US3816109A - Copper base alloy - Google Patents
Copper base alloy Download PDFInfo
- Publication number
- US3816109A US3816109A US00268485A US26848572A US3816109A US 3816109 A US3816109 A US 3816109A US 00268485 A US00268485 A US 00268485A US 26848572 A US26848572 A US 26848572A US 3816109 A US3816109 A US 3816109A
- Authority
- US
- United States
- Prior art keywords
- percent
- alloy
- cobalt
- copper base
- 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
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 77
- 239000000956 alloy Substances 0.000 title claims abstract description 77
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 title claims abstract description 29
- 229910052802 copper Inorganic materials 0.000 title claims abstract description 29
- 239000010949 copper Substances 0.000 title claims abstract description 29
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 56
- 229910017052 cobalt Inorganic materials 0.000 claims abstract description 33
- 239000010941 cobalt Substances 0.000 claims abstract description 33
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract description 32
- 229910052742 iron Inorganic materials 0.000 claims abstract description 28
- 239000011701 zinc Substances 0.000 claims abstract description 19
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 18
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 18
- 238000005260 corrosion Methods 0.000 claims description 7
- 230000007797 corrosion Effects 0.000 claims description 7
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 5
- 229910052698 phosphorus Inorganic materials 0.000 claims description 5
- 239000011574 phosphorus Substances 0.000 claims description 5
- 238000005299 abrasion Methods 0.000 claims description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 abstract description 13
- 241001275902 Parabramis pekinensis Species 0.000 abstract description 10
- 238000005266 casting Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 238000000137 annealing Methods 0.000 description 4
- 238000005097 cold rolling Methods 0.000 description 4
- 239000012535 impurity Substances 0.000 description 3
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 2
- 229910001297 Zn alloy Inorganic materials 0.000 description 2
- 230000002411 adverse Effects 0.000 description 2
- 229910021529 ammonia Inorganic materials 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 229910000967 As alloy Inorganic materials 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- UREBDLICKHMUKA-CXSFZGCWSA-N dexamethasone Chemical compound C1CC2=CC(=O)C=C[C@]2(C)[C@]2(F)[C@@H]1[C@@H]1C[C@@H](C)[C@@](C(=O)CO)(O)[C@@]1(C)C[C@@H]2O UREBDLICKHMUKA-CXSFZGCWSA-N 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 230000002195 synergetic effect Effects 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
- C22C9/04—Alloys based on copper with zinc as the next major constituent
Definitions
- ABSTRACT A copper base alloy having a combination of strength and electrical conductivity which make it a suitable replacement for the C.D.A. 400 series tin brasses.
- the alloy contains from about 0.5 to about 2.8 percent iron and, preferably, from about 1.0 to about 2.0 percent iron; from about 0.2 to about 2.0 percent cobalt and, preferably, from about 0.3 to about 1.0% cobalt; from about 5 to about 15 percent zinc and, preferably, from about 7 to about 13 percent zinc; provided that the sum of the iron plus cobalt should be from about 0.8 to about 3.0 percent and, preferably, from about 1.5 to about 2.5 percent.
- Tin brasses namely, the C.D.A. 400 series alloys are commonly used for this type of application since they combine the above described properties.
- the electrical conductivity of these 400 series alloys range from 28 percent IACS for C.D.A. Alloy 425 which is the strongest of the series to 41 percent IACS for C.D.A. Alloy 405 which possesses the lowest strength of the series.
- Various of these alloys particularly those containing higher tin concentrations are difficult to manufacture, particularly with regard to casting and hot rollability.
- a copper base alloy containing from about 0.5 to about 2.8 percent iron and, preferably, from about 1.0 to about 2.0 percentiron; from about 0.2 to about 2.0 percent cobalt and, preferably, from about 0.3 to about 1.0 percent cobalt; from about 5 to about percent zinc and, preferably, from about 7 to about 13 percent zinc; provided that the sum of the iron plus cobalt should be from about 0.8 to about 3.0 percent, and, preferably, from about 1.5 to about 2.5 percent.
- novel alloys provide electrical conductivity that is superior to those of the 400 series tin brasses at a comparable strength to limiting bend radius ratio; or at comparable conductivity, they provide superior strength to limiting bend radius ratio.
- copper base alloys are provided having an electrical conductivity that is superior to that of the tin brasses at a comparable strength or at comparable conductivity, they provide superior strength.
- the copper base alloys in accordance with this invention contain about 0.5 to about 2.8 percent iron, about 0.2 to about 2.0 percent cobalt, about 5 to about 15 percent zinc, balance copper, provided that the sum of the iron plus cobalt contents is from about 0.8 to about 3.0 percent.
- the alloys in'accordance with this invention consist essentially of about 1.0 to about 2.0 percent iron, about 0.3 to about 1.0 percent cobalt,
- Impurities at the following levels separately or in combination cause no deleterious effect on the casting or hot and cold rolling characteristics of the alloy of this invention: phosphorus less than about 0.03 percent, lead less than about-0.03 percent, tin less than about 0.05 percent, nickel less than about 0.05 percent, manganese less than about 0.10 percent, aluminum less than about 0.10 percent, silver less than about 0.05 percent and silicon less than about 0.10 percent. It is preferred that the maximum. total impurities be limited to less than 0.2 percent to minimize adverse affects on the properties of the alloys.
- the preferred limit for iron plus cobalt was established at 2.5 percent.
- the minimum limit for the sum of the iron and cobalt contents is the amount necessary to achieve desirable mechanical properties.
- the maximum zinc content was established on the basis of stress corrosion resistance.
- the minimum zinc content is based on the necessity to achieve desired mechanical properties.
- the phosphorus content should be minimized and preferably should not exceed 0.02 percent.
- alloys in accordance with this invention may be prepared in accordance with the following practice.
- Melting and Casting Melt the copper, add the iron and cobalt, heat to 1,300C, and hold until the iron and cobalt are thoroughly dissolved, reduce the temperature to 1,200C and add the zinc. Cast at a temperature high enough to assure minimum mold temperature of l,lC. Other casting parameters are in accordance with conventional practice in the art.
- Hot Rolling Soak at a temperature of about 915 to about 975C; soak time and pass schedule may be set as desired; last pass temperature preferably should be above 500C.
- the alloys of this invention have better than 75 percent cold rollability after hot rolling above 500C or after interannealing. A minimum of 50 percent cold reduction prior to annealing is preferred.
- Annealing for softening can be performed either by bell annealing or strip annealing.
- the choice of bell annealing versus strip annealing is predicated upon desired electrical conductivity. Where maximum conductivity is required, bell annealing is preferred.
- 1t is preferred in accordance with this invention in order to maintain the improved strength in the annealed and cold worked conditions that interanneals and the final anneal during the cold working be carried out in the range of 400 to 600C.
- the alloy may be cleaned by conventional procedures and it has been found that standard sulfuric acid cleaning is acceptable.
- the alloy in accordance with this invention may be readily fabri- Cated without the difficulty encountered with the tin brasses. Further, the alloy is readily joinable by soldering and it should tin, nickel or chrome plate as well as tin brasses.
- the alloyv shows unusually good wear resistance as compared to C.D.A. Alloy 411 as well as C.D.A. Alloy 425. This may make it suitable for bearing applications for which Alloy 41 l is now used.
- ALLOYS Composition in wt.%
- ALLOYS Composition in wt./r
- Alloys A, B and C representing the alloys of the invention were processed by melting at 1,300C and Durville casting at a temperature of 1,175C; hot rolling from a thickness of 1% inches to approximately 0.5 inch at a starting temperature of 950C and a finishing temperature of about 600C; surface milling to produce a clean surface; cold rolling to 0.080 inch gage for Alloys A and B and 0.060 inch for Alloy C; annealing at 500C for hours for Alloys A and B and at 500C for 16 hours for Alloy C; then cold rolling to various reductions.
- novel alloys in accordance with this invention provide superior electrical conductivity to those of the 400 series tin brasses at comparable strength to limiting bend radius ratio; or at a comparable conductivity, they provide superior strength to limiting bend radius ratio.
- Alloy 405, Alloy D, while attaining a higher conductiv- EXAMPLE 11 A series of alloys in accordance with this invention were prepared in a manner similar to that set forth in Example I, The compositions of the alloys so prepared were as follows.
- ALLOYS Composition in wt.
- Table 111 The tensile and yield strengths and electrical conductivity in the annealed condition are presented in Table 111 below. Table 111 further gives these strengths of the alloys after cold rolling 30 and 50 percent from the 0.080 inch gage.
- the data further establish that the alloys of this invention can obtain in the annealed condition an ultimate tensile strength of at least 60 ksi and, preferably, at least 62 ksi and an electrical conductivity of at least 33 percent IACS. Further, in the 30 percent annealed and cold rolled condition the alloys. can obtain a tensile strength of at least 86 ksi and in the annealed and cold rolled 50 percent condition, they can obtain a tensile strength of at least 93 ksi.
- alloys of this invention have particular application in structural electrical components such as electrical contacts, electrical receptacles, electrical connectors and the like.
- a copper base alloy consisting essentially of about 0.5 to about 2.8 percent iron, about 0.2 to about 2.0 percent cobalt, about 5 to about 15 percent zinc, and the balance copper, provided that the sum of the iron plus cobalt contents shall be from about 0.8 to about 3.0 percent.
- a copper base alloy as in claim 1 consisting essentially of about 1.0 to about 2.0 percent iron, about 0.3 to about 1.0 percent cobalt, about 7 to about 13 percent zinc, and the balance copper, provided that the sum of the iron plus cobalt contents shall be from about 1.5 to about 2.5 percent.
- a copper base alloy as in claim 2 containing less than 0.03 percent phosphorus.
- a copper base alloy as in claim 4 which is abrasion and stress corrosion resistant and which has an ultimate tensile strength of at least 60 ksi and an electrical conductivity of at least 33 percent IACS.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Conductive Materials (AREA)
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
- Contacts (AREA)
Priority Applications (13)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00268485A US3816109A (en) | 1972-07-03 | 1972-07-03 | Copper base alloy |
CA169,996A CA985069A (en) | 1972-07-03 | 1973-04-27 | Copper base alloy |
AU55178/73A AU473155B2 (en) | 1972-07-03 | 1973-05-03 | Copper base alloy |
GB2234173A GB1399195A (en) | 1972-07-03 | 1973-05-10 | Copper base alloy |
IT49966/73A IT985043B (it) | 1972-07-03 | 1973-05-15 | Lega a base di rame |
BR4845/73A BR7304845D0 (pt) | 1972-07-03 | 1973-06-29 | Edades de resistencia de ligas a base de cobre liga a base de cobre e processo para aperfeicoar as propr |
SE7309321A SE397369B (sv) | 1972-07-03 | 1973-07-02 | Kopparlegering i synnerhet i form av ett elektriskt kontaktorgan |
JP7467273A JPS5314489B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1972-07-03 | 1973-07-02 | |
DE2366062A DE2366062B2 (de) | 1972-07-03 | 1973-07-03 | Verfahren zur Verbesserung der Eigenschaften von Kupfer-Eisen-Kobalt-Zink-Legierungen |
BE133064A BE801845A (fr) | 1972-07-03 | 1973-07-03 | Alliages a base de cuivre |
DE2333820A DE2333820C3 (de) | 1972-07-03 | 1973-07-03 | Verwendung einer Kupfer-Zink-Eisen-Kobalt-Legierung |
FR7324467A FR2236954B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1972-07-03 | 1973-07-03 | |
US00399073A US3852121A (en) | 1972-07-03 | 1973-09-20 | Process for making a novel copper base alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00268485A US3816109A (en) | 1972-07-03 | 1972-07-03 | Copper base alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US3816109A true US3816109A (en) | 1974-06-11 |
Family
ID=23023216
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00268485A Expired - Lifetime US3816109A (en) | 1972-07-03 | 1972-07-03 | Copper base alloy |
Country Status (11)
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4259124A (en) * | 1978-06-28 | 1981-03-31 | Olin Corporation | Modified brass alloys with improved stress relaxation resistance |
DE102012002450A1 (de) | 2011-08-13 | 2013-02-14 | Wieland-Werke Ag | Verwendung einer Kupferlegierung |
WO2013023717A2 (de) | 2011-08-13 | 2013-02-21 | Wieland-Werke Ag | Kupferlegierung |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5924170B2 (ja) | 1977-11-10 | 1984-06-07 | 秀夫 金子 | 放電加工用ワイヤ電極用合金 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1723922A (en) * | 1926-04-13 | 1929-08-06 | Electro Metallurg Co | Copper cobalt alloy |
US1959509A (en) * | 1930-06-14 | 1934-05-22 | Lucius Pitkin Inc | Copper base alloy |
US2126827A (en) * | 1936-01-20 | 1938-08-16 | American Brass Co | Copper-cobalt-zinc alloy |
US2147844A (en) * | 1937-06-19 | 1939-02-21 | Westinghouse Electric & Mfg Co | Copper base alloy |
US2169188A (en) * | 1938-10-21 | 1939-08-08 | Westinghouse Electric & Mfg Co | Copper base alloy |
US2295180A (en) * | 1940-05-20 | 1942-09-08 | Western Cartridge Co | Copper alloy |
-
1972
- 1972-07-03 US US00268485A patent/US3816109A/en not_active Expired - Lifetime
-
1973
- 1973-04-27 CA CA169,996A patent/CA985069A/en not_active Expired
- 1973-05-03 AU AU55178/73A patent/AU473155B2/en not_active Expired
- 1973-05-10 GB GB2234173A patent/GB1399195A/en not_active Expired
- 1973-05-15 IT IT49966/73A patent/IT985043B/it active
- 1973-06-29 BR BR4845/73A patent/BR7304845D0/pt unknown
- 1973-07-02 SE SE7309321A patent/SE397369B/xx unknown
- 1973-07-02 JP JP7467273A patent/JPS5314489B2/ja not_active Expired
- 1973-07-03 DE DE2366062A patent/DE2366062B2/de not_active Ceased
- 1973-07-03 DE DE2333820A patent/DE2333820C3/de not_active Expired
- 1973-07-03 FR FR7324467A patent/FR2236954B1/fr not_active Expired
- 1973-07-03 BE BE133064A patent/BE801845A/xx not_active IP Right Cessation
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1723922A (en) * | 1926-04-13 | 1929-08-06 | Electro Metallurg Co | Copper cobalt alloy |
US1959509A (en) * | 1930-06-14 | 1934-05-22 | Lucius Pitkin Inc | Copper base alloy |
US2126827A (en) * | 1936-01-20 | 1938-08-16 | American Brass Co | Copper-cobalt-zinc alloy |
US2147844A (en) * | 1937-06-19 | 1939-02-21 | Westinghouse Electric & Mfg Co | Copper base alloy |
US2169188A (en) * | 1938-10-21 | 1939-08-08 | Westinghouse Electric & Mfg Co | Copper base alloy |
US2295180A (en) * | 1940-05-20 | 1942-09-08 | Western Cartridge Co | Copper alloy |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4259124A (en) * | 1978-06-28 | 1981-03-31 | Olin Corporation | Modified brass alloys with improved stress relaxation resistance |
DE102012002450A1 (de) | 2011-08-13 | 2013-02-14 | Wieland-Werke Ag | Verwendung einer Kupferlegierung |
WO2013023717A2 (de) | 2011-08-13 | 2013-02-21 | Wieland-Werke Ag | Kupferlegierung |
US9493858B2 (en) | 2011-08-13 | 2016-11-15 | Wieland-Werke Ag | Copper alloy |
US9702027B2 (en) | 2011-08-13 | 2017-07-11 | Wieland-Werke Ag | Copper alloy |
Also Published As
Publication number | Publication date |
---|---|
DE2333820C3 (de) | 1978-05-03 |
DE2366062A1 (de) | 1977-07-28 |
DE2333820A1 (de) | 1974-01-17 |
BR7304845D0 (pt) | 1974-08-15 |
JPS4956819A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1974-06-03 |
AU5517873A (en) | 1974-11-07 |
FR2236954B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1976-06-18 |
DE2333820B2 (de) | 1977-09-08 |
FR2236954A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1975-02-07 |
JPS5314489B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1978-05-18 |
CA985069A (en) | 1976-03-09 |
AU473155B2 (en) | 1976-06-17 |
DE2366062B2 (de) | 1980-03-06 |
SE397369B (sv) | 1977-10-31 |
GB1399195A (en) | 1975-06-25 |
IT985043B (it) | 1974-11-30 |
BE801845A (fr) | 1974-01-03 |
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