Patent US4189525A successfully refreshed from Google Patents.
US4189525A
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US
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Bearing metal for large engines
Assignee: Daido Metal Co Ltd
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Filing: 1978-09-26
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Granted: 1980-02-19
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Expires: 1998-09-26
Abstract
Abstract A bearing metal for large size engines having excellent compatibility and as well as embeddability even when used under a poorly lubricated condition. Such bearing metal consists of three or four layers, including a layer of a bearing alloy which contains more than 50% and up to 65% by weight of tin, with the remainder being made up of aluminum, and which may also include less than 0.5% by weight of copper. This bearing alloy has a hardness at high temperature exceeding 100 DEG C. lying between that of aluminum-tin bearing alloys which contain up to 50% by weight of tin and that of tin base or lead base white metal bearing alloys.
Inventors
- 👤 Sanae Mori
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 09:44
CPC Classifications
C; C23; C23C; C23C28/00; C23C28/02; C23C28/023; C23C28/021; F; F16; F16C; F16C33/00; F16C33/02; F16C33/04; F16C33/06; F16C33/12; F16C33/122; F16C2204/00; F16C2204/20; F16C2204/60; Y; Y10; Y10T; Y10T428/00; Y10T428/12; Y10T428/12493; Y10T428/12687; Y10T428/12708; Y10T428/12722; Y10T428/12736; Y10T428/1275; Y10T428/12757; Y10T428/12764; Y10T428/12771; Y10T428/12861; Y10T428/12951; Y10T428/12972
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
103 words
A bearing metal for large engines consisting of three layers, a steel backing layer, an aluminum or aluminum alloy middle layer, and a bearing alloy layer; wherein the composition of the bearing alloy layer consists essentially of more than 50% and up to 65% by weight of tin, up to 0.5% by weight of copper and the remainder substantially being aluminum and the said bearing alloy having a hardness at high temperatures exceeding 100° C. lying between that of aluminum-tin bearing alloys which contain up to 50% by weight of tin and that of tin base or lead base white metal bearing alloys.
Claim 2
Dependent Claim
103 words
A bearing metal for large engines consisting of three layers, a steel backing layer, an aluminum or aluminum alloy middle layer, and a bearing alloy layer; wherein the composition of the bearing alloy layer consists essentially of more than 50% and up to 65% by weight of tin, up to 0.5% by weight of copper and the remainder substantially being aluminum and the said bearing alloy having a hardness at high temperatures exceeding 100° C. lying between that of aluminum-tin bearing alloys which contain up to 50% by weight of tin and that of tin base or lead base white metal bearing alloys.
Claim 3
Dependent Claim
104 words
A bearing metal for large engines consisting of a steel backing layer, an aluminum or aluminum alloy middle layer, a bearing alloy layer and a lead-base alloy surface layer on the bearing alloy layer; wherein the composition of said bearing alloy layer consists essentially of more than 50% and up to 65% by weight of tin and the remainder substantially being aluminum, and said bearing alloy having a hardness at high temperatures exceeding 100° C. lying midway between that of aluminum-tin bearing alloys which contain up to 50% by weight of tin and that of tin base or lead base white metal bearing alloys.
Claim 4
Dependent Claim
104 words
A bearing metal for large engines consisting of a steel backing layer, an aluminum or aluminum alloy middle layer, a bearing alloy layer and a lead-base alloy surface layer on the bearing alloy layer; wherein the composition of said bearing alloy layer consists essentially of more than 50% and up to 65% by weight of tin and the remainder substantially being aluminum, and said bearing alloy having a hardness at high temperatures exceeding 100° C. lying midway between that of aluminum-tin bearing alloys which contain up to 50% by weight of tin and that of tin base or lead base white metal bearing alloys.
Claim 5
Dependent Claim
109 words
A bearing metal for large engine consisting of a steel backing layer, an aluminum or aluminum alloy middle layer, a bearing alloy layer, and a lead-base alloy surface layer on the bearing alloy layer; wherein the composition of said bearing alloy layer consists essentially of more than 50% and up to 65% by weight of tin, up to 0.5% by weight of copper and the remainder substantially being aluminum, and the bearing alloy having a hardness at temperatures exceeding 100° C. lying between that of aluminum-tin bearing alloys which contain up to 50% by weight of tin, and that of tin base or lead base white metal bearing alloys.
Claim 6
Dependent Claim
109 words
A bearing metal for large engine consisting of a steel backing layer, an aluminum or aluminum alloy middle layer, a bearing alloy layer, and a lead-base alloy surface layer on the bearing alloy layer; wherein the composition of said bearing alloy layer consists essentially of more than 50% and up to 65% by weight of tin, up to 0.5% by weight of copper and the remainder substantially being aluminum, and the bearing alloy having a hardness at temperatures exceeding 100° C. lying between that of aluminum-tin bearing alloys which contain up to 50% by weight of tin, and that of tin base or lead base white metal bearing alloys.
Claim 7
Dependent Claim
146 words
A cross-head pin bearing for large marine diesel engines comprising a steel backing layer; a middle bonding layer of foil thickness and consisting of aluminum or aluminum alloy containing no added tin; and a bearing alloy layer disposed over said middle layer and consisting essentially of more than 50% and up to 65% by weight of tin with the remainder being substantially aluminum, said bearing alloy having a hardness at temperatures above 100° C. between that of aluminum-tin alloys containing up to 50% by weight tin and that of tin base or lead base white metal bearing alloys, whereby said bearing alloy has a hardness at 100° C. below 25 Hv and above 17 Hv, and a hardness at 200° C. less than 20 HV and greater than 12 Hv; and wherein said bearing alloy has a low hardness at room temperature not exceeding 27 Hv.
Claim 8
Dependent Claim
146 words
A cross-head pin bearing for large marine diesel engines comprising a steel backing layer; a middle bonding layer of foil thickness and consisting of aluminum or aluminum alloy containing no added tin; and a bearing alloy layer disposed over said middle layer and consisting essentially of more than 50% and up to 65% by weight of tin with the remainder being substantially aluminum, said bearing alloy having a hardness at temperatures above 100° C. between that of aluminum-tin alloys containing up to 50% by weight tin and that of tin base or lead base white metal bearing alloys, whereby said bearing alloy has a hardness at 100° C. below 25 Hv and above 17 Hv, and a hardness at 200° C. less than 20 HV and greater than 12 Hv; and wherein said bearing alloy has a low hardness at room temperature not exceeding 27 Hv.
Claim 9
Dependent Claim
17 words
A bearing in accordance with claim 1, wherein said bearing alloy comprises approximately 55% by weight tin.
Claim 10
Dependent Claim
18 words
A bearing in accordance with claim 5, wherein said bearing alloy further comprises up to about 0.3% copper.
Claim 11
Dependent Claim
35 words
A bearing in accordance with claim 1, wherein said bearing alloy further comprises one or more of nickel, silicon, antimony, manganese, lead or zinc, with the total sum thereof being less than 2% by weight.
References Cited (Backward Citations)
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Cited
GB666087A
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US2586099A
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GB722552A
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US2741016A
Cited
US2852365A
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US3809551A
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-02-18 | 1983-08-20 | 1984-02-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-02-18 | 1987-08-20 | 1988-02-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-02-18 | 1991-08-20 | 1992-02-19 | $7700.00 | Window Closed / Lapsed |