US2210593A - Bearing alloy - Google Patents
Bearing alloy Download PDFInfo
- Publication number
- US2210593A US2210593A US287681A US28768139A US2210593A US 2210593 A US2210593 A US 2210593A US 287681 A US287681 A US 287681A US 28768139 A US28768139 A US 28768139A US 2210593 A US2210593 A US 2210593A
- Authority
- US
- United States
- Prior art keywords
- alloys
- bearing
- tin
- alloy
- silver
- 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
- 239000001996 bearing alloy Substances 0.000 title description 4
- 229910045601 alloy Inorganic materials 0.000 description 17
- 239000000956 alloy Substances 0.000 description 17
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 7
- 229910052718 tin Inorganic materials 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 229910001316 Ag alloy Inorganic materials 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 3
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 3
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 229910052802 copper Inorganic materials 0.000 description 3
- 239000010949 copper Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 239000004332 silver Substances 0.000 description 3
- 229910000897 Babbitt (metal) Inorganic materials 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- NTSDHVIXFWZYSM-UHFFFAOYSA-N [Ag].[Sb].[Sn] Chemical compound [Ag].[Sb].[Sn] NTSDHVIXFWZYSM-UHFFFAOYSA-N 0.000 description 2
- 229910052787 antimony Inorganic materials 0.000 description 2
- 239000010974 bronze Substances 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000010956 nickel silver Substances 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- JIAARYAFYJHUJI-UHFFFAOYSA-L zinc dichloride Chemical compound [Cl-].[Cl-].[Zn+2] JIAARYAFYJHUJI-UHFFFAOYSA-L 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- -1 Copper Silver Antimony Tin Lead Chemical compound 0.000 description 1
- 101100379080 Emericella variicolor andB gene Proteins 0.000 description 1
- 241000630665 Hada Species 0.000 description 1
- NEAPKZHDYMQZCB-UHFFFAOYSA-N N-[2-[4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]piperazin-1-yl]ethyl]-2-oxo-3H-1,3-benzoxazole-6-carboxamide Chemical compound C1CN(CCN1CCNC(=O)C2=CC3=C(C=C2)NC(=O)O3)C4=CN=C(N=C4)NC5CC6=CC=CC=C6C5 NEAPKZHDYMQZCB-UHFFFAOYSA-N 0.000 description 1
- 241001387976 Pera Species 0.000 description 1
- 229910001245 Sb alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 239000010951 brass Substances 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
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910002058 ternary alloy Inorganic materials 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 229960001939 zinc chloride Drugs 0.000 description 1
- 235000005074 zinc chloride Nutrition 0.000 description 1
- 239000011592 zinc chloride 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
- C22C13/00—Alloys based on tin
Definitions
- the invention relates to alloys and more particularly to alloys adapted for use as bearings, as for example a lining in a shell of a dlfierent metal. 7
- One of the principal objects of the invention is to obtain an alloy which has better properties and characteristics than Babbitt metal. More particularly, it is an object of the invention to obtain an alloy having higher compression 10 strength at elevated temperature, greater resistance to cracking due to fatigue, more effective bonding to the backing metal while at the same time having at least as good resistance to shaft wear as Babbitt.
- my invention comprises alloys having the following analysis:
- iron, zinc, cadmium and lead may be present singly or in combination providing the total of so these metals is not substantially in excess of 1.5%.
- Example 1 85 Alloy Silver Antimony Tin Percent Percent Example 1 2.12 7. 57 Balance Example 2. 3. 7.32 Do. Example 3 4. 56 4. 49 Do. Example 4 6. 98 6. 72 D0. 40 Example 5 7. 51 6. 89 Do.
- my new silver 'alloys have higher com- My improved bearing alloys are essentially ternary alloys of tin, silver and antimony, although I pression strength at elevated temperatures than Babbitt 'alloys containing corresponding amounts of copper. This is illustrated by the following tests which compare the compression strength both at room and elevated temperatures. In carrying out the tests, cylinders of four compositions, A, B, C and D as listed below, were cast in graphite molds and machined to one-half inch diameter and one and one-half inches length.
- tion D fully machined by turning, boring and broachingin a well known manner.
- the lining metal machined very well and after broaching of the lining had a mirror-like surface, free from porosity, gas holes, oxides or any other defects.
- the bearing lined with composition D was cut into half shells, flattened with a hammer, and after repeated bendings, it was impossible to separate the silver-antimony-tin lining from the steel shell by use of a chisel or any other means except to conventional production practice to fit a wellknown automotive connecting rod.
- the bearings were tested in a standard and generally used testing machine under conditions of loading, shaft speed, oil temperature and duration to simulate extreme hard conditions of engine o pera tion. Similar bearings lined with composition D were tested under the same conditions.
- a hearing alloy comprising antimony 5 to 15%, silver 0.5 to 7.6% and the balance of tin.
- a bearing alloy comprising antimony 6.5% to 8.0%, silver 2 to 7.5% and the balance of tin.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Sliding-Contact Bearings (AREA)
Description
Patented Aug. 6, 1940 Q UNITED STATES 'BEARING ALLOY William E. McCullough, Detroit, Mich., assignor to Bohn Aluminum & Brass Corporation, Detroit, Micln, a corporation of Michigan No Drawing. Application July 31, 1939,
i Serial No. 287,681
2 Claims.
The invention relates to alloys and more particularly to alloys adapted for use as bearings, as for example a lining in a shell of a dlfierent metal. 7
One of the principal objects of the invention is to obtain an alloy which has better properties and characteristics than Babbitt metal. More particularly, it is an object of the invention to obtain an alloy having higher compression 10 strength at elevated temperature, greater resistance to cracking due to fatigue, more effective bonding to the backing metal while at the same time having at least as good resistance to shaft wear as Babbitt.
small amounts of othermetals may sometimes be present either as impurities or intentlonallyf added. p. In its broader aspects, my invention comprises alloys having the following analysis:
Per cent A 0.5 to 1.6 Sh 5.0] to 15.0
Sn Balance However, other metals such as copper, nickel,
iron, zinc, cadmium and lead may be present singly or in combination providing the total of so these metals is not substantially in excess of 1.5%.
As illustrative of my invention, the following specific examples are given:
85 Alloy Silver Antimony Tin Percent Percent Example 1 2.12 7. 57 Balance Example 2. 3. 7.32 Do. Example 3 4. 56 4. 49 Do. Example 4 6. 98 6. 72 D0. 40 Example 5 7. 51 6. 89 Do.
bronze or wrought bronze. In preparingsuch composite bearings, it is desirable to use a flux such as acidified zincchloride on the shells and then to tin the shells. The tinning may be carried outwith pure commercial tin or with an alloy of such tin with up to 15% of lead. Generally speaking, I prefer to use commercially pure tin for the first coating prior to lining with my new alloys.
As before stated, one of the advantages of my new silver 'alloys is that they have higher com- My improved bearing alloys are essentially ternary alloys of tin, silver and antimony, although I pression strength at elevated temperatures than Babbitt 'alloys containing corresponding amounts of copper. This is illustrated by the following tests which compare the compression strength both at room and elevated temperatures. In carrying out the tests, cylinders of four compositions, A, B, C and D as listed below, were cast in graphite molds and machined to one-half inch diameter and one and one-half inches length.
Alloy Copper Silver Antimony Tin Lead Percent Percent Percent I Percent A 2. 12 None 7. 22 Balance 0.'15 B 3. 66 None 6; 79 .do 15 C None 2. 12 7. 57 do 10 D None 3. 40 7. 32 do l5 .it will be observed in the above table that .Babbitt alloys A andB were substantially the same as my new silver alloys C and D except that they had copper instead of the sliver of my alloys. The cylinders were tested under compression and the loads determined at 1% permanent reduction in height of the specimens at F. and
17 permanen 1'7 rmanent 33% time F. 831%; W F.
Lbs. per sq. in. Lbs. per rq. in.
tion D and fully machined by turning, boring and broachingin a well known manner. The lining metal machined very well and after broaching of the lining hada mirror-like surface, free from porosity, gas holes, oxides or any other defects.
To illustrate another advantage of my alloys the bearing lined with composition D was cut into half shells, flattened with a hammer, and after repeated bendings, it was impossible to separate the silver-antimony-tin lining from the steel shell by use of a chisel or any other means except to conventional production practice to fit a wellknown automotive connecting rod. The bearings were tested in a standard and generally used testing machine under conditions of loading, shaft speed, oil temperature and duration to simulate extreme hard conditions of engine o pera tion. Similar bearings lined with composition D were tested under the same conditions.
that Time beam] Shaft Bearing of op- 011 was Oil Bearing speed, load, erasure, temp., temp., R. P. M. P. s. 1. tion, P. s. I. F. F mm hours alloy 2 3200 1382 1 75 221 250 240 3750 1897 1 75 238 276 266 4000 2159 20 75 273 1 D 1800 437 l 75 207 g 2800 1058 1 75 205 $1 1 3200 1382 1 75 210 g 3750 1897 1 75 233 273 278 4000 2159 20 75 242 297 297 The schedule of oil and bearing temperatures show the variations normally experienced in such testing, the early variations occurring during the conformation of the bearing surfaces to the .shafts. At the end of the tests the bearings were ings after approximately 30,000-40,000 miles of 3 engine operation in an automobile, the superiority of my alloys when used as'bearing liningslfor 1 engines is clearly indicated.
The above tests show thattmy new silver-alloys have physical properties of such a character 1 as to make them more desirable for use as linings in bearing shells than the Babbitt metal of the prior art. Thus by means of my invention I have produced an improved composite bearing. a
What I claim as my invention is:
1. A hearing alloy comprising antimony 5 to 15%, silver 0.5 to 7.6% and the balance of tin.
2. A bearing alloy comprising antimony 6.5% to 8.0%, silver 2 to 7.5% and the balance of tin.
W'HLIAM E. MCCULLOUGH.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US287681A US2210593A (en) | 1939-07-31 | 1939-07-31 | Bearing alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US287681A US2210593A (en) | 1939-07-31 | 1939-07-31 | Bearing alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2210593A true US2210593A (en) | 1940-08-06 |
Family
ID=23103902
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US287681A Expired - Lifetime US2210593A (en) | 1939-07-31 | 1939-07-31 | Bearing alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2210593A (en) |
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2479500A (en) * | 1946-08-26 | 1949-08-16 | Harry E Longberg | Illuminating means |
| US4170472A (en) * | 1977-04-19 | 1979-10-09 | Motorola, Inc. | Solder system |
| US4869871A (en) * | 1988-03-17 | 1989-09-26 | Toyota Motor Corporation | Pb-Sn-Sb-In solder alloy |
| US5314758A (en) * | 1992-03-27 | 1994-05-24 | The Louis Berkman Company | Hot dip terne coated roofing material |
| US5354624A (en) * | 1992-07-15 | 1994-10-11 | The Louis Berkman Company | Coated copper roofing material |
| US5395702A (en) * | 1992-03-27 | 1995-03-07 | The Louis Berkman Company | Coated metal strip |
| US5397652A (en) * | 1992-03-27 | 1995-03-14 | The Louis Berkman Company | Corrosion resistant, colored stainless steel and method of making same |
| US5455122A (en) * | 1993-04-05 | 1995-10-03 | The Louis Berkman Company | Environmental gasoline tank |
| US5470667A (en) * | 1993-04-05 | 1995-11-28 | The Louis Berkman Company | Coated metal strip |
| US5489490A (en) * | 1993-04-05 | 1996-02-06 | The Louis Berkman Company | Coated metal strip |
| US5491035A (en) * | 1992-03-27 | 1996-02-13 | The Louis Berkman Company | Coated metal strip |
| US5491036A (en) * | 1992-03-27 | 1996-02-13 | The Louis Berkman Company | Coated strip |
| US5492772A (en) * | 1993-04-05 | 1996-02-20 | The Louis Berkman Company | Building material coating |
| US5597656A (en) * | 1993-04-05 | 1997-01-28 | The Louis Berkman Company | Coated metal strip |
| US6080497A (en) * | 1992-03-27 | 2000-06-27 | The Louis Berkman Company | Corrosion-resistant coated copper metal and method for making the same |
| US6652990B2 (en) | 1992-03-27 | 2003-11-25 | The Louis Berkman Company | Corrosion-resistant coated metal and method for making the same |
| US6794060B2 (en) | 1992-03-27 | 2004-09-21 | The Louis Berkman Company | Corrosion-resistant coated metal and method for making the same |
| US20040214029A1 (en) * | 1992-03-27 | 2004-10-28 | The Louis Berkman Company, An Ohio Corporation | Corrosion-resistant coated copper and method for making the same |
-
1939
- 1939-07-31 US US287681A patent/US2210593A/en not_active Expired - Lifetime
Cited By (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2479500A (en) * | 1946-08-26 | 1949-08-16 | Harry E Longberg | Illuminating means |
| US4170472A (en) * | 1977-04-19 | 1979-10-09 | Motorola, Inc. | Solder system |
| US4869871A (en) * | 1988-03-17 | 1989-09-26 | Toyota Motor Corporation | Pb-Sn-Sb-In solder alloy |
| US5491035A (en) * | 1992-03-27 | 1996-02-13 | The Louis Berkman Company | Coated metal strip |
| US20070023111A1 (en) * | 1992-03-27 | 2007-02-01 | The Louis Berkman Company, A Corporation Of Ohio | Corrosion-resistant fuel tank |
| US5395702A (en) * | 1992-03-27 | 1995-03-07 | The Louis Berkman Company | Coated metal strip |
| US5395703A (en) * | 1992-03-27 | 1995-03-07 | The Louis Berkman Company | Hot dip terne coated roofing material |
| US5397652A (en) * | 1992-03-27 | 1995-03-14 | The Louis Berkman Company | Corrosion resistant, colored stainless steel and method of making same |
| US5314758A (en) * | 1992-03-27 | 1994-05-24 | The Louis Berkman Company | Hot dip terne coated roofing material |
| US7575647B2 (en) | 1992-03-27 | 2009-08-18 | The Louis Berkman Co. | Corrosion-resistant fuel tank |
| US5480731A (en) * | 1992-03-27 | 1996-01-02 | The Louis Berkman Company | Hot dip terne coated roofing material |
| US20070104975A1 (en) * | 1992-03-27 | 2007-05-10 | The Louis Berkman Company | Corrosion-resistant coated copper and method for making the same |
| US6858322B2 (en) | 1992-03-27 | 2005-02-22 | The Louis Berkman Company | Corrosion-resistant fuel tank |
| US5491036A (en) * | 1992-03-27 | 1996-02-13 | The Louis Berkman Company | Coated strip |
| US6811891B2 (en) | 1992-03-27 | 2004-11-02 | The Louis Berkman Company | Corrosion-resistant coated metal and method for making the same |
| US5520964A (en) * | 1992-03-27 | 1996-05-28 | The Louis Berkman Company | Method of coating a metal strip |
| US7045221B2 (en) | 1992-03-27 | 2006-05-16 | The Louis Berkman Company | Corrosion-resistant coated copper and method for making the same |
| US5616424A (en) * | 1992-03-27 | 1997-04-01 | The Louis Berkman Company | Corrosion-resistant coated metal strip |
| US5667849A (en) * | 1992-03-27 | 1997-09-16 | The Louis Berkman Company | Method for coating a metal strip |
| US6861159B2 (en) | 1992-03-27 | 2005-03-01 | The Louis Berkman Company | Corrosion-resistant coated copper and method for making the same |
| US6080497A (en) * | 1992-03-27 | 2000-06-27 | The Louis Berkman Company | Corrosion-resistant coated copper metal and method for making the same |
| US6652990B2 (en) | 1992-03-27 | 2003-11-25 | The Louis Berkman Company | Corrosion-resistant coated metal and method for making the same |
| US6794060B2 (en) | 1992-03-27 | 2004-09-21 | The Louis Berkman Company | Corrosion-resistant coated metal and method for making the same |
| US20040213916A1 (en) * | 1992-03-27 | 2004-10-28 | The Louis Berkman Company, A Corporation Of Ohio | Corrosion-resistant fuel tank |
| US20040214029A1 (en) * | 1992-03-27 | 2004-10-28 | The Louis Berkman Company, An Ohio Corporation | Corrosion-resistant coated copper and method for making the same |
| US5354624A (en) * | 1992-07-15 | 1994-10-11 | The Louis Berkman Company | Coated copper roofing material |
| US5455122A (en) * | 1993-04-05 | 1995-10-03 | The Louis Berkman Company | Environmental gasoline tank |
| US5695822A (en) * | 1993-04-05 | 1997-12-09 | The Louis Berkman Company | Method for coating a metal strip |
| US5597656A (en) * | 1993-04-05 | 1997-01-28 | The Louis Berkman Company | Coated metal strip |
| US5492772A (en) * | 1993-04-05 | 1996-02-20 | The Louis Berkman Company | Building material coating |
| US5489490A (en) * | 1993-04-05 | 1996-02-06 | The Louis Berkman Company | Coated metal strip |
| US5470667A (en) * | 1993-04-05 | 1995-11-28 | The Louis Berkman Company | Coated metal strip |
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