[go: up one dir, main page]

US3514286A - Wear-resisting aluminum alloys - Google Patents

Wear-resisting aluminum alloys Download PDF

Info

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
Application number
US835416A
Inventor
Yataro Unai
Makoto Komatsu
Yasushi Hoshi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Riken Piston Ring Industrial Co Ltd
Original Assignee
Riken Piston Ring Industrial Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Riken Piston Ring Industrial Co Ltd filed Critical Riken Piston Ring Industrial Co Ltd
Application granted granted Critical
Publication of US3514286A publication Critical patent/US3514286A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys 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.
US835416A 1969-06-23 1969-06-23 Wear-resisting aluminum alloys Expired - Lifetime US3514286A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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