US2296706A - Copper-zinc alloy - Google Patents
Copper-zinc alloy Download PDFInfo
- Publication number
- US2296706A US2296706A US408760A US40876041A US2296706A US 2296706 A US2296706 A US 2296706A US 408760 A US408760 A US 408760A US 40876041 A US40876041 A US 40876041A US 2296706 A US2296706 A US 2296706A
- Authority
- US
- United States
- Prior art keywords
- copper
- alloy
- range
- zinc alloy
- zinc
- 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
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
- C22C9/04—Alloys based on copper with zinc as the next major constituent
Description
Patented Sept. 22, 1942 COPPER-ZIN C ALLOY Michael George Corson, New York, N. Y., assignor to The Beryllium Corporation, Temple, Pa., a corporation of Delaware No Drawing.
3 Claims.
This invention relates to metallurgy and more particularly to copper-zinc alloys.
One of the objects of the present invention is to provide an age hardenable copper-zinc alloy.
Another object is to provide a copper-zinc alloy suitable for hot stamping and extrusion operations.
Other objects and advantages will be apparent as the invention is more fully hereinafter disclosed.
In accordance with these objects I have discovered that the hot working properties of copper-zinc alloys, containing from 30 to 35% zinc, balance copper, are materially improved by adding thereto from .20 to 1% Be and from .30 to 2.0% of one of the metals Ni and Co, and that the said Cu.Zn alloys containing Be and one of the metals Ni and Co in the proportions specified on precipitation hardening'by heat treatment within the range 220-380" C. will develop a tensile strength of from 90,000" to 125,000 pounds per square inch with an elongation of 37 to 15% and a hardness approximating 95-115 Rockwell B (Rockwell C 32 or Brinell 300).
Heretofore in the art aluminum and nickel additions to copper-zinc alloys have been proposed for the purpose of forming a precipitation hardening alloy. These alloys, however, after a homogenizing heat treatment at temperatures approximating 800 C. are hot worked with difficulty even at temperatures as high as 800-850" C. and are totally unsuitable for-hot stamping and extrusion operations at temperatures as low 7 the range .30 to 2.0% as to form nickel or cobalt beryllide compounds, I have found that such beryllide compounds may be dissolved substantially completely in the alpha phase of the Cu.Zn alloy on heat treatment at temperatures approximating 800 C. and where-so dissolved appear to improve the working properties of the alloy at temperatures within the range 650-800 C. to the extent that such alloys may be readily mechanically deformed by hot stamping and extrusion operations to which the Al-Ni-contalning brasses and other brasses are not well suited. Moreover, thealloys subsequently to such hot mechanical deformation may be precipitation hardened without prior heating to about 800 C. for prolonged time intervals to homogenize the structure as heretofore required.
Application August 29, 1941, Serial No. 408,760
On precipitation hardening I have'found that the alloys of the present invention develop materially higher tensile strength and hardness with lower elongation than the Cu.Zn alloy containing Al and Ni as heretofore I employed in the art. As an example, of the present'invention an alloy containing Zn Be 1%, Ni 50%, balance copper developed on precipitation hardening a hardness of 98-102 Rockwell B; a tensile strength of about 105,000 pounds per square inch and an elongation of about 20%.
In the Cu-Zn alloy of thepresent invention it is preferred to maintain the Be content below the solid solubility limit of Be in the alloy at atmospheric temperatures to avoid the precipitation of copper or zinc beryllide at temperatures within the range 400 to 800 C. The solid solubility of Be in the Cu.Zn alloy approximates 1%, however, I prefer to employ between .50 to .75% Be.
The Ni or C0 content in the alloy may vary widely within the range .50 to 2.0% without material effect upon the precipitation hardening properties of the alloy with any given Be content within the range .50, to .75%. The rate of precipitation hardening, however, normally increases with increase-in the Ni or C0 content increases with increase in Be content within the range .2 to 1.0% from a hardness approximating 95, Rockwell B to a hardness approximating 115 Rockwell B. The tensile strengthv increases with decrease in Be content within the range .20 to 1.0% from a tensile of about 125,000 pounds per square inch to a tensile of about 90,000
pounds per square inch.
From the above description of the present invention it is believed apparent that the same may to 35%, Be .50 to .75%, Ni .30 to 2.0%, bal-- ance Cu.
3. A precipitation hardenable Cu-Zn alloy, said alloy containing about 30% Zn, about 1% Be, about .50% Ni, balance copper.
MICHAEL GEORGE CORSONQ
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US408760A US2296706A (en) | 1941-08-29 | 1941-08-29 | Copper-zinc alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US408760A US2296706A (en) | 1941-08-29 | 1941-08-29 | Copper-zinc alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US2296706A true US2296706A (en) | 1942-09-22 |
Family
ID=23617646
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US408760A Expired - Lifetime US2296706A (en) | 1941-08-29 | 1941-08-29 | Copper-zinc alloy |
Country Status (1)
Country | Link |
---|---|
US (1) | US2296706A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3166410A (en) * | 1963-04-29 | 1965-01-19 | Beryllium Corp | Forging brass alloy containing small amounts of beryllium |
US4094671A (en) * | 1976-05-07 | 1978-06-13 | Osamu Hayashi | Gold color copper alloy for restorative dentistry |
US4139378A (en) * | 1973-11-21 | 1979-02-13 | The New Jersey Zinc Company | Powder-metallurgy of cobalt containing brass alloys |
-
1941
- 1941-08-29 US US408760A patent/US2296706A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3166410A (en) * | 1963-04-29 | 1965-01-19 | Beryllium Corp | Forging brass alloy containing small amounts of beryllium |
US4139378A (en) * | 1973-11-21 | 1979-02-13 | The New Jersey Zinc Company | Powder-metallurgy of cobalt containing brass alloys |
US4094671A (en) * | 1976-05-07 | 1978-06-13 | Osamu Hayashi | Gold color copper alloy for restorative dentistry |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2210670A (en) | Copper alloy | |
US4067750A (en) | Method of processing copper base alloys | |
US3827917A (en) | Aluminum electrical conductor and process for making the same | |
US3703367A (en) | Copper-zinc alloys | |
US2296706A (en) | Copper-zinc alloy | |
US2281691A (en) | Process for heat treating copper alloys | |
US2027750A (en) | Copper base alloy | |
US2126827A (en) | Copper-cobalt-zinc alloy | |
US3039868A (en) | Magnesium base alloys | |
US3816187A (en) | Processing copper base alloys | |
US3366476A (en) | Aluminum base alloy | |
US3684496A (en) | Solder having improved strength at high temperatures | |
US2879159A (en) | Copper and copper base alloys and methods of making the same | |
US2823995A (en) | Aluminum base alloy die casting | |
US6074499A (en) | Boron-copper-magnesium-tin alloy and method for making same | |
US2795501A (en) | Copper base alloys | |
US2258492A (en) | Electric contacting element | |
US2371531A (en) | Magnesium base alloy | |
US1974839A (en) | Alloy | |
US2586647A (en) | Aluminum alloy | |
US2243827A (en) | Zinc alloy | |
US2123330A (en) | Palladium alloy | |
US2026209A (en) | Copper alloy | |
US2126750A (en) | Alloy | |
US2130996A (en) | Copper-zmcontom-manganese allot |