US2156348A - Copper-zinc alloys - Google Patents
Copper-zinc alloys Download PDFInfo
- Publication number
- US2156348A US2156348A US29102A US2910235A US2156348A US 2156348 A US2156348 A US 2156348A US 29102 A US29102 A US 29102A US 2910235 A US2910235 A US 2910235A US 2156348 A US2156348 A US 2156348A
- Authority
- US
- United States
- Prior art keywords
- copper
- alloys
- content
- cobalt
- manganese
- 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
-
- E—FIXED CONSTRUCTIONS
- E02—HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
- E02F—DREDGING; SOIL-SHIFTING
- E02F3/00—Dredgers; Soil-shifting machines
- E02F3/04—Dredgers; Soil-shifting machines mechanically-driven
- E02F3/76—Graders, bulldozers, or the like with scraper plates or ploughshare-like elements; Levelling scarifying devices
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C18/00—Alloys based on zinc
- C22C18/02—Alloys based on zinc with copper as the next major constituent
Definitions
- gamma-brass that is to say copper zinc alloys'with a copper 'content of about 31-40%,1.
- alloys which are characterised by a low copper content are more resistant to corrosion than the brass alloys of the alpha and alpha and beta region with for instance 68-72% and more of copper, i. e. ahigher'copper content.
- the technical employment of gamma-alloys poor in copper is however impossible, since these alloys are extremely hard and brittle and are consequently not machinable.
- the present invention is based on the discovery that such copper-zinc alloys containing cobalt,
- nickel or the like which contain copper in such an amount that they have a homogeneous mixed crystal or solid solution structure-that is to say in a binary system copper-zinc alloyswith approximately 31-40% copper--, can be substantially improved in their properties by the addition of other metals, i. e. metals which are soluble in the solid solution of the alloy and are added or alloyed in an amount that is not greater than corresponds to their solubility in the solid solution. It has been found that such alloys can be made capable of being moulded in the cold state, i. e. rolled, pressed and drawn in the cold state by the addition of such metals in amounts which are soluble in the solid solutions so that the solid solution formation is maintained and the occurrence of a heterogeneous structure is avoided.
- Such metals are for instance aluminium, tungsten, tin, chromium, selenium, tellurium, titanl-- um, silver, silicon, iron, manganese, lead, molybdenum, zirconium etc. individually or two or more such metals combined as desired, and of thesemetals, the best effect is obtained 'by those which cause-an increase in fineness of the grain, that is to say more especially manganese, iron, lead,
- the region of the solid solution can also be somewhat extended with respect to that of the binary alloy, and alloyswith asomewhat higher copper content for instance with 45% copper content, which come in the beta and gamma region in the binary alloy, can be made suitable for purposes for which they would otherwise be impossible owing to their copper content, such as for instance for cold rolling or for a drawing process.
- alloys with a copper content of at least 35% are suitable.
- the alloy can be I improved in colour, more especially made whiter, and also favourably influenced as regards other properties, more especially made tougher, thus improving the capacityfor being machined.
- Suitable is an alloy which beside manganese, contains iron up to the limit-of solubility. which, depending on the composition of the alloy', may be 1 to 1.5%.
- the cobalt or nickel content or content of cobalt and nickel in such alloys according to the invention may be between about 3-12%.
- Suitable alloys according to the invention with manganese as added metal have for instance the following composition, it being clearly specified manganese content is smaller in the alloys of relatively high copper content than in the alloys of relatively low copper content.
Description
' be rolled hot.
Patented May 2, 1939 PATENT OFFICE COPPER-ZINC ALLOYS Wolf Johannes Miiller and Moritz Niessner, Vienna, Austria, assignors to Oesterreichische Dynamit Nobel Aktiengesellschaft, Vienna, Austria, a .firm of Austria No Drawing. Application June 29, 1935, Serial No. 29,102. In Austria July 21, 1934 3 Claims.
It is known that gamma-brass, that is to say copper zinc alloys'with a copper 'content of about 31-40%,1. e. alloys which are characterised by a low copper content, are more resistant to corrosion than the brass alloys of the alpha and alpha and beta region with for instance 68-72% and more of copper, i. e. ahigher'copper content. The technical employment of gamma-alloys poor in copper is however impossible, since these alloys are extremely hard and brittle and are consequently not machinable.
From such alloys as is described in our prior Patent Nos. 2,006,598 and 2,006,599, it has been disclosed that it is possible, by the addition of a few percent of a metal soluble in gamma-brass or alloyable therewith, such as nickel or, with more advantage cobalt, preferably by a simultaneous addition of nickel and cobalt, to obtain alloys, which possess the good resistance to corrosion of gamma-alloys poor in copper, but are also capable of being worked up, that is to say can be treated with machine tools and can also Such alloys with an addition of approximately 340% of cobalt, nickel or the like individually or in mixture, that is to say for instance pure copper-zinc alloys with a minimum content of nickel of approximately 7-8% or of cobalt of approximately 5-6% have extremely good technical properties, and when cobalt and nickel are used simultaneously it is possible with a much smaller cobalt content to obtain the same effects as with the use of cobalt alone. Consequently alloys that are deficient in copper, even those most deficient, can be made utilisable for industrial purposes or as constructional material for the production of articles, if the copper-zinc alloys are alloyed with cobalt, nickel or the like individually or in mixture.
The present invention is based on the discovery that such copper-zinc alloys containing cobalt,
nickel or the like, which contain copper in such an amount that they have a homogeneous mixed crystal or solid solution structure-that is to say in a binary system copper-zinc alloyswith approximately 31-40% copper--, can be substantially improved in their properties by the addition of other metals, i. e. metals which are soluble in the solid solution of the alloy and are added or alloyed in an amount that is not greater than corresponds to their solubility in the solid solution. It has been found that such alloys can be made capable of being moulded in the cold state, i. e. rolled, pressed and drawn in the cold state by the addition of such metals in amounts which are soluble in the solid solutions so that the solid solution formation is maintained and the occurrence of a heterogeneous structure is avoided. Such metals are for instance aluminium, tungsten, tin, chromium, selenium, tellurium, titanl-- um, silver, silicon, iron, manganese, lead, molybdenum, zirconium etc. individually or two or more such metals combined as desired, and of thesemetals, the best effect is obtained 'by those which cause-an increase in fineness of the grain, that is to say more especially manganese, iron, lead,
silver. Phosphorus also produces this effect. By
such additions the region of the solid solution can also be somewhat extended with respect to that of the binary alloy, and alloyswith asomewhat higher copper content for instance with 45% copper content, which come in the beta and gamma region in the binary alloy, can be made suitable for purposes for which they would otherwise be impossible owing to their copper content, such as for instance for cold rolling or for a drawing process.
In particular suitable are alloys with a copper content of at least 35%; such alloys, as compared with alloys with less copper content, have the advantage of better workability.
By addition of such metals the alloy can be I improved in colour, more especially made whiter, and also favourably influenced as regards other properties, more especially made tougher, thus improving the capacityfor being machined.
It is easily possible by empiric means to determine for each metal the amount which produces the most favourable effects.
It is more especially advisable to use the metals of the iron group,'more particularly manganese. 46
- be assumed as more than 4% manganese.
which as compared with other metals, for instance as compared with aluminium, has the efiect that with an increasing content, i. e. up to about 10%, there is an approximately proportional improvement in the capacity of working up cold, whereas for instance aluminium in amounts of about 0.3% has an extremely favourable action, but in amounts of more than 1. shows a diminished efiect.
The more deficient the alloy is in copper, the greater addition of manganese is necessary, and the lower limit for alloys deficient in copper must The higher the content of manganese, the better is the capacity for being worked up cold, and one can go up to an addition of about 15% manganese. Suitable is an alloy which beside manganese, contains iron up to the limit-of solubility. which, depending on the composition of the alloy', may be 1 to 1.5%.
The addition of manganese has also the effect however that the addition of cobalt and nickel or the like can be reduced.
It is advisable to add very small amounts of phosphorus to such alloys, whereby a very considerable increase in the fineness of the grain oi the alloys can be obtained.
The cobalt or nickel content or content of cobalt and nickel in such alloys according to the invention may be between about 3-12%.
Examples Suitable alloys according to the invention with manganese as added metal have for instance the following composition, it being clearly specified manganese content is smaller in the alloys of relatively high copper content than in the alloys of relatively low copper content.
however that the invention is naturally not limited to these examples:
Percent by weight What we claim is: 1. A corrosion resistant copper-zinc alloy,
which is workable in the cold state, containing copper in an amount of 30 to 45%, at least one metal of the group cobalt and nickel in an amount of 3 to 12% and in addition thereto manganese in an amount 4 to 15%, the zinc, constituting substantially the the remainder.
2. An alloy according to claim 1 wherein the 3. An alloy according to claim 1 -containing less than copper.-
WOLF JOHANNES Mt'irLLER. 35
MORITZ N'IESSNER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US148506A US2144993A (en) | 1935-06-29 | 1937-06-16 | Copper-zinc alloys |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT2156348X | 1934-07-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2156348A true US2156348A (en) | 1939-05-02 |
Family
ID=3689991
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US29102A Expired - Lifetime US2156348A (en) | 1934-07-21 | 1935-06-29 | Copper-zinc alloys |
Country Status (1)
Country | Link |
---|---|
US (1) | US2156348A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2752242A (en) * | 1950-08-08 | 1956-06-26 | Gen Motors Corp | Copper-nickel-titanium alloy and process for making same |
-
1935
- 1935-06-29 US US29102A patent/US2156348A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2752242A (en) * | 1950-08-08 | 1956-06-26 | Gen Motors Corp | Copper-nickel-titanium alloy and process for making same |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1973428A (en) | Cemented hard carbide material | |
US2156348A (en) | Copper-zinc alloys | |
US1850819A (en) | Alloy | |
US2236975A (en) | Copper-zinc alloys | |
US2273806A (en) | Platinum alloy | |
US2030343A (en) | Alloys | |
US2076577A (en) | Free cutting alloys | |
US2076575A (en) | Free cutting alloys | |
US1602995A (en) | Nonferrous alloy | |
US2076571A (en) | Free cutting alloys | |
US2076569A (en) | Free cutting alloys | |
US2259078A (en) | Copper-zinc alloy | |
US2026541A (en) | Free cutting alloys | |
US2206109A (en) | Copper-zinc alloys | |
US1986825A (en) | Free cutting alloy | |
US2144993A (en) | Copper-zinc alloys | |
US2256788A (en) | Copper-zinc alloy | |
US2270716A (en) | Copper alloy | |
US2047873A (en) | Free cutting alloys | |
US2046702A (en) | Copper alloy | |
US2858243A (en) | Process for production of improved free machining steels | |
US2147637A (en) | Alloy | |
US2026540A (en) | Free cutting alloys | |
US2288660A (en) | Electric resistance alloy | |
US2026576A (en) | Free cutting alloys |