US3816109A - Copper base alloy - Google Patents

Copper base alloy Download PDF

Info

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
Application number
US00268485A
Other languages
English (en)
Inventor
J Crane
S Friedman
M Pryor
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Olin Corp
Original Assignee
Olin Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Olin Corp filed Critical Olin Corp
Priority to US00268485A priority Critical patent/US3816109A/en
Priority to CA169,996A priority patent/CA985069A/en
Priority to AU55178/73A priority patent/AU473155B2/en
Priority to GB2234173A priority patent/GB1399195A/en
Priority to IT49966/73A priority patent/IT985043B/it
Priority to BR4845/73A priority patent/BR7304845D0/pt
Priority to SE7309321A priority patent/SE397369B/xx
Priority to JP7467273A priority patent/JPS5314489B2/ja
Priority to DE2366062A priority patent/DE2366062B2/de
Priority to BE133064A priority patent/BE801845A/xx
Priority to DE2333820A priority patent/DE2333820C3/de
Priority to FR7324467A priority patent/FR2236954B1/fr
Priority to US00399073A priority patent/US3852121A/en
Application granted granted Critical
Publication of US3816109A publication Critical patent/US3816109A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/04Alloys 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)
US00268485A 1972-07-03 1972-07-03 Copper base alloy Expired - Lifetime US3816109A (en)

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)

Country Link
US (1) US3816109A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPS5314489B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
AU (1) AU473155B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
BE (1) BE801845A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
BR (1) BR7304845D0 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CA (1) CA985069A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (2) DE2366062B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2236954B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB1399195A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IT (1) IT985043B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
SE (1) SE397369B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Cited By (3)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (6)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
EP0175183B1 (en) Copper alloys having an improved combination of strength and conductivity
US4559200A (en) High strength and high conductivity copper alloy
KR100349934B1 (ko) 구리 합금과 그의 제조방법
US3923558A (en) Copper base alloy
JP2002180165A (ja) プレス打ち抜き性に優れた銅基合金およびその製造方法
US5024814A (en) Copper alloy having excellent hot rollability and excellent adhesion strength of plated surface thereof when heated
US5508001A (en) Copper based alloy for electrical and electronic parts excellent in hot workability and blankability
US3364016A (en) Copper alloys for springs
JP3413864B2 (ja) Cu合金製電気電子機器用コネクタ
DE3908513C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP2521880B2 (ja) 電子電気機器用銅合金とその製造法
CN111118336A (zh) 一种耐腐蚀高弹性铜合金插套材料及制备方法
US2445868A (en) Copper base alloys
US3816109A (en) Copper base alloy
JPH1143731A (ja) スタンピング加工性及び銀めっき性に優れる高力銅合金
JPS62182240A (ja) 導電性高力銅合金
JPS63307232A (ja) 銅合金
JPH0718355A (ja) 電子機器用銅合金およびその製造方法
US3852121A (en) Process for making a novel copper base alloy
JPH01165733A (ja) 高強度高導電性銅合金
JPH0469217B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JPS62185847A (ja) 熱・電気高伝導用高力銅合金とその製造法
KR20120097748A (ko) 고전기전도도 및 고강도 Cu-Cr-Mg-P-Zr 합금 및 그 제조방법
US3150969A (en) Beryllium-bronze alloy
JPS5989743A (ja) 高強度高導電性電線用銅合金