EP0793554B1 - Method of producing light metal castings and casting mould for carrying out the method - Google Patents

Method of producing light metal castings and casting mould for carrying out the method Download PDF

Info

Publication number
EP0793554B1
EP0793554B1 EP96930074A EP96930074A EP0793554B1 EP 0793554 B1 EP0793554 B1 EP 0793554B1 EP 96930074 A EP96930074 A EP 96930074A EP 96930074 A EP96930074 A EP 96930074A EP 0793554 B1 EP0793554 B1 EP 0793554B1
Authority
EP
European Patent Office
Prior art keywords
core
riser
sand
casting mould
mold
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.)
Expired - Lifetime
Application number
EP96930074A
Other languages
German (de)
French (fr)
Other versions
EP0793554A1 (en
Inventor
Manfred Buchborn
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Eisenwerk Bruehl GmbH
Original Assignee
Eisenwerk Bruehl GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Eisenwerk Bruehl GmbH filed Critical Eisenwerk Bruehl GmbH
Publication of EP0793554A1 publication Critical patent/EP0793554A1/en
Application granted granted Critical
Publication of EP0793554B1 publication Critical patent/EP0793554B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/08Features with respect to supply of molten metal, e.g. ingates, circular gates, skim gates
    • B22C9/082Sprues, pouring cups
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/09Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting by using pressure

Definitions

  • the invention relates to a method for manufacturing of light metal castings, in particular cylinder heads, Cylinder blocks and / or crankcases for internal combustion engines, with a mold cavity for the casting forming lost form based on sand that Outer mold parts, at least one core and at least one Has feeder to form a pressure mass, the Form is provided with a gate for the molten metal and the metal melt under the influence of gravity in the Mold cavity filled and then with a compressed gas is applied.
  • the low pressure casting of light metal melts is also known in permanent molds, with a Pressurizing the melt in the mold with a gas a fine, dense structure can be achieved (DE-A-21 33421, DE-A-28 18 442). Pressurization poses because of the Strength of the mold is not a problem.
  • the mold have a very long cooling time is - for high Production speeds - a very large number very expensive molds required. With the frequently occurring changes the castings are then a large number of molds to change; also make new.
  • a sand casting process is known in which the molten metal is poured into the sand mold under gravity and then pressurized with a pressurized gas.
  • a pressurized gas application is as A molded part made of temperature-resistant material based on aluminum-alumina-silica-iron oxide put on.
  • This feeder is made of metal produced, in the sand mold in addition to the molded food part molded pressure chamber enclosed. This pressure chamber is connected to a compressed gas supply.
  • the molded molded part must be shaped from the cooled casting and the pressure chamber is first removed from the sand mold, before it is completely disassembled and the sand if necessary can be worked up again.
  • the invention has for its object the casting of castings made of light metal under the influence of gravity and in lost forms based on sand regarding the Quality of the casting produced, especially in relation to a particularly dense and fine-grained structure with avoidance of improving microporosity as well as volume the feed material in the form of a pressure mass to reduce.
  • Light metal in the sense of the invention includes in particular Aluminum and aluminum alloys.
  • the invention achieves the stated object in relation to the Procedure in that a lid core on the mold Sand base is placed, which contains at least one feeder and at least in the areas that can be pressurized with compressed gas is designed gas-impermeable and that immediately after the filling process, the one filled with molten metal Feeder pressurized with the compressed gas becomes.
  • the method according to the invention provides that the pressurization of the molten metal in the feeder during the first critical solidification phase of the molten metal is executed, d. H. while the molten metal is still hot is, so that a corresponding influence by the pressure exerted the still flowable melt in the entire molding space is possible.
  • This first critical solidification phase goes up to a cooling temperature of the light metal melt of 500 ° C, below this temperature Pressurization only limited effect (claims 5 and 6).
  • a (lost) mold is also used the features of the preamble of claim 9 for implementation proposed the method according to the invention, the marked is by at least one containing a feeder Sand-based lid core, on one of which the dining area sealing pressure mask can be placed, and wherein the Cover core gas-impermeable at least in the contact area of the pressure mask is trained.
  • the one containing the feeder was made on the basis of sand Cover core by one on its surface at least Core coating applied in the area of the print mask is designed to be gas-impermeable.
  • the lid core itself can again composed of several individual cores to form a lid core be, each individual core formed gas-impermeable is, and wherein the individual cores at least in the area the feeder must be tightly connected.
  • This Lid core or the lid cores make it possible, according to Filling the mold with metal on the in the lid core attached feeders to exert pressure by means of compressed gas, to be an improved finer and denser in this way Microstructure of the casting produced at the same time lower feeder volume - pressure volume - during the To achieve solidification.
  • the lid core through an appropriate choice of the molding material and to design the binder so that it can withstand a pressure withstands up to 1 bar.
  • Process are only low pressures below up to 1 bar required to achieve the desired density and fine grain to achieve the structure.
  • the print mask that is on the lid core to make one Cavity is provided for pressurization can can also be used in a further development of the invention due to the thermal influence of the molten metal to vacuum the molding sand and the core sand. It is therefore designed so that immediately after solidification of the molten metal and termination of the pressurization the pressure gasses a negative pressure to that of the Print mask covered cavity can be created.
  • the print mask is provided with a further connection to be provided, which can be connected to a suction device.
  • An advantageous embodiment of the seal of the lid core consists of using a core size as a dispersion Apply diving or spraying.
  • the surface treatment with a core size also causes an improved Strength of the lid core.
  • Core sizes are fundamental for the equipment of sand cores for the production of Cast iron castings to achieve smoother and non-porous Known surfaces.
  • refractory fillers for the equipment of a lid core according to the invention, um Making these gas-impermeable will become core sizes based on a dispersion of refractory fillers in provided an organic solvent. These core sizes can also contain graphite. As refractory fillers come for example silicate refractories, such as zirconium silicate, magnesium and / or aluminum silicate in question. In addition, iron oxide can also be used as refractory filler can be contained in the core size. The core sizes also contain minor ones Amounts up to 1% by weight of a synthetic resin.
  • Possible core sizes are the dispersions explained above, however, other material compositions are also can be used which has a gas impermeable surface of the sand cores cause.
  • the support shells which preferably consist of one durable material, for example metal, serve to support the pressure from the outside of the mold during of casting and pressurization in the critical first solidification phase of the molten metal in the casting mold.
  • the casting mold according to the invention enables a new and economical Process for making castings from Light metals by gravity casting, especially also of such complicated parts as cylinder heads and cylinder blocks of internal combustion engines with high quality castings using sand molds for both the outer shape for the cores as well.
  • the molten metal in the feeder is pressurized it, a dense fine structure evenly throughout to produce cast part, so that on the one hand the advantages of the lost forms based on sand can and on the other hand the high quality is achieved like otherwise it can only be achieved with castings in permanent mold casting.
  • Fig. 1 is a mold 1 in cross section for a simple rotationally symmetrical casting with a mold cavity 2 shown.
  • Form 1 is a lost form with outer mold parts 3.1, 3.2 and a core 4 used and provided with a lid core 5, the feeder 6 for Has formation of the pressure mass.
  • the outer mold parts 3.1 and 3.2 are put together in the parting lines 7, likewise
  • the core 4 can be composed of several parts to form a core package his. The number and subdivisions of the outer mold parts and the cores 7 or core packages produced according to the shape of the casting to be cast.
  • the lid core 5 can also consist of several Core parts are put together and one or have several feeders 6.
  • a gas pressure P is exerted.
  • This pressure P can be up to to be 1 bar.
  • a pressure mask 11 is placed in a sealed manner on the cover core 5.
  • the print mask 11 has a connection 12 for the compressed air supply.
  • Cover core 5 is usually microporous and therefore air-permeable.
  • the lid core 5 In order to exert pressure via the feeder 6 To allow compressed air to the molten metal melt, is the lid core 5 at least on its surface in the coverage area through the pressure mask 11 by means of a Core size coated and thus in the coated area gas impermeable. This seal the surface of the lid core 5 can, for example, by immersing the lid core 5 in a core size.
  • the core size for example, based on a refractory dispersion Fillers in an organic solvent, such as Zirconium silicate and carbon, small amounts of synthetic resin and isoropanol, denatured with acetone and some water containing, the surface of the lid core 5 becomes so dense and made stable that the lid core 5 is airtight and that, as shown schematically in Fig. 2, via the print mask withstands the additional pressure P applied.
  • an organic solvent such as Zirconium silicate and carbon
  • lid core 5 is composed of several parts is, each part is assembled before using a Sealing core sizing externally.
  • the core size applied to the lid core must be in front dry and harden using the lid core.
  • Applying the pressure P to the cast part by means of the print mask 11 placed on the mold is done in this way long until the solidification process of the light metal melt comes to an end, d. H. to a temperature below 500 ° C is achieved. This time depends on the size of the Workpiece that is manufactured, for example in a Cylinder block with a casting weight of approx. 20 to 22 kg for internal combustion engines approx. 1.5 minutes.
  • Fig. 3 is the application of the invention to the manufacture of a crankcase for internal combustion engines in exploded view of the mold parts required for this shown.
  • the outer mold is hereby formed by the upper mold block 3.4, the side Moldings 3.5 and the lower mold parts 3.6, which in turn can be composed of individual core parts, depending on the configuration.
  • the core block 4.1 also the crankcase core block is again made up of individual core parts composed.
  • the upper end of the form is the Lid core 5. All mold parts and the core block 4.1 and the lid core 5 are based on sand as lost Shape.
  • the lid core 5 can be a additional part 13, namely a cylinder liner, included, which remains in the cast casting later.
  • the lid core 5 contains at least one feeder 6 for the pressure mass and is further on the top with the Print mask 11 can be covered.
  • the print mask 11 is sealed placed on the lid core 5 and so over the lid core 5 formed cavity 14 can then by means the compressed air supplied via connection 12 Pressure are applied, so that additionally on the molten metal a pressure on the molten metal in the feeder area can be exercised in the form until it solidifies.
  • the lid core 5 can also be on the opposite Side of the crankcase so that the shape is 180 ° is rotated.
  • support shells 16 can be provided be that act on the outer mold parts 3.4, 3.5, 3.6. These support shells 16 can be removed before the cast mold after solidification, for example of can be folded away from the pouring station.
  • Fig. 4 the lost shape is schematically based of sand, as described in Fig. 3 for a crankcase, in the assembled state schematized in section shown.
  • the arrow 17 is the direction in which the Ejector after the support shells have been moved sideways 16 works.
  • the cover core 5 is also on here its surface coated with a core size and treated so that it is airtight and sealed the application of a pressure of up to 1 bar by means of the Print mask 11 is enabled.
  • FIG. 5 shows a further development of the invention, with a further suction bell 19 on the pressure mask 11 Distance is applied so that this second suction bell also covers the area of the outer mold parts in the upper area, so that all escaping from the form, evolving from the heat of smoke under the Suction bell 19 are sucked off via the connecting piece 20 can.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
  • Forging (AREA)

Abstract

PCT No. PCT/EP96/03691 Sec. 371 Date Apr. 25, 1997 Sec. 102(e) Date Apr. 25, 1997 PCT Filed Aug. 22, 1996 PCT Pub. No. WO97/07914 PCT Pub. Date Mar. 6, 1997A method for producing light metal castings, in particular cylinder heads, cylinder blocks and/or crankcases for internal combustion engines, includes a sand mold which forms a mold cavity for the casting. The sand mold includes outer mold parts, at least one core and at least one feeder for forming a riser, wherein the mold is provided with an in-gate for receiving the metal melt and the metal melt is filled into the mold cavity under the effect of gravity. A cover core (5) is fitted onto the mold that is at least in partial regions designed to be impermeable to gas and which contains at least one feeder, and wherein immediately after the filling operation, the feeder filled with metal melt is admitted with a pressure via a pressurized gas.

Description

Die Erfindung bezieht sich auf ein Verfahren zum Herstellen von Gußstücken aus Leichtmetall, insbesondere Zylinderköpfen, Zylinderblöcken und/oder Kurbelgehäusen für Brennkraftmaschinen, mit einer einen Formhohlraum für das Gußstück bildenden verlorenen Form auf der Basis von Sand, die Formaußenteile, mindestens einen Kern und mindestens einen Speiser zur Bildung einer Druckmassel aufweist, wobei die Form mit einem Einguß für die Metallschmelze versehen ist und die Metallschmelze unter Wirkung der Schwerkraft in den Formhohlraum eingefüllt und anschließend mit einem Druckgas beaufschlagt wird.The invention relates to a method for manufacturing of light metal castings, in particular cylinder heads, Cylinder blocks and / or crankcases for internal combustion engines, with a mold cavity for the casting forming lost form based on sand that Outer mold parts, at least one core and at least one Has feeder to form a pressure mass, the Form is provided with a gate for the molten metal and the metal melt under the influence of gravity in the Mold cavity filled and then with a compressed gas is applied.

Es ist bekannt, bei der Herstellung von Gußstücken aus Leichtmetall sowohl verlorene Formen auf der Basis von Sand als auch Dauerformen, sogenannte Kokillen, als auch Formen zu verwenden, die aus Dauerformteilen, sogenannte Halbkokillen, und Sandgußformteilen zusammengesetzt sind. Hierbei liegt für die Serienproduktion von Gußstücken der Hauptvorteil der verlorenen Formen auf der Basis von Sand in der hohen Produktionsgeschwindigkeit der Fertigung der Sandformen einerseits und auch der hohen Produktionsgeschwindigkeit beim Gießen in bezug auf den Gießtakt andererseits, da im Gegensatz zum Kokillenguß das Abkühlen der Kokille bis zum Wiedereinsatz nach jedem Gießvorgang nicht abgewartet werden muß. Da es möglich ist, auch den für die Herstellung der Formaußenteile und Kerne benutzten Sand zu recyceln, werden neuerdings Gußstücke aus Leichtmetall, wie beispielsweise Zylinderköpfe für Brennkraftmaschinen, bei hoher Produktivität in verlorenen Formen auf der Basis von Sand gegossen. Das Gießen der Metallschmelze in die Sandform erfolgt hierbei stets unter Einwirkung der Schwerkraft, meistens im sogenannten Bodenguß. Zur Gefügeverbesserung werden an der Form Speiser eingesetzt, die bei hochwertigen Gußstücken eine der Masse des Gußstückes entsprechende Speisermasse enthalten, die als sogenannte Druckmassel wirkt. Hierbei nimmt man als nachteilig das etwas gröbere Gefüge sowie möglicherweise auftretende Mikroporosität beim Gießen in Sandformen gegenüber dem Gießen in Kokillen in Kauf.It is known in the manufacture of castings Light metal and both lost forms based on sand as well as permanent forms, so-called molds, as well as forms too use, which consist of permanent molded parts, so-called half molds, and sand moldings are assembled. Here lies for the serial production of castings the main advantage of lost molds based on sand in the high production speed the production of the sand molds on the one hand and also the high production speed at Pouring in relation to the pouring stroke on the other hand, as opposed to it for casting the mold, cooling the mold until it is used again do not wait after each pouring process got to. Since it is possible to also manufacture the Recycle mold parts and cores used sand recently castings made of light metal, such as cylinder heads for internal combustion engines, with high productivity poured in lost molds based on sand. The The molten metal is poured into the sand mold always under the influence of gravity, mostly in the so-called Floor pouring. To improve the structure, feeders are used on the mold used in mass castings of high quality of the casting contain appropriate feeder mass, which acts as a so-called pressure mass. This is considered a disadvantage the somewhat coarser structure as well as possibly occurring Microporosity when pouring into sand molds compared to that Pour into molds in purchase.

Bekannt ist des weiteren das Niederdruckgießen von Leichtmetallschmelzen in Kokillen-Dauerformen, wobei durch eine Druckbeaufschlagung der Schmelze in der Kokille mit einem Gas ein feines, dichtes Gefüge erreichbar ist (DE-A-21 33421, DE-A-28 18 442). Eine Druckbeaufschlagung stellt wegen der Festigkeit der Kokille kein Problem dar. Da jedoch die Kokillen eine sehr lange Abkühlungsdauer aufweisen, ist - für hohe Produktionsgeschwindigkeiten - eine sehr große Anzahl sehr teurer Kokillen erforderlich. Bei den häufig auftretenden Änderungen der Gußstücke sind dann eine große Zahl von Kokillen zu ändern; auch neu zu machen.The low pressure casting of light metal melts is also known in permanent molds, with a Pressurizing the melt in the mold with a gas a fine, dense structure can be achieved (DE-A-21 33421, DE-A-28 18 442). Pressurization poses because of the Strength of the mold is not a problem. However, since the mold have a very long cooling time is - for high Production speeds - a very large number very expensive molds required. With the frequently occurring changes the castings are then a large number of molds to change; also make new.

Aus DE-B-11 35 619 ist es bekannt, eine übliche Sandform mit festem Oberkasten und festem Unterkasten zu verwenden, wobei zum Erzeugen von Metallgußstücken mit dichtem Gefüge die aus Oberkasten und Unterkasten zusammengesetzte Sandform mit einer abgedichteten Haube überdeckt wird oder aber Oberkasten und Unterkasten abgedichtet miteinander zu verbinden und auf die freie Kastenoberfläche eine ebenfalls abgedichtete Haube aufzusetzen, nachdem der Formhohlraum mit der Metallschmelze gefüllt worden ist. Der Haubeninnenraum wird mit einem Druckgas beaufschlagt, der dann über die Porosität des Formsandes, insbesondere aber über die freien Schmelzoberflächen im Bereich der Speiser und Steiger verdichtend auf die Schmelze einwirkt. Trotz der Verwendung von Sandformen ist dieses Verfahren zeitaufwendig, da entweder jeweils eine vollständige Haube über die Sandform gesetzt werden muß oder aber beim Zusammensetzen der Sandform Sorge dafür getragen werden muß, daß Unterkasten und Oberkasten sowie die darauf aufgesetzte Druckhaube einwandfrei abgedichtet miteinander verbunden sind.From DE-B-11 35 619 it is known to have a common sand mold fixed top box and fixed bottom box to be used, whereby to produce metal castings with a dense structure Upper box and lower box composite sand mold with one sealed hood is covered or top box and the sub-box sealed to connect with each other and on the free box surface also a sealed hood after the mold cavity with the molten metal has been filled. The interior of the hood is pressurized applied, which then about the porosity of the molding sand, but especially about the free melt surfaces in the area the feeder and riser condensing onto the melt acts. Despite the use of sand molds, this procedure is time consuming since either complete each Hood must be placed over the sand mold or when putting it together the sand form must be taken care of that lower box and upper box as well as the ones placed on them Pressure hood connected to each other in a perfectly sealed manner are.

Aus US-A-2 960 736 ist es zur Lösung der Abdichtungsprobleme bekannt, auf die Speiseröffnung eine Druckhaube aufzusetzen, die mit einem Dichtkragen versehen ist, der in die Schmelze im Speiser eintaucht. Der Nachteil dieses Systems besteht unter anderem darin, daß zum Zwecke der Abdichtung im Endteil des Speisers unabhängig von der Größe der zu gießenden Gußstücke eine verhältnismäßig große Schmelzoberfläche vorhanden sein muß, so daß nach dem Abtrennen der Speiser vom fertigen Gußstück auch eine dementsprechend große Materialmenge wieder aufgeschmolzen werden muß.From US-A-2 960 736 it is used to solve the sealing problems known to put a pressure hood on the feed opening, which is provided with a sealing collar that goes into the melt immersed in the feeder. The disadvantage of this system is below other in that for the purpose of sealing in the end part of the feeder regardless of the size of the castings to be cast a relatively large enamel surface is available must be so that after separating the feeder from the finished Cast a correspondingly large amount of material again must be melted.

Aus JP-A-61 052 978 ist ein Sandgußverfahren bekannt, bei dem die Metallschmelze unter Schwerkraft in die Sandform eingefüllt und anschließend mit einem Druckgas beaufschlagt wird. Um die Druckgasbeaufschlagung durchführen zu können, ist als Speiser ein Formteil aus temperaturwiderstandsfähigem Material auf der Basis von Aluminium-Aluminiumoxid-Siliziumoxid-Eisenoxid aufgesetzt. Dieser Speiser wird von einer aus Metall hergestellten, in die Sandform zusätzlich zum Speiserformteil eingeformten Druckkammer umschlossen. Diese Druckkammer steht mit einer Druckgasversorgung in Verbindung. Beim Ausformen des erkalteten Gußstücks muß das Speiserformteil und die Druckkammer zunächst aus der Sandform entfernt werden, bevor diese vollständig zerlegt und der Sand gegebenenfalls wieder aufgearbeitet werden kann.From JP-A-61 052 978 a sand casting process is known in which the molten metal is poured into the sand mold under gravity and then pressurized with a pressurized gas. To be able to carry out the pressurized gas application, is as A molded part made of temperature-resistant material based on aluminum-alumina-silica-iron oxide put on. This feeder is made of metal produced, in the sand mold in addition to the molded food part molded pressure chamber enclosed. This pressure chamber is connected to a compressed gas supply. At the The molded molded part must be shaped from the cooled casting and the pressure chamber is first removed from the sand mold, before it is completely disassembled and the sand if necessary can be worked up again.

Der Erfindung liegt die Aufgabe zugrunde, das Gießen von Gußstücken aus Leichtmetall unter Einwirkung von Schwerkraft und in verlorenen Formen auf der Basis von Sand bezüglich der Qualität des hergestellten Gußstückes insbesondere in bezug auf ein besonders dichtes und feinkörniges Gefüge unter Vermeidung von Mikroporosität zu verbessern sowie das Volumen der in Form einer Druckmassel anfallenden Speisermaterials zu reduzieren. Leichtmetall im Sinne der Erfindung umfaßt insbesondere Aluminium und Aluminiumlegierungen.The invention has for its object the casting of castings made of light metal under the influence of gravity and in lost forms based on sand regarding the Quality of the casting produced, especially in relation to a particularly dense and fine-grained structure with avoidance of improving microporosity as well as volume the feed material in the form of a pressure mass to reduce. Light metal in the sense of the invention includes in particular Aluminum and aluminum alloys.

Die Erfindung löst die gestellte Aufgabe in bezug auf die Verfahrensweise dadurch, daß auf die Form ein Deckelkern auf Sandbasis aufgelegt wird, der zumindest einen Speiser enthält und der zumindest in den mit Druckgas beaufschlagbaren Bereichen gasundurchlässig ausgebildet ist und daß unmittelbar nach Beendigung des Füllvorgangs der mit Metallschmelze gefüllte Speiser über das Druckgas mit einem Druck beaufschlagt wird.The invention achieves the stated object in relation to the Procedure in that a lid core on the mold Sand base is placed, which contains at least one feeder and at least in the areas that can be pressurized with compressed gas is designed gas-impermeable and that immediately after the filling process, the one filled with molten metal Feeder pressurized with the compressed gas becomes.

Mit der erfindungsgemäßen Verfahrensweise ist es möglich, auch bei verlorenen Formen aus Sand das Gefüge der erstarrenden Metallschmelze durch eine zusätzliche Druckgasbeaufschlagung über die Druckmasseln zu verbessern, zu verdichten und zu verfeinern, da durch die Anordnung eines luftundurchlässigen Deckelkerns eine unmittelbare Möglichkeit für die Druckgaszufuhr gegeben ist. Gleichzeitig kann das Volumen bzw. die Masse der Druckmassel gegenüber den herkömmlichen Gießverfahren mit verlorener Form um bis zur Hälfte verringert werden, so daß eine hohe Einsparung an Umlaufmaterial erzielt werden kann. Der Begriff "gasundurchlässig" im Sinne der vorliegenden Erfindung umfaßt neben einer Gasundurchlässigkeit im Wortsinne auch noch eine Gasdurchlässigkeit mit hohem Durchflußwiderstand, die bei einer Druckgasbeaufschlagung den gewünschten Druckaufbau oberhalb der Schmelze bei vertretbaren geringen Leckverlusten gewährleistet.With the procedure according to the invention it is possible even with lost forms made of sand, the structure of the solidifying Molten metal through additional pressurized gas to improve, condense and refine it because of the arrangement of an airtight Lid core an immediate possibility for the supply of compressed gas given is. At the same time, the volume or Mass of the pressure mass compared to the conventional casting process can be reduced by up to half if the shape is lost, so that a high saving of circulating material can be achieved can. The term "gas impermeable" in the sense of the present In addition to a gas impermeability in the invention Word sense also a gas permeability with high flow resistance, the desired when pressurized with gas Pressure build-up above the melt at a reasonable level ensures low leakage losses.

Vorteilhafte Weiterbildungen des erfindungsgemäßen Verfahrens sind in den Ansprüchen 2 bis 8 angegeben. In bevorzugter Ausführung des erfindungsgemäßen Verfahrens ist vorgesehen, daß die Druckbeaufschlagung der Metallschmelze im Speiser während der ersten kritischen Erstarrungsphase der Metallschmelze ausgeführt wird, d. h. während die Metallschmelze noch heiß ist, so daß durch den ausgeübten Druck eine entsprechende Beeinflussung der noch fließfähigen Schmelze im gesamten Formraum möglich ist. Diese erste kritische Erstarrungsphase geht bis etwa zu einer Abkühlungstemperatur der Leichtmetallschmelze von 500°C, unterhalb dieser Temperatur hat die Druckbeaufschlagung nur noch begrenzte Wirkung (Ansprüche 5 und 6).Advantageous further developments of the method according to the invention are given in claims 2 to 8. In a preferred version the method according to the invention provides that the pressurization of the molten metal in the feeder during the first critical solidification phase of the molten metal is executed, d. H. while the molten metal is still hot is, so that a corresponding influence by the pressure exerted the still flowable melt in the entire molding space is possible. This first critical solidification phase goes up to a cooling temperature of the light metal melt of 500 ° C, below this temperature Pressurization only limited effect (claims 5 and 6).

Um in einfacher Weise eine erfindungsgemäße Druckbeaufschlagung der Metallschmelze im Speiser zu dem Zeitpunkt zu erreichen, in dem der Einfüllvorgang beendet, die eingefüllte Metallschmelze jedoch noch nicht erstarrt ist, wird vorgeschlagen, oberhalb des Speisers und des den Speiser enthaltenden Deckelkerns einen Hohlraum abzuteilen, diesen abzudichten und dann mit einem Anschluß für die Beaufschlagung von Druckluft zu versehen (Anspruch 7). Nachdem die Druckbeaufschlagung des Speisers beendet ist, kann dieser abgeteilte Hohlraum in einem weiteren Verfahrensschritt dazu benutzt werden, um dann an diesen Raum oberhalb des Speisers einen Unterdruck anzulegen und dabei gleichzeitig die beim heißen Gießen, insbesondere aus den Formen entweichenden Gase abzusaugen (Anspruch 8).To a pressurization according to the invention in a simple manner to reach the molten metal in the feeder at the time in which the filling process ends, the filled metal melt but has not yet solidified, it is proposed above the feeder and the one containing the feeder To divide the core of the lid, to seal it and then with a connection for the admission of compressed air to be provided (claim 7). After pressurizing the Feeder is finished, this divided cavity in one further process step can be used to then apply a vacuum to this space above the feeder and at the same time the hot pouring, especially to extract gases escaping from the molds (claim 8th).

Gemäß der Erfindung wird ferner eine (verlorene) Gießform mit den Merkmalen des Oberbegriffs des Anspruchs 9 zur Durchführung des erfindungsgemäßen Verfahrens vorgeschlagen, die gekennzeichnet ist durch wenigstens einen einen Speiser enthaltenden Deckelkern auf Sandbasis, auf den eine den Speiserbereich abdichtende Druckmaske aufsetzbar ist, und wobei der Deckelkern zumindest im Anlagebereich der Druckmaske gasundurchlässig ausgebildet ist. According to the invention, a (lost) mold is also used the features of the preamble of claim 9 for implementation proposed the method according to the invention, the marked is by at least one containing a feeder Sand-based lid core, on one of which the dining area sealing pressure mask can be placed, and wherein the Cover core gas-impermeable at least in the contact area of the pressure mask is trained.

Um eine einwandfreie Druckbeaufschlagung auch bei Ausbildung des Deckelkerns auf der Basis von Sand zu erzielen, wird in Weiterbildung der erfindungsgemäßen Form vorgeschlagen, daß der den Speiser enthaltende, auf der Basis von Sand gefertigte Deckelkern durch eine auf seine Oberfläche zumindest im Anlagebreich für die Druckmaske aufgebrachte Kernschlichte gasundurchlässig ausgebildet ist. Der Deckelkern selbst kann wiederum aus mehreren Einzelkernen zu einem Deckelkern zusammengesetzt sein, wobei jeder Einzelkern gasundurchlässig ausgebildet ist, und wobei die Einzelkerne zumindest im Bereich der Speiser dicht miteinander verbunden sein müssen. Dieser Deckelkern bzw. die Deckelkerne ermöglichen es, nach der Befüllung der Gießform mit Metall auf die in den Deckelkern angebrachten Speiser einen Druck auszuüben mittels Druckgas, um auf diese Weise eine verbesserte feinere und dichtere Gefügebildung des hergestellten Gußstückes bei gleichzeitig geringerem Speiservolumen - Druckmasselvolumen - während der Erstarrung zu erzielen.To ensure perfect pressurization even during training of the lid core on the basis of sand proposed in a development of the form according to the invention, that the one containing the feeder was made on the basis of sand Cover core by one on its surface at least Core coating applied in the area of the print mask is designed to be gas-impermeable. The lid core itself can again composed of several individual cores to form a lid core be, each individual core formed gas-impermeable is, and wherein the individual cores at least in the area the feeder must be tightly connected. This Lid core or the lid cores make it possible, according to Filling the mold with metal on the in the lid core attached feeders to exert pressure by means of compressed gas, to be an improved finer and denser in this way Microstructure of the casting produced at the same time lower feeder volume - pressure volume - during the To achieve solidification.

Nach einer weiteren vorteilhaften Ausgestaltung ist vorgesehen, den Deckelkern durch eine entsprechende Wahl des Formstoffs und des Binders so zu gestalten, daß er einem Druck von bis zu 1 bar standhält. Zur Ausübung des erfindungsgemäßen Verfahrens sind nur geringe Drücke unterhalb bis zu 1 bar erforderlich, um die gewünschte Dichte und Feinkörnigkeit des Gefüges zu erzielen. According to a further advantageous embodiment, the lid core through an appropriate choice of the molding material and to design the binder so that it can withstand a pressure withstands up to 1 bar. To exercise the invention Process are only low pressures below up to 1 bar required to achieve the desired density and fine grain to achieve the structure.

Die Druckmaske, die auf den Deckelkern zum Herstellen eines Holraumes für die Druckbeaufschlagung vorgesehen ist, kann auch in Weiterbildung der Erfindung dazu benutzt werden, den durch die thermische Einwirkung der Metallschmelze auf den Formsand und den Kernsand entstehenden Rauch abzusaugen. Sie ist deshalb so gestaltet, daß unmittelbar nach der Erstarrung der Metallschmelze und Beendigung der Druckbeaufschlagung der Druckmasseln ein Unterdruck an den von der Druckmaske abgedeckten Hohlraum angelegt werden kann. Hierzu ist vorgesehen, die Druckmaske mit einem weiteren Anschluß zu versehen, der an eine Absaugvorrichtung anschließbar ist.The print mask that is on the lid core to make one Cavity is provided for pressurization can can also be used in a further development of the invention due to the thermal influence of the molten metal to vacuum the molding sand and the core sand. It is therefore designed so that immediately after solidification of the molten metal and termination of the pressurization the pressure gasses a negative pressure to that of the Print mask covered cavity can be created. For this the print mask is provided with a further connection to be provided, which can be connected to a suction device.

Eine vorteilhafte Ausgestaltung der Abdichtung des Deckelkerns besteht darin, eine Kernschlichte als Dispersion mittels Tauchen oder Ansprühen aufzubringen. Die Oberflächenbehandlung mit einer Kernschlichte bewirkt auch eine verbesserte Festigkeit des Deckelkerns. Kernschlichten sind grundsätzlich für die Ausrüstung von Sandkernen zur Herstellung von Gußstücken aus Grauguß zum Erzielen glatter und porenfreier Oberflächen bekannt.An advantageous embodiment of the seal of the lid core consists of using a core size as a dispersion Apply diving or spraying. The surface treatment with a core size also causes an improved Strength of the lid core. Core sizes are fundamental for the equipment of sand cores for the production of Cast iron castings to achieve smoother and non-porous Known surfaces.

Für die erfindungsgemäße Ausrüstung eines Deckelkerns, um diesen gasundurchlässig auszubilden, werden Kernschlichten auf der Basis einer Dispersion feuerfester Füllstoffe in einem organischen Lösungsmittel vorgesehen. Diese Kernschlichten können auch zusätzlich Graphit enthalten. Als feuerfeste Füllstoffe kommen beispielsweise Silikat-Feuerfeststoffe, wie Zirkon-Silikat, Magnesium- und/oder Aluminium-Silikat in Frage. Zusätzlich kann auch Eisenoxyd als feuerfester Füllstoff in der Kernschlichte enthalten sein. Darüber hinaus enthalten die Kernschlichten auch geringe Mengen bis zu 1 Gew.-% eines Kunstharzes.For the equipment of a lid core according to the invention, um Making these gas-impermeable will become core sizes based on a dispersion of refractory fillers in provided an organic solvent. These core sizes can also contain graphite. As refractory fillers come for example silicate refractories, such as zirconium silicate, magnesium and / or aluminum silicate in question. In addition, iron oxide can also be used as refractory filler can be contained in the core size. The core sizes also contain minor ones Amounts up to 1% by weight of a synthetic resin.

Mögliche Kernschlichten sind die vorangehend erläuterten Dispersionen, jedoch sind auch andere Materialzusammensetzungen einsetzbar, die eine gasundurchlässige Oberfläche der Sandkerne bewirken. Possible core sizes are the dispersions explained above, however, other material compositions are also can be used which has a gas impermeable surface of the sand cores cause.

Um die Gefügeausbildung in der erfinderischen Form auf Basis von Sand für Leichtmetallgußstücke weiter zu verbessern, wird vorgeschlagen, den Formaußenteilen aus Sand, zumindest teilweise umfassende auf die Form zu und weg bewegbare Stützschalen zuzuordnen. Die Stützschalen, die vorzugsweise aus einem dauerhaften Material, beispielsweise Metall bestehen können, dienen der Druckabstützung von außen auf die Gießform während des Gießens und der Druckbeaufschlagung in der kritischen ersten Erstarrungsphase der Metallschmelze in der Gießform.Based on the microstructure in the inventive form of sand for light metal castings will continue to improve suggested the mold outer parts made of sand, at least partially comprehensive support shells that can be moved towards and away from the mold assign. The support shells, which preferably consist of one durable material, for example metal, serve to support the pressure from the outside of the mold during of casting and pressurization in the critical first solidification phase of the molten metal in the casting mold.

Die erfindungsgemäße Gießform ermöglicht ein neues und wirtschaftliches Verfahren zum Herstellen von Gußstücken aus Leichtmetallen durch Schwerkraftgießen, insbesondere auch von so komplizierten Teilen, wie Zylinderköpfen und Zylinderblöcken von Brennkraftmaschinen mit hoher Qualität des Gusses unter Verwendung von sandformen sowohl für die Außenform als auch für die Kerne. Mittels der unmittelbar nach Beendigung des Gießvorganges zusätzlich auf das Gußstück über die Metallschmelze im Speiser ausgeübten Druckbeaufschlagung gelingt es, ein dichtes feines Gefüge gleichmäßig überall im gegossenen Teil zu erzeugen, so daß einerseits die Vorteile der verlorenen Formen auf der Basis von Sand genutzt werden können und andererseits die hohe Qualität erreicht wird, wie sie sonst nur bei Gußstücken im Kokillenguß erzielbar ist.The casting mold according to the invention enables a new and economical Process for making castings from Light metals by gravity casting, especially also of such complicated parts as cylinder heads and cylinder blocks of internal combustion engines with high quality castings using sand molds for both the outer shape for the cores as well. By means of immediately after termination of the casting process in addition to the casting on the The molten metal in the feeder is pressurized it, a dense fine structure evenly throughout to produce cast part, so that on the one hand the advantages of the lost forms based on sand can and on the other hand the high quality is achieved like otherwise it can only be achieved with castings in permanent mold casting.

Die Erfindung wird anhand schematischer Zeichnungen von Ausführungsbeispielen näher erläutert. Es zeigen

Fig. 1
schematisch die Darstellung einer Gießform,
Fig. 2
die Ausrüstung der Gießform gem. Fig. 1 mit einer Druckmaske,
Fig. 3
eine schematisierte Explosionsdarstellung einer Gießform in Seitenansicht für ein Kurbelgehäuse,
Fig. 4
eine schematisierte Darstellung der Gießform gem. Fig. 3 in zusammengebautem Zustand,
Fig. 5
die Darstellung gem. Fig. 1 mit zusätz licher Glocke für die Absaugung.
The invention is explained in more detail with reference to schematic drawings of exemplary embodiments. Show it
Fig. 1
schematic representation of a casting mold,
Fig. 2
the equipment of the casting mold acc. 1 with a print mask,
Fig. 3
2 shows a schematic exploded view of a casting mold in side view for a crankcase,
Fig. 4
a schematic representation of the mold according to. 3 in the assembled state,
Fig. 5
the representation acc. Fig. 1 with additional bell bell for suction.

In Fig. 1 ist im Querschnitt eine Gießform 1 für ein einfaches rotationssymmetrisches Gußstück mit einem Formhohlraum 2 dargestellt. Die Form 1 ist als verlorene Form mit Formaußenteilen 3.1, 3.2 sowie einem eingesetzten Kern 4 ausgebildet und mit einem Deckelkern 5 versehen, der Speiser 6 zur Bildung der Druckmassel aufweist. Die Formaußenteile 3.1 und 3.2 sind in den Teilungsfugen 7 zusammengefügt, ebenso kann der Kern 4 aus mehreren Teilen zu einem Kernpaket zusammengesetzt sein. Die Anzahl und Unterteilungen der Formaußenteile und der hergestellten Kerne 7 oder Kernpakete richtet sich nach der jeweils zu gießenden Gestalt des Gußstückes. Des weiteren ist ein Einguß 8 für die Metallschmelze an der Gießform 1 ausgebildet. Auch der Deckelkern 5 kann aus mehreren Kernteilen zusammengesetzt werden und einen oder mehrere Speiser 6 aufweisen.In Fig. 1 is a mold 1 in cross section for a simple rotationally symmetrical casting with a mold cavity 2 shown. Form 1 is a lost form with outer mold parts 3.1, 3.2 and a core 4 used and provided with a lid core 5, the feeder 6 for Has formation of the pressure mass. The outer mold parts 3.1 and 3.2 are put together in the parting lines 7, likewise The core 4 can be composed of several parts to form a core package his. The number and subdivisions of the outer mold parts and the cores 7 or core packages produced according to the shape of the casting to be cast. Furthermore, a gate 8 for the molten metal on the Mold 1 formed. The lid core 5 can also consist of several Core parts are put together and one or have several feeders 6.

In Fig. 2 ist die Form 1 nach dem Eingießen der Metallschmelze und dem Ausfüllen des Formhohlraumes zum Herstellen eines Gußstückes 9 dargestellt, wobei in den Speisern des Deckelkerns 5 die Druckmasseln 10 vorhanden sind.2 is the shape 1 after pouring the molten metal and filling the mold cavity to create a Casting 9 shown, being in the feeders of the lid core 5 the pressure masses 10 are present.

Um nach dem Befüllen des Formhohlraumes mit der Metallschmelze eine Verdichtung und Vergleichmäßigung des Gefüges und Vermeidung von Mikroporosität zu erreichen, wird über die Speiser 6 auf die die Druckmassel 10 bildende Metallschmelze ein Gasdruck P ausgeübt. Dieser Druck P kann bis zu 1 bar betragen.In order to fill the mold cavity with the molten metal a densification and homogenization of the structure and to avoid microporosity is about the feeder 6 on the molten metal forming the pressure mass 10 a gas pressure P is exerted. This pressure P can be up to to be 1 bar.

Um diesen Druck über die Speiser 6 auf die Metallschmelze im Formhohlraum bis zum Erstarren ausüben zu können, ist auf den Deckelkern 5 eine Druckmaske 11 abgedichtet aufgesetzt. Die Druckmaske 11 verfügt über einen Anschluß 12 für die Druckluftzufuhr.To this pressure on the feeder 6 on the molten metal to be able to exercise in the mold cavity until it solidifies a pressure mask 11 is placed in a sealed manner on the cover core 5. The print mask 11 has a connection 12 for the compressed air supply.

Der auf der Basis von Sand in bekannter Weise hergestellte Deckelkern 5 ist üblicherweise mikroporös und damit luftdurchlässig. Um die Druckausübung über die Speiser 6 mittels Druckluft auf die noch flüssige Metallschmelze zu ermöglichen, ist der Deckelkern 5 auf seiner Oberfläche zumindest im Abdeckungsbereich durch die Druckmaske 11 mittels einer Kernschlichte beschichtet und somit im beschichteten Bereich gasundurchlässig. Diese Abdichtung der Oberfläche des Deckelkerns 5 kann beispielsweise durch Tauchen des Deckelkerns 5 in eine Kernschlichte erfolgen. Mit Hilfe der Kernschlichte, beispielsweise auf der Basis einer Dispersion feuerfester Füllstoffe in einem organischen Lösungsmittel, wie beispielsweise Zirkonsilikat und Kohlenstoff, geringe Mengen Kunstharz und Isoropanol, vergällt mit Aceton und etwas Wasser enthaltend, wird die Oberfläche des Deckelkerns 5 so dicht und stabil gemacht, daß der Deckelkern 5 luftdicht ist und dem, wie in Fig. 2 schematisch dargestellt, über die Druckmaske ausgeübten zusätzlichen Druck P standhält.The one based on sand in a known way Cover core 5 is usually microporous and therefore air-permeable. In order to exert pressure via the feeder 6 To allow compressed air to the molten metal melt, is the lid core 5 at least on its surface in the coverage area through the pressure mask 11 by means of a Core size coated and thus in the coated area gas impermeable. This seal the surface of the lid core 5 can, for example, by immersing the lid core 5 in a core size. With the help of the core size, for example, based on a refractory dispersion Fillers in an organic solvent, such as Zirconium silicate and carbon, small amounts of synthetic resin and isoropanol, denatured with acetone and some water containing, the surface of the lid core 5 becomes so dense and made stable that the lid core 5 is airtight and that, as shown schematically in Fig. 2, via the print mask withstands the additional pressure P applied.

Es ist im wesentlichen nur erforderlich, den Deckelkern 5 in all den Bereichen durch Beschichtung abzudichten und luftdicht zu machen, die mit der Druckluft in Berührung kommen. Ein wirtschaftliches Verfahren hingegen ist jedoch, den Deckelkern in seiner Gänze in eine entsprechende Kernschlichte zu tauchen, die nicht nur eine entsprechende Abdichtwirkung an der Oberfläche des Deckelkerns sondern auch eine erhöhte Festigkeit bewirkt.It is essentially only necessary to cover the core 5 sealing in all areas by coating and to make it airtight, in contact with the compressed air come. However, an economical process is the lid core in its entirety in a corresponding core size to dive, which not only has an appropriate sealing effect on the surface of the lid core but also causes increased strength.

Falls der Deckelkern 5 aus mehreren Teilen zusammengesetzt ist, ist jedes Teil vor dem Zusammensetzen mittels einer Kernschlichte äußerlich abzudichten. If the lid core 5 is composed of several parts is, each part is assembled before using a Sealing core sizing externally.

Die auf den Deckelkern aufgebracht Kernschlichte muß vor der Verwendung des Deckelkerns trocknen und aushärten.The core size applied to the lid core must be in front dry and harden using the lid core.

Das Aufbringen des Druckes P auf das gegossene Teil mittels der auf die Form aufgesetzten Druckmaske 11 erfolgt so lange, bis der Erstarrungsvorgang der Leichtmetallschmelze zu Ende geht, d. h. bis eine Temperatur unterhalb von 500°C erreicht wird. Diese Zeit richtet sich nach der Größe des Werkstückes, das hergestellt wird, beispielsweise bei einem Zylinderblock mit einem Gießgewicht von ca. 20 bis 22 kg für Brennkraftmaschinen ca. 1,5 Minuten.Applying the pressure P to the cast part by means of the print mask 11 placed on the mold is done in this way long until the solidification process of the light metal melt comes to an end, d. H. to a temperature below 500 ° C is achieved. This time depends on the size of the Workpiece that is manufactured, for example in a Cylinder block with a casting weight of approx. 20 to 22 kg for internal combustion engines approx. 1.5 minutes.

In Fig. 3 ist die Anwendung der Erfindung auf die Herstellung eines Kurbelraumgehäuses für Brennkraftmaschinen in explosionsartiger Darstellung der hierfür benötigten Gießformteile dargestellt. Die äußere Gießform wird hierbei gebildet von dem oberen Formblock 3.4, den seitlichen Formteilen 3.5 sowie den unteren Formteilen 3.6, die wiederum aus einzelnen Kernteilen zusammengesetzt sein können, je nach Konfiguration. Der Kernblock 4.1, auch Kurbelraumkernblock genannt, ist wiederum aus einzelnen Kernteilen zusammengesetzt. Den oberen Abshluß der Form bildet der Deckelkern 5. Alle Gießformteile sowie der Kernblock 4.1 und der Deckelkern 5 sind auf der Basis von Sand als verlorene Form hergestellt. Der Deckelkern 5 kann dabei ein zusätzliches Teil 13, nämlich eine Zylinderlaufbüchse, enthalten, die im gegossenen Gußstück später verbleibt.In Fig. 3 is the application of the invention to the manufacture of a crankcase for internal combustion engines in exploded view of the mold parts required for this shown. The outer mold is hereby formed by the upper mold block 3.4, the side Moldings 3.5 and the lower mold parts 3.6, which in turn can be composed of individual core parts, depending on the configuration. The core block 4.1, also the crankcase core block is again made up of individual core parts composed. The upper end of the form is the Lid core 5. All mold parts and the core block 4.1 and the lid core 5 are based on sand as lost Shape. The lid core 5 can be a additional part 13, namely a cylinder liner, included, which remains in the cast casting later.

Der Deckelkern 5 enthält mindestens einen Speiser 6 für die Druckmassel und ist des weiteren oberseitig mit der Druckmaske 11 abdeckbar. Die Druckmaske 11 wird abgedichtet auf den Deckelkern 5 aufgesetzt und der so über den Deckelkern 5 gebildete abgeschlossene Hohlraum 14 kann dann mittels der über den Anschluß 12 zugeführten Druckluft mit Druck beaufschlagt werden, so daß zusätzlich über die Metallschmelze im Speiserbereich ein Druck auf die Metallschmelze in der Form bis zu ihrer Erstarrung ausgeübt werden kann. The lid core 5 contains at least one feeder 6 for the pressure mass and is further on the top with the Print mask 11 can be covered. The print mask 11 is sealed placed on the lid core 5 and so over the lid core 5 formed cavity 14 can then by means the compressed air supplied via connection 12 Pressure are applied, so that additionally on the molten metal a pressure on the molten metal in the feeder area can be exercised in the form until it solidifies.

Der Deckelkern 5 kann sich auch auf der gegenüberliegenden Seite des Kurbelgehäuses befinden, so daß die Form um 180° gedreht ist.The lid core 5 can also be on the opposite Side of the crankcase so that the shape is 180 ° is rotated.

Um während des Gießens zur Erhöhung der Formgenauigkeit die Gießform zu stabilisieren und noch einen Druck von außen auf die Gießform auszuüben, können Stützschalen 16 vorgesehen sein, die auf die Formaußenteile 3.4, 3.5, 3.6 einwirken. Diese Stützschalen 16 können vor dem Entnehmen der abgegossenen Gießform nach Erstarrung beispielsweise von dem Gießplatz abgeklappt werden.In order to increase the dimensional accuracy during casting Stabilize casting mold and add pressure from the outside to support the casting mold, support shells 16 can be provided be that act on the outer mold parts 3.4, 3.5, 3.6. These support shells 16 can be removed before the cast mold after solidification, for example of can be folded away from the pouring station.

In Fig. 4 ist schematisch die verlorene Form auf der Basis von Sand, wie in Fig. 3 für ein Kurbelraumgehäuse beschrieben, im zusammengebauten Zustand schematisiert im Schnitt dargestellt. Mit dem Pfeil 17 ist die Richtung, in der der Auswerfer nach dem seitlichen Wegbewegen der Stützsschalen 16 arbeitet, bezeichnet. Auch hier ist der Deckelkern 5 an seiner Oberfläche mittels einer Kernschlichte beschichtet und so behandelt, daß er luftdicht abgedichtet ist und damit die Beaufschlagung mit einem Druck bis zu 1 bar mittels der Druckmaske 11 ermöglicht ist.In Fig. 4 the lost shape is schematically based of sand, as described in Fig. 3 for a crankcase, in the assembled state schematized in section shown. The arrow 17 is the direction in which the Ejector after the support shells have been moved sideways 16 works. The cover core 5 is also on here its surface coated with a core size and treated so that it is airtight and sealed the application of a pressure of up to 1 bar by means of the Print mask 11 is enabled.

Nach der Druckbeaufschlagung des Deckelkerns 5, d. h. nach Beendigung derselben, ist es möglich, über einen zweiten Anschluß 18 sich in dem von der Druckmaske 11 gebildeten Hohlraum 14 oberhalb des Deckelkerns 5 angesammelte Rauchgase, die insbesondere durch die Einwirkung der heißen Schmelze aus den Formteilen und Kernen entweichen und ansammeln, abzusaugen.After pressurizing the lid core 5, d. H. to Completing the same, it is possible to go through a second one Port 18 in the formed by the print mask 11 Cavity 14 above the lid core 5 accumulated flue gases, which are called especially by the action of the Escape and collect melt from the molded parts and cores, suck off.

In Fig. 5 ist eine Weiterbildung der Erfindung dargestellt, wobei auf die Druckmaske 11 eine weitere Absaugglocke 19 mit Abstand aufgebracht ist, so daß diese zweite Absaugglocke auch den Bereich der Formaußenteile im oberen Bereich abdeckt, so daß alle von der Form nach oben entweichenden, sich durch die Gießwärme entwickelnden Rauchgase unter der Absaugglocke 19 über den Anschlußstutzen 20 abgesaugt werden können. Es ist möglich, die Druckmaske 11 und die Absaugglocke 19 miteinander über Stützen 21 zu verbinden. Sowohl die Druckmaske 11 als auch die Absaugglocke 19 werden abgedichtet auf den Deckelkern 5 bzw. die Formaußenteile aufgesetzt. Die Anschlüsse 12 und 20 werden an entsprechende Druckgaszufuhr- und Absaugvorrichtungen angeschlossen.5 shows a further development of the invention, with a further suction bell 19 on the pressure mask 11 Distance is applied so that this second suction bell also covers the area of the outer mold parts in the upper area, so that all escaping from the form, evolving from the heat of smoke under the Suction bell 19 are sucked off via the connecting piece 20 can. It is possible to use the pressure mask 11 and the suction bell 19 to connect to each other via supports 21. Both the pressure mask 11 and the suction bell 19 are sealed to the lid core 5 or the outer mold parts put on. Ports 12 and 20 are connected to corresponding ones Pressurized gas supply and suction devices connected.

Claims (15)

  1. A process for manufacturing castings of lightweight metal, in particular cylinder heads, cylinder blocks and/or crankcases for internal combustion engines, with a sand-based lost casting mould forming a mould cavity (2) for the casting, which mould has outer mould parts (3), at least one core (7) and at least one riser (6) for forming a pressure pig, the casting mould being provided with a runner gate (8) for a molten metal and the molten metal being poured into the mould cavity (2) under the action of gravity and then being pressurised, characterised in that a sand-based cover core (5) is laid on the casting mould, which core contains at least one riser (6), which is made impermeable to gas at least in the regions which can be acted upon by compressed gas, and that immediately after the filling operation has ended the riser (6) filled with molten metal is pressurised using the compressed gas.
  2. A process according to Claim 1, characterised in that once the filling operation has ended a feed means for the compressed gas is placed in sealing manner against the partial regions which are made impermeable to gas in order to pressurise the riser (6) filled with molten metal.
  3. A process according to Claim 1 or 2, characterised in that the riser (6) filled with molten metal is pressurised by a compressed gas up to about 1 bar.
  4. A process according to one of Claims 1 to 3, characterised in that the impermeability to gas of the cover core (5) is brought about by applying a core dressing at least to partial regions of the cover core (5).
  5. A process according to one of Claims 1 to 4, characterised in that the pressurisation of the molten metal in the riser (6) is effected during the first critical solidification phase of the molten metal.
  6. A process according to one of Claims 1 to 5, characterised in that once a temperature of the metal poured into the casting mould which is below 500°C is reached, the pressurisation of the molten metal in the riser (6) is terminated.
  7. A process according to one of Claims 1 to 6, characterised in that to pressurise the riser region a cavity (14) located above the cover core (5) and sealed off therefrom is pressurised with the compressed gas.
  8. A process according to one of Claims 1 to 7, characterised in that once the pressurisation at the cavity (14) which can be pressurised has ended a partial vacuum is applied.
  9. A casting mould for manufacturing castings of lightweight metal, in particular cylinder heads, cylinder blocks and/or crankcases for internal combustion engines, with outer mould parts (3), at least one core (4) and at least one riser (6) for forming a pressure pig, which can be connected to a means for pressurising using a pressurised gas, for performing the process according to one of Claims 1 to 8, characterised in that a sand-based cover core (5) containing at least one riser (6) is provided, on which a pressure mask (11) sealing off the riser region can be placed, and that the cover core (5) is made impermeable to gas at least in the contact region of the pressure mask (11).
  10. A casting mould according to Claim 9, characterised in that the sand-based cover core (5) containing the riser (6) is made impermeable to gas by a core dressing applied to its surface at least in the region of contact for the pressure mask (11).
  11. A casting mould according to one of Claims 9 or 10, characterised in that the sand-based cover core (5) withstands a pressure of up to 1 bar when the riser region is pressurised.
  12. A casting mould according to one of Claims 9 to 11, characterised in that the core dressing is applied to the cover core (5) as a dispersion by means of dipping or spraying.
  13. A casting mould according to one of Claims 9 to 12, characterised in that the outer mould parts (3) are allocated supporting shells (16) which at least partially surround them and move towards and away from the mould.
  14. A casting mould according to one of Claims 9 to 13, characterised in that the pressure mask (11) has a connection (18) for extracting gases.
  15. A casting mould according to one of Claims 9 to 14, characterised in that a bell (19) which can be placed hermetically over the pressure mask (11) on the casting mould, at least extending over the cover core (5), with a connection (20) for producing a partial vacuum, is provided.
EP96930074A 1995-08-28 1996-08-22 Method of producing light metal castings and casting mould for carrying out the method Expired - Lifetime EP0793554B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19531551 1995-08-28
DE19531551A DE19531551A1 (en) 1995-08-28 1995-08-28 Process for producing castings from light metal and lost mold based on sand therefor
PCT/EP1996/003691 WO1997007914A1 (en) 1995-08-28 1996-08-22 Method of producing light metal castings and casting mould for carrying out the method

Publications (2)

Publication Number Publication Date
EP0793554A1 EP0793554A1 (en) 1997-09-10
EP0793554B1 true EP0793554B1 (en) 2000-02-23

Family

ID=7770545

Family Applications (1)

Application Number Title Priority Date Filing Date
EP96930074A Expired - Lifetime EP0793554B1 (en) 1995-08-28 1996-08-22 Method of producing light metal castings and casting mould for carrying out the method

Country Status (7)

Country Link
US (1) US5954113A (en)
EP (1) EP0793554B1 (en)
CN (1) CN1164837A (en)
AT (1) ATE189867T1 (en)
DE (2) DE19531551A1 (en)
ES (1) ES2146016T3 (en)
WO (1) WO1997007914A1 (en)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3188279B2 (en) * 1997-03-18 2001-07-16 ゲオルグ フィッチャー ディサ アクツイエセルスカプ Method, pressure supply member and pressure supply system for positive post-feeding of casting
DE19803397A1 (en) * 1998-01-29 1999-08-05 Volkswagen Ag Casting mold for making castings
DE19830025B4 (en) * 1998-07-04 2004-06-17 Audi Ag Process for die casting light alloys
DE10019310C1 (en) * 2000-04-19 2001-10-25 Vaw Mandl & Berger Gmbh Linz Casting mold, comprising outer molded parts and molded material cores inserted therein
EP1153678B1 (en) * 2000-05-10 2006-08-23 Nissin Kogyo Co., Ltd Method of casting and casting machine
CN1130271C (en) * 2000-08-07 2003-12-10 史保萱 Casting technology by squeezing riser head for compensating shrink
ITTO20010287A1 (en) * 2001-03-27 2002-09-27 Teksid Spa CASTING EQUIPMENT FOR THE PRODUCTION OF METALLIC CASTINGS USING "LOST-FOAM" TECHNOLOGY.
JP3592252B2 (en) * 2001-04-05 2004-11-24 日信工業株式会社 Casting method and casting apparatus
US6763876B1 (en) 2001-04-26 2004-07-20 Brunswick Corporation Method and apparatus for casting of metal articles using external pressure
US6957489B2 (en) * 2001-06-23 2005-10-25 Mahle Gmbh Method for producing a light-alloy bearing bush with a rough external surface
FR2841163B1 (en) * 2002-06-21 2005-01-28 Montupet Sa METHOD FOR MOLDING FOUNDRY PARTS, IN PARTICULAR BLOCK-MOTORS, IN LIGHT ALLOY
US6883580B1 (en) 2003-01-27 2005-04-26 Brunswick Corporation Apparatus and improved method for lost foam casting of metal articles using external pressure
JP4150764B2 (en) * 2005-09-15 2008-09-17 政人 五家 Casting method
DE102006030699B4 (en) * 2006-06-30 2014-10-02 Daimler Ag Cast steel piston for internal combustion engines
DE102006053404A1 (en) * 2006-11-10 2008-05-15 Hydro Aluminium Alucast Gmbh Casting mold for casting a casting and use of such a casting mold
CN101254521B (en) * 2007-08-31 2010-09-29 广州驭风旭铝铸件有限公司 Cast form device, foundry method and method for coating cast form with paint
US7814879B2 (en) * 2008-04-23 2010-10-19 Techtronic Outdoor Products Technology Limited Monolithic block and valve train for a four-stroke engine
CN101323015B (en) * 2008-08-28 2010-06-16 南昌航空大学 Rotated mold technique of iron mold using compound punch type pressure heat-preserving casting system
KR101108515B1 (en) * 2010-02-25 2012-01-30 주식회사 동서기공 Molding method using mold assembly
CN102152672B (en) * 2010-11-03 2013-01-16 湖州电力局 Semi-automatic feeding seal die-casting machine
CN102672443B (en) * 2012-04-28 2013-08-14 苏州雅尔塑业科技有限公司 Process for machining molding core
CN102941334B (en) * 2012-11-27 2015-07-01 山东圣泉新材料股份有限公司 Casting pressurizing system and casting pressurizing method
CN103212672B (en) * 2013-03-15 2015-07-22 马钢(集团)控股有限公司 Method for casting low speed diesel engine cylinder cap for large cylinder diameter boat
EP3012045B1 (en) * 2013-06-20 2017-09-06 Hitachi Metals, Ltd. Cast article manufacturing method
US9950363B2 (en) * 2013-09-30 2018-04-24 Hitachi Metals, Ltd. Casting apparatus and method for producing castings using it
CN105364047B (en) * 2015-10-22 2017-05-24 顺德职业技术学院 Gypsum type rapid precision casting method for nonferrous metal
CN106077517B (en) * 2016-07-27 2017-09-26 三鑫重工机械有限公司 A kind of casting method of high-speed steel roll
CN107774914A (en) * 2017-12-12 2018-03-09 重庆乐迪机车车辆配件有限公司 A kind of exothermic riser neck structure of casting
CN112846088A (en) * 2020-12-31 2021-05-28 重庆长江造型材料(集团)股份有限公司 Riser with multiple thermal efficiency and machining method

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6152978A (en) * 1984-08-22 1986-03-15 Daido Steel Co Ltd Casting method
JPH03142056A (en) * 1989-10-28 1991-06-17 Asahi Tec Corp Low-pressure casting device and low-pressure casting device for wheel for vehicle

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
LU34671A1 (en) * 1956-05-30
DE1135619B (en) * 1958-10-25 1962-08-30 Metallgesellschaft Ag Method and device for producing castings in sand molds using pressurized gas
DE2133421C3 (en) * 1971-07-05 1973-12-06 Copal Foundries Ltd., West Bromwich, Staffordshire (Grossbritannien) Device for casting aluminum alloys with preheated, multi-part molds
DE2818442A1 (en) * 1978-04-27 1979-10-31 Dieter Dr Ing Leibfried Low pressure die casting for non-ferrous metals - applying vacuum followed by finishing pressure
JPS59209456A (en) * 1983-05-13 1984-11-28 Hitachi Ltd Production of steel ingot
CH668205A5 (en) * 1986-01-09 1988-12-15 Fischer Ag Georg Treatment of melt during casting in sand mould - with pulsed pressure ensuring movement of whole melt volume to stop dendritic growth
JP2857415B2 (en) * 1989-05-16 1999-02-17 マツダ株式会社 Pressure casting method
JPH03230860A (en) * 1990-02-06 1991-10-14 Mazda Motor Corp Pressurized casting method
RO114880B1 (en) * 1994-01-03 1999-08-30 Dansk Ind Syndikat Casting mould, casting and cooling station of a continuous forming installation

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6152978A (en) * 1984-08-22 1986-03-15 Daido Steel Co Ltd Casting method
JPH03142056A (en) * 1989-10-28 1991-06-17 Asahi Tec Corp Low-pressure casting device and low-pressure casting device for wheel for vehicle

Also Published As

Publication number Publication date
DE59604490D1 (en) 2000-03-30
ES2146016T3 (en) 2000-07-16
WO1997007914A1 (en) 1997-03-06
ATE189867T1 (en) 2000-03-15
EP0793554A1 (en) 1997-09-10
DE19531551A1 (en) 1997-03-06
US5954113A (en) 1999-09-21
CN1164837A (en) 1997-11-12

Similar Documents

Publication Publication Date Title
EP0793554B1 (en) Method of producing light metal castings and casting mould for carrying out the method
EP1268104B1 (en) Method and mould for the counter gravity casting in sand dies with directional solidification
DE60111190T2 (en) METHOD AND DEVICE FOR PRODUCING CAST FOAM BODIES
DE69725315T3 (en) Method of making feeders and other feed and feed elements for molds and composition for making feeders and elements
DE2258461A1 (en) CASTING PROCESS
DE2738635A1 (en) MULTIPLE CASTING FORM
DE3004209C2 (en) Process for compacting powders and metals and their alloys into pre-pressed bodies
DE112014004716T5 (en) Method and casting machine for casting metal parts
EP1786576B1 (en) Method and device for casting molten metal
DE8990036U1 (en) Ladle sleeve with jointly pressed gas-permeable ring
DE2255644A1 (en) CHOCOLATE FOR POURING FLASKS
DE3300701A1 (en) DIE CASTING METHOD AND DEVICE FOR ITS IMPLEMENTATION
DE3015575A1 (en) METHOD FOR PRODUCING AN OBJECT FROM CERAMIC OR METAL MATERIAL BY ISOSTATIC PRESSING
DE10346917B4 (en) Device for casting with lost foam model for improved recycling of sprue metal
DE68903103T2 (en) METHOD FOR FULL MOLDING METALLIC OBJECTS UNDER PRESSURE.
EP1147836B1 (en) Casting mould comprising outer mould parts and cores of moulding material inserted into these parts
DE68924941T2 (en) Counter-gravity casting device and method for casting thin-walled parts.
DE3621334C1 (en) Method and device for the production of metallic mouldings
DE202018102896U1 (en) casting system
DE1076901B (en) Method and device for producing casting molds
DE2926906A1 (en) Sand mould riser liners - filled with gasifying expanded polystyrene for easier handling
WO2005097378A2 (en) Method for the production of moulded parts
DE2133421A1 (en) Gravity die casting appts
DE102004034802B4 (en) Metallic permanent mold for the production of large castings from metal alloys
DE10361535B4 (en) Method for casting molded parts

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19970417

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT DE ES FR GB IT

17Q First examination report despatched

Effective date: 19981012

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT DE ES FR GB IT

REF Corresponds to:

Ref document number: 189867

Country of ref document: AT

Date of ref document: 20000315

Kind code of ref document: T

REF Corresponds to:

Ref document number: 59604490

Country of ref document: DE

Date of ref document: 20000330

ITF It: translation for a ep patent filed

Owner name: BARZANO' E ZANARDO ROMA S.P.A.

ET Fr: translation filed
GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20000525

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2146016

Country of ref document: ES

Kind code of ref document: T3

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

Ref country code: GB

Payment date: 20000807

Year of fee payment: 5

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

Ref country code: ES

Payment date: 20000822

Year of fee payment: 5

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

Ref country code: AT

Payment date: 20000824

Year of fee payment: 5

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

Ref country code: FR

Payment date: 20000831

Year of fee payment: 5

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
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: 20010822

Ref country code: AT

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

Effective date: 20010822

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

Ref country code: ES

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

Effective date: 20010823

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

Effective date: 20010822

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

Ref country code: DE

Payment date: 20020812

Year of fee payment: 7

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

Ref country code: FR

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

Effective date: 20030430

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

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

Ref country code: DE

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

Effective date: 20040302

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20020911

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 NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

Effective date: 20050822

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

Ref country code: FR

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

Effective date: 20010831