EP0974414B1 - Casting mould and a casting process for the production of an engine block - Google Patents

Casting mould and a casting process for the production of an engine block Download PDF

Info

Publication number
EP0974414B1
EP0974414B1 EP99113976A EP99113976A EP0974414B1 EP 0974414 B1 EP0974414 B1 EP 0974414B1 EP 99113976 A EP99113976 A EP 99113976A EP 99113976 A EP99113976 A EP 99113976A EP 0974414 B1 EP0974414 B1 EP 0974414B1
Authority
EP
European Patent Office
Prior art keywords
cylinder
casting
channel
engine block
cooling channel
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
EP99113976A
Other languages
German (de)
French (fr)
Other versions
EP0974414A1 (en
Inventor
Herbert Smetan
Klaus Dr. Lellig
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.)
Nemak Dillingen GmbH
Original Assignee
Hydro Aluminium Alucast 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
Priority claimed from DE1998132718 external-priority patent/DE19832718A1/en
Priority claimed from DE1999125512 external-priority patent/DE19925512B4/en
Application filed by Hydro Aluminium Alucast GmbH filed Critical Hydro Aluminium Alucast GmbH
Priority to DE29924794U priority Critical patent/DE29924794U1/en
Priority to DK99113976T priority patent/DK0974414T3/en
Publication of EP0974414A1 publication Critical patent/EP0974414A1/en
Application granted granted Critical
Publication of EP0974414B1 publication Critical patent/EP0974414B1/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
    • B22C9/10Cores; Manufacture or installation of cores
    • B22C9/105Salt cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/0009Cylinders, pistons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/02Cylinders; Cylinder heads  having cooling means
    • F02F1/10Cylinders; Cylinder heads  having cooling means for liquid cooling
    • F02F1/14Cylinders with means for directing, guiding or distributing liquid stream
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F7/00Casings, e.g. crankcases or frames
    • F02F7/0002Cylinder arrangements
    • F02F7/0007Crankcases of engines with cylinders in line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/02Light metals
    • F05C2201/021Aluminium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2251/00Material properties
    • F05C2251/04Thermal properties
    • F05C2251/042Expansivity

Definitions

  • the invention relates to a casting mold for the production an engine block, which is a between Cylinder recesses extending a cylinder row Cooling channel, wherein between the cylinder recesses a minimum Gußmaterialwanddicke of less than 5 mm is provided, wherein in the mold to form the Cooling channel between the cylinder recesses forming Cores of the mold only at its ends held channel shaped core is arranged.
  • the invention relates to a method for producing a Engine block with at least one cooling channel in one Intermediate wall between adjacent cylinder recesses, wherein the wall thickness formed by casting material less than 5 mm, the engine block by pouring of Casting material is imaged in a mold and wherein in the mold the cores forming the cylinder recesses be inserted.
  • the present invention is based on the object, a Mold to create, on the one hand, the production of tight building engines without the use of sand cores themselves enabling restrictions and, on the other hand ensures high productivity during production.
  • a procedure should be created that with reduced manufacturing costs the production of in their Quality improved engine blocks allows.
  • This task is related to the mold of the beginning specified type solved in that the channel mold core Glass is made.
  • this object is achieved by that in the mold to form the cooling channel between the the cylinder recesses forming cores made of glass existing channel mold core is arranged so that it only on his ends are held.
  • the casting mold according to the invention makes it possible to use a To produce an engine block in which the strength and Service life compared to a known such engine block is increased by the fact that not to form the cooling channel by machining in the solidification structure of Casting material has been intervened.
  • the cross-sectional area of the cooling channel of its ends to a cylinder axis perpendicular crossing Reduce the transverse axis of the cooling channel. With this reduction becomes the decrease of the cylinder intermediate wall to this axis taken into account. With to both sides increasing intermediate wall thickness also increases the Cross-sectional area of the cooling channel, which is advantageous the flow resistance of the channel decreases and the Coolant flow rate increased.
  • the minimum width of the cooling channel in the direction of the Cylinder axes perpendicular crossing channel transverse axis can between 0.5 and 1.5 mm.
  • the channel cross-sectional area is preferably elongate formed and extends parallel to a longitudinal axis to the cylinder axes. While the latitude of the Cooling channel by the strength of the cylinder intermediate wall is limited, the cooling channel in the direction of Cylinder axes increasing the passage cross section to stretch relatively far.
  • the cooling channel can be straight between each other opposite sections of a cylinder bank extend surrounding cooling jacket.
  • a G goformkern from a Soluble in a liquid combustible and / or brittle Material consists, in particular a salt or carbon.
  • a salt core can be left after the casting and solidification of the Remove casting material from the casting by removing it. It is understood that a soluble salt with a Melting point must be selected, which is above the temperature the casting material used is. Leave a carbon core burn out, including, where appropriate, to promote the Combustion oxygen is supplied. It is further conceivable to use a pyrotechnic core material that besides carbon, one added to the carbon Includes oxidizing agent, wherein by the Material composition complete burnout of the Kern's secured, however, an explosive combustion can be avoided.
  • An inventively used brittle glass core can be from a narrow cooling channel, even if the cooling channel inputs not accessible by tools, remove by removing e.g. by ultrasound effect into small pieces smashed, the glass core for this purpose by education can be pretreated by voltages accordingly.
  • the glass core can be pressurized standing water jet to be removed.
  • the mold core at one end at one of the cores for the formation of the cylinder having casting mold part supported is the mold core at one end at one of the cores for the formation of the cylinder having casting mold part supported.
  • the mold part 1 further comprises blocks 4 and 5 with a groove 6 and 7, respectively.
  • a groove 6 and 7 In the groove 6 and 7 is with its ends a salt core 8 used.
  • Each of the grooves 6, 7 is so long that for the salt core 8 is given in each groove an expansion clearance.
  • the blocks form a breakthrough in the cylinder head facing ceiling 11 of the engine block. While fixing the salt core 8 in the grooves 6, 7 adjoin the blocks 4, 5 against another mold part 12, through which a Cylinder surrounding cooling jacket is formed.
  • a cylinder intermediate wall made of cast material formed whose minimum width indicated by the arrows is.
  • Fig. 1 takes the initially constant width of the salt core 8 of his Ends on to a cylinder axis perpendicular crossing transverse axis 14 down and reached a width of 1 mm in this axis, while the outer portions of the salt core in The embodiment have a width of 2.5 mm.
  • the mininmale, by casting material formed wall thickness of the cylinder intermediate wall at 13 is inclusive of minimum channel width 2.5 mm. Not shown are in the engine block einzug devisende gray cast iron bushings, so that the total web width is 5.5 mm.
  • the salt core 8 has a rectangular in cross section, with the long rectangle side of the cross section extends perpendicular to the cylinder axes and in the embodiment shown 4 mm is.
  • the salt core 8 is made of NaCl, which has a melting point above the Temperature of the liquid aluminum casting material used to make the engine block lies. Depending on the casting material, other salts and salt mixtures can be used.
  • the salt core 8 is in the embodiment shown by pressing and then Sintered.
  • the salt core could to its ends with the cooling effect amplified wider than shown.
  • Fig. 3 appear a first cylinder recess 15 of an engine block with a lining 16, a first cylinder intermediate wall 17 and a lining 18 of a next Cylinder recess 19.
  • Graphite plate 26 In the framed sections A and B of the water jacket 22 forming mandrel is 24 shown. In this molded with two thicker end portions 25 a Graphite plate 26. The graphite plate has a between the thicker end portions 25 a Thickness of about 1.2 mm and a height of about 12 mm. Extends with these dimensions it is centered by the thickness of the cylinder intermediate wall 17, in a height directly under the stud bolts 23.
  • the Grapfitplatte 26 is finally removed by burning out. She is under blowing ignited by oxygen and burns out continuously, if continuous oxygen in the blown through its channel burned out. This can help to speed up done from both sides. Deviating from this embodiment, the Graphite material to be mixed with an oxidizing agent that no such support needy burnout allows.
  • the water flow in the engine block is with a certain pressure gradient between the one side of the cylinder bank and the other side provided. This will be through the graphite plate 26 flows through channel generated and thus a removal of heat allows.
  • the method can also be used advantageously, in particular Also for a narrow water flow between the valve holes of a cylinder head.
  • FIGS. 5 and 6 denotes an engine block formed by casting.
  • the by soft hatching in the Cross-section engine block 27 is made of an aluminum alloy.
  • the reference number 28 is a mold part for forming a cylinder surrounding the engine block 27 Cooling jacket called.
  • cylinder liners 29 are through Encapsulated with casting material.
  • the cylinder liners 29 are seated in the mold with their entire inner surface each on a hollow cylindrical Kokillendorn 30 of the mold on.
  • the casting mold which is otherwise not shown, is a sand mold.
  • reference numeral 31 designates a glass core which is located between adjacent ones Cylinder recesses 32 of the engine block 27 of a sand mold part 33rd zuckt to a sand mold part 34.
  • the Sandg tellformmaschine 33, 34 are with the cooling jacket forming sand mold part 28 connected and serve to form openings of the cooling jacket to the cylinder head contact surface of the engine block 1.
  • the laid in an arc glass core is respectively at its ends in the mold part 33 and 34 embedded.
  • the glass material has a thermal expansion coefficient which is slightly below 10 -6 K -1 .
  • the glass transition temperature is 700 ° C.
  • the glass core 31 has a diameter of 1 mm.
  • a core is arranged, as is apparent from Figs. 5 and 6.
  • the glass core 31 is encapsulated, wherein the glass material with withstanding the pouring associated with temperature stress.
  • a short time after pouring the glass core reaches the temperature of the casting material and thus its maximum thermal expansion during the casting process.
  • the glass core now cools in temperature weight along with the casting material, wherein the casting material due to its higher thermal expansion coefficient shrinks more than the glass core 31.
  • This Shrinkage regularly causes the glass core 31 to shatter.
  • the glass core Be suitably pretreated by quenching, blasting, etching and / or scribing, in particular such that a plurality of easily removable fragments is formed.
  • the glass core 31 is laid in the bow so that through the to the cylinder head bearing surface formed through openings a flexible impact tool can be introduced, with the help of which in the event that the glass core in the shrinkage is not or only partially broken, a demoulding takes place.
  • the curved in the embodiment shown Glasaskem could also be straight.
  • an ultrasonic treatment or high-pressure jet treatment of the casting is a very important property for the casting.
  • Salt cores, graphite cores or glass cores may deviate from the one shown Engine block with a cooling channel between the cylinders related examples also on other locations of the engine block are used, e.g. To form channels through which Coolant or oil can be supplied to certain functional parts in the engine.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

The engine block has structured cooling channels in the walls between the cylinders with a reduced cross section where the channel axis intersects the cylinder axes. The cast engine block has a cooling channel in the intermediate cylinder wall with a minimum cast wall thickness of less than or equal to 5 mm. The cooling channel is wholly defined by a skin of the cast material. The cross section surface of the cooling channel is reduced from its end to a cross section surface of the cooling channel axis (14) where it intersects the cylinder axis. The minimum width of the cooling channel at the cross section surface axis at the intersection with the cylinder axis is 0.5-1.5 mm. The mold has channel molding cores (8) at the ends of the cores (2,3) to give the cylinder openings.

Description

Die Erfindung betrifft eine Gießform für die Herstellung eines Motorblocks, der einen sich zwischen Zylinderausnehmungen einer Zylinderreihe erstreckenden Kühlkanal aufweist, wobei zwischen den Zylinderausnehmungen eine minimale Gußmaterialwanddicke von weniger als 5 mm vorgesehen ist, wobei in der Gießform zur Bildung des Kühlkanals zwischen den die Zylinderausnehmungen bildenden Kernen der Gießform ein lediglich an seinen Enden gehalterter Kanalformkern angeordnet ist.Darüber hinaus betrifft die Erfindung ein Verfahren zur Herstellung eines Motorblocks mit wenigstens einem Kühlkanal in einer Zwischenwand zwischen benachbarten Zylinderausnehmungen, wobei die durch Gußmaterial gebildete Wanddicke weniger als 5 mm beträgt, wobei der Motorblock durch Eingießen von Gußmaterial in eine Gießform abgebildet wird und wobei in die Gießform die Zylinderausnehmungen bildende Kerne eingelegt werden.The invention relates to a casting mold for the production an engine block, which is a between Cylinder recesses extending a cylinder row Cooling channel, wherein between the cylinder recesses a minimum Gußmaterialwanddicke of less than 5 mm is provided, wherein in the mold to form the Cooling channel between the cylinder recesses forming Cores of the mold only at its ends held channel shaped core is arranged.In addition The invention relates to a method for producing a Engine block with at least one cooling channel in one Intermediate wall between adjacent cylinder recesses, wherein the wall thickness formed by casting material less than 5 mm, the engine block by pouring of Casting material is imaged in a mold and wherein in the mold the cores forming the cylinder recesses be inserted.

Um die Baulänge eines z.B. aus Aluminium gegossenen Motorblocks möglichst gering zu halten, ist man bestrebt, die Zylinderausnehmungen einer Zylinderreihe eng beieinander anzuordnen, wodurch sich entsprechend dünne Zylinderzwischenwände ergeben. Durch die enger beieinanderliegenden Brennräume und die verminderte Wärmeableitung unterliegen diese verdünnten Zwischenwände, insbesondere an den dem Zylinderkopf zugewandten Ende der Zylinderlauffläche, einer erhöhten thermischen Belastung, die es erforderlich macht, in der Zwischenwand einen Kühlkanal vorzusehen.To keep the length of a e.g. cast aluminum To keep engine blocks as low as possible, one endeavors the cylinder recesses of a cylinder bank close together to arrange, resulting in correspondingly thin Cylinder partitions result. By the narrower adjacent combustion chambers and the diminished Heat dissipation are subject to these dilute partitions, in particular to the cylinder head end facing the Cylinder surface, an increased thermal load, which makes it necessary in the partition one Provide cooling duct.

Es ist bekannt, einen Kühlkanal durch spanabhebende Bearbeitung dadurch zu bilden, daß von der Zylinderkopfanlagefläche des Motorblocks her in den Motorblock eingeschnitten und der Einschnitt wieder verschlossen wird, wobei ein Kühlkanal verbleibt, der sich auf gegenüberliegenden Seiten der Zylinderreihe erstreckende Kühlmantelabschnitte eines die Zylinderreihe umgebenden Kühlmantels verbindet. Alternativ wird der Motorblock zur Bildung eines solchen Kühlkanals seitlich angebohrt, wonach es erforderlich ist, den Bohrungsdurchgang zwischen dem Kühlmantel und der Motorblockaußenseite wieder zu verschließen.It is known to cut a cooling channel by cutting Processing by the fact that of the Cylinder head contact surface of the engine block forth in the Engine block cut in and the incision again is closed, leaving a cooling channel, which is extending on opposite sides of the cylinder bank Cooling jacket sections of a cylinder row surrounding Cooling jacket connects. Alternatively, the engine block is for Forming of such a cooling channel drilled laterally, after which it is necessary to drill the passage between the Cooling jacket and the engine block outside again close.

Neben dem voranstehend erläuterten Stand der Technik sind aus der EP 0 197 365 A2 eine Vorrichtung und ein Verfahren zur gießtechnischen Herstellung eines eng bauenden Zylinderblocks bekannt, bei denen Kühlmäntel um die im gegossenen Motorblock angeordneten Zylinderbohrungen vorgesehen sind, die durch Kühlkanäle zwischen den Zylinderzwischenwänden verbunden sind. Die Kühlkanäle werden durch separate Kerne in der Gießform abgebildet, die in einer Ausführungsform an ihren beiden Enden in den Mantelkern eingepasst sind. Als Material für die Kanalkerne ist in der EP 0 197 365 A2 Zirkonsand vorgeschlagen, weil dieser Sand eine hohe Schüttdichte und damit eine große Festigkeit besitzt. In der Praxis zeigt sich jedoch, daß es bei geringen Querschnitten des Kanalkerns in Folge der bei der Fertigung von Gießkernen unvermeidbar auftretenden Belastungen zu einem Bruch des Kanalgießkerns kommt.In addition to the above-described prior art from EP 0 197 365 A2 a device and a method for the casting production of a tight-fitting Cylinder blocks are known in which cooling jackets around in the cast engine block arranged cylinder bores are provided by the cooling channels between the Cylinder partitions are connected. The cooling channels are represented by separate cores in the mold, which in an embodiment at its two ends in the Mantelkern are fitted. As material for the channel cores is proposed in EP 0 197 365 A2 zirconsand, because This sand has a high bulk density and therefore a large one Has strength. In practice, however, it turns out that it in small cross sections of the channel core in consequence of at the production of foundry cores unavoidably occurring Strains to a fraction of the channel casting core comes.

Schließlich sind aus der US 5 217 059 A auch noch ein Gießkern sowie ein Verfahren zur Bildung einer Wassermantelkammer innerhalb eines gegossenen Zylinderblocks bekannt. Dabei ist vorgesehen, durch eine aus einem geeigneten Feuerfestmaterial hergestellte Platte zwischen zwei Zylinderkammern einen Kühlkanal auszubilden.Finally, from US 5 217 059 A also still a Casting core and a method for forming a Water jacket chamber inside a cast cylinder block known. It is provided by one of a suitable refractory produced plate between two cylinder chambers form a cooling channel.

Der vorliegenden Erfindung liegt die Aufgabe zugrunde, eine Gießform zu schaffen, die einerseits die Herstellung von eng bauenden Motoren ohne die bei Verwendung von Sandkernen sich einstellenden Beschränkungen ermöglicht und andererseits eine hohe Produktivität bei der Herstellung sicherstellt. Darüber hinaus soll ein Verfahren geschaffen werden, das bei verringertem Herstellaufwand die Erzeugung von in ihrer Qualität verbesserten Motorblöcken ermöglicht.The present invention is based on the object, a Mold to create, on the one hand, the production of tight building engines without the use of sand cores themselves enabling restrictions and, on the other hand ensures high productivity during production. In addition, a procedure should be created that with reduced manufacturing costs the production of in their Quality improved engine blocks allows.

Diese Aufgabe wird in Bezug auf die Gießform der eingangs angegebenen Art dadurch gelöst, daß der Kanalformkern aus Glas hergestellt ist. In Bezug auf das Verfahren der eingangs genannten Art wird diese Aufgabe dadurch gelöst, daß in der Gießform zur Bildung des Kühlkanals zwischen den die Zylinderausnehmungen bildenden Kernen ein aus Glas bestehender Kanalformkern so angeordnet wird, daß er nur an seinen Enden gehaltert ist.This task is related to the mold of the beginning specified type solved in that the channel mold core Glass is made. Regarding the procedure of initially mentioned type, this object is achieved by that in the mold to form the cooling channel between the the cylinder recesses forming cores made of glass existing channel mold core is arranged so that it only on his ends are held.

Die erfindungsgemäße Gießform ermöglicht es, einen Motorblock herzustellen, bei dem die Festigkeit und Standzeit gegenüber einem bekannten derartigen Motorblock dadurch erhöht ist, daß zur Bildung des Kühlkanals nicht durch spanabhebende Bearbeitung in das Erstarrungsgefüge des Gußmaterials eingegriffen worden ist.The casting mold according to the invention makes it possible to use a To produce an engine block in which the strength and Service life compared to a known such engine block is increased by the fact that not to form the cooling channel by machining in the solidification structure of Casting material has been intervened.

Dabei kann sich die Querschnittsfläche des Kühlkanals von seinen Enden zu einer die Zylinderachsen senkrecht kreuzende Querachse des Kühlkanals verringern. Mit dieser Verringerung wird der Abnahme der Zylinderzwischenwand zu dieser Achse hin Rechnung getragen. Mit nach beiden Seiten hin zunehmender Zwischenwanddicke vergrößert sich auch die Querschnittsfläche des Kühlkanals, wodurch sich vorteilhaft der Strömungswiderstand des Kanals verringert und die Kühlmitteldurchgangsmenge erhöht.In this case, the cross-sectional area of the cooling channel of its ends to a cylinder axis perpendicular crossing Reduce the transverse axis of the cooling channel. With this reduction becomes the decrease of the cylinder intermediate wall to this axis taken into account. With to both sides increasing intermediate wall thickness also increases the Cross-sectional area of the cooling channel, which is advantageous the flow resistance of the channel decreases and the Coolant flow rate increased.

Die minimale Breite des Kühlkanals in Richtung der die Zylinderachsen senkrecht kreuzenden Kanalquerachse kann zwischen 0,5 und 1,5 mm betragen.The minimum width of the cooling channel in the direction of the Cylinder axes perpendicular crossing channel transverse axis can between 0.5 and 1.5 mm.

Während beliebige Querschnittsflächenformen denkbar sind, ist die Kanalquerschnittsfläche vorzugsweise länglich ausgebildet und erstreckt sich mit einer Längsachse parallel zu den Zylinderachsen. Während die Breitenausdehnung des Kühlkanals durch die Stärke der Zylinderzwischenwand begrenzt ist, kann sich der Kühlkanal in Richtung der Zylinderachsen unter Erhöhung des Durchlaßquerschnitts verhältnismäßig weit ausdehnen.While any cross-sectional surface shapes are conceivable, the channel cross-sectional area is preferably elongate formed and extends parallel to a longitudinal axis to the cylinder axes. While the latitude of the Cooling channel by the strength of the cylinder intermediate wall is limited, the cooling channel in the direction of Cylinder axes increasing the passage cross section to stretch relatively far.

Dabei kann sich der Kühlkanal geradlinig zwischen einander gegenüberliegenden Abschnitten eines die Zylinderreihe umgebenden Kühlmantels erstrecken.In this case, the cooling channel can be straight between each other opposite sections of a cylinder bank extend surrounding cooling jacket.

Grundsätzlich ist es denkbar, daß ein Gießformkern aus einem in einer Flüssigkeit lösbaren brennbaren oder /und spröden Material besteht, insbesondere einem Salz oder Kohlenstoff.Basically, it is conceivable that a Gießformkern from a Soluble in a liquid combustible and / or brittle Material consists, in particular a salt or carbon.

Ein Salzkern läßt sich nach dem Gießen und Erstarren des Gußmaterials aus dem Gußstück durch Herauslösen entfernen. Es versteht sich, daß ein lösliches Salz mit einem Schmelzpunkt gewählt werden muß, der oberhalb der Temperatur des verwendeten Gußmaterials liegt. Ein Kohlenstoffkem läßt sich ausbrennen, wozu gegebenenfalls zur Förderung der Verbrennung Sauerstoff zugeführt wird. Es ist ferner denkbar, ein pyrotechnisches Kernmaterial zu verwenden, daß neben Kohlenstoff ein dem Kohlenstoff zugesetztes Oxydationsmittel umfaßt, wobei durch die Materialzusammensetzung ein vollständiges Ausbrennen des Kerns gesichert, eine explosionsartige Verbrennung jedoch vermieden werden kann.A salt core can be left after the casting and solidification of the Remove casting material from the casting by removing it. It is understood that a soluble salt with a Melting point must be selected, which is above the temperature the casting material used is. Leave a carbon core burn out, including, where appropriate, to promote the Combustion oxygen is supplied. It is further conceivable to use a pyrotechnic core material that besides carbon, one added to the carbon Includes oxidizing agent, wherein by the Material composition complete burnout of the Kern's secured, however, an explosive combustion can be avoided.

Ein erfindungsgemäß eingesetzter spröder Glaskern läßt sich aus einem engen Kühlkanal, auch wenn die Kühlkanaleingänge nicht durch Werkzeuge zugänglich sind, entfernen, indem er z.B. durch Ultraschalleinwirkung in kleine Stücke zertrümmert wird, wobei der Glaskern hierfür durch Bildung von Spannungen entsprechend vorbehandelt sein kann. Alternativ kann der Glaskern durch einen unter Druck stehenden Wasserstrahl entfernt werden.An inventively used brittle glass core can be from a narrow cooling channel, even if the cooling channel inputs not accessible by tools, remove by removing e.g. by ultrasound effect into small pieces smashed, the glass core for this purpose by education can be pretreated by voltages accordingly. Alternatively, the glass core can be pressurized standing water jet to be removed.

In einer weiteren bevorzugten Ausführungsform der Erfindung ist der Gießformkem an seinen Enden an einem die Kerne für die Bildung der Zylinder aufweisenden Gießformteil gehaltert. Durch diese Maßnahme läßt sich mit geringen Toleranzabweichungen sichern, daß der Kühlkanal bezogen auf die die Zylinderausnehmungen bildende Kerne und damit bezogen auf die Zylinderausnehmungen innerhalb der Zwischenwand in der vorgesehenen Position angeordnet ist. Bei Halterung des Kanalformkerns an einem anderen Gießformteil müßten infolge Schwankungen der Paßgenauigkeit der Gießformteile untereinander bezüglich der Positionierung des Kühlkanals größere Fertigungstoleranzen in Kauf genommen werden.In a further preferred embodiment of the invention is the mold core at one end at one of the cores for the formation of the cylinder having casting mold part supported. By this measure can be with low Tolerance deviations ensure that the cooling channel based on the cores forming the cylinder recesses and thus based on the cylinder recesses within the Intermediate wall is arranged in the intended position. When holding the channel mold core on another Molded part would have due to fluctuations in the fit the mold parts with each other with respect to the positioning the cooling channel larger manufacturing tolerances accepted become.

Die Erfindung soll nun anhand von Ausführungsbeispielen und der beiliegenden, sich auf diese Ausführungsbeispiele beziehenden Zeichnungen näher erläutert und beschrieben werden. Es zeigen:

  • Fig.1 einen Teil einer erfindungsgemäßen Gießform in einer Draufsicht,
  • Fig. 2 eine den Gießformteil von Fig 1 enthaltende Querschnittsansicht der genannten Gießform,
  • Fig. 3 einen Motorblock nach der Erfindung in einer geschnittenen Seitenansicht,
  • Fig. 4 den Motorblock von Fig. 3 in einer Querschnittsansicht,
  • Fig. 5 ein weiteres Ausführungsbeispiel für einen erfindungsgemäßen Motorblock mit einem gebogenen Kühlkanal in einer Querschnittsansicht, und
  • Fig. 6 den Motorblock von Fig. 5 in einer Draufsicht.
  • The invention will now be explained and described in more detail with reference to embodiments and the accompanying drawings relating to these embodiments. Show it:
  • 1 shows a part of a casting mold according to the invention in a plan view,
  • FIG. 2 shows a cross-sectional view of said casting mold containing the casting mold part of FIG. 1, FIG.
  • 3 shows a motor block according to the invention in a sectional side view,
  • 4 shows the engine block of FIG. 3 in a cross-sectional view, FIG.
  • Fig. 5 shows a further embodiment of an engine block according to the invention with a curved cooling channel in a cross-sectional view, and
  • Fig. 6 shows the engine block of Fig. 5 in a plan view.
  • Mit dem Bezugszeichen 1 ist in den Fig. 1 und 2 ein Gießformteil mit Kernen 2 und 3 für die Bildung einer Zylinderausnehmung bezeichnet.By the reference numeral 1 is in Figs. 1 and 2, a mold part with cores 2 and 3 for the Formation of a cylinder recess called.

    Der Gießformteil 1 weist ferner Böcke 4 und 5 mit einer Nut 6 bzw. 7 auf. In die Nut 6 bzw. 7 ist mit seinen Enden ein Salzkern 8 eingesetzt. Jede der Nuten 6, 7 ist so lang, daß für den Salzkern 8 in jeder Nut ein Ausdehnungsfreiraum gegeben ist.The mold part 1 further comprises blocks 4 and 5 with a groove 6 and 7, respectively. In the groove 6 and 7 is with its ends a salt core 8 used. Each of the grooves 6, 7 is so long that for the salt core 8 is given in each groove an expansion clearance.

    Wie Fig. 2 zu entnehmen ist, bilden die Böcke einen Durchbruch in der dem Zylinderkopf zugewandten Decke 11 des Motorblocks. Unter Festlegung des Salzkerns 8 in den Nuten 6, 7 grenzen die Böcke 4, 5 gegen einen weiteren Gießformteil 12 an, durch welchen ein die Zylinder umgebender Kühlmantel gebildet wird.As can be seen in FIG. 2, the blocks form a breakthrough in the cylinder head facing ceiling 11 of the engine block. While fixing the salt core 8 in the grooves 6, 7 adjoin the blocks 4, 5 against another mold part 12, through which a Cylinder surrounding cooling jacket is formed.

    Bei 13 wird zwischen den Zylinderausnehmungen eine Zylinderzwischenwand aus Gußmaterial gebildet, deren minimale Breite durch die eingezeichneten Pfeile gekennzeichnet ist.At 13, between the cylinder recesses is a cylinder intermediate wall made of cast material formed, whose minimum width indicated by the arrows is.

    Wie aus Fig. 1 hervorgeht, nimmt die anfänglich konstante Breite des Salzkerns 8 von seinen Enden an zu einer die Zylinderachsen senkrecht kreuzenden Querachse 14 hin ab und erreicht bei dieser Achse eine Breite von 1 mm, während die Außenabschnitte des Salzkerns in dem Ausführungsbeispiel eine Breite von 2,5 mm aufweisen. Die mininmale, durch Gußmaterial gebildete Wanddicke der Zylinderzwischenwand bei 13 beträgt einschließlich der minimalen Kanalbreite 2,5 mm. Nicht gezeigt sind in den Motorblock einzugießende Graugußbuchsen, so daß die Gesamtstegbreite 5,5 mm beträgt. Der Salzkern 8 weist einen rechteckigen Querschnitt auf, wobei sich die lange Rechteckseite des Querschnitts senkrecht zu den Zylinderachsen erstreckt und in dem gezeigten Ausführungsbeispiel 4 mm beträgt.As is apparent from Fig. 1, takes the initially constant width of the salt core 8 of his Ends on to a cylinder axis perpendicular crossing transverse axis 14 down and reached a width of 1 mm in this axis, while the outer portions of the salt core in The embodiment have a width of 2.5 mm. The mininmale, by casting material formed wall thickness of the cylinder intermediate wall at 13 is inclusive of minimum channel width 2.5 mm. Not shown are in the engine block einzugießende gray cast iron bushings, so that the total web width is 5.5 mm. The salt core 8 has a rectangular in cross section, with the long rectangle side of the cross section extends perpendicular to the cylinder axes and in the embodiment shown 4 mm is.

    Der Salzkern 8 ist aus NaCl hergestellt, das einen Schmelzpunkt aufweist, der oberhalb der Temperatur des zur Herstellung des Motorblocks verwendeten flüssigen Aluminiumgußmaterials liegt. Je nach Gußmaterial sind andere Salze und Salzmischungen verwendbar.The salt core 8 is made of NaCl, which has a melting point above the Temperature of the liquid aluminum casting material used to make the engine block lies. Depending on the casting material, other salts and salt mixtures can be used.

    Der Salzkern 8 ist in dem gezeigten Ausführungsbeispiel durch Pressen und anschließendes Sintern hergestellt.The salt core 8 is in the embodiment shown by pressing and then Sintered.

    Nach einem Guß- und Erstarrungsvorgang wird der Salzkern durch heißes Wasser aus dem Gußteil herausgelöst. und es entsteht ein die Kühlmantelabschnitte zu beiden Seiten der Zylinderreihe verbindender Kühlkanal, der ausschließlich durch eine durchgehende Gußmaterialhaut begrenzt ist, was der dünnen Zylinderzwischenwand eine hohe Festigkeit verleiht. Durch den Kühlkanal ist für eine ausreichende Wärmeabfuhr und damit hohe Wärmestandfestigkeit des aus dem Motorblock hergestellten Motors gewährleistet.After a casting and solidification process, the salt core by hot water from the Cast out. and there is a cooling jacket sections on both sides of the Cylinder row connecting cooling channel, which only by a continuous Gußmaterialhaut is limited, which gives the thin cylinder intermediate wall high strength. Through the cooling channel is sufficient heat dissipation and thus high heat resistance ensured the engine made from the engine block.

    Während des Gießvorgangs dehnt sich der Salzkem aus, wobei die Nuten 6, 7 mit ihrer Länge ausreichend Freiraum für diese Ausdehnung bieten.During the casting process, the Salzkem expands, the grooves 6, 7 with their Provide sufficient space for this extension.

    Abweichend von dem gezeigten Ausführungsbeispiel könnte der Salzkern zu seinen Enden hin unter Verstärkung des Kühleffekts breiter als gezeigt auslaufen.Notwithstanding the embodiment shown, the salt core could to its ends with the cooling effect amplified wider than shown.

    Durch die Anbringung des Salzkerns auf den Böcken 4,5, welche Bestandteil des die Kerne 2,3 enthaltenen Gießformteils 1 sind, ist gewährleistet, daß sich der Kühlkanal in der Zwischenwand bei 13 mit geringen Toleranzabweichungen in der gewünschten Position bezogen auf die Zylinderachsen anordnen lassen. Würde der Kern 8 stattdessen auf dem den Kühlmantel bildenden Gießformteil 12 gehaltert, würde die Position des Kühlkanals größeren Schwankungen unterliegen.By attaching the salt core on the trestles 4,5, which are part of the cores 2.3 contained mold part 1 are, it is ensured that the cooling channel in the Intermediate wall at 13 with small tolerance deviations in the desired position Arrange with respect to the cylinder axes. Instead, the core 8 would be on the held the cooling jacket forming mold part 12, the position of the cooling channel subject to greater fluctuations.

    Beim Herauslösen des Kerns 8 aus dem gebildeten Gußteil kann zur Beschleunigung des Lösungsvorgangs heißes und ggf. unter Druck stehendes Wasser angewendet werden.When detaching the core 8 from the formed casting can be used to accelerate the Dissolution process hot and possibly pressurized water can be applied.

    Es wird nun bezug auf Fig. 3 und 4 bezug genommen.Reference will now be made to FIGS. 3 and 4.

    In Fig. 3 erscheinen eine erste Zylinderausnehmung 15 eines Motorblocks mit einer Auskleidung 16, eine erste Zylinderzwischenwand 17 und eine Auskleidung 18 einer nächsten Zylinderausnehmung 19.In Fig. 3 appear a first cylinder recess 15 of an engine block with a lining 16, a first cylinder intermediate wall 17 and a lining 18 of a next Cylinder recess 19.

    In Fig. 4 erscheinen die Zylinderausnehmungen 15, 19 je zur Hälfte mit der Zylinderzwischenwand 17 in der Mitte. In eingekreisten Abschnitten A und B ist zusätzlich der Zustand der Gießform dargestellt.In Fig. 4, the cylinder recesses 15, 19 appear half each with the cylinder intermediate wall 17 in the middle. In circled sections A and B is in addition the state of Mold shown.

    Zu erkennen sind ferner eine Außenwand 20 des Motorblocks, eine Zylinderkopffläche 21, ein Wassermantel 22 und zwei Stehbolzen 23 zur Befestigung eines Zylinderkopfes.Also visible are an outer wall 20 of the engine block, a cylinder head surface 21, a Water jacket 22 and two studs 23 for attachment of a cylinder head.

    In den eingerahmten Abschnitten A und B ist der den Wassermantel 22 ausbildende Formkern 24 dargestellt. In diesen eingeformt ist mit zwei dickeren Endabschnitten 25 eine Graphitplatte 26. Die Graphitplatte hat zwischen den dickeren Endabschnitten 25 eine Dicke von etwa 1,2 mm und eine Höhe von etwa 12 mm. Mit diesen Abmessungen erstreckt sie sich mittig durch die Dicke der Zylinderzwischenwand 17, und zwar in einer Höhe unmittelbar unter den Stehbolzen 23.In the framed sections A and B of the water jacket 22 forming mandrel is 24 shown. In this molded with two thicker end portions 25 a Graphite plate 26. The graphite plate has a between the thicker end portions 25 a Thickness of about 1.2 mm and a height of about 12 mm. Extends with these dimensions it is centered by the thickness of the cylinder intermediate wall 17, in a height directly under the stud bolts 23.

    In Fig. 3 und 4 außerhalb der eingekreisten Abschnitte A und B zeigen die Graphitplatte 26 in dem nach dem Gießen entformten Motorblock vor ihrem entfernen.In Figs. 3 and 4 outside of the circled sections A and B, the graphite plate 26 in Remove the molded block from the mold before casting.

    Die Grapfitplatte 26 wird abschließend entfernt durch Ausbrennen. Sie wird unter Anblasen von Sauerstoff gezündet und brennt durchgehend aus, wenn fortdauernd Sauerstoff in den durch ihr Ausbrennen freigelegten Kanal eingeblasen wird. Dies kann zur Beschleunigung von beiden Seiten her geschehen. Abweichend zu dieser Ausführungsform könnte dem Graphitmaterial ein Oxydationsmittel beigemischt sein, daß ein keiner solchen Unterstützung bedürftiges Ausbrennen ermöglicht.The Grapfitplatte 26 is finally removed by burning out. She is under blowing ignited by oxygen and burns out continuously, if continuous oxygen in the blown through its channel burned out. This can help to speed up done from both sides. Deviating from this embodiment, the Graphite material to be mixed with an oxidizing agent that no such support needy burnout allows.

    Die Wasserführung in dem Motorblock ist mit einem gewissen Druckgefälle zwischen der einen Seite der Zylinderreihe und der anderen Seite vorgesehen. Dadurch wird der durch die Graphitplatte 26 erzeugte Kanal durchströmt und damit ein Abtransport von Wärme ermöglicht.The water flow in the engine block is with a certain pressure gradient between the one side of the cylinder bank and the other side provided. This will be through the graphite plate 26 flows through channel generated and thus a removal of heat allows.

    Für andere wasserführende, ölführende oder gasführende dünne Kanäle in einem Zylinderblock oder Zylinderkopf läßt sich das Verfahren gleichfalls vorteilhaft anwenden, insbesondere auch für eine schmale Wasserführung zwischen den Ventilbohrungen eines Zylinderkopfes.For other water-bearing, oil-bearing or gas-carrying thin channels in a cylinder block or cylinder head, the method can also be used advantageously, in particular Also for a narrow water flow between the valve holes of a cylinder head.

    Es wird nun auf die Fig. 5 und 6 bezug genommen. Mit dem Bezugszeichen 27 ist in den Fig. 5 und 6 ein durch Gießen gebildeter Motorblock bezeichnet. Der durch weiche Schraffur im Querschnitt dargestellte Motorblock 27 besteht aus einer Aluminiumlegierung. Mit dem Bezugszeichen 28 ist ein Gießformteil zur Bildung eines die Zylinder des Motorblocks 27 umgebenden Kühlmantels bezeichnet. In den Motorblock 27 sind Zylinderlaufbuchsen 29 durch Umgießen mit Gußmaterial eingebunden. Die Zylinderlaufbuchsen 29 sitzen in der Gießform mit ihrer gesamten Innenfläche jeweils auf einem hohlzylindrischen Kokillendorn 30 der Gießform auf. Bei der im übrigen nicht gezeigten Gießform handelt es sich um eine Sandgießform.Reference will now be made to FIGS. 5 and 6. The reference numeral 27 is shown in FIG. 5 and Fig. 6 denotes an engine block formed by casting. The by soft hatching in the Cross-section engine block 27 is made of an aluminum alloy. With the reference number 28 is a mold part for forming a cylinder surrounding the engine block 27 Cooling jacket called. In the engine block 27 cylinder liners 29 are through Encapsulated with casting material. The cylinder liners 29 are seated in the mold with their entire inner surface each on a hollow cylindrical Kokillendorn 30 of the mold on. The casting mold, which is otherwise not shown, is a sand mold.

    In den Fig. 5 und 6 ist dem Bezugszeichen 31 ein Glaskern bezeichnet, der sich zwischen benachbarten Zylinderausnehmungen 32 des Motorblocks 27 von einem Sandgießformteil 33 zu einem Sandgießformteil 34 ersteckt. Die Sandgießformteile 33, 34 sind mit dem den Kühlmantel bildenden Sandgießformteil 28 verbunden und dienen zur Bildung von Öffnungen des Kühlmantels zur Zylinderkopfanlagefläche des Motorblocks 1.In Figs. 5 and 6, reference numeral 31 designates a glass core which is located between adjacent ones Cylinder recesses 32 of the engine block 27 of a sand mold part 33rd zuckt to a sand mold part 34. The Sandgießformteile 33, 34 are with the cooling jacket forming sand mold part 28 connected and serve to form openings of the cooling jacket to the cylinder head contact surface of the engine block 1.

    Der in einem Bogen verlegte Glaskern ist jeweils an seinen Enden in den Gießformteil 33 bzw. 34 eingebettet.The laid in an arc glass core is respectively at its ends in the mold part 33 and 34 embedded.

    In dem gezeigten Ausführungsbeispiel hat das Glasmaterial einen thermischen Ausdehnungskoeffizienten, der etwas unterhalb von 10-6K-1 liegt. Die Glasübergangstemperatur beträgt 700°C. Der Glaskern 31 hat einen Durchmesser von 1 mm.In the embodiment shown, the glass material has a thermal expansion coefficient which is slightly below 10 -6 K -1 . The glass transition temperature is 700 ° C. The glass core 31 has a diameter of 1 mm.

    Zwischen jeder der Zylinderausnehmungen 32 des Motorblocks 27 ist ein Kern angeordnet, wie er aus den Fig. 5 und 6 hervorgeht.Between each of the cylinder recesses 32 of the engine block 27, a core is arranged, as is apparent from Figs. 5 and 6.

    Während des Gießvorgangs wird der Glaskem 31 umgossen, wobei das Glasmaterial der mit dem Eingießen verbundenen Temperaturbelastung widersteht. Kurze Zeit nach dem Eingießen errreicht der Glaskern die Temperatur des Gußmaterials und damit seine maximale thermische Ausdehnung während des Gießvorgangs. Der Glaskern kühlt nun im Temperaturgewicht zusammen mit dem Gußmaterial ab, wobei das Gußmaterial aufgrund seines höheren Wärmeausdehnungskoeffizienten stärker schrumpft als der Glaskem 31. Diese Schrumpfung führt regelmäßig dazu, daß der Glaskern 31 zerspringt. Dazu kann der Glaskem 31 durch Abschrecken, Strahlen, Ätzen oder/und Ritzen geeignet vorbehandelt sein, insbesondere derart, daß eine Vielzahl von leicht entfernbaren Bruchstücken entsteht.During the casting process, the glass core 31 is encapsulated, wherein the glass material with withstanding the pouring associated with temperature stress. A short time after pouring the glass core reaches the temperature of the casting material and thus its maximum thermal expansion during the casting process. The glass core now cools in temperature weight along with the casting material, wherein the casting material due to its higher thermal expansion coefficient shrinks more than the glass core 31. This Shrinkage regularly causes the glass core 31 to shatter. For this, the glass core Be suitably pretreated by quenching, blasting, etching and / or scribing, in particular such that a plurality of easily removable fragments is formed.

    In dem gezeigten Ausführungsbeispiel ist der Glaskern 31 im Bogen so verlegt, daß durch die zur Zylinderkopfanlagefläche hin gebildeten Öffnungen hindurch ein flexibles Stoßwerkzeug eingeführt werden kann, mit dessen Hilfe für den Fall, daß der Glaskem bei der Schrumpfung nicht oder nur teilweise gebrochen ist, eine Entformung erfolgt.In the embodiment shown, the glass core 31 is laid in the bow so that through the to the cylinder head bearing surface formed through openings a flexible impact tool can be introduced, with the help of which in the event that the glass core in the shrinkage is not or only partially broken, a demoulding takes place.

    Der in dem gezeigten Ausführungsbeispiel gebogene Glaskem könnte auch gerade sein. Zum Entfernen des Glaskerns aus dem Gußstück kommt dann eine Ultraschallbehandlung oder Hochdruckstrahlbehandlung des Gußstücks in Betracht.The curved in the embodiment shown Glasaskem could also be straight. To remove the glass core from the casting then comes an ultrasonic treatment or high-pressure jet treatment of the casting.

    Auf die vorangehend beschriebene Weise lassen sich ohne Eingriff in das Gußgefüge Kanäle mit sehr glatten Innenwänden ähnlich der Qualität von Bohrungen herstellen. Vorteilhaft können sich in diesen Kanälen keine Ablagerungen aus dem Kühlmittel festsetzen. Ohne Beschädigung des Motorblocks ließen sich solche Kühlkanäle zwischen den Zylinderausnehmungen im Motorblock durch Bohrung nicht herstellen. In the manner described above can be without intervention in the cast structure Produce channels with very smooth inner walls similar to the quality of holes. Advantageous can not accumulate deposits from the coolant in these channels. Without damaging the engine block, such cooling channels could be located between the cylinder recesses Do not make a hole in the engine block.

    Die obengenannte Vorbehandlung, bei welcher der Glaskern einen den Glasbruch beim Schrumpfen oder durch nachträgliches Ausbrechen erleichternde Struktur, insbesondere Spannungsstruktur, erhält, ist zweckmäßig.The above pretreatment, in which the glass core a the glass breakage Shrinking or by subsequent breaking facilitating structure, in particular Tension structure, receives, is expedient.

    Salzkerne, Graphitkerne oder Glaskerne können abweichend von den gezeigten, einen Motorblock mit einem Kühlkanal zwischen den Zylindern betreffenden Beispielen auch an anderen Stellen des Motorblocks eingesetzt werden, um z.B. Kanäle zu bilden, durch die Kühlmittel oder Öl bestimmten Funktionsteilen im Motor zugeleitet werden kann.Salt cores, graphite cores or glass cores may deviate from the one shown Engine block with a cooling channel between the cylinders related examples also on other locations of the engine block are used, e.g. To form channels through which Coolant or oil can be supplied to certain functional parts in the engine.

    Claims (4)

    1. A casting mould for the manufacture of an engine block having a cooling channel extending between cylinder recesses (15, 19, 32) of a cylinder bank, with a minimum casting material wall thickness between the cylinder recesses of less than 5 mm wherein for the purpose of forming the cooling channel there is arranged inside the casting mould between the cores (2, 3) of the mould that form the cylinder recesses, a channel-forming core (8, 26) which is supported only at its ends, characterised in that the channel-forming core (8, 26) is made of glass.
    2. A casting mould according to claim 1 characterised in that the channel-forming core (8) is supported at its ends on a casting mould part (1) which contains the cores (2, 3) for forming the cylinder recess.
    3. A casting mould according to any one of the preceding claims characterised in that spaces are provided in the supports (4-7) for the channel-forming core (8) allowing it to expand in the longitudinal direction during casting.
    4. A process for the manufacture of an engine block having at least one cooling channel (31) in a dividing wall between adjacent cylinder recesses (32), the wall thickness formed by the casting material being less than 5 mm, wherein the engine block is formed by casting a casting material into a casting mould and wherein cores forming the cylinder recesses are placed inside the casting mould, characterised in that for the purpose of forming the cooling channel a channel-forming core consisting of glass is arranged inside the casting mould between the cores that form the cylinder recesses in such a manner that it is supported only at its ends.
    EP99113976A 1998-07-21 1999-07-17 Casting mould and a casting process for the production of an engine block Expired - Lifetime EP0974414B1 (en)

    Priority Applications (2)

    Application Number Priority Date Filing Date Title
    DE29924794U DE29924794U1 (en) 1998-07-21 1999-07-17 Cast aluminum engine block for internal combustion motor
    DK99113976T DK0974414T3 (en) 1998-07-21 1999-07-17 Mold and molding method for manufacturing an engine block

    Applications Claiming Priority (4)

    Application Number Priority Date Filing Date Title
    DE1998132718 DE19832718A1 (en) 1998-07-21 1998-07-21 Cast aluminum engine block for internal combustion motor
    DE19832718 1998-07-21
    DE1999125512 DE19925512B4 (en) 1999-06-02 1999-06-02 mold
    DE19925512 1999-06-02

    Publications (2)

    Publication Number Publication Date
    EP0974414A1 EP0974414A1 (en) 2000-01-26
    EP0974414B1 true EP0974414B1 (en) 2005-04-06

    Family

    ID=26047579

    Family Applications (1)

    Application Number Title Priority Date Filing Date
    EP99113976A Expired - Lifetime EP0974414B1 (en) 1998-07-21 1999-07-17 Casting mould and a casting process for the production of an engine block

    Country Status (6)

    Country Link
    US (1) US6205959B1 (en)
    EP (1) EP0974414B1 (en)
    AT (1) ATE292534T1 (en)
    DE (2) DE29924794U1 (en)
    DK (1) DK0974414T3 (en)
    ES (1) ES2241215T3 (en)

    Cited By (5)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE102007009776A1 (en) 2007-02-27 2008-08-28 Fritz Winter Eisengiesserei Gmbh & Co. Kg Production of a casting mold for casting components, e.g. engine block, comprises forming a molding element on the mold using a liquid jet
    EP2727668A1 (en) 2012-11-06 2014-05-07 Martinrea Honsel Germany GmbH Method for producing a cylinder crankcase and casting assembly for a cylinder crankcase
    DE102013101942B3 (en) * 2013-02-27 2014-07-31 Ks Aluminium-Technologie Gmbh Coolant jacket core and method for producing a coolant jacket core
    DE102014109598A1 (en) 2014-07-09 2016-01-14 Tenedora Nemak, S.A. De C.V. Casting core, use of a foundry core and method of making a foundry core
    DE102017213542A1 (en) * 2017-08-04 2019-02-07 Bayerische Motoren Werke Aktiengesellschaft Casting mold and method for producing a crankcase

    Families Citing this family (27)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US6298899B1 (en) * 1999-07-13 2001-10-09 Ford Global Tech., Inc. Water jacket core
    MY122487A (en) * 2000-12-21 2006-04-29 Petroliam Nasional Berhad Interbore cooling system
    DE10112135A1 (en) * 2001-03-14 2002-10-02 Bayerische Motoren Werke Ag Cast core for the coolant jacket of a crankcase of an internal combustion engine
    DE10153721C5 (en) * 2001-10-31 2011-04-28 Daimler Ag Casting tool for producing a cylinder crankcase
    JP2005532911A (en) * 2002-07-11 2005-11-04 コンソリデイテッド エンジニアリング カンパニー, インコーポレイテッド Method and apparatus for assisting removal of sand mold from castings
    US7220492B2 (en) * 2003-12-18 2007-05-22 3M Innovative Properties Company Metal matrix composite articles
    WO2005060343A2 (en) * 2003-12-18 2005-07-07 Tenedora Nemak, S.A. De C.V. Method and apparatus for manufacturing strong thin-walled castings
    WO2005102560A2 (en) * 2004-04-20 2005-11-03 Tenedora Nemak, S.A. De C.V. Method and apparatus for casting aluminum engine blocks with cooling liquid passage in ultra thin interliner webs
    DE102007044105A1 (en) 2007-04-27 2008-10-30 Mahle International Gmbh Casting core for forming a cooling channel in a piston produced by casting
    DE102007020927A1 (en) * 2007-05-04 2008-11-06 GM Global Technology Operations, Inc., Detroit Cylinder head and manufacturing process for a cylinder head
    DE102012101893C5 (en) * 2012-03-06 2022-06-23 Ks Huayu Alutech Gmbh Device for manufacturing a cylinder crankcase
    WO2014085430A2 (en) * 2012-11-27 2014-06-05 Quinton Aaron S Stabilized engine casting core assembly, method for making an engine body, and engine body formed thereby
    JP2015075018A (en) * 2013-10-08 2015-04-20 トヨタ自動車株式会社 Cylinder block
    KR101637638B1 (en) * 2014-02-18 2016-07-07 현대자동차주식회사 Casting product and manufacturing method thereof
    US9528464B2 (en) 2014-08-11 2016-12-27 Ford Global Technologies, Llc Bore bridge cooling passage
    CN204357543U (en) 2014-11-21 2015-05-27 康明斯排放处理公司 Nitrogen oxide signal multiplex system
    US9950449B2 (en) 2015-03-02 2018-04-24 Ford Global Technologies, Llc Process and tool for forming a vehicle component
    US10371087B2 (en) 2015-08-11 2019-08-06 Exco Engineering Die cast closed deck engine block manufacture
    DE102015012554A1 (en) 2015-09-25 2017-03-30 Neue Halberg-Guss Gmbh Cast body of a cylinder crankcase and method of manufacturing using a casting mold with a filigree one-piece insert core
    US10113504B2 (en) * 2015-12-11 2018-10-30 GM Global Technologies LLC Aluminum cylinder block and method of manufacture
    CN105772647A (en) * 2016-05-25 2016-07-20 宁波市鄞州德来特技术有限公司 Device for casting engine cylinder interval water hole and casting technology
    US10094328B2 (en) 2016-07-22 2018-10-09 Ford Global Technologies, Llc Forming assembly and method to provide a component with a passageway
    DE102017206716B4 (en) 2017-04-21 2021-05-06 Ford Global Technologies, Llc Cylinder block of an internal combustion engine
    FR3075676B1 (en) * 2017-12-22 2021-10-15 Renault Sas PROCESS FOR REALIZING INTERFUT CHANNELS IN A CYLINDER CRANKCASE
    DE102018121847A1 (en) * 2018-09-07 2020-03-12 Hengst Se Process for metal die casting with lost core
    US10781769B2 (en) * 2018-12-10 2020-09-22 GM Global Technology Operations LLC Method of manufacturing an engine block
    KR102638649B1 (en) * 2020-07-07 2024-02-19 세메스 주식회사 Semiconductor device pressing apparatus and test handler comprising the same

    Family Cites Families (7)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US4446906A (en) * 1980-11-13 1984-05-08 Ford Motor Company Method of making a cast aluminum based engine block
    GB2102317B (en) * 1981-07-03 1985-10-09 Rolls Royce Internally reinforced core for casting
    GB2123727B (en) * 1982-06-25 1985-11-20 Ae Plc Pressure-casting pistons
    DE3300924A1 (en) * 1983-01-13 1984-07-19 Volkswagenwerk Ag, 3180 Wolfsburg Device for the cooling of cylinder lands
    DE3512076C1 (en) * 1985-04-02 1988-01-21 Halbergerhütte GmbH, 6600 Saarbrücken Device for the casting production of a cooling device for webs between adjacent cylinders of a cylinder block and a correspondingly produced cylinder block
    AT388319B (en) * 1987-08-20 1989-06-12 Avl Verbrennungskraft Messtech CASTING CORE FOR THE WATER JACKET OF A CYLINDER BLOCK OF A MULTI-CYLINDER PISTON PISTON COMBUSTION ENGINE
    US5217059A (en) * 1992-01-16 1993-06-08 Cmi International Casting core and method for forming a water jacket chamber within a cast cylinder block

    Cited By (8)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE102007009776A1 (en) 2007-02-27 2008-08-28 Fritz Winter Eisengiesserei Gmbh & Co. Kg Production of a casting mold for casting components, e.g. engine block, comprises forming a molding element on the mold using a liquid jet
    EP2727668A1 (en) 2012-11-06 2014-05-07 Martinrea Honsel Germany GmbH Method for producing a cylinder crankcase and casting assembly for a cylinder crankcase
    DE102012110592A1 (en) 2012-11-06 2014-05-08 Martinrea Honsel Germany Gmbh A method of manufacturing a cylinder crankcase and a casting block assembly for a cylinder crankcase
    DE102013101942B3 (en) * 2013-02-27 2014-07-31 Ks Aluminium-Technologie Gmbh Coolant jacket core and method for producing a coolant jacket core
    DE102014109598A1 (en) 2014-07-09 2016-01-14 Tenedora Nemak, S.A. De C.V. Casting core, use of a foundry core and method of making a foundry core
    WO2016005806A1 (en) 2014-07-09 2016-01-14 Tenedora Nemak, S.A. De C.V. Core, use of a core, and mehtod for the production of a core
    DE102017213542A1 (en) * 2017-08-04 2019-02-07 Bayerische Motoren Werke Aktiengesellschaft Casting mold and method for producing a crankcase
    US11420251B2 (en) 2017-08-04 2022-08-23 Bayerische Motoren Werke Aktiengesellscaft Casting mold and process for manufacturing a crankcase

    Also Published As

    Publication number Publication date
    DE29924794U1 (en) 2005-09-08
    DK0974414T3 (en) 2005-07-25
    ES2241215T3 (en) 2005-10-16
    EP0974414A1 (en) 2000-01-26
    ATE292534T1 (en) 2005-04-15
    US6205959B1 (en) 2001-03-27
    DE59911865D1 (en) 2005-05-12

    Similar Documents

    Publication Publication Date Title
    EP0974414B1 (en) Casting mould and a casting process for the production of an engine block
    EP2091678B1 (en) Casting mould for casting a cast part and use of such a casting mould
    DE102007002208B4 (en) Formation of a partition window of a cylinder block casting
    EP2727668B1 (en) Method for producing a cylinder crankcase and casting assembly for a cylinder crankcase
    EP1817147A1 (en) Heat shield element, method and form for the production thereof, hot gas lining and combustion chamber
    EP1188500A1 (en) Apparatus and method for producing a turbine blade and turbine blade
    DE102017206716B4 (en) Cylinder block of an internal combustion engine
    DE10033271B4 (en) Water jacket core
    EP2059356B1 (en) Single-part expendable casting mould with a controlled temperature for cast metal parts and associated production method
    EP2738377B1 (en) Process for manufacturing a cylinder crankcase
    WO1998030345A1 (en) Method of producing a cooling plate for iron and steel-making furnaces
    EP1790865B1 (en) Cast hollow crankshaft
    EP0899042B1 (en) Fabrication method of a casted cylinder head
    EP2454037B1 (en) Mold insert for a casting core and/or a casting mold and casting core and/or casting mold comprising a mold insert
    EP2421666A1 (en) Casting apparatus for producing a turbine rotor blade of a gas turbine and turbine rotor blade
    EP2636467B1 (en) Device for manufacturing a cylinder crank case in V design
    DE4100779C2 (en)
    EP1797976A2 (en) Conical bubble brick
    DE3401024C2 (en) Casting nozzle consisting of several longitudinal sections for feeding molten metal into a continuous casting mold and method for producing the mouthpiece of such a casting nozzle
    WO2006061046A1 (en) Casting mould for casting a motor block for an internal combustion engine, motor block for an internal combustion engine and use of a hollow profile
    DE328578C (en) Cast iron roller with high breaking strength
    DE102019106643A1 (en) Water jacket core
    DE102004034802A1 (en) Durable mold, for large ferrous alloy castings, has mold units assembled with expansion gaps filled with a pliable sealing to give inner/outer shapes and be dismantled for further use on removing the cooled casting
    DE1204364B (en) Process for the production of a repeatable casting mold
    DE102004009112A1 (en) Cylinder head is for fluid-cooled internal combustion engine and has at least two outlet channels and a formation between them provided with a coolant channel

    Legal Events

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

    Free format text: ORIGINAL CODE: 0009012

    AK Designated contracting states

    Kind code of ref document: A1

    Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

    AX Request for extension of the european patent

    Free format text: AL;LT;LV;MK;RO;SI

    17P Request for examination filed

    Effective date: 20000719

    AKX Designation fees paid

    Free format text: AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

    17Q First examination report despatched

    Effective date: 20021113

    GRAP Despatch of communication of intention to grant a patent

    Free format text: ORIGINAL CODE: EPIDOSNIGR1

    RTI1 Title (correction)

    Free format text: CASTING MOULD AND A CASTING PROCESS FOR THE PRODUCTION OF AN ENGINE BLOCK

    GRAS Grant fee paid

    Free format text: ORIGINAL CODE: EPIDOSNIGR3

    GRAA (expected) grant

    Free format text: ORIGINAL CODE: 0009210

    AK Designated contracting states

    Kind code of ref document: B1

    Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

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

    Ref country code: NL

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

    Effective date: 20050406

    Ref country code: FI

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

    Effective date: 20050406

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

    Owner name: HYDRO ALUMINIUM ALUCAST GMBH

    REG Reference to a national code

    Ref country code: GB

    Ref legal event code: FG4D

    Free format text: NOT ENGLISH

    REG Reference to a national code

    Ref country code: CH

    Ref legal event code: EP

    REG Reference to a national code

    Ref country code: IE

    Ref legal event code: FG4D

    Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

    REF Corresponds to:

    Ref document number: 59911865

    Country of ref document: DE

    Date of ref document: 20050512

    Kind code of ref document: P

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

    Ref country code: GR

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

    Effective date: 20050706

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

    Ref country code: LU

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

    Effective date: 20050717

    Ref country code: CY

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

    Effective date: 20050717

    REG Reference to a national code

    Ref country code: SE

    Ref legal event code: TRGR

    REG Reference to a national code

    Ref country code: DK

    Ref legal event code: T3

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

    Ref country code: MC

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

    Effective date: 20050731

    Ref country code: LI

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

    Effective date: 20050731

    Ref country code: CH

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

    Effective date: 20050731

    Ref country code: BE

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

    Effective date: 20050731

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

    Effective date: 20050708

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

    Ref country code: PT

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

    Effective date: 20050908

    NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
    REG Reference to a national code

    Ref country code: ES

    Ref legal event code: FG2A

    Ref document number: 2241215

    Country of ref document: ES

    Kind code of ref document: T3

    PLBE No opposition filed within time limit

    Free format text: ORIGINAL CODE: 0009261

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

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

    REG Reference to a national code

    Ref country code: CH

    Ref legal event code: PL

    ET Fr: translation filed
    26N No opposition filed

    Effective date: 20060110

    BERE Be: lapsed

    Owner name: HYDRO ALUMINIUM ALUCAST G.M.B.H.

    Effective date: 20050731

    REG Reference to a national code

    Ref country code: DK

    Ref legal event code: EBP

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

    Ref country code: DK

    Payment date: 20060714

    Year of fee payment: 8

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

    Ref country code: DK

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

    Effective date: 20070731

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

    Ref country code: IE

    Payment date: 20090130

    Year of fee payment: 10

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

    Ref country code: SE

    Payment date: 20090723

    Year of fee payment: 11

    REG Reference to a national code

    Ref country code: IE

    Ref legal event code: MM4A

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

    Ref country code: IE

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

    Effective date: 20090717

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

    Ref country code: SE

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

    Effective date: 20100718

    REG Reference to a national code

    Ref country code: FR

    Ref legal event code: PLFP

    Year of fee payment: 18

    REG Reference to a national code

    Ref country code: FR

    Ref legal event code: PLFP

    Year of fee payment: 19

    REG Reference to a national code

    Ref country code: FR

    Ref legal event code: PLFP

    Year of fee payment: 20

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

    Ref country code: FR

    Payment date: 20180723

    Year of fee payment: 20

    Ref country code: ES

    Payment date: 20180823

    Year of fee payment: 20

    Ref country code: DE

    Payment date: 20180723

    Year of fee payment: 20

    Ref country code: IT

    Payment date: 20180730

    Year of fee payment: 20

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

    Ref country code: GB

    Payment date: 20180723

    Year of fee payment: 20

    Ref country code: AT

    Payment date: 20180724

    Year of fee payment: 20

    REG Reference to a national code

    Ref country code: DE

    Ref legal event code: R071

    Ref document number: 59911865

    Country of ref document: DE

    REG Reference to a national code

    Ref country code: GB

    Ref legal event code: PE20

    Expiry date: 20190716

    REG Reference to a national code

    Ref country code: AT

    Ref legal event code: MK07

    Ref document number: 292534

    Country of ref document: AT

    Kind code of ref document: T

    Effective date: 20190717

    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 EXPIRATION OF PROTECTION

    Effective date: 20190716

    REG Reference to a national code

    Ref country code: ES

    Ref legal event code: FD2A

    Effective date: 20201202

    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 EXPIRATION OF PROTECTION

    Effective date: 20190718