EP1713603A2 - Procede et appareil pour fabriquer des moulages a parois minces tres resistants - Google Patents
Procede et appareil pour fabriquer des moulages a parois minces tres resistantsInfo
- Publication number
- EP1713603A2 EP1713603A2 EP04816622A EP04816622A EP1713603A2 EP 1713603 A2 EP1713603 A2 EP 1713603A2 EP 04816622 A EP04816622 A EP 04816622A EP 04816622 A EP04816622 A EP 04816622A EP 1713603 A2 EP1713603 A2 EP 1713603A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- casting
- block
- interliner
- mold
- insert
- 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.)
- Withdrawn
Links
- 238000000034 method Methods 0.000 title claims abstract description 24
- 238000005266 casting Methods 0.000 title claims description 25
- 238000004519 manufacturing process Methods 0.000 title claims description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910000838 Al alloy Inorganic materials 0.000 claims description 23
- 239000007787 solid Substances 0.000 claims description 17
- 238000007711 solidification Methods 0.000 claims description 7
- 230000008023 solidification Effects 0.000 claims description 7
- 229910001338 liquidmetal Inorganic materials 0.000 claims description 2
- 229910001018 Cast iron Inorganic materials 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 abstract description 23
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 23
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 abstract description 18
- 229910052742 iron Inorganic materials 0.000 abstract description 9
- 229910045601 alloy Inorganic materials 0.000 abstract description 6
- 239000000956 alloy Substances 0.000 abstract description 6
- 239000000110 cooling liquid Substances 0.000 abstract description 2
- 238000001816 cooling Methods 0.000 description 22
- 239000007788 liquid Substances 0.000 description 16
- 239000000463 material Substances 0.000 description 10
- 239000012809 cooling fluid Substances 0.000 description 6
- 230000035882 stress Effects 0.000 description 6
- 238000013461 design Methods 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 238000003754 machining Methods 0.000 description 4
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 239000004576 sand Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 239000010974 bronze Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 230000002028 premature Effects 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 241001391944 Commicarpus scandens Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000011358 absorbing material Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 239000007767 bonding agent Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 239000003562 lightweight material Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/0009—Cylinders, pistons
Definitions
- the invention broadly relates to the art of manufacturing thin-walled castings and is particularly useful for the manufacture of cast aluminum automotive engine blocks with very thin interliner walls.
- the design of the engine blocks has been changing over the time with a tendency to increase the power of engines.
- the dimensions of the motor blocks tend to be fixed by the dimensions of the car body.
- the blocks need to accommodate cylinders of larger volume, meaning larger diameter, within the same block volume.
- These designs pose a challenging problem to block manufacturers, because the cylinder liners (usually made of iron) are sought to be so close together that the aluminum wall formed as a web in the gap between said cylinder liners is becoming ever thinner (less than about 3 mm). With the gap between adjacent pairs of cylinder liners being so thin, the liquid aluminum volume filling such interliner cavity is relatively small and rapidly loses heat upon contacting said iron liners and consequently solidifies prematurely thus plugging the cavity and preventing liquid aluminum from filling the rest of said cavity.
- This insert is preferably made of aluminum of the same alloy or optionally of a different alloy or even of some other suitable material (such as bronze or copper) and is positioned in the desired place at the same time that the sand core defining the water jacket of the block is produced.
- This insert can have an hourglass shape similar to the pre-formed core discussed in U.S. Patent No. 6,298,899 and also similarly has the advantage of avoiding the "angle of inclination" discussed therein. Though similar in shape due to its positioning, the '899 core serves a very different purpose (involving a different concept). The applicants' pre-formed insert is significantly different with many more advantages.
- the '899 core is an impermanent sand core
- Applicants' pre-formed insert is a permanent solid structure that effectively remains in place as part of the casting after the water jacket core is removed.
- the Applicants' pre-formed insert can be a solid, or can additionally incorporate a thin- walled pipe, or preferably can alternatively have an integrally formed passage in it. The pipe or passage in such an insert is thus able to provide an effective stable cooling fluid passage through the ultra-nanow interliner gap.
- a method of casting a cast product comprising pre-formed solid elements having at least one dimension thinner than about 3mm and separately casting thereafter the rest of the product with liquid metal with the pre-formed elements already in place thereby to form the final cast product.
- a method of manufacturing an engine block of aluminum alloy having cylinder liners comprising providing a mold for casting said engine block; inserting pre-formed solid elements each between a pair of said cylinder liners and filling said mold with molten aluminum alloy to form said motor block.
- an engine block made of aluminum alloy is provided, comprising relatively stress-free pre-formed solid elements between said cylinder liners and the rest of said engine block being cast from said aluminum alloy forming an integral block after solidification of said casting.
- the solid elements can incorporate a cooling passage pipe, or the pre-formed solid insert can have a cooling passage already formed therein (optionally with an in-place removable core).
- Figure 1 is an isometric view of the core of a mold for forming the water jacket (i.e. cooling passages) of an aluminum engine block incorporating three pre-formed solid aluminum inserts (according to one prefened embodiment of the present invention), with each such insert having a bridging cooling passage core and each being incorporated by means of the bridging core with the jacket core at a respective interliner gap position
- Figure 2 shows a top stylized view of an engine cylinder block with a cylindrical iron liner closely fitted into each of the cylinder bores and with a solid aluminum insert (having no passages therein) positioned in the interliner gap of each pair of liners in the finished block (thus showing the relationship of engine parts in which the invention can effectively be practiced).
- Figure 3 shows a stylized vertical section taken along section line A- A of Figure 2.
- Figure 4 shows a top stylized view similar to figure 2, but according to a different prefened embodiment of the present invention wherein the pre-formed inserts each incorporate a bridging cooling fluid flow passage (shown in dotted lines).
- Figure 5 shows a stylized vertical section taken along section line A-A of Figure 4..
- Figure 6 is an isometric view a solid pre-formed insert showing two bridging cores, passing through and extending out from either end of the upper portion of the pre-formed insert, for forming interliner-gap-bridging cooling-fluid flow passages.
- Figure 7 is an isometric view showing two iron liners mounted on the core of a mold with a solid pre-formed insert (according to the prefened embodiment of figures 2 and 3) fitted in the interliner gap.
- a solid pre-formed insert according to the prefened embodiment of figures 2 and 3 fitted in the interliner gap.
- the solution to the problems of filling a casting mold for an engine-block 8 having thin interliner walls 9 with a liquid aluminum alloy comprises incorporating a solid insert 10 made of a suitable material, for example the same aluminum alloy which will form the rest of the cast block.
- suitable materials for the pre-formed insert include, for example, bronze, copper and alloys and equivalents thereof.
- the pre-formed insert (designated generally by reference number 10) may be forged or extruded.
- the pre-formed insert 10 is placed between the cylinder liners 12 before introducing the liquid aluminum alloy into said mold.
- the insert 10 will be contained and locked in place by the liquid aluminum which solidifies forming the rest of the block 8.
- the perform insert (see inserts 10a or 10b) has grooves 14 to engage the liquid aluminum, thereby providing a better bond between the insert and the aluminum when the liquid aluminum cools and sets. Bonding may also occur from surface melting of the insert 10 during the casting pour. This may be aided by the addition of a bonding agent such as low melting zinc.
- one of the advantages of the present invention is that the pre-formed inserts 10 do not result in residual tension.
- the inserts 10 are not made of the same alloy, little or no thermal stresses are induced in the pre-formed inserts 10 due to shrinking of aluminum or due to expansion of the iron cylinder liners 12 (since the inserts 10 are already cooled to solid stress free form).
- the invention advantageously resists tensions or cracking caused by post-machining, procedures such as boring.
- a cooling-liquid passage 15 is preferably formed in or as part of a pre-formed insert 10; for example, by placing an insert 10b or 10c with a conduit for said cooling-fluid having the required shape to fit in the gap between the cylinder liners.
- the passage 15 can take the form of an embedded thin walled pipe 17 (made of steel or the like), see Figure 1 , or may be integrally form with the insert by use of a bridging core 16, see Figure 6.
- the removable bridging core 16 when used to form the passage 15 in the pre-formed insert 10b will remain in place until after the casting of the engine block is completed (and thereafter be removed with the removal of the jacket core 6).
- Known examples of such bridging cores include salt, carbon, or glass (see U.S. Patent No. 6,205,959).
- the present invention can be practiced, for example, with cunent processes and equipment, which can comprise a holding furnace for liquid aluminum alloy, a source of pressurized gas, normally nitrogen, which is injected into said holding furnace for pushing upwardly said liquid aluminum alloy through a suitable connecting conduit into a gate of a mold placed on top of said holding furnace.
- a suitable device for example a slide valve or gate and said mold is then disconnected from the holding furnace and the process is repeated by a subsequent mold to be filled up.
- a mass of a heat-absorbing material also known as a chill (or a heat sink device) can be cunently placed under a proprietary process of the assignee of this application in contact with the liquid aluminum alloy in order to direct the solidification in the desired direction in order to produce good-quality castings.
- Such controlled cooling can be disrupted by the small interliner gaps that are now encountered in modern aluminum automotive engine blocks; but are overcome by use of the present invention.
- Less than 3 mm is a prefened condition for using this invention, but the method applies as well to thicker interliner dimensions when there is a need to provide interliner cross sections with reduced residual stresses due to the solidification process or for any of the other reasons discussed above.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US53127803P | 2003-12-18 | 2003-12-18 | |
PCT/IB2004/004401 WO2005060343A2 (fr) | 2003-12-18 | 2004-12-20 | Procede et appareil pour fabriquer des moulages a parois minces tres resistants |
Publications (1)
Publication Number | Publication Date |
---|---|
EP1713603A2 true EP1713603A2 (fr) | 2006-10-25 |
Family
ID=34710217
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP04816622A Withdrawn EP1713603A2 (fr) | 2003-12-18 | 2004-12-20 | Procede et appareil pour fabriquer des moulages a parois minces tres resistants |
Country Status (5)
Country | Link |
---|---|
US (1) | US20050173091A1 (fr) |
EP (1) | EP1713603A2 (fr) |
JP (1) | JP2007514550A (fr) |
CA (1) | CA2550033A1 (fr) |
WO (1) | WO2005060343A2 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100044003A1 (en) * | 2008-08-25 | 2010-02-25 | Mark A. Baumgarten | Insert molding |
DE102010047325B4 (de) * | 2010-10-01 | 2021-11-18 | Daimler Ag | Brennkraftmaschine mit einem Zylindergehäuse aus Leichtmetallguss und mit Zylinderlaufbuchsen aus Rauguss |
CN103541828B (zh) * | 2012-07-17 | 2014-10-08 | 安徽华菱汽车有限公司 | 发动机及其缸套缸体的冷却结构 |
DE102012025333B4 (de) * | 2012-12-21 | 2021-09-30 | Audi Ag | Kurbelgehäuse einer Brennkraftmaschine sowie Verfahren zum Herstellen eines Kurbelgehäuses |
US9416749B2 (en) | 2013-12-09 | 2016-08-16 | Ford Global Technologies, Llc | Engine having composite cylinder block |
US9341136B2 (en) | 2013-12-09 | 2016-05-17 | Ford Global Technologies, Llc | Engine having composite cylinder block |
US10113504B2 (en) * | 2015-12-11 | 2018-10-30 | GM Global Technologies LLC | Aluminum cylinder block and method of manufacture |
US10781769B2 (en) * | 2018-12-10 | 2020-09-22 | GM Global Technology Operations LLC | Method of manufacturing an engine block |
US11174813B1 (en) * | 2020-09-30 | 2021-11-16 | Caterpillar Inc. | Liner for engine block and systems, assemblies, components, and methods thereof |
Family Cites Families (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2880485A (en) * | 1954-12-08 | 1959-04-07 | Gen Motors Corp | Water jacket coring for casting internal combustion engine blocks |
US2991520A (en) * | 1956-01-13 | 1961-07-11 | Howard Foundry Company | Cored passageway formation |
US2897556A (en) * | 1957-09-04 | 1959-08-04 | Sperry Rand Corp | Method of coring holes in castings |
DE1576713B2 (de) * | 1967-12-13 | 1972-04-13 | Daimler Benz Ag | Zylinderblock für Brennkraftmaschinen, insbesondere für Kraftfahrzeuge |
SE360813B (fr) * | 1971-03-15 | 1973-10-08 | Saab Scania Ab | |
US4008747A (en) * | 1974-11-04 | 1977-02-22 | General Motors Corporation | Method for locating insert in cast iron |
US4446906A (en) * | 1980-11-13 | 1984-05-08 | Ford Motor Company | Method of making a cast aluminum based engine block |
DE3512076C1 (de) * | 1985-04-02 | 1988-01-21 | Halbergerhütte GmbH, 6600 Saarbrücken | Vorrichtung zur gießtechnischen Herstellung einer Kühleinrichtung von Stegen zwischen benachbarten Zylindern eines Zylinderblocks sowie entsprechend hergestellter Zylinderblock |
FR2609501B1 (fr) * | 1987-01-09 | 1991-01-11 | Peugeot | Moteur a combustion interne muni de moyens perfectionnes de refroidissement du bloc-cylindres |
AT388319B (de) * | 1987-08-20 | 1989-06-12 | Avl Verbrennungskraft Messtech | Giesskern fuer den wassermantel eines zylinderblockes einer mehrzylinder-hubkolben-brennkraftmaschine |
JPH071023B2 (ja) * | 1988-10-14 | 1995-01-11 | いすゞ自動車株式会社 | 内燃機関用シリンダライナー |
US4903652A (en) * | 1989-07-31 | 1990-02-27 | Ford Motor Company | Cylinder liner insert and method of making engine block therewith |
EP0527948B1 (fr) * | 1990-05-09 | 1996-11-13 | Lanxide Technology Company, Lp | Composites minces a matrice metallique et leurs procedes de production |
SE470055B (sv) * | 1991-03-05 | 1993-11-01 | Volvo Ab | Sätt och verktyg för pressgjutning |
US5333668A (en) * | 1991-12-09 | 1994-08-02 | Reynolds Metals Company | Process for creation of metallurgically bonded inserts cast-in-place in a cast aluminum article |
DE69228954T2 (de) * | 1992-01-06 | 1999-08-12 | Honda Giken Kogyo K.K., Tokio/Tokyo | Gussverfahren eines Zylinderblockes |
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 |
US5188071A (en) * | 1992-01-27 | 1993-02-23 | Hyundai Motor Company | Cylinder block structure |
US5421397A (en) * | 1993-01-19 | 1995-06-06 | Hembree; Robert K. | Method of and system for casting engine blocks having defect free thin walls |
US5800902A (en) * | 1995-03-15 | 1998-09-01 | Nelson Metal Products Corporation | Metal die cast article with reinforcing insert |
JPH09151782A (ja) * | 1995-11-29 | 1997-06-10 | Toyota Motor Corp | シリンダブロックの製造方法 |
DE19633419C1 (de) * | 1996-08-20 | 1997-11-20 | Porsche Ag | Zylinderblock einer Brennkraftmaschine |
SE9702055L (sv) * | 1997-05-30 | 1998-11-30 | Volvo Ab | Förbränningsmotor |
JPH11200943A (ja) * | 1998-01-12 | 1999-07-27 | Isuzu Motors Ltd | シリンダブロック構造 |
DE59911865D1 (de) * | 1998-07-21 | 2005-05-12 | Hydro Aluminium Alucast Gmbh | Giessform und Giessverfahren zur Herstellung eines Motorblocks |
US6129057A (en) * | 1999-02-05 | 2000-10-10 | Daimlerchrysler Corporation | Engine block casing and insert member diecast from permanent molds |
US6298899B1 (en) * | 1999-07-13 | 2001-10-09 | Ford Global Tech., Inc. | Water jacket core |
JP2001164985A (ja) * | 1999-09-28 | 2001-06-19 | Kubota Corp | 多気筒エンジンのシリンダブロック及びその鋳造方法 |
US6349681B1 (en) * | 2000-05-22 | 2002-02-26 | General Motors Corporation | Cylinder block for internal combustion engine |
MY122487A (en) * | 2000-12-21 | 2006-04-29 | Petroliam Nasional Berhad | Interbore cooling system |
JP4408005B2 (ja) * | 2001-01-31 | 2010-02-03 | 富士重工業株式会社 | シリンダブロック構造 |
EP1321207B1 (fr) * | 2001-12-21 | 2006-03-08 | Ford Global Technologies, LLC | Procédé pour couler sous pression un bloc moteur ,pour moteur à combustion interne , en alliage d'aluminium comportant un renforcement en alliage de fer ainsi que bloc moteur obtenu par ce procédé |
US20050247428A1 (en) * | 2004-04-20 | 2005-11-10 | Tenedora Nemak, S.A. De C.V. | Method and apparatus for casting aluminum engine blocks with cooling liquid passage in ultra thin interliner webs |
-
2004
- 2004-12-20 EP EP04816622A patent/EP1713603A2/fr not_active Withdrawn
- 2004-12-20 JP JP2006544602A patent/JP2007514550A/ja active Pending
- 2004-12-20 WO PCT/IB2004/004401 patent/WO2005060343A2/fr not_active Application Discontinuation
- 2004-12-20 US US11/018,941 patent/US20050173091A1/en not_active Abandoned
- 2004-12-20 CA CA002550033A patent/CA2550033A1/fr not_active Abandoned
Non-Patent Citations (1)
Title |
---|
See references of WO2005060343A2 * |
Also Published As
Publication number | Publication date |
---|---|
US20050173091A1 (en) | 2005-08-11 |
CA2550033A1 (fr) | 2005-07-07 |
WO2005060343A3 (fr) | 2006-03-23 |
JP2007514550A (ja) | 2007-06-07 |
WO2005060343A8 (fr) | 2007-02-15 |
WO2005060343A2 (fr) | 2005-07-07 |
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