmittelkanalCoolant channel
- 33
- Kühlmittelzuflusscoolant supply
- 44
- KühlmittelabflussCoolant outflow
- 99
- Außenformexternal form
- 1010
- Innenforminterior shape
- 1111
- erste Formschalefirst molded shell
- 1313
- zweite Formschalesecond molded shell
- 1717
- Ausnehmungrecess
- 18a18a
- Endabschnittend
- 18b18b
- Endabschnittend
- 1919
- Mittelabschnittmidsection
- 2020
- erster Schalenträgerfirst shell carrier
- 20A20A
- Trägerabschnittsupport section
- 20B20B
- Trägerabschnittsupport section
- 2121
- Zylindercylinder
- 2222
- Armpoor
- 2424
- Öffnungopening
- 2525
- Führungguide
- 25A25A
- Führungsabschnittguide section
- 25B25B
- Führungsabschnittguide section
- 2626
- Nutgroove
- 2727
- Anschlagattack
- 3030
- zweiter Schalenträgersecond shell support
- 3535
- Führungguide
- 3636
- Nutgroove
- 3737
- Anschlagattack
- 3838
- Längsschlitzlongitudinal slot
- 3939
- Stegweb
- AA
- zentrale Achse, Längsachsecentral axis, longitudinal axis
Claims (9)
- Mould for producing a casting core (1), which illustrates coolant channels (2) as well as coolant inflows and outflows (3, 4) of a cooling jacket of an electric motor using casting technology, with a core box space to be filled with core material, which is designed substantially cylindrically around a central axis (A), and the external wall of which is formed by an external mould (9) and its internal wall by an internal mould (10) completely enclosed by the external mould, wherein components of the internal mould (10) are:- two first mould shells (11) and two second mould shells (13), all four of which together delimit the internal wall of the core box space, wherein the second mould shells (13) are each arranged between the first mould shells (11),- a first demoulding mechanism, which is arranged between the first mould shells (11) and is formed for moving these towards each other, wherein the first demoulding mechanism comprises a shell support (20) that is longitudinally moveable in the direction of the axis (A), with two guides (25) arranged on the same, wherein one of these is displaceably mounted in one guide, and the other one of the two first mould shells (11) on the other guide, and wherein the longitudinal directions of the two guides (25) converge towards each other,- a second demoulding mechanism, which is arranged between the second mould shells (13) and is formed for moving these towards each other, wherein the second demoulding mechanism comprises a shell support (30) that is longitudinally moveable in the direction of the axis (A), with two guides (35) arranged on the same, wherein one of these is displaceably mounted in one guide, and the other one of the two second mould shells (13) on the other guide, and wherein the longitudinal directions of the two guides (35) converge towards each other,wherein one of the shell supports (30) including the guides (35) arranged on the same is a one-piece design and the other shell support (20) including the guides (25) arranged on the same is a two-piece design consisting of two support sections (20A, 20B) arranged one behind the other in the direction of axis (A).
- Mould according to claim 1, characterised in that the two shell supports (20, 30) are designed to be longitudinally moveable towards each other in the direction of axis (A).
- Mould according to claim 2, characterised in that the guides (35) on the shell support (30) and the guides (25) on the other shell support (20) converge in the same direction.
- Mould according to claim 2 or 3, characterised by shoulders (37, 27) formed on the shell supports (30, 20), which delimit the reciprocal longitudinal movability of the shell supports (30, 20) at least in the direction opposite the converging of the guides (35, 25).
- Mould according to claim 1, characterised by a division of the guide (25) arranged on the other shell support (20) in such a way that guide sections (25A, 25B) are present on each of the support sections (20A, 20B), wherein the guide sections (25A) of one support section are flush with the guide sections (25B) of the other support section.
- Mould according to claim 1 or 5, characterised in that the one-piece design shell support (30) is divided into two segments by a longitudinal slot (38), and in that the segments are connected to each other only via bridges (39).
- Mould according to one of the claims 2-6, characterised in that one of the shell supports (30) has a frustoconical base shape, that the other shell support (20) has a base shape composed of a cylinder and arms radially projecting from the same, and that the cylinder is longitudinally held in the frustoconical shell support (30).
- Mould according to one of the claims 2-7, characterised in that the guides (35, 25) have a T-shaped cross-section and engage with grooves (36, 26) of an undercut design on the insides of the respective mould shells (13 or 11).
- Mould according to one of the preceding claims, characterised in that the internal sides of the two first mould shells (11) facing each other successively have one end section (18a), one middle section (19) and one further end section (18b) each, and that the internal sides recede back to the middle section (19) compared to the two end sections (18a, 18b) whilst forming a recess (17).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102017109921.2A DE102017109921A1 (en) | 2017-05-09 | 2017-05-09 | Mold for producing a casting core |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3401037A1 EP3401037A1 (en) | 2018-11-14 |
EP3401037B1 true EP3401037B1 (en) | 2020-01-22 |
Family
ID=62142971
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP18171173.0A Active EP3401037B1 (en) | 2017-05-09 | 2018-05-08 | Mold for producing a casting core |
Country Status (4)
Country | Link |
---|---|
US (1) | US10384261B2 (en) |
EP (1) | EP3401037B1 (en) |
CN (1) | CN108856651A (en) |
DE (1) | DE102017109921A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102017105478A1 (en) * | 2017-03-15 | 2018-09-20 | Nemak, S.A.B. De C.V. | Apparatus for shooting a casting core |
DE102019110580A1 (en) * | 2019-04-24 | 2020-10-29 | Nemak, S.A.B. De C.V. | Device and method for removing at least one cooling element from an at least partially demolded casting, method for introducing at least one cooling element into a mold core of a casting mold, cooling element and casting |
CN110328348B (en) * | 2019-06-27 | 2021-12-31 | 广东银迪压铸有限公司 | Production method of new energy automobile motor aluminum shell |
CN110548856B (en) * | 2019-10-10 | 2021-09-07 | 北京航星机器制造有限公司 | Composite casting mold of aluminum alloy shell casting and forming method thereof |
CN114454308A (en) * | 2022-03-01 | 2022-05-10 | 北京利尔高温材料股份有限公司 | Current regulator slidingtype inner core assembling die |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT328177B (en) | 1973-11-23 | 1976-03-10 | Osterreichische Symalen Ges M | DEVICE FOR MOLDING SLEEVES |
JPH07266000A (en) | 1994-03-28 | 1995-10-17 | Koyama:Kk | Forming mold for core and core |
JP4445335B2 (en) * | 2004-06-21 | 2010-04-07 | 本田技研工業株式会社 | Mold apparatus and cylinder block manufacturing method |
GB0514751D0 (en) * | 2005-07-19 | 2005-08-24 | Holset Engineering Co | Method and apparatus for manufacturing turbine or compressor wheels |
CN201132201Y (en) * | 2007-11-30 | 2008-10-15 | 李春奎 | Combined casting die with metal inner core |
AT511230A1 (en) | 2011-04-15 | 2012-10-15 | Ifw Manfred Otte Gmbh | FORM CORE FOR MOLDING TOOL |
JP2015044217A (en) * | 2013-08-28 | 2015-03-12 | 本田金属技術株式会社 | Core molding device |
DE102014207333A1 (en) * | 2014-04-16 | 2015-10-22 | Mahle International Gmbh | Apparatus for producing a piston |
-
2017
- 2017-05-09 DE DE102017109921.2A patent/DE102017109921A1/en not_active Withdrawn
-
2018
- 2018-05-08 EP EP18171173.0A patent/EP3401037B1/en active Active
- 2018-05-08 US US15/973,857 patent/US10384261B2/en not_active Expired - Fee Related
- 2018-05-09 CN CN201810434458.6A patent/CN108856651A/en active Pending
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
US20180326474A1 (en) | 2018-11-15 |
US10384261B2 (en) | 2019-08-20 |
EP3401037A1 (en) | 2018-11-14 |
DE102017109921A1 (en) | 2018-11-15 |
CN108856651A (en) | 2018-11-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3401037B1 (en) | Mold for producing a casting core | |
DE4126041C2 (en) | Injection mold with rotatable male and female molds that can be combined in different combinations | |
DE69826526T2 (en) | METHOD AND DEVICE FOR FORMING A COMPOSITE OBJECT | |
CH650970A5 (en) | MACHINE FOR THE PRESSURE AND / OR INJECTION MOLDING OF COMPOSITE SHAPES MADE OF TWO MATERIALS. | |
EP2202044B2 (en) | Method for injection moulding of a pump propeller | |
DE3639313A1 (en) | RETURNABLE MOLDING DEVICE | |
DE102019001725B4 (en) | TOOLING FOR INJECTION MOLDING OF PLASTIC PARTS AND METHOD OF MOVING A SLIDE OF A MOLD HALF OF THE TOOL, METHOD OF PIVOTING A SECTION OF A ONE-PIECE PLASTIC MOLDING PRESENT IN AN EJECTOR COMPONENT, AND METHOD OF DESIGNING A MOLDING CAVITY IN ONE MOLD HALF DURING INJECTION MOLDING | |
WO2017215801A1 (en) | Injection moulding tool with adjustable core centring device | |
EP1636473B1 (en) | Piston for a combustion engine and casting method for the production thereof | |
DE3909521A1 (en) | FOAM MOLDING MODEL AND METHOD AND DEVICE FOR ITS PRODUCTION | |
DE2917799C2 (en) | Plastic injection mold or compression mold with a displaceably guided molded part | |
EP3595829B1 (en) | Device for shooting a casting core | |
EP0183278A2 (en) | Process and apparatus for making long plastic pipes by way of injection-moulding | |
DE102005041874A1 (en) | Throttle valve unit manufacturing method for automotive industry, involves filling circular slot between throttle valve blank and support with plastic material, and adjusting slot dimension by predetermined shrinkage of material | |
DE1529776B2 (en) | INJECTION MOLDING DEVICE FOR MANUFACTURING COMPLETE SHOES | |
DE2914363A1 (en) | DEVICE AND METHOD FOR DIE CASTING | |
DE840905C (en) | Injection mold | |
DE19536759C2 (en) | Process for making a pipe | |
EP2489491B1 (en) | Method and device for producing ball bearing rings | |
DE102011015943A1 (en) | Locking device for locking tool clamping plate with column of e.g. injection molding machine, has locking jaws that are switchable between open and closed positions and are connected with each other by link mechanism | |
DE2536142A1 (en) | Handling and injection moulding device - for aluminium squirrel cage has rotary support moving on rails between mould halves | |
DE10224708C1 (en) | Collapsible core for injection molding of plastics, or pressure die casting, has converging control surfaces at its free end to move mold sections to shape a cut-back in the molding with relatively large radial dimensions | |
DE2619066A1 (en) | Expanding core for injection-moulding of articles - with complicated interior or exterior surfaces has segmented sleeve whose components move radially inwards to facilitate removal of moulding | |
EP1254753B1 (en) | Mould for multicomponent injection moulding of plastic objects | |
DE102015220980A1 (en) | Mold with multi-part slide for the production of metallic cast components, thus executable casting method and hereby produced planet carrier |
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 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED |
|
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 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20190430 |
|
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 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R079 Ref document number: 502018000651 Country of ref document: DE Free format text: PREVIOUS MAIN CLASS: B22C0007060000 Ipc: B22C0013120000 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: B22C 9/10 20060101ALI20190703BHEP Ipc: B22C 7/06 20060101ALI20190703BHEP Ipc: B22C 13/12 20060101AFI20190703BHEP Ipc: B22C 17/00 20060101ALI20190703BHEP |
|
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: 20190823 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502018000651 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1226599 Country of ref document: AT Kind code of ref document: T Effective date: 20200215 |
|
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: NL Ref legal event code: MP Effective date: 20200122 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200614 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: 20200422 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: 20200122 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: 20200122 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: 20200122 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200422 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: 20200522 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: 20200122 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: 20200122 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: 20200423 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: 20200122 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502018000651 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200122 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: 20200122 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: 20200122 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: 20200122 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: 20200122 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: 20200122 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: 20200122 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: 20200122 |
|
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 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 502018000651 Country of ref document: DE |
|
26N | No opposition filed |
Effective date: 20201023 |
|
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: 20200122 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: 20200122 |
|
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: 20200122 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: 20200122 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20200531 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200508 |
|
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: 20200508 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200531 |
|
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: 20200531 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201201 |
|
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: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210531 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210531 |
|
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: 20200122 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: 20200122 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: 20200122 |
|
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: 20200122 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: 20200122 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20220508 |
|
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: 20220508 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 1226599 Country of ref document: AT Kind code of ref document: T Effective date: 20230508 |