US2288655A - Metal alloy - Google Patents
Metal alloy Download PDFInfo
- Publication number
- US2288655A US2288655A US167707A US16770737A US2288655A US 2288655 A US2288655 A US 2288655A US 167707 A US167707 A US 167707A US 16770737 A US16770737 A US 16770737A US 2288655 A US2288655 A US 2288655A
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- US
- United States
- Prior art keywords
- cadmium
- alloy
- indium
- alloys
- silver
- Prior art date
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- 229910001092 metal group alloy Inorganic materials 0.000 title description 2
- 229910052793 cadmium Inorganic materials 0.000 description 41
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 40
- 229910045601 alloy Inorganic materials 0.000 description 39
- 239000000956 alloy Substances 0.000 description 39
- 229910052738 indium Inorganic materials 0.000 description 29
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 29
- 239000002253 acid Substances 0.000 description 15
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 12
- 150000007513 acids Chemical class 0.000 description 11
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 9
- 239000004332 silver Substances 0.000 description 9
- 238000005260 corrosion Methods 0.000 description 8
- 230000007797 corrosion Effects 0.000 description 8
- 229910052709 silver Inorganic materials 0.000 description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 7
- 229910052802 copper Inorganic materials 0.000 description 7
- 239000010949 copper Substances 0.000 description 7
- 239000001996 bearing alloy Substances 0.000 description 6
- 239000000314 lubricant Substances 0.000 description 6
- 239000010687 lubricating oil Substances 0.000 description 6
- 229910052759 nickel Inorganic materials 0.000 description 6
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 5
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 5
- 229910052749 magnesium Inorganic materials 0.000 description 5
- 239000011777 magnesium Substances 0.000 description 5
- 229910000925 Cd alloy Inorganic materials 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 229910001316 Ag alloy Inorganic materials 0.000 description 3
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 3
- 229910052787 antimony Inorganic materials 0.000 description 3
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 3
- NSAODVHAXBZWGW-UHFFFAOYSA-N cadmium silver Chemical compound [Ag].[Cd] NSAODVHAXBZWGW-UHFFFAOYSA-N 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 229910052725 zinc Inorganic materials 0.000 description 3
- 239000011701 zinc Substances 0.000 description 3
- XKMAKWPZGDBONG-UHFFFAOYSA-N [Co].[Cd] Chemical compound [Co].[Cd] XKMAKWPZGDBONG-UHFFFAOYSA-N 0.000 description 2
- PLZFHNWCKKPCMI-UHFFFAOYSA-N cadmium copper Chemical compound [Cu].[Cd] PLZFHNWCKKPCMI-UHFFFAOYSA-N 0.000 description 2
- OJIJEKBXJYRIBZ-UHFFFAOYSA-N cadmium nickel Chemical compound [Ni].[Cd] OJIJEKBXJYRIBZ-UHFFFAOYSA-N 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000002480 mineral oil Substances 0.000 description 2
- 150000007524 organic acids Chemical class 0.000 description 2
- 235000005985 organic acids Nutrition 0.000 description 2
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 229910000979 O alloy Inorganic materials 0.000 description 1
- 238000010521 absorption reaction Methods 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
- 230000015572 biosynthetic process Effects 0.000 description 1
- WZGKIRHYWDCEKP-UHFFFAOYSA-N cadmium magnesium Chemical compound [Mg].[Cd] WZGKIRHYWDCEKP-UHFFFAOYSA-N 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 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
- 238000004070 electrodeposition Methods 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 230000005764 inhibitory process Effects 0.000 description 1
- 239000010699 lard oil Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 235000010446 mineral oil Nutrition 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000002633 protecting effect Effects 0.000 description 1
- PMXCMJLOPOFPBT-HNNXBMFYSA-N purvalanol A Chemical compound C=12N=CN(C(C)C)C2=NC(N[C@@H](CO)C(C)C)=NC=1NC1=CC=CC(Cl)=C1 PMXCMJLOPOFPBT-HNNXBMFYSA-N 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
Images
Classifications
-
- 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
- F16C9/00—Bearings for crankshafts or connecting-rods; Attachment of connecting-rods
- F16C9/04—Connecting-rod bearings; Attachments thereof
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C20/00—Alloys based on cadmium
-
- 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
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/10—Sliding-contact bearings for exclusively rotary movement for both radial and axial load
-
- 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
- F16C33/122—Multilayer structures of sleeves, washers or liners
- F16C33/125—Details of bearing layers, i.e. the lining
-
- 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
- F16C2204/00—Metallic materials; Alloys
- F16C2204/30—Alloys based on one of tin, lead, antimony, bismuth, indium, e.g. materials for providing sliding surfaces
-
- 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
- Y10S29/00—Metal working
- Y10S29/022—Method or apparatus using indium
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49709—Specific metallic composition
Definitions
- This invention relates to alloys and more particularly to alloys containing a substantial amount'of cadmium.
- Various alloys of cadmium without tin have been proposed for use in the surface portions oi relatively moving parts.
- Such alloys may include cadmium-copper, cadmium-- nickel, cadmium-silver, cadmium-cobalt, cadmium-magnesium and various other alloys containing two or more metals including cadmium in the absence of tin.
- the additional metalsadded to the cadmium act as .hardening and strengthening agents.
- Cadmium alone has been contacting areas of cylindersand pistons.
- alloys of cadmium and silver'lto be highly satisfactory-dot friction surfaces, particularly in the presence of small percentages of additional metals, such as nickel, copper or antimony, which form relatively hard inclusions or particles within the ground mass of the alloy.
- the proportion of the'ingredients of the'cadmium-silver alloy are preferably within the limits 01' 54% silver, .25-1% hardening metal and the balance cadmium. More specificallyfl prefer the composition silver 1.75.2.50%, copper,
- One cadmium-copper alloy employed for bearings includes 95-97% cadmium and from 34% 30 of copper. Magnesium up to .5% may be added to this alloy.
- Another known cadmium-coppermagnesium bearing alloy contains copper .2%- 1.5%, magnesium .1%-.'l5%, balance cadmium.
- the cadmium-nickel bearing alloys have usually contained from .25%-'l% nickel and the balance substantially cadmium, Magnesium, zinc, copper, antimony and aluminum up to 3% may be added to this alloy. It has also been proposed to employ an alloy for bearings composed of cadmium and magnesium withoutcopper. In this case the magnesium may be present in amount up to 5%,with the balance cadmium.
- the cadmium-cobalt bearing alloys consist of cobalt 1.5%-% and the balance cadmium.
- Other lubricants for example, some mineral oil lubricants, when subjected to high temperatures, as
- the alloy When applied electrolytically, or otherwise, to the surface it may be desirable to thereafter subject'the alloy to heat treatment to diffuse the indium into the alloy to some extent.
- heat treatment may be carried'out by merely subject ing the material which has been preliminarily coated with metallic indium, to a temperature below the melting point of the material but sufthrough .10-.l5" of a cadmium or a cadmium base alloy is accomplished in about two hours at 340 F.
- indium within the range .4-.8% substantially prevents corrosion even when the bearing alloy is tested in prepared oils having a much greater corrosive effect than average lubricating oils after high temperature service.
- the indium is applied to the surface portion only of the cadmium or alloythereof, the amount required obviously will depend upon the extent of absorption of the indium or the depth of penetration in the cadmium or cadmium alloy. In cases in which it is desired to substantially uniformly difiuse the indium throughout the cadmium or alloy thereof the amount necessary will be comparable with that in which the bearing is originally made from a homogeneous alloy.
- the cadmiumnickel bonding alloy may be composed of nickel from .75-2% with the balance substantially all cadmium. Preferably, the nickel is used in a percentage of around 1%.
- the cadmium-zinc bonding alloy may contain zinc from 5-20%.
- the remainder substantially cadmium.
- the alloy given in this example compares favorindium and having 2% or more of silver with the advantage for the indium containing alloy of greatly increased resistance to acid.
- Alloys containing substantial amounts of tin, as the usuaIBabbitt metals, are not subject to attack by the acids occurring in lubricating oils.
- Tin may be added to cadmium and alloys thereof in order to protect the cadmium from corrosive agencies. However, when tin is added to cadmium in sufficient quantity to protect the same from acids in lubricating oils the alloy is too brittle for satisfactory use in bearings.
- indium necessary to protect cadmium and alloys containing a substantial amount of cadmium from other corrosive media will, of course, depend on the corrosive characteristics of the particular medium. In general, from .1%l% of indium has a substantial effect in preventing 0r-resisting corrosion of thecadmium or cadmium base alloys. poses where the cost of the indium is not a deciding factor and/or the medium has excessive corrosive properties greater amounts of indium For some purv to a steel backing. For this reason it is highly desirable to bond the cadmium or cadmium al- 10y to the steel backing and thereafter apply the indium to the bearing surface, as by electrodeposition. Thereupon the indium may be diffused into the bearing by heat treatment at a temperature of 340 F. or higher. In this way the alloy may be readily bonded to the steel backing.
- the cadmium-nickel bonding alloy is greatly preferred since with this alloy the bond is not weakened during the subsequent step of diffusing the indiuminto the bearing.
- a bearing alloy composed of silver 2.25%, 0.25% copper and the balance cadmium may be readily bonded to a steel backing by the use of a cadmium-nickel bonding alloy. 'I'hereupon the bearing surface may be electroplated with the desired amount of indium and that strength of the bond apparently is not affected even after holding at this temperature for sixty hours.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Sliding-Contact Bearings (AREA)
Description
proposed as a bearing surface for Patented July 7,
METAL ALLOY Clarence F. Smart, Pontiac, Mich., asslgnor to General Motors Corporation, Detroit, Mich., a
corporation of Delaware Application October 7, 1937, Serial No. 167,707
Claims.
This invention relates to alloys and more particularly to alloys containing a substantial amount'of cadmium. Various alloys of cadmium without tin have been proposed for use in the surface portions oi relatively moving parts. Such alloys may include cadmium-copper, cadmium-- nickel, cadmium-silver, cadmium-cobalt, cadmium-magnesium and various other alloys containing two or more metals including cadmium in the absence of tin. In general, the additional metalsadded to the cadmium act as .hardening and strengthening agents. Cadmium alone has been contacting areas of cylindersand pistons.
I have found, for example, alloys of cadmium and silver'lto be highly satisfactory-dot friction surfaces, particularly in the presence of small percentages of additional metals, such as nickel, copper or antimony, which form relatively hard inclusions or particles within the ground mass of the alloy. p
The proportion of the'ingredients of the'cadmium-silver alloy are preferably within the limits 01' 54% silver, .25-1% hardening metal and the balance cadmium. More specificallyfl prefer the composition silver 1.75.2.50%, copper,
nickel or antimony, separately or in mixtures .25-.5% cadmium 97-98%;
One cadmium-copper alloy employed for bearings includes 95-97% cadmium and from 34% 30 of copper. Magnesium up to .5% may be added to this alloy. Another known cadmium-coppermagnesium bearing alloy contains copper .2%- 1.5%, magnesium .1%-.'l5%, balance cadmium.
The cadmium-nickel bearing alloys have usually contained from .25%-'l% nickel and the balance substantially cadmium, Magnesium, zinc, copper, antimony and aluminum up to 3% may be added to this alloy. It has also been proposed to employ an alloy for bearings composed of cadmium and magnesium withoutcopper. In this case the magnesium may be present in amount up to 5%,with the balance cadmium.
The cadmium-cobalt bearing alloys consist of cobalt 1.5%-% and the balance cadmium.
Cadmium and the above described alloys thereoi, as well as other alloys containing a substantial amount of cadmium, are subject to attack by various acids and other corrosive media. The commercial use of thecadmium base alloys for bearings, for example, has been retarded due to the corrosive action of acids present in, or formed during the use of certain lubricants. Some lubricants or ingredients thereof, such as rode cadmium and cadmium base alloys. Other lubricants, for example, some mineral oil lubricants, when subjected to high temperatures, as
.275" F. or higher, in the presence of air tend to oxidize to produce acids which have a similar eifect. Long life of bearings containing a substantial amount of cadmium may, therefore, be
seriously affected by the presence of such acids,
particularly under hard service conditions, such as those that occur in automobile engines.
I have found that corrosion of cadmium and alloys thereof by certain acids and other corrosive media may be substantially prevented by the presence of small quantities of indium. I contemplate the use of the indium either as a constituent in a substantially homogeneous alloy or by applying the indium to the surface of the cadmium or cadmium alloys, for example, by
electrolytic processes.
When applied electrolytically, or otherwise, to the surface it may be desirable to thereafter subject'the alloy to heat treatment to diffuse the indium into the alloy to some extent. Such heat treatment may be carried'out by merely subject ing the material which has been preliminarily coated with metallic indium, to a temperature below the melting point of the material but sufthrough .10-.l5" of a cadmium or a cadmium base alloy is accomplished in about two hours at 340 F.
* The, amount of indium required to effect a commercially satisfactory prevention of attack by the acids present in, or formed during use of 'certain'lubricants is relatively small. When the indium is introduced into the bearing by formation of a homogeneous alloy, from one-tenth of one per cent to one per cent is ioundto be suflicient, the amount varying, of course, with the degree of inhibition desired or to the extent to 5 which corrosive acids are present or are produced in lubricants. Larger amounts might, of course, be used butthe cost of indium renders it desirable to restrict the content to the amount necessary to effect the desired inertness to attack by acid products in lubricating oil. In many instances indipm within the range .2-.4%
has proven suflicient to substantially retard corrosion of cadmium and cadmiumbase alloys when subjected to corrosive media'such as the lard oil, contain organic acids that tend to cor 56 acids present in lubricating oils. However, where conditions are quite severe a higher content of indium is preferred. For example, indium within the range .4-.8% substantially prevents corrosion even when the bearing alloy is tested in prepared oils having a much greater corrosive effect than average lubricating oils after high temperature service. I
If, however, the indium is applied to the surface portion only of the cadmium or alloythereof, the amount required obviously will depend upon the extent of absorption of the indium or the depth of penetration in the cadmium or cadmium alloy. In cases in which it is desired to substantially uniformly difiuse the indium throughout the cadmium or alloy thereof the amount necessary will be comparable with that in which the bearing is originally made from a homogeneous alloy.
aaaaeae containing cadmium and nickel or cadmium and zinc the facing i having at least at the surface a content or coating of indium 9. The cadmiumnickel bonding alloy may be composed of nickel from .75-2% with the balance substantially all cadmium. Preferably, the nickel is used in a percentage of around 1%. The cadmium-zinc bonding alloy may contain zinc from 5-20%. and
- cadmium from 80-95%.
, bonding a homogeneous alloy containing indium When the indium is employed as a constituent of a homogeneous alloy its presence has efiects similar in some respects to those produced by silver. It is therefore possible to reduce the silver content of cadmium-silver alloys to some extent while still retaining the desirable hardness and toughness imparted otherwise by a larger silver content. The following may be given as an example of a composition which has been found to have satisfactory properties as a bearing alloy and suitable resistance to corrosion of acids resulting from oxidation of mineral oils:
heated to a temperature of 340 F. Tests show per cent Silver 1-1.25 Copper 0.25 Indium 0.2-0.4
The remainder substantially cadmium.
The alloy given in this example compares favorindium and having 2% or more of silver with the advantage for the indium containing alloy of greatly increased resistance to acid.
Alloys containing substantial amounts of tin, as the usuaIBabbitt metals, are not subject to attack by the acids occurring in lubricating oils. Tin may be added to cadmium and alloys thereof in order to protect the cadmium from corrosive agencies. However, when tin is added to cadmium in sufficient quantity to protect the same from acids in lubricating oils the alloy is too brittle for satisfactory use in bearings.
The amount of indium necessary to protect cadmium and alloys containing a substantial amount of cadmium from other corrosive media will, of course, depend on the corrosive characteristics of the particular medium. In general, from .1%l% of indium has a substantial effect in preventing 0r-resisting corrosion of thecadmium or cadmium base alloys. poses where the cost of the indium is not a deciding factor and/or the medium has excessive corrosive properties greater amounts of indium For some purv to a steel backing. For this reason it is highly desirable to bond the cadmium or cadmium al- 10y to the steel backing and thereafter apply the indium to the bearing surface, as by electrodeposition. Thereupon the indium may be diffused into the bearing by heat treatment at a temperature of 340 F. or higher. In this way the alloy may be readily bonded to the steel backing.
The cadmium-nickel bonding alloy is greatly preferred since with this alloy the bond is not weakened during the subsequent step of diffusing the indiuminto the bearing. For example, I have found that a bearing alloy composed of silver 2.25%, 0.25% copper and the balance cadmium may be readily bonded to a steel backing by the use of a cadmium-nickel bonding alloy. 'I'hereupon the bearing surface may be electroplated with the desired amount of indium and that strength of the bond apparently is not affected even after holding at this temperature for sixty hours.
trated is merely an example of one use of the invention and is not intended as any limitation of the scope of the invention.
While I have set' forth herein specific examples of alloys protected against acid attack by the presence of indium, it is not intended to restrict the invention to any specific alloy nor any particular amount of indium. I believe that I am the first to have discovered the protecting effect of indium in preventing the corrosion of cadmium and cadmium base alloys and especially the inhibiting effect of indium in preventing corrosion due to organic acids in lubricating oils, and it is therefore desired to cover such discovery in broad terms.
This application is a continuation in part of my copending application S. N. 43,468 filed Oc-' 0 alloy being characterized by substantial freedom from corrosion caused by acid products in lubrican s.
(lLARENCE F. SMART.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US167707A US2288655A (en) | 1937-10-07 | 1937-10-07 | Metal alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US167707A US2288655A (en) | 1937-10-07 | 1937-10-07 | Metal alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2288655A true US2288655A (en) | 1942-07-07 |
Family
ID=22608476
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US167707A Expired - Lifetime US2288655A (en) | 1937-10-07 | 1937-10-07 | Metal alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2288655A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2456594A (en) * | 1945-03-22 | 1948-12-14 | Monroe Sherman | Brazing alloy |
| US2845918A (en) * | 1955-03-07 | 1958-08-05 | Gen Motors Corp | Bearing surfaces |
| US3150901A (en) * | 1961-11-17 | 1964-09-29 | Gen Electric | Bearing surfaces |
| US3449032A (en) * | 1965-07-16 | 1969-06-10 | Schmidt Gmbh Karl | Bearing and housing installation |
| US3805972A (en) * | 1971-09-21 | 1974-04-23 | Nadella | Stack of coaxial race plates for a thrust needle or roller bearing |
| US5468071A (en) * | 1992-07-10 | 1995-11-21 | Centre Stephanois De Recherches Mecaniques Hydromecanique Et Frottement | Bearing shell for heavily loaded bearings with a rolled strip interference or force fit lining |
-
1937
- 1937-10-07 US US167707A patent/US2288655A/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2456594A (en) * | 1945-03-22 | 1948-12-14 | Monroe Sherman | Brazing alloy |
| US2845918A (en) * | 1955-03-07 | 1958-08-05 | Gen Motors Corp | Bearing surfaces |
| US3150901A (en) * | 1961-11-17 | 1964-09-29 | Gen Electric | Bearing surfaces |
| US3449032A (en) * | 1965-07-16 | 1969-06-10 | Schmidt Gmbh Karl | Bearing and housing installation |
| US3805972A (en) * | 1971-09-21 | 1974-04-23 | Nadella | Stack of coaxial race plates for a thrust needle or roller bearing |
| US5468071A (en) * | 1992-07-10 | 1995-11-21 | Centre Stephanois De Recherches Mecaniques Hydromecanique Et Frottement | Bearing shell for heavily loaded bearings with a rolled strip interference or force fit lining |
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