US1911023A - Method for preventing embrittlement of copper - Google Patents
Method for preventing embrittlement of copper Download PDFInfo
- Publication number
- US1911023A US1911023A US449020A US44902030A US1911023A US 1911023 A US1911023 A US 1911023A US 449020 A US449020 A US 449020A US 44902030 A US44902030 A US 44902030A US 1911023 A US1911023 A US 1911023A
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- copper
- temperature
- wire
- metal
- annealing
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/08—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon
Definitions
- the present invention relates to a method for treating copper to prevent cmbrittlement thereof when heated in a reducing atmosphere.
- illuminating gas to heat the copper to the desired soldering or welding temperature. This temperature is usually well below 850 C.
- a considerable l0 amount of reducing gas, for example carbon monoxide is usually present in illuminating gas. Since oxygen in the form of copper oxide is usually present between the grains of untreated copper wire, the carbon monoxide gas reduces the oxide leaving a spongy copper between the copper grains which thereby causes embrittlement of the wire. Substantially the same action occurs in the presence of hydrogen gas which combines with the oxygen in the copper forming steam which blows the copper grains apart and renders the resultant product brittle.
- copper to be treated is heated to a temperature between 600 and 800 C. in a hydrogen atmosphere for a period of time necessary to remove substantially all the oxygen in the. copper.
- the length of time that the copper should be heated depend-s uponthe temperature employed and also on the dimensions of the metal article being treated. If the treatment is applied to copper wire the proper length of the heating period may be determined easily by bending the wire. When the oxygen is substantially entirely removed therefrom. the. wire is very brittle and W111 break easilv when bent even slightly.
- the oxygen After the oxygen has been substantially entirely removed from the copper, it is heated in a hydrogen or other non-oxidizing en: vironment to a temperature between 850 and 1000 C. At 850 C. the copper tends to re- Application filed May 1, 1930. Serial No. 449,020.
- the copper is heated in the 8501000 C. zone for an appreciable time, for example two or three hours.
- the copper wire is then cooled to room temperature and cold worked by drawing through a suitable die.
- the annealing and subsequent cold working is repeated several times, the wire being heated each time to a temperature between 850 and 1000 C. then cooled and cold Worked by drawing through a die.
- the annealing and cold working operations have been repeated several times, it will befound that the normal physical and electrical characteristics of the copper are restored. Thereafter heating the copper wire in a reducing atmosphere to any temperature below the melting point of the copper will not cause embrittlement thereof.
- an ordinary untreated copper wire of about 102 mils diameter has a conductivity of about 100.7.
- the wire When annealed for about three hours at a temperature of about 900 and 950 C. the wire has a diameter of about 104.75 mils and a conductivity of about 93. lVhen cooled to room temperature and then drawn through a die and reduced about in diameter the wire has a conductivity of about 95.6.
- the wire When annealed again for two hours at 900 C. the
- conductivity is increased to about 96.2 and when drawn through a die the conductivity is further increased to about 07.1.
- the conductivity of the wire is about 101.3.
- the method of treating copper which comprises annealing the metal at a temperature above 850 C. in a non-oxidizing environment and subsequently cold working it.
- the method of treating copper which comprises annealing it above 850 C. in a reducing atmosphere, cooling to room temperature, cold working the metal and again annealing the metal and subsequently cold working it.
- the method of treating copper which comprises heating the metal in a reducing atmosphere at an elevated temperature lower than 850 C. to thereby substantially remove all the oxygen therefrom, annealing the metal in a non-oxidizing environment and at a temperature between 850 C. and 1000 0., coollng substantially to room temperature, cold working the metal, re-annealing the metal in a non-oxidizing environment at a temperature between 850 C. and 1000 C. and again cold working the metal.
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- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Metal Extraction Processes (AREA)
Description
Patented May 23, 1933 UNITED STATES PATENT OFFICE FLOYD G. KELLEY, OF SCHENECTADY, NEW YORK, ASSIGNOR TO GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK METHOD FOR PREVENTING EMBRITTLEMENT OF COPPER No Drawing.
The present invention relates to a method for treating copper to prevent cmbrittlement thereof when heated in a reducing atmosphere. Heretofore, when soldering or welding ordinary copper wire, it has been customary to employ illuminating gas to heat the copper to the desired soldering or welding temperature. This temperature is usually well below 850 C. A considerable l0 amount of reducing gas, for example carbon monoxide, is usually present in illuminating gas. Since oxygen in the form of copper oxide is usually present between the grains of untreated copper wire, the carbon monoxide gas reduces the oxide leaving a spongy copper between the copper grains which thereby causes embrittlement of the wire. Substantially the same action occurs in the presence of hydrogen gas which combines with the oxygen in the copper forming steam which blows the copper grains apart and renders the resultant product brittle.
It is an object of the present invention to provide an improved method for treating copper to prevent embrittlement thereof when the copper isheated in a reducing atmosphere. It is a further ObJGCt of the invention to provide means for restoring the physical and electrical properties of brittle copper to a normal condition.
In carrying out my invention, copper to be treated is heated to a temperature between 600 and 800 C. in a hydrogen atmosphere for a period of time necessary to remove substantially all the oxygen in the. copper. The length of time that the copper should be heated depend-s uponthe temperature employed and also on the dimensions of the metal article being treated. If the treatment is applied to copper wire the proper length of the heating period may be determined easily by bending the wire. When the oxygen is substantially entirely removed therefrom. the. wire is very brittle and W111 break easilv when bent even slightly.
After the oxygen has been substantially entirely removed from the copper, it is heated in a hydrogen or other non-oxidizing en: vironment to a temperature between 850 and 1000 C. At 850 C. the copper tends to re- Application filed May 1, 1930. Serial No. 449,020.
cover a portion of its original ductility and this tendency increases as the temperature of the copper is raised to 1000 C. However, merely heating the copper does not restore its original, physical and electrical properties. In order to procure such a result, the copper is heated in the 8501000 C. zone for an appreciable time, for example two or three hours. The copper wire is then cooled to room temperature and cold worked by drawing through a suitable die. The annealing and subsequent cold working is repeated several times, the wire being heated each time to a temperature between 850 and 1000 C. then cooled and cold Worked by drawing through a die. When the annealing and cold working operations have been repeated several times, it will befound that the normal physical and electrical characteristics of the copper are restored. Thereafter heating the copper wire in a reducing atmosphere to any temperature below the melting point of the copper will not cause embrittlement thereof.
As an example, I have found that an ordinary untreated copper wire of about 102 mils diameter has a conductivity of about 100.7. When annealed for about three hours at a temperature of about 900 and 950 C. the wire has a diameter of about 104.75 mils and a conductivity of about 93. lVhen cooled to room temperature and then drawn through a die and reduced about in diameter the wire has a conductivity of about 95.6. When annealed again for two hours at 900 C. the
conductivity is increased to about 96.2 and when drawn through a die the conductivity is further increased to about 07.1. When the wire is reannealed and cold worked several times so that its diameter is reduced about 60% or to about mils diameter the conductivity of the wire is about 101.3.
What I claim as new and desire to secure by Letters Patent of the United States, is:
1. The method of treating copper which comprises annealing the metal at a temperature above 850 C. in a non-oxidizing environment and subsequently cold working it.
2. The method of treating copper which comprises annealing it above 850 C. in a reducing atmosphere, cooling to room temperature, cold working the metal and again annealing the metal and subsequently cold working it.
3. The method of treating copper which comprises heating the metal in a reducing atmosphere at an elevated temperature lower than 850 C. to thereby substantially remove all the oxygen therefrom, annealing the metal in a non-oxidizing environment and at a temperature between 850 C. and 1000 0., coollng substantially to room temperature, cold working the metal, re-annealing the metal in a non-oxidizing environment at a temperature between 850 C. and 1000 C. and again cold working the metal.
In Witness whereof, I have hereunto set my hand this 30th day of April, 1930.
FLOYD C. KELLEY.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US449020A US1911023A (en) | 1930-05-01 | 1930-05-01 | Method for preventing embrittlement of copper |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US449020A US1911023A (en) | 1930-05-01 | 1930-05-01 | Method for preventing embrittlement of copper |
Publications (1)
Publication Number | Publication Date |
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US1911023A true US1911023A (en) | 1933-05-23 |
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Application Number | Title | Priority Date | Filing Date |
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US449020A Expired - Lifetime US1911023A (en) | 1930-05-01 | 1930-05-01 | Method for preventing embrittlement of copper |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3121034A (en) * | 1962-03-13 | 1964-02-11 | Anderko Kurt | Zirconium alloy treatment process |
US3717745A (en) * | 1970-02-25 | 1973-02-20 | Outokumpu Oy | Continuous resistance annealing method for wires |
US4443274A (en) * | 1982-12-03 | 1984-04-17 | Olin Corporation | Process for forming a protective film on Cu-Sn alloys |
US5702543A (en) * | 1992-12-21 | 1997-12-30 | Palumbo; Gino | Thermomechanical processing of metallic materials |
-
1930
- 1930-05-01 US US449020A patent/US1911023A/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3121034A (en) * | 1962-03-13 | 1964-02-11 | Anderko Kurt | Zirconium alloy treatment process |
US3717745A (en) * | 1970-02-25 | 1973-02-20 | Outokumpu Oy | Continuous resistance annealing method for wires |
US4443274A (en) * | 1982-12-03 | 1984-04-17 | Olin Corporation | Process for forming a protective film on Cu-Sn alloys |
US5702543A (en) * | 1992-12-21 | 1997-12-30 | Palumbo; Gino | Thermomechanical processing of metallic materials |
US5817193A (en) * | 1992-12-21 | 1998-10-06 | Palumbo; Gino | Metal alloys having improved resistance to intergranular stress corrosion cracking |
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