EP3600718B1 - Casting core and method for the production thereof - Google Patents
Casting core and method for the production thereof Download PDFInfo
- Publication number
- EP3600718B1 EP3600718B1 EP18721843.3A EP18721843A EP3600718B1 EP 3600718 B1 EP3600718 B1 EP 3600718B1 EP 18721843 A EP18721843 A EP 18721843A EP 3600718 B1 EP3600718 B1 EP 3600718B1
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- foundry core
- casting
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- 238000005266 casting Methods 0.000 title description 96
- 238000004519 manufacturing process Methods 0.000 title description 11
- 238000000034 method Methods 0.000 title description 4
- 239000011230 binding agent Substances 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 6
- 239000000654 additive Substances 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 4
- 238000000465 moulding Methods 0.000 claims description 3
- 239000004576 sand Substances 0.000 claims 1
- 239000011162 core material Substances 0.000 description 105
- 239000012778 molding material Substances 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 239000003110 molding sand Substances 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 238000007493 shaping process Methods 0.000 description 3
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 238000013507 mapping Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000012495 reaction gas Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- 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
- B22C9/103—Multipart cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C21/00—Flasks; Accessories therefor
- B22C21/12—Accessories
- B22C21/14—Accessories for reinforcing or securing moulding materials or cores, e.g. gaggers, chaplets, pins, bars
-
- 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
- B22C9/108—Installation of cores
Definitions
- the invention relates to a casting core which has the basic shape of a hollow body, the casting core being formed from a molding material which consists of a mixture formed from a molding sand and a binder and optionally from additives added to adjust its properties.
- Casting cores of the type in question are used for the casting production of cast parts from a metal melt.
- the casting cores form cavities, such as channels or chambers, in the respective cast part. These cavities can be provided to save weight. As a rule, however, a fluid flows through them in practical use.
- the molding material mixture mixed in the manner explained above is introduced (“shot") into the molding cavity of a core-shooting device at high pressure.
- the flowability of the molding material, the shooting pressure and the positions at which the molding material is introduced into the mold cavity of the machine provided for manufacturing the cores are coordinated so that complete mold filling is achieved even with particularly fine-grained cores.
- the cores are solidified by applying heat or gassing with a reaction gas so that they are out removed from the core shooter and inserted into the respective casting mold, where they can withstand the stresses that occur when the molten metal is poured off.
- Typical examples of cast parts in which such channels and cavities are molded using casting cores are housings for drive machines that have to be cooled during operation.
- so-called "cooling jackets” are generally provided, i.e. a system of ducts that surround the area of the machine in which heat is generated during operation as a result of energy conversion.
- cooling jackets are generally provided, i.e. a system of ducts that surround the area of the machine in which heat is generated during operation as a result of energy conversion.
- casting cores of the type in question usually do not form a solid body, but are often perforated, so that their walls form finely divided structures, the islands, in which larger amounts of the Core material are gathered, larger and thicker webs, finely branched webs, larger bridges and other filigree shaped elements.
- Due to the circumferentially closed basic shape of the casting cores, typically circular or ellipsoid in cross-section, with such finely divided casting cores demolding the cores from the core shooting machine is only possible with great effort.
- Complex slide designs and the like must be provided in order to be able to separate the shaping components of the core shooting machine from the finished core despite the large number of undercuts and openings. Apart from the high costs that such a complex machine entails, this effort complicates the large-scale, rapidly clocked series production of casting cores of the type in question.
- a casting core for the manufacture of a turbine blade is known.
- This casting core is formed from a molding material that is mixed, for example, from ceramic particles and a suitable binder.
- the casting core is composed of two subsegments, which have form elements that interact with each other in a form-fitting manner on those edge sides with which they abut, via which the adjacent part segments in two spatial directions, namely a direction normal to the outside of the segments and a transverse direction in the longitudinal direction of the segments aligned direction, are fixed immovably with respect to one another by positive locking.
- a casting core which is composed of subsegments which are formed from a molding material and, when the casting core is assembled, are positively coupled to one another via interlocking projections and recesses formed on them.
- the invention has achieved this object by a casting core which has at least the features specified in claim 1.
- a casting core according to the invention which has the basic shape of a hollow body, the casting core being formed from a molding material which is composed of a mixture, which is formed from a molding sand and a binder and optionally from additives added to adjust its properties, is thus characterized according to the invention in that the casting core is divided into at least two sub-segments and on the edge sides, with which sub-segments arranged adjacent to one another abut, or in the vicinity of these edge sides with each other positively cooperating form elements are provided, by means of which the mutually adjacent part segments are fixed immovably against each other at least in one direction by a form fit.
- a casting core according to the invention is therefore not made in one piece, but rather is composed of two or more subsegments. Since these individual segments themselves no longer define a cavity, they can be produced in the conventional core shooting process with simply designed core tools. Complex slide arrangements, such as those required for mapping hollow bodies, are not required to produce the subsegments. At the same time, the sub-segments formed according to the invention are also comparatively insensitive due to their limited spatial extent if they are designed in a filigree manner with many openings and the like. This allows the subsegments to be stored in an uncomplicated manner and transported for assembling the casting core. The assembly of the casting core according to the invention can be carried out in the course of the assembly of the entire casting mold in which it is to be used or at a point separated therefrom.
- the form-fitting co-operating mold elements ensures, on the one hand, that the sub-segments find their correct position in a simple manner when assembling the casting core.
- the form-fitting coupling ensures that that the subsegments maintain their position during the casting process even under the load of the melt that is poured into the casting mold and penetrates the casting core.
- the secure hold of the subsegments can be supported by the fact that the subsegments are glued to one another in the area of the form elements that are positively coupled to one another.
- the mold elements can couple the casting core according to the invention to the other casting cores or mold parts of the respective casting mold.
- it can be expedient to form the shaped elements, via which the adjacent subsegments of a casting core according to the invention are fixed in relation to one another so as to be immovable in at least one direction, as projections protruding in the radial direction.
- Form elements designed as projections in this way and securing the sub-segments positively against one another allow, for example, a simple coupling of the sub-segments to the molded parts and cores surrounding the casting core in the casting mold, such as side cores, and thus a simple, automatable assembly of the casting mold according to the invention.
- the projections which are formed by the molded parts provided for the positive, mutual fixing of the partial segments, then form openings on the finished cast part, which lead to the cavities, channels, etc. depicted by the casting mold in the cast part.
- These openings can be closed by plugs that are subsequently inserted and connected to the surrounding material of the cast part, for example cohesively, for example by gluing or welding, or closed in some other way with additional material, for example in a welding process.
- the openings depicted by the projections can be used to overcast a possibly existing web, which can be formed by molten metal that has penetrated into the joint between two sub-segments that meet one another.
- a suitable cutting tool such as a drill or milling cutter, can be passed through the respective opening.
- the casting core has the basic shape of a hollow cylinder extending in a longitudinal direction with two end faces lying opposite one another in the longitudinal direction.
- the individual subsegments can be shaped like a shell in the case of a casting core designed in the shape of a cylinder tube in this way.
- a design of a casting core according to the invention is achieved in that the casting core is designed according to the invention at least over a section as a band running around the space delimited by the casting core.
- the course of the dividing joint between the sub-segments of a casting core according to the invention is selected in accordance with the course and the arrangement of the structures that are provided in the area of its wall to create cavities, channels and the like in the cast part map.
- the dividing joint can extend at least in sections in the longitudinal direction of the casting core or at least in sections in the circumferential direction of the casting core.
- a dividing joint can also change direction in its course, that is to say extend over a section in the longitudinal direction of the casting core and over another section in the circumferential direction and so on.
- the dividing plane extends between at least two mutually adjacent subsegments from one end to the other of the casting core.
- the abutting sub-segments of a casting mold For the positive definition of the abutting sub-segments of a casting mold according to the invention, it has been found to be particularly suitable if the form elements via which the adjacent sub-segments are fixed in at least one direction non-displaceably by positive locking, on the edge side of the first sub-segment and on the edge side of the second sub-segment a recess is formed which fills the projection of the first sub-segment.
- the recess can be designed, for example, as a wedge-shaped, conical-shaped or half-shell-shaped depression and the projection can be designed as a wedge-shaped or semicircular cross-section or shaped as a cone.
- the core idea of the invention is therefore to split a complexly shaped casting core, which is a hollow body in its basic shape, into subsegments, which are easier to manufacture due to their spatially no longer closed shape, but at the same time in the casting core via suitably designed mold elements against each other are specified that a precise mapping of the cavities, channels and the like to be shaped by the casting core in the casting is guaranteed.
- “Spatially separated” and “physically independent” in this context means that a separate shaping cavity is provided in a core shooting machine for each of the subsegments. This of course includes the possibility, which is important in practice, of shaping the subsegments jointly and simultaneously in a core shooting box in which a mold cavity is provided for each of the subsegments.
- This variant of the method according to the invention enables a cost-effective and time-saving production of a respective set of subsegments which can be assembled together to form a casting core according to the invention.
- the casting core 1 has the basic shape of a cylindrical hollow body and accordingly delimits an interior IR, which extends in the longitudinal direction LR from the lower end face SU to the upper end face SO of the casting core 1.
- the peripheral wall 2 of the casting core 1 is formed by a ring segment-like ring section 3 that runs around the longitudinal axis LX of the casting core 1 and a meandering section 4.
- the ring section 3 shaped like a band with a certain thickness, extends over approximately three quarters of the circumference of the casting core 1.
- the beginning of the meander section 4 is connected to the end of the ring section 3.
- the turns 6 of the meander section 4 are each placed such that its longitudinal sections 7 are axially parallel to the longitudinal axis LX.
- the meander section 4 runs from the end of the ring section 3 in the opposite direction of the ring section 3 around the interior space IR delimited by the casting core 1 until it reaches the beginning of the meander section 4 with its end provided at the end of a longitudinal section 7 '.
- the projection 8 protruding radially outward there forms the outflow opening of the water jacket to be formed by the casting core 1 in the finished housing.
- the casting core 1 is divided into nine subsegments 9-17.
- the first sub-segment 9 extends, starting from the projection 5, over half the length of the ring section 3.
- the second sub-segment 10 occupies the second half of the ring section 3.
- the third to ninth subsegments 11-17 each extend over approximately one seventh the length of the meander section 4, the ninth subsegment 17 being longer than the other subsegments 11-16 of the meander section 4 by the longitudinal section leading to the end of the meander section 4.
- the dividing joints (of those in Fig. 1 the dividing joints 18-24 are visible), in which the subsegments 9,10; 10.11; 11.12; 12.13; 13; 14; 14; 15; 15.16; 16; 17 meet, each run in a first section 25 in the longitudinal direction LR and in an adjoining section 26 in the circumferential direction UR, the angle enclosed between the sections 25 and 26 being not equal to 90 °, i.e. the orientation of the section 25 not only one component in the longitudinal direction LR, but also in the circumferential direction UR and the alignment of the section 26 can have not only one component in the circumferential direction UR, but also in the longitudinal direction LR.
- a shaped element 27a, 27b, 28a, 28b, 29a, 29b, 30a, 30b in the form of a radially outward direction is adjacent to the edge sides of the subsegments 9-16 that meet in the dividing joint 18-24 protruding projection formed.
- pairs 27a, 27b; 28a, 28b; 29a, 29b; 30a, 30b of shaped elements 27a-30b have one Shaped element 27a, 28a, 29a, 30a each have a recess 31 which extends over its projection length LV and which is shaped like a notch with a cross section corresponding to a third of a circle.
- the shaped elements 27b, 28b, 29b, 30b respectively assigned to the shaped elements 27a, 28a, 29a, 30a are accordingly wedge-shaped with a cross-section that is also third-circular.
- the shaped elements 27b, 28b, 29b, 30b each fill the recess 31 of the associated shaped elements 27a, 28a, 29a, 30a, so that pairs of shaped elements 27a, 27b; 28a, 28b; 29a, 29b; 30a, 30b formed, radially outwardly projecting projections have an overall circular cross section.
- the subsegments 9-17 are positively fixed to one another in the circumferential direction UR and in the longitudinal direction LR so that a relative movement in the circumferential direction UR and is prevented in the longitudinal direction LR on the lower face SU.
- a core shooting box is provided, of which in Fig. 3 the lower part 40 is shown.
- the core shooting box which is not shown here for the sake of clarity, is set up in such a way that the subsegments 9-17 for two toroidal cores 1 of the same type can be shot in it.
- two sets of spatially separated mold cavities 49-57 are formed in the lower part 40 of the core shooting box and in the associated upper part of the core shooting box (not shown here) in a corresponding manner.
- two sets of subsegments 9-17 can be shot in a manner known per se in this way. These are then combined to form two toroidal cores 1. This assembly can take place before the casting cores 1 are placed in the respective casting mold, or the Subsegments 9-17 can be assembled in the respective casting mold to form the casting core 1 provided in it.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Description
Die Erfindung betrifft einen Gießkern, der die Grundform eines Hohlkörpers aufweist, wobei der Gießkern aus einem Formstoff geformt ist, welcher aus einer Mischung besteht, die aus einem Formsand und einem Binder sowie optional aus zur Einstellung seiner Eigenschaften zugegebenen Additiven gebildet ist.The invention relates to a casting core which has the basic shape of a hollow body, the casting core being formed from a molding material which consists of a mixture formed from a molding sand and a binder and optionally from additives added to adjust its properties.
Gießkerne der hier in Rede stehenden Art dienen zur gießtechnischen Herstellung von Gussteilen aus einer Metallschmelze. In dem jeweiligen Gussteil bilden die Gießkerne Hohlräume, wie Kanäle oder Kammern, aus. Diese Hohlräume können zur Einsparung von Gewicht vorgesehen sein. In der Regel werden sie aber im praktischen Gebrauch von einem Fluid durchströmt.Casting cores of the type in question are used for the casting production of cast parts from a metal melt. The casting cores form cavities, such as channels or chambers, in the respective cast part. These cavities can be provided to save weight. As a rule, however, a fluid flows through them in practical use.
Um die Gießkerne nach der Erstarrung des Gussmaterials aus dem Gussteil entfernen zu können, werden sie als so genannte "verlorene Kerne" eingesetzt. Zu ihrer Herstellung wird das in der oben erläuterten Weise gemischte Formstoffgemisch mit hohem Druck in die formgebende Kavität einer Kernschießvorrichtung eingebracht ("geschossen"). Die Fließfähigkeit des Formstoffs, der Schießdruck und die Positionen, an denen der Formstoff in den Formhohlraum der zur Herstellung der Kerne vorgesehenen Maschine eingebracht wird, sind dabei so abgestimmt, dass eine vollständige Formfüllung auch bei besonders feinteiligen Kernen erzielt wird. Nach dem Kernschießen werden die Kerne durch Beaufschlagung mit Wärme oder Begasung mit einem Reaktionsgas so verfestigt, dass sie aus der Kernschießmaschine entnommen und in die jeweilige Gießform eingesetzt werden können, wo sie den beim Abgießen der Metallschmelze auftretenden Belastungen standhalten.In order to be able to remove the casting cores from the cast part after the casting material has solidified, they are used as so-called "lost cores". To produce them, the molding material mixture mixed in the manner explained above is introduced ("shot") into the molding cavity of a core-shooting device at high pressure. The flowability of the molding material, the shooting pressure and the positions at which the molding material is introduced into the mold cavity of the machine provided for manufacturing the cores are coordinated so that complete mold filling is achieved even with particularly fine-grained cores. After the core shooting, the cores are solidified by applying heat or gassing with a reaction gas so that they are out removed from the core shooter and inserted into the respective casting mold, where they can withstand the stresses that occur when the molten metal is poured off.
Typische Beispiele für Gussteile, in denen derartige Kanäle und Hohlräume mittels Gießkernen abgeformt werden, sind Gehäuse für Antriebsmaschinen, die im Betrieb gekühlt werden müssen. In derartigen Maschinengehäusen sind in der Regel so genannte "Kühlmäntel" vorgesehen, d.h., ein System von Kanälen, das den Bereich der Maschine umgibt, in dem im Betrieb in Folge von Energieumsätzen Wärme entsteht. Um hierbei eine optimale Durchströmung der kritischen Bereiche der Maschine und auf diese Weise einen maximalen Kühleffekt bei geringen Abmessungen zu sichern, werden höchste Anforderungen an die Qualität der Oberflächen der durch den Gießkern jeweils abgebildeten Kanäle gestellt.Typical examples of cast parts in which such channels and cavities are molded using casting cores are housings for drive machines that have to be cooled during operation. In such machine housings, so-called "cooling jackets" are generally provided, i.e. a system of ducts that surround the area of the machine in which heat is generated during operation as a result of energy conversion. In order to ensure an optimal flow through the critical areas of the machine and in this way a maximum cooling effect with small dimensions, the highest demands are placed on the quality of the surfaces of the channels represented by the casting core.
Die besondere Herausforderung bei der Herstellung von Gießkernen der hier in Rede stehenden Art besteht darin, dass die Gießkerne in der Regel keinen massiven Körper bilden, sondern vielfach durchbrochen sind, so dass ihre Wände fein zergliederte Strukturen bilden, die Inseln, in denen größere Mengen des Kernmaterials versammelt sind, größere und dickere Bahnen, fein verästelte Stege, größere Brücken und andere filigran geformte Formelemente umfassen können. Aufgrund der umlaufend geschlossenen, im Querschnitt typischerweise kreisförmigen oder ellipsoiden Grundgestalt der Gießkerne ist bei derart feinzergliederten Gießkernen das Entformen der Kerne aus der Kernschießmaschine nur mit großem Aufwand möglich. So müssen komplexe Schieberkonstruktionen und desgleichen vorgesehen werden, um trotz der großen Zahl von Hinterschnitten und Durchbrechungen die formgebenden Bauteile der Kernschießmaschine vom fertigen Kern trennen zu können. Abgesehen von den hohen Kosten, die eine derart komplexe Maschine mit sich bringt, erschwert dieser Aufwand eine großtechnische, schnell getaktete Serienfertigung von Gießkernen der hier in Rede stehenden Art.The particular challenge in the production of casting cores of the type in question is that the casting cores usually do not form a solid body, but are often perforated, so that their walls form finely divided structures, the islands, in which larger amounts of the Core material are gathered, larger and thicker webs, finely branched webs, larger bridges and other filigree shaped elements. Due to the circumferentially closed basic shape of the casting cores, typically circular or ellipsoid in cross-section, with such finely divided casting cores demolding the cores from the core shooting machine is only possible with great effort. Complex slide designs and the like must be provided in order to be able to separate the shaping components of the core shooting machine from the finished core despite the large number of undercuts and openings. Apart from the high costs that such a complex machine entails, this effort complicates the large-scale, rapidly clocked series production of casting cores of the type in question.
Aus der
Ebenso ist aus der
Vor dem Hintergrund des voranstehend erläuterten Standes der Technik hat sich die Aufgabe ergeben, einen in seiner Grundform einem Hohlkörper entsprechenden Gießkern zu gestalten, der eine einfache Herstellung ermöglicht.Against the background of the prior art explained above, the task has arisen to design a casting core that corresponds in its basic shape to a hollow body and that enables simple manufacture.
Die Erfindung hat diese Aufgabe durch einen Gießkern gelöst, der mindestens die in Anspruch 1 angegebenen Merkmale besitzt.The invention has achieved this object by a casting core which has at least the features specified in claim 1.
Vorteilhafte Ausgestaltungen der Erfindung sind in den abhängigen Ansprüchen angegeben und werden nachfolgend wie der allgemeine Erfindungsgedanke im Einzelnen erläutert.Advantageous embodiments of the invention are specified in the dependent claims and are explained in detail below, like the general inventive concept.
Ein erfindungsgemäßer Gießkern, der die Grundform eines Hohlkörpers aufweist, wobei der Gießkern aus einem Formstoff geformt ist, welcher aus einer Mischung besteht, die aus einem Formsand und einem Binder sowie optional aus zur Einstellung seiner Eigenschaften zugegebenen Additiven gebildet ist, ist somit erfindungsgemäß dadurch gekennzeichnet, dass der Gießkern in mindestens zwei Teilsegmente geteilt ist und an den Randseiten, mit denen zueinander benachbart angeordnete Teilsegmente aneinander stoßen, oder in der Nachbarschaft von diesen Randseiten miteinander formschlüssig zusammenwirkende Formelemente vorgesehen sind, über die die zueinander benachbart angeordneten Teilesegmente mindestens in einer Richtung durch Formschluss gegeneinander unbeweglich festgelegt sind.A casting core according to the invention, which has the basic shape of a hollow body, the casting core being formed from a molding material which is composed of a mixture, which is formed from a molding sand and a binder and optionally from additives added to adjust its properties, is thus characterized according to the invention in that the casting core is divided into at least two sub-segments and on the edge sides, with which sub-segments arranged adjacent to one another abut, or in the vicinity of these edge sides with each other positively cooperating form elements are provided, by means of which the mutually adjacent part segments are fixed immovably against each other at least in one direction by a form fit.
Ein erfindungsgemäßer Gießkern ist also nicht in einem Stück hergestellt, sondern aus zwei oder mehr Teilsegmenten zusammengesetzt. Da diese Einzelsegmente selbst keinen Hohlraum mehr umgrenzen, können sie im konventionellen Kernschießprozess mit einfach gestalteten Kernwerkzeugen hergestellt werden. Komplexe Schieberanordnungen, wie sie zur Abbildung von Hohlkörpern benötigt werden, sind zur Herstellung der Teilsegmente nicht erforderlich. Gleichzeitig sind die erfindungsgemäß gebildeten Teilsegmente aufgrund ihrer begrenzten räumlichen Ausdehnung auch dann vergleichbar unempfindlich, wenn sie filigran mit vielen Durchbrechungen und desgleichen gestaltet sind. Dies erlaubt es, die Teilsegmente unkompliziert zu lagern und zum Zusammenbau des Gießkerns zu transportieren. Dabei kann der Zusammenbau des erfindungsgemäßen Gießkerns im Zuge des Zusammenbaus der gesamten Gießform, in der er eingesetzt werden soll oder an einer hiervon separierten Stelle, vorgenommen werden.A casting core according to the invention is therefore not made in one piece, but rather is composed of two or more subsegments. Since these individual segments themselves no longer define a cavity, they can be produced in the conventional core shooting process with simply designed core tools. Complex slide arrangements, such as those required for mapping hollow bodies, are not required to produce the subsegments. At the same time, the sub-segments formed according to the invention are also comparatively insensitive due to their limited spatial extent if they are designed in a filigree manner with many openings and the like. This allows the subsegments to be stored in an uncomplicated manner and transported for assembling the casting core. The assembly of the casting core according to the invention can be carried out in the course of the assembly of the entire casting mold in which it is to be used or at a point separated therefrom.
Dadurch, dass die Teilsegmente der erfindungsgemäßen Gießform durch die formschlüssig zusammenwirkenden Formelemente in ihrer relativen Lage fixiert sind, ist einerseits sichergestellt, dass die Teilsegmente beim Zusammenbau des Gießkerns auf einfache Weise ihre korrekte Position finden. Andererseits ist über die formschlüssige Verkopplung gewährleistet, dass die Teilsegmente beim Gießvorgang auch unter der Last der in die Gießform eingegossenen und den Gießkern penetrierenden Schmelze ihre Position beibehalten.The fact that the sub-segments of the casting mold according to the invention are fixed in their relative position by the form-fitting co-operating mold elements ensures, on the one hand, that the sub-segments find their correct position in a simple manner when assembling the casting core. On the other hand, the form-fitting coupling ensures that that the subsegments maintain their position during the casting process even under the load of the melt that is poured into the casting mold and penetrates the casting core.
Unterstützt werden kann bei einer erfindungsgemäßen Gießform der sichere Halt der Teilsegmente untereinander dadurch, dass die Teilsegmente im Bereich der sie formschlüssig miteinander verkoppelnden Formelemente miteinander verklebt sind. Alternativ oder ergänzend ist es auch möglich, die Formelemente dazu zu nutzen, den erfindungsgemäßen Gießkern an die anderen Gießkerne oder Formteile der jeweiligen Gießform anzukoppeln. So kann es beispielsweise zweckmäßig sein, die Formelemente, über die benachbarte Teilsegmente eines erfindungsgemäßen Gießkerns gegeneinander in mindestens einer Richtung unverschiebbar durch Formschluss festgelegt sind, als in radialer Richtung vorstehende Vorsprünge auszubilden. Derart als Vorsprünge ausgebildete, die Teilsegmente formschlüssig gegeneinander festlegende Formelemente ermöglichen beispielsweise ein einfaches Ankoppeln der Teilsegmente an die den Gießkern in der Gießform umgebenden Formteile und Kerne, wie Seitenkerne, und damit einen einfachen automatisierbaren Zusammenbau der erfindungsgemäßen Gießform.In the case of a casting mold according to the invention, the secure hold of the subsegments can be supported by the fact that the subsegments are glued to one another in the area of the form elements that are positively coupled to one another. Alternatively or in addition, it is also possible to use the mold elements to couple the casting core according to the invention to the other casting cores or mold parts of the respective casting mold. For example, it can be expedient to form the shaped elements, via which the adjacent subsegments of a casting core according to the invention are fixed in relation to one another so as to be immovable in at least one direction, as projections protruding in the radial direction. Form elements designed as projections in this way and securing the sub-segments positively against one another allow, for example, a simple coupling of the sub-segments to the molded parts and cores surrounding the casting core in the casting mold, such as side cores, and thus a simple, automatable assembly of the casting mold according to the invention.
Nach dem Entformen bilden die Vorsprünge, die durch die zur formschlüssigen gegenseitigen Festlegung der Teilsegmente vorgesehenen Formteile gebildet sind, am fertigen Gussteil dann Öffnungen ab, die zu den durch die Gießform im Gussteil abgebildeten Hohlräumen, Kanälen etc. führen. Diese Öffnungen können durch nachträglich eingesetzte und mit dem umgebenden Material des Gussteils beispielsweise stoffschlüssig, z.B. durch Kleben oder Schweißen, verbundene Stopfen verschlossen oder in anderer Weise mit Zusatzmaterial, beispielsweise in einem Schweißvorgang, verschlossen werden.After removal from the mold, the projections, which are formed by the molded parts provided for the positive, mutual fixing of the partial segments, then form openings on the finished cast part, which lead to the cavities, channels, etc. depicted by the casting mold in the cast part. These openings can be closed by plugs that are subsequently inserted and connected to the surrounding material of the cast part, for example cohesively, for example by gluing or welding, or closed in some other way with additional material, for example in a welding process.
Vor dem Verschließen können die durch die Vorsprünge abgebildeten Öffnungen zum Versäubern eines möglicherweise vorhandenen Stegs genutzt werden, der sich durch Metallschmelze bilden kann, die in die Fügefuge zwischen zwei aufeinander treffenden Teilsegmenten gedrungen ist. Hierzu kann ein geeignetes spanabhebendes Werkzeug, wie ein Bohrer oder Fräser, durch die jeweilige Öffnung geführt werden.Before closing, the openings depicted by the projections can be used to overcast a possibly existing web, which can be formed by molten metal that has penetrated into the joint between two sub-segments that meet one another. For this purpose, a suitable cutting tool, such as a drill or milling cutter, can be passed through the respective opening.
Erfindungsgemäß hat der Gießkern die Grundform eines sich in einer Längsrichtung erstreckenden Hohlzylinders mit zwei in Längsrichtung einander gegenüberliegenden Stirnseiten. Durch entsprechend gelegte Teilungsfugen zwischen den Teilsegmenten können bei einem derart zylinderrohrförmig gestalteten Gießkern die einzelnen Teilsegmente schalenartig geformt sein. Genauso kann es aber auch zweckmäßig sein, ein oder mehrere Teilsegmente so von den anderen Teilsegmenten der Gießform zu trennen, dass die betreffenden Teilsegmente ringförmig sind. Es versteht sich dabei von selbst, dass eine derartige ringförmige Gestaltung auch für alle Teilsegmente der Gießform vorteilhaft sein kann, wenn die Formgebung des Gießkerns einen entsprechenden Verlauf der Teilungsfugen zwischen den Teilsegmenten hergibt.According to the invention, the casting core has the basic shape of a hollow cylinder extending in a longitudinal direction with two end faces lying opposite one another in the longitudinal direction. By appropriately placed dividing joints between the subsegments, the individual subsegments can be shaped like a shell in the case of a casting core designed in the shape of a cylinder tube in this way. However, it can also be expedient to separate one or more subsegments from the other subsegments of the casting mold in such a way that the subsegments in question are annular. It goes without saying that such an annular design can also be advantageous for all sub-segments of the casting mold if the shape of the casting core produces a corresponding course of the dividing joints between the sub-segments.
Eine insbesondere für die Herstellung eines Kühlmantels einer elektrisch betriebenen Antriebsmaschine typische Gestaltung eines erfindungsgemäßen Gießkerns wird dabei dadurch erreicht, dass der Gießkern erfindungsgemäß mindestens über einen Abschnitt als um den vom Gießkern umgrenzten Raum mäanderförmig verlaufendes Band ausgebildet ist.A design of a casting core according to the invention, particularly typical for the production of a cooling jacket of an electrically operated drive machine, is achieved in that the casting core is designed according to the invention at least over a section as a band running around the space delimited by the casting core.
Wie voranstehend schon angedeutet, wird bei einem erfindungsgemäßen Gießkern der Verlauf der Teilungsfuge zwischen den Teilsegmenten eines erfindungsgemäßen Gießkern entsprechend dem Verlauf und der Anordnung der Strukturen gewählt, die im Bereich seiner Wandung vorgesehen sind, um im Gussteil Hohlräume, Kanäle und desgleichen abzubilden. Dabei kann sich die Teilungsfuge zwischen zwei benachbarten Teilsegmenten mindestens abschnittsweise in Längsrichtung des Gießkerns erstrecken oder zumindest abschnittsweise in Umfangsrichtung des Gießkerns verlaufen. Selbstverständlich kann eine Teilungsfuge auch in ihrem Verlauf ihre Richtung wechseln, also über einen Abschnitt in Längsrichtung des Gießkerns und über einen anderen Abschnitt in Umfangsrichtung und so fort verlaufen. Insbesondere im Fall, dass der Gießkern die Form eines Zylinderhohlkörpers aufweist, hat es sich dabei als zweckmäßig erwiesen, wenn sich die Teilungsebene zwischen mindestens zwei zueinander benachbarten Teilsegmenten von der einen bis zur anderen Stirnseite des Gießkerns erstreckt.As already indicated above, in a casting core according to the invention, the course of the dividing joint between the sub-segments of a casting core according to the invention is selected in accordance with the course and the arrangement of the structures that are provided in the area of its wall to create cavities, channels and the like in the cast part map. The dividing joint can extend at least in sections in the longitudinal direction of the casting core or at least in sections in the circumferential direction of the casting core. Of course, a dividing joint can also change direction in its course, that is to say extend over a section in the longitudinal direction of the casting core and over another section in the circumferential direction and so on. In particular in the event that the casting core has the shape of a hollow cylinder body, it has proven to be expedient if the dividing plane extends between at least two mutually adjacent subsegments from one end to the other of the casting core.
Für die formschlüssige Festlegung der aneinander stoßenden Teilsegmente einer erfindungsgemäßen Gießform besonders geeignet herausgestellt hat es sich, wenn als Formelemente, über die benachbarte Teilsegmente gegeneinander in mindestens einer Richtung unverschiebbar durch Formschluss festgelegt sind, an der Randseite des ersten Teilsegments ein Vorsprung und an der Randseite des zweiten Teilsegments eine Ausnehmung ausgebildet ist, die der Vorsprung des ersten Teilsegments füllt. Die Ausnehmung kann dabei beispielsweise als keil-, konus- oder halbschalenförmige Einsenkung und der Vorsprung im Querschnitt entsprechend keil- oder halbkreisförmig ausgebildet oder als Konus geformt sein. Auf diese Weise finden die miteinander zu verkoppelnden Teilsegmente über ihre miteinander formschlüssig zusammenwirkenden Formelemente nach Art einer Selbstzentrierung beim Zusammensetzen des Gießkerns präzise ihre vorgesehene Relativposition.For the positive definition of the abutting sub-segments of a casting mold according to the invention, it has been found to be particularly suitable if the form elements via which the adjacent sub-segments are fixed in at least one direction non-displaceably by positive locking, on the edge side of the first sub-segment and on the edge side of the second sub-segment a recess is formed which fills the projection of the first sub-segment. The recess can be designed, for example, as a wedge-shaped, conical-shaped or half-shell-shaped depression and the projection can be designed as a wedge-shaped or semicircular cross-section or shaped as a cone. In this way, the sub-segments to be coupled to one another find their intended relative position precisely via their form elements interacting in a form-fitting manner in the manner of self-centering when the casting core is assembled.
Der Kerngedanke der Erfindung besteht folglich darin, einen komplex geformten, in seiner Grundform einen Hohlkörper darstellenden Gießkern in Teilsegmente zu zerlegen, die aufgrund ihrer räumlich nicht mehr geschlossenen Gestalt einfacher herzustellen sind, gleichzeitig aber in dem Gießkern über geeignet gestaltete Formelemente so gegeneinander festgelegt sind, dass eine präzise Abbildung der jeweils durch den Gießkern im Gussteil abzuformenden Hohlräume, Kanäle und desgleichen gewährleistet ist.The core idea of the invention is therefore to split a complexly shaped casting core, which is a hollow body in its basic shape, into subsegments, which are easier to manufacture due to their spatially no longer closed shape, but at the same time in the casting core via suitably designed mold elements against each other are specified that a precise mapping of the cavities, channels and the like to be shaped by the casting core in the casting is guaranteed.
Diesem Kerngedanken folgend sieht das Verfahren zur Herstellung eines erfindungsgemäßen Gießkerns mindestens folgende Arbeitsschritte vor:
- a) Herstellen der Teilsegmente des Gießkerns, wobei die Teilsegmente zueinander räumlich getrennt und körperlich unabhängig voneinander aus einem Formstoff geformt werden, der aus einem Formsand und einem Binder sowie optional zur Einstellung seiner Eigenschaften zugegebenen Additiven besteht;
- b) Zusammenfügen der räumlich getrennt voneinander hergestellten Teilsegmente zu dem Gießkern.
- a) producing the sub-segments of the casting core, the sub-segments being spatially separated from one another and physically formed independently of one another from a molding material consisting of a molding sand and a binder and additives optionally added to adjust its properties;
- b) joining the subsegments produced spatially separately from one another to form the casting core.
"Räumlich getrennt" und "körperlich unabhängig" bedeutet in diesem Zusammenhang, dass für jedes der Teilsegmente jeweils ein eigener formgebender Hohlraum in einer Kernschießmaschine vorgesehen ist. Dies schließt selbstverständlich die für die Praxis wichtige Möglichkeit ein, die Teilsegmente gemeinsam und gleichzeitig in einem Kernschießkasten zu formen, in dem für jedes der Teilsegmente ein Formhohlraum vorgesehen ist. Diese Variante des erfindungsgemäßen Verfahrens ermöglicht eine kostengünstige und zeitsparende Herstellung jeweils eines Satzes von Teilsegmenten, die gemeinsam zu einem erfindungsgemäßen Gießkern zusammengesetzt werden können."Spatially separated" and "physically independent" in this context means that a separate shaping cavity is provided in a core shooting machine for each of the subsegments. This of course includes the possibility, which is important in practice, of shaping the subsegments jointly and simultaneously in a core shooting box in which a mold cavity is provided for each of the subsegments. This variant of the method according to the invention enables a cost-effective and time-saving production of a respective set of subsegments which can be assembled together to form a casting core according to the invention.
Nachfolgend wird die Erfindung anhand einer ein Ausführungsbeispiel darstellenden Zeichnung näher erläutert. Deren Figuren zeigen jeweils schematisch:
-
Fig. 1 einen Gießkern in einer perspektivischen Ansicht von oben; -
Fig. 2 einen Ausschnitt A des Gießkerns gemäßFig. 1 ; -
Fig. 3 das Unterteil eines Kernschießkastens in Draufsicht.
-
Fig. 1 a casting core in a perspective view from above; -
Fig. 2 a section A of the casting core according toFig. 1 ; -
Fig. 3 the lower part of a core shooting box in plan view.
Der Gießkern 1 weist die Grundform eines zylindrischen Hohlkörpers auf und umgrenzt dementsprechend einen Innenraum IR, der sich in Längsrichtung LR von der unteren Stirnseite SU zur oberen Stirnseite SO des Gießkerns 1 erstreckt.The casting core 1 has the basic shape of a cylindrical hollow body and accordingly delimits an interior IR, which extends in the longitudinal direction LR from the lower end face SU to the upper end face SO of the casting core 1.
Der aus einem hierzu bewährten, aus einem Formsand und einem organischen oder anorganischen Binder in an sich bekannter Weise gemischten Formstoff geformte Gießkern 1 dient zum Abbilden eines Kühlwassermantels in einem Gehäuse für einen als Fahrzeugantrieb dienenden Elektromotor, der in einer hier weiter nicht dargestellten, beispielsweise als Kernpaket zusammengesetzten Gießform aus einer Leichtmetallschmelze, wie beispielsweise aus einem konventionellen Aluminiumgusswerkstoff, gegossen wird.The casting core 1 formed from a mold material, which has been tried and tested for this purpose and is mixed in a known manner from a molding sand and an organic or inorganic binder, is used to form a cooling water jacket in a housing for an electric motor serving as a vehicle drive, which is used in a not shown here, for example as Core package composed casting mold from a light metal melt, such as from a conventional aluminum casting material, is poured.
Die Umfangswand 2 des Gießkerns 1 ist durch einen ringsegmentartigen, um die Längsachse LX des Gießkerns 1 umlaufenden Ringabschnitt 3 und einen Mäanderabschnitt 4 gebildet.The peripheral wall 2 of the casting core 1 is formed by a ring segment-like ring section 3 that runs around the longitudinal axis LX of the casting core 1 and a meandering section 4.
Ausgehend von einem in radialer Richtung RR nach außen abstehenden, im fertigen Gehäuse eine Einströmöffnung darstellenden Vorsprung 5 erstreckt sich der nach Art eines Bandes mit einer gewissen Dicke geformte Ringabschnitt 3 über etwa drei Viertel des Umfangs des Gießkerns 1.Starting from a
An das Ende des Ringabschnitts 3 ist der Beginn des Mäanderabschnitts 4 angeschlossen. Die Windungen 6 des Mäanderabschnitts 4 sind jeweils so gelegt, dass seine Längsabschnitte 7 achsparallel zur Längsachse LX liegen. Dabei verläuft der Mäanderabschnitt 4 ausgehend von dem Ende des Ringabschnitts 3 in entgegengesetzter Richtung des Ringabschnitts 3 um den vom Gießkern 1 umgrenzten Innenraum IR, bis er mit seinem am Ende eines Längsabschnitts 7' vorgesehenen Ende benachbart zum Beginn des Mäanderabschnitts 4 angelangt. Der dort radial nach außen abstehende Vorsprung 8 bildet im fertigen Gehäuse die Abströmöffnung des durch den Gießkern 1 zu formenden Wassermantels ab.The beginning of the meander section 4 is connected to the end of the ring section 3. The turns 6 of the meander section 4 are each placed such that its
Der Gießkern 1 ist in neun Teilsegmente 9 - 17 aufgeteilt. Das erste Teilsegment 9 erstreckt sich ausgehend vom Vorsprung 5 über die Hälfte der Länge des Ringabschnitts 3. Das zweite Teilsegment 10 nimmt die zweite Hälfte des Ringabschnitts 3 ein. Das dritte bis neunte Teilsegment 11 - 17 erstreckt sich jeweils über etwa ein siebtel der Länge des Mäanderabschnitts 4, wobei das neunte Teilsegment 17 um den zum Ende des Mäanderabschnitts 4 führenden Längsabschnitt länger ist als die anderen Teilsegmente 11 - 16 des Mäanderabschnitts 4.The casting core 1 is divided into nine subsegments 9-17. The
Die Teilungsfugen (von denen in
Dabei ist im Bereich jeder Teilungsfuge 18 - 24 angrenzend an die jeweils in der Teilungsfuge 18 - 24 aufeinander treffenden Randseiten der Teilsegmente 9 - 16 ein Formelement 27a,27b,28a,28b,29a,29b,30a,30b in Form eines radial nach außen vorstehenden Vorsprungs ausgebildet. Von den an den Teilungsfugen 18 - 24 derart gebildeten Paaren 27a,27b; 28a,28b; 29a,29b; 30a,30b von Formelementen 27a - 30b weist das eine Formelement 27a,28a,29a,30a jeweils eine sich über seine Vorsprungslänge LV erstreckende Ausnehmung 31 auf, die nach Art einer im Querschnitt einem Drittelkreis entsprechend geformten Einkerbung geformt ist. Die den Formelementen 27a, 28a,29a,30a jeweils zugeordneten Formelemente 27b,28b,29b,30b sind dementsprechend keilförmig mit einem ebenfalls drittelkreisförmigen Querschnitt. Auf diese Weise füllen die Formelemente 27b,28b,29b,30b jeweils die Ausnehmung 31 der zugeordneten Formelemente 27a,28a,29a,30a, so dass aus Formelemente-Paaren 27a,27b; 28a,28b; 29a,29b; 30a,30b gebildete, radial nach außen vorstehende Vorsprünge einen insgesamt kreisförmigen Querschnitt besitzen.In this case, in the area of each dividing joint 18-24, a
Über die an den Teilsegmenten 9 -17 jeweils vorgesehenen Formelemente 27a - 30b und ihre im Bereich der Teilungsfugen 18 - 24 aneinander stoßenden Randseiten sind die Teilsegmente 9 - 17 in Umfangsrichtung UR und in Längsrichtung LR gegeneinander formschlüssig so festgelegt, dass eine Relativbewegung in Umfangsrichtung UR und in Längsrichtung LR auf die untere Stirnseite SU verhindert ist.By means of the shaped
Zur Herstellung des Ringkerns 1 wird ein Kernschießkasten bereitgestellt, von dem in
- 11
- GießkernCasting core
- 22
- Umfangswand des Gießkerns 1Peripheral wall of the casting core 1
- 33
- Ringabschnitt des Gießkerns 1Ring section of the casting core 1
- 44th
- Mäanderabschnitt des Gießkerns 1Meander section of the casting core 1
- 55
- Vorsprunghead Start
- 66th
- WindungenTurns
- 7, 7'7, 7 '
- LängsabschnitteLongitudinal sections
- 88th
- Vorsprunghead Start
- 9 - 179-17
- TeilsegmenteSubsegments
- 18 - 2418 - 24
- TeilungsfugenDividing joints
- 2525th
- in Längsrichtung LR verlaufender Abschnitt der TeilungsfugenSection of the dividing joints running in the longitudinal direction LR
- 2626th
- in Umfangsrichtung UR verlaufender Abschnitt der TeilungsfugenSection of the dividing joints running in the circumferential direction UR
- 27a - 30b27a-30b
- FormelementeForm elements
- 3131
- AusnehmungRecess
- 4040
- Kernkasten-UnterteilCore box lower part
- 49 - 5749-57
- FormhohlräumeMold cavities
- IRIR
- vom Gießkern umgrenzter InnenraumInterior delimited by the casting core
- LRLR
- Längsrichtung des Gießkerns 1Longitudinal direction of the casting core 1
- LVLV
- VorsprungslängeProtrusion length
- URUR
- Umfangsrichtung des Gießkerns 1Circumferential direction of the casting core 1
- RRRR
- radiale Richtungradial direction
- SUSU
- untere Stirnseite des Gießkerns 1lower face of the casting core 1
- SOSO
- obere Stirnseite des Gießkerns 1upper face of the casting core 1
- LXLX
- Längsachse des Gießkerns 1Longitudinal axis of the casting core 1
Claims (7)
- Foundry core, wherein the foundry core (1) is shaped from a moulding material consisting of a mixture which is formed from a moulding sand and a binder and optionally from additives added to set its properties wherein the foundry core (1) is divided into at least two sub-segments (9 - 17) and wherein forming elements (28a - 30b) interacting with one another in a positive-locking manner are provided on the edge sides, with which sub-segments (9 - 17) arranged adjacent to one another abut on one another, or in proximity to these edge sides, via which forming elements the sub-segments (9 - 17) arranged adjacent to one another are fixed by positive locking immovably against one another at least in one direction (LR, UR), characterised in that it has the base form of a hollow cylinder extending in a longitudinal direction (LR) with two end faces (SO, SU) opposed to one another in the longitudinal direction (LR) and that it is formed at least over one section (4) as a strip running in a meandering shape around the space (IR) delimited by the foundry core (1).
- Foundry core according to claim 1, characterised in that the sub-segments (9 - 17) are adhered to one another at least in the region of their forming elements (28a - 30b) fixed against one another in a positive-locking manner.
- Foundry core according to any one of the preceding claims, characterised in that the separating joint (18 - 24) extends between two adjacent sub-segments (9 - 17) at least in sections in the longitudinal direction (LR) of the foundry core (1).
- Foundry core according to claim 2, characterised in that the separating joint (18 - 24) extends between at least two sub-segments (9 - 17) adjacent to one another from one end face of the foundry core (1) to the other.
- Foundry core according to any one of the preceding claims, characterised in that the separating joint (18 - 24) runs between two sub-segments (9 - 17) adjacent to one another in the circumferential direction (UR) of the foundry core (1).
- Foundry core according to any one of the preceding claims, characterised in that as forming elements (28a - 30b), via which adjacent sub-segments (9 - 17) are fixed by positive locking immovably against one another in at least one direction (LR, UR), on the edge side of the first sub-segment (9 - 17) a projection is formed and on the edge side of the second sub-segment (9 - 17) a recess (31) is formed, which fills the projection of the first sub-segment (9 - 17).
- Foundry core according to any one of the preceding claims, characterised in that the forming elements (28a - 30b) are formed as projections protruding in the radial direction, via which adjacent sub-segments (9 - 17) are fixed by positive locking immovably against one another in at least one direction (LR, UR).
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---|---|---|---|---|
US4093018A (en) * | 1976-10-19 | 1978-06-06 | Deere & Company | Casting methods with composite molded core assembly |
US5295530A (en) | 1992-02-18 | 1994-03-22 | General Motors Corporation | Single-cast, high-temperature, thin wall structures and methods of making the same |
JP2003053478A (en) | 2001-08-13 | 2003-02-26 | Mitsubishi Heavy Ind Ltd | Lost foam pattern casting method |
US7172012B1 (en) * | 2004-07-14 | 2007-02-06 | United Technologies Corporation | Investment casting |
US7438117B2 (en) * | 2006-01-19 | 2008-10-21 | Gm Global Technology Operations, Inc. | Cylinder block casting bulkhead window formation |
US20070221359A1 (en) | 2006-03-21 | 2007-09-27 | United Technologies Corporation | Methods and materials for attaching casting cores |
GB2455560B (en) * | 2007-12-14 | 2009-12-16 | Rolls Royce Plc | Core for casting |
US8215372B2 (en) | 2008-10-17 | 2012-07-10 | Brp Us Inc. | Method and apparatus for consumable-pattern casting |
US20110204205A1 (en) * | 2010-02-25 | 2011-08-25 | Ahmed Kamel | Casting core for turbine engine components and method of making the same |
DE102010047952A1 (en) * | 2010-10-08 | 2012-04-12 | Continental Automotive Gmbh | Method for producing a housing, in particular a housing of a turbocharger |
DE102010054496B4 (en) * | 2010-12-14 | 2020-06-18 | Volkswagen Ag | Casting-made electric motor housing part for an electric motor |
JP2015044217A (en) * | 2013-08-28 | 2015-03-12 | 本田金属技術株式会社 | Core molding device |
DE102014102724A1 (en) | 2013-12-03 | 2015-06-03 | Nemak Linz Gmbh | Process for the casting production of castings from a molten metal |
-
2017
- 2017-03-29 DE DE102017106775.2A patent/DE102017106775A1/en not_active Withdrawn
-
2018
- 2018-03-28 MX MX2019011689A patent/MX2019011689A/en unknown
- 2018-03-28 KR KR1020197031561A patent/KR102162930B1/en active IP Right Grant
- 2018-03-28 WO PCT/IB2018/000316 patent/WO2018178762A1/en active Search and Examination
- 2018-03-28 JP JP2019552952A patent/JP6677862B1/en active Active
- 2018-03-28 CN CN201880021596.XA patent/CN110461499B/en active Active
- 2018-03-28 US US16/497,170 patent/US10843255B2/en active Active
- 2018-03-28 EP EP18721843.3A patent/EP3600718B1/en active Active
-
2019
- 2019-09-27 ZA ZA2019/06398A patent/ZA201906398B/en unknown
Non-Patent Citations (1)
Title |
---|
None * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2023248170A1 (en) | 2022-06-24 | 2023-12-28 | Nemak, S.A.B. De C.V. | Casting mould for producing a cast part formed from a light-metal alloy |
LU502349B1 (en) | 2022-06-24 | 2024-01-09 | Nemak Sab De Cv | Casting mold for producing a casting made from a light metal alloy |
Also Published As
Publication number | Publication date |
---|---|
US10843255B2 (en) | 2020-11-24 |
DE102017106775A1 (en) | 2018-10-04 |
WO2018178762A1 (en) | 2018-10-04 |
EP3600718A1 (en) | 2020-02-05 |
JP6677862B1 (en) | 2020-04-08 |
CN110461499A (en) | 2019-11-15 |
US20200316677A1 (en) | 2020-10-08 |
MX2019011689A (en) | 2019-11-28 |
ZA201906398B (en) | 2023-05-31 |
JP2020512937A (en) | 2020-04-30 |
CN110461499B (en) | 2021-01-29 |
KR102162930B1 (en) | 2020-10-08 |
KR20190128718A (en) | 2019-11-18 |
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