GB2297053A - .Cylinder liner for a reciprocating piston engine and method of producing such a cylinder liner. - Google Patents

.Cylinder liner for a reciprocating piston engine and method of producing such a cylinder liner. Download PDF

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Publication number
GB2297053A
GB2297053A GB9604138A GB9604138A GB2297053A GB 2297053 A GB2297053 A GB 2297053A GB 9604138 A GB9604138 A GB 9604138A GB 9604138 A GB9604138 A GB 9604138A GB 2297053 A GB2297053 A GB 2297053A
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United Kingdom
Prior art keywords
particles
cylinder liner
alloy
honing
primary crystals
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Granted
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GB9604138A
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GB9604138D0 (en
GB2297053B (en
Inventor
Franz Ruckert
Peter Stocker
Roland Biedermann
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Daimler Benz AG
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Daimler Benz AG
Mercedes Benz AG
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Priority claimed from DE4438550A external-priority patent/DE4438550C2/en
Application filed by Daimler Benz AG, Mercedes Benz AG filed Critical Daimler Benz AG
Publication of GB9604138D0 publication Critical patent/GB9604138D0/en
Publication of GB2297053A publication Critical patent/GB2297053A/en
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Publication of GB2297053B publication Critical patent/GB2297053B/en
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Classifications

    • 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
    • F02F7/0085Materials for constructing engines or their parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24BMACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B33/00Honing machines or devices; Accessories therefor
    • B24B33/02Honing machines or devices; Accessories therefor designed for working internal surfaces of revolution, e.g. of cylindrical or conical shapes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24BMACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B37/00Lapping machines or devices; Accessories
    • B24B37/02Lapping machines or devices; Accessories designed for working surfaces of revolution
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • 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 
    • F02F1/004Cylinder liners
    • 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
    • F02F7/0085Materials for constructing engines or their parts
    • F02F2007/009Hypereutectic aluminum, e.g. aluminum alloys with high SI content
    • 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Geometry (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

The invention relates to a cylinder liner sealed into a reciprocating piston engine and comprising a strongly supereutectic aluminium/silicon alloy which is free of melt-independent particles of hard material and which is composed in such a way that fine silicon primary crystals 8 and intermetallic phases 9, 10 automatically form from the melt as hard particles. By means of spray compaction, a blank is allowed to grow from finely sprayed melt droplets, with a fine distribution of the hard particles being produced by the setting of small melt droplets. The blank can then be formed by cold extrusion to give a shape approximating the cylinder lining. After subsequent premachining, the face is fine machined, subsequently honed in at least one stage and then the hard particles lying at the face are exposed, forming plateau areas of the particles which project above the remaining surface of the base microstructure of the alloy. The mechanical exposure of the primary crystals or particles is carried out in the manner of a honing process using felt strips 16 which are cylindrically shaped on the outside and a slurry of SiC particles in honing oil.

Description

Cylinder liner for a reciprocating piston engine and method of producing such a cylinder liner The invention relates to a cylinder liner comprising a supereutectic aluminium/silicon alloy for sealing into a reciprocating piston engine, and to a method of forming such a liner.
EP 367 229 Al discloses a cylinder liner which is produced from metal powder and mixed-in graphite particles (from 0.5 to 3%; with a particle diameter at most 10 pm or less, measured in a plane perpendicular to the cylinder axis) and particles of hard material without sharp edges (from 3 to 5%; particle diameter at most 30 pm, on average 10 pm or less), in particular aluminium oxide.The metal powder is first produced on its own, i.e. without mixed-in nonmetallic particles, by air atomization of a supereutectic aluminium/silicon alloy having the following composition the remainder being aluminium (figures in % by weight based on the total metal content of the alloy, i.e. without the particles of hard material and amounts of graphite foreign to the melt): Silicon from 16 to 18%, Iron from 4 to 6%, Copper from 2 to 4%, Magnesium from 0.5 to 2% and Manganese from 0.1 to 0.8%.
The metal powder is mixed with nonmetallic particles and this powder mixture is pressed at about 2000 bar to give a preferably tubular body. This powdermetallurgically produced blank is inserted into a soft aluminium tube of corresponding shape and the double-layer tube thus obtained is jointly sintered and shaped in an extrusion process, preferably at elevated temperatures, to give a tubular blank from which the individual cylinder liners can be produced. The embedded particles of hard material are intended to give the cylinder liner good wear resistance, while the graphite particles serve as dry lubricant. To avoid oxidation of the graphite particles, the hot extrusion should take place with exclusion of oxygen.
There is also the danger of the graphite reacting with the silicon at high processing temperatures and forming hard SiC on the surface, which impairs the dry-lubrication properties of the embedded graphite particles. Since the powder mixture is always more or less complete, the local occurrence on the surface of the workpiece of more or less great concentration fluctuations of particles of hard material and/or of graphite particles can never be entirely ruled out. Owing to the embedded particles of hard material, the hot-pressing die wears relatively quickly, because the particles of hard material, despite their rounded edges, still have a strong abrasive action in any case, only a partial rounding of the edges on the particles formed by crushing can be achieved with justifiable effort.The subsequent machining of the face of the cylinder liner is also associated with high tool wear and thus with high tool costs. The particles of hard material exposed on the face have sharp edges after the surface machining and cause relatively high wear of the piston and the piston rings, so that these have to be made of a wear-resistant material or be provided with an appropriately wear-resistant coating. Overall, the known cylinder liner is not only relatively expensive because of the starting materials with a plurality of separate components, but the high tool costs associated with the plastic forming and the cutting machining drive up the costs per item.Apart from this, the way in which the known cylinder liners are produced from a heterogeneous powder mixture involves the danger of inhomogeneities which may result in impairment of their function, and thus in rejects, but in any case require complex quality control. In addition, it requires complicated piston constructions in engine operation, which make the entire reciprocating piston engine more expensive.
Mention may also be made of US-A 4 938 810 which likewise discloses a powder-metallurgically produced cylinder liner. In that document, a great number of alloy examples are provided and measurement and operating data of the cylinder liners produced therewith are also given. The silicon contents of the examples provided are in the range from 17.2 to 23.6%, although in this respect the claim of this document recommends a wider range of from 10 to 30%, which extends into the subeutectic region. At least one of the metals nickel, iron or manganese should likewise be present in the alloy, indeed at least to the extent of 5% or (iron) to the extent of at least 3%.As a representative, mention is here made only of an alloy composition in % by weight, the remainder is aluminium; zinc and manganese contents are not specified, from which it can be concluded that these metals should not be present apart from traces: Silicon: 22.8%, Copper: 3.1%, Magnesium: 1.3%, Iron: 0.5% and Nickel: 8.0%.
The nickel content in the alloy example given is very high.
A blank for a cylinder liner is hot-extruded from the powder mixture.
Finally, mention may also be made of US-A 4 155 756 which is concerned with the same subject. In that document, inter alia, the following composition of a powdermetallurgically produced cylinder liner is given as an example of others - remainder aluminium: Silicon: 25%, Copper: 4.3%, Magnesium: 0.65% and Iron: 0.8%.
The present invention seeks to provide a method of producing a cylinder liner comprising a supereutetctic aluminium/silicon alloy.
According to the present invention there is provided a method of producing a cylinder liner comprising a supereutectic aluminium/silicon alloy, in which the face thereof is first roughly premachined and then fine machined by means of boring or turning and subsequently honed in at least one stage and in which the particles lying in the face which are harder than the base microstructure of the alloy, such as silicon crystals and/or intermetallic phases, are then exposed in such a way that plateau areas of the particles project above the remaining surface of the base microstructure of the alloy, comprising mechanically exposing primary crystals or particles embedded at the surface out of the face of the cylinder liner by means of a grinding or polishing process using at least one compliant shaped polishing or grinding body and an abrasive, amorphous grinding or polishing medium containing particles of hard material whose grain size is less than or at most the same as the desired roughness.
Owing to the specific alloy composition of the material for the cylinder liner, silicon primary crystals and intermetallic phases are formed directly from the melt; the mixing in of separate hard particles can therefore be omitted. Furthermore, the spray compaction of the alloy, which can readily be mastered in methodology and is comparatively inexpensive, is used together with subsequent, energy-saving cold extrusion of the blank. This method gives a particularly low oxidation of the droplet surfaces and a particularly low porosity of the liner. The alloy compositions mentioned hereinafter are optimized for use with iron-coated pistons (alloy A) or with uncoated aluminium pistons (alloy B). The hard particles formed from the melt possess, on the one hand, a high hardness and give the face good wear resistance, on the other hand these hard particles formed from the melt do not seriously impede the machining of the material, so that the face is sufficiently readily machinable. Owing to the formation of the primary crystals and intermetallic phases in each melt droplet sprayed onto and subsequently solidifying on the growing blank, the process results in a very uniform distribution of the hard particles in the workpiece. The particles formed from the melt are also less angular and tribologically less aggressive than crushed particles.Moreover, the metallic hard particles formed from the melt are more intimately embedded in the basic alloy microstructure than are nonmetallic crushed particles which have been mixed in, so that the danger of crack formation at the hard material boundaries is less. In addition, the hard particles formed from the melt display a better running-in behaviour and a lower abrasive aggressivity towards the piston and its rings, so that higher lifetimes result or, with acceptance of conventional lifetimes, less complex designs of the piston can be permitted.
Advantageous embodiments of the invention are illustrated below with the aid of the drawings; in the drawings: Fig. 1 shows a partially sectioned view of a reciprocating piston engine having a sealed-in cylinder liner, Fig. 2 shows a greatly magnified part of a cross-section through a region of the cylinder liner close to the surface, taken parallel to a cylinder wall line, Fig. 2a shows a further enlargement of a detail of Figure 2, Fig. 3 is a bar graph showing the particle sizes of the various hard particles formed from the melt and Fig. 4 shows a modified honing machine for mechanically exposing the hard particles out of the surface of the cylinder liner.
The reciprocating piston engine partly shown in Figure 1 comprises a diecast crankcase 2 in which there is arranged the cylinder wall 4 for accommodating a cylinder liner 6 in which a piston 3 is installed so as to be able to move up and down. On top of the crankcase 2 there is attached a cylinder head 1 fitted with the devices for charge change and charge ignition. Within the crankcase there is provided, around the cylinder wall 4, a hollow space for forming a water jacket 5 for cylinder cooling.
The cylinder liner 6 is made as an individual part by a method described in detail below of a supereutectic composition, on the subject of which further details will likewise be given below, then is sealed as a blank part into the crankcase 2 and is machined together with the crankcase.
For this purpose, inter alia, the face of the cylinder liner is first roughly premachined and subsequently fine machined by means of boring or turning. The face 7 is subsequently honed in at least one stage. After honing, the particles lying in the face which are harder than the base microstructure of the alloy, such as silicon crystals and intermetallic phases, are exposed out of the face in such a way that plateau surfaces of the particles project above the remaining surface of the base microstructure of the alloy.
To improve the cylinder liners in respect of the wear resistance and the lubricating oil consumption and thus to improve the emission of hydrocarbons by the internal combustion engine, the invention provides a series of measures which jointly act together for this purpose.
Firstly, mention should here be made of optimization of the composition of the alloy, where two alternative types of alloy have here been found to be optimal, with one alloy type A being recommended for use together with iron-coated pistons and the other alloy type B being optimized in connection with uncoated aluminium pistons. The percentages below are by weight. The alloy A has the following composition: Silicon from 23.0 to 28.0%, preferably about 25%, Magnesium from 0.80 to 2.0%, preferably about 1.2%, Copper from 3.0 to 4.5%, preferably about 3.9%, Iron max. 0.25% Manganese, nickel and zinc max. 0.01% and the remainder aluminium.
The alloy B for operation together with uncoated aluminium pistons has the same composition as the alloy A in respect of the proportions of silicon, copper, manganese and zinc; only the iron and nickel contents are somewhat higher, namely Iron from 1.0 to 1.4% and Nickel from 1.0 to 5.0%.
A melt of the aluminium/silicon alloy is finely sprayed into an oxygen-free atmosphere and the mist of melt is deposited to give a growing body, first producing a knob containing fine-grained silicon primary crystals 8 and intermetallic phases 9 and 10, with the intermetallic phases being those containing magnesium and silicon (Mg2Si) and containing aluminium and copper (A12Cu). The atomized melt is very quickly cooled in a jet of nitrogen, with cooling rates in the range of 105 K/sec being achieved.This socalled spray compacting enables production of a microstructure having a very narrow grain size distribution with a range of about + 5 ... 10 pm about a mean value, with the mean value being able to be adjusted within a relatively wide particle size range from about 7 to 200 pm. A very fine grain setting, particle size of Mg2Si from 2 to 10 Mm, is used here, so that a correspondingly fine microstructure having a fine and uniform silicon distribution is formed.
Each powder particle contains all the alloy constituents.
The powder particles are sprayed onto a rotating plate on which the knob mentioned having a diameter of, for example, 300 or 1000 mm grows. This depends on the design of the apparatus. Subsequently, the knobs have to be extruded on an extruder to form tubes. It is also conceivable that the knob is not allowed to grow axially on a rotating plate, but the atomized melt is allowed to grow radially on a rotating cylinder, so that an essentially tubular preproduct is formed.
During spraying, the melt is so finely atomized that the silicon primary crystals 8 and the intermetallic phases 9 and 10 which form in the growing knob have very small grain sizes of the following dimensions: Si primary crystals: from 2 to 15 pm, preferably from 4 to 10 pm, A12Cu phase: from 0.1 to 5.0 pm, preferably from 0.8 to 1.8 Crm, Mg2Si phase: from 2.0 to 10.0 pm, preferably from 2.5 to 4.5 pm.
This fine grained nature gives, on the one hand, a finely dispersed distribution of the hard particles within the base microstructure of the alloy and a homogeneous material is obtained. Since a single melt is atomized, no mixing inhomogeneities can be formed. The compacting of the atomized melt droplets also results in a very intimate bonding of the droplets to one another and in substantial avoidance of porosity.
The method of spray compacting aluminium alloys is known per se and is intended to be used here only as an advantageous procedure. The extrusion of knobs produced in this way to give tubes from which individual liners can then be cut is likewise known per se. For this reason, no further details of these methods shall be given here.
The blanks of the cylinder liner produced in such a way and possibly brought to a certain further-processing dimension by machining are sealed into a crankcase comprising a readily castable aluminium alloy, with a pressure diecasting process being preferably recommended here. For this purpose, the prefabricated cylinder liners to be sealed in are pushed onto a guide pin with the diecasting mould open, the mould is closed and the diecasting material is injected. Owing to the fast cooling time and the ability to cool the cylinder liner to be sealed in via the guide pin, there is no danger of the material of the cylinder liner being thermally affected in an uncontrolled manner by the melt of the diecast part. The alloy used for diecasting is subeutectic and therefore readily processable by casting.
Moreover, the thermal expansion of the alloy of the diecast part on the one hand and the cylinder liner on the other hand is approximately equal, so that no uncontrolled thermal stresses occur between the two.
After sealing the cylinder liner into the crankcase, this is machined on the appropriate surfaces, particularly on the faces 7 of the cylinder liner 6. These machining processes - mention is here made only of boring and honing are also known per se, for which reason no further details on them will be given here. Subsequent to the honing, the silicon primary crystals 8 and the particles of intermetallic phases 9 and 10 embedded at the surface have to be exposed. This exposure is usually carried out chemically by means of etching, which is not only timeconsuming, but is also associated with a certain pollution of the workplace environment by evaporation of etching liquid. In addition, a certain inhomogeneity is unavoidable in etching, because the etching conditions are not completely uniform everywhere.For this reason, a certain minimum exposure depth has to be sought, so as to obtain, in every case, a certain minimum exposure depth even at the unfavourable places. The time expended on etching, the safety precautions in the workplace and the ongoing operation costs, primarily costs for chemicals, waste water and disposal, add up to quite considerable amounts per cylinder liner. The present invention here takes another route: the primary crystals 8 and particles 9 and 10 embedded in the face are mechanically exposed by a grinding or polishing process using compliant, shaped polishing or grinding bodies 16. This avoids not only the disadvantages and costs of etching, but also gives, in particular, use advantages and functional advantages for the face 7 of the cylinder liner, further details on which will be given below.The costs incurred by the mechanical exposure per cylinder liner are not higher than the costs of a honing process.
In connection with the mechanical exposure, further details should be given on the honing machine shown in Fig.
4 which is also to be used in this polishing process. The honing machine 13 shown there has a movable machine table 18 on which the crankcase 2 is accommodated in a pan 19. Above the machine table 18 there is arranged at least one vertical honing spindle 14 into which is fitted a honing tool 15 which can be lowered into a cylinder bore of the crankcase.
The special thing about the honing machine is, on the one hand, that the honing tool 15 is fitted not with hard honing stones, but is fitted on its circumference with a plurality of axially orientated felt strips 16 which, owing to the felt being compliant, automatically give a cylindrical fit to the inner surface of the cylinder liner. These serve as shape-matched polishing or grinding bodies. The construction of the honing tool includes metal abrasive carriers which are fitted in the honing tool so as to be radially movable and which can be pressed with adjustable force against the inner surface of the cylinder liner. The metal abrasive carriers were planar, i.e. not cylindrical, on their side facing radially outwards.Matching cut pieces of a felt mat having a thickness of 9 mm were in each case glued onto these flat surfaces, with the felt pieces glued on not being formed on the outside in the manner of a cylindrical surface. Rather, the required cylindrical shape resulted automatically on commencing the honing-like polishing or grinding under the pressure of the felt pieces against the inner surface of the cylinder liner. The felt material is a felt designated as Stückfilz Tm 30 - 9, DIN 61206; a felt designated as Stuckfilz Tm 32 - 9, DIN 61206 would also certainly be suitable.The individual data in the designation have the following meanings: m - mixed, 30 - bulk density of 0.3 g/cm3 or 32 - bulk density of 0.32 g/cm3, 9 - 9 mm in thickness.
The hardness of the felt pieces used was M6 (medium 6) in accordance with DIN 61200; in the case of Stckfilz Tm 32 9, DIN 61206, a hardness according to DIN 61200 with the designation F1 (firm 1) could be recommended.
Since this mechanical exposure is also carried out in the presence of an abrasive, amorphous grinding or polishing medium having particles of hard material present therein, provisions are also made on the honing machine 13 for supplying the grinding medium. For this purpose, a reservoir 20 for holding a slurry 23 of fine particles of hard material, preferably silicon carbide particles in honing oil, is placed by the machine. To avoid sedimentation of the particles of hard material, the reservoir is provided with a stirrer 21. A circulation pump 22 conveys the slurry from the reservoir 20 to an annular sprinkling head 17 which goes around the honing tool above the cylinder liner and supplies plenty of grinding fluid to this.During the mechanical exposure, the rotating honing tool performs, in a known manner, an axially oscillating up and down movement so that all parts of the face 7 are reached by the felt strips 16. The honing tool is, in a known manner, configured in such a way that the felt strips can be pressed with an adjustable pressure against the face 7. The mechanical exposure is preferably carried out with application of a pressure of from about 3 to 5 bar, preferably about 4 bar.
By means of this method of machining, the material of the base alloy material located between the individual harder particles at the surface is removed to some extent, so that the harder particles project above the abraded base material 12 with a plateau area 11. The measure t represents the exposure depth. In this method of operation, the edges of the plateau areas 11 are rounded so that they gently go over into the base alloy material 12. This configuration of the plateau areas 11 is very advantageous for the piston or the piston rings sliding over them, because it is tribologically not very aggressive in comparison with the sharp-edged particles of hard material in the case of chemical exposure.
The measure of the exposure depth t can, apart from the pressing force of the felt strips, be determined primarily by the duration of the honing-like process during mechanical exposure. This is because with increasing time of the exposure process the plateau areas 11 are increasingly rounded and abraded into a dome-like shape. It has therefore been found to be advantageous to carry out the mechanical exposure process in the manner described for from about 20 to 60 seconds, preferably about 40 seconds. This gives an exposure depth of from about 0.2 to 0.3 pm. In any case, on this exposure depth there is superimposed a surface roughness which is at least of the same order of magnitude if not even greater, but this is not shown in Fig. 2a. The roughness of the surface is essentially determined by the grain size of the particles of hard material in the slurry 23; the roughness values (Rz) on machined cylinder faces are in the range from 0.7 to 1.0 pm. These roughness values and the low exposure depth enable very low oil consumptions and thus very low emissions of hydrocarbons to be achieved. In addition, the wear resistance and the sliding properties of the cylinder liners thus produced are excellent.

Claims (8)

Claims
1. A method of producing a cylinder liner comprising a supereutectic aluminium/silicon alloy, in which the face thereof is first roughly premachined and then fine machined by means of boring or turning and subsequently honed in at least one stage and in which the particles lying in the face which are harder than the base microstructure of the alloy, such as silicon crystals and/or intermetallic phases, are then exposed in such a way that plateau areas of the particles project above the remaining surface of the base microstructure of the alloy, comprising mechanically exposing primary crystals or particles embedded at the surface out of the face of the cylinder liner by means of a grinding or polishing process using at least one compliant shaped polishing or grinding body and an abrasive, amorphous grinding or polishing medium containing particles of hard material whose grain size is less than or at most the same as the desired roughness.
2. A method according to Claim 1, wherein the mechanical exposure of the primary crystals and particles is carried out in the manner of a honing process using felt strips having an outer cylindrical shape and a slurry of particles of hard material
3. A method according to claim 2, wherein the said hard particles in the slurry are SiC particles in honing oil.
4. A method according to Claim 2 or 3, wherein the mechanical exposure of the primary crystals and particles is carried out with the felt strips being pressed against the contact point at a pressure of from 3 to 5 bar.
5. A method according to Claim 4, wherein the mechanical exposure of the primary crystals and particles is carried out at a pressure of 4 bar.
6. A method according to Claim 2, wherein the honing-like process for the mechanical exposure of the primary crystals and particles is carried out for from about 20 to 60 seconds
7. A method according to Claim 2, wherein the honing-like process for the mechanical exposure of the primary crystals and particles is carried out for about 40 seconds.
8. A method of forming a cylinder liner according to claim 1 substantially as described herein with reference to and as illustrated in the accompanying drawings.
GB9604138A 1994-10-28 1995-10-03 Cylinder liner for a reciprocating piston engine and method of producing such a cylinder liner Expired - Fee Related GB2297053B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4438550A DE4438550C2 (en) 1994-10-28 1994-10-28 Process for producing a cylinder liner cast from a hypereutectic aluminum-silicon alloy into a crankcase of a reciprocating piston machine
GB9520107A GB2294471B (en) 1994-10-28 1995-10-03 Cylinder liner for a recprocating piston engine.

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GB9604138D0 GB9604138D0 (en) 1996-05-01
GB2297053A true GB2297053A (en) 1996-07-24
GB2297053B GB2297053B (en) 1996-11-06

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1174524A2 (en) * 2000-06-14 2002-01-23 Sulzer Metco AG Surface layer for forming a running layer on a cylinder wall, coating powder therefor and process for producing such a surface layer
US7128948B2 (en) * 2003-10-20 2006-10-31 The Boeing Company Sprayed preforms for forming structural members
CN109812349A (en) * 2012-05-03 2019-05-28 H.E.F.公司 Internal combustion engine bushing

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102018216615A1 (en) * 2018-09-17 2020-03-19 Aktiebolaget Skf Process for processing a surface of a metal object

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1174524A2 (en) * 2000-06-14 2002-01-23 Sulzer Metco AG Surface layer for forming a running layer on a cylinder wall, coating powder therefor and process for producing such a surface layer
US6578539B2 (en) 2000-06-14 2003-06-17 Sulzer Metco Ag Surface layer forming a cylinder barrel surface, a spraying powder suitable therefor and a method of creating such a surface layer
EP1174524A3 (en) * 2000-06-14 2009-03-11 Sulzer Metco AG Surface layer for forming a running layer on a cylinder wall, coating powder therefor and process for producing such a surface layer
US7128948B2 (en) * 2003-10-20 2006-10-31 The Boeing Company Sprayed preforms for forming structural members
CN109812349A (en) * 2012-05-03 2019-05-28 H.E.F.公司 Internal combustion engine bushing

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GB9604138D0 (en) 1996-05-01
GB2297053B (en) 1996-11-06

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