EP1721072B1 - Cylinder sleeve for an internal combustion engine - Google Patents
Cylinder sleeve for an internal combustion engine Download PDFInfo
- Publication number
- EP1721072B1 EP1721072B1 EP05714992.4A EP05714992A EP1721072B1 EP 1721072 B1 EP1721072 B1 EP 1721072B1 EP 05714992 A EP05714992 A EP 05714992A EP 1721072 B1 EP1721072 B1 EP 1721072B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cylinder sleeve
- bushing
- raugussbuchsen
- der
- und
- 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.)
- Not-in-force
Links
- 238000002485 combustion reaction Methods 0.000 title claims description 6
- 238000005266 casting Methods 0.000 claims description 15
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- 238000000034 method Methods 0.000 claims description 8
- 238000009750 centrifugal casting Methods 0.000 claims description 5
- 230000004323 axial length Effects 0.000 claims description 3
- 229910001018 Cast iron Inorganic materials 0.000 claims description 2
- 238000010114 lost-foam casting Methods 0.000 claims description 2
- 229910000789 Aluminium-silicon alloy Inorganic materials 0.000 claims 1
- 230000003068 static effect Effects 0.000 claims 1
- 238000007788 roughening Methods 0.000 description 24
- 239000000463 material Substances 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 125000006850 spacer group Chemical group 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 229910000676 Si alloy Inorganic materials 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000006260 foam Substances 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 229910000679 solder Inorganic materials 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
-
- 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
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/02—Cylinders; Cylinder heads having cooling means
- F02F1/10—Cylinders; Cylinder heads having cooling means for liquid cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/02—Cylinders; Cylinder heads having cooling means
- F02F1/10—Cylinders; Cylinder heads having cooling means for liquid cooling
- F02F1/16—Cylinder liners of wet type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
- F05C2201/0436—Iron
- F05C2201/0439—Cast iron
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/90—Alloys not otherwise provided for
- F05C2201/903—Aluminium alloy, e.g. AlCuMgPb F34,37
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2251/00—Material properties
- F05C2251/04—Thermal properties
- F05C2251/042—Expansivity
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/4927—Cylinder, cylinder head or engine valve sleeve making
- Y10T29/49272—Cylinder, cylinder head or engine valve sleeve making with liner, coating, or sleeve
Definitions
- the invention relates to a bushing for an internal combustion engine according to the preamble of claim 1.
- the roughening on the outer surface of the Raugussbuchse provides a very large standing in contact with the material of the engine block outer surface over which the heat of combustion can be well dissipated.
- the plurality of elevations with undercuts results in a tight clamping between the bushing and engine block, which prevents the formation of a thermally insulating gap between the bush and engine block with different expansion coefficients due to different materials of bushing and engine block.
- Fig. 1 shows in perspective and Fig. 2 in top view, one of four Raugussbuchsen 1 to 4 existing bushing package 5.
- the 4 Raugussbuchsen 1 to 4 have roughened over their entire axial length outer surfaces.
- the common wall areas 6 to 8 adjacent jacks 1 to 4 a web width x, which corresponds to the other wall thickness of the Raugussbuchsen 1 to 4.
- the entire bushing package 5 is made in a single casting process from an aluminum-silicon alloy using the cast-on-casting or lost-foam casting process. Both casting methods are known from the prior art (see DE 199 58 185 A1 to the "lost-foam" casting method) and will not be explained here. In the manufacture of an engine block, the entire bushing package 5 is placed in the mold provided for this purpose and molded with casting material.
- the in the 3 and 4 illustrated cross sections 9 and 10 through parts of the wall of the Raugussbuchsen show embodiments of the roughening, wherein the roughening according to section 9 irregularly distributed elevations 11 and the roughening according to cross section 10 regularly distributed elevations 12 has.
- the elevations 10 and 11 are shaped so that they form undercuts 13 and 14, whose function is to anchor the Raugussbuchsen in the surrounding material of the engine block.
- the height of the elevations 11 and 12 and thus the depth y of the roughening have a value of 0.2 mm to 2 mm.
- the in the FIGS. 5 to 15 flattened Raugussbuchsen shown in cross section may consist of cast iron and are then preferably prepared by centrifugal casting. But they can also consist of an aluminum-silicon alloy, which opens up the possibility to produce the Raugussbuchsen in the stand casting process, by centrifugal casting or in the "lost-foam" casting process. Ultimately, it is possible to produce the Raugussbuchsen of a sintered metal. In this case, the bushes can already get their final, one- or two-sided flattened shape as part of the casting process. But it is also possible to flatten the bushes after casting by mechanical processing (milling).
- an engine block made of light metal such as aluminum, magnesium or an alloy with these metals
- the bushes can be joined together via their flattened areas, that is to say they are welded, soldered or adhesively bonded to one another via their flattened lateral surfaces so that spectacle-shaped arrangements of the bushings result on average.
- the bushing packages thus obtained are then inserted into the casting tool and encapsulated with the light metal of the engine block.
- FIG. 17 Another way to connect jacks together before pouring into an engine block is in Fig. 17 shown. Used here are bridges 45 and 46 which are glued or soldered to adjacent areas of the end faces 47 and 48 and 49 and 50 of the sockets 51 and 52 and connect the jacks 51 and 52 thereby.
- the bridges 45, 46 may be in the shape of round discs.
- Fig. 19 can be given to the bridges 45 ', 46' but also the shape of rectangular slices.
- the bridges are made of light metal or a light metal alloy.
- the gap between the sockets can not be arbitrarily narrow so that the light metal of the engine block flows through the gap between the sockets, fills the space between the sockets, and after cooling, makes a firm connection between the sockets creates.
- bushings are flattened on opposite jacket areas, it is necessary for this purpose to ensure that the bushings always assume a clearly defined rotational position when mounted on the sleeves, so that the gap between the flattened areas of the bushings retains its maximum width and not is reduced by partially twisted sockets or completely closed. This is achieved by the fact that the opposing flattenings of the bushing lateral surfaces in their lower, the crankshaft facing areas 53, 53 ', which in the Fig. 20 .
- the steps 53, 53 ' likewise have flattened regions 54, 54' ( Fig. 20 . 23, 24 ), which must be aligned parallel to each other when pushing the bushings on quills, so that the sockets fit on the sleeves, and thus ensure that the jacks always take a clearly defined rotational position to each other.
- the bushes can be joined to one another via the flattened regions 54, 54 'of the steps 53, 53', ie, glued together, or soldered.
- the width of the gap 55 is 1 mm to 3.5 mm for a Raugussbuchse with a wall thickness 56 of 2.5 mm and a depth 57 of the roughening of 1.5 mm.
- the web width 60 is 5.5 mm for bushes with a cylinder diameter 58 of 82 mm.
- Achievable here is a cylinder spacing 59 of 87.5 mm.
- Fig. 23 is in side view and in Fig. 24 to see well in plan view formed in the sleeve outer surface flattening 61, which has no roughening in contrast to the other sleeve outer surface.
- FIGS. 25 and 26 Another solution to the problem of keeping the flats of the Raugussbuchsen at a distance, and to ensure that the sockets are arranged in a clearly defined rotational position to each other, is according to FIGS. 25 and 26 in a spacer 62 arranged between the flattened regions 63 and 64.
- This has the further advantage that space is available for the cooling bores to be introduced into the engine block between the flattened regions 63 and 64 of the bushings held at a distance from one another.
- opposing areas of the outer surfaces of juxtaposed bushings may be concave.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Description
Die Erfindung betrifft eine Laufbuchse für einen Verbrennungsmotor nach dem Oberbegriff des Anspruches 1.The invention relates to a bushing for an internal combustion engine according to the preamble of
Aus der Europäischen Patentschrift
Hierbei ist jedoch nur der temperaturmäßig relativ wenig belastete, untere Buchsenbereich in den Motorblock eingegossen. Der obere Bereich der Laufbuchse ist temperaturmäßig sehr viel höher belastet, da hier die Verbrennung abläuft, und da die Laufbuchsen wegen ihrer seitlich abgeflachten Bereiche sehr eng nebeneinander angeordnet sind. Deshalb ist dieser Bereich gemäß Stand der Technik von einem Spalt umgeben, in den Wasser zum Kühlen dieses Bereiches der Laufbuchse eingeleitet wird. Dies ergibt eine sehr aufwendige Konstruktion, die zudem dem oberen Bereich der Laufbuchse, auf den die aus dem Zünddruck der hier stattfindenden Verbrennung resultierenden Kräfte einwirken, und der ausschließlich von einem Wassermantel umgeben ist, wenig Festigkeit bietet.Here, however, only the temperature moderately little loaded, lower bushing area is poured into the engine block. The upper portion of the liner is loaded much higher in temperature, since the combustion takes place here, and since the liners are arranged very close to each other because of their laterally flattened areas. Therefore, this prior art area is surrounded by a gap into which water is introduced to cool this portion of the bushing. This results in a very complex construction, which also offers little strength to the upper portion of the bushing, to which the forces resulting from the ignition pressure of the combustion occurring here take place, and which is surrounded exclusively by a water jacket.
Es ist somit Aufgabe der Erfindung, eine seitlich abgeflachte Laufbuchse zu schaffen, die platzsparend angeordnet werden kann, und die so ausgebildet ist, dass sie trotzdem vollständig in einen Motorblock eingegossen werden kann, ohne dass sich während des Motorbetriebes wegen mangelnder Wärmeabfuhr Temperaturprobleme ergeben.It is therefore an object of the invention to provide a laterally flattened liner, which can be arranged to save space, and which is designed so that they anyway can be completely poured into an engine block, without resulting during engine operation due to lack of heat dissipation temperature problems.
Gelöst wird die Aufgabe mit den im Kennzeichen des Hauptanspruches stehenden Merkmalen. Zweckmäßige Ausgestaltungen der Erfindung sind Gegenstand der Unteransprüche.The problem is solved with the features in the characterizing part of the main claim. Advantageous embodiments of the invention are the subject of the dependent claims.
Hierbei bietet die Aufrauung auf der Außenfläche der Raugussbuchse eine sehr große in Kontakt zum Material des Motorblockes stehende Außenfläche, über die die Verbrennungswärme gut abgeleitet werden kann. Zudem ergibt die Vielzahl der Erhebungen mit Hinterschnitten eine enge Verklammerung zwischen Buchse und Motorblock, die bei unterschiedlichen Ausdehnungskoeffizienten wegen unterschiedlicher Materialien von Buchse und Motorblock die Bildung eines thermisch isolierenden Spaltes zwischen Buchse und Motorblock verhindert.Here, the roughening on the outer surface of the Raugussbuchse provides a very large standing in contact with the material of the engine block outer surface over which the heat of combustion can be well dissipated. In addition, the plurality of elevations with undercuts results in a tight clamping between the bushing and engine block, which prevents the formation of a thermally insulating gap between the bush and engine block with different expansion coefficients due to different materials of bushing and engine block.
Einige Ausführungsbeispiele der Erfindung werden im Folgenden anhand der Zeichnungen beschrieben. Es zeigen
- Fig. 1
- ein aus 4 Raugussbuchsen bestehendes Buchsenpaket zur Verwendung in einem Vierzylindermotor,
- Fig. 2
- das Raugussbuchsenpaket gemäß
Fig. 1 in Draufsicht, - Fig. 3, 4
- vergrößerte Querschnitte durch Teile der Buchsenwand mit Ausgestaltungsmöglichkeiten deren Oberflächenrauheit,
- Fig. 5 - 7
- Beispiele abgeflachter Raugussbuchsen mit variabler Buchsenwanddicke und konstanter Tiefe der Aufrauung,
- Fig. 8
- eine Anordnung von 4 Raugussbuchsen mit elliptischer Außenkontur gemäß
Fig. 5 zur Verwendung in einem Vierzylindermotor, - Fig. 9 - 11
- Ausgestaltungen abgeflachter Raugussbuchsen mit konstanter Buchsenwanddicke und variabler Tiefe der Aufrauung,
- Fig. 12
- eine Anordnung von 4 Raugussbuchsen mit elliptischer Außenkontur gemäß
Fig. 9 zur Verwendung in einem Vierzylindermotor, - Fig. 13 - 15
- Beispiele abgeflachter Raugussbuchsen mit variabler Buchsenwanddicke, konstanter Tiefe der Aufrauung und ohne Raugussstrukturen auf den Außenflächen derjenigen Buchsenbereiche, die bei den zu Buchsenpaketen zusammengefassten Raugussbuchsen einander gegenüberliegen und abgeflacht sind,
- Fig. 16
- zwei über ihre abgeflachten Bereiche zusammengefügte Raugussbuchsen,
- Fig. 17
- zwei mit Hilfe zweier Brücken zusammengefügte Raugussbuchsen,
- Fig. 18
- eine Ausgestaltung einer Brücke zum Zusammenfügen von Raugussbuchsen,
- Fig. 19
- eine weitere Ausgestaltung einer Brücke zum Zusammenfügen von Raugussbuchsen,
- Fig. 20-24
- Raugussbuchsen mit je einer Abflachung, die in ihrem unteren Bereich eine Stufe aufweist,
- Fig. 25
- zwei aneinandergefügte Raugussbuchsen mit einem Abstandshalter zwischen den Abflachungen und
- Fig. 26
- eine vergrößerte Darstellung des Abstandshalters gemäß
Fig. 25 .
- Fig. 1
- a bushing package consisting of 4 bushings for use in a four-cylinder engine,
- Fig. 2
- the Raugussbuchsenpaket according to
Fig. 1 in plan view, - Fig. 3, 4
- enlarged cross-sections through parts of the bushing wall with possibilities of designing their surface roughness,
- Fig . 5 - 7
- Examples of flattened Raugussbuchsen with variable socket wall thickness and constant depth of roughening,
- Fig. 8
- an arrangement of 4 Raugussbuchsen with elliptical outer contour according to
Fig. 5 for use in a four-cylinder engine, - Fig. 9 - 11
- Embodiments of flattened Raugussbuchsen with constant bushing wall thickness and variable depth of the roughening,
- Fig. 12
- an arrangement of 4 Raugussbuchsen with elliptical outer contour according to
Fig. 9 for use in a four-cylinder engine, - Fig. 13 - 15
- Examples of flattened Raugussbuchsen with variable bushing wall thickness, constant depth of roughening and without Raugussstrukturen on the outer surfaces of those bushing areas which face each other and are flattened in the Raugussbuchsen combined into bushing packages,
- Fig. 16
- two Raugussbuchsen assembled over their flattened areas,
- Fig. 17
- two Raugussbuchsen, assembled with the help of two bridges,
- Fig. 18
- an embodiment of a bridge for assembling Raugussbuchsen,
- Fig. 19
- Another embodiment of a bridge for joining Raugussbuchsen,
- Fig. 20-24
- Raugussbuchsen with one flattening, which has a step in its lower part,
- Fig. 25
- two joined Raugussbuchsen with a spacer between the flats and
- Fig. 26
- an enlarged view of the spacer according to
Fig. 25 ,
Das gesamte Buchsenpaket 5 wird in einem einzigen Gussverfahren aus einer Aluminium-Siliziumlegierung hergestellt, wobei das Standgussverfahren oder das "lost-foam"-Gussverfahren angewandt wird. Beide Gussverfahren sind aus dem Stand der Technik bekannt (siehe
Die in den
Die in den
Bei der Herstellung eines Motorblockes aus Leichtmetall, wie beispielsweise aus Aluminium, Magnesium oder aus einer Legierung mit diesen Metallen gibt es zum einen die Möglichkeit, die Buchsen auf Pinolen des Gießwerkzeuges aufzustecken, derart auszurichten, dass die abgeflachten Bereiche der Buchsen einander gegenüberliegen, und die Buchsen dann mit dem Leichtmetall des Motorblockes zu umgießen. Zum anderen können die Buchsen über ihre Abflachungen aneinandergefügt werden, d.h., über ihre abgeflachten Mantelflächen miteinander verschweißt, verlötet oder verklebt werden, sodass sich im Schnitt brillenförmige Anordnungen der Buchsen ergeben. Die so erhaltenen Buchsenpakete werden dann in das Gießwerkzeug eingelegt und mit dem Leichtmetall des Motorblockes umgossen.In the manufacture of an engine block made of light metal, such as aluminum, magnesium or an alloy with these metals, there is the opportunity to plug the sockets on quills of the casting tool, to align so that the flattened portions of the bushes face each other, and the Bushings then with the light metal of the engine block to encase. On the other hand, the bushes can be joined together via their flattened areas, that is to say they are welded, soldered or adhesively bonded to one another via their flattened lateral surfaces so that spectacle-shaped arrangements of the bushings result on average. The bushing packages thus obtained are then inserted into the casting tool and encapsulated with the light metal of the engine block.
Die folgenden in den
-
Fig. 5 : Dargestelltist eine Buchse 15 mit im Querschnitt elliptischer Außenform, variablerDicke der Buchsenwand 19 und konstanter Tiefe derAufrauung 20. -
Fig. 6 : Dargestelltist eine Buchse 16 mit variabler Dicke der Buchsenwand 19', mit konstanter Tiefe der Aufrauung 20 und mit einer Außenform, die im Querschnitt aus vier näherungsweise gleich großen, kreisbogenförmigen Segmenten 21bis 24 besteht, wobei die einander gegenüberliegenden Segmente 21 und 22 dickere Bereiche der Buchsenwand 19' und die einander gegenüberliegenden Segmente 23 und 24 dünnere Bereiche der Buchsenwand 19', d.h., deren abgeflachte Bereiche nach außen begrenzen.
Fig. 7 : Dargestelltist eine Buchse 17 mit variablerDicke der Buchsenwand 19", mit konstanter Tiefe der Aufrauung 20 und mit einer Außenform, die sich im Querschnitt aus zwei einander gegenüberliegenden kreisbogenförmigen Segmenten 25 und 26 und zwei einander gegenüberliegenden, ebenen Segmenten 27 und 28 zusammensetzt. Hierbei werden die einander gegenüberliegenden abgeflachten Bereiche der Buchse 17von den Segmenten 27 und 28 nach außen begrenzt.
Fig. 8 zeigt eine Möglichkeit, dieRaugussbuchsen 15 mit elliptischer Außenkontur auf platzsparende Weise nebeneinander anzuordnen, sodass sich ein für einen Vierzylindermotor geeignetes Buchsenpaket 18 ergibt. Hierbei begrenzen die Nebenachsenbereiche der elliptischen Kontur die abgeflachten Bereiche der Buchsen 15, welche abgeflachten Bereiche bei der Anordnung der Buchsen 15 zu einem Buchsenpaket 18 auf Abstand einander gegenüberliegen.
Fig. 9 : Dargestelltist eine Buchse 29 mit konstanterDicke der Buchsenwand 32, mit variabler Tiefe der Aufrauung 33 und mit einer im Querschnitt elliptischen Außenkontur, die der Außenform der Buchse 15 gemäßFig. 5 gleicht.
Fig. 10 : Dargestelltist eine Buchse 30 mit konstanterDicke der Buchsenwand 32, mit variabler Tiefe der Aufrauung 33' und mit einer im Querschnitt aus kreisbogenförmigen Segmenten bestehenden Außenkontur, die der Außenform der Buchse 16 gemäßFig. 6 gleicht.
Fig. 11 : Dargestelltist eine Buchse 31 mit konstanterDicke der Buchsenwand 32, mit variabler Tiefe der Aufrauung 33" und mit einer im Querschnitt aus zwei kreisbogenförmigen Segmenten und zwei ebenen Segmenten, die jeweils einander gegenüberliegen, gebildeten Außenkontur, die der Außenform der inFig. 7 dargestellten Buchse 17 gleicht. Hergestellt werden die in denFig. 9 dargestellten Raugussbuchsen 29bis 11bis 31 im Schleudergussverfahren, wobei die Variation der Tiefe der Aufrauungen 33, 33'und 33" durch eine entsprechende Einstellung der Verfahrensparameter erreichbar ist. -
Fig. 12 zeigteine Anordnung von 4 der inFig. 9 gezeigten Raugussbuchsen 29 zu einem Buchsenpaket 34 ähnlich dem inFig. 8 dargestellten Buchsenpaket 18 zur Verwendung in einem Vierzylindermotor. Die Raugussbuchsen der gezeigten Art können hierbei auf einenAbstand z von 0,5 mm bis 0,05 mm nebeneinander angeordnet werden. -
Fig. 13 : Dargestelltist eine Buchse 35 mit variabler Buchsenwanddicke, konstanter Tiefe der Aufrauung und einer elliptischen Außenkontur, die der Außenkontur der inFig. 5 dargestellten Buchse 15 gleicht. Die einander gegenüberliegenden, abgeflachten Buchsenbereiche 38 und 39 weisen hierbei keine Raugussstrukturen auf. -
Fig. 14 : Dargestelltist eine Buchse 36 mit variabler Buchsenwanddicke, konstanter Tiefe der Aufrauung und einer im Querschnitt aus mehreren kreisbogenförmigen Segmenten bestehenden Außenkontur, die der Außenform der inFig. 6 dargestellten Buchse 16 gleicht. Die einander gegenüberliegenden, abgeflachten Buchsenbereiche 40 und 41 weisen keine Raugussstrukturen auf. -
Fig. 15 : Dargestelltist eine Buchse 37 mit variabler Buchsenwanddicke, konstanter Tiefe der Aufrauung und einer Außenkontur, die im Querschnitt aus zwei kreisbogenförmigen und zwei ebenen Segmenten besteht, und die der Außenform der inFig. 7 dargestellten Buchse 17 gleicht. Hierbei kann, wenn die Buchse das erste oder das letzte Element eines in einer Reihe angeordneten Buchsenpaketes ist,ein ebenes Segment 43 der Außenkontur mit einer Raugussstruktur versehen sein und dasdem gegenüberliegende Segment 42 ohne Raugussstruktur ausgebildet sein. Hierbei können diejenigen Segmente 38bis 42 der Außenkonturen der Raugussbuchsen 35bis 37, die keine Raugussstrukturen aufweisen, bereits im Rahmen der Gießvorganges hergestellt werden. Möglich ist aber auch, die gesamte Mantelfläche der Buchse mit einer Raugussstruktur zu versehen und im Anschluss daran die Raugussstrukturen der abzuflachenden Buchsenbereiche wegzufräsen.
-
Fig. 5 A bush 15 with an elliptical outer shape, variable thickness of thebushing wall 19 and a constant depth of the roughening 20 is shown. -
Fig. 6 FIG. 4 illustrates avariable thickness bushing 16 of the bushing wall 19 ', having a constant depth of roughening 20 and having an outer shape that is four cross-sectionally approximately circulararcuate segments 21 to 24, with the 21 and 22 being thicker Portions of the bushing wall 19 'and the opposingopposed segments 23 and 24 thinner portions of the bushing wall 19', ie, limit their flattened areas to the outside.segments
Fig. 7 FIG. 4 illustrates avariable thickness bushing 17 ofbushing wall 19 ", with a constant depth of roughening 20 and an outer shape which is composed in cross section of two opposing circular 25 and 26 and two oppositearcuate segments 27 and 28. Here, the opposing flattened portions of theplanar segments bushing 17 are bounded by the 27 and 28 to the outside.segments
Fig. 8 shows a way to arrange theRaugussbuchsen 15 elliptical outer contour in a space-saving manner next to each other, so that there is a suitable for a four-cylinderengine bushing package 18. In this case, the minor axis regions of the elliptical contour limit the flattened regions of thebushings 15, which flattened regions lie opposite each other in the arrangement of thebushes 15 to form abushing package 18.
Fig. 9 FIG. 2 shows abushing 29 of constant thickness of thebushing wall 32, with variable depth of theroughening 33 and with an elliptical outer contour in the cross-section corresponding to the outer shape of thebush 15 according to FIGFig. 5 like.
Fig. 10 FIG. 1 shows abushing 30 with a constant thickness of thebushing wall 32, with a variable depth of the roughening 33 'and with an outer contour consisting of circular-arc-shaped segments in cross-section corresponding to the outer shape of thebushing 16Fig. 6 like.
Fig. 11 FIG. 1 shows abushing 31 of constant thickness, thebushing wall 32, with variable depth of the roughening 33 "and with an outer contour formed in cross-section from two arcuate segments and two planar segments, which face each other, corresponding to the outer shape of the inFig. 7 illustratedsocket 17 is similar. The are made in theFig. 9 to 11 shownRaugussbuchsen 29 to 31 by centrifugal casting, the variation of the depth of the 33, 33 'and 33 "can be achieved by a corresponding adjustment of the process parameters.roughening -
Fig. 12 FIG. 4 shows an arrangement of FIG. 4 of FIGFig. 9 shownRaugussbuchsen 29 to asocket package 34 similar to the inFig. 8 shown bushingpackage 18 for use in a four-cylinder engine. The Raugussbuchsen the type shown here can be arranged side by side to a distance z of 0.5 mm to 0.05 mm. -
Fig. 13 : Shown is abushing 35 with variable bushing wall thickness, constant depth of roughening and an elliptical outer contour corresponding to the outer contour of the inFig. 5 illustratedsocket 15 is similar. The mutually opposite, flattened 38 and 39 in this case have no Raugussstrukturen.bushing areas -
Fig. 14 FIG. 3 shows abushing 36 with variable bushing wall thickness, constant depth of the roughening and an outer contour consisting of a plurality of arcuate segments in cross-section, corresponding to the outer shape of the inFig. 6 representedsocket 16 is similar. The opposing, flattened 40 and 41 have no Raugussstrukturen.sleeve portions -
Fig. 15 FIG. 3 shows abushing 37 with variable bushing wall thickness, constant depth of roughening and an outer contour, which in cross section consists of two arcuate and two planar segments, and which corresponds to the outer shape of the inFig. 7 illustratedsocket 17 is similar. Here, if the bushing is the first or the last element of a bushing package arranged in a row, aflat segment 43 of the outer contour may be provided with a Raugussstruktur and theopposite segment 42 may be formed without Raugussstruktur. In this case, thosesegments 38 to 42 of the outer contours of theRaugussbuchsen 35 to 37, which have no Raugussstrukturen, already be prepared in the context of the casting process. But it is also possible to provide the entire lateral surface of the sleeve with a Raugussstruktur and subsequently milled away the Raugussstrukturen the flattened bushing areas.
Die in den
Eine weitere Möglichkeit, Buchsen vor dem Eingießen in einen Motorblock miteinander zu verbinden, ist in
Gemäß
Wenn Buchsen vor dem Vergießen auf Pinolen befestigt werden, kann der Spalt zwischen dem Buchsen nicht beliebig eng sein, damit das Leichtmetall des Motorblockes durch den Spalt zwischen den Buchsen fließt, den Raum zwischen den Buchsen ausfüllt und nach dem Erkalten eine feste Verbindung zwischen den Buchsen schafft. Sind Buchsen auf einander gegenüberliegenden Mantelbereichen abgeflacht, ist es zu diesem Zweck erforderlich, dafür zu sorgen, dass die Buchsen bei der Montage auf den Pinolen immer eine eindeutig definierte Drehstellung einnehmen, damit der Spalt zwischen den abgeflachten Bereichen der Buchsen seine maximale Breite beibehält und nicht durch teilweise verdrehte Buchsen verkleinert oder komplett verschlossen wird. Erreichbar ist dies dadurch, dass die einander gegenüberliegenden Abflachungen der Buchsenmantelflächen in ihren unteren, der Kurbelwelle zugewandten Bereichen Stufen 53, 53' aufweisen, die in den
Idealerweise beträgt die Weite des Spaltes 55 1 mm bis 3,5 mm bei einer Raugussbuchse mit einer Wanddicke 56 von 2,5 mm und einer Tiefe 57 der Aufrauung von 1,5 mm. Die Stegbreite 60 beträgt 5,5 mm bei Buchsen mit einem Zylinderdurchmesser 58 von 82 mm. Erreichbar ist hierbei ein Zylinderabstand 59 von 87,5 mm.Ideally, the width of the
In
Eine weitere Lösung des Problemes, die Abflachungen der Raugussbuchsen auf Abstand zu halten, und dafür zu sorgen, dass die Buchsen in einer eindeutig definierten Drehstellung zueinander angeordnet sind, besteht gemäß
Gemäß einer in den Figuren nicht dargestellten Ausgestaltung der Raugussbuchsen können einander gegenüberliegende Bereiche der Außenflächen nebeneinander angeordneter Buchsen konkav ausgebildet sein.According to an embodiment of the Raugussbuchsen not shown in the figures, opposing areas of the outer surfaces of juxtaposed bushings may be concave.
- xx
- Stegbreiteweb width
- yy
- Tiefe der AufrauungDepth of roughening
- zz
- Abstand zwischen zwei RaugussbuchsenDistance between two Raugussbuchsen
- 1 bis 41 to 4
- Raugussbuchserough-cast sleeve
- 55
- Buchsenpaketsleeve package
- 6 bis 86 to 8
- Wandbereichwall area
- 9, 109, 10
- Querschnittcross-section
- 11, 1211, 12
- Erhebungsurvey
- 13,1413.14
- Hinterschnittundercut
- 15 bis 1715 to 17
- Buchse, LaufbuchseBushing, bushing
- 1818
- Buchsenpaketsleeve package
- 19, 19', 19"19, 19 ', 19 "
- Buchsenwandwall socket
- 2020
- Aufrauungroughening
- 21 bis 2421 to 24
-
Segment der Außenform der Buchse 16Segment of the outer shape of the
socket 16 - 25 bis 2825 to 28
-
Segment der Außenform der Buchse 17Segment of the outer shape of the
bush 17 - 29 bis 3129 to 31
- Buchse, LaufbuchseBushing, bushing
- 3232
- Buchsenwandwall socket
- 33, 33', 33"33, 33 ', 33 "
- Aufrauungroughening
- 3434
- Buchsenpaketsleeve package
- 35 bis 3735 to 37
- Buchse, LaufbuchseBushing, bushing
- 38, 3938, 39
-
abgeflachter Bereich der Buchse 35flattened portion of the
bush 35 - 40, 4140, 41
-
abgeflachter Bereich der Buchse 36flattened portion of the
bush 36 - 42, 4342, 43
-
Segment der Außenkontur der Buchse 37Segment of the outer contour of the
bush 37 - 4444
- Klebe- oder LötschichtAdhesive or solder layer
- 45, 45', 46, 46'45, 45 ', 46, 46'
- Brückebridge
- 47 bis 5047 to 50
- Stirnseitefront
- 51, 5251, 52
- Buchse, LaufbuchseBushing, bushing
- 53, 53'53, 53 '
- Stufestep
- 54, 54'54, 54 '
-
abgeflachter Bereich der Stufe 53flattened area of
level 53 - 5555
- Spaltbreitegap width
- 5656
- Wanddickewall thickness
- 5757
- Tiefe der AufrauungDepth of roughening
- 5858
- ZylinderdurchmesserCylinder diameter
- 6060
- Stegbreiteweb width
- 6161
- Abflachungflattening
- 6262
- Abstandhalterspacer
- 63, 6463, 64
- abgeflachter Bereichflattened area
Claims (9)
- Cylinder sleeve (29) for an internal combustion engine, the outer surface of which comprises at least one flat region (54, 54', 61) that extends along the entire axial length thereof, and comprises, at least in the lower region thereof facing the crankcase, at least one engaging section having at least one projection comprising an undercut,
characterised in that
the cylinder sleeve is embodied as a rough cast sleeve whose outer surface comprises a rough zone (33) that extends along the entire axial length thereof and consists of a plurality of elevations (11, 12) with undercuts (13, 14),
the cylinder sleeve comprises an outer contour that is elliptical in cross-section, and
the outer shape of the cylinder sleeve is formed at constant wall thickness (32) by a depth of the rough zone (33) varying over the circumference. - Cylinder sleeve according to claim 1, characterised in that the height of the elevations (11, 12) is 0.2 mm to 2 mm.
- Cylinder sleeve according to one of the preceding claims, characterised in that the at least one flat region is provided on the underside thereof facing the crankcase, with a step (53) having a radially outer flat region (54).
- Cylinder sleeve according to one of the preceding claims, characterised in that said cylinder sleeve consists of cast-iron and is produced by the centrifugal casting method.
- Cylinder sleeve according to claim 1 to 4, characterised in that said cylinder sleeve consists of an aluminium-silicon alloy.
- Cylinder sleeve according to claim 5, characterised in that the cylinder sleeve is produced by the static casting method.
- Cylinder sleeve according to claim 5, characterised in that the cylinder sleeve is produced by the centrifugal casting method.
- Cylinder sleeve according to claim 5, characterised in that the cylinder sleeve is produced by the lost-foam casting method.
- Cylinder sleeve according to claim 1 to 3, characterised in that the cylinder sleeve consists of sintered metal.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004007774A DE102004007774A1 (en) | 2004-02-18 | 2004-02-18 | Bushing for an internal combustion engine |
PCT/DE2005/000283 WO2005078265A1 (en) | 2004-02-18 | 2005-02-18 | Cylinder sleeve for an internal combustion engine |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1721072A1 EP1721072A1 (en) | 2006-11-15 |
EP1721072B1 true EP1721072B1 (en) | 2017-04-05 |
Family
ID=34853501
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05714992.4A Not-in-force EP1721072B1 (en) | 2004-02-18 | 2005-02-18 | Cylinder sleeve for an internal combustion engine |
Country Status (8)
Country | Link |
---|---|
US (1) | US7806098B2 (en) |
EP (1) | EP1721072B1 (en) |
JP (1) | JP4653762B2 (en) |
KR (1) | KR101279846B1 (en) |
CN (1) | CN2900814Y (en) |
BR (1) | BRPI0507731A (en) |
DE (1) | DE102004007774A1 (en) |
WO (1) | WO2005078265A1 (en) |
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-
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- 2005-02-18 US US10/589,792 patent/US7806098B2/en not_active Expired - Fee Related
- 2005-02-18 BR BRPI0507731-1A patent/BRPI0507731A/en not_active Application Discontinuation
- 2005-02-18 KR KR1020067016912A patent/KR101279846B1/en active IP Right Grant
- 2005-02-18 WO PCT/DE2005/000283 patent/WO2005078265A1/en active Application Filing
- 2005-02-18 JP JP2006553431A patent/JP4653762B2/en not_active Expired - Fee Related
- 2005-02-18 CN CNU200590000003XU patent/CN2900814Y/en not_active Expired - Lifetime
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Also Published As
Publication number | Publication date |
---|---|
JP2007524787A (en) | 2007-08-30 |
CN2900814Y (en) | 2007-05-16 |
BRPI0507731A (en) | 2007-07-10 |
KR20060129027A (en) | 2006-12-14 |
DE102004007774A1 (en) | 2005-09-15 |
EP1721072A1 (en) | 2006-11-15 |
JP4653762B2 (en) | 2011-03-16 |
KR101279846B1 (en) | 2013-06-28 |
US20070209627A1 (en) | 2007-09-13 |
US7806098B2 (en) | 2010-10-05 |
WO2005078265A1 (en) | 2005-08-25 |
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