USRE27081E - 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
- Publication number
- USRE27081E USRE27081E US27081DE USRE27081E US RE27081 E USRE27081 E US RE27081E US 27081D E US27081D E US 27081DE US RE27081 E USRE27081 E US RE27081E
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- US
- United States
- Prior art keywords
- silicon
- aluminum
- cylinder
- alloy
- engine
- Prior art date
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- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 title abstract description 16
- 230000015572 biosynthetic process Effects 0.000 title description 4
- 229910000676 Si alloy Inorganic materials 0.000 title description 3
- 229910045601 alloy Inorganic materials 0.000 abstract description 38
- 239000000956 alloy Substances 0.000 abstract description 38
- 229910052710 silicon Inorganic materials 0.000 abstract description 35
- 239000010703 silicon Substances 0.000 abstract description 34
- 229910052782 aluminium Inorganic materials 0.000 abstract description 32
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 32
- 238000000034 method Methods 0.000 abstract description 22
- 238000005498 polishing Methods 0.000 abstract description 9
- 239000002344 surface layer Substances 0.000 abstract description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 31
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 9
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 9
- 239000000203 mixture Substances 0.000 description 9
- 239000003921 oil Substances 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 7
- 235000010446 mineral oil Nutrition 0.000 description 6
- 239000011856 silicon-based particle Substances 0.000 description 6
- 239000002253 acid Substances 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 5
- 230000007797 corrosion Effects 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
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-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
- 229910017604 nitric acid Inorganic materials 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 230000003750 conditioning effect Effects 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
- 229910001366 Hypereutectic aluminum Inorganic materials 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 238000007792 addition Methods 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
- 229940005574 sodium gluconate Drugs 0.000 description 2
- 235000012207 sodium gluconate Nutrition 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
- QKMNFFSBZRGHDJ-UHFFFAOYSA-N 1,4-dichloro-2-methoxybenzene Chemical compound COC1=CC(Cl)=CC=C1Cl QKMNFFSBZRGHDJ-UHFFFAOYSA-N 0.000 description 1
- 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
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 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
- 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
-
- 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
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J10/00—Engine or like cylinders; Features of hollow, e.g. cylindrical, bodies in general
- F16J10/02—Cylinders designed to receive moving pistons or plungers
- F16J10/04—Running faces; Liners
-
- 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
- Y10T29/49703—Sealing
Definitions
- ABSTRACT OF THE DISCLOSURE Method of treating the surface of a hypereutectic silicon aluminum base alloy article which comprises the steps of preferentially removing aluminum from and polishing surface layer of the article to provide plateaus of silicon which are substantially free of sharp edges where they protrude above the surrounding surface and the resultant high silicon aluminum base alloy article having plateaus of silicon above the surrounding surface thereo) which are substantially free of sharp edges.
- 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 sending and scoring and corrosion.
- 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 comprising the step of preferentially removing aluminum at the surface of the alloy to expose particles of silicon pro truding 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 16-18% 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 powdery phosphorous admixture identified as Alphosit identified as Alphosit
- 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 fiat 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 ccordance with the invention, by employing as a lapping ompound a suspension or dispersion of finely divided lemental silicon in a mineral oil, and honing the alloy urface therewith to produce initially a preferential atack on the aluminum alloy matrix, removing the aluninum, and forming a surface in which the silicon crystals re very little attacked and extend or protrude above the .lloy surface.
- the honing with the silicon-oil lap omposition is continued, the sharp edges of the proruding alloy silicon are levelled off, and "at the same time ome silicon from the lap composition is deposited. This -rduces, in effect, a conditioning of the alloy surface 0 provide a low-friction glaze finish of great resistance 0 scuffing and scoring, and to wear corrosion.
- the lap composition comprises a mixture of elemental ilicon and a mineral oil, forming a paste.
- the elemental ilicon is preferably of high purity, for example 98% Si. .”he silicon is in finely divided condition, the average partile size ranging from about 2 to about 200 microns, referably about 150 microns.
- the mineral oil phase is ureferably an automotive engine oil, such as, for examle, a l0-W grade engine oil, but any suitable lapping il, or an oil of the type conventionally used as an engine un-in oil may be employed.
- the silicon and the mineral Ill are admixed in a proportion ranging from about 40% ilicon and about 60% oil to about 85% silicon and about 5% oil, by weight. The preferred proportion is 70% ilicon to about 30% oil, by weight.
- the honing or lapping operation employing the novel apping composition of the invention may be performed with any conventional type of honing equipment, for xample, a machine employing a vitrified bonded fused tlumina honing stone, to which the lapping composition 5 applied.
- a machine employing a vitrified bonded fused tlumina honing stone to which the lapping composition 5 applied.
- the object to be honed s a cast aluminum alloy cylinder block
- the surfaces of he board or reamed or cast cylinders can be completely moothed and provided with a glaze surface by the use vf honing machines of the vertical type wherein the honng tool is rotated and reciprocated while the work is teld stationary, by suitable power actuating means.
- the toning stones or abrasive elements are expanded radialy outward to exert a substantial pressure on the cylinder urfaces, while at the same time they are rubbed over he surface with simultaneous rotational and reciproatory movements
- he preferential removal of the aluminum from the alloy tnd exposure of the silicon is carried out by a chemical reatment.
- the exposure of the silicon particles may be tccomplished, in accordance with the invention, by disolving away the surrounding aluminum with either an LCid or an alkaline treating bath.
- the acid treating bath i advantageously an aqueous nineral acid solution of the type employed in etching Lfld bright dipping of aluminum alloys.
- a solution rf phosphoric acid and nitric acid, or of nitric acid and lydrotfluoric acid is advantageous to use.
- a preferred type of treatment bath is me having the composition, by volume, from about 60% 0 about 90% phosphoric acid (85% grade), from about i% to about 16% of nitric acid (70% grade), remainder vater up to A small amount of a wetting agent may ae included in the bath.
- the surface is treated with this olution for a period of from 30 seconds to 3 minutes, tt a temperature of the bath between about 180 F. and LbOllt 220 F.
- -A preferred practice of the acid treatment nvolves the use of a bath composed of 80% by volume rf 85 grade phosphoric acid, 15% by volume of nitric tcid (70%), and 5% water, treatment time being of the rder of 45 seconds.
- an alkaline type treating bath such as a soluion of sodium hydroxide or sodium carbonate, which ucludes a small amount of sodium gluconate.
- an alkaline type treating bath such as a soluion of sodium hydroxide or sodium carbonate, which ucludes 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%) NaOI-I.
- Sodium gluconate is present in about 0.01 lb. per gallon.
- the treatment temperature range is from about F. to about 160 F., preferably about F., while the time of treatment i from 1 to 10 minutes, preferably about 2.5 minutes.
- the silicon particles and 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 scuffing 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% hours.
- the engine is disassembled for inspection and measurement, it is found that excessive scufiing 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 3.115", displacement 45.58 cu. in, compression ratio 7.25 to 1. Cylinders N0. 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 plug 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 scuffing 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 A" after rough honing with a No. 320 honing stone, were treated with an acid bath composed of 80% phosphoric acid (85% strength), 15% nitric acid (70% grade), and water, all by volume. The treatment affected the cylinder bores to a depth of between about 0.0005 and 0.001", and exposed silicon particles and crystals. The engine was assembled and subjected to a 12 minute breakin and 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.
- 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 aluminum 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 glaze-like 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 OAS-0.65% titanium about ODS-0.2%, 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.
- Method of conditioning the surface of a hypereutectic ilicon aluminum base alloy engine cylinder which comprises preferentially removing aluminum from and polishing the interior surface of said cylinder to provide plateaus of silicon which are substantially free of sharp edges where they protrude above the surrounding surface, thereby affording resistance to scuffing and scoring particularly during break-in or run-in operations at low temperature.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
METHOD OF TREATING THE SURFACE OF A HYPEREUTECTIC SILICON ALUMINUM BASE ALLOY ARTICLE WHICH COMPRISES THE STEPS OF PREFERENTIALLY REMOVING ALUMINUM FROM THE POLISHING SURFACE LAYER OF THE ARTICLE TO PROVIDE PLATEAUS OF SILICON WHICH ARE SUBSTANTIALLY FREE OF SHARP EDGES WHERE THEY PROTRUDE ABOVE THE SURROUNDING SURFACE AND THE RESSULTANT HIGH SILICON ALUMINUM BASE ALLOY ARTICLE HAVING PLATEAUS OF SILICON ABOVE THE SURROUNDING SURFACE THEREOF WHICH ARE SUBSTANTIALLY FREE OF SHARP EDGES.
Description
United States Patent 27,081 FORMATION OF LOW FRICTION GLASS-LIKE SURFACE ON ALUMINUM SILICON ALLOY FOR ENGINE OPERATION Gilbert R. Shockley, Richmond, Harold H. Macklin, Jr., Ban-Air, and Erik F. Barkman and Harold J. Coates, Henrico County, Va., assignors to Reynolds Metals Company, Richmond, Va.
No Drawing. Original No. 3,333,579, dated Aug. 1, 1967, Ser. No. 378,944, June 29, 1964. Application for reissue July 28, 1969, Ser. No. 860,443
Int. Cl. F02f 5/00; C23 l/OO U.S. Cl. 123-193 Claims Matter enclosed in heavy brackets appears in the original patent but forms no part of this reissue specification; matter printed in italics indicates the additions made by reissue.
ABSTRACT OF THE DISCLOSURE Method of treating the surface of a hypereutectic silicon aluminum base alloy article which comprises the steps of preferentially removing aluminum from and polishing surface layer of the article to provide plateaus of silicon which are substantially free of sharp edges where they protrude above the surrounding surface and the resultant high silicon aluminum base alloy article having plateaus of silicon above the surrounding surface thereo) which are substantially free of sharp edges.
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 sending 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 difficult to achieve good piston ring and cylinder surface compatibility under run-in conditions, with the result that scuffing 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 piston 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 Re-issuecl Mar. 2, 1971 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 scuffing 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 comprising the step of preferentially removing aluminum at the surface of the alloy to expose particles of silicon pro truding 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 16-18% 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 fiat 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 ccordance with the invention, by employing as a lapping ompound a suspension or dispersion of finely divided lemental silicon in a mineral oil, and honing the alloy urface therewith to produce initially a preferential atack on the aluminum alloy matrix, removing the aluninum, and forming a surface in which the silicon crystals re very little attacked and extend or protrude above the .lloy surface. As the honing with the silicon-oil lap omposition is continued, the sharp edges of the proruding alloy silicon are levelled off, and "at the same time ome silicon from the lap composition is deposited. This -rduces, in effect, a conditioning of the alloy surface 0 provide a low-friction glaze finish of great resistance 0 scuffing and scoring, and to wear corrosion.
The lap composition comprises a mixture of elemental ilicon and a mineral oil, forming a paste. The elemental ilicon is preferably of high purity, for example 98% Si. ."he silicon is in finely divided condition, the average partile size ranging from about 2 to about 200 microns, referably about 150 microns. The mineral oil phase is ureferably an automotive engine oil, such as, for examle, a l0-W grade engine oil, but any suitable lapping il, or an oil of the type conventionally used as an engine un-in oil may be employed. The silicon and the mineral Ill are admixed in a proportion ranging from about 40% ilicon and about 60% oil to about 85% silicon and about 5% oil, by weight. The preferred proportion is 70% ilicon to about 30% oil, by weight.
The honing or lapping operation employing the novel apping composition of the invention may be performed with any conventional type of honing equipment, for xample, a machine employing a vitrified bonded fused tlumina honing stone, to which the lapping composition 5 applied. Where, for example, the object to be honed s a cast aluminum alloy cylinder block, the surfaces of he board or reamed or cast cylinders can be completely moothed and provided with a glaze surface by the use vf honing machines of the vertical type wherein the honng tool is rotated and reciprocated while the work is teld stationary, by suitable power actuating means. The toning stones or abrasive elements are expanded radialy outward to exert a substantial pressure on the cylinder urfaces, while at the same time they are rubbed over he surface with simultaneous rotational and reciproatory movements.
. In accordance with the second aspect of the invention, he preferential removal of the aluminum from the alloy tnd exposure of the silicon is carried out by a chemical reatment. The exposure of the silicon particles may be tccomplished, in accordance with the invention, by disolving away the surrounding aluminum with either an LCid or an alkaline treating bath.
The acid treating bath i advantageously an aqueous nineral acid solution of the type employed in etching Lfld bright dipping of aluminum alloys. For the treatment If high silicon alloys, it is advantageous to use a solution rf phosphoric acid and nitric acid, or of nitric acid and lydrotfluoric acid. A preferred type of treatment bath is me having the composition, by volume, from about 60% 0 about 90% phosphoric acid (85% grade), from about i% to about 16% of nitric acid (70% grade), remainder vater up to A small amount of a wetting agent may ae included in the bath. The surface is treated with this olution for a period of from 30 seconds to 3 minutes, tt a temperature of the bath between about 180 F. and LbOllt 220 F. -A preferred practice of the acid treatment nvolves the use of a bath composed of 80% by volume rf 85 grade phosphoric acid, 15% by volume of nitric tcid (70%), and 5% water, treatment time being of the rder of 45 seconds.
Alternatively, there may be employed for aluminum emoval an alkaline type treating bath, such as a soluion of sodium hydroxide or sodium carbonate, which ucludes 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%) NaOI-I. Sodium gluconate is present in about 0.01 lb. per gallon. The treatment temperature range is from about F. to about 160 F., preferably about F., while the time of treatment i from 1 to 10 minutes, preferably about 2.5 minutes.
The silicon particles and 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 scuffing 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% hours. When the engine is disassembled for inspection and measurement, it is found that excessive scufiing 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 3.115", displacement 45.58 cu. in, compression ratio 7.25 to 1. Cylinders N0. 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 plug 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 scuffing 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 A" after rough honing with a No. 320 honing stone, were treated with an acid bath composed of 80% phosphoric acid (85% strength), 15% nitric acid (70% grade), and water, all by volume. The treatment affected the cylinder bores to a depth of between about 0.0005 and 0.001", and exposed silicon particles and crystals. The engine was assembled and subjected to a 12 minute breakin and 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 aluminum 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 glaze-like 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 OAS-0.65% titanium about ODS-0.2%, 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.
11. Method of conditioning the surface of a hypereutectic ilicon aluminum base alloy engine cylinder which comprises preferentially removing aluminum from and polishing the interior surface of said cylinder to provide plateaus of silicon which are substantially free of sharp edges where they protrude above the surrounding surface, thereby affording resistance to scuffing and scoring particularly during break-in or run-in operations at low temperature.
12. A high silicon aluminum base alloy engine cylinder having substantially flat plateaus of silicon above the surrounding piston ring engaging surface thereof produced by the method of claim 11.
References Cited The following references, cited by the Examiner, are of record in the patented file of this patent or the original JACOB H. STEINBERG, Primary Examiner U.'S. Cl. X.R.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US86044369A | 1969-07-28 | 1969-07-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| USRE27081E true USRE27081E (en) | 1971-03-02 |
Family
ID=25333235
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US27081D Expired USRE27081E (en) | 1969-07-28 | 1969-07-28 | Formation of low friction glass-like surface on aluminum silicon alloy for engine operation |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | USRE27081E (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5057274A (en) * | 1985-06-19 | 1991-10-15 | Taiho Kogyo Co., Ltd. | Die cast heat treated aluminum silicon based alloys and method for producing the same |
| US6050881A (en) | 1998-07-27 | 2000-04-18 | Ford Global Technologies, Inc. | Surface finishing covalent-ionic ceramics |
| US6511226B2 (en) | 2000-09-05 | 2003-01-28 | Federal-Mogul World Wide, Inc. | Aluminum thrust washer |
| US20090151689A1 (en) * | 2006-12-28 | 2009-06-18 | Yamaha Hatsudoki Kabushiki Kaisha | Internal combustion engine component and method for producing the same |
-
1969
- 1969-07-28 US US27081D patent/USRE27081E/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5057274A (en) * | 1985-06-19 | 1991-10-15 | Taiho Kogyo Co., Ltd. | Die cast heat treated aluminum silicon based alloys and method for producing the same |
| US6050881A (en) | 1998-07-27 | 2000-04-18 | Ford Global Technologies, Inc. | Surface finishing covalent-ionic ceramics |
| US6511226B2 (en) | 2000-09-05 | 2003-01-28 | Federal-Mogul World Wide, Inc. | Aluminum thrust washer |
| US20090151689A1 (en) * | 2006-12-28 | 2009-06-18 | Yamaha Hatsudoki Kabushiki Kaisha | Internal combustion engine component and method for producing the same |
| US8047174B2 (en) | 2006-12-28 | 2011-11-01 | Yamaha Hatsudoki Kabushiki Kaisha | Internal combustion engine component and method for producing the same |
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