US3333579A - Formation of low friction glass-like surface on aluminum silicon alloy for engine operation - Google Patents
Formation of low friction glass-like surface on aluminum silicon alloy for engine operation Download PDFInfo
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- US3333579A US3333579A US378944A US37894464A US3333579A US 3333579 A US3333579 A US 3333579A US 378944 A US378944 A US 378944A US 37894464 A US37894464 A US 37894464A US 3333579 A US3333579 A US 3333579A
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- silicon
- aluminum
- alloy
- cylinder
- engine
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- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 title claims description 11
- 230000015572 biosynthetic process Effects 0.000 title description 4
- 229910000676 Si alloy Inorganic materials 0.000 title description 3
- 229910052710 silicon Inorganic materials 0.000 claims description 37
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 36
- 239000010703 silicon Substances 0.000 claims description 36
- 229910045601 alloy Inorganic materials 0.000 claims description 35
- 239000000956 alloy Substances 0.000 claims description 35
- 229910052782 aluminium Inorganic materials 0.000 claims description 30
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 30
- 238000000034 method Methods 0.000 claims description 19
- 238000005498 polishing Methods 0.000 claims description 7
- 239000002245 particle Substances 0.000 claims description 6
- 239000002344 surface layer Substances 0.000 claims description 2
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 12
- 239000000203 mixture Substances 0.000 description 10
- 239000003921 oil Substances 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 9
- 229910000838 Al alloy Inorganic materials 0.000 description 8
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 8
- 239000002480 mineral oil Substances 0.000 description 8
- 235000010446 mineral oil Nutrition 0.000 description 7
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 5
- 239000002253 acid Substances 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 5
- 230000007797 corrosion Effects 0.000 description 5
- 229910017604 nitric acid Inorganic materials 0.000 description 5
- 239000011856 silicon-based particle Substances 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 229910001018 Cast iron Inorganic materials 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 4
- 229910000147 aluminium phosphate Inorganic materials 0.000 description 4
- 238000005266 casting Methods 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 239000013078 crystal Substances 0.000 description 4
- 238000005530 etching Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 239000011777 magnesium Substances 0.000 description 4
- 229910052749 magnesium Inorganic materials 0.000 description 4
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 238000007689 inspection Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000004575 stone Substances 0.000 description 3
- 239000000725 suspension Substances 0.000 description 3
- AEQDJSLRWYMAQI-UHFFFAOYSA-N 2,3,9,10-tetramethoxy-6,8,13,13a-tetrahydro-5H-isoquinolino[2,1-b]isoquinoline Chemical compound C1CN2CC(C(=C(OC)C=C3)OC)=C3CC2C2=C1C=C(OC)C(OC)=C2 AEQDJSLRWYMAQI-UHFFFAOYSA-N 0.000 description 2
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 2
- 229910001366 Hypereutectic aluminum Inorganic materials 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 230000003750 conditioning effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000010705 motor oil Substances 0.000 description 2
- CDBYLPFSWZWCQE-UHFFFAOYSA-L sodium carbonate Substances [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 description 2
- 239000000176 sodium gluconate Substances 0.000 description 2
- 235000012207 sodium gluconate Nutrition 0.000 description 2
- 229940005574 sodium gluconate Drugs 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 238000011179 visual inspection Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 238000010306 acid treatment Methods 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 235000010755 mineral Nutrition 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 230000002085 persistent effect Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000003507 refrigerant Substances 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000011734 sodium Substances 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 229910000029 sodium carbonate Inorganic materials 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000080 wetting agent Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F1/00—Etching metallic material by chemical means
- C23F1/10—Etching compositions
- C23F1/14—Aqueous compositions
- C23F1/16—Acidic compositions
- C23F1/20—Acidic compositions for etching aluminium or alloys thereof
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K3/00—Materials not provided for elsewhere
- C09K3/14—Anti-slip materials; Abrasives
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F1/00—Etching metallic material by chemical means
- C23F1/10—Etching compositions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/02—Surface coverings of combustion-gas-swept parts
-
- 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
- F02F1/04—Cylinders; Cylinder heads having cooling means for air cooling
- F02F1/06—Shape or arrangement of cooling fins; Finned cylinders
- F02F1/08—Shape or arrangement of cooling fins; Finned cylinders running-liner and cooling-part of cylinder being different parts or of different material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/121—Use of special materials
-
- 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
- F05C2203/00—Non-metallic inorganic materials
- F05C2203/04—Phosphor
-
- 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
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49709—Specific metallic composition
-
- 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
- Y10T29/49995—Shaping one-piece blank by removing material
- Y10T29/49996—Successive distinct removal operations
Definitions
- the aluminum casting alloys otherwise are well suited for the production of engine blocks, cylinder heads, and other motor parts. These alloys include alloying elements such as silicon either alone or in combination with, magnesium, or copper, or combinations of these elements. Silicon is essential for many reasons including that it improves a fluidity of the molten aluminum in the casting operation, decreases leaks in the finished casting, and contributes to strength and weldability.
- high silicon aluminum base alloys can be provided with a low friction surface by a novel process compris- See ing the steps of preferentially removing aluminum at the surface of the alloy to expose particles of silicon protruding above the surrounding aluminum alloy surface, thereby enriching the surface in silicon, and then mechanically polishing the protruding silicon surfaces to form a glaze-like surface or finish on the alloy.
- high silicon aluminum base alloys refers to hypereutectic aluminum base casting alloys containing up to about 20% silicon by weight, as Well as to such alloys which further contain from about 3% to about 11% copper, or from about 7% to about 9% magnesium.
- An alloy which has proved especially useful for engine block and piston manufacture and which is readily adapted to treatment in accordance with the invention is a hypereutectic aluminum base alloy containing about 1618% silicon, together with about 4.24.9% copper and small amounts of magnesium, iron and titanium.
- the alloy is advantageously subjected to a preparatory treatment in molten condition by the addition of about 0.01% sodium and about 0.75% of a' powdery phosphorous admixture identified as Alphosit, by weight, in conventional manner, so as to develop a silicon particle size in the cast condition of typically 10 to 40 microns (compared to about 50-100 microns in the absence of such treatment).
- a preparatory treatment in molten condition by the addition of about 0.01% sodium and about 0.75% of a' powdery phosphorous admixture identified as Alphosit, by weight, in conventional manner, so as to develop a silicon particle size in the cast condition of typically 10 to 40 microns (compared to about 50-100 microns in the absence of such treatment).
- novel treatment of the invention is believed to transform the sharp protruding edges of the silicon particles or crystals extending above the surface of the alloy into comparatively flat plateaus of silicon which provide a low friction finish of remarkable smoothness and hardness.
- This finish renders the aluminum alloy thus treated especially suitable for wear surfaces, such as those of cylinders and pistons and piston rings of engines, as well as bearing surfaces of all types.
- An enriched silicon surface of the kind provided by the method of the invention would not result from the application of conventional honing, lapping or etching method which attacks and removes the silicon particles in the alloy as Well as the aluminum, leaving no basis for the subsequent formation of a silicon glaze.
- the preferential removal of aluminum at the surface of the alloy to expose particles of silicon protruding above the surface, thereby enriching the surface in silicon may be performed either mechanically or chemically.
- the preferential removal of aluminum is carried out by first lapping the surface of the alloy to a rough finish, employing for this purpose any suitable rough lapping composition, such as, for example, a mixture of aluminum oxide or silicon carbide and a mineral oil.
- any suitable rough lapping composition such as, for example, a mixture of aluminum oxide or silicon carbide and a mineral oil.
- the removal of the aluminum is then accomplished, in accordance with the invention, by employing as a lapping compound a suspension or dispersion of finely divided elemental silicon in a mineral oil, and honing the alloy surface therewith to produce initially a preferential attack on the aluminum alloy matrix, removing the aluminum, and forming a surface in which the silicon crystals are very little attacked and extend or protrude above the alloy surface.
- the honing with the silicon-oil lap composition is continued, the sharp edges of the protruding alloy silicon are levelled off, and at the same time some silicon from the lap composition is deposited. This produces, in effect, a conditioning of the alloy surface to provide a low-friction glaze finish of great resistance to scuffing and scoring, and to wear corrosion.
- the lap composition comprises a mixture of elemental silicon and a mineral oil, forming a paste.
- the elemental silicon is preferably of high purity, for example 98% Si.
- the silicon is in finely divided condition, the average particle size ranging from about 2 to about 200 microns,
- the mineral oil phase is preferably an automotive engine oil, such as, for example, a 10-W grade engine oil, but any suitable lapping oil, or an oil of the type conventionally used as an engine run-in oil may be employed.
- the silicon and the mineral oil are admixed in a proportion ranging from about 40% silicon and about 60% oil to about 85% silicon and about 15% oil, by weight. The preferred proportion is 70% silicon to about 30% oil, by weight.
- the honing or lapping operation employing the novel lapping composition of the invention may be performed with any conventional type of honing equipment, for example, a machine employing a vitrified bonded fused alumina honing stone, to which the lapping composition is applied.
- a machine employing a vitrified bonded fused alumina honing stone to which the lapping composition is applied.
- the object to be honed is a cast aluminum alloy cylinder block
- the surfaces of the board or reamed or cast cylinders can be completely smoothed and provided with a glaze surface by the use of honing machines of the vertical type wherein the honing tool is rotated and reciprocated while the work is held stationary, by suitable power actuating means.
- the honing stones or abrasive elements are expanded radially outward to exert a substantial pressure on the cylinder surfaces, while at the same time they are rubbed over the surfaces with simultaneous rotational and reciprocatory movements.
- the preferential removal of the aluminum from the alloy and exposure of the silicon is carried out by a chemical treatment.
- the exposure of the silicon particles may be accomplished, in accordance with the invention, by dissolving away the surrounding aluminum with either an acid or an alkaline treating bath.
- the acid treating bath is advantageously an aqueous mineral acid solution of the type employed in etching and bright dipping of aluminum alloys.
- a solution of phosphoric acid and nitric acid, or of nitric acid and hydrofluoric acid is one having the. composition, by volume, from about 60% to about 90% phosphoric acid (85 grade), from about 5% to about 15% of nitric acid (70% grade), remainder water up to 15%.
- a small amount of a wetting agent may be included in the bath.
- the surface is treated with this solution for a period of from 30 seconds to 3 minutes, at a temperature of the bath between about 180 F. and about 220 F.
- a preferred practice of the acid treatment involves the use of a bath composed of 80% by volume of 85 grade phosphoric acid, 15 by volume of nitric acid (70%), and 5% water, treatment time being of the order of 45 seconds.
- an alkaline type treating bath such as a solution of sodium hydroxide or sodium carbonate, which includes a small amount of sodium gluconate.
- a solution of sodium hydroxide containing from about 3 to 9 ounces (2% to 6%) of solid sodium hydroxide per gallon of solution, the preferred concentration being about 6 ounces (5%) NaOH.
- Sodium gluconate is present in about 0.01 lb. per gallon.
- the treatment temperature range is from about 90 F. to about 160 F., preferably about 130 F., While the time of treatment is from 1 to 10 minutes, preferably about 2.5 minutes.
- the silicon particlesand crystals thus exposed by chemical treatment of the alloy, and protruding above the alloy surface, are conditioned by the treatment and when subjected to mechanical deformation, as by lapping or polishing, form a dense smooth glaze finish upon the alloy surface.
- This mechanical treatment may be accomplished by means of the lapping composition of silicon and mineral oil previously described. It may also be accomplished by the application of a metal surface under pressure, as in the case of a cylinder and piston, or of a bearing element.
- the glaze finish of the invention results in increased wear compatibility with piston'surfaces, as well as increased corrosion wear protection. Moreover, the lubrication is improved by reason of better wettability of the glaze coated cylinder and piston ring surfaces toward the lubricating oil. Another advantage of the invention is the ability to conduct the break-in or run-in procedure with greatly reduced operating time, and at low temperatures, with substantial absence of scufiing and scoring and corrosion effects.
- the beneficial effects of the glaze finish of the invention in high silicon aluminum base alloy engine cylinders and other components may be demonstrated by means of an accelerated cold scuff test.
- the glaze finished engine is run for 12 minutes at room temperature, and then the water jacket temperature is reduced by circulating refrigerant therethrough at a temperature of 30 F., and the engine is run under these conditions for an additional 2 /2 hours.
- the engine is disassembled for inspection and measurement, it is found that excessive scuffing and scoring are eliminated.
- Example 1 A Renault type I water-cooled automotive engine was fitted with aluminum base alloy cast cylinder sleeves, the alloy containing about 17% silicon, and standard pistons equipped with chromium-plated iron rings. The engine characteristics were: 4 cylinder, bore 2.146, stroke 3.15", displacement 45.58 cu. in., compression ratio 7.25 to 1. Cylinders No. 2 and 4 were similarly rough honed, and then lapped with a conventional cast iron lap together with the aforementioned silicon-oil lapping paste.
- the engine was assembled and run at ambient temperature for a break-in period of 12 minutes. Then the spark plugs were removed and the inside of the cylinder bore inspected with a horoscope, an instrument permitting illuminated visual inspection. A smooth surface appeared upon this inspection. Then refrigerated water at 30 F. was circulated through the engine cooling jacket and the engine was run for 2 /2 hours, at the end of which time it was disassembled for inspection. Visual inspection of the cylinder bores revealed no scufling or scoring; wear on the cylinder surfaces and ring surfaces appeared equal. Despite the short time of operation, a hard glaze was found on the surfaces of the cylinders.
- Example 2 Using the same type of engine as in Example 1, the cylinder sleeves having a wall thickness of approximately 4" after rough honing with a No. 320 honing stone, were treated with an acid bath composed of phosphoric acid strength), 15 nitric acid (70% grade), and 5% water, all by volume. The treatment affected the cylinder bores to a depth of between about 0.000 and 0.001", and exposed silicon particles and crystals. The engine was assembled and subjected to a 12 minute breakin and 2 /2 hour run-in test at 30 F., as in Example 1.
- Method of forming a low friction finish on the surface of a hypereutectic silicon aluminum base alloy article which comprises the steps of preferentially removing aluminum from a surface layer of said article to expose particles of silicon protruding above the surrounding alloy surface, and then mechanically polishing the protruding silicon surfaces to produce a glaze-like finish on the surface of said article.
- Method of conditioning the surface of a hypereutectic silicon alminum base alloy engine cylinder to form thereon a low friction finish which comprises the steps of preferentially removing aluminum from the interior of said cylinder to expose particles of silicon protruding above the interior surface, and then mechanically polishing the protruding silicon surfaces to produce a glazelike finish on the surface of said cylinder interior.
- the aluminum base alloy consists essentially of silicon about 16-18%, copper about 4.2-4.9%, iron up to about 1.0%, magnesium about 6 OAS-0.65%, titanium about 0.080.2%, manganese about 0.1% maX., balance substantially aluminum.
- a high silicon aluminum base alloy engine cylinder having on the piston ring engaging surface thereof a low friction finish produced by the method of claim 2.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Combustion & Propulsion (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- ing And Chemical Polishing (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Braking Arrangements (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Description
United States Patent 3,333,579 FORMATION OF LOW FRICTION GLASS-LIKE SURFACE ON ALUMINUM SILICON ALLOY FOR ENGINE OPERATION Gilbert R. Shockley, Richmond, Harold H. Macklin, Jr., Bon Air, and Erik F. Barkman and Harold J. Coates, Henrico County, Va., assignors to Reynolds Metals Company, Richmond, Va., a corporation of Delaware No Drawing. Filed June 29, 1964, Ser. No. 378,944 Claims. (Cl. 123-193) This invention relates to a novel method for the production of a low friction surface on the face of high silicon aluminum base alloys. More particularly, the invention concerns a novel method of treating the working surfaces of engine cylinders made of high silicon aluminum alloys to impart to said surfaces increased resistance to scufling and scoring and corrosion.
In the automotive industry, it is standard practice to prepare internal combustion engines for service by means of a break-in or run-in operation. The run-in is intended to establish proper cylinder and piston ring surface conditions whereby these parts attain compatibility in as short a time as possible under specific load and temperature conditions. The formation of an optimum surface finish, particularly on the cylinders, reduces the run-in time and increases the operating life of the engine parts. It is usually difi'icult to achieve good piston ring and cylinder surface compatibility under run-in conditions, with the result that sending and scoring of the compression ring and cylinder surfaces occurs, shortening engine life, promoting wear corrosion, and loss of compression. Methods to improve cylinder and ring surfaces which have been proposed in the prior art include cross-hatching of cylinder surfaces and filling the grooves with a lubricant such as graphite, or the successive lapping of cylinder walls with coarse and fine lapping compounds. These methods have had limited success in the case of engines employing cast iron cylinders and piston rings.
In the development of automotive engines employing cast aluminum cylinder blocks, or employing aluminum cylinder liners in cast iron cylinder blocks, and aluminum pistons and rings, the achievement of cylinder-ring compatibility has proved a much more serious obstacle than in the case of conventional iron engine parts, and prior to the present invention, had remained unsolved. Thus, even where engines utilized aluminum cylinder blocks, as well as an aluminum crankcase and an aluminum cylinder head, it was still necessary to resort to the use of cast iron cylinder sleeves in the block.
Efforts to operate engines with bare aluminum or aluminum alloy pistons or rings on bare aluminum walls resulted in unsatisfactory low temperature compatibility, partly because the aluminum surfaces are not characterized by persistent oil retention, as in the case with iron surfaces. The oil drains off the aluminum surface, resulting in scufling and scoring, when the parts are brought together in sliding motion through piston ring engagement.
The aluminum casting alloys otherwise are well suited for the production of engine blocks, cylinder heads, and other motor parts. These alloys include alloying elements such as silicon either alone or in combination with, magnesium, or copper, or combinations of these elements. Silicon is essential for many reasons including that it improves a fluidity of the molten aluminum in the casting operation, decreases leaks in the finished casting, and contributes to strength and weldability.
In accordance with the invention, it has been found that high silicon aluminum base alloys can be provided with a low friction surface by a novel process compris- See ing the steps of preferentially removing aluminum at the surface of the alloy to expose particles of silicon protruding above the surrounding aluminum alloy surface, thereby enriching the surface in silicon, and then mechanically polishing the protruding silicon surfaces to form a glaze-like surface or finish on the alloy.
The expression high silicon aluminum base alloys as employed herein refers to hypereutectic aluminum base casting alloys containing up to about 20% silicon by weight, as Well as to such alloys which further contain from about 3% to about 11% copper, or from about 7% to about 9% magnesium. An alloy which has proved especially useful for engine block and piston manufacture and which is readily adapted to treatment in accordance with the invention is a hypereutectic aluminum base alloy containing about 1618% silicon, together with about 4.24.9% copper and small amounts of magnesium, iron and titanium. The alloy is advantageously subjected to a preparatory treatment in molten condition by the addition of about 0.01% sodium and about 0.75% of a' powdery phosphorous admixture identified as Alphosit, by weight, in conventional manner, so as to develop a silicon particle size in the cast condition of typically 10 to 40 microns (compared to about 50-100 microns in the absence of such treatment).
The novel treatment of the invention is believed to transform the sharp protruding edges of the silicon particles or crystals extending above the surface of the alloy into comparatively flat plateaus of silicon which provide a low friction finish of remarkable smoothness and hardness. This finish renders the aluminum alloy thus treated especially suitable for wear surfaces, such as those of cylinders and pistons and piston rings of engines, as well as bearing surfaces of all types.
An enriched silicon surface of the kind provided by the method of the invention would not result from the application of conventional honing, lapping or etching method which attacks and removes the silicon particles in the alloy as Well as the aluminum, leaving no basis for the subsequent formation of a silicon glaze.
In accordance with the invention, the preferential removal of aluminum at the surface of the alloy to expose particles of silicon protruding above the surface, thereby enriching the surface in silicon, may be performed either mechanically or chemically.
According to a first aspect of the invention, the preferential removal of aluminum is carried out by first lapping the surface of the alloy to a rough finish, employing for this purpose any suitable rough lapping composition, such as, for example, a mixture of aluminum oxide or silicon carbide and a mineral oil.
The removal of the aluminum is then accomplished, in accordance with the invention, by employing as a lapping compound a suspension or dispersion of finely divided elemental silicon in a mineral oil, and honing the alloy surface therewith to produce initially a preferential attack on the aluminum alloy matrix, removing the aluminum, and forming a surface in which the silicon crystals are very little attacked and extend or protrude above the alloy surface. As the honing with the silicon-oil lap composition is continued, the sharp edges of the protruding alloy silicon are levelled off, and at the same time some silicon from the lap composition is deposited. This produces, in effect, a conditioning of the alloy surface to provide a low-friction glaze finish of great resistance to scuffing and scoring, and to wear corrosion.
The lap composition comprises a mixture of elemental silicon and a mineral oil, forming a paste. The elemental silicon is preferably of high purity, for example 98% Si.
, The silicon is in finely divided condition, the average particle size ranging from about 2 to about 200 microns,
preferably about 150 microns. The mineral oil phase is preferably an automotive engine oil, such as, for example, a 10-W grade engine oil, but any suitable lapping oil, or an oil of the type conventionally used as an engine run-in oil may be employed. The silicon and the mineral oil are admixed in a proportion ranging from about 40% silicon and about 60% oil to about 85% silicon and about 15% oil, by weight. The preferred proportion is 70% silicon to about 30% oil, by weight.
The honing or lapping operation employing the novel lapping composition of the invention may be performed with any conventional type of honing equipment, for example, a machine employing a vitrified bonded fused alumina honing stone, to which the lapping composition is applied. Where, for example, the object to be honed is a cast aluminum alloy cylinder block, the surfaces of the board or reamed or cast cylinders can be completely smoothed and provided with a glaze surface by the use of honing machines of the vertical type wherein the honing tool is rotated and reciprocated while the work is held stationary, by suitable power actuating means. The honing stones or abrasive elements are expanded radially outward to exert a substantial pressure on the cylinder surfaces, while at the same time they are rubbed over the surfaces with simultaneous rotational and reciprocatory movements.
In accordance with the second aspect of the invention, the preferential removal of the aluminum from the alloy and exposure of the silicon is carried out by a chemical treatment. The exposure of the silicon particles may be accomplished, in accordance with the invention, by dissolving away the surrounding aluminum with either an acid or an alkaline treating bath.
The acid treating bath is advantageously an aqueous mineral acid solution of the type employed in etching and bright dipping of aluminum alloys. For the treatment of high silicon alloys, it is advantageous to use a solution of phosphoric acid and nitric acid, or of nitric acid and hydrofluoric acid. A preferred type of treatment bath is one having the. composition, by volume, from about 60% to about 90% phosphoric acid (85 grade), from about 5% to about 15% of nitric acid (70% grade), remainder water up to 15%. A small amount of a wetting agent may be included in the bath. The surface is treated with this solution for a period of from 30 seconds to 3 minutes, at a temperature of the bath between about 180 F. and about 220 F. A preferred practice of the acid treatment involves the use of a bath composed of 80% by volume of 85 grade phosphoric acid, 15 by volume of nitric acid (70%), and 5% water, treatment time being of the order of 45 seconds.
Alternatively, there may be employed for aluminum removal an alkaline type treating bath, such as a solution of sodium hydroxide or sodium carbonate, which includes a small amount of sodium gluconate. There may be advantageously employed a solution of sodium hydroxide containing from about 3 to 9 ounces (2% to 6%) of solid sodium hydroxide per gallon of solution, the preferred concentration being about 6 ounces (5%) NaOH. Sodium gluconate is present in about 0.01 lb. per gallon. The treatment temperature range is from about 90 F. to about 160 F., preferably about 130 F., While the time of treatment is from 1 to 10 minutes, preferably about 2.5 minutes.
The silicon particlesand crystals thus exposed by chemical treatment of the alloy, and protruding above the alloy surface, are conditioned by the treatment and when subjected to mechanical deformation, as by lapping or polishing, form a dense smooth glaze finish upon the alloy surface. This mechanical treatment may be accomplished by means of the lapping composition of silicon and mineral oil previously described. It may also be accomplished by the application of a metal surface under pressure, as in the case of a cylinder and piston, or of a bearing element.
When applied to aluminum alloy engine cylinders, the glaze finish of the invention results in increased wear compatibility with piston'surfaces, as well as increased corrosion wear protection. Moreover, the lubrication is improved by reason of better wettability of the glaze coated cylinder and piston ring surfaces toward the lubricating oil. Another advantage of the invention is the ability to conduct the break-in or run-in procedure with greatly reduced operating time, and at low temperatures, with substantial absence of scufiing and scoring and corrosion effects.
The beneficial effects of the glaze finish of the invention in high silicon aluminum base alloy engine cylinders and other components may be demonstrated by means of an accelerated cold scuff test. In this test, the glaze finished engine is run for 12 minutes at room temperature, and then the water jacket temperature is reduced by circulating refrigerant therethrough at a temperature of 30 F., and the engine is run under these conditions for an additional 2 /2 hours. When the engine is disassembled for inspection and measurement, it is found that excessive scuffing and scoring are eliminated.
The practice of the invention is illustrated by the following examples, which are not, however, to be considered as limiting.
Example 1 A Renault type I water-cooled automotive engine Was fitted with aluminum base alloy cast cylinder sleeves, the alloy containing about 17% silicon, and standard pistons equipped with chromium-plated iron rings. The engine characteristics were: 4 cylinder, bore 2.146, stroke 3.15", displacement 45.58 cu. in., compression ratio 7.25 to 1. Cylinders No. 2 and 4 were similarly rough honed, and then lapped with a conventional cast iron lap together with the aforementioned silicon-oil lapping paste.
The engine was assembled and run at ambient temperature for a break-in period of 12 minutes. Then the spark plugs were removed and the inside of the cylinder bore inspected with a horoscope, an instrument permitting illuminated visual inspection. A smooth surface appeared upon this inspection. Then refrigerated water at 30 F. was circulated through the engine cooling jacket and the engine was run for 2 /2 hours, at the end of which time it was disassembled for inspection. Visual inspection of the cylinder bores revealed no scufling or scoring; wear on the cylinder surfaces and ring surfaces appeared equal. Despite the short time of operation, a hard glaze was found on the surfaces of the cylinders.
Example 2 Using the same type of engine as in Example 1, the cylinder sleeves having a wall thickness of approximately 4" after rough honing with a No. 320 honing stone, were treated with an acid bath composed of phosphoric acid strength), 15 nitric acid (70% grade), and 5% water, all by volume. The treatment affected the cylinder bores to a depth of between about 0.000 and 0.001", and exposed silicon particles and crystals. The engine was assembled and subjected to a 12 minute breakin and 2 /2 hour run-in test at 30 F., as in Example 1.
.Upon disassembling, the cylinder bores and ring surfaces were free from scufiing and scoring, and the cylinder bores were found to exhibit a smooth glaze-like finish.
While presently preferred embodiments of the invention and its practice have been described, it will be apparent that the invention may be otherwise variously embodied and practiced Within the scope of the following claims.
What is claimed is:
1. Method of forming a low friction finish on the surface of a hypereutectic silicon aluminum base alloy article, which comprises the steps of preferentially removing aluminum from a surface layer of said article to expose particles of silicon protruding above the surrounding alloy surface, and then mechanically polishing the protruding silicon surfaces to produce a glaze-like finish on the surface of said article.
2. Method of conditioning the surface of a hypereutectic silicon alminum base alloy engine cylinder to form thereon a low friction finish, which comprises the steps of preferentially removing aluminum from the interior of said cylinder to expose particles of silicon protruding above the interior surface, and then mechanically polishing the protruding silicon surfaces to produce a glazelike finish on the surface of said cylinder interior.
3. The method of claim 2 in which the aluminum is removed by lapping the cylinder interior with a suspension of finely divided silicon in a mineral oil.
4. The method of claim 2 in which the aluminum is removed by etching with an acid bath.
5. The method of claim 2 in which the aluminum is removed by etching with an alkaline bath.
6. The method of claim 2 in which the aluminum base alloy consists essentially of silicon about 16-18%, copper about 4.2-4.9%, iron up to about 1.0%, magnesium about 6 OAS-0.65%, titanium about 0.080.2%, manganese about 0.1% maX., balance substantially aluminum.
7. The method of claim 3 in which the mechanical polishing step is performed by further lapping with a silicon-mineral oil suspension.
8. The method of claim 3 in which the mechanical polishing step is performed by the reciprocating action of a piston ring in engine operation.
9. A high silicon aluminum base alloy article having on a surface thereof a low friction finish produced by the method of claim 1.
10. A high silicon aluminum base alloy engine cylinder having on the piston ring engaging surface thereof a low friction finish produced by the method of claim 2.
References Cited UNITED STATES PATENTS 3;l61,181 12/1964 Wiese 123--1 JACOB H. STEINBERG, Primary Examiner.
Claims (1)
1. METHOD OF FORMING A LOW FRICTION FINISH ON THE SURFACE OF A HYPEREUTECTIC SILICON ALUMINUM BASE ALLOY ARTICLE, WHICH COMPRISES THE STEPS OF PREFERENTIALLY REMOVING ALUMINUM FROM A SURFACE LAYER OF SAID ARTICLE TO EXPOSE PARTICLES OF SILICON PROTRUDING ABOVE THE SURROUNDING ALLOY SURFACE, AND THEN MECHANICALLY POLISHING THE PROTRUDING SILICON SURFACES TO PRODUCE A GLAZE-LIKE FINISH ON THE SURFACE OF SAID ARTICLE.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US378944A US3333579A (en) | 1964-06-29 | 1964-06-29 | Formation of low friction glass-like surface on aluminum silicon alloy for engine operation |
| GB21930/65A GB1109084A (en) | 1964-06-29 | 1965-05-24 | Treatment of aluminium alloy surfaces |
| DE1521939A DE1521939C2 (en) | 1964-06-29 | 1965-06-25 | Process for the production of finely finished surfaces, low friction of bodies made of aluminum-based alloys with high silicon content |
| SE8508/65A SE309896B (en) | 1964-06-29 | 1965-06-28 | |
| ES0314740A ES314740A1 (en) | 1964-06-29 | 1965-06-28 | A method for forming a low friction finish. (Machine-translation by Google Translate, not legally binding) |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US378944A US3333579A (en) | 1964-06-29 | 1964-06-29 | Formation of low friction glass-like surface on aluminum silicon alloy for engine operation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3333579A true US3333579A (en) | 1967-08-01 |
Family
ID=23495175
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US378944A Expired - Lifetime US3333579A (en) | 1964-06-29 | 1964-06-29 | Formation of low friction glass-like surface on aluminum silicon alloy for engine operation |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3333579A (en) |
| DE (1) | DE1521939C2 (en) |
| ES (1) | ES314740A1 (en) |
| GB (1) | GB1109084A (en) |
| SE (1) | SE309896B (en) |
Cited By (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3505037A (en) * | 1967-04-24 | 1970-04-07 | English Electric Co Ltd | Hypereutectic silicon alloys |
| US3789647A (en) * | 1972-10-20 | 1974-02-05 | United States Steel Corp | Method of surface-conditioning heat-treating-furnace hearth rolls having sleeves of rebonded fused silica thereon by processing silicon steel strip |
| DE2252607A1 (en) * | 1972-10-26 | 1974-05-09 | Yanmar Diesel Engine Co | CYLINDERS FOR COMBUSTION MACHINES |
| US3896009A (en) * | 1974-05-21 | 1975-07-22 | Kioritz Corp | Aluminum alloy cylinder |
| US3907514A (en) * | 1972-10-19 | 1975-09-23 | Pure Carbon Company Inc | Aluminum carbon composite seal material |
| JPS50137811A (en) * | 1974-06-08 | 1975-11-01 | ||
| JPS5116243A (en) * | 1974-07-31 | 1976-02-09 | Toyota Motor Co Ltd | ARUMINIUMUGOKINSEISHUDOBUZAINO SUKATSUFUINGUBOSHIHOHO |
| US3962003A (en) * | 1973-11-08 | 1976-06-08 | Xerox Corporation | Method of forming magnetic brush support member |
| US4074956A (en) * | 1975-11-29 | 1978-02-21 | Riken Piston Ring Kogyo Kabushiki Kaisha | Sulphur and nitrogen treated iron based rotor for rotary piston engine |
| US4106977A (en) * | 1975-05-09 | 1978-08-15 | Audi Nsu Auto Union Aktiengesellschaft | Process for production of oil control rings |
| US4212602A (en) * | 1974-08-14 | 1980-07-15 | Goetzewerke Friedrich Goetze Ag | Wear-resistant coating for sealing strips in rotary engines |
| US4651395A (en) * | 1980-02-11 | 1987-03-24 | Laystall Engraving Co. Ltd. | Manufacture of piston rings |
| US4669019A (en) * | 1980-08-30 | 1987-05-26 | Sony Corporation | Magnetic head drum assembly |
| US5303682A (en) * | 1991-10-17 | 1994-04-19 | Brunswick Corporation | Cylinder bore liner and method of making the same |
| US5355930A (en) * | 1992-09-04 | 1994-10-18 | Brunswick Corporation | Method of expendable pattern casting of hypereutectic aluminum-silicon alloys using sand with specific thermal properties |
| US5355931A (en) * | 1992-09-04 | 1994-10-18 | Brunswick Corporation | Method of expendable pattern casting using sand with specific thermal properties |
| US5383429A (en) * | 1994-02-23 | 1995-01-24 | Brunswick Corporation | Hypereutectic aluminum-silicon alloy connecting rod for a two-cycle internal combustion engine |
| FR2736067A1 (en) * | 1995-06-28 | 1997-01-03 | Daimler Benz Ag | ALUMINUM ALLOY / HYPEREUTECTIC SILICON CYLINDER SHAFT TO BE INCORPORATED IN CASTING IN AN ALTERNATIVE PISTON MACHINE BASE AND METHOD OF MANUFACTURING SUCH A SHIRT |
| DE19607979A1 (en) * | 1996-03-01 | 1997-09-04 | Asea Brown Boveri | Waste gas path of combustion apparatus for burning heavy oil |
| US6511226B2 (en) | 2000-09-05 | 2003-01-28 | Federal-Mogul World Wide, Inc. | Aluminum thrust washer |
| WO2005083253A1 (en) * | 2004-02-27 | 2005-09-09 | Yamaha Hatsudoki Kabushiki Kaisha | Engine component part and method for producing the same |
| US20060182990A1 (en) * | 2005-02-17 | 2006-08-17 | Central Motor Wheel Co., Ltd. | Aluminum composite material and method of producing the same |
| US20080184879A1 (en) * | 2007-01-09 | 2008-08-07 | Lobiondo Nicholas | Piston having improved wear resistance and method of making |
| WO2009043549A1 (en) * | 2007-09-26 | 2009-04-09 | Ks Aluminium Technologie Gmbh | Aluminum-silicon casting alloy for monolithic cylinder crankcases |
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| US4075934A (en) * | 1975-12-29 | 1978-02-28 | Karl Schmidt Gmbh | Piston for internal combustion engines |
| DE3822169A1 (en) † | 1988-06-30 | 1990-01-04 | Kadia Diamant | METHOD FOR EXPOSING SILICON CRYSTALS |
| JP2740112B2 (en) * | 1993-06-21 | 1998-04-15 | 株式会社豊田自動織機製作所 | Swash plate compressor |
| DE9422167U1 (en) * | 1994-10-28 | 1999-05-12 | DaimlerChrysler AG, 70567 Stuttgart | Cylinder liner made of a hypereutectic aluminum / silicon alloy cast into a crankcase of a reciprocating piston engine |
| US6096143A (en) * | 1994-10-28 | 2000-08-01 | Daimlerchrysler Ag | Cylinder liner of a hypereutectic aluminum/silicon alloy for use in a crankcase of a reciprocating piston engine and process for producing such a cylinder liner |
| US5916390A (en) * | 1995-10-30 | 1999-06-29 | Mercedes-Benz Ag | Cylinder liner comprising a supereutectic aluminum/silicon alloy for sealing into a crankcase of a reciprocating piston engine and method of producing such a cylinder liner |
| DE10006269A1 (en) * | 2000-02-12 | 2001-08-16 | Bayerische Motoren Werke Ag | Method for producing a metal component for a drive unit, in particular an internal combustion engine, which interacts with a friction partner via a sliding surface |
| JP3719971B2 (en) | 2001-11-06 | 2005-11-24 | 株式会社椿本チエイン | Silent chain with wear-resistant coating |
| DE102006059045A1 (en) * | 2006-12-14 | 2008-06-19 | Mahle International Gmbh | Treatment of running surface of IC engine cylinder made from alloy containing magnesium silicide comprises selectively dissolving out magnesium silicide using acid, so that pores are formed in surface |
| EP2058478B1 (en) * | 2007-11-09 | 2014-08-20 | hofer mechatronik GmbH | Adjustment device for modification of the relative position of a camshaft |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3161181A (en) * | 1962-05-25 | 1964-12-15 | British Petroleum Co | Process for running-in internal combustion engines |
-
1964
- 1964-06-29 US US378944A patent/US3333579A/en not_active Expired - Lifetime
-
1965
- 1965-05-24 GB GB21930/65A patent/GB1109084A/en not_active Expired
- 1965-06-25 DE DE1521939A patent/DE1521939C2/en not_active Expired
- 1965-06-28 ES ES0314740A patent/ES314740A1/en not_active Expired
- 1965-06-28 SE SE8508/65A patent/SE309896B/xx unknown
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3161181A (en) * | 1962-05-25 | 1964-12-15 | British Petroleum Co | Process for running-in internal combustion engines |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3505037A (en) * | 1967-04-24 | 1970-04-07 | English Electric Co Ltd | Hypereutectic silicon alloys |
| US3907514A (en) * | 1972-10-19 | 1975-09-23 | Pure Carbon Company Inc | Aluminum carbon composite seal material |
| US3789647A (en) * | 1972-10-20 | 1974-02-05 | United States Steel Corp | Method of surface-conditioning heat-treating-furnace hearth rolls having sleeves of rebonded fused silica thereon by processing silicon steel strip |
| DE2252607A1 (en) * | 1972-10-26 | 1974-05-09 | Yanmar Diesel Engine Co | CYLINDERS FOR COMBUSTION MACHINES |
| US3962003A (en) * | 1973-11-08 | 1976-06-08 | Xerox Corporation | Method of forming magnetic brush support member |
| US3896009A (en) * | 1974-05-21 | 1975-07-22 | Kioritz Corp | Aluminum alloy cylinder |
| JPS50137811A (en) * | 1974-06-08 | 1975-11-01 | ||
| JPS5116243A (en) * | 1974-07-31 | 1976-02-09 | Toyota Motor Co Ltd | ARUMINIUMUGOKINSEISHUDOBUZAINO SUKATSUFUINGUBOSHIHOHO |
| US4212602A (en) * | 1974-08-14 | 1980-07-15 | Goetzewerke Friedrich Goetze Ag | Wear-resistant coating for sealing strips in rotary engines |
| US4106977A (en) * | 1975-05-09 | 1978-08-15 | Audi Nsu Auto Union Aktiengesellschaft | Process for production of oil control rings |
| US4074956A (en) * | 1975-11-29 | 1978-02-21 | Riken Piston Ring Kogyo Kabushiki Kaisha | Sulphur and nitrogen treated iron based rotor for rotary piston engine |
| US4651395A (en) * | 1980-02-11 | 1987-03-24 | Laystall Engraving Co. Ltd. | Manufacture of piston rings |
| US4669019A (en) * | 1980-08-30 | 1987-05-26 | Sony Corporation | Magnetic head drum assembly |
| US5303682A (en) * | 1991-10-17 | 1994-04-19 | Brunswick Corporation | Cylinder bore liner and method of making the same |
| US5355930A (en) * | 1992-09-04 | 1994-10-18 | Brunswick Corporation | Method of expendable pattern casting of hypereutectic aluminum-silicon alloys using sand with specific thermal properties |
| US5355931A (en) * | 1992-09-04 | 1994-10-18 | Brunswick Corporation | Method of expendable pattern casting using sand with specific thermal properties |
| US5383429A (en) * | 1994-02-23 | 1995-01-24 | Brunswick Corporation | Hypereutectic aluminum-silicon alloy connecting rod for a two-cycle internal combustion engine |
| FR2736067A1 (en) * | 1995-06-28 | 1997-01-03 | Daimler Benz Ag | ALUMINUM ALLOY / HYPEREUTECTIC SILICON CYLINDER SHAFT TO BE INCORPORATED IN CASTING IN AN ALTERNATIVE PISTON MACHINE BASE AND METHOD OF MANUFACTURING SUCH A SHIRT |
| DE19607979A1 (en) * | 1996-03-01 | 1997-09-04 | Asea Brown Boveri | Waste gas path of combustion apparatus for burning heavy oil |
| US6511226B2 (en) | 2000-09-05 | 2003-01-28 | Federal-Mogul World Wide, Inc. | Aluminum thrust washer |
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| WO2005083253A1 (en) * | 2004-02-27 | 2005-09-09 | Yamaha Hatsudoki Kabushiki Kaisha | Engine component part and method for producing the same |
| EP2241741A1 (en) * | 2004-02-27 | 2010-10-20 | Yamaha Hatsudoki Kabushiki Kaisha | Engine component part and method for producing the same |
| US20070012173A1 (en) * | 2004-02-27 | 2007-01-18 | Hirotaka Kurita | Engine component part and method for producing the same |
| US20060182990A1 (en) * | 2005-02-17 | 2006-08-17 | Central Motor Wheel Co., Ltd. | Aluminum composite material and method of producing the same |
| US7097780B1 (en) * | 2005-02-17 | 2006-08-29 | Central Motor Wheel Co., Ltd. | Aluminum composite material and method of producing the same |
| US20080184879A1 (en) * | 2007-01-09 | 2008-08-07 | Lobiondo Nicholas | Piston having improved wear resistance and method of making |
| WO2009043549A1 (en) * | 2007-09-26 | 2009-04-09 | Ks Aluminium Technologie Gmbh | Aluminum-silicon casting alloy for monolithic cylinder crankcases |
| US20120227699A1 (en) * | 2011-03-08 | 2012-09-13 | GM Global Technology Operations LLC | Linerless engine |
| CN102678369A (en) * | 2011-03-08 | 2012-09-19 | 通用汽车环球科技运作有限责任公司 | Linerless engine |
Also Published As
| Publication number | Publication date |
|---|---|
| DE1521939B1 (en) | 1970-10-22 |
| SE309896B (en) | 1969-04-08 |
| ES314740A1 (en) | 1965-10-01 |
| GB1109084A (en) | 1968-04-10 |
| DE1521939C2 (en) | 1973-10-04 |
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