US3039867A - Copper-base alloys - Google Patents
Copper-base alloys Download PDFInfo
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- US3039867A US3039867A US17311A US1731160A US3039867A US 3039867 A US3039867 A US 3039867A US 17311 A US17311 A US 17311A US 1731160 A US1731160 A US 1731160A US 3039867 A US3039867 A US 3039867A
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- 229910045601 alloy Inorganic materials 0.000 title claims description 64
- 239000000956 alloy Substances 0.000 title claims description 64
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 69
- 229910052742 iron Inorganic materials 0.000 claims description 34
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 claims description 22
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 26
- 229910052802 copper Inorganic materials 0.000 description 26
- 239000010949 copper Substances 0.000 description 26
- 238000001556 precipitation Methods 0.000 description 12
- 238000000137 annealing Methods 0.000 description 10
- 239000004020 conductor Substances 0.000 description 8
- 238000005482 strain hardening Methods 0.000 description 7
- 238000011282 treatment Methods 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 6
- 229910000881 Cu alloy Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000005096 rolling process Methods 0.000 description 4
- 238000005266 casting Methods 0.000 description 3
- 238000005275 alloying Methods 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- QQFKZUCZVUBDIK-UHFFFAOYSA-N [Fe].[Cd].[Cu] Chemical compound [Fe].[Cd].[Cu] QQFKZUCZVUBDIK-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011328 necessary treatment Methods 0.000 description 1
- 230000000135 prohibitive effect Effects 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
Images
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
Definitions
- a casting 1 /2 inches thick can be obtained of an alloy composed of 2.3% iron, 0.023% to 0.024% phosphorous and remainder copper, hot rolled to reduce the bar to 0.200 gauge with further cold rolling to obtain a thickness of 0.05 inch.
- the alloy was then annealed to effect a complete solution of the various elemental components at varying temperatures of 700, 800 and 900 C.
- the alloy is then cold rolled to further reduce the metal to 0.025 inch in thickness, and precipitation treated at 480 C. for various lengths of time.
- the phosphorous is not understood, however, it is believed that it, both, does alloy with the iron, and does act as a dioxidizer. Irrespective of the function of the phosphorous in the alloy, to obtain a conductor having desirable properties of combined high tensile strength and high electrical conductivity, it is essential that the phosphorous be present from a minute or residual amount to a maximum of 0.04%
- a copper-base alloy consisting essentially of 2.3% iron, 0.023% to 0.024% phosphorous and balance copper.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Conductive Materials (AREA)
Description
O O O 4 3 2 w 0 l O 8 3 \CSRQERS #QEEE N. wEm kituaqaou ,8 b58328 N w m 8 m 4 IN VEN TOR.
June 19, 1962 c. D. M LAIN COPPER-BASE. ALLOYS Filed March 24, 1960 FIGI ANNEAL/NG TIME HOURS FIG? 01 Ikbihkhm TIME HOURS F I G. 5
TENS/LE As nsco. ANNE/MING TIME HOURS CHARLES. DONALD M LAIN Lil My A T TOPNEYS United States Patent Ofiice 3,039,867 Patented .inne 19, 1962 3,039,867 C(BPPER-BASE ALLGYS Charles Donald McLain, Alton, 111., assignor to 03m Mathieson Chemical Corporation, East Alton, Iii, a corporation of Virginia Filed Mar. 24, 1960, Ser. No. 17,311 4 Claims. (Cl. 75-153) This invention relates to a copper-base alloy and more particularly to an alloy suitable for use for electrical conductors.
Although copper is an excellent conductor of electricity, it is deficient in strength for many applications. Heretofore, it has been proposed to increase the strength of copper by the addition of small amounts of various elements such as tin, iron, cadmium and the like, however, by so doing, electrical conductivity of copper is reduced by marked amounts. Since high conductivity combined with increased strength is desired for various applications, optimum combinations of increased strength with high conductivity have been the subject of extensive research.
Among the elements proposed to be added to copper, iron has been found to greatly increase tensile strength of the resultant allo however, rapidly lowering the conductivity of copper to as much as 40% with an iron con- .tent of 0.4%, and to a conductivity of 30% for an iron content of 0.7%, It has heretofore been assumed that the reduction of conductivity of copper is directly proportional to the iron content, and accordingly, that large amounts of iron, above 1.0%, should be avoided. However, in spite of the aforesaid disadvantages, the addition or" iron imparts to the alloy properties which are desirable if they could be obtained without any prohibitive loss in conductivity. An additional benefit of iron addition to copper is a widening of the temperature range in which the alloy may be treated at low temperatures. Since the presence of iron makes the alloy more stabie to variations in temperatures encountered in conventional heat treating furnaces, the iron addition makes it possible to obtain uniform hardness and properties in the alloys. In view of the above advantages, iron has heretofore been proposed to be incorporated with the copper by the addition of other alloying elements to form ternary or higher alloys in order to minimize the loss in conductivity.
Accordingly, it has been proposed to incorporate iron with copper as an iron-cadmium-copper alloy, a nickelzinccadmium-iron-copper alloy and in the form of a manganese-phosphorous-iron and copper alloy. However, the methods heretofore proposed for alloying iron, copper and other elements are extremely difficult to control and highly sensitive to minor variations in chemical analysis, with the alloy having fixed properties of conductivity and strength.
Accordingly, it is an object of this invention to provide an electric conductor composed of relatively inexpensive elements whose properties of conductivity and strength can be varied above a minimum combination of electric conductivity and physical strength.
Another object of this invention is to provide a novel and economical method for obtaining an improved copperbase alloy,
Still another object of this invention is to provide a novel copper-base alloy having a high electrical conductivity combined with a high tensile strength.
A further object of this invention is to provide a novel copper-base alloy having increased resistance to softening.
A still further object of this invention is to provide an improved electric conductor formed largely of copper which is more easily fabricated.
Other objects and advantages of the invention will become more apparent in the following description and drawings in which:
ZGURE 1 is a graph illustrating the relationship between electrical conductivity, tensile strength and elongation of the alloy which is one embodiment of this invention and subjected to varying solution annealing temperatures and precipitation treatments.
FIGURE 2 is a graph illustrating the relationship between electrical conductivity, tensile strength and elongation when the alloy which is another embodiment of this invention after subjecting to a series of operations, hereinafter described; and
FIGURE 3 is a graph illustrating the relationship between electrical conductivity, tensile strength and elongation when the alloy of this invention is subjected to an additional operation to those employed for FIGURE 2.
It has been discovered that the above objects may be accomplished in accordance with this invention by providing, as the metal for the conductor, an alloy composed of 2.0% to 3.0% iron, phosphorous to a maximum content of 0.04% with the balance copper. A preferred composition of the alloy in accordance to this invention is a composition consisting of 0.02% to 0.04% phosphorous, 2.1% to 2.6% iron and 97.3% to 97.8% copper as the balance. With the compositions of this invention, alloys can be obtained having a tensile strength greater than 50,000 psi. and a conductivity greater than 50% IACS (International Standard for Annealed Copper) an elongation greater than 5% and a resistance to grain growth at a temperature of about and above 1300 F. for a period of time up to eight seconds, With the preferred composition, an alloy was obtained having electrical conductivity of approximately 70% IACS with a tensile strength exceeding 50,000 p.s.i., and an elongation exceeding 5% minimum and was able to withstand rapid heating to 13 00 F. for a period of eight seconds Without recrystallizing to a grain size greater than 0.020 mm.
Although the phophorous may be present in the alloy from a maximum 0.04% to a minimum limit consisting of at least a trace, it is essential that the phosphorous be present, even though in minute amounts. Accordingly, in the composition described above and hereinafter, the phosphorous content ranges from a trace to 0.04%.
Further, with the phosphorous present within the aforedescribed limits, it has been found the iron must be present with the range of 2.0% to 3.0% if the prescribed minimum limits of electrical conductivity and strength are to be obtained. Variation in either the iron content or phosphorous content from the prescribed combined limits produces alloys in which the conductivity and/or the strength is unalterably below the prescribed minimums, that is, either the conductivity will fall below 50% and/ or the tensile strength will be below 50,000 psi.
In addition, the alloys obtained in accordance with this invention can be readily Worked to alter the proportion of tensile strength to electrical conductivity to provide a specific combination of properties, desired for specific applications well above the minimum of 50,000 p.s.i., and 50% electrical conductivity. Also, with the alloys of this invention, the electrical conductivity can be held at a fairly high percent while mechanical properties are varied by cold working procedures. Thus, in accordance with this invention, a versatile alloy is obtained whose properties may be varied to yield varied combinations of tensile strength and electrical conductivity.
The importance in the discovery of the critical limits required of the components in the alloy of this invention is evidenced in the versatility and capability of the novel alloy in having its properties of tensile strength and electrical conductivity varied, at will, above the prescribed minimum combined limits of 50,000 p.s.i. tensile strength and 50% electrical conductivity. This versatility of the alloy permits its use in various applications heretofore thought impossible for a single copper alloy. These applications range from use in electrical transmission lines to current carrying contact members in various electrical devices. Although various copper alloys containing iron and phosphorous have been known, the alloy of this invention and the critical limitations thereof have not heretofore been disclosed. Accordingly, as a part of the present invention, it has been determined that in order to obtain the aforesaid versatility and combined high tensile strength and high electrical conductivity, it is critical that the phosphorous be present at or below a maximum of 0.04% together and with iron present in a range of 2.0% to 3.0% by weight.
' In the fabrication of the alloy of this invention, it is preferred to cast the alloy into billets of conventional size, subjecting them to hot working, as by rolling in the conventional size. Although hot working alone has been found to be sufiicient to obtain a solution of the iron and copper in the preferred process, the billet after hot working, may be subjected to a solution anneal to insure that a solution of the iron and copper is complete. The alloy is then precipitation treated by annealing at low temperatures to increase its electrical conductivity. Thereafter, the alloy is cold worked, as by rolling or drawing, to finished size and to increase its tensile strength, during which the electrical conductivity remains relatively constant.
By way of example, a series of castings /2 inch thick were formed of an alloy composed of copper 97.7%, iron 2.2% and phosphorous 0.026% to 0.027%, and rolled at 900 C. to different thicknesses, of 0.05 inch to 0.025 inch gauge, without annealing. It was found that solution annealing although optional, if desired as noted above, is not a necessary treatment if the hot rolling is carried out at a temperature of 900 C.
The rolled bars were then given a precipitation treatment at various temperatures and times, and tests made thereon for tensile strength and electrical conductivity. The results are tabulated in Table 1. Thereafter each bar after the precipitation treatment was then cold rolled to a 50% reduction and tests were again carried out to determine the corresponding tensile strength and conductivity as set forth below in Table 1.
Table 1 Without Reduction With 50% Reduction Precipitation 7 by Cold Rolling Treatment, Bar Temp. C. and
Time in Hrs. Tensile Percent Tensile Percent Strength, Oonduc- Strength, Conducp.s.i. tivity p.s.i. min. tivity 480 at 24 hrs... 50, 400 70. 1 68, 900 67. 9 480 at 24 hrs.-- 50, 700 70. 2 70, 400 66. 8 480 at 40 hrs.-- 49, 000 72. 68, 500 69. 9 480 at 40 hrs.-. 52, 300 71.5 72, 000 69. 3 480 at 48 hrs... 51, 300 73. 5 68, 400 70.2 480 at 48 hrs.-- 51, 000 71. 4 71, 400 68. 4 550 at 8 hrs"-.. 49, 000 62. 4 67, 100 60. 6 550 at 8 hrs.-.- 50, 100 62. 0 70, 800 58. 8 550 at 16 hrs..- 48, 400 63. 4 67, 800 61. 5 550 at 16 hrs... 49,700 63. 8 71, 200 60. 3 550 at; 24 hrs.-- 47, 100 63.8 67, 500 63v 0 550 at 24 hrs.-- 49, 400 64. 5 70, 100 60. 7 600 at 8 hrs. 47, 600 57. 6 67, 200 55. 2 600 at 8 hrs...- 48, 600 56. 4 68, 700 53. 8 600 at 16 hrs.-- 47, 400 56. 4 67,000 54.1 600 at 16 hrs.-- 47, 600 55. 4 68, 300 54. 4 600 at 24 hrs.-. 46, 600 56. 9 66, 400 55. 5 600 at 24 hrs.-- 47, 600 56. 3 69, 100 54.7
As can be seen from the above table, by selection of the temperature at which the alloy is precipitation treated, alone or combined with further cold working, any variation of properties may be imparted into the alloy. As can be further seen, electric conductors prepared in the manner deseeribed above can be obtained having a minimum tensile strength of 50,000 p.s.i. to as high as 71,-
000+ p.s.i. with conductivity well above 50%, with values exceeding The production of electric conductors in accordance with this invention can further be varied as compared with the examples given above. For example, a casting 1 /2 inches thick can be obtained of an alloy composed of 2.3% iron, 0.023% to 0.024% phosphorous and remainder copper, hot rolled to reduce the bar to 0.200 gauge with further cold rolling to obtain a thickness of 0.05 inch. The alloy was then annealed to effect a complete solution of the various elemental components at varying temperatures of 700, 800 and 900 C. The alloy is then cold rolled to further reduce the metal to 0.025 inch in thickness, and precipitation treated at 480 C. for various lengths of time. After precipitation treating, the alloy is then cold rolled to 0.0125 inch in thickness. The results of this last example are shown in FIGURE 1 which correlates the tensile strength of the alloy with the electrical conductivity and the elongation. As can be seen by observation of FIGURE 1, the alloy has after a short period of precipitation treatment has an electrical conductivity exceeding well above 50% with a tensile strength above 65,000.
To further illustrate the versatility of the novel alloy obtained in accordance with this invention, another casting 1 /2 inches thick was formed of an alloy composed essentially of 2.3% iron, 0.024% phosphorous with the remainder essentially copper, heated to 900 C. and hot rolled to a thickness of 0.200 inch. The bar was then cold rolled to a thickness of 0.025 inch. A series of samples were then taken from the bar and annealed at 480 C. for a varying length of time, as indicated in FIGURE 2, and tested for electrical conductivity and tensile strength. The results obtained are illustrated in FIGURE 2, having conductivity extending to above 70% with tensile strength above 50,000 p.s.i.
As is seen, a solution of the components, of the alloy of this invention, can be obtained either by subjecting the alloy to sustained heat above 700 C. or by hot rolling the cast alloy at 900 C. Accordingly, hereinafter and in the claims, the hot Working of the alloy at 900 C. is deemed the equivalent of the annealing operation above 700 C.
The remainder of the annealed samples were then further cold rolled to a thickness of 0.0125 inch and again tested for electrical conductivity and tensile strength with the results illustrated in FIGURE 3.
As can be seen by the above, although optimum properties of combined tensile strength and electrical conductivity can be obtained by a precipitation treatment, low temperature anneal followed by cold working, as by rolling, the cold working operation may be omitted to give combined tensile strength and electrical conductivity above 50,000 p.s.i. and 50% conductivity. By reference to FIGURE 2, graphically illustrating the results obtained by a final operation consisting of a low temperature annealing, a sample annealed for 24 hours at 480 C. can be seen to have a tensile strength of approximately 52,000 p.s.i. and an electrical conductivity of 71%. If a corresponding sample is further cold worked to 0.025 inch in thickness, the sample 'is found to have a 70,000 p.s.i. tensile strength and a 70% electrical conductivity. In like manner, a sample with only a final anneal has a 52,000 p.s.i. tensile Strength and a 69.+% conductivity which upon being subjected to additional cold working is found to have its tensile strength increased to approximately 71,000 p.s.i. with only a slight decrease in electrical conductivity to a value of 67%.
Although in the last described example, the amount of cold working was performed to an extent of 50%, it has also been found that after precipitation treatment by annealing at the desired temperature, approximately 450 to 600 C., the strength of the metal can bealtered to give increased tensile strength while maintaining the electrical conductivity fairly constant.
Although a 50% reduction has been set forth in the examples given above, it is to be understood that the reduction may be varied, with the above specific value of 50% setting the preferred amount of reduction. Further, although rolling has been specifically applied as a means of working the alloy, it is to be understood that it is intended to include other operations which result in altering dimensions in a mass of metal as produced by drawing, extruding or the like.
The low temperature annealing step is essential to obtaining the advantages of high electrical conductivity and tensile strength. It is believed that during the initial high temperature annealing, of approximately 900 C., the iron is completely in solution within the copper. When the alloy is subjected to the low temperature annealing operation, i.e., 480 C., the iron is precipitated from solution to form in the boundaries of the grains of the alloy and during the precipitation it is modified by the presence of the phosphorous to give increased conductivity with corresponding decrease in the strength of the alloy to above 50,000 p.s.i. tensile strength. The alloy may then be fabricated into the shape required for specific applications or may be further strengthened to increase the tensile strength of the metal by conventional cold Working operations.
The specific function of the phosphorous is not understood, however, it is believed that it, both, does alloy with the iron, and does act as a dioxidizer. Irrespective of the function of the phosphorous in the alloy, to obtain a conductor having desirable properties of combined high tensile strength and high electrical conductivity, it is essential that the phosphorous be present from a minute or residual amount to a maximum of 0.04%
Although it is preferable that the alloy consist essentially of iron, phosphorous and copper, it is to be understood that when it is stated that the alloy consists essentially of iron, phosphorous and copper, that small amounts of impurities may be permitted in the alloy, provided such impurities are not present in sufiicient amount to deleteriously alter the conductivity, strength and other desirable properties of the alloy.
Although the invention has been described with reference to specific embodiments, materials and details, various modifications and changes will be apparent to one skilled in the art and are contemplated to be embraced Within the invention.
What is claimed is:
1. A copper-base alloy consisting essentially of 2.1% to 2.6% iron, a trace to a maximum 0.04% phosphorous and balance copper.
2. A copper-base alloy consisting essentially of 2.1% to 2.6% iron, 0.024% to 0.04% phosphorous and remainder copper.
3. A copper-base alloy consisting essentially of 2.3% iron, 0.023% to 0.024% phosphorous and balance copper.
4. A copper-base alloy consisting essentially of 2.3% iron, 0.024% phosphorous and balance copper.
References Cited in the file of this patent UNITED STATES PATENTS 2,027,750 Munson Jan. 14, 1936 2,126,827 Smith Aug. 16, 1938 2,142,671 Hensel et a1 Jan. 3, 1939 FOREIGN PATENTS 915,392 Germany July 8, 1949 OTHER REFERENCES The Journal of the Institute of Metals, November 2, 1924, volume 32, page 338, Table l.
Claims (1)
1. A COPPER-BASE ALLOY CONSISTING ESSENTIALLY OF 2.1% TO 2.6% IRON, A TRACE TO A MAXIMUM 0.04% PHOSPHOROUS AND BALANCE COPPER.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US17311A US3039867A (en) | 1960-03-24 | 1960-03-24 | Copper-base alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US17311A US3039867A (en) | 1960-03-24 | 1960-03-24 | Copper-base alloys |
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| Publication Number | Publication Date |
|---|---|
| US3039867A true US3039867A (en) | 1962-06-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US17311A Expired - Lifetime US3039867A (en) | 1960-03-24 | 1960-03-24 | Copper-base alloys |
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Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3366477A (en) * | 1967-04-17 | 1968-01-30 | Olin Mathieson | Copper base alloys |
| US3522038A (en) * | 1967-06-26 | 1970-07-28 | Olin Corp | Copper base alloy |
| US3522112A (en) * | 1967-06-26 | 1970-07-28 | Olin Corp | Process for treating copper base alloy |
| DE1758122A1 (en) * | 1967-06-26 | 1971-01-14 | Olin Mathieson | Copper alloy and process for its manufacture |
| US3640779A (en) * | 1969-09-30 | 1972-02-08 | Olin Corp | High-conductivity copper alloys |
| DE1758123B1 (en) * | 1967-06-26 | 1972-10-19 | Olin Mathieson | COPPER ALLOY AND PROCESS TO INCREASE THEIR ELECTRICAL CONDUCTIVITY AND STRENGTH |
| DE1758121C (en) | 1967-06-26 | 1973-06-07 | Ohn Mathieson Chemical Corp , New Haven, Conn (V St A ) | Copper alloy and methods of improving the electrical conductivity and strength of this alloy |
| JPS5174925A (en) * | 1974-12-26 | 1976-06-29 | Nippon Musical Instruments Mfg | DOGOKIN |
| JPS5224918A (en) * | 1975-08-22 | 1977-02-24 | Sumitomo Electric Ind Ltd | Process for producing copper alloy containing iron |
| FR2360681A1 (en) * | 1976-08-06 | 1978-03-03 | Kabel Metallwerke Ghh | COPPER ALLOY FOR CASTING SHELLS |
| US4194928A (en) * | 1978-02-21 | 1980-03-25 | Olin Corporation | Corrosion resistant copper base alloys for heat exchanger tube |
| US4605532A (en) * | 1984-08-31 | 1986-08-12 | Olin Corporation | Copper alloys having an improved combination of strength and conductivity |
| US5853505A (en) * | 1997-04-18 | 1998-12-29 | Olin Corporation | Iron modified tin brass |
| US5882442A (en) * | 1995-10-20 | 1999-03-16 | Olin Corporation | Iron modified phosphor-bronze |
| US6132528A (en) * | 1997-04-18 | 2000-10-17 | Olin Corporation | Iron modified tin brass |
| US6632300B2 (en) | 2000-06-26 | 2003-10-14 | Olin Corporation | Copper alloy having improved stress relaxation resistance |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2027750A (en) * | 1934-10-20 | 1936-01-14 | American Brass Co | Copper base alloy |
| US2126827A (en) * | 1936-01-20 | 1938-08-16 | American Brass Co | Copper-cobalt-zinc alloy |
| US2142671A (en) * | 1936-11-09 | 1939-01-03 | Mallory & Co Inc P R | Copper alloy |
| DE915392C (en) * | 1942-05-24 | 1954-07-22 | Dr Carl Schaarwaechter | Copper alloy for studs |
-
1960
- 1960-03-24 US US17311A patent/US3039867A/en not_active Expired - Lifetime
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2027750A (en) * | 1934-10-20 | 1936-01-14 | American Brass Co | Copper base alloy |
| US2126827A (en) * | 1936-01-20 | 1938-08-16 | American Brass Co | Copper-cobalt-zinc alloy |
| US2142671A (en) * | 1936-11-09 | 1939-01-03 | Mallory & Co Inc P R | Copper alloy |
| DE915392C (en) * | 1942-05-24 | 1954-07-22 | Dr Carl Schaarwaechter | Copper alloy for studs |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3366477A (en) * | 1967-04-17 | 1968-01-30 | Olin Mathieson | Copper base alloys |
| JPS549129B1 (en) * | 1967-06-26 | 1979-04-21 | ||
| JPS5514132B1 (en) * | 1967-06-26 | 1980-04-14 | ||
| DE1758122A1 (en) * | 1967-06-26 | 1971-01-14 | Olin Mathieson | Copper alloy and process for its manufacture |
| US3522038A (en) * | 1967-06-26 | 1970-07-28 | Olin Corp | Copper base alloy |
| DE1758123B1 (en) * | 1967-06-26 | 1972-10-19 | Olin Mathieson | COPPER ALLOY AND PROCESS TO INCREASE THEIR ELECTRICAL CONDUCTIVITY AND STRENGTH |
| DE1758121C (en) | 1967-06-26 | 1973-06-07 | Ohn Mathieson Chemical Corp , New Haven, Conn (V St A ) | Copper alloy and methods of improving the electrical conductivity and strength of this alloy |
| JPS5514134B1 (en) * | 1967-06-26 | 1980-04-14 | ||
| JPS5514133B1 (en) * | 1967-06-26 | 1980-04-14 | ||
| US3522112A (en) * | 1967-06-26 | 1970-07-28 | Olin Corp | Process for treating copper base alloy |
| US3640779A (en) * | 1969-09-30 | 1972-02-08 | Olin Corp | High-conductivity copper alloys |
| JPS5174925A (en) * | 1974-12-26 | 1976-06-29 | Nippon Musical Instruments Mfg | DOGOKIN |
| JPS5224918A (en) * | 1975-08-22 | 1977-02-24 | Sumitomo Electric Ind Ltd | Process for producing copper alloy containing iron |
| FR2360681A1 (en) * | 1976-08-06 | 1978-03-03 | Kabel Metallwerke Ghh | COPPER ALLOY FOR CASTING SHELLS |
| US4194928A (en) * | 1978-02-21 | 1980-03-25 | Olin Corporation | Corrosion resistant copper base alloys for heat exchanger tube |
| US4605532A (en) * | 1984-08-31 | 1986-08-12 | Olin Corporation | Copper alloys having an improved combination of strength and conductivity |
| US5882442A (en) * | 1995-10-20 | 1999-03-16 | Olin Corporation | Iron modified phosphor-bronze |
| US5853505A (en) * | 1997-04-18 | 1998-12-29 | Olin Corporation | Iron modified tin brass |
| US6132528A (en) * | 1997-04-18 | 2000-10-17 | Olin Corporation | Iron modified tin brass |
| US6632300B2 (en) | 2000-06-26 | 2003-10-14 | Olin Corporation | Copper alloy having improved stress relaxation resistance |
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