US2166794A - Copper-cobalt-beryllium alloys - Google Patents
Copper-cobalt-beryllium alloys Download PDFInfo
- Publication number
- US2166794A US2166794A US112999A US11299936A US2166794A US 2166794 A US2166794 A US 2166794A US 112999 A US112999 A US 112999A US 11299936 A US11299936 A US 11299936A US 2166794 A US2166794 A US 2166794A
- Authority
- US
- United States
- Prior art keywords
- cobalt
- copper
- beryllium
- alloy
- alloys
- 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
- 229910000952 Be alloy Inorganic materials 0.000 title description 2
- 229910045601 alloy Inorganic materials 0.000 description 14
- 239000000956 alloy Substances 0.000 description 14
- 229910052790 beryllium Inorganic materials 0.000 description 10
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 9
- 229910017052 cobalt Inorganic materials 0.000 description 6
- 239000010941 cobalt Substances 0.000 description 6
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 6
- 238000001556 precipitation Methods 0.000 description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 238000005482 strain hardening Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- WJUQEHIOSQMNMB-UHFFFAOYSA-N [Be].[Co].[Cu] Chemical compound [Be].[Co].[Cu] WJUQEHIOSQMNMB-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
- 238000000137 annealing Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/06—Alloys based on copper with nickel or cobalt as the next major constituent
Definitions
- the present invention relates to precipitation hardened alloys consisting of copper, cobalt and beryllium and particularly to alloys of this composition which are employed as springs.
- Dahl Patent 1,847,929 and Horstkotte Patent 1,957,214 both disclose precipitation hardened copper-cobalt-beryliium alloys containing not more than 1% beryllium and preferably about .4% beryllium. I have found however that precipitation hardened alloys of the above composition develop a network of line cracks when subjected to bending or cold working. These cracks are due to oxygen which, during the heat treatment, penetrates the alloy along the grain boundaries yielding a weak brittle film aroundthe grains. This oxidation occurs at all temperatures above 500 C. and even in furnaces employing line or commercial hydrogen.
- an atmosphere which is oxygen free for example a pure dry hydrogen atmosphere such as employed in producing bright annealed surfaces on stainless steel, it is possible to avoid embrittlement of the alloy and subsequent cracking during cold working.-
- an atmosphere entirely free from oxygen is expensive and not always feasible.
- the alloy is precipitation hardened in the manner disclosed in the Horstkotte patent. For example, it is heated to about 900 C., quenched in water, and thereafter heated at about 500 to 600 C. for about one hour and then allowed to cool.
- the alloy thus produced may I be forged and rolled into thin sheets and formed 0 into springs such as Sylphon bellows and like devices which are'subject to cold working or use at elevated temperatures. Alloys of this composition are free from intergranular oxidation when heated in oxidizing atmospheres.
- a preferred composition contains 2.6% cobalt, 1.5% beryllium and the remainder copper.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Adornments (AREA)
- Mechanical Operated Clutches (AREA)
Description
Patented July 18, 1939 UNITED STATES COPPER-COBALT-BERYLLIUM ALLOYS Gerald R. Brophy, Schenectady, N. Y., assignor to General Electric Company, a corporation of New York No Drawing. Application November 2'7, 1936, Serial No. 112,999
1 Claim.
The present invention relates to precipitation hardened alloys consisting of copper, cobalt and beryllium and particularly to alloys of this composition which are employed as springs.
Dahl Patent 1,847,929 and Horstkotte Patent 1,957,214 both disclose precipitation hardened copper-cobalt-beryliium alloys containing not more than 1% beryllium and preferably about .4% beryllium. I have found however that precipitation hardened alloys of the above composition develop a network of line cracks when subjected to bending or cold working. These cracks are due to oxygen which, during the heat treatment, penetrates the alloy along the grain boundaries yielding a weak brittle film aroundthe grains. This oxidation occurs at all temperatures above 500 C. and even in furnaces employing line or commercial hydrogen.
By employing, during the heat treatment, an atmosphere which is oxygen free, for example a pure dry hydrogen atmosphere such as employed in producing bright annealed surfaces on stainless steel, it is possible to avoid embrittlement of the alloy and subsequent cracking during cold working.- However, the use of an atmosphere entirely free from oxygen is expensive and not always feasible.
It is an object of the .present invention to provide a precipitation hardened copper-cobaltberyllium alloy which is free from cracks or embrittlement and which may be heat treated in any atmosphere commonly employed in annealing furnaces.
In carrying out my invention I preferably employ an alloy which contains not less than 1.5%
beryllium and about 2.6% cobalt with the remainder copper. About 0.4% of the beryllium combines with the cobalt leaving an excess of 1.1% beryllium. The alloy is precipitation hardened in the manner disclosed in the Horstkotte patent. For example, it is heated to about 900 C., quenched in water, and thereafter heated at about 500 to 600 C. for about one hour and then allowed to cool. The alloy thus produced may I be forged and rolled into thin sheets and formed 0 into springs such as Sylphon bellows and like devices which are'subject to cold working or use at elevated temperatures. Alloys of this composition are free from intergranular oxidation when heated in oxidizing atmospheres.
While I prefer to employ a minimum of 1.5% beryllium in the alloy, higher percentages may be employed if desired, also a portion of the beryllium in excess of that combined with the cobalt may be replaced by any protective metal such as aluminum, titanium, zirconium, silicon and calcium which protects the alloy against intergranular oxidation. A preferred composition contains 2.6% cobalt, 1.5% beryllium and the remainder copper. During heat treatment, 25 I employ air or hydrogen as the furnace atmosphere although nitrogen, carbon monoxide or any atmosphere commonly employed in the heat treatment of metals may be employed if desired.
What I claim as new and desire to secure by Letters Patent of the United States, is:
A precipitation hardened alloy containing 1.5%
- beryllium, 2.6% cobalt with the remainder copper.
GERALD a. BROPHY.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US112999A US2166794A (en) | 1936-11-27 | 1936-11-27 | Copper-cobalt-beryllium alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US112999A US2166794A (en) | 1936-11-27 | 1936-11-27 | Copper-cobalt-beryllium alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2166794A true US2166794A (en) | 1939-07-18 |
Family
ID=22347015
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US112999A Expired - Lifetime US2166794A (en) | 1936-11-27 | 1936-11-27 | Copper-cobalt-beryllium alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2166794A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2797300A (en) * | 1955-03-03 | 1957-06-25 | Revere Copper & Brass Inc | Welding |
| US2867714A (en) * | 1955-04-21 | 1959-01-06 | Philips Corp | Support for stud-welding gun |
| US3216870A (en) * | 1961-03-10 | 1965-11-09 | Ilikon Corp | Stabilized precipitation hardening alloys and method of making |
| US3376171A (en) * | 1963-04-11 | 1968-04-02 | Cirex Nv | Copper alloy |
-
1936
- 1936-11-27 US US112999A patent/US2166794A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2797300A (en) * | 1955-03-03 | 1957-06-25 | Revere Copper & Brass Inc | Welding |
| US2867714A (en) * | 1955-04-21 | 1959-01-06 | Philips Corp | Support for stud-welding gun |
| US3216870A (en) * | 1961-03-10 | 1965-11-09 | Ilikon Corp | Stabilized precipitation hardening alloys and method of making |
| US3376171A (en) * | 1963-04-11 | 1968-04-02 | Cirex Nv | Copper alloy |
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