US3514286A - Wear-resisting aluminum alloys - Google Patents
Wear-resisting aluminum alloys Download PDFInfo
- Publication number
- US3514286A US3514286A US835416A US3514286DA US3514286A US 3514286 A US3514286 A US 3514286A US 835416 A US835416 A US 835416A US 3514286D A US3514286D A US 3514286DA US 3514286 A US3514286 A US 3514286A
- Authority
- US
- United States
- Prior art keywords
- aluminum
- wear
- tin
- lead
- alloys
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
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
Definitions
- This invention pertains to improvements in hyper-eutectic aluminum-silicon alloys containing optionally copper, magnesium, nickel and other ordinary contents, to which are added lead and tin, which alloys are adapted primarily for use in cylinders and cylinder liners of internal combustion engines assembled with aluminum pistons.
- pistons, cylinders and cylinder liners have been made of cast iron, and in part pistons made of aluminum alloys have been used.
- u-Phase aluminum is precipitated (primary or eutectic) in aluminum alloys particularly aluminum-silicon alloys.
- This a-phase aluminum is low in wear-resistance, especially when two materials containing u-phase aluminum are mated, an abnormal wear of galling or scuffing will occur. That is why aluminum cylinders and cylinder liners are not used together with aluminum pistons.
- the alloys of the present invention contain 3 to 10% lead and 3 to 20% tin, added to 12% to 25% silicon hyper-eutectic aluminum-silicon alloys comprising optionally small quantities of copper, magnesium, nickel and other ordinary contents. And these alloys are dotted with well lubricated lead particles and hard primary silicon, or formed with aluminum-eutectic matrix abundant in tin, or mixed with a combination of these lead and tin particles or materials providing thereby a high wear-resistance not only to conventional cast iron or chrome plated materials, but also even to aluminum-alloys.
- FIG. 1 is a microscopic section of a hyper-eutectic aluminum-silicon alloy containing lead and tin;
- FIG. 2 represents the results of the metal-to-metal sliding wear test using an ordinary aluminum-alloy, a cast 3,514,286 Patented May 26, 1970 iron and an aluminum alloy of the present invention as one specimen and chrome-plated materials as the other mating specimens;
- FIG. 3 shows the results of the metal-t0-metal sliding wear test using an ordinary aluminum alloy and an aluminum alloy of the present invention as one specimen and an ordinary aluminum as the other mating specimens.
- FIG. 1 shows the micro structure of aluminum-alloy containing 25% silicon, 2% copper, 1% magnesium, 3% tin, 10% lead and the balance substantially all aluminum.
- aluminum-tin-eutectic matrix 4 big eutectic silicon as crystal 2, tiny fine eutectic silicon 5, and minute particles of lead or lead and tin-eutectic 3a come out as a number of black dots.
- FIGS. 2 and 3 respresent the results of comparative wear tests using aluminum-alloys of the present invention or cast iron as one specimen and chrome-plated material as its other mating specimen and aluminum castings containing 12% silicon, 1% magnesium, 1.2% nickel and the balance all aluminum as its other mating specimen, respectively.
- a conventional aluminum-alloy is most remarkably poor in wear-resistance to chrome plated metal and aluminum-alloy containing neither lead nor tin, particularly in the case of the latter, scufling or galling occurs at the point of about 0.2 m./sec. of wear-friction.
- the curves I and II which contain lead or tin alone show high resistance to wear
- the curve III containing both lead and tin show the highest resistance to wear in use in association with chrome-plated metal.
- Conventional aluminum-alloy has very poor wear-resistance, and the new alloys show better results of wear-resistance than the conventional cast iron (curve IV) which has fairly high wear-resistance.
- the new alloys require both lead and tin therein in the ranges stated.
- Small amounts of copper, magnesium and/or nickel may be present in the alloy up to a total of about 7% so that one or more of these materials may be present within such range and excellent wear-resistance is still obtained.
- the remainder is all aluminum subject to the presence of normal incidentaliimpurities therein in very small quantities.
- the lubricating qualities of the alloys and wear resistance are believed to come from the characteristic of the tin and lead particles and the silicon crystals in the aluminum-eutectic matrix 4 which is abundant in tin.
- a wear-resisting aluminum alloy which consists of 10 from 12 to 25% silicon, from 3 to 10% lead, from 3 to 20% tin; and the balance essentially aluminum.
- a modificationof an alloy as claimed in claim 1 4 which contains small quantities of at least one element of the group consisting of magnesium, copper and nickel, and the total amount of additional elements does not exceed 7%.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
May 26, 1970 YATARO UNAI EI'AL 3,514,236
WEAR-RESISTING ALUMINUM ALLOYS Filed June 25, 1969 I HM 0.05- E 4 FIG. 2
0 I l 0.5 I v.0
m/sec FIG. 3
I I M United States Patent Int. Cl. C22c 21/02 us. or. 75-148 2 Claims ABSTRACT OF THE DISCLOSURE A wear-resisting aluminum alloy containing silicon from about 12% to about 25%, lead from about 3% to about tin from about 3% to about 20% and the balance consisting essentially of aluminum.
This is a continuationdnpart of my prior application Ser. No. 495,109, filed Oct. 12, 1965 now abandoned.
This invention pertains to improvements in hyper-eutectic aluminum-silicon alloys containing optionally copper, magnesium, nickel and other ordinary contents, to which are added lead and tin, which alloys are adapted primarily for use in cylinders and cylinder liners of internal combustion engines assembled with aluminum pistons.
In conventional internal combustion engines, pistons, cylinders and cylinder liners have been made of cast iron, and in part pistons made of aluminum alloys have been used.
Recently hyper-eutectic aluminum alloys containing over 12% silicon are also adapted for improving wearresistance. Today, the developments and studies on substitution by aluminum alloys not only for pistons, but for cylinders and cylinder liners are being carried out in order to make less in weight the engine as a whole.
u-Phase aluminum is precipitated (primary or eutectic) in aluminum alloys particularly aluminum-silicon alloys. This a-phase aluminum is low in wear-resistance, especially when two materials containing u-phase aluminum are mated, an abnormal wear of galling or scuffing will occur. That is why aluminum cylinders and cylinder liners are not used together with aluminum pistons.
The alloys of the present invention contain 3 to 10% lead and 3 to 20% tin, added to 12% to 25% silicon hyper-eutectic aluminum-silicon alloys comprising optionally small quantities of copper, magnesium, nickel and other ordinary contents. And these alloys are dotted with well lubricated lead particles and hard primary silicon, or formed with aluminum-eutectic matrix abundant in tin, or mixed with a combination of these lead and tin particles or materials providing thereby a high wear-resistance not only to conventional cast iron or chrome plated materials, but also even to aluminum-alloys.
The invention will become apparent from the following detailed description with reference to the accompanying drawings, wherein:
FIG. 1 is a microscopic section of a hyper-eutectic aluminum-silicon alloy containing lead and tin;
FIG. 2 represents the results of the metal-to-metal sliding wear test using an ordinary aluminum-alloy, a cast 3,514,286 Patented May 26, 1970 iron and an aluminum alloy of the present invention as one specimen and chrome-plated materials as the other mating specimens; and
FIG. 3 shows the results of the metal-t0-metal sliding wear test using an ordinary aluminum alloy and an aluminum alloy of the present invention as one specimen and an ordinary aluminum as the other mating specimens.
FIG. 1 shows the micro structure of aluminum-alloy containing 25% silicon, 2% copper, 1% magnesium, 3% tin, 10% lead and the balance substantially all aluminum. In aluminum-tin-eutectic matrix 4 big eutectic silicon as crystal 2, tiny fine eutectic silicon 5, and minute particles of lead or lead and tin-eutectic 3a come out as a number of black dots.
FIGS. 2 and 3 respresent the results of comparative wear tests using aluminum-alloys of the present invention or cast iron as one specimen and chrome-plated material as its other mating specimen and aluminum castings containing 12% silicon, 1% magnesium, 1.2% nickel and the balance all aluminum as its other mating specimen, respectively. The results of wear tests using specimens as follows: the aluminum-alloy containing 20% silicon, 2% copper, 1% magnesium, 5% lead and the balance substantially all aluminum; the aluminum-alloy containing 20% silicon, 2% copper, 1% magnesium, 20% tin, and the balance substantially all aluminum; the aluminumalloy containing 25 silicon, 2% copper, 1% magnesium, 3% tin, 10% lead and the balance substantially all aluminum; cast iron; and one of conventional aluminumalloysthat is-aluminum-alloy containing 7% silicon, 0.2% copper, 3% magnesium, and the balance substantially all aluminum as each one specimen, are shown in the respective curves I, II, III, IV, and V, drawn as coordinates of the longitudinal lines showing quantity of wear (mm?) and the lateral lines showing friction velocity (m./s.). As shown in curve V, a conventional aluminum-alloy is most remarkably poor in wear-resistance to chrome plated metal and aluminum-alloy containing neither lead nor tin, particularly in the case of the latter, scufling or galling occurs at the point of about 0.2 m./sec. of wear-friction. Although the curves I and II which contain lead or tin alone show high resistance to wear, the curve III containing both lead and tin show the highest resistance to wear in use in association with chrome-plated metal. Conventional aluminum-alloy has very poor wear-resistance, and the new alloys show better results of wear-resistance than the conventional cast iron (curve IV) which has fairly high wear-resistance.
The aforesaid improvement in Wear-resistance of the alloy results from the good lubrication of the lead and tin materials in the alloys. Consequently, the aforesaid high resistance is not achieved by minor additions of lead or tin. And best results cannot be secured by the major additions, which will lead only to the increase of weight of its products. For preferred contents of lead and tin, the former ranges from 3 to 10% and the latter from 3 to 20%.
Hence, the new alloys require both lead and tin therein in the ranges stated. Small amounts of copper, magnesium and/or nickel may be present in the alloy up to a total of about 7% so that one or more of these materials may be present within such range and excellent wear-resistance is still obtained. In all alloys, the remainder is all aluminum subject to the presence of normal incidentaliimpurities therein in very small quantities.
The lubricating qualities of the alloys and wear resistance are believed to come from the characteristic of the tin and lead particles and the silicon crystals in the aluminum-eutectic matrix 4 which is abundant in tin.
Thus, it is believed that the objects of the invention have been achieved.
What is claimed is:
1. A wear-resisting aluminum alloy which consists of 10 from 12 to 25% silicon, from 3 to 10% lead, from 3 to 20% tin; and the balance essentially aluminum. 2. A modificationof an alloy as claimed in claim 1 4 which contains small quantities of at least one element of the group consisting of magnesium, copper and nickel, and the total amount of additional elements does not exceed 7%.
References Cited UNITED STATES PATENTS 2,026,542 11/1936 Kempfetal 75148 2,075,089 3/1937 Bonsack etal 75-143 RICHARD o. DEAN, Primary Examiner US. 01. X.R.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US83541669A | 1969-06-23 | 1969-06-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3514286A true US3514286A (en) | 1970-05-26 |
Family
ID=25269457
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US835416A Expired - Lifetime US3514286A (en) | 1969-06-23 | 1969-06-23 | Wear-resisting aluminum alloys |
Country Status (1)
Country | Link |
---|---|
US (1) | US3514286A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4847608A (en) * | 1971-10-19 | 1973-07-06 | ||
US3868250A (en) * | 1971-06-14 | 1975-02-25 | Honsel Werke Ag | Heat resistant alloys |
JPS5056304A (en) * | 1973-09-20 | 1975-05-17 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2026542A (en) * | 1933-09-18 | 1936-01-07 | Aluminum Co Of America | Free cutting alloys |
US2075089A (en) * | 1936-08-17 | 1937-03-30 | Nat Smelting Co | Aluminum alloy |
-
1969
- 1969-06-23 US US835416A patent/US3514286A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2026542A (en) * | 1933-09-18 | 1936-01-07 | Aluminum Co Of America | Free cutting alloys |
US2075089A (en) * | 1936-08-17 | 1937-03-30 | Nat Smelting Co | Aluminum alloy |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3868250A (en) * | 1971-06-14 | 1975-02-25 | Honsel Werke Ag | Heat resistant alloys |
JPS4847608A (en) * | 1971-10-19 | 1973-07-06 | ||
JPS5056304A (en) * | 1973-09-20 | 1975-05-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4297976A (en) | Piston and cylinder assemblies | |
US4817578A (en) | Internal combustion engine | |
US4268309A (en) | Wear-resisting sintered alloy | |
US4590133A (en) | Bearing material | |
US2210593A (en) | Bearing alloy | |
US3918923A (en) | Wear resistant sintered alloy | |
US3909252A (en) | Wear-resistant cast iron for sliding surfaces | |
US4471032A (en) | Aluminum base bearing alloy and bearing composite | |
GB2252773A (en) | Copper alloys | |
KR940004031B1 (en) | Sliding bearing layer composition | |
US5429876A (en) | Copper-lead based bearing alloy material excellent in corrosion resistance and a method of producing the same | |
US3514286A (en) | Wear-resisting aluminum alloys | |
US3983615A (en) | Sliding seal member for an internal combustion engine | |
US5512242A (en) | Tin-base white metal bearing alloy excellent in heat resistance and fatigue resistance | |
US5000915A (en) | Wear-resistant copper alloy | |
US3567436A (en) | Compression resistant zinc base alloy | |
US2357106A (en) | Bearing construction | |
US2357450A (en) | Aluminum alloy | |
US4994235A (en) | Wear-resistance aluminum bronze alloy | |
JP2923578B2 (en) | Wear resistant aluminum alloy | |
US2845918A (en) | Bearing surfaces | |
US5882587A (en) | Lead alloy used for sliding bearing | |
US1940629A (en) | Piston alloy | |
JPH0237418B2 (en) | ||
JPS6210236A (en) | Aluminum alloy cylinder |