US3753695A - Bearing materials - Google Patents
Bearing materials Download PDFInfo
- Publication number
- US3753695A US3753695A US00114660A US3753695DA US3753695A US 3753695 A US3753695 A US 3753695A US 00114660 A US00114660 A US 00114660A US 3753695D A US3753695D A US 3753695DA US 3753695 A US3753695 A US 3753695A
- Authority
- US
- United States
- Prior art keywords
- percent
- bismuth
- aluminium
- weight
- bearing
- 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
- 239000000463 material Substances 0.000 title claims abstract description 21
- 229910052797 bismuth Inorganic materials 0.000 claims abstract description 44
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims abstract description 44
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical group [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 32
- 229910052782 aluminium Inorganic materials 0.000 abstract description 30
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 abstract description 16
- 239000010949 copper Substances 0.000 abstract description 9
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract description 8
- 229910052802 copper Inorganic materials 0.000 abstract description 8
- 229910052759 nickel Inorganic materials 0.000 abstract description 8
- 229910052710 silicon Inorganic materials 0.000 abstract description 7
- 239000010703 silicon Substances 0.000 abstract description 7
- 239000000470 constituent Substances 0.000 abstract description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 abstract description 2
- 239000004411 aluminium Substances 0.000 description 29
- 229910045601 alloy Inorganic materials 0.000 description 20
- 239000000956 alloy Substances 0.000 description 20
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 8
- 229910000831 Steel Inorganic materials 0.000 description 7
- 239000010959 steel Substances 0.000 description 7
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 239000001996 bearing alloy Substances 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 3
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- 229910000978 Pb alloy Inorganic materials 0.000 description 3
- DBRHOLYIDDOQSD-UHFFFAOYSA-N alumane;lead Chemical compound [AlH3].[Pb] DBRHOLYIDDOQSD-UHFFFAOYSA-N 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 229910052748 manganese Inorganic materials 0.000 description 3
- 239000011572 manganese Substances 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 239000012535 impurity Substances 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 239000010705 motor oil Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 229910001152 Bi alloy Inorganic materials 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- -1 lead impurities Chemical compound 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
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
-
- 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
- C22C21/003—Alloys based on aluminium containing at least 2.6% of one or more of the elements: tin, lead, antimony, bismuth, cadmium, and titanium
-
- 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
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/923—Physical dimension
- Y10S428/924—Composite
- Y10S428/925—Relative dimension specified
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12458—All metal or with adjacent metals having composition, density, or hardness gradient
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/1275—Next to Group VIII or IB metal-base component
- Y10T428/12757—Fe
Definitions
- the invention is a bearing material of which a major Cl 38, constituent is aluminum characterised by between 1 75/139, 75/144, 75/148 percent and 16 percent (preferably between 3 percent [51] Int. Cl. C22c 21/02 and 7 percent or between 7 percent and 10 percent or [58] Field of Search 75/138, 139, 143, between 10 percent'and 16 percent of bismuth by 1 75/148, 144; 148/32, 32.5; 29/ 196.2 weight, and optionally including 0 3 percent copper, 1 i 0 3 percent nickel, O 3 percent manganese, 0 1 l [56] References Cited percent silicon.
- a bearing alloy comprises aluminium and more than 1 percent of bismuth by weight. Preferably there is from 7-l0 percent bismuth; or for some purposes there may be up to 16 percent by weight bismuth.
- the aluminium may or not constitute the balance, but will usually constitute at least 50 percent by weight of the material.
- Aluminium/bismuth is an alternative and is believed to have surface properties equal to or better than the three alloys for alloys with the same percentage of the low melting point constituent.
- This desirable property of aluminium/bismuth is believed to be due to the Rhomboidal structure of bismuth.
- the corrosion resistance of bismuth in engine oils is believed to be betterthan, for example, a similar alloy of aluminium-lead.
- Tin is conventionally added to aluminium-lead alloys to increase the corrosion resistance to engine oils and in the comparison we are referring to aluminium-lead without a tin additive.
- Bismuth is also unusual in that it expands when solidifying, and it is believed that this phenomenonmay assist in reducing the tension forces existing along the boundary between the soft material and the surrounding stronger matrix thereby increasing the fatigue strength of the material.
- the porosity of the alloy is reduced if the bismuth expands to fill the interstices in the surrounding aluminium.
- the bismuth provides the surface properties required of a bearing alloy and so the defined composition could be only at or near the bearing surface. However, the whole alloy could also be of uniform composition.
- the bismuth has good surface properties in that it can accommodate dirt being embodied in it without its bearing properties being seriously lost and accordingly it is not necessary to provide a lead/tin or other plated over-lay on the bearing surface as has been found to be necessary in the past for many bearing materials which are primarily of aluminium. The extra expense of including the hismuth is, therefore, compensated for by avoiding the need for such an overlay.
- the invention includes a bearing comprising at least a bearing-surface-layer of an alloy as defined, and also a layer of the alloy bonded to a steel or other backing.
- aluminium/- lead alloys are less than that of an aluminium/bismuth alloy having the same proportion of bismuth.
- the bismuth in an aluminium alloy when rolled down to a thickness suitable for bonding to a steel backing tends to form long stringers which readily form into globules when the alloy is annealed. This contrasts with aluminium/lead alloys which do not form globules readily on annealing.
- This property of aluminium/bismuth in conjunction with the expansion on solidification reduces the forces occurring along the aluminium boundary as compared with tin or lead and provides a potentially greater fatigue strength.
- a bearing alloy consists of:
- Bismuth 3 percent by weight Copper 1 percent by weight Aluminium 96 percent by weight The component metals in correct proportions are introduced into a tun dish and raised to a temperature sufficient to melt them all, after which a billet of the alloy is cast and subsequently rolled into a slab with a thickness of about 0.050 inches. The slab is then bonded to a steel backing to make a bearing strip.
- Bismuth l6 percent by weight Copper l percent by weight Nickel l percent by weight Manganese l percent by weight Silicon ll percent by weight Aluminium percent by weight is melted in a tun dish and poured as a slab into a shallow mould. The alloy is allowed to cool slowly so that most of the bismuth tends to drop through the aluminium which is much lighter, so that at the bottom surface the percentage of bismuth is high, whereas at the top surface there may be very little bismuth. This forms a satisfactory bearing with the high bismuth surface acting as the bearing surface and the low bismuth surface bonded to the steel backing.
- Bismuth l percent by weight Copper 2 percent by weight Silicon 1 percent by weight Aluminium 87 percent by weight The appropriate proportions of the metals were mixed in powder form and the composite powder was sintered on a backing and bonded to the backing by rolling.
- the accompanying drawing shows some test results obtained with aluminium based alloys with bismuth and tin as the second phase. It will be seen that even an alloy with a tin content of about 18.3 percent by weight its cycle to seizure is not significantly better than an alloy with a bismuth content of 13.6 percent. The drawing also shows that an alloy containing 6.2 percent by weight of bismuth gives 200 cycles of seizure while an alloy containing 6.2 percent of tin gives only 140 cycles to seizure.
- a bearing material consisting essentially of bismuth about 16 wt.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Sliding-Contact Bearings (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB705870 | 1970-02-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3753695A true US3753695A (en) | 1973-08-21 |
Family
ID=9825813
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00114660A Expired - Lifetime US3753695A (en) | 1970-02-13 | 1971-02-11 | Bearing materials |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3753695A (enExample) |
| CA (1) | CA958565A (enExample) |
| DE (1) | DE2106391A1 (enExample) |
| FR (1) | FR2078514A5 (enExample) |
| GB (1) | GB1340489A (enExample) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4590133A (en) * | 1985-02-01 | 1986-05-20 | D.A.B. Industries | Bearing material |
| US4747889A (en) * | 1985-05-22 | 1988-05-31 | Sumitomo Electric Industries, Ltd. | Interconnecting wire for semiconductor devices |
| US4957822A (en) * | 1986-11-26 | 1990-09-18 | Glyco-Metall-Werke Daelen & Loos Gmbh | Laminated material for friction bearing elements, comprising an antifriction layer of an aluminum based bearing material |
| US5286445A (en) * | 1990-11-30 | 1994-02-15 | Taiho Kogyo Co., Ltd. | Aluminium bearing alloy containing bismuth |
| US5300368A (en) * | 1990-02-03 | 1994-04-05 | Glyco-Metall-Werke Glyco B.V. & Co. Kg | Highly wear-resistant overlay with improved slip and a method of its production |
| US6315947B1 (en) | 2000-05-23 | 2001-11-13 | Reynolds Metals Company | Free-machining aluminum alloy and method of use |
| US6409966B1 (en) | 1998-05-19 | 2002-06-25 | Reynolds Metals Company | Free machining aluminum alloy containing bismuth or bismuth-tin for free machining and a method of use |
| US6510726B1 (en) | 1998-12-23 | 2003-01-28 | Federal-Mogul World Wide, Inc. | Bismuth tracer bearings |
| US20030143096A1 (en) * | 2002-01-29 | 2003-07-31 | Teruo Shimizu | Sintered alloy article, its production method and a motorized fuel pump comprising a bearing comprised of sintered alloy article |
| US6746154B2 (en) | 2001-10-08 | 2004-06-08 | Federal-Mogul World Wide, Inc. | Lead-free bearing |
| US20160010185A1 (en) * | 2014-07-08 | 2016-01-14 | Samara State Aerospace University | High-temperature stable electro-conductive aluminum-base alloy |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5638667B2 (enExample) * | 1972-01-20 | 1981-09-08 | ||
| US5122207A (en) * | 1991-07-22 | 1992-06-16 | General Motors Corporation | Hypo-eutectic aluminum-silicon-copper alloy having bismuth additions |
| US5106436A (en) * | 1991-09-30 | 1992-04-21 | General Motors Corporation | Wear resistant eutectic aluminum-silicon alloy |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2026546A (en) * | 1933-09-18 | 1936-01-07 | Aluminum Co Of America | Free cutting alloys |
| US2752240A (en) * | 1952-12-27 | 1956-06-26 | Gen Motors Corp | Aluminum base alloy bearing |
| US3410331A (en) * | 1966-03-16 | 1968-11-12 | Gen Motors Corp | Method of casting an aluminumbased bearing alloy |
| US3562884A (en) * | 1968-10-29 | 1971-02-16 | Gen Motors Corp | Aluminum-based alloy bearing material and method of making |
-
1971
- 1971-02-11 US US00114660A patent/US3753695A/en not_active Expired - Lifetime
- 1971-02-11 DE DE19712106391 patent/DE2106391A1/de active Pending
- 1971-02-12 FR FR7104722A patent/FR2078514A5/fr not_active Expired
- 1971-02-12 CA CA105,186A patent/CA958565A/en not_active Expired
- 1971-04-19 GB GB705870A patent/GB1340489A/en not_active Expired
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2026546A (en) * | 1933-09-18 | 1936-01-07 | Aluminum Co Of America | Free cutting alloys |
| US2752240A (en) * | 1952-12-27 | 1956-06-26 | Gen Motors Corp | Aluminum base alloy bearing |
| US3410331A (en) * | 1966-03-16 | 1968-11-12 | Gen Motors Corp | Method of casting an aluminumbased bearing alloy |
| US3562884A (en) * | 1968-10-29 | 1971-02-16 | Gen Motors Corp | Aluminum-based alloy bearing material and method of making |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4590133A (en) * | 1985-02-01 | 1986-05-20 | D.A.B. Industries | Bearing material |
| US4747889A (en) * | 1985-05-22 | 1988-05-31 | Sumitomo Electric Industries, Ltd. | Interconnecting wire for semiconductor devices |
| US4957822A (en) * | 1986-11-26 | 1990-09-18 | Glyco-Metall-Werke Daelen & Loos Gmbh | Laminated material for friction bearing elements, comprising an antifriction layer of an aluminum based bearing material |
| US5300368A (en) * | 1990-02-03 | 1994-04-05 | Glyco-Metall-Werke Glyco B.V. & Co. Kg | Highly wear-resistant overlay with improved slip and a method of its production |
| US5286445A (en) * | 1990-11-30 | 1994-02-15 | Taiho Kogyo Co., Ltd. | Aluminium bearing alloy containing bismuth |
| US6409966B1 (en) | 1998-05-19 | 2002-06-25 | Reynolds Metals Company | Free machining aluminum alloy containing bismuth or bismuth-tin for free machining and a method of use |
| US6510726B1 (en) | 1998-12-23 | 2003-01-28 | Federal-Mogul World Wide, Inc. | Bismuth tracer bearings |
| US6315947B1 (en) | 2000-05-23 | 2001-11-13 | Reynolds Metals Company | Free-machining aluminum alloy and method of use |
| US6746154B2 (en) | 2001-10-08 | 2004-06-08 | Federal-Mogul World Wide, Inc. | Lead-free bearing |
| US20040111892A1 (en) * | 2001-10-08 | 2004-06-17 | Greene Robert L. | Lead-free bearing |
| US6854183B2 (en) | 2001-10-08 | 2005-02-15 | Federal-Mogul World Wide, Inc. | Lead-free bearing |
| US20030143096A1 (en) * | 2002-01-29 | 2003-07-31 | Teruo Shimizu | Sintered alloy article, its production method and a motorized fuel pump comprising a bearing comprised of sintered alloy article |
| US20160010185A1 (en) * | 2014-07-08 | 2016-01-14 | Samara State Aerospace University | High-temperature stable electro-conductive aluminum-base alloy |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2078514A5 (enExample) | 1971-11-05 |
| GB1340489A (en) | 1973-12-12 |
| DE2106391A1 (de) | 1971-08-19 |
| CA958565A (en) | 1974-12-03 |
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