US1904176A - Cadmium-nickel alloy - Google Patents
Cadmium-nickel alloy Download PDFInfo
- Publication number
- US1904176A US1904176A US646976A US64697632A US1904176A US 1904176 A US1904176 A US 1904176A US 646976 A US646976 A US 646976A US 64697632 A US64697632 A US 64697632A US 1904176 A US1904176 A US 1904176A
- Authority
- US
- United States
- Prior art keywords
- alloy
- cadmium
- nickel
- metal
- 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
- 229910000990 Ni alloy Inorganic materials 0.000 title description 5
- OJIJEKBXJYRIBZ-UHFFFAOYSA-N cadmium nickel Chemical compound [Ni].[Cd] OJIJEKBXJYRIBZ-UHFFFAOYSA-N 0.000 title description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 34
- 229910045601 alloy Inorganic materials 0.000 description 18
- 239000000956 alloy Substances 0.000 description 18
- 229910052759 nickel Inorganic materials 0.000 description 16
- 229910052793 cadmium Inorganic materials 0.000 description 9
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 9
- 229910000897 Babbitt (metal) Inorganic materials 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 8
- 239000002184 metal Substances 0.000 description 8
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 7
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 7
- 229910052749 magnesium Inorganic materials 0.000 description 7
- 239000011777 magnesium Substances 0.000 description 7
- 229910052725 zinc Inorganic materials 0.000 description 7
- 239000011701 zinc Substances 0.000 description 7
- 230000008018 melting Effects 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 4
- 239000000470 constituent Substances 0.000 description 4
- 229910001092 metal group alloy Inorganic materials 0.000 description 4
- 229910052787 antimony Inorganic materials 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 229910000925 Cd alloy Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 238000007792 addition Methods 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- -1 popper Chemical compound 0.000 description 2
- JIAARYAFYJHUJI-UHFFFAOYSA-L zinc dichloride Chemical compound [Cl-].[Cl-].[Zn+2] JIAARYAFYJHUJI-UHFFFAOYSA-L 0.000 description 2
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 description 1
- 239000001996 bearing alloy Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000000979 retarding effect Effects 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 238000006467 substitution reaction Methods 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
- C22C20/00—Alloys based on cadmium
Definitions
- This invention relatesto metal alloys and more particularly to alloys of cadmium and nickel which may contain small amounts of another metal or other metals, such as alumi:
- the invention relates particularly to an alloy which may successfully be utilized as bearing metal at relatively high temperatures, that is, ,temperatures considerably in excess of those permissible when the conventional tin babbitts are employed.
- bearing metal alloys are composed of two distinct phases of widely vary ing physical properties.
- One of these phases is relatively soft, ductile, malleable; deforms with comparative ease, and is capable of creeping.
- the other phase is harder than the soft phase, but at the same time, 'is softer than the softest constituent of the shaft or similar structure which is supported or surrounded by the bearing metal.
- the soft phase accommodates the individual characteristic of the shaft and, as this phase wears away, the hard phase becomes exposed, and, in addition to carrying the load, may make the actual metal to metal contact between shaft and the bearing in the momentary absence of lubricant.
- the alloy may be introduced into a suitable kettle and heated to a temperature of 400 to 450 C. under a suitable flux, which prevents oxidation and the production of undesirable dross and compounds during the formation of the alloy.
- a low melting chloride slag such as zinc chloride
- Pure, thin, sheet nickel may then be introduced and the molten bath agitated until the nickel is incorporated therein.
- Small quantities of other metals such as aluminum,- antimony, copper, magnesium, zinc or the like, may then be added in amounts varying from traces up ,to 2 or 3%, depending on the particular metal added and the effect desired by its presence, such as the lessening of oxidation during casting, resistance to corrosion, increased strength and the like.
- the alloy may be cast i n'suitable molds to be used as desired.
- the alloy When employed as hearing metal the alloy exhibits many desirable features and'characteristics. In the first place, the alloy may be successfully used at temperatures approaching 318 C. This is very important when it is remembered that ordinary tin babbitt has a maximum working temperature of approximately 200 C. due to the low melting point of its soft constituent.
- the cadmiumnickel alloy possesses approximately 50% greater tensile strength. Elongation of the alloy exceeds babbitt by approximately 35%; the yield'point in compression is nearly 40% greater; reduction of area in tension is approximately double and compression strength is about one-fourth greater.
- the creep value of the cadmium-nickel alloy is higher than the creep value of babbitts, it is appreciably lower than the creep values of bearing bronzes. In other words, the alloy of our invention will creep under a lower load than will the bronzes. This is of especial importance during the period when a bearing is running in and setting a shaft.
- the coeflicient of friction of an alloy of 1 to 1.5% nickel and the balance cadmium is about equal to that of babbitt.
- the properties of the cadmium-nickel alloy may be modified by the addition of small amounts of other metals.
- the tensile-strength is nearly double that of tin babbitt, while, at the same time, elongation and reduction of area in tension compares favorably with babbitts.
- small quantities of magnesium aid in retarding oxidation of the alloys. Similar beneficial results are obtained with small additions of aluminum, antimony and/or zinc.
- the nickel content may vary from 0.25% to 7% as specified, we find that, for most purposes, a range in the nickel content of from 0.6% to 4% gives the better results. In other words, a minimum of 0.25% nickel is necessary, while, if more than 7% nickel is used, the characteristics which make the alloy desirable for use as bearing metal are modified or disappear.
- a bearing metal alloy comprising 0.25% to 7% nickel, magnesium and zinc in appreciable quantities not exceeding a total of 3% and the balance cadmium.
- a metal alloy comprising 0.25% to 7% nickel, magnesium a total of 3% and the balance cadmium.
- a bearing metal alloy comprising 0.25% to 7% nickel, magnesium in amounts not exceeding a total of 3% and the balance cadmium.
- a metal alloy comprising 0.25% to 7% nickel, zinc in amounts not exceeding a total of 3% and the balance cadmium.
- a bearing metal alloy comprising 0.25% to 7% nickel, zinc in amounts not exceeding a total of 3% and the balance cadmium.
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 Apr. 18, 1933 UNITED STATES PATENT OFFICE CARL Es SWARTZ, OF PARK, ALBERT J. PHILLIPS, OF METU'GHEN, NEW JERSEY, ASSIGNORS TO AMERICAN SMELTINO- AND REFINING- COMPANY, OF NEW YORK, N. Y., A CORPORATION O]! NEW JERSEY CADMIUM-NICKEL ALLOY No Drawing.
This invention relatesto metal alloys and more particularly to alloys of cadmium and nickel which may contain small amounts of another metal or other metals, such as alumi:
num, antimony, popper, magnesium, zinc or the like. 4
The invention relates particularly to an alloy which may successfully be utilized as bearing metal at relatively high temperatures, that is, ,temperatures considerably in excess of those permissible when the conventional tin babbitts are employed.
Invgeneral, bearing metal alloys are composed of two distinct phases of widely vary ing physical properties. One of these phases is relatively soft, ductile, malleable; deforms with comparative ease, and is capable of creeping. The other phase is harder than the soft phase, but at the same time, 'is softer than the softest constituent of the shaft or similar structure which is supported or surrounded by the bearing metal. In use, the soft phase accommodates the individual characteristic of the shaft and, as this phase wears away, the hard phase becomes exposed, and, in addition to carrying the load, may make the actual metal to metal contact between shaft and the bearing in the momentary absence of lubricant.
In addition, it is fundamental that the,
range of operating or working temperature of any bearing is limited by the melting point of the bearing alloy or'the melting point of the lowest melting constituent present in appreciable amounts in the alloy. Be-
cause of this fact further advance in manymetals is admirably suited for use as bearing metal or the like.
In compounding the alloy, cadmium may Application filed December 13, 1982. Serial 1V0. 646,976.
be introduced into a suitable kettle and heated to a temperature of 400 to 450 C. under a suitable flux, which prevents oxidation and the production of undesirable dross and compounds during the formation of the alloy. For this purpose we find a low melting chloride slag, such as zinc chloride, gives excellent results. Pure, thin, sheet nickel may then be introduced and the molten bath agitated until the nickel is incorporated therein. Small quantities of other metals, such as aluminum,- antimony, copper, magnesium, zinc or the like, may then be added in amounts varying from traces up ,to 2 or 3%, depending on the particular metal added and the effect desired by its presence, such as the lessening of oxidation during casting, resistance to corrosion, increased strength and the like. When the nickel or nickel and accompanying constituents, if any, are thoroughly incorporated in and alloyed with the molten cadmium, the alloy may be cast i n'suitable molds to be used as desired.
When employed as hearing metal the alloy exhibits many desirable features and'characteristics. In the first place, the alloy may be successfully used at temperatures approaching 318 C. This is very important when it is remembered that ordinary tin babbitt has a maximum working temperature of approximately 200 C. due to the low melting point of its soft constituent.
As compared to tin babbitt, the cadmiumnickel alloy possesses approximately 50% greater tensile strength. Elongation of the alloy exceeds babbitt by approximately 35%; the yield'point in compression is nearly 40% greater; reduction of area in tension is approximately double and compression strength is about one-fourth greater. Again, the
Rockwell test shows greater hardness values for the new alloy.
While the creep value of the cadmium-nickel alloy is higher than the creep value of babbitts, it is appreciably lower than the creep values of bearing bronzes. In other words, the alloy of our invention will creep under a lower load than will the bronzes. This is of especial importance during the period when a bearing is running in and setting a shaft.
The coeflicient of friction of an alloy of 1 to 1.5% nickel and the balance cadmium is about equal to that of babbitt.
As previously mentioned, the properties of the cadmium-nickel alloy may be modified by the addition of small amounts of other metals. For example, by adding, say, 0.5% copper to a cadmium alloy containing 1.5% nickel, the tensile-strength is nearly double that of tin babbitt, while, at the same time, elongation and reduction of area in tension compares favorably with babbitts. Again, small quantities of magnesium aid in retarding oxidation of the alloys. Similar beneficial results are obtained with small additions of aluminum, antimony and/or zinc.
Although the nickel content may vary from 0.25% to 7% as specified, we find that, for most purposes, a range in the nickel content of from 0.6% to 4% gives the better results. In other words, a minimum of 0.25% nickel is necessary, while, if more than 7% nickel is used, the characteristics which make the alloy desirable for use as bearing metal are modified or disappear.
The present application is a continuationin-part of our copending application, Serial No. 620,305, filed June 30, 1932.
While certain novel features of the invention have been disclosed and are pointed out in the annexed claims, it will be understood that various omissions, substitutions and changes may be effected by those skilled in the art without departing from the spirit of the invention.
What is claimed is:
1. A metal alloy containing from 0.25%
to 7% nickel, magnesium and zinc in appreciable quantities not exceeding a total of 3% and the balance cadmium. 2. A bearing metal alloy comprising 0.25% to 7% nickel, magnesium and zinc in appreciable quantities not exceeding a total of 3% and the balance cadmium.
3. A metal alloy comprising 0.25% to 7% nickel, magnesium a total of 3% and the balance cadmium.
4. A bearing metal alloy comprising 0.25% to 7% nickel, magnesium in amounts not exceeding a total of 3% and the balance cadmium.
5. A metal alloy comprising 0.25% to 7% nickel, zinc in amounts not exceeding a total of 3% and the balance cadmium.
6. A bearing metal alloy comprising 0.25% to 7% nickel, zinc in amounts not exceeding a total of 3% and the balance cadmium.
In testimony whereof we have hereunto set our hands.
CARL E. SWARTZ. ALBERT J. PHILLIPS.
in amounts not exceeding
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US646976A US1904176A (en) | 1932-12-13 | 1932-12-13 | Cadmium-nickel alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US646976A US1904176A (en) | 1932-12-13 | 1932-12-13 | Cadmium-nickel alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1904176A true US1904176A (en) | 1933-04-18 |
Family
ID=24595211
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US646976A Expired - Lifetime US1904176A (en) | 1932-12-13 | 1932-12-13 | Cadmium-nickel alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1904176A (en) |
-
1932
- 1932-12-13 US US646976A patent/US1904176A/en not_active Expired - Lifetime
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